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| issue date = 07/24/2015
| issue date = 07/24/2015
| title = Purdue University - Request for Additional Information Regarding the Purdue University Reactor License Renewal Application (TAC No. ME1594), Responses to Letter Dated August 29, 2014 (ML14115A221). Part 5 of 5
| title = Purdue University - Request for Additional Information Regarding the Purdue University Reactor License Renewal Application (TAC No. ME1594), Responses to Letter Dated August 29, 2014 (ML14115A221). Part 5 of 5
| author name = Bean R S
| author name = Bean R
| author affiliation = Purdue Univ
| author affiliation = Purdue Univ
| addressee name = Montgomery C K
| addressee name = Montgomery C
| addressee affiliation = NRC/NRR
| addressee affiliation = NRC/NRR
| docket = 05000182
| docket = 05000182
Line 15: Line 15:
| page count = 101
| page count = 101
| project = TAC:ME1594
| project = TAC:ME1594
| stage = RAI
| stage = Request
}}
}}


=Text=
=Text=
{{#Wiki_filter:APPENDIX 2: NATCON INFORMATION Hot Channel Factors in the NATCON Code Version 1.0The NATOON code version 1.0 [Ref. ANL/RERTR/TM-12]
{{#Wiki_filter:APPENDIX 2: NATCON INFORMATION Hot Channel Factors in the NATCON Code Version 1.0 The NATOON code version 1.0 [Ref. ANL/RERTR/TM-12] uses three hot channel factors (FQ, FW, FH). Using the source code and documentation, the factor FH used in NATCON is found to be the same as the factor FNUSLT used by E. E. Feldman. Table 1 shows the tolerances and uncertainties included in each of the six hot channel factors used by E. E. Feldman. The correspondence between the NATCON hot channel factors and E. E. Feldman's six hot channel factors is as follows.
uses three hot channel factors (FQ,FW, FH). Using the source code and documentation, the factor FH used in NATCON is found tobe the same as the factor FNUSLT used by E. E. Feldman.
Feldman's Hot Channel FactorNC                                                   CNInu Variable System-wide Factors:
Table 1 shows the tolerances anduncertainties included in each of the six hot channel factors used by E. E. Feldman.
FFLOW         a factor to account for the uncertainty in total reactor  FW (approximately) flow FPOWER        a factor to account for the uncertainty in total reactor          FQ power FNUSLT        a factor to account for the uncertainty in Nu number              FH correlation Local Factors:
Thecorrespondence between the NATCON hot channel factors and E. E. Feldman's six hot channelfactors is as follows.Feldman's Hot Channel FactorNC CNInuVariableSystem-wide Factors:FFLOW a factor to account for the uncertainty in total reactorflowFPOWER a factor to account for the uncertainty in total reactorpowerFNUSLT a factor to account for the uncertainty in Nu numbercorrelation FW (approximately)
FBULK         a   hot channel factor     for local bulk   coolant  FBULK (new input) temperature rise FFILM        a hot channel factor for local temperature rise across FFILM (new input) the coolant film FFLUX        a hot channel factor for local heat flux from cladding    FFLUX (new input) surface Hot Channel Factors in the NATCON Code Version 2.0 PUR-1 SAR                                    Appendix 2-1                        PUR-SARAppndix2-1Rev 2, July 23, 2015
FQFHLocal Factors:FBULK a hot channel factor for local bulk coolanttemperature riseFFILM a hot channel factor for local temperature rise acrossthe coolant filmFFLUX a hot channel factor for local heat flux from claddingsurfaceFBULK (new input)FFILM (new input)FFLUX (new input)Hot Channel Factors in the NATCON Code Version 2.0PUR-1 SARAppendix 2-1PUR- SARAppndix2-1Rev 2, July 23, 2015 Sections 2.1 and 2.2 develop, for laminar natural convection, two thermal-hydraulic relationships that are used in section 2.3 to obtain formulas for the hot channel factors from user-supplied manufacturing tolerances and measurement uncertainties.
 
The results of section 2.3 aresummarized here for convenience.
Sections 2.1 and 2.2 develop, for laminar natural convection, two thermal-hydraulic relationships that are used in section 2.3 to obtain formulas for the hot channel factors from user-supplied manufacturing tolerances and measurement uncertainties. The results of section 2.3 are summarized here for convenience. The first three are local/random hot channel factors, and the last three are system-wide. An example of the use of these hot channel factors is given in section 4, with NATCON running instructions in section 3, and the new input description in section 5.
The first three are local/random hot channel factors, and thelast three are system-wide.
FBULK- 1 +j{(1+ u)2a+(1+ u 2 )2+-r-:U1           2--*      +u62 FBULK is higher (conservative) if the temperature dependence of water viscosity is ignored.
An example of the use of these hot channel factors is given insection 4, with NATCON running instructions in section 3, and the new input description insection 5.FBULK- 1 +j{(1 + u)2a+ (1+ u2)2+-r-:U1 +u62FBULK is higher (conservative) if the temperature dependence of water viscosity is ignored.FFILM = 11u12+/-+u22+/-+u32 +u42+/-+u52FFLUX -- 12 +u22+/-+u32 +u4FQ = 1 +u-FW = 1 + u8FH = 1 +- u9whereul= Fractional uncertainty in neiitronics calculation of power in a plateu2= Fractional uncertainty in U-235 mass per plate =Am/_Mu3 Fractional uncertainty in local (at an axial position) fuel meat thickness u4= Fractional uncertainty in U-235 local (at an axial position) homogeneity u5 = Fractional uncertainty in coolant channel thickness  
FFILM = 11u    1 2+/-+u  2 2+/-+u 3 2 +u4 2+/-+u 5 2 FFLUX -- l*u        2 +u 2 +/-+u2  +u4 1    2    3 FQ  = 1 +u-FW = 1 + u8 FH  = 1 +- u9 where ul= Fractional uncertainty in neiitronics calculation of power in a plate u2= Fractional uncertainty in U-235 mass per plate =Am/_M u3    Fractional uncertainty in local (at an axial position) fuel meat thickness u4= Fractional uncertainty in U-235 local (at an axial position) homogeneity u5     = Fractional uncertainty in coolant channel thickness     = (tnc - thc) / tn u6    = Fractional uncertainty in flow distribution among channels u7= Fractional uncertainty in reactor power measurement u8= Fractional uncertainty in flow due to uncertainty in friction factor Ug    = Fractional uncertainty in convective heat transfer coefficient, or in the Nu number correlation M     = Nominal mass of U-235 per plate, gram Am    = Tolerance allowed in U-235 mass per plate, gram PUR-1 SAR                                    Appendix 2-2                              PUR-SARAppndix2-2Rev 2, July 23, 2015
= (tnc -thc) / tnu6  = Fractional uncertainty in flow distribution among channelsu7= Fractional uncertainty in reactor power measurement u8= Fractional uncertainty in flow due to uncertainty in friction factorUg = Fractional uncertainty in convective heat transfer coefficient, or in the Nu numbercorrelation M = Nominal mass of U-235 per plate, gramAm = Tolerance allowed in U-235 mass per plate, gramPUR-1 SARAppendix 2-2PUR- SARAppndix2-2Rev 2, July 23, 2015 The code obtains, for an input nominal reactor power CPWR, a thermal-hydraulic solution usingthe three systematic hot channel factors FW, EQ and FH. If the user-input reactor power is zero,then the code itself chooses the nominal power from a series of power levels (10 kW, 100 kW,200 kW, and so on increasing in steps of 100 kW). This thermal-hydraulic calculation is done fora hot plate power of CPWR*FQ*(Radial power peaking factor RPEAK)/(Total number of fuelplates in standard and control assemblies).
 
Also, the frictional resistance to flow is multiplied byFW2, and the convective heat transfer coefficient found for laminar flow in a rectangular channelis divided by FH. The random hot channel factors FBULK, FFILM and FFLUX are not used inthis solution.
The code obtains, for an input nominal reactor power CPWR, a thermal-hydraulic solution using the three systematic hot channel factors FW, EQ and FH. If the user-input reactor power is zero, then the code itself chooses the nominal power from a series of power levels (10 kW, 100 kW, 200 kW, and so on increasing in steps of 100 kW). This thermal-hydraulic calculation is done for a hot plate power of CPWR*FQ*(Radial power peaking factor RPEAK)/(Total number of fuel plates in standard and control assemblies). Also, the frictional resistance to flow is multiplied by FW 2 , and the convective heat transfer coefficient found for laminar flow in a rectangular channel is divided by FH. The random hot channel factors FBULK, FFILM and FFLUX are not used in this solution.
Having obtained the above solution, the random hot channel factors FBULK, FFILM and FFLUXare applied to the temperatures  
Having obtained the above solution, the random hot channel factors FBULK, FFILM and FFLUX are applied to the temperatures obtained, using the following equations. The temperatures calculated with all six hot channel factors are printed after the above solution. The onset of nucleate boiling ratio, ONBR, is computed using the temperatures with all six hot channel factors applied (using the equation below). If the user-input nominal power is zero, then the last nominal power for which the code prints a solution is that at which the ONBR is 1.0.
: obtained, using the following equations.
Ti,6hcf       = To + (Ti- To)*FBULK Twalj,i,6hcf = Ti,6hcf + (TwaiiUi- Ti)*FFILM Tmax,j,6hcf = TwaII,i,6hcf + (Tmax~i - TwaIlU)*FFLUX where To        = Bulk water temperature at the coolant channel inlet, i.e., the pool temperature, T*        = Bulk water temperature in node i of the channel with only systematic hot channel factors applied, 00 Twai,i             Cladding surface temperature in node i with only systematic hot channel factors applied, °C Tmax,i           =Fuel     meat centerline temperature in node i with only systematic hot channel factors applied, °C TI,6hof         = Bulk water temperature in node i of the channel with all six hot channel factors,
The temperatures calculated with all six hot channel factors are printed after the above solution.
                          °C TwaII,i,6hcf     = Cladding surface temperature in node i with all six hot channel factors,   0C Tmax,i,6hcf     = Fuel meat centerline temperature in node i with all six hot channel factors, C T~o,           = Incipient boiling temperature in node i with only systematic hot channel factors applied, C PUR-1 SAR                                          Appendix 2-3                      PuR-SARAppndix2-3Rev 2, July 23, 2015
The onset ofnucleate boiling ratio, ONBR, is computed using the temperatures with all six hot channelfactors applied (using the equation below). If the user-input nominal power is zero, then the lastnominal power for which the code prints a solution is that at which the ONBR is 1.0.Ti,6hcf = To + (Ti- To)*FBULK Twalj,i,6hcf  
 
= Ti,6hcf + (TwaiiUi-Ti)*FFILM Tmax,j,6hcf  
Flow Rate in a Coolant Channel versus Power of a Fuel Plate NATCON is a laminar natural circulation code. The flow rate is calculated in the code by balancing the buoyancy pressure force to the laminar friction pressure drop. Following this concept, an analytical relationship is developed here (with some approximation) for the coolant flow rate in a single coolant channel in terms of the power generated in a fuel plate and the channel geometrical dimensions. The analytical relationship is needed for obtaining hot channel factors.
= TwaII,i,6hcf  
The hot channel factor FW used in the code to account for the uncertainty in coolant flow rate is actually applied to the laminar friction factor in the code, that is, the laminar friction factor is multiplied by FW 2. It is not applied directly to the flow rate. The relationship developed here explains how this technique works.
+ (Tmax~i -TwaIlU)*FFLUX whereTo = Bulk water temperature at the coolant channel inlet, i.e., the pool temperature,= Bulk water temperature in node i of the channel with only systematic hotchannel factors applied, 00Twai,i Cladding surface temperature in node i with only systematic hot channel factorsapplied,  
p1 , T1 at channel outlet IL  = Channel height containing hot coolant (hotter than pool), m IP  =   Power in a single fuel plate or the two half plates, W IW=Upward       flow rate in a single channel, kg/s po, To at channel inlet Schematic of what the code analyses, that is, a single rectangular coolant channel heated by a half of a fuel plate on each side (right and left sides).
°CTmax,i =Fuel meat centerline temperature in node i with only systematic hot channelfactors applied,  
The above schematic shows what the code analyses, that is, a single rectangular coolant channel heated by a half of a fuel plate on each side (right and left sides). See Fig. 1 for details.
°CTI,6hof = Bulk water temperature in node i of the channel with all six hot channel factors,°CTwaII,i,6hcf  
The buoyancy pressure force is caused by the decrease in water density due to heating in the channel. The temperature dependence of water density can be written as
= Cladding surface temperature in node i with all six hot channel factors, 0CTmax,i,6hcf  
,p(T)=po       - ,p0 ,8 (T -To )                                                                 (I) where T1= Bulk water temperature at channel outlet, C AT    =   T1 - To = Temperature rise in channel from inlet to outlet, C PUR-1 SAR                                        Appendix 2-4                    PUR-SARAppndix2-4Rev 2, July 23, 2015
= Fuel meat centerline temperature in node i with all six hot channel factors, CT~o, = Incipient boiling temperature in node i with only systematic hot channel factorsapplied, CPUR-1 SARAppendix 2-3PuR- SARAppndix2-3Rev 2, July 23, 2015 Flow Rate in a Coolant Channel versus Power of a Fuel PlateNATCON is a laminar natural circulation code. The flow rate is calculated in the code bybalancing the buoyancy pressure force to the laminar friction pressure drop. Following thisconcept, an analytical relationship is developed here (with some approximation) for the coolantflow rate in a single coolant channel in terms of the power generated in a fuel plate and thechannel geometrical dimensions.
 
The analytical relationship is needed for obtaining hot channelfactors.The hot channel factor FW used in the code to account for the uncertainty in coolant flow rate isactually applied to the laminar friction factor in the code, that is, the laminar friction factor ismultiplied by FW2.It is not applied directly to the flow rate. The relationship developed hereexplains how this technique works.p1 , T1 at channel outletIL = Channel height containing hot coolant (hotter than pool), mIP = Power in a single fuel plate or the two half plates, WIW=Upward flow rate in a single channel, kg/spo, To at channel inletSchematic of what the code analyses, that is, a single rectangular coolant channel heated by ahalf of a fuel plate on each side (right and left sides).The above schematic shows what the code analyses, that is, a single rectangular coolantchannel heated by a half of a fuel plate on each side (right and left sides). See Fig. 1 for details.The buoyancy pressure force is caused by the decrease in water density due to heating in thechannel.
p0   = Water density at channel inlet, i.e., the water density in the pool, kg/rn 3 I?   = Volumetric expansion coefficient of water, per C
The temperature dependence of water density can be written as,p(T) =po -,p0,8 (T -To )(I)whereT1= Bulk water temperature at channel outlet, CAT = T1-To = Temperature rise in channel from inlet to outlet, CPUR-1 SARAppendix 2-4PUR- SARAppndix2-4Rev 2, July 23, 2015 p0 = Water density at channel inlet, i.e., the water density in the pool, kg/rn3I? = Volumetric expansion coefficient of water, per C,p = Average coolant density in the channel, kg/rn3L= Channel height that contains hotter coolant (hotter than pool), m. It is the sum ofheat generating length of fuel plate, non-heat generating fuel plate length at top,and the assembly duct length above the top of fuel plateg = Acceleration due to gravity, 9.8 m/s2The buoyancy pressure force is given byBuoyancyAp
      ,p   = Average coolant density in the channel, kg/rn 3 L= Channel height that contains hotter coolant (hotter than pool), m. It is the sum of heat generating length of fuel plate, non-heat generating fuel plate length at top, and the assembly duct length above the top of fuel plate g    = Acceleration due to gravity, 9.8 m/s 2 The buoyancy pressure force is given by BuoyancyAp        =(po -p)gL                                                                             (2)
=(po -p)gL (2)The average coolant density p is given byp =O0.5 (po+p,) = p0 -0.5,po /J(T1 -To )= p0 -0.5,O p0 fAT (3)Buoyancy Ap = 0.5 p0 ,/1 AT g L (4)The coolant temperature rise AT can be written in terms of the input power P generated in afuel plate, as shown by Eq. (5) below, and then the buoyancy A p of Eq. (4) can be written interms of the input power P, as shown by Eq. (6).AT = P/ (W Cp) (5)_ o0/gLPBuoyancyAp
The average coolant density p is given by p =O0.5 (po+p,) = p0 -0.5,po /J(T 1-To )= p 0 - 0.5,Op0 fAT                                             (3)
-WC(6)Ignoring the minor losses at channel inlet and outlet, the laminar frictional pressure drop in thechannel is written below as Eq. (9) after using the laminar friction factor given by Eq. (7), andafter replacing the coolant velOcity by mass flow rate using Eq. (8). The parameter C in Eq. (7)is a constant for a given channel cross section, but it depends upon the channel cross sectionaspect ratio width/thickness, and varies from 57 for aspect ratio 1.0 (square channel) to 96 foran infinite aspect ratio (infinitely wide channel).
Buoyancy Ap       = 0.5 p 0 ,/1 AT g L                                                                   (4)
f =C /Re (7)W= pAV (8)PUR-1 SARAppendix 2-5PUR- SARAppndix2-5Rev 2, July 23, 2015 Fritioal
The coolant temperature rise AT can be written in terms of the input power P generated in a fuel plate, as shown by Eq. (5) below, and then the buoyancy A p of Eq. (4) can be written in terms of the input power P, as shown by Eq. (6).
_ p 2 = C4ULcW(9Fritioal P 2D 2 p AD2  9wheref -Moody friction factor for laminar flow in the channelRe -Reynolds number in the channel = ,oVD/,uA = Flow area of the channel cross section, m2D = Equivalent hydraulic diameter of the channel cross section, mLc = Total coolant channel length causing frictional pressure drop, m.V = Coolant velocity averaged over the channel cross section, m/sW = Coolant mass flow rate in the channel, kg/s11 = Average coolant dynamic viscosity in the channel, N-s/rn2/u (T) = Temperature-dependent dynamic viscosity of water, N-s/rn2/-Uo =1 , (To) = Coolant dynamic viscosity at the channel inlet temperature ToFor the PUR-1 reactor, the temperature dependence of the dynamic viscosity of water over thetemperature range 27 00 < T < 50 &deg;0 can be approximated as follows.pz(T)= ,p(To) (1+T-T)0)- (10)where a = 0.12, To = 2700C, , ( To) = 0.875x10  
AT = P/ (W Cp)                                                                                       (5)
-3 N-s/in 2The average coolant dynamic viscosity  
_ 0o/gLP BuoyancyAp        -     WC(6)
,p used in Eq. (9) can be set equal to the viscosity atthe average coolant temperature (To + 0.5AT) in the channel.
Ignoring the minor losses at channel inlet and outlet, the laminar frictional pressure drop in the channel is written below as Eq. (9) after using the laminar friction factor given by Eq. (7), and after replacing the coolant velOcity by mass flow rate using Eq. (8). The parameter C in Eq. (7) is a constant for a given channel cross section, but it depends upon the channel cross section aspect ratio width/thickness, and varies from 57 for aspect ratio 1.0 (square channel) to 96 for an infinite aspect ratio (infinitely wide channel).
Putting this temperature in Eq.(10), the average viscosity  
f =C /Re                                                                                                 (7)
,u is found to be= ,p(To) (1 +0.5AT)0-. (11 )Equation (11) indicates that the average viscosity 41 can be set equal to ,p ( To) if AT is just afew 00 (this is the case for the PUR-1 reactor at the operating power of 1 kW). If AT is greaterthan a few 00, i.e., 1 <<0.5AT (this is the case for the PUR-1 reactor at an ONB power of about100 kW), then Eq. (11) simplifies to the following.
W= pAV                                                                                                   (8)
PUR-1 SARAppendix 2-6PUR- SARAppndix2-6Rev 2, July 23, 20i5  
PUR-1 SAR                                      Appendix 2-5                          PUR-SARAppndix2-5Rev 2, July 23, 2015
,u= ,u ( To) (0.5AT)-0i T 201aif AT >> 2 &deg;C(12a)/1u /u(To) if AT<<2 &deg;C (12b)Substituting Eq. (12a) into Eq. (9), the frictional Ap becomesFrictional Ap =
 
C'U&deg;LcW (-'W-p' (13)21-a p AD2  21-&deg; 7 AD2\ /-, PEquating the frictional A p of Eq. (13) to the buoyancy A p of Eq. (6) to find the steady-state coolant flow rate W in the channel, one obtains Eq. (14) below. Equation (14) can be rewritten as Eq. (15).P0flgLP-_ C 'u-----&deg;L-W--  
2 = C ULcW(9 Fritioal Fritioal P p_ *'k-'V 2D       24p AD 2                                                           9 where f        - Moody friction factor for laminar flow in the channel Re        - Reynolds number in the channel = ,oVD/,u A        = Flow area of the channel cross section, m2 D        = Equivalent hydraulic diameter of the channel cross section, m Lc      = Total coolant channel length causing frictional pressure drop, m.
(-W " (14)2WCp 21-a p AD2  )W -+ p0 poAD2 /3 gLPl+a 152' CltoLc 15Equation (15) relates the fuel plate power to the channel flow rate in natural circulation.
V       = Coolant velocity averaged over the channel cross section, m/s W        = Coolant mass flow rate in the channel, kg/s 11      = Average coolant dynamic viscosity in the channel, N-s/rn 2
It isused to find the dependence of the flow rate on the parameter C in the laminar friction factor (atconstant power). All parameters in this equation are constant is also practically constant) except the parameter C in the laminar friction factor. Based on Eq.(15),
        /u (T) = Temperature-dependent dynamic viscosity of water, N-s/rn 2
the relationship betweenthe flow rate W and the parameter C is given by Eq. (16) below.Wcc I (16)Equation (16) shows that the friction factor parameter C is multiplied by a factor (FW)2, the2coolant flow rate W will be reduced by the factor (FW)2+a,. This has been verified by actuallyrunning the NATCON code for the PUR-1 reactor.
        /-Uo   =1, (To) = Coolant dynamic viscosity at the channel inlet temperature To For the PUR-1 reactor, the temperature dependence of the dynamic viscosity of water over the temperature range 27       00 < T < 50 &deg;0 can be approximated as follows.
Since a is small (a = 0.12 for the PUR-1reactor),
pz(T)= ,p(To)(1+T-T) )-     0                                                                    (10) where a = 0.12, To = 2700C, , ( To) = 0.875x10 -3N-s/in       2 The average coolant dynamic viscosity ,p used in Eq. (9) can be set equal to the viscosity at the average coolant temperature (To + 0.5AT) in the channel. Putting this temperature in Eq.
21(2+a) is nearly 1.0, and the flow rate W is reduced approximately by the factor FW.Bulk Coolant Temperature Rise versus Power of a Fuel PlateEquation (5) expresses, for laminar natural circulation, the bulk coolant temperature rise interms of fuel plate power, coolant flow rate and specific heat. Putting the value of flow rateobtained in Eq. (15) into Eq. (5), the bulk coolant temperature rise is given by Eq. (17) below,purely in terms of power and the geometrical dimensions of the channel.
(10), the average viscosity ,u is found to be p* = ,p(To)(1 +0.5AT) -.0                                                                        (11 )
The right hand side ofEq. (17) is rearranged into two factors in Eq. (18), such that the second factor is sensitive topower and channel geometrical dimensions that usually have manufacturing tolerances andPUR-1 SARAppendix 2-7PUR- SARAppndix2-7Rev 2, July 23, 2015 measurement uncertainties, and the first factor is insensitive to power and channel geometrical dimensions.
Equation (11) indicates that the average viscosity 41 can be set equal to ,p ( To) if AT is just a few 00 (this is the case for the PUR-1 reactor at the operating power of 1 kW). If AT is greater than a few 00, i.e., 1 <<0.5AT (this is the case for the PUR-1 reactor at an ONB power of about 100 kW), then Eq. (11) simplifies to the following.
AT =::" 2;Q ---j2&#xf7; (17)'AT[C~p~po/gL  
PUR-1 SAR                                      Appendix 2-6                        PUR-SARAppndix2-6Rev 2, July 23, 20i5
.A (18)The nominal flow area and hydraulic diameter of a rectangular coolant channel are given byA = tnc Wn (1 9)P w= 2 (tnc + W ~c) (20)D = 4 A/ P~, = 2 tnc Who / (tnc + Wnc) (21)whereto = Channel thickness (spacing between fuel plates),
 
mto = Nominal channel thickness (spacing between fuel plates),
    ,u= ,u ( To) (0.5AT)- 0      ifi ATT>> 22 0&deg;C                                               1a (12a)
mthc = Minimum channel thickness in hot channel (spacing between fuel plates),
/ 1u   /u(To)                   if AT<<2 &deg;C                                                   (12b)
mWc =Channel width, assumed not to change from its nominal value, mPw = Wetted perimeter of the nominal channel, mPc = Power generated in a fuel plate, without applying manufacturing tolerances, WPhc = Power generated in a fuel plate, after applying manufacturing tolerances, WBecause the channel thickness to, is much smaller than the channel width Wc in mostexperimental
Substituting Eq. (12a) into Eq. (9), the frictional Ap becomes Frictional Ap         = Cui&deg;(AT)-*LcW=- C'U&deg;LcW (-'W-p'                                           (13) 21-a p AD 2          21-&deg; 7 AD 2 \ /-,
: reactors, Eq. (21) reduces too 2 tc, (22)Using the channel area and hydraulic diameter given by Eqs. (19) and (22) into Eq. (18), thebulk coolant temperature rise can be written in terms of power, channel thickness, and channelwidth. This is the desired relationship for use in finding hot channel factors.PUR-1 SAP,Appendix 2-8PUR- SARAppndix2-8Rev 2, July 23, 2015  
P Equating the frictional A p of Eq. (13) to the buoyancy A p of Eq. (6) to find the steady-state coolant flow rate W in the channel, one obtains Eq. (14) below. Equation (14) can be rewritten as Eq. (15).
-- --CfOL -7_- 1 (23)C 4w~t3Formulas for Hot Channel FactorsFor use in the NATCON version 2.0, six hot channel factors (three global/systemic and threelocal/random) are obtained from 9 manufacturing tolerances and measurement uncertainties u1,u=,..., u9 that are defined below. These are fractional uncertainties rather than percent.
P0 flgLP-_ C 'u-----&deg;L-W-- (-W         "                                                         (14) 2WCp           21-a p AD 2        )
Of thesenine uncertainties, those affecting a particular hot channel factor are indicated in Table 1. Thesystemic hot channel factors are given by Eqs. (24) through (26), and the random hot channelfactors are given by Eqs. (27) through (29). A utility Fortran computer program NATCON_HCF and a Microsoft spreadsheet NATCON.HotChanFactors.xls have also been developed tocompute the hot channel factors using these formulas.
W   -+ p0poAD2 /3gLPl+a                                                                     15 2' CltoLc C*                                                                        15 Equation (15) relates the fuel plate power to the channel flow rate in natural circulation. It is used to find the dependence of the flow rate on the parameter C in the laminar friction factor (at constant power). All parameters in this equation are constant (p* is also practically constant) except the parameter C in the laminar friction factor. Based on Eq.(15), the relationship between the flow rate W and the parameter C is given by Eq. (16) below.
EQ = 1 + u7 (24)FW =1 + u8 (25)FH = 1 + u9 (26)The ratio of the power generated in hot plate to its nominal power, caused by the uncertainties in neutronics-computed power and in U-235 mass per plate, can be written asPh...._c (1 +u1)(1+/-+u2) (27)nPoThe ratio of bulk coolant temperature rise in hot channel to the temperature rise in the nominalChannel, caused by the uncertainties in neutronics-computed power, U-235 mass per plate, andchannel thickness, is obtained from Eq. (23). Only the quantity in the second parentheses isimportant here because the quantity in the first parentheses is insensitive to these uncertainties.
Wcc     I                                                                                       (16)
~h 1 (28)The uncertainty in flow distribution is assumed to reduce the channel flow to (1- U6) times theflow without this uncertainty, and therefore the bulk coolant temperature rise is increased by thefactor (1+ u6). This uncertainty in bulk coolant temperature rise is statistically combined with thatgiven by Eq. (28) to obtain the following formula for the hot channel factor FBULK for input tothe NATOON version 2.0.FBULK= 1 +,  
Equation (16) shows that the friction factor parameter C is multiplied by a factor (FW) 2, the 2
: 1. -1+u2 (29)PUR-1 SARAppendix 2-9PuR- SARAppndix2-9Rev 2, July 23, 2015 The temperature drop across coolant film on the cladding surface at an axial location is given byEq. (30). Here the heat flux q" (W/m2) on the cladding surface is replaced by tf q'"/2 in terms ofthe volumetric power density q"'" (W/m3) in the fuel meat.Aflh 2h (0The convective heat transfer coefficient h (W/m2-C) is given by Eq. (31). Here the laminarNusselt number Nu is independent of flow rate, and varies only slowly with the aspect ratio(width/thickness) of coolant channel.
coolant flow rate W will be reduced by the factor (FW) 2+a,. This has been verified by actually running the NATCON code for the PUR-1 reactor. Since a is small (a = 0.12 for the PUR-1 reactor), 21(2+a) is nearly 1.0, and the flow rate W is reduced approximately by the factor FW.
The main variation of the heat transfer coefficient withchannel thickness is due to the denominator of Eq. (31). The numerator of Eq. (31) isconsidered to be constant.
Bulk Coolant Temperature Rise versus Power of a Fuel Plate Equation (5) expresses, for laminar natural circulation, the bulk coolant temperature rise in terms of fuel plate power, coolant flow rate and specific heat. Putting the value of flow rate obtained in Eq. (15) into Eq. (5), the bulk coolant temperature rise is given by Eq. (17) below, purely in terms of power and the geometrical dimensions of the channel. The right hand side of Eq. (17) is rearranged into two factors in Eq. (18), such that the second factor is sensitive to power and channel geometrical dimensions that usually have manufacturing tolerances and PUR-1 SAR                                          Appendix 2-7                PUR-SARAppndix2-7Rev 2, July 23, 2015
h -NKc&deg;&deg; -N"IKC&deg;&deg;!  
 
(31)D 2tcUsing Eq. (31) for the heat transfer coefficient, the temperature drop across coolant film can bewritten as Eq. (32).fil~m -Nco (32)Equation (32) states that ATift,~ is directly proportional to the fuel meat thickness (havinguncertainty u3), the channel thickness (having uncertainty u5), and the power density in meat.The uncertainty in power density is caused by three uncertainties, that is, u1, u2 and u4.Statistically combining these five uncertainties gives the following formula for the hot channelfactor FFILM for input to the NATCON version 2.0.FFILM =1+4Ul2+/-+u 22+/-+u32+/-u-/452 (33)The uncertainty in the heat flux at the cladding surface is included in the hot channel factorFFILM given by Eq. (33). A hot channel factor FFLUX for the heat flux alone can be found fromEq. (34) for heat flux in terms of the power density q"'" in the fuel meat and the thickness of themeat. The fractional uncertainty in heat flux is the sum of fractional uncertainties in powerdensity and meat thickness, as given by Eq. (35).q" t- (34)2Sq"_ Sq '" Ste__ +/- fe (35)q,, q,, tfuelIn Eq. (35), the uncertainty in power density is caused by three uncertainties, that is, u1, u2 andu4.The uncertainty in the meat thickness is given by u3.Statistically combining these fouruncertainties gives the following formula for the hot channel factor FFLUX for input to theNATCON version 2.0.PUR-1 SARAppendix 2-10PUR- SARAppedix  
measurement uncertainties, and the first factor is insensitive to power and channel geometrical dimensions.
-10Rev 2, July 23, 2015 FFLUX= 1+ u12+//2 -+/-u32+u42(6(36)The uncertainty in the temperature drop ATmetal from fuel meat centerline to cladding surface isnot important in the case of the PUR-1 reactor because ATmetai is very small compared to ATritm.For example, ATmetai is 0.05 00 and ATfilm is 34.5 00 at 100 kW without any hot channel factors.Table A2-1. Uncertainties Included in the Six Hot Channel Factors Used in NATCON Version2.0 (X implies that an uncertainty affects a hot channel factor)Uncertainty Fraction FQ FW {FH FBULK FFILM FFLUXLocal or random uncertainties I Neutronics calculation ofXXXpower in a plate, u12 U-235 mass per plate, u2  X X X3 Local fuel meat thickness,XX u34 U-235 axial homogeneity,XX 5 Coolant channel thickness,XX u56 Flow distribution amongXXchannels, u6System-wide uncertainties 7 Reactor powermeasurement uncertainty, X8 Flow uncertainty due to X___uncertainty in friction_____
AT =::" 2;Q     ---&deg;c;-]*P    j2&#xf7;                                                                 (17)'
PUR-1 SARAppendix 2-11PUR- SARAppedix  
AT[C~p~po/gL               .A                                                                 (18)
-1 1Rev 2, July 23, 2015 factor, u89 Heat transfer coefficient uncertainty due to uncertainty inNu number correlation, u9The following information was presented as answers to Requests for Additional Information (RAIs) during the conversion process.
The nominal flow area and hydraulic diameter of a rectangular coolant channel are given by A = tnc Wn                                                                                         (1 9)
This information is not presented in the SAR chapters onthermal hydraulics.
Pw= 2 (tnc+ W~c)                                                                                 (20)
Question 2828. Appendix  
D = 4 A/ P~, = 2   tnc Who / (tnc + Wnc)                                                         (21) where to = Channel thickness (spacing between fuel plates), m to = Nominal channel thickness (spacing between fuel plates), m thc      = Minimum channel thickness in hot channel (spacing between fuel plates), m Wc =Channel width, assumed not to change from its nominal value, m Pw = Wetted perimeter of the nominal channel, m Pc = Power generated in a fuel plate, without applying manufacturing tolerances, W Phc      = Power generated in a fuel plate, after applying manufacturing tolerances, W Because the channel thickness to, is much smaller than the channel width Wc in most experimental reactors, Eq. (21) reduces to o  ,* 2 tc,                                                                                       (22)
: 1. From the information in Appendix 1 it is not clear how insignificant are thechannel inlet and outlet losses when compared to the wall shear. Please clarify.Response:
Using the channel area and hydraulic diameter given by Eqs. (19) and (22) into Eq. (18), the bulk coolant temperature rise can be written in terms of power, channel thickness, and channel width. This is the desired relationship for use in finding hot channel factors.
The information in Appendix 1 was used only to obtain hot channel factors for input to a moredetailed thermal-hydraulic calculation using the NATCON code [Ref. 8 of the conversion proposal].
PUR-1 SAP,                                   Appendix 2-8                          PUR-SARAppndix2-8Rev 2, July 23, 2015
Therefore, Appendix 1 is a simplified modeling of what is calculated in detail inNATCON, and it is used only for the purpose of obtaining closed-form equations from which hotchannel factors could be found. Appendix 1 does not include the minor losses. The minor lossescalculated by NATCON are reported below, and found to be about 16% of the total frictional pressure drop in the HEU core, and 14% of the total frictional pressure drop in the LEU core(see Table 027-1 ).The pressure drop due to inlet and outlet losses were calculated (by the NATCON code) usingloss coefficients of 0.5 and 1.0 respectively.
 
The pressure drop due to wall shear along thechannel length is found by summing the pressure drop for each axial mesh which is calculated using temperature-dependent coolant viscosity and density for the axial mesh (14 meshintervals were used over the channel length in all calculations).
CfOL
The pressure drops arecalculated by NATCON assuming fully developed laminar flow in a rectangular cross-section
            --     --           -7_- 1                                                             (23)
: channel, and then multiplied by a factor FW2 (FW squared) where FW is an input which may beused to account for the increased pressure drop due to hydrodynamically developing laminarflow. In the calculations presented in the conversion  
C   /o3afgL'*    4w~t3 Formulas for Hot Channel Factors For use in the NATCON version 2.0, six hot channel factors (three global/systemic and three local/random) are obtained from 9 manufacturing tolerances and measurement uncertainties u1 ,
: proposal, FW was always set to 1.0, andthus the increased pressure drop due to developing laminar flow was not included.
u=,..., u 9 that are defined below. These are fractional uncertainties rather than percent. Of these nine uncertainties, those affecting a particular hot channel factor are indicated in Table 1. The systemic hot channel factors are given by Eqs. (24) through (26), and the random hot channel factors are given by Eqs. (27) through (29). A utility Fortran computer program NATCON_HCF and a Microsoft spreadsheet NATCON.HotChanFactors.xls have also been developed to compute the hot channel factors using these formulas.
It is includedin the calculations presented here (Table 027-1). The method used is described below.For the most limiting fuel plate in Table 4-27 of the conversion proposal for each core (HEU andLEU), a comparison of the pressure drops due to inlet plus outlet loss and wall shear, with andwithout the effect of developing laminar flow, are tabulated in Table 027-1.NATCON calculates the Darcy-Weisbach friction factor f = C/Re for laminar flow, using a built-intable of the parameter C for different aspect ratios of the rectangular channel cross sectionPUR-1 SARAppendix 2-12PUR- SARAppedix  
EQ = 1 + u7                                                                                           (24)
-12Rev 2, July 23, 2015 (values of parameter C are given in the response to Question number 29). An apparent value ofthe parameter C averaged over the channel length, called Capp, was calculated using Eq. (576)of Shah and London [Ref. 2 listed at the end of all responses]
FW =1 + u8                                                                                             (25)
to account for the increased pressure drop due to hydrodynamically developing laminar flow in the channel.
FH = 1 + u9                                                                                           (26)
The ratio Capp/Cwas found to be 1.1105 for the 207 mil HEU channel, 1.0985 for the 197 mil LEU channel.
The ratio of the power generated in hot plate to its nominal power, caused by the uncertainties in neutronics-computed power and in U-235 mass per plate, can be written as Ph...._c(1 +u1 )(1+/-+u  2)                                                                             (27) nPo The ratio of bulk coolant temperature rise in hot channel to the temperature rise in the nominal Channel, caused by the uncertainties in neutronics-computed power, U-235 mass per plate, and channel thickness, is obtained from Eq. (23). Only the quantity in the second parentheses is important here because the quantity in the first parentheses is insensitive to these uncertainties.
Sincethe NATOON code multiplies the fully developed friction factor by FW2 as mentioned above, theinput FW equals 1.054 and 1.048 for the HEU and LEU channels respectively.
            ~h 1                                                                                     (28)
NATCONcalculations were done using these values of FW, and the pressure drops due to inlet plus outletloss and wall shear are compared in Table Q27-1 (column B for the HEU channel, and column Ffor the LEU channel).
The uncertainty in flow distribution is assumed to reduce the channel flow to (1-         U6 ) times the flow without this uncertainty, and therefore the bulk coolant temperature rise is increased by the factor (1+ u 6 ). This uncertainty in bulk coolant temperature rise is statistically combined with that given by Eq. (28) to obtain the following formula for the hot channel factor FBULK for input to the NATOON version 2.0.
Table Q27-1 shows that the pressure drops due to wall shear and minor losses are 84% and16%, respectively, of the total pressure drop in the HEU channel at its ONB power; and thepressure drops due to wall shear and inlet plus outlet loss are 86% and 14%, respectively, ofthe total pressure drop in the LEU channel at its ONB power.Question 2929. Appendix  
FBULK= 1 +,           lu)*g'~22T            1.       -1+u2                                           (29)
: 1. From the information in Appendix 1 it is not clear what is the functional dependency of the laminar friction parameter C to the channel cross-section dimensions.
PUR-1 SAR                                      Appendix 2-9                          PuR-SARAppndix2-9Rev 2, July 23, 2015
Provide a reference for the evaluation of C.Response:
 
The following values (rows 1 and 2 of Table Q29-1) of the parameter C for fully developed laminar flow in a channel of rectangular cross section versus the width-to-thickness aspect ratio(Wc/tc) of the channel are used in the NATCON code that was used in the thermal-hydraulics calculations.
The temperature drop across coolant2 film on the cladding surface at an axial location is given by Eq. (30). Here the heat flux q" (W/m ) on the cladding surface is replaced by tf q'"/2 in terms of the volumetric power density q"'" (W/m 3 ) in the fuel meat.
The table starts from the square cross section (aspect ratio = 1.0) and goes to theinfinite value of the aspect ratio (parallel plates).
Aflh         2h                                                                         (0 The convective heat transfer coefficient h (W/m 2 -C) is given by Eq. (31). Here the laminar Nusselt number Nu is independent of flow rate, and varies only slowly with the aspect ratio (width/thickness) of coolant channel. The main variation of the heat transfer coefficient with channel thickness is due to the denominator of Eq. (31). The numerator of Eq. (31) is considered to be constant.
In order to find the parameter C for the aspectratio of the PUR-1 reactor, the NATCON code simply interpolates between the tabulated values.The original author of the code obtained these values from an old Reference  
h - NKc&deg;&deg;       - N"IKC&deg;&deg;!                                                                     (31)
[E. R. G. Eckertand T. F. Irvine, Heat Transfer Laboratory, University of Minnesota (1957)] but these values arealso given in a textbook by Frank Incropera  
D           2tc Using Eq. (31) for the heat transfer coefficient, the temperature drop across coolant film can be written as Eq. (32).
[Ref. 3]. These values are obtained from the closed-form analytical solution for the fully developed laminar velocity distribution in a rectangular channel summarized by R. K. Shah and A. L. London [Ref. 2]. Equation (341) in [Ref. 2] is afitted equation to easily find the parameter C. It should be noted that the aspect ratio used in[Ref. 2] is channel thickness-to-width ratio (the reciprocal of that used in NATOON and shownbelow in Table A2-2), and the friction factor in [Ref. 2] should be multiplied by 4 to get theDarcy-Weisbach friction factor that is used in NATCON and tabulated below.Table A2-2. Friction Parameter C Used in the NATCON Codewtc 1.0 2.0 3.0 4.0 5.0 6.3 8.0 11.0 15.0 18.0 100.0C in 58.0 63.0 69.0 72.5 77.0 80.0 83.0 85.0 88.0 89.0 96.0NATCONPUR-1 SARAppendix 2-13PUR- SARAppedix  
fil~m -   Nco                                                                                 (32)
-13Rev 2, July 23, 2015 C in 57.0 62.0 69.0 73.0 82.0 96.0Ref. 3C in 56.9 62.2 68.4 72.9 76.3 79.5 82.4 85.6 88.1 89.3 94.7Ref. 2Question 3030. Appendix  
Equation (32) states that ATift,~is directly proportional to the fuel meat thickness (having uncertainty u3 ), the channel thickness (having uncertainty u5 ), and the power density in meat.
: 1. From the information in Appendix 1 in both the calculation of the channelflow and the calculation of the bulk coolant temperature rise the ratio of the coolant kinematic viscosity to density (pip) was assumed to be insensitive to temperature.
The uncertainty in power density is caused by three uncertainties, that is, u1 , u2 and u4 .
Please demonstrate thevalidity of this assumption.
Statistically combining these five uncertainties gives the following formula for the hot channel factor FFILM for input to the NATCON version 2.0.
FFILM =1+4Ul2+/-+u           2 2+/-+u 3 2+/-u-/
4 2+/-*U5 2                                                    (33)
The uncertainty in the heat flux at the cladding surface is included in the hot channel factor FFILM given by Eq. (33). A hot channel factor FFLUX for the heat flux alone can be found from Eq. (34) for heat flux in terms of the power density q"'" in the fuel meat and the thickness of the meat. The fractional uncertainty in heat flux is the sum of fractional uncertainties in power density and meat thickness, as given by Eq. (35).
q"       t-                                                                                   (34) 2 Sq"_ Sq       '" Ste
__          +/-   fe                                                                         (35) q,, q,,     tfuel In Eq. (35), the uncertainty in power density is caused by three uncertainties, that is, u1 , u 2 and u4 . The uncertainty in the meat thickness is given by u3 . Statistically combining these four uncertainties gives the following formula for the hot channel factor FFLUX for input to the NATCON version 2.0.
PUR-1 SAR                                      Appendix 2-10                      PUR-SARAppedix
                                                                                          -10Rev 2, July 23, 2015
 
FFLUX= 1+ */~u1 2 +//2     -+/-u32 +u 42                                                                (6 (36)
The uncertainty in the temperature drop ATmetal from fuel meat centerline to cladding surface is not important in the case of the PUR-1 reactor because ATmetai is very small compared to ATritm.
For example, ATmetai is 0.05 00 and ATfilm is 34.5 00 at 100 kW without any hot channel factors.
Table A2-1. Uncertainties Included in the Six Hot Channel Factors Used in NATCON Version 2.0 (X implies that an uncertainty affects a hot channel factor)
Uncertainty Fraction             FQ   FW   {FH     FBULK   FFILM         FFLUX Local or random uncertainties I   Neutronics calculation       ofXXX power in a plate, u1 2 U-235 mass per plate, u 2                                X        X               X 3 Local fuel meat thickness,XX u3 4 U-235 axial homogeneity,XX 5 Coolant channel thickness,XX u5 6 Flow distribution         amongXX channels, u6 System-wide uncertainties 7       Reactor                 power measurement uncertainty,         X 8        Flow     uncertainty   due to           X
___uncertainty        in     friction_____
PUR-1 SAR                                      Appendix 2-11                          PUR-SARAppedix
                                                                                              -11Rev 2, July 23, 2015
 
factor, u 8 9    Heat transfer     coefficient uncertainty due to uncertainty in Nu number correlation, u9 The following information was presented as answers to Requests for Additional Information (RAIs) during the conversion process. This information is not presented in the SAR chapters on thermal hydraulics.
Question 28
: 28.     Appendix 1. From the information in Appendix 1 it is not clear how insignificant are the channel inlet and outlet losses when compared to the wall shear. Please clarify.
 
===Response===
The information in Appendix 1 was used only to obtain hot channel factors for input to a more detailed thermal-hydraulic calculation using the NATCON code [Ref. 8 of the conversion proposal]. Therefore, Appendix 1 is a simplified modeling of what is calculated in detail in NATCON, and it is used only for the purpose of obtaining closed-form equations from which hot channel factors could be found. Appendix 1 does not include the minor losses. The minor losses calculated by NATCON are reported below, and found to be about 16% of the total frictional pressure drop in the HEU core, and 14% of the total frictional pressure drop in the LEU core (see Table 027-1 ).
The pressure drop due to inlet and outlet losses were calculated (by the NATCON code) using loss coefficients of 0.5 and 1.0 respectively. The pressure drop due to wall shear along the channel length is found by summing the pressure drop for each axial mesh which is calculated using temperature-dependent coolant viscosity and density for the axial mesh (14 mesh intervals were used over the channel length in all calculations). The pressure drops are calculated by NATCON assuming fully developed laminar flow in a rectangular cross-section channel, and then multiplied by a factor FW 2 (FW squared) where FW is an input which may be used to account for the increased pressure drop due to hydrodynamically developing laminar flow. In the calculations presented in the conversion proposal, FW was always set to 1.0, and thus the increased pressure drop due to developing laminar flow was not included. It is included in the calculations presented here (Table 027-1). The method used is described below.
For the most limiting fuel plate in Table 4-27 of the conversion proposal for each core (HEU and LEU), a comparison of the pressure drops due to inlet plus outlet loss and wall shear, with and without the effect of developing laminar flow, are tabulated in Table 027-1.
NATCON calculates the Darcy-Weisbach friction factor f = C/Re for laminar flow, using a built-in table of the parameter C for different aspect ratios of the rectangular channel cross section PUR-1 SAR                                  Appendix 2-12                        PUR-SARAppedix
                                                                                          -12Rev 2, July 23, 2015
 
(values of parameter C are given in the response to Question number 29). An apparent value of the parameter C averaged over the channel length, called Capp, was calculated using Eq. (576) of Shah and London [Ref. 2 listed at the end of all responses] to account for the increased pressure drop due to hydrodynamically developing laminar flow in the channel. The ratio Capp/C was found to be 1.1105 for the 207 mil HEU channel, 1.0985 for the 197 mil LEU channel. Since the NATOON code multiplies the fully developed friction factor by FW 2 as mentioned above, the input FW equals 1.054 and 1.048 for the HEU and LEU channels respectively. NATCON calculations were done using these values of FW, and the pressure drops due to inlet plus outlet loss and wall shear are compared in Table Q27-1 (column B for the HEU channel, and column F for the LEU channel).
Table Q27-1 shows that the pressure drops due to wall shear and minor losses are 84% and 16%, respectively, of the total pressure drop in the HEU channel at its ONB power; and the pressure drops due to wall shear and inlet plus outlet loss are 86% and 14%, respectively, of the total pressure drop in the LEU channel at its ONB power.
Question 29
: 29.       Appendix 1. From the information in Appendix 1 it is not clear what is the functional dependency of the laminar friction parameter C to the channel cross-section dimensions.
Provide a reference for the evaluation of C.
 
===Response===
The following values (rows 1 and 2 of Table Q29-1) of the parameter C for fully developed laminar flow in a channel of rectangularcross section versus the width-to-thickness aspect ratio (Wc/tc) of the channel are used in the NATCON code that was used in the thermal-hydraulics calculations. The table starts from the square cross section (aspect ratio = 1.0) and goes to the infinite value of the aspect ratio (parallel plates). In order to find the parameter C for the aspect ratio of the PUR-1 reactor, the NATCON code simply interpolates between the tabulated values.
The original author of the code obtained these values from an old Reference [E. R. G. Eckert and T. F. Irvine, Heat Transfer Laboratory, University of Minnesota (1957)] but these values are also given in a textbook by Frank Incropera [Ref. 3]. These values are obtained from the closed-form analytical solution for the fully developed laminar velocity distribution in a rectangular channel summarized by R. K. Shah and A. L. London [Ref. 2]. Equation (341) in [Ref. 2] is a fitted equation to easily find the parameter C. It should be noted that the aspect ratio used in
[Ref. 2] is channel thickness-to-width ratio (the reciprocal of that used in NATOON and shown below in Table A2-2), and the friction factor in [Ref. 2] should be multiplied by 4 to get the Darcy-Weisbach friction factor that is used in NATCON and tabulated below.
Table A2-2. Friction Parameter C Used in the NATCON Code wtc      1.0     2.0     3.0     4.0     5.0     6.3     8.0     11.0 15.0   18.0     100.0 C in     58.0   63.0   69.0     72.5   77.0     80.0   83.0     85.0 88.0   89.0       96.0 NATCON PUR-1 SAR                                    Appendix 2-13                        PUR-SARAppedix
                                                                                            -13Rev 2, July 23, 2015
 
C in       57.0     62.0   69.0     73.0                   82.0                           96.0 Ref. 3 C in       56.9     62.2   68.4     72.9     76.3     79.5 82.4 85.6   88.1     89.3       94.7 Ref. 2 Question 30
: 30.     Appendix 1. From the information in Appendix 1 in both the calculation of the channel flow and the calculation of the bulk coolant temperature rise the ratio of the coolant kinematic viscosity to density (pip) was assumed to be insensitive to temperature. Please demonstrate the validity of this assumption.


===Response===
===Response===
The information in Appendix 1 was used only to obtain hot channel factors for input to a moredetailed thermal-hydraulic calculation using the NATCON code [Ref. 8 of the conversion proposal].
The information in Appendix 1 was used only to obtain hot channel factors for input to a more detailed thermal-hydraulic calculation using the NATCON code [Ref. 8 of the conversion proposal]. NATCON does account for the temperature dependence of coolant viscosity and density in the calculation of the channel flow and the calculation of the bulk coolant temperature rise. Therefore, Appendix 1 is a simplified modeling of what is calculated in detail in NATCON, for the purpose of obtaining closed-form equations from which hot channel factors could be found.
NATCON does account for the temperature dependence of coolant viscosity anddensity in the calculation of the channel flow and the calculation of the bulk coolant temperature rise. Therefore, Appendix 1 is a simplified modeling of what is calculated in detail in NATCON,for the purpose of obtaining closed-form equations from which hot channel factors could befound.As suggested in the question, water viscosity is temperature-dependent, i.e., it decreases withrising temperature.
As suggested in the question, water viscosity is temperature-dependent, i.e., it decreases with rising temperature. Appendix 1 was revised to account for the effect of temperature dependence of viscosity on hot channel factors, and the revised Appendix 1 is enclosed herewith. The temperature dependence of the dynamic viscosity of water over the temperature range 27 00 <
Appendix 1 was revised to account for the effect of temperature dependence of viscosity on hot channel factors, and the revised Appendix 1 is enclosed herewith.
T < 50 00 (adequate for the PUR-1 reactor) can be written as follows.
Thetemperature dependence of the dynamic viscosity of water over the temperature range 27 00 <T < 50 00 (adequate for the PUR-1 reactor) can be written as follows./()= /z(T0) (1+T-T0)-0 (Al)where a=0.12To= 27 00 = Pool temperature of PUR-1,u ( To) = 0.875x10  
              /()= /z(T 0 ) (1+T-T 0 )-0                                                       (Al) where     a=0.12 To= 27 00 = Pool temperature of PUR-1
-3 N-s/rn 2,p (T) = Temperature-dependent dynamic viscosity of water, N-s/in2As shown in the revised Appendix 1, the revised relationship between the flow rate W in achannel and the friction parameter C is given by Eq. (A2). The revised formula for hot channelfactor FBULK for bulk coolant temperature rise is given by Eq. (A3).(A2PUR-1 SARAppendix 2-14PuR- SARAppedix  
                    ,u ( To) = 0.875x10   -3 N-s/rn 2
-14Rev 2, July 23, 2015 FRUlLu )=+, (l+u9)2+- lJ l -1} u (A3)The exponent on the right hand side of Eq. (A2) changed from 0.5 (in the conversion proposalignoring temperature dependence of p) to the revised value 1/2.12 = 0.4717. There exponents in Eq. (A3) for EBULK also changed, e.g., from 3/2 to 3/2.12 =1.415. As a result of this revision, the hot channel factor FBULK decreased from 1.312 (in the conversion proposal) to 1.301 forthe most limiting fuel plate 262 in the HEU core. Similarly, FBULK decreased from 1.321 (in theconversion proposal) to 1.308 for the most limiting fuel plate 1348 in the LEU core. The effect ofignoring the temperature dependence of viscosity is conservative.
                    ,p (T) = Temperature-dependent dynamic viscosity of water, N-s/in 2 As shown in the revised Appendix 1, the revised relationship between the flow rate W in a channel and the friction parameter C is given by Eq. (A2). The revised formula for hot channel factor FBULK for bulk coolant temperature rise is given by Eq. (A3).
NATCON calculations were done with these revised values of EBULK along with a value of FW> 1.0 to account for the increased friction due to developing laminar flow (in response toQuestion number 33). The results are shown in Table Q27-1 (column C for the HEU core, andcolumn G for the LEU core).As a consequence of the two effects (i.e., increased friction due to developing laminar flow andthe temperature dependence of viscosity) on hot channel factors FW and EBULK, the ONBpower of the HEU core changes from 76.3 kW (reported in the conversion proposal) to 75.9 kW,and the ONB power of the LEU core changes from 96.1 kW (reported in the conversion proposal) to 95.8 kW. The effect is small for the PUR-1 reactor.Question 3232. Appendix  
(A2 PUR-1 SAR                                        Appendix 2-14                  PuR-SARAppedix
: 1. Equation (30) has two terms and the conversion proposal states that theexpression within the parenthesis on the right hand side of the equation varies slowly comparedto the heat flux tfuel q'"/2. Demonstrate the validity of the statement with reference to the PUR-1fuel plate.Response:
                                                                                          -14Rev 2, July 23, 2015
Equation (30) of Appendix 1 is for finding a hot channel factor for the temperature drop from themeat mid-plane to cladding surface (ATmetai).
 
This temperature drop is very small compared tothe temperature drop from the cladding surface to bulk coolant (ATflrn).
FRUlLu               )=+,(l+u9 )2+- lJ           l -1}   u                               (A3)
For example, in thePUR-1 HEU fuel plate 262 without hot channel factors, Ammetai iS 0.07 &deg;C and ATfi~m is 46.98 &deg;C(at meat mid-height) at a high power of 100 kW. Similarly, in the PUR-1 LEU fuel plate 1348without hot channel factors, Ammetai is 0.05 &deg;C and ATfi m is 34.5 &deg;C at a power of 100 kW.Therefore, the hot channel factor for Ammetai iS not important for PUR-1. The important hotchannel factor is the factor FFILM for ATf, m. In the case of PUR-1, ATtim is the biggercomponent (bigger than the bulk coolant temperature rise) in the total temperature rise from theinlet temperature to the cladding surface temperature at the axial level experiencing the onset ofnucleate boiling.
The exponent on the right hand side of Eq. (A2) changed from 0.5 (in the conversion proposal ignoring temperature dependence of p) to the revised value 1/2.12 = 0.4717. There exponents in Eq. (A3) for EBULK also changed, e.g., from 3/2 to 3/2.12 =1.415. As a result of this revision, the hot channel factor FBULK decreased from 1.312 (in the conversion proposal) to 1.301 for the most limiting fuel plate 262 in the HEU core. Similarly, FBULK decreased from 1.321 (in the conversion proposal) to 1.308 for the most limiting fuel plate 1348 in the LEU core. The effect of ignoring the temperature dependence of viscosity is conservative.
The hot channel factor FFILM found by Eq. (29) of Appendix 1 in theconversion proposal remains unchanged.
NATCON     calculations were done with these revised values of EBULK along with a value of FW
It depends on the uncertainties in q'"tfuel and channelthickness (as shown in Eq. 28), but not on the uncertainty in [tfuel/(4KfueI) + tcdad/Kclad].
> 1.0 to   account for the increased friction due to developing laminar flow (in response to Question    number 33). The results are shown in Table Q27-1 (column C for the HEU core, and column G   for the LEU core).
In short, PUR-1 is not limited by the fuel peak temperature, but by the onset of nucleate boiling,and the uncertainty in [tfuel/(4KfueI) + tclad/Kclad]
As a consequence of the two effects (i.e., increased friction due to developing laminar flow and the temperature dependence of viscosity) on hot channel factors FW and EBULK, the ONB power of the HEU core changes from 76.3 kW (reported in the conversion proposal) to 75.9 kW, and the ONB power of the LEU core changes from 96.1 kW (reported in the conversion proposal) to 95.8 kW. The effect is small for the PUR-1 reactor.
is not important for PUR-1. We believe that thehot channel factor FFILM has been determined accurately.
Question 32
PUR-1 SARAppendix 2-15PUR- SARAppedix  
: 32.     Appendix 1. Equation (30) has two terms and the conversion proposal states that the expression within the parenthesis on the right hand side of the equation varies slowly compared to the heat flux tfuel q'"/2. Demonstrate the validity of the statement with reference to the PUR-1 fuel plate.
-15Rev 2, July 23, 2015 Question 3333. Section 4.7.2. According to Appendix 1 the systematic uncertainty in flow rate isaccounted for by applying the hot channel factor Fw to the laminar friction factor C. Explain thereason for the value of the flow friction factor Fw being unity in Tables 4-25 and 4-26.Response:
 
As suggested in the question, a value of FW (hot channel factor for flow) greater than 1.0 shouldbe used to account for the increased frictional pressure drop due to the hydrodynamically developing laminar flow in the entrance region of the coolant channel, otherwise the code(NATCON) accounts only for the fully developed frictional pressure drop. This has been donenow and the results are presented in Table Q27-1. Since each coolant channel creates its ownbuoyancy to drive its own coolant flow, there is no uncertainty due to redistribution of a totalreactor flow rate. The loss coefficients of 0.5 and 1.0 at channel inlet and outlet are used in thecalculations.
===Response===
To account for the reduction in flow rate due to the hydrodynamically developing laminar flow in the channel, the values of FW were calculated for the most limiting channels inthe HEU and LEU cores as follows.NATOON calculates the Darcy-Weisbach friction factor f = C/Re using a built-in table of theparameter C for different aspect ratios of the rectangular channel cross section (values ofparameter C are given in the answer to Question number 29). These values of parameter C arefor the fully developed laminar flow in a rectangular cross-section channel.
Equation (30) of Appendix 1 is for finding a hot channel factor for the temperature drop from the meat mid-plane to cladding surface (ATmetai). This temperature drop is very small compared to the temperature drop from the cladding surface to bulk coolant (ATflrn). For example, in the PUR-1 HEU fuel plate 262 without hot channel factors, Ammetai iS 0.07 &deg;C and ATfi~m is 46.98 &deg;C (at meat mid-height) at a high power of 100 kW. Similarly, in the PUR-1 LEU fuel plate 1348 without hot channel factors, Ammetai is 0.05 &deg;C and ATfi m is 34.5 &deg;C at a power of 100 kW.
An apparent value ofthe parameter C averaged over the channel length, called Capp, was calculated using Eq. (576)of Shah and London [Ref. 2] to account for the increased pressure drop due tohydrodynamically developing laminar flow in the channel.
Therefore, the hot channel factor for Ammetai iS not important for PUR-1. The important hot channel factor is the factor FFILM for ATf, m. In the case of PUR-1, ATtim is the bigger component (bigger than the bulk coolant temperature rise) in the total temperature rise from the inlet temperature to the cladding surface temperature at the axial level experiencing the onset of nucleate boiling. The hot channel factor FFILM found by Eq. (29) of Appendix 1 in the conversion proposal remains unchanged. It depends on the uncertainties in q'"tfuel and channel thickness (as shown in Eq. 28), but not on the uncertainty in [tfuel/( 4 KfueI) + tcdad/Kclad].
The ratio Capp/C was found to be1.1105 for the 207 rail HEU channel, and 1.0985 for the 197 mil LEU channel.
In short, PUR-1 is not limited by the fuel peak temperature, but by the onset of nucleate boiling, and the uncertainty in [tfuel/( 4 KfueI) + tclad/Kclad] is not important for PUR-1. We believe that the hot channel factor FFILM has been determined accurately.
Since theNATCON code multiplies the fully developed frictional factor by FW2, the input FW equals 1.054and 1.048 for the HEU and LEU channels respectively.
PUR-1 SAR                                        Appendix 2-15                        PUR-SARAppedix
The flow reduction factor is input factorFW or more accurately FW2/(2+a) FW&deg;'9434 (noting that a = 0.12 for the PUR-1 reactor asmentioned in the revised Appendix 1 enclosed herewith).
                                                                                                  -15Rev 2, July 23, 2015
The results of using these values of FW in NATCON calculations (excluding the effect oftemperature dependence of p on hot channel factors) are shown in Table Q27-1. The ONBpower of the HEU core changes to 75.8 kW from 76.3 kW reported in the conversion proposal.
 
Question 33
: 33.      Section 4.7.2. According to Appendix 1 the systematic uncertainty in flow rate is accounted for by applying the hot channel factor Fw to the laminar friction factor C. Explain the reason for the value of the flow friction factor Fw being unity in Tables 4-25 and 4-26.
 
===Response===
As suggested in the question, a value of FW (hot channel factor for flow) greater than 1.0 should be used to account for the increased frictional pressure drop due to the hydrodynamically developing laminar flow in the entrance region of the coolant channel, otherwise the code (NATCON) accounts only for the fully developed frictional pressure drop. This has been done now and the results are presented in Table Q27-1. Since each coolant channel creates its own buoyancy to drive its own coolant flow, there is no uncertainty due to redistribution of a total reactor flow rate. The loss coefficients of 0.5 and 1.0 at channel inlet and outlet are used in the calculations. To account for the reduction in flow rate due to the hydrodynamically developing laminar flow in the channel, the values of FW were calculated for the most limiting channels in the HEU and LEU cores as follows.
NATOON calculates the Darcy-Weisbach friction factor f = C/Re using a built-in table of the parameter C for different aspect ratios of the rectangular channel cross section (values of parameter C are given in the answer to Question number 29). These values of parameter C are for the fully developed laminar flow in a rectangular cross-section channel. An apparent value of the parameter C averaged over the channel length, called Capp, was calculated using Eq. (576) of Shah and London [Ref. 2] to account for the increased pressure drop due to hydrodynamically developing laminar flow in the channel. The ratio Capp/C was found to be 1.1105 for the 207 rail HEU channel, and 1.0985 for the 197 mil LEU channel. Since the NATCON code multiplies the fully developed frictional factor by FW 2 , the input FW equals 1.054 and 1.048 for the HEU and LEU channels respectively. The flow reduction factor is input factor FW or more accurately FW2/( 2+a) FW&deg;'94 34 (noting that a = 0.12 for the PUR-1 reactor as mentioned in the revised Appendix 1 enclosed herewith).
The results of using these values of FW in NATCON calculations (excluding the effect of temperature dependence of p on hot channel factors) are shown in Table Q27-1. The ONB power of the HEU core changes to 75.8 kW from 76.3 kW reported in the conversion proposal.
The ONB power of the LEU core changes to 95.7 kW from 96.1 kW reported in the conversion proposal.
The ONB power of the LEU core changes to 95.7 kW from 96.1 kW reported in the conversion proposal.
The channel flow indeed gets reduced by the factor FW0"9434 as expected.
The channel flow indeed gets reduced by the factor FW0 9434    "   as expected. For the HEU plate 262, the flow reduces from 0.02083 kg/s to 0.01 989 kg/s (see Table Q27-1) when the input hot channel factor FW is changed from 1.0 to 1.054. The expected reduced flow should be 0.02083/(1.054)0"9434   = 0.01982 kg/s which is close to the NATCON-calculated value of 0.01 989 kg/s. For the LEU plate 1348, the flow reduces from 0.01 912 kg/s to 0.01834 kg/s (see Table Q27-1) when the input FW is changed from 1.0 to 1.048. The expected reduced flow should be 0.01 912/(1 .048)0.9434 = 0.01 829 kg/s which is close to the NATCON-calculated value of 0.01834 kg/s.
For the HEU plate262, the flow reduces from 0.02083 kg/s to 0.01 989 kg/s (see Table Q27-1) when the input hotchannel factor FW is changed from 1.0 to 1.054. The expected reduced flow should be0.02083/(1.054)0"9434  
Question 36
= 0.01982 kg/s which is close to the NATCON-calculated value of 0.01 989kg/s. For the LEU plate 1348, the flow reduces from 0.01 912 kg/s to 0.01834 kg/s (see TableQ27-1) when the input FW is changed from 1.0 to 1.048. The expected reduced flow should be0.01 912/(1 .048)0.9434  
: 36.     Table 4-28. Define the parameter "margin to incipient boiling."
= 0.01 829 kg/s which is close to the NATCON-calculated value of 0.01834kg/s.Question 3636. Table 4-28. Define the parameter "margin to incipient boiling."
PUR-1 SAR                                    Appendix 2-16                        PuR-SARAppedix
PUR-1 SARAppendix 2-16PuR- SARAppedix  
                                                                                          -16Rev 2, July 23, 2015
-16Rev 2, July 23, 2015  


===Response===
===Response===
The margin to incipient boiling shown in Table 4-28 was calculated at the nominal operating power of PUR-1 (i.e., 1 kW), and it is the smallest value of the temperature difference (ToNg -Tw) over the coolant channel length in the hottest channel where Tw is cladding surfacetemperature with all hot channel factors applied, and TONB is the local onset-of-nucleate-boiling temperature.
The margin to incipient boiling shown in Table 4-28 was calculated at the nominal operating power of PUR-1 (i.e., 1 kW), and it is the smallest value of the temperature difference (ToNg -
This basically gives an idea of how far below the onset of nucleate boilingcondition the reactor is operating.
Tw) over the coolant channel length in the hottest channel where Tw is cladding surface temperature with all hot channel factors applied, and TONB is the local onset-of-nucleate-boiling temperature. This basically gives an idea of how far below the onset of nucleate boiling condition the reactor is operating. This definition can be written as an equation as follows:
This definition can be written as an equation as follows:whereT(z) = Bulk coolant temperature at axial position z in the channel heated by theplate power of PopFr EQ/N and applying the global hot channel factors forflow and Nusselt number of Fw and FhTwani(Z)  
where T(z)                 = Bulk coolant temperature at axial position z in the channel heated by the plate power of PopFr EQ/N and applying the global hot channel factors for flow and Nusselt number of Fw and Fh Twani(Z)             = Cladding surface temperature at axial position z in the channel heated by a plate power of Pop~r EQ/N and applying the global hot channel factors for flow and Nusselt number of Fw and Fh q"(z)               =   Heat flux at position z for the plate power of Pop~r EQ/N and applying the global hot channel factors for flow and Nusselt number of Fw and Fh p(z)                 = Absolute pressure in the channel at axial position z T~nop(p(z), q"(z)Fnux) = Onset of nucleate boiling temperature at absolute pressure p(z) and heat flux q"(z)Fflux Pop           = Operating power of the reactor (e.g., 1 kW for PUR-1)
= Cladding surface temperature at axial position z in the channel heated by aplate power of Pop~r EQ/N and applying the global hot channel factors forflow and Nusselt number of Fw and Fhq"(z) = Heat flux at position z for the plate power of Pop~r EQ/N and applying theglobal hot channel factors for flow and Nusselt number of Fw and Fhp(z) = Absolute pressure in the channel at axial position zT~nop(p(z),
N                   = Number of fuel plates in the core (e.g., 190 for PUR-1 LEU core)
q"(z)Fnux)  
To                   = Coolant temperature at the channel inlet Fr                  = RPEAK = Radial power factor of the plate cooled by the channel Fw            = Hot channel factor for flow in the channel EQ                  = Hot channel factor for reactor power Fh                    =Hot channel factor for Nusselt number Fflrn                =   FFILM = Hot channel factor for temperature drop across the coolant film on cladding surface EFlux                - FFLUX = Hot channel factor for heat flux FbuIk                = FBULK =         Hot channel factor for bulk coolant temperature rise in the channel PUR-1 SAR                                      Appendix 2-17                      PUR-SARAppedix
= Onset of nucleate boiling temperature at absolute pressure p(z) and heatflux q"(z)Fflux Pop = Operating power of the reactor (e.g., 1 kW for PUR-1)N = Number of fuel plates in the core (e.g., 190 for PUR-1 LEU core)To = Coolant temperature at the channel inletFr = RPEAK = Radial power factor of the plate cooled by the channelFw = Hot channel factor for flow in the channelEQ = Hot channel factor for reactor powerFh =Hot channel factor for Nusselt numberFflrn = FFILM = Hot channel factor for temperature drop across the coolant film oncladding surfaceEFlux -FFLUX = Hot channel factor for heat fluxFbuIk = FBULK = Hot channel factor for bulk coolant temperature rise in thechannelPUR-1 SARAppendix 2-17PUR- SARAppedix  
                                                                                          -17Rev 2, July 23, 2015
-17Rev 2, July 23, 2015 APPENDIX 3: FUEL SPECIFICATIONS Pages Appendix 3-2 through Appendix 3-62 are the specification document Specification forPurdue University Standard and Control Fuel Elements  
 
-Assembled for the Purdue University
APPENDIX 3: FUEL SPECIFICATIONS Pages Appendix 3-2 through Appendix 3-62 are the specification document Specification for Purdue University Standard and Control Fuel Elements - Assembled for the Purdue University Reactor, idaho NationalLaboratory, SPC-382, Rev 1, January 27, 2007..
: Reactor, idaho National Laboratory, SPC-382, Rev 1, January 27, 2007..Pages Appendix 3-63 through Appendix 3-84 are engineering drawings of the PUR-1 fueiassemblies.
Pages Appendix 3-63 through Appendix 3-84 are engineering drawings of the PUR-1 fuei assemblies.
PUR-1 SARAppendix 3-1PuR- SARAppndix3-1Rev 2, July 23, 2015 Document ID: SPC-382Revision ID: IEffective Date: 01/24/07Specification Specification for PurdueUniversity Standard andControl Fuel Elements  
PUR-1 SAR                              Appendix 3-1                    PuR-SARAppndix3-1Rev 2, July 23, 2015
-Assem bled for thePurdue University ReactorIdaho NationalLaboratory The INL is a U.S. Department of Energy National Laboratory operated by Battelle Energy Alliance.
 
PUR-1 SARAppendix 3-2FUR- SARAppndix3-2Rev  
Document ID: SPC-382 Revision ID: I Effective Date: 01/24/07 Specification Specification for Purdue University Standard and Control Fuel Elements -
: 2. July 23, 2015 INTENTIONALLY BLANKPUR-1 SARAppendix 3-3PUR- SARAppndix3-3Rev  
Assem bled for the Purdue University Reactor The INL is a U.S. Department of Energy National Laboratory operated by Battelle Energy Alliance.
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Idaho National Laboratory PUR-1 SAR                  Appendix 3-2                            FUR-SARAppndix3-2Rev
ENGIE-RNG U N SI IMWDCNRLFESHO NIERN*ELEMENTS  
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Review annually. Cutoff when Record superseded, obsolete or Uniform File                                                   Disposition                           Retention cancelled. Destroy 75 years
1ELEMENTS
: 15. Code:                   0250                 16.                 Authority: ENVl-b-4-a                   Period: after cutoff.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: ii of iiPURDUE UNIVERSITY REACTORINTENTIONALLY BLANKPUR-1 SARAppendix 3-5PUR- SARAppndix3-5Rev  
: 17. For QA Records Classification Only:                   Lifetime [-i,             Nonpermanent         LI-,           Permanent     LI Item or activity to which the QA Records apply:                                                   _____________________________
: 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Periodic Review Frequency: N/A                 Li,   5 years [], or
SPC-382STANDARD AND CONTROL FUEL Revision:
: 18. Other___________________                                                                                                                           ____
1ELEMENTS
Nuclear Engineering Building [] 400 Central Drive ta West Lafayette, IN 47907-2017 PUR-I SAR   (765) 494-5739 m Fax: (765) 494-9570 [] https:/lengineerin~dplj.N4E Rev 2. July 23, 2015
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 1 of 57PURDUE UNIVERSITY REACTOR[Purdue University Reactor [Specification  
 
[ DAR Number: 511249 [REVISION LOGRev. Date Affected Pages Revision Description 0 05/31/06 All New Document.
Form 412.09 (Rev. 09)
1 0 1/24/07 All Revised to add Program Anneal requirements and_____ ________
Ida ho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                 SPC-382 STANDARD AND CONTROL FUEL                 Revision:       1 ELEMENTS        - ASSEMBLED FOR THE         Effective Date: 01/24/07     Page: ii of ii PURDUE UNIVERSITY REACTOR INTENTIONALLY BLANK PUR-1 SAR                                Appendix 3-5                      PUR-SARAppndix3-5Rev
____________update Drawing Titles 1 4-I- + II- 4F + I.I. + I-PUR-1 SARAppendix 3-6FUR- SARAppndix3-6Rev  
: 2. July 23, 2015
: 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
 
SPC-382STANDARD AND CONTROL FUEL Revision:
Form 412.09 (Rev. 09)
1ELEMENTS
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                                       SPC-382 STANDARD AND CONTROL FUEL                                     Revision:       1 ELEMENTS - ASSEMBLED FOR THE                                   Effective Date: 01/24/07         Page: 1 of 57 PURDUE UNIVERSITY REACTOR
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 2 of 57PURDUE UNIVERSITY REACTORCONTENTS1. SUMMARY...............................................................................................
[Purdue University Reactor         [Specification                 [                 DAR Number: 511249           [
51.1 General ..............................................................................................  
REVISION LOG Rev.           Date           Affected Pages                           Revision Description 0         05/31/06                     All         New Document.
: 52. APPLICABLE CODES, PROCEDURES, AND REFERENCES......................................
1         0 1/24/07                     All         Revised to add Program Anneal requirements and
52.1 Standards, Specifications, Drawings and Attachments..........................................
_____  ________   ____________update             Drawing Titles 1                     4
52.1.1 Specifications and Standards  
          -I-                 +                     I I-                 4 F                  +                     I.
.........................................................
I.                 +                     I-PUR-1 SAR                                                    Appendix 3-6                            FUR-SARAppndix3-6Rev
52.1.2 Drawings (INL)........................................................................  
: 2. July 23, 2015
: 83. TECHNICAL REQUIREMENTS..........................................................................
 
93.1 Production Qualification..................  
Form 412.09 (Rev. 09)
.........................................................
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                                           SPC-382 STANDARD AND CONTROL FUEL                                 Revision:               1 ELEMENTS - ASSEMBLED FOR THE                                 Effective Date: 01/24/07                             Page: 2 of 57 PURDUE UNIVERSITY REACTOR CONTENTS
93.1.1 Fuel Plate Qualification:  
: 1.  
..............................................................
 
93.1.2 Fuel Element Qualification:.........................................................
==SUMMARY==
103.1.3 Requalification:
...............................................................................................                   5 1.1   General ..............................................................................................             5
......................................................................
: 2. APPLICABLE CODES, PROCEDURES, AND REFERENCES......................................                                       5 2.1   Standards, Specifications, Drawings and Attachments.......................................... 5 2.1.1       Specifications and Standards ......................................................... 5 2.1.2       Drawings (INL)........................................................................ 8
103.1.4 Operator Qualification:...........................................
: 3. TECHNICAL REQUIREMENTS.......................................................................... 9 3.1   Production Qualification..................             ......................................................... 9 3.1.1       Fuel Plate Qualification: ..............................................................             9 3.1.2       Fuel Element Qualification:.........................................................                 10
113.2 Materials
...........................................................................................
123.2.1 Fuel Bearing Plates ..................................................................
123.2.2 Aluminum Weld Filler Metal: ......................................................
123.2.3 Dummy (Non-Fueled)
Plate:........................................................
123.2.4 Material Requirements
..............................................................
133.3 Mechanical Requirements........................................................................
133.3.1 Fuel Plate Requirements
............................................................
133.3.2 Non-fueled (dummy) plates:........................................................
153.3.3 Fuel Element Requirements.........................................................
153.4 Physical Properties................................................................................
153.4.1 Fuel Plate Requirements
............................................................
153.5 Surface Condition
.................................................................................
173.5.1 Surface Defects ......................................................................
173.5.2 Cleanliness:
..........................................................................
173.5.3 Contamination:
.......................................................................
183.6 Marking............................................................................................
183.6.1 Fuel Plate Identification:
............................................................
183.6.2 Fuel Assembly Identification:.......................................................
183.6.3 Dummy Element Identification:
....................................................
193.7 Storage .............................................................................................
193.8 Fuel Element Surface Treatment
................................................................
19PUR-1 SAR Appendix 3-7 Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 3 of 57PURDUE UNIVERSITY REACTOR3.8.1............................................................................................
193.8.2............................................................................................
203.8.3............................................................................................
203.9 Graphite Reflectors and Graphite Radiation Baskets ..........................................
203.9.1 Material:
..............................................................................
203.9.2 Assembly:.............................................................................
203.9.3 Welding:
..............................................................................
203.9.4 Identification:
........................................................................
203.9.5 Dimensional Inspection:.............................................................
213.9.6 Surface Finish and Defects:
.........................................................
213.9.7 Storage:
...............................................................................
214. QUALITY ASSURANCE.................................................................................
214.1 Materials
...........................................................................................
224.2 Core Density.......................................................................................
224.3 Fuel Loading.......................................................................................
244.4 Fuel Homogeneity
................................................................................
244.5 Core Configuration................................................................................
264.6 Bond Integrity
.....................................................................................
264.6.1 Blister Anneal: .......................................................................
264.6.2 Ultrasonic Scanning:
................................................................
274.6.3 Metallographic Examination........................................................
274.7 Internal Defects ...................................................................................
274.8 Surface Finish and Defects.......................................................................
284.9 Clad-Core-Clad Dimensions.....................................................................
284.10 Cleanliness.........................................................................................
294.11 Contamination.....................................................................................
294.12 Dimensional
.......................................................................................
294.12.1 Final Dimensional Inspection.......................................................
294.13 Reactor Components and Spare Fuel Element Parts...........................................
295. PACKAGING AND SHIPPING..........................................................................
306. NOTES ......................................................................................................
30PUR-1 SAR Appendix 3-8 Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY
!Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 4 of 57PURDUE UNIVERSITY REACTOR6.1 Definitions.........................................................................................
306.2 Purchaser Tests....................................................................................
336.3 Submittals..........................................................................................
336.3.1 Preproduction:........................................................................
336.3.2 Pre-repair:.............................................................................
346.3.3 Manufacturing Schedule:
...........................................................
346.3.4 Delivery Submittals:
.................................................................
346.3.5 Fuel Plate Radiographs:.............................................................
356.3.6 Core Compact Data Sheets: .........................................................
356.3.7 Report of Production by Unapproved Process:....................................
35APPENDIX A ......................................................................................................
37APPENDIX B......................................................................................................
39FIGURES1. Purdue University Fuel Plate Sampling Procedures For Destructive Tests.......................
36PUR-1 SARAppendix 3-9PUR- SARAppndix3-9Rev
: 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 5 of 57PURDUE UNIVERSITY REACTOR1.SUMMARY 1.1 GeneralThis specification (see def.) defines the materials, components,
: testing, inspection, certain processes, quality control (see def.) requirements and acceptance criteriafor the fabrication of standard and control fuel elements (see def.) and fuelelement containers for the Purdue University Reactor at Purdue University atWest Lafayette, Indiana.2. APPLICABLE CODES, PROCEDURES, AND REFERENCES 2.1 Standards, Specifications, Drawings and Attachments The applicable portions of the following documents as defined herein, form a partof this specification.
Where there is a conflict between the documents cited andthe latest revision
: thereof, the supplier (see def.) shall notify the purchaser (see def.) of the conflict and use the latest revision in effect at the signing of thecontract, unless otherwise directed by the purchaser.
2.1 .1 Specifications and Standards National Codes and Standards ASTM E 1742-00ASTM E 1417-99MIL-C-45 662RDT F6-2TAmerican Society for TestingASTM B 209-00ASTM B 210-04ASTM B 211-00ASTM B 214-99ASTM B 221-00Standard Practice for Radiograph Examination Standard Practice for Liquid Penetrant Examination Calibration System Requirements Welding of Reactor Core Components, Sections 1,2,3 and 6and Materials (ASTM)Standard Specification for Aluminumand Aluminum-Alloy Sheet and PlateAluminum and Aluminum-Alloy DrawnSeamless TubesStandard Specification for Aluminumand Aluminum-Alloy Bar, Rod and WireStandard Test Method for Sieve Analysisof Granular Metal PowdersStandard Specification for AluminumPUR-1 SARPUR-1 SAR ~~~Appendix 3-10 2 uy2,212. July 23,2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382 5STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 6 of 5PURDUE UNIVERSITY REACTORand Aluminum-Alloy Extruded Bars,Rods, Wires, Profiles and TubesASTM B 24 1-02ASTM E 8-00ASTM E 29-93 a (1999)ASTM E 2016-99Aluminum and Aluminum-Alloy Seamless Pipe and Seamless ExtrudedTubeMethods of Tension Testing of MetallicMaterials Recommended Practice for Indicating Which Places of Figures are to beConsidered Significant in Specified Limiting ValuesStandard Specification for Industrial Woven Wire ClothAmerican Welding Society (AWS')AWS A5.10-1995 Aluminum and Aluminum AlloyWelding Rod and Bare Electrodes American National Standards Institute (ANSI)ANSI B46.1-1994 Surface TextureANSI Y14.5-1994 Dimensioning and Tolerancing forEngineering DrawingsAmerican Society of Mechanical Engineers (ASME)ASME Section V -2001,without addendumASME Section IX -2001ASME NQA- 1-1997Boiler and Pressure Vessel CodeSection VBoiler and Pressure Vessel CodeSection IXQuality Assurance Requirements forNuclear Facility Applications PUR-1 SARPUR-1 SAR ~~~Appendix 3-11 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382 5STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 7 of 5PURDUE UNIVERSITY REACTORIdaho National Laboratory (INL)TRTR- 11TRTR- 14IN-F-4-TRA STD 7022ASpecification for Low Enriched UraniumMetal in Test Reactor FuelSpecification for Reactor Grade LowEnriched Uranium Silicide Fuel PowderSpecification for Aluminum Powder forMatrix Material in Test Reactor FuelCleanliness Acceptance Levels forNuclear or Non-Nuclear ServiceComponents American Society for Nondestructive Test (ASNT)SNT-TC-lA (1996 or later) American Society For Nondestructive Testing (ASNT) Recommended PracticePUR-1 SARPUR-1 SAR ~~~Appendix 3-12 2 uy2,212. July 23,2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 8 of 57PURDUE UNIVERSITY REACTOR2.1.2 Drawings (JNL)635454635455635456635457635458635459635460635461635462635463635464635465Purdue University Test Research andTraining Reactor Graphite Reflector Assembly and Source Drive AssemblyPurdue University Test Research andTraining Reactor Standard Fuel, Partial,& Dummy Element Assemblies Purdue University Test Research andTraining Reactor Control Fuel ElementAssembly and Dummy Control FuelElement AssemblyPurdue University Test Research andTraining Reactor Fission Chamber FuelElement AssemblyPurdue University Test Research andTraining Reactor Standard FuelContainer AssemblyPurdue University Test Research andTraining Reactor Control Fuel Container AssemblyPurdue University Test Research andTraining Reactor Irradiation FacilityAssemblyPurdue University Test Research and.Training Reactor Capsule Holder andCapsule Insert Assemblies and DetailsPurdue University Test Research andTraining Reactor Graphite Container
: Assembly, and Source Drive Container AssemblyPurdue University Test Research andTraining Reactor Fuel Plate Assemblyand Dummy Fuel Plate DetailPurdue University Test Research andTraining Reactor Container TubeAssembly and DetailsPurdue University Test Research andPUR-1 SARPUR-1 SAR ~~~Appendix 3-13 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1of5ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 9of5PURDUE UNIVERSITY REACTORTraining Reactor Graphite Block DetailAnd Graphite Capsule Holder Detail635466 Purdue University Test Research andTraining Reactor Miscellaneous Details635467 Purdue University Test Research andTraining Reactor Source Drive NozzleAssembly and Source Drive Top635468 Purdue University Test Research andTraining Reactor Nozzle Preliminary Machined and Fission Chamber Top3. TECHNICAL REQUIREMENTS 3.1 Production Qualification The supplier is required to qualify the processes or portions of the process or beexempt from same by written approval of the purchaser.
In qualifcation (seedef.), only materials that comply with this specification shall be used.Qualification processes, equipment, and operator qualificationltraining programsshall be identical to those used during production (see def.). To qualify, thesupplier must demonstrate, to the satisfaction of the purchaser, that the process iscapable of producing a product, which satisfies all the requirements of thespecifications.
Assembly of production fuel elements shall not be initiated until:(1) all required data, to assure compliance with the qualification requirements, hasbeen submitted to the purchaser; (2) data and records required by Section 6.3 havebeen submitted; and (3) written approval of qualification has been received by thesupplier from the purchaser.
3.1.1 Fuel Plate Qualification:
Fuel plate (see def.) qualification shall be satisfied by supplierproduction of a minimum of two consecutively produced plate lots (seedef.), in lot quantities of 24 plates (see def.). The plates shall be madeusing low enriched uranium in the form of Silicide (see def.) powder,which have a yield of no less than 65% acceptable fuel plates meeting allapplicable requirements of this specification.
The supplier may combinethe results of two consecutive lots into a production run in determining the 65% yield requirement provided that there have been no changes inthe manufacturing (see def.) procedure (see def.) between lots whichwould require requalifcation (see def.) in accordance with Section 3.1.3.PUR-1 SARPUR-1 SAR ~~~Appendix 3-14 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 10of5PURDUE UNIVERSITY REACTORIn the event that fuel plate qualification has been performed by thesupplier meeting all the requirements of this specification during the pasttwelve months, and qualified operators are performing the fabrication, fuel plate qualification requirements listed above will be waived.Fuel plates made in development (see def.) (prior to and including qualification runs that fail to meet the 65% yield requirements) will notbe used in fabricating production fuel elements without prior approval ofthe purchaser.
3.1.2 Fuel Element Qualification:
The supplier shall fabricate 1 dummy standard fuel element assembly(see def.), which shall meet the requirements of this specification.


====3.1.3 Requalification====
====3.1.3 Requalification====
The supplier shall notify the purchaser of any proposed process change.A changed process may not be used in production until the supplier hasmet all the requirements of Section 3.1.3, submits the results and data ofthe requalification effort, and receives written approval from thepurchaser.
......................................................................            10 3.1.4       Operator Qualification:...........................................                                  11 3.2   Materials ...........................................................................................            12 3.2.1       Fuel Bearing Plates ..................................................................               12 3.2.2       Aluminum Weld Filler Metal: ......................................................                  12 3.2.3       Dummy (Non-Fueled) Plate:........................................................                  12 3.2.4       Material Requirements ..............................................................               13 3.3   Mechanical Requirements........................................................................                  13 3.3.1       Fuel Plate Requirements ............................................................               13 3.3.2       Non-fueled (dummy) plates:........................................................                  15 3.3.3       Fuel Element Requirements.........................................................                   15 3.4   Physical Properties................................................................................              15 3.4.1       Fuel Plate Requirements ............................................................ 15 3.5     Surface Condition ................................................................................. 17 3.5.1       Surface Defects ...................................................................... 17
Requalification for any fuel plate attribute to the requirements of thespecification will be required when the processes, materials, fuelloadings, equipment or equipment operators (welding and rolling) whichhave been previously qualified are changed, unless the supplier candemonstrate to the satisfaction of the purchaser by engineering explanation or proof test that such changes will have no detrimental effect on the product.Requalification for compacting, pack (see def.) assembly, and rollingmill operators can be less than qualification basis, since the procedure has already been established.
 
Candidate operators who are not qualified for compacting operations, pack assembly operations, and hot/coldrolling mill operations must demonstrate their abilities in performing theindividual operations they are assigned.
====3.5.2 Cleanliness====
An operator must qualify by processing two lots of fuel plates withminimum lot size of 24, for the operation he is assigned to qualify,before performing any production operation independently.
.......................................................................... 17
Each lot offuel plates shall be processed through final inspection, with a minimumyield rate of 90% acceptable fuel plates required for the operator to betermed qualified.
PUR-1 SARPUR-1 SAR ~~~Appendix 3-15 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 11of5PURDUE UNIVERSITY REACTORNOTE: Failure of an operator to qualify',
because of fuel piate deviations, must be based on deviations related to the operation being qualified.
The purchaser on a case-by-case basis will determine the quantities and sizes of requali~fication fuel plates selected to be destructively examined.
3.1.4 Operator Qualification:
Operator qualification will be accomplished via an approved supplierinternal qualification program for the following operations:
A. Arc meltingB. Compacting C. Pack assemblyD. Hot rollingB. Cold rollingF. Final machining.
3.1.4.1In addition to the operations specified above, the suppliershall also show evidence of the training and competency ofthose individuals who perform any of the following fuelelement fabrication and inspection activities:
A. Powder sieving,
: weighing, and testingB. Compact weighing, visual and dimensional inspection C. Fuel plate/element and component cleaningD. Fuel plate annealing operations B. Dimensional inspection of plates, elements, andsubcomponents F. Metallographic sample preparation and inspection
: 0. Visual inspection of plates, elements, andsubcomponents H. Void volume inspection I. Fluoroscope inspection of fuel platesPUR-1 SARPUR-1 SAR ~~~Appendix 3-16 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 12 of 57PURDUE UNIVERSITY REACTORJ. Radiography and inspection of fuel plate radiographs K. Ultrasonic testing and interpretation.
The individuals performing these operations shall havespecific requirements imposed on them that willdemonstrate their knowledge and ability to perform theirrespective assignments.
Documented evidence of thetraining of these individuals shall be maintained and shall bemade available to the purchaser upon request.3.2 Materials The material requirements for the components comprising the fuel element are asspecified on Drawings per Section 2.1.2 and requirements of this section.3.2.1 Fuel Bearin2 Plates3.2.1.1 Fuel Cores: The fuel cores (see def.) of the fuel plates shallbe uranium silicide powder dispersed in aluminum alloypowder which meet the requirements of IN.-F-4-TRA andTRTR- 14, per Section 2.1.1 of this specification.
3.2.1.2 Frames and Covers: Aluminum for the frames and coverplates shall conform to ASTM B209, Alloy 606 1-0. Thealuminum plate stock used for frame and cover plates shallbe certified by the supplier to contain less than 30 PPMboron, 80 PPM cadmium, and 80 PPM lithium.The subcontractor shall furnish certified physical properties and chemical analyses of ingots or plates of the 6061materials to INL.3.2.2 Aluminum Weld Filler Metal:All aluminum weld filler metal shall be ER4043 as required bySpecification AWS A5.10-1995.
3.2.3 Dummy (Non-Fueled)
Plate:Dummy (non-fueled) plates (see def.) shall be fabricated from aluminumType 6061-0, that meets the requirements of Section 3.2.1.2.PUR-1 SARPUR-1 SAR ~~~Appendix 3-17 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTSuRU UIEST- ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 13 of 573.2.4 Material Reqiuirements All material used or contained in the product shall comply with all therequirements of this specification and Drawings per Section 2.1.2 unlessexempted by written document by the purchaser.
3.3 Mechanical Requirements 3.3.1 Fuel Plate Requirements 3.3.1.1 Fabrication:
The supplier shall furnish the details of his fuelplate rolling schedule and component cleaning process tothe purchaser for approval prior to use in production per 6.3.1.Compacting details shall include silicide
-aluminumcompacting pressure and compacting press dwell time.After hot rolling, each fuel plate shall be blister annealed perSection 4.6.1 and then cold rolled to final thickness at roomtemperature.
After cold rolling operation, the fuel platesshall be subjected to program annealing.
The rollingschedule shall contain, at a minimum, the following:
A. Nominal plate reduction B. Minimum number of hot roll passesC. Nominal inter-pass reduction and target thickness D. Hot rolling furnace temperature E. Preheat time for all hot roll passesF. Final hot roll plate thickness G. Type and frequency of roll lubricant utilizedH. Nominal cold roll reduction.
I. Final cold roll thickness.
Fuel plate cladding (see def.) thickness required bySection 3.3.1.4 and fuel core homogeneity requirements ofSection 4.4 are independent requirements that must be met.PUR-I SARAppendix 3-18PUR- SARAppedix
-152. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 14 of 57PURDUE UNIVERSITY REACTOR3.3.1.2 Core Configuration:
No fuel particles are allowed within thefuel free zones located at the ends of the plates as shown onDrawing 635463.The nominally unfueled area of each fuel plate as defined byDrawing 635463 may contain random fuel particles definedas flaking and limited in size, location, and spacing per thisSection, as determined by Section 4.5.The presence of fuel particles detected between themaximum fuel core outline and fuel plate edges and ends isallowed provided they do not violate the following restrictions:
-One or more fuel particles, which fit in a rectangle whosearea is not more than 4x1 0-4 in2 is acceptable AND-The fuel particle(s) are no closer than 0.080 in. to anyother particle edge to edgeAND-No particle is closer to the plate edge or end than themajor dimension of the particle.
Stray fuel particles (see def.) that violate the aboverequirements may be removed from fuel plate edges byfiling, provided the following:
-The filed out area is no deeper into the edge of the platethan 0.050 in., no longer than 0.250 in.ANDEach filed area is at least 1.0 in. apart3.3.1.3Filing of fuel plate ends, for the removal of stray particles, isnot allowed, unless previously approved by the purchaser.
Internal Defects and Bond Integrity:
Metallurgical bond, asdetermined by Section 4.6 is required at interface areas ofthe finished fuel plates, specifically fuel core-to-clad andclad-to-frame.
The presence of grain growth across the fuelPUR-1 SARPUR-1 SAR ~~~Appendix 3-19 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 15 of 57PURDUE UNIVERSITY REACTORmatrix-cladding interface and across the aluminumframe-cladding interface of at least 50% is required.
Fuelcore defects in excess of 0.06 in. in any dimension asdetermined by Section 4.7 are not allowed.3.3.1.4 Cladding Thickness:
During production, all plates will besubjected to UT mmn-clad inspection.
The standard will becalibrated at the nominal 0.008-inch scan depth. The gagewill then be adjusted to a 0.010 inch scanning depth and thefuel plates will be scanned at 0.0 10 inch. Fuel plate UTtraces, which display mmi-clad indications at the 0.010-inch depth, shall be visually compared with the 0.008-inch Standard trace. Fuel plates for which the UT reports show acomparable density of indications, or worse, than theindications displayed on the standard UT report areunacceptable.
Fuel plates, which fail the 0.010-inch UTscan, shall be rescanned at 0.008 inch. Only fuel plateswhich are acceptable when rescanned at 0.008 inch shall besubmitted to the Purchaser and User for evaluation.
3.3.2 Non-fueled (dummy) plates:The supplier shall use a cold rolling method to obtain plate thickness.
Non-fueled (dummy) plates shall be subjected to program anneal.3.3.3 Fuel Element Reqiuirements 3.3.3.1 Weldinp:
All welding shall be performed using procedures and welding personnel qualified in accordance with ASMESection IX or the criteria defined in Appendix B. Qualityacceptance of production welds shall be in accordance withAppendix B, Section 5.3.4 Physical Properties Fuel plates shall have a core of U3 Si2 and aluminum and completed fuel platesand fuel elements shall have fuel loadings per Sections 3.4.1.2, and 3.4.1.5.3.4.1 Fuel Plate Requirements 3.4.1.1 Fuel Core: The fuel core shall consist of 19.75 "0.2 weight% enriched uranium silicide powder dispersed in aluminumpowder. The uranium silicide powder shall be -100, +325U.S. standard mesh particles.  
: However, a blend mayPUR-1 SARPUR-1 SAR ~~~Appendix 3-20 2 uy2,212. July 23,2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 16 of 57PURDUE UNIVERSITY REACTORcontain up to 35 weight percent of -325 U.S. standard meshparticles.
Any powder particles greater than 100 meshparticles shall be reground such that they will go thru the100 mesh sieve. The fuel core shall be fabricated according to standard powder-metallurgical and roll-bonding techniques.
The supplier shall provide to the purchaser, awritten procedure for pack assembly and the initial rollingstep which describes the method used to prevent excessive oxidation that causes non-bond of fuel core to the cladding.
3.4.1.2 Fuel Loading:
By using the approved supplier's method ofassigning U-23 5 content, per a detailed description as to theweighing procedure by which the supplier proposes toassign fuel plate U-235 content.
Each fuel plate shallcontain 12.5 "0.35 grams U-235. The weight of each coreshall be measured and recorded to within 0.01 gram U-235based upon weight of the final compact and chemical andisotopic analysis of the constituents.
3.4.1.3 Fuel Homogeneity:
Fuel homogeneity requirements arelocated in section 4.4.3.4.1.4 Void Volume: In the qualification
: process, all fuel platesshall be inspected for void volume using the methoddescribed in Section 4.2. The percent voids in the fuel coresof all fuel plates shall be determined by the inspection procedure developed by the supplier.
The percent voids inthe fuel cores shall be at least 3.0% and not more than11.0%.3.4.1.5 Fuel Element Requirements 3.4.1.6 Fuel Loading:
Assigned fuel loading for each fuel elementshall be 175.006-4.90 grams of U-235. Each Control FuelElement shall contain 100 grams of U-235. Controllimits for the method used to measure this weight areestablished at the 95% confidence level for a significant population of measurements of a particular standard.
TheU-235 enrichment shall be 19.75 '-0.2 weight % of totaluranium per specification TRTR- 11.PUR-1 SARPUR-1 SAR ~~Appendix 3-212.Jl3,01
: 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 17of5PURDUE UNIVERSITY REACTOR3.5 Surface Condition Fuel plates and completed fuel elements must comply with the surface condition requirements of Section 3.5.1, 3.5.2, and 3.5.3 and drawings of Section 2.1.2, perANSI B46. 1. Sanding, or any other finishing procedure that will smear thealuminum
: surface, will not be allowed on fuel plates unless approved by thepurchaser.
3.5.1 Surface Defects3.5.1.1 Compliance with surface finish and defect requirements shall be established by 100% visual inspection of all fuelplates and elements.
The surface of the finished fuel platesshall be smooth and free of gouges, scratches, pits, orremoval of metal in excess of 0.005 inch in depth. Dents inthe fuel plate shall not exceed 0.0 12 inch in depth or 0.25inch in diameter.
If there is evidence of dogboning in theplates, surface defects in the dogbone (see def.) area shallnot exceed 0.003 inch in depth. No degradation of the fuelplates beyond these limits shall be permitted.
3.5.1.2 Fuel Plates shall be free of stringiness, scabs, or cracks.Surface finish shall be as required by Drawing 635463.Compliance with requirements of this section shall beaccomplished by visual inspection of all fuel plates and fuelelements.
3.5.1.3 Defects on fuel plate edges or ends are permissible providedthey are evaluated and acceptable to the requirements ofParagraph 3.3.1.2.3.5.1.4 Compliance with surface finish and defect requirements shall be established by 100% visual inspection of all fuelelement containers.
Fuel element containers shall be free ofsurface defects such as pits, dents, or scratches in excess of0.0 10 inch in depth and 0.12 inch in diameter or equivalent area.3.5.2 Cleanliness:
The suppliers fabrication,
: assembly, and storage areas used for theproduction of Purdue University fuel elements and/or components shallconform to the requirements of "controlled work area" (see def.) asdefined in Paragraph 1.3.6 of INL Standard 7022A. Cleanliness shall bePUR-1 SARPUR-1 SAR ~~~Appendix 3-22 2 uy2,212. July 23, 2015 Form 4l2.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
SPC-382STANDARD AND CONTROL FUEL Revision:
1ELEMENTS
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 18 of 57PURDUE UNIVERSITY REACTORin compliance with INL Standard 7022A, Paragraphs 1.1, 1.2.3, 3.1, 3.2-b, d, i, 3.3 -d, e, 4.1.3, 4.2, and 4.3. Freon shall not be used to clean fuelelements or components.
As determined by Section 4.10 of this specification, there shall be noforeign materials on the finished fuel plates or surfaces of the finishedfuel elements.
All oil, metal chips, turnings, dusts, abrasives and spatter,scale, and other particles shall be removed from the fuel surfaces byprocedures which assure that the minimum cladding thickness has notbeen violated.
All components shall be cleaned by a method approved bythe purchaser.


====3.5.3 Contamination====
====3.5.3 Contamination====
The surfaces of each fuel plate shall be counted or smeared and countedfor alpha-beta-gamma contamination.
....................................................................... 18 3.6    Marking............................................................................................ 18 3.6.1      Fuel Plate Identification: ............................................................            18 3.6.2      Fuel Assembly Identification:.......................................................                18 3.6.3      Dummy Element Identification: ....................................................                  19 3.7    Storage .............................................................................................          19 3.8    Fuel Element Surface Treatment ................................................................ 19 PUR-1 SAR                                                  Appendix 3-7                                              Rev 2. July 23, 2015
The alpha count shall be less thanfive dpm per 100 cm2, and the beta-gamma count shall be less than200 dpm per 100 cm2.Each fuel element shall be smeared and counted for radioactive contamination.
 
The alpha count shall be less than five dpm per 100 cm2,and the beta-gamma count shall be less than 200 dpm per 100 cm23.6 MarkingNOTE: All/fuel plates, fuel assemblies, and fuel element containers will bemarked per this section.3.6.1 Fuel Plate Identification:
Form 412.09 (Rev. 09)
Each finished fuel plate shall be identified, as shown onDrawing 635463, by a combination of numbers and/or letters that willmaintain positive identification relative to the complete traceability tothe supplier fabrication
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                                      SPC-382 STANDARD AND CONTROL FUEL                                  Revision:            1 ELEMENTS        - ASSEMBLED FOR THE                          Effective Date:      01/24/07                Page: 3 of 57 PURDUE UNIVERSITY REACTOR 3.8.1............................................................................................      19 3.8.2............................................................................................      20 3.8.3............................................................................................      20 3.9      Graphite Reflectors and Graphite Radiation Baskets ..........................................          20
: history, including the basic material lots, heat ormetal, manufacturing cycle, and quality control phases. Theidentification number shall be stamped, etched or vibro-peened at thelocation specified by Drawing 635463. The depth of the identification characters shall not exceed 0.010 in.3.6.2 Fuel Assembly Identification:
 
rEach fuel assembly shall have an identifying number such as 07-XX (07signifying year of fabrication).
====3.9.1 Material====
The number shall be placed on thecontainer assembly as shown on Drawings 635455, 635456 and 635457.PUR-I EARPUR-l SAR ~~~Appendix 3-23 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
.............................................................................. 20 3.9.2      Assembly:.............................................................................      20
SPC-382STANDARD AND CONTROL FUEL Revision:
 
1ELEMENTS
====3.9.3 Welding====
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 19 of 57PURDUE UNIVERSITY REACTORThe identification shall be stamped or entered by a method approved bythe purchaser, with two inch block characters not in excess of 0.010inches in depth. Standard assemblies should be labeled:
..............................................................................      20
E2, F2, G2,H2, F3, H3, E4, F4, G4, H4, F5, H5. Control assemblies should belabeled:
 
E3, G3, and E5. The fission chamber assembly should belabeled as G5. The source assembly shall be labeled as C3. The spareStandard Assemblies should be labeled:
====3.9.4 Identification====
SP-1, SP-2, SP-3. The spareControl Assembly should be labeled as SP-4.3.6.3 Dummy Element Identification:
........................................................................ 20 3.9.5      Dimensional Inspection:.............................................................        21 3.9.6      Surface Finish and Defects: .........................................................        21
The dummy standard fuel element assembly shall have the identifyring number DUM-1. The number shall be placed on the container assemblyas shown on Drawing 635455. The identification shall be stamped orentered by a method approved by the purchaser, with two inch blockcharacters not in excess of 0.010 inches in depth.3.7 StorageAll fuel plates, fuel assemblies, and fuel element containers that have receivedfinal cleaning per Section 3.5.2 shall be protected in clean polyethylene containers or other containers approved by the purchaser while (1) awaiting final assembly, (2) being transferred into or being maintained in storage, or (3) being prepared forpackaging or shipment.
 
Any material exposed to contamination shall bereinspected to the requirements of Section 3.5.3.8 Fuel Element Surface Treatment If boehnmite treatment is required during fuel element fabrication, the following shall apply. After fuel elements are assembled and inspected they shall besubjected to an environment that will cause an evenly distributed boehmite layerof 0.00006 to 0.0003 in. thickness (averaged over the surface using eddy currentinstrumentation) to form on all surfaces of the entire assembly.
====3.9.7 Storage====
The treatment process shall be performed under controlled conditions, which shall require thesupplier to maintain a record of the thermal history of the autoclave.
............................................................................... 21
The recordsshall include heat charts of recorded time and temperature.
: 4. QUALITY ASSURANCE.................................................................................              21 4.1    Materials ........................................................................................... 22 4.2      Core Density....................................................................................... 22 4.3    Fuel Loading....................................................................................... 24 4.4    Fuel Homogeneity ................................................................................ 24 4.5      Core Configuration................................................................................      26 4.6    Bond Integrity ..................................................................................... 26 4.6.1      Blister Anneal: .......................................................................      26 4.6.2      Ultrasonic Scanning: ................................................................      27 4.6.3      Metallographic Examination........................................................          27 4.7    Internal Defects ................................................................................... 27 4.8      Surface Finish and Defects....................................................................... 28 4.9      Clad-Core-Clad Dimensions..................................................................... 28 4.10    Cleanliness......................................................................................... 29 4.11    Contamination..................................................................................... 29 4.12    Dimensional ....................................................................................... 29 4.12.1    Final Dimensional Inspection....................................................... 29 4.13    Reactor Components and Spare Fuel Element Parts........................................... 29
Documented evidenceof the controls placed on the autoclave shall be maintained by the supplier.
: 5. PACKAGING AND SHIPPING.......................................................................... 30
3.8.1 After the boehmite process has been qualified, one fuel element fromevery 2n autoclave run shall be inspected following a procedure approved by the Purchaser.
: 6. NOTES ...................................................................................................... 30 PUR-1 SAR                                                Appendix 3-8                                        Rev 2. July 23, 2015
PUR-1 SARPUR-1 SAR ~~~Appendix 3-24 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
 
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
Form 412.09 (Rev. 09)
1ELEMENTS
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY !Identifier:                                      SPC-382 STANDARD AND CONTROL FUEL                                Revision:            1 ELEMENTS - ASSEMBLED FOR THE                                Effective Date: 01/24/07                    Page: 4 of 57 PURDUE UNIVERSITY REACTOR 6.1    Definitions......................................................................................... 30 6.2    Purchaser Tests.................................................................................... 33 6.3    Submittals.......................................................................................... 33 6.3.1      Preproduction:........................................................................      33 6.3.2      Pre-repair:............................................................................. 34 6.3.3      Manufacturing Schedule: ...........................................................        34 6.3.4      Delivery Submittals: .................................................................      34 6.3.5      Fuel Plate Radiographs:.............................................................        35 6.3.6      Core Compact Data Sheets: .........................................................        35 6.3.7      Report of Production by Unapproved Process:....................................            35 APPENDIX A ...................................................................................................... 37 APPENDIX B...................................................................................................... 39 FIGURES
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 20of5PURDUE UNIVERSITY REACTOR3.8.2 Each fuel element shall have a corresponding aluminum plate coupon,made from fuel plate end crops, placed near the fuel element during theboehmite formation process.
: 1. Purdue University Fuel Plate Sampling Procedures For Destructive Tests....................... 36 PUR-1 SAR                                              Appendix 3-9                                      PUR-SARAppndix3-9Rev
The aluminum plate coupon shall besubjected to the same environment as the fuel elements and each couponmeasured for boehmite thickness.
: 2. July 23, 2015
3.8.3 Fuel elements and aluminum plate coupons subjected to the boehmiteformation process must be carefully handled to preclude scratches, dents,and gouges that would cause removal of boehmite.
 
3.9 Graphite Reflectors and Graphite Radiation BasketsGraphite reflector assemblies (see def.) and irradiation facility assemblies (seedef.) shall be fabricated as per requirements contained in this section and indrawings 635454, 635460, 635461, and 635465.3.9.1 Material:
Form 412.09 (Rev. 09)
All materials used shall comply with all the requirements of thisspecification and applicable drawings.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                            SPC-382 STANDARD AND CONTROL FUEL                          Revision:        1 ELEMENTS - ASSEMBLED FOR THE                          Effective Date:  01/24/07          Page: 5 of 57 PURDUE UNIVERSITY REACTOR 1.
 
==SUMMARY==
 
1.1    General This specification (see def.) defines the materials, components, testing, inspection, certain processes, quality control (see def.) requirements and acceptance criteria for the fabrication of standard and controlfuel elements (see def.) and fuel element containers for the Purdue University Reactor at Purdue University at West Lafayette, Indiana.
: 2.      APPLICABLE CODES, PROCEDURES, AND REFERENCES 2.1    Standards, Specifications, Drawings and Attachments The applicable portions of the following documents as defined herein, form a part of this specification. Where there is a conflict between the documents cited and the latest revision thereof, the supplier (see def.) shall notify the purchaser (see def.) of the conflict and use the latest revision in effect at the signing of the contract, unless otherwise directed by the purchaser.
2.1 .1    Specifications and Standards National Codes and Standards ASTM E 1742-00                    Standard Practice for Radiograph Examination ASTM E 1417-99                    Standard Practice for Liquid Penetrant Examination MIL-C-45 662                      Calibration System Requirements RDT F6-2T                        Welding of Reactor Core Components, Sections 1,2,3 and 6 American Society    for Testing and Materials (ASTM)
ASTM B 209-00                    Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate ASTM B 210-04                    Aluminum and Aluminum-Alloy Drawn Seamless Tubes ASTM B 211-00                    Standard Specification for Aluminum and Aluminum-Alloy Bar, Rod and Wire ASTM B 214-99                    Standard Test Method for Sieve Analysis of Granular Metal Powders ASTM B 221-00                    Standard Specification for Aluminum PUR-1 SAR                                          SAR ~~~Appendix PUR-1  3-10                                  2  uy2,21
: 2. July 23,2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382                            5 STANDARD AND CONTROL FUEL                        Revision:      1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07          Page: 6 of 5 PURDUE UNIVERSITY REACTOR and Aluminum-Alloy Extruded Bars, Rods, Wires, Profiles and Tubes ASTM B 24 1-02                  Aluminum and Aluminum-Alloy Seamless Pipe and Seamless Extruded Tube ASTM E 8-00                      Methods of Tension Testing of Metallic Materials ASTM E 29-93 a (1999)            Recommended Practice for Indicating Which Places of Figures are to be Considered Significant in Specified Limiting Values ASTM E 2016-99                  Standard Specification for Industrial Woven Wire Cloth American Welding Society (AWS')
AWS A5.10-1995                  Aluminum and Aluminum Alloy Welding Rod and Bare Electrodes American National Standards Institute (ANSI)
ANSI B46.1-1994                  Surface Texture ANSI Y14.5-1994                  Dimensioning and Tolerancing for Engineering Drawings American Society of Mechanical Engineers (ASME)
ASME Section V - 2001,          Boiler and Pressure Vessel Code without addendum                Section V ASME Section IX - 2001          Boiler and Pressure Vessel Code Section IX ASME NQA- 1-1997                Quality Assurance Requirements for Nuclear Facility Applications PUR-1 SAR                                    ~~~Appendix PUR-1 SAR        3-11                                22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                        SPC-382                        5 STANDARD AND CONTROL FUEL                      Revision:        1 ELEMENTS - ASSEMBLED FOR THE                    Effective Date: 01/24/07          Page: 7 of 5 PURDUE UNIVERSITY REACTOR Idaho National Laboratory (INL)
TRTR- 11                      Specification for Low Enriched Uranium Metal in Test Reactor Fuel TRTR- 14                      Specification for Reactor Grade Low Enriched Uranium Silicide Fuel Powder IN-F-4-TRA                    Specification for Aluminum Powder for Matrix Material in Test Reactor Fuel STD 7022A                    Cleanliness Acceptance Levels for Nuclear or Non-Nuclear Service Components American Society for Nondestructive Test (ASNT)
SNT-TC-lA (1996 or later)    American Society For Nondestructive Testing (ASNT) Recommended Practice PUR-1 SAR                                      SAR ~~~Appendix PUR-1  3-12                                2  uy2,21
: 2. July 23,2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:              SPC-382 STANDARD AND CONTROL FUEL              Revision:      1 ELEMENTS - ASSEMBLED FOR THE            Effective Date: 01/24/07          Page: 8 of 57 PURDUE UNIVERSITY REACTOR 2.1.2    Drawings (JNL) 635454                Purdue University Test Research and Training Reactor Graphite Reflector Assembly and Source Drive Assembly 635455                Purdue University Test Research and Training Reactor Standard Fuel, Partial,
                                              & Dummy Element Assemblies 635456                Purdue University Test Research and Training Reactor Control Fuel Element Assembly and Dummy Control Fuel Element Assembly 635457                Purdue University Test Research and Training Reactor Fission Chamber Fuel Element Assembly 635458                Purdue University Test Research and Training Reactor Standard Fuel Container Assembly 635459                Purdue University Test Research and Training Reactor Control Fuel Container Assembly 635460                Purdue University Test Research and Training Reactor Irradiation Facility Assembly 635461                Purdue University Test Research and.
Training Reactor Capsule Holder and Capsule Insert Assemblies and Details 635462                Purdue University Test Research and Training Reactor Graphite Container Assembly, and Source Drive Container Assembly 635463                Purdue University Test Research and Training Reactor Fuel Plate Assembly and Dummy Fuel Plate Detail 635464                Purdue University Test Research and Training Reactor Container Tube Assembly and Details 635465                Purdue University Test Research and PUR-1 SAR                              SAR ~~~Appendix PUR-1  3-13                                22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                                SPC-382 STANDARD AND CONTROL FUEL                              Revision:      1of5 ELEMENTS - ASSEMBLED FOR THE                              Effective Date: 01/24/07        Page: 9of5 PURDUE UNIVERSITY REACTOR Training Reactor Graphite Block Detail And Graphite Capsule Holder Detail 635466                              Purdue University Test Research and Training Reactor Miscellaneous Details 635467                                Purdue University Test Research and Training Reactor Source Drive Nozzle Assembly and Source Drive Top 635468                                Purdue University Test Research and Training Reactor Nozzle Preliminary Machined and Fission Chamber Top
: 3.      TECHNICAL REQUIREMENTS 3.1    Production Qualification The supplier is required to qualify the processes or portions of the process or be exempt from same by written approval of the purchaser. In qualifcation (see def.), only materials that comply with this specification shall be used.
Qualification processes, equipment, and operator qualificationltraining programs shall be identical to those used during production (see def.). To qualify, the supplier must demonstrate, to the satisfaction of the purchaser, that the process is capable of producing a product, which satisfies all the requirements of the specifications. Assembly of production fuel elements shall not be initiated until:
(1) all required data, to assure compliance with the qualification requirements, has been submitted to the purchaser; (2) data and records required by Section 6.3 have been submitted; and (3) written approval of qualification has been received by the supplier from the purchaser.
3.1.1    Fuel Plate Qualification:
Fuelplate (see def.) qualification shall be satisfied by supplier production of a minimum of two consecutively produced plate lots (see def.), in lot quantities of 24 plates (see def.). The plates shall be made using low enriched uranium in the form of Silicide (see def.) powder, which have a yield of no less than 65% acceptable fuel plates meeting all applicable requirements of this specification. The supplier may combine the results of two consecutive lots into a production run in determining the 65% yield requirement provided that there have been no changes in the manufacturing (see def.) procedure (see def.) between lots which would require requalifcation(see def.) in accordance with Section 3.1.3.
PUR-1 SAR                                          ~~~Appendix PUR-1 SAR        3-14                              22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382of5 STANDARD AND CONTROL FUEL                          Revision:      1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07          Page: 10of5 PURDUE UNIVERSITY          REACTOR In the event that fuel plate qualification has been performed by the supplier meeting all the requirements of this specification during the past twelve months, and qualified operators are performing the fabrication, fuel plate qualification requirements listed above will be waived.
Fuel plates made in development (see def.) (prior to and including qualification runs that fail to meet the 65% yield requirements) will not be used in fabricating production fuel elements without prior approval of the purchaser.
3.1.2    Fuel Element Qualification:
The supplier shall fabricate 1 dummy standardfuel element assembly (see def.), which shall meet the requirements of this specification.
 
====3.1.3 Requalification====
The supplier shall notify the purchaser of any proposed process change.
A changed process may not be used in production until the supplier has met all the requirements of Section 3.1.3, submits the results and data of the requalification effort, and receives written approval from the purchaser.
Requalification for any fuel plate attribute to the requirements of the specification will be required when the processes, materials, fuel loadings, equipment or equipment operators (welding and rolling) which have been previously qualified are changed, unless the supplier can demonstrate to the satisfaction of the purchaser by engineering explanation or proof test that such changes will have no detrimental effect on the product.
Requalification for compacting, pack (see def.) assembly, and rolling mill operators can be less than qualification basis, since the procedure has already been established. Candidate operators who are not qualified for compacting operations, pack assembly operations, and hot/cold rolling mill operations must demonstrate their abilities in performing the individual operations they are assigned.
An operator must qualify by processing two lots of fuel plates with minimum lot size of 24, for the operation he is assigned to qualify, before performing any production operation independently. Each lot of fuel plates shall be processed through final inspection, with a minimum yield rate of 90% acceptable fuel plates required for the operator to be termed qualified.
PUR-1 SAR                                        SAR ~~~Appendix PUR-1    3-15                                22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                              SPC-382of5 STANDARD AND CONTROL FUEL                              Revision:      1 ELEMENTS - ASSEMBLED FOR THE                            Effective Date: 01/24/07    Page: 11of5 PURDUE UNIVERSITY REACTOR NOTE:        Failure of an operatorto qualify', because offuel piate deviations, must be based on deviations related to the operation being qualified.
The purchaser on a case-by-case basis will determine the quantities and sizes of requali~ficationfuel plates selected to be destructively examined.
3.1.4    Operator Qualification:
Operator qualification will be accomplished via an approved supplier internal qualification program for the following operations:
A.      Arc melting B.      Compacting C.      Pack assembly D.      Hot rolling B.      Cold rolling F.      Final machining.
3.1.4.1      In addition to the operations specified above, the supplier shall also show evidence of the training and competency of those individuals who perform any of the following fuel element fabrication and inspection activities:
A.      Powder sieving, weighing, and testing B.      Compact weighing, visual and dimensional inspection C.      Fuel plate/element and component cleaning D.      Fuel plate annealing operations B.      Dimensional inspection of plates, elements, and subcomponents F.      Metallographic sample preparation and inspection
: 0.      Visual inspection of plates, elements, and subcomponents H.      Void volume inspection I.      Fluoroscope inspection of fuel plates PUR-1 SAR                                        ~~~Appendix PUR-1 SAR        3-16                            2  uy2,21
: 2. July 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382 STANDARD AND CONTROL FUEL                          Revision:      1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07          Page: 12 of 57 PURDUE UNIVERSITY REACTOR J.      Radiography and inspection of fuel plate radiographs K.      Ultrasonic testing and interpretation.
The individuals performing these operations shall have specific requirements imposed on them that will demonstrate their knowledge and ability to perform their respective assignments. Documented evidence of the training of these individuals shall be maintained and shall be made available to the purchaser upon request.
3.2    Materials The material requirements for the components comprising the fuel element are as specified on Drawings per Section 2.1.2 and requirements of this section.
3.2.1    Fuel Bearin2 Plates 3.2.1.1      Fuel Cores: The fuel cores (see def.) of the fuel plates shall be uranium silicide powder dispersed in aluminum alloy powder which meet the requirements of IN.-F-4-TRA and TRTR- 14, per Section 2.1.1 of this specification.
3.2.1.2      Frames and Covers: Aluminum for the frames and cover plates shall conform to ASTM B209, Alloy 606 1-0. The aluminum plate stock used for frame and cover plates shall be certified by the supplier to contain less than 30 PPM boron, 80 PPM cadmium, and 80 PPM lithium.
The subcontractor shall furnish certified physical properties and chemical analyses of ingots or plates of the 6061 materials to INL.
3.2.2  Aluminum Weld Filler Metal:
All aluminum weld filler metal shall be ER4043 as required by Specification AWS A5.10-1995.
3.2.3  Dummy (Non-Fueled) Plate:
Dummy (non-fueled) plates (see def.) shall be fabricated from aluminum Type 6061-0, that meets the requirements of Section 3.2.1.2.
PUR-1 SAR                                          SAR ~~~Appendix PUR-1  3-17                                2  uy2,21
: 2. July 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382 STANDARD AND CONTROL FUEL                          Revision:        1 ELEMENTSuRU UIEST-ASSEMBLEDRECoFOR THE                Effective Date: 01/24/07          Page: 13 of 57 3.2.4  Material Reqiuirements All material used or contained in the product shall comply with all the requirements of this specification and Drawings per Section 2.1.2 unless exempted by written document by the purchaser.
3.3    Mechanical Requirements 3.3.1  Fuel Plate Requirements 3.3.1.1      Fabrication: The supplier shall furnish the details of his fuel plate rolling schedule and component cleaning process to the purchaser for approval prior to use in production per 6.3.1.
Compacting details shall include silicide - aluminum compacting pressure and compacting press dwell time.
After hot rolling, each fuel plate shall be blister annealed per Section 4.6.1 and then cold rolled to final thickness at room temperature. After cold rolling operation, the fuel plates shall be subjected to program annealing. The rolling schedule shall contain, at a minimum, the following:
A.      Nominal plate reduction B.      Minimum number of hot roll passes C.      Nominal inter-pass reduction and target thickness D.      Hot rolling furnace temperature E.      Preheat time for all hot roll passes F.      Final hot roll plate thickness G.      Type and frequency of roll lubricant utilized H.      Nominal cold roll reduction.
I.      Final cold roll thickness.
Fuel plate cladding (see def.) thickness required by Section 3.3.1.4 and fuel core homogeneity requirements of Section 4.4 are independent requirements that must be met.
PUR-I SAR                                        Appendix 3-18                                PUR-SARAppedix July -152.
23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382 STANDARD AND CONTROL FUEL                      Revision:          1 ELEMENTS - ASSEMBLED FOR THE                    Effective Date: 01/24/07              Page: 14 of 57 PURDUE UNIVERSITY REACTOR 3.3.1.2 Core Configuration: No fuel particles are allowed within the fuel free zones located at the ends of the plates as shown on Drawing 635463.
The nominally unfueled area of each fuel plate as defined by Drawing 635463 may contain random fuel particles defined as flaking and limited in size, location, and spacing per this Section, as determined by Section 4.5.
The presence of fuel particles detected between the maximum fuel core outline and fuel plate edges and ends is allowed provided they do not violate the following restrictions:
                                    -  One or more fuel particles, which fit in a rectangle whose area is not more than 4x1 0-4 in2 is acceptable AND
                                    -  The fuel particle(s) are no closer than 0.080 in. to any other particle edge to edge AND
                                    -  No particle is closer to the plate edge or end than the major dimension of the particle.
Stray fuel particles (see def.) that violate the above requirements may be removed from fuel plate edges by filing, provided the following:
                                    -  The filed out area is no deeper into the edge of the plate than 0.050 in., no longer than 0.250 in.
AND Each filed area is at least 1.0 in. apart Filing of fuel plate ends, for the removal of stray particles, is not allowed, unless previously approved by the purchaser.
3.3.1.3 Internal Defects and Bond Integrity: Metallurgical bond, as determined by Section 4.6 is required at interface areas of the finished fuel plates, specifically fuel core-to-clad and clad-to-frame. The presence of grain growth across the fuel PUR-1 SAR                                    SAR ~~~Appendix PUR-1    3-19                                    22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382 STANDARD AND CONTROL FUEL                        Revision:        1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07          Page: 15 of 57 PURDUE UNIVERSITY REACTOR matrix-cladding interface and across the aluminum frame-cladding interface of at least 50% is required. Fuel core defects in excess of 0.06 in. in any dimension as determined by Section 4.7 are not allowed.
3.3.1.4      Cladding Thickness: During production, all plates will be subjected to UT mmn-clad inspection. The standard will be calibrated at the nominal 0.008-inch scan depth. The gage will then be adjusted to a 0.010 inch scanning depth and the fuel plates will be scanned at 0.0 10 inch. Fuel plate UT traces, which display mmi-clad indications at the 0.010-inch depth, shall be visually compared with the 0.008-inch Standard trace. Fuel plates for which the UT reports show a comparable density of indications, or worse, than the indications displayed on the standard UT report are unacceptable. Fuel plates, which fail the 0.010-inch UT scan, shall be rescanned at 0.008 inch. Only fuel plates which are acceptable when rescanned at 0.008 inch shall be submitted to the Purchaser and User for evaluation.
3.3.2    Non-fueled (dummy) plates:
The supplier shall use a cold rolling method to obtain plate thickness.
Non-fueled (dummy) plates shall be subjected to program anneal.
3.3.3    Fuel Element Reqiuirements 3.3.3.1    Weldinp: All welding shall be performed using procedures and welding personnel qualified in accordance with ASME Section IX or the criteria defined in Appendix B. Quality acceptance of production welds shall be in accordance with Appendix B, Section 5.
3.4    Physical Properties Fuel plates shall have a core of U3 Si2 and aluminum and completed fuel plates and fuel elements shall have fuel loadings per Sections 3.4.1.2, and 3.4.1.5.
3.4.1    Fuel Plate Requirements 3.4.1.1    Fuel Core: The fuel core shall consist of 19.75 "0.2 weight
                                    % enriched uranium silicide powder dispersed in aluminum powder. The uranium silicide powder shall be -100, +325 U.S. standard mesh particles. However, a blend may PUR-1 SAR                                        SAR ~~~Appendix PUR-1  3-20                                22. July uy2,21 23,2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                      SPC-382 STANDARD AND CONTROL FUEL                    Revision:      1 ELEMENTS - ASSEMBLED FOR THE                    Effective Date: 01/24/07        Page: 16 of 57 PURDUE UNIVERSITY REACTOR contain up to 35 weight percent of -325 U.S. standard mesh particles. Any powder particles greater than 100 mesh particles shall be reground such that they will go thru the 100 mesh sieve. The fuel core shall be fabricated according to standard powder-metallurgical and roll-bonding techniques. The supplier shall provide to the purchaser, a written procedure for pack assembly and the initial rolling step which describes the method used to prevent excessive oxidation that causes non-bond of fuel core to the cladding.
3.4.1.2 Fuel Loading: By using the approved supplier's method of assigning U-23 5 content, per a detailed description as to the weighing procedure by which the supplier proposes to assign fuel plate U-235 content. Each fuel plate shall contain 12.5 "0.35 grams U-235. The weight of each core shall be measured and recorded to within 0.01 gram U-235 based upon weight of the final compact and chemical and isotopic analysis of the constituents.
3.4.1.3 Fuel Homogeneity: Fuel homogeneity requirements are located in section 4.4.
3.4.1.4 Void Volume: In the qualification process, all fuel plates shall be inspected for void volume using the method described in Section 4.2. The percent voids in the fuel cores of all fuel plates shall be determined by the inspection procedure developed by the supplier. The percent voids in the fuel cores shall be at least 3.0% and not more than 11.0%.
3.4.1.5 Fuel Element Requirements 3.4.1.6 Fuel Loading: Assigned fuel loading for each fuel element shall be 175.006-4.90 grams of U-235. Each Control Fuel Element shall contain 100 *2.80 grams of U-235. Control limits for the method used to measure this weight are established at the 95% confidence level for a significant population of measurements of a particular standard. The U-235 enrichment shall be 19.75 '-0.2 weight % of total uranium per specification TRTR- 11.
PUR-1 SAR                                  PUR-1 SAR    ~~Appendix 3-212.Jl3,01                        2. July 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                              SPC-382of5 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS - ASSEMBLED FOR THE                            Effective Date: 01/24/07      Page: 17of5 PURDUE UNIVERSITY REACTOR 3.5    Surface Condition Fuel plates and completed fuel elements must comply with the surface condition requirements of Section 3.5.1, 3.5.2, and 3.5.3 and drawings of Section 2.1.2, per ANSI B46. 1. Sanding, or any other finishing procedure that will smear the aluminum surface, will not be allowed on fuel plates unless approved by the purchaser.
3.5.1    Surface Defects 3.5.1.1      Compliance with surface finish and defect requirements shall be established by 100% visual inspection of all fuel plates and elements. The surface of the finished fuel plates shall be smooth and free of gouges, scratches, pits, or removal of metal in excess of 0.005 inch in depth. Dents in the fuel plate shall not exceed 0.0 12 inch in depth or 0.25 inch in diameter. If there is evidence of dogboning in the plates, surface defects in the dogbone (see def.) area shall not exceed 0.003 inch in depth. No degradation of the fuel plates beyond these limits shall be permitted.
3.5.1.2      Fuel Plates shall be free of stringiness, scabs, or cracks.
Surface finish shall be as required by Drawing 635463.
Compliance with requirements of this section shall be accomplished by visual inspection of all fuel plates and fuel elements.
3.5.1.3      Defects on fuel plate edges or ends are permissible provided they are evaluated and acceptable to the requirements of Paragraph 3.3.1.2.
3.5.1.4      Compliance with surface finish and defect requirements shall be established by 100% visual inspection of all fuel element containers. Fuel element containers shall be free of surface defects such as pits, dents, or scratches in excess of 0.0 10 inch in depth and 0.12 inch in diameter or equivalent area.
 
====3.5.2 Cleanliness====
The suppliers fabrication, assembly, and storage areas used for the production of Purdue University fuel elements and/or components shall conform to the requirements of "controlledwork area" (see def.) as defined in Paragraph 1.3.6 of INL Standard 7022A. Cleanliness shall be PUR-1 SAR                                        ~~~Appendix PUR-1 SAR        3-22                              22. July uy2,21 23, 2015
 
Form 4l2.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                              SPC-382 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS - ASSEMBLED FOR THE                            Effective Date: 01/24/07          Page: 18 of 57 PURDUE UNIVERSITY REACTOR in compliance with INL Standard 7022A, Paragraphs 1.1, 1.2.3, 3.1, 3.2-b, d, i, 3.3 - d, e, 4.1.3, 4.2, and 4.3. Freon shall not be used to clean fuel elements or components.
As determined by Section 4.10 of this specification, there shall be no foreign materials on the finished fuel plates or surfaces of the finished fuel elements. All oil, metal chips, turnings, dusts, abrasives and spatter, scale, and other particles shall be removed from the fuel surfaces by procedures which assure that the minimum cladding thickness has not been violated. All components shall be cleaned by a method approved by the purchaser.
 
====3.5.3 Contamination====
The surfaces of each fuel plate shall be counted or smeared and counted for alpha-beta-gamma contamination. The alpha count shall be less than five dpm per 100 cm 2, and the beta-gamma count shall be less than 200 dpm per 100 cm2.
Each fuel element shall be smeared and counted for radioactive contamination. The alpha count shall be less than five dpm per 100 cm 2 ,
and the beta-gamma count shall be less than 200 dpm per 100 cm2 3.6    Marking NOTE:        All/fuel plates, fuel assemblies, andfuel element containers will be markedper this section.
3.6.1    Fuel Plate Identification:
Each finished fuel plate shall be identified, as shown on Drawing 635463, by a combination of numbers and/or letters that will maintain positive identification relative to the complete traceability to the supplier fabrication history, including the basic material lots, heat or metal, manufacturing cycle, and quality control phases. The identification number shall be stamped, etched or vibro-peened at the location specified by Drawing 635463. The depth of the identification characters shall not exceed 0.010 in.
3.6.2    Fuel Assembly Identification:
r Each fuel assembly shall have an identifying number such as 07-XX (07 signifying year of fabrication). The number shall be placed on the container assembly as shown on Drawings 635455, 635456 and 635457.
PUR-I EAR                                            SAR~~~Appendix PUR-l    3-23                                22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382 STANDARD AND CONTROL FUEL                        Revision:      1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07          Page: 19 of 57 PURDUE UNIVERSITY REACTOR The identification shall be stamped or entered by a method approved by the purchaser, with two inch block characters not in excess of 0.010 inches in depth. Standard assemblies should be labeled: E2, F2, G2, H2, F3, H3, E4, F4, G4, H4, F5, H5. Control assemblies should be labeled: E3, G3, and E5. The fission chamber assembly should be labeled as G5. The source assembly shall be labeled as C3. The spare Standard Assemblies should be labeled: SP-1, SP-2, SP-3. The spare Control Assembly should be labeled as SP-4.
3.6.3    Dummy Element Identification:
The dummy standard fuel element assembly shall have the identifyring number DUM-1. The number shall be placed on the container assembly as shown on Drawing 635455. The identification shall be stamped or entered by a method approved by the purchaser, with two inch block characters not in excess of 0.010 inches in depth.
3.7    Storage All fuel plates, fuel assemblies, and fuel element containers that have received final cleaning per Section 3.5.2 shall be protected in clean polyethylene containers or other containers approved by the purchaser while (1) awaiting final assembly, (2) being transferred into or being maintained in storage, or (3) being prepared for packaging or shipment. Any material exposed to contamination shall be reinspected to the requirements of Section 3.5.
3.8    Fuel Element Surface Treatment If boehnmite treatment is required during fuel element fabrication, the following shall apply. After fuel elements are assembled and inspected they shall be subjected to an environment that will cause an evenly distributed boehmite layer of 0.00006 to 0.0003 in. thickness (averaged over the surface using eddy current instrumentation) to form on all surfaces of the entire assembly. The treatment process shall be performed under controlled conditions, which shall require the supplier to maintain a record of the thermal history of the autoclave. The records shall include heat charts of recorded time and temperature. Documented evidence of the controls placed on the autoclave shall be maintained by the supplier.
3.8.1    After the boehmite process has been qualified, one fuel element from every 2n autoclave run shall be inspected following a procedure approved by the Purchaser.
PUR-1 SAR                                        SAR ~~~Appendix PUR-1  3-24                                22. July uy2,21 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382of5 STANDARD AND CONTROL FUEL                          Revision:      1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07          Page: 20of5 PURDUE UNIVERSITY REACTOR 3.8.2    Each fuel element shall have a corresponding aluminum plate coupon, made from fuel plate end crops, placed near the fuel element during the boehmite formation process. The aluminum plate coupon shall be subjected to the same environment as the fuel elements and each coupon measured for boehmite thickness.
3.8.3    Fuel elements and aluminum plate coupons subjected to the boehmite formation process must be carefully handled to preclude scratches, dents, and gouges that would cause removal of boehmite.
3.9    Graphite Reflectors and Graphite Radiation Baskets Graphite reflector assemblies (see def.) and irradiationfacility assemblies (see def.) shall be fabricated as per requirements contained in this section and in drawings 635454, 635460, 635461, and 635465.
 
====3.9.1 Material====
All materials used shall comply with all the requirements of this specification and applicable drawings.


====3.9.2 Assembly====
====3.9.2 Assembly====
The assembly of the graphite reflector assemblies and irradiation facilityassemblies shall be as shown on the applicable drawings.
The assembly of the graphite reflector assemblies and irradiation facility assemblies shall be as shown on the applicable drawings.
3.9.3 Welding:All welding shall be performed using procedures and welding personnel qualified in accordance with ASME Section IX or the criteria defined inAppendix B. Quality acceptance of production welds shall be inaccordance with Appendix B, Section 5.3.9.4 Identification:
 
The graphite reflector assemblies shall have identifying numbers such asGR-X placed on the side of the assembly as shown drawing 635454.The graphite reflector shall be labeled as follows:
====3.9.3 Welding====
Dl, D2, D3, D4, D5,El, Fl, G1, Hl, I1, 12, 13, 14, and I5. The irradiation facility assemblies shall have identifying numbers such as IF-X placed on the side of theassembly as shown on drawing 635460. The irradiation facilityassemblies shall be labeled as follows:
All welding shall be performed using procedures and welding personnel qualified in accordance with ASME Section IX or the criteria defined in Appendix B. Quality acceptance of production welds shall be in accordance with Appendix B, Section 5.
D6, E6, F6, G6, H6, and 16. Theidentification shall be stamped or entered by a method approved by thepurchaser, with two inch block not in excess of 0.0 10 inches in depth.PUR-1 SARPUR-1 SAR ~~~Appendix 3-25 2 uy2,212. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
 
SPC-382STANDARD AND CONTROL FUEL Revision:
====3.9.4 Identification====
1ELEMENTSuRU U VEST- ASSEMBLED ECoFOR THE Effective Date: 01/24/07 Page: 21 of 573.9.5 Dimensional Inspection:
The graphite reflector assemblies shall have identifying numbers such as GR-X placed on the side of the assembly as shown drawing 635454.
Verification of all external dimensions of the graphite reflector assemblies and irradiation facility assemblies shall be by 100%inspection, in accordance with drawings 635454 and 635460. Alldimensions of this specification shall apply at a temperature of 75&deg;F+/-5&deg;"3.9.6 Surface Finish and Defects:The graphite reflector assemblies and irradiation facility assemblies shallbe free of surface defects such as pits, dents, scratches in excess of 0.010inch deep and 0.12 inch diameter or equivalent area.3.9.7 Storage:All graphite reflector assemblies and irradiation facility assemblies shallhave received final cleaning and shall be protected in clean polyethylene containers or other containers approved by the purchaser while (a) beingtransferred into storage, (b) being maintained in storage, or (c) beingprepared for shipment or packaging.
The graphite reflector shall be labeled as follows: Dl, D2, D3, D4, D5, El, Fl, G1, Hl, I1, 12, 13, 14, and I5. The irradiation facility assemblies shall have identifying numbers such as IF-X placed on the side of the assembly as shown on drawing 635460. The irradiation facility assemblies shall be labeled as follows: D6, E6, F6, G6, H6, and 16. The identification shall be stamped or entered by a method approved by the purchaser, with two inch block not in excess of 0.0 10 inches in depth.
: 4. QUALITY ASSURANCE The supplier shall document, implement, and maintain a quality program in compliance with ASME NQA-1-1997.
PUR-1 SAR                                          SAR ~~~Appendix PUR-1  3-25                                 2   uy2,21
The supplier shall permit the purchaser to conduct pre-award and continuing evaluation of the Quality Program.Personnel performing NDE examinations, specifically radiographic, ultrasonic, liquidpenetrant, and visual shall be certified to American Society for Nondestructive Testing(ASNT) Number SNT-TC-1A and certification documentation shall be made available tothe purchaser.
: 2. July 23, 2015
Unless otherwise specified, the supplier shall be responsible for the performance of alltests and inspections required prior to submission to the purchaser of any fuel element foracceptance.  
 
: Provided, however, that the performance of such tests and inspections is inaddition to, and does not limit, the right of the purchaser to conduct such other tests andinspections as the purchaser deems necessary to assure that all fuel elements are in-conformance with all requirements of this specification.
Form 412.09 (Rev. 09)
Except as otherwise specified, the supplier may use for inspection purposes either his own or any commercial laboratory acceptable to the purchaser.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTSuRU U ASSEMBLED VEST- ECoFOR THE                   Effective Date: 01/24/07         Page: 21 of 57 3.9.5   Dimensional Inspection:
Records of all tests and examinations shall be kept completePUR-1 SARPUR-1 SAR ~~Appendix 3-262.Jl3,01
Verification of all external dimensions of the graphite reflector assemblies and irradiation facility assemblies shall be by 100%
: 2. July 23, 2015 Forn 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
inspection, in accordance with drawings 635454 and 635460. All dimensions of this specification shall apply at a temperature of 75&deg;F+/-
SPC-382STANDARD AND CONTROL FUEL Revision:
5&deg;"
1ELEMENTS
3.9.6   Surface Finish and Defects:
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 22 of 57PURDUE UNIVERSITY REACTORand available to the purchaser.
The graphite reflector assemblies and irradiation facility assemblies shall be free of surface defects such as pits, dents, scratches in excess of 0.010 inch deep and 0.12 inch diameter or equivalent area.
All test and measuring equipment shall be calibrated perthe requirements of Standard MIL-C-45 662.The following applies to specified limits for requirements on core density perSection 3.4.1.1 and 4.2 and all dimensional requirements of this specification.
 
Forpurposes of determining conformance with this specification an observed value or acalculated value shall be rounded off to the nearest unit in the last right hand place offigures used in expressing the limiting value in accordance with the rounding-off methodof the Recommended Practices for Designating Significant Places in Specified LimitingValues (ASTM E29).The supplier shall prepare for his use and the purchaser's approval an integrated manufacturing and inspection test plan. The plan shall include all manufacturing operations, equipment and tooling used, inspection requirements and gaging used, andmandatory hold points established by the purchaser.
====3.9.7 Storage====
Any materials or fuel element components that are fabricated using equipment, personnel, or processes that are not in accordance with approvals as previously grantedby the purchaser are subject to rejection (see def.). A report of any such incident must besubmitted in accordance with Section 6.3.7.Fuel element inspection for shipment or rejection will be made by the on-site purchaser's representative at the supplier's plant. Final fuel element acceptance will be made by thepurchaser at the User's facility.
All graphite reflector assemblies and irradiation facility assemblies shall have received final cleaning and shall be protected in clean polyethylene containers or other containers approved by the purchaser while (a) being transferred into storage, (b) being maintained in storage, or (c) being prepared for shipment or packaging.
: 4.     QUALITY ASSURANCE The supplier shall document, implement, and maintain a quality program in compliance with ASME NQA-1-1997.
The supplier shall permit the purchaser to conduct pre-award and continuing evaluation of the Quality Program.
Personnel performing NDE examinations, specifically radiographic, ultrasonic, liquid penetrant, and visual shall be certified to American Society for Nondestructive Testing (ASNT) Number SNT-TC-1A and certification documentation shall be made available to the purchaser.
Unless otherwise specified, the supplier shall be responsible for the performance of all tests and inspections required prior to submission to the purchaser of any fuel element for acceptance. Provided, however, that the performance of such tests and inspections is in addition to, and does not limit, the right of the purchaser to conduct such other tests and inspections as the purchaser deems necessary to assure that all fuel elements are in-conformance with all requirements of this specification. Except as otherwise specified, the supplier may use for inspection purposes either his own or any commercial laboratory acceptable to the purchaser. Records of all tests and examinations shall be kept complete PUR-1 SAR                                          PUR-1 SAR   ~~Appendix 3-262.Jl3,01                         2. July 23, 2015


===4.1 Materials===
Forn 412.09 (Rev. 09)
Compliance with the material requirements of Section 3.2 shall be established bysupplier certification.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                            SPC-382 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS - ASSEMBLED FOR THE                          Effective Date: 01/24/07          Page: 22 of 57 PURDUE UNIVERSITY REACTOR and available to the purchaser. All test and measuring equipment shall be calibrated per the requirements of Standard MIL-C-45 662.
A "Certification of Chemical Analysis" or a certified milltest report shall be supplied to the purchaser for each lot of material used in thefabrication of fuel elements.
The following applies to specified limits for requirements on core density per Section 3.4.1.1 and 4.2 and all dimensional requirements of this specification. For purposes of determining conformance with this specification an observed value or a calculated value shall be rounded off to the nearest unit in the last right hand place of figures used in expressing the limiting value in accordance with the rounding-off method of the Recommended Practices for Designating Significant Places in Specified Limiting Values (ASTM E29).
This certificate shall give the results of the chemicalanalysis for the material.
The supplier shall prepare for his use and the purchaser's approval an integrated manufacturing and inspection test plan. The plan shall include all manufacturing operations, equipment and tooling used, inspection requirements and gaging used, and mandatory hold points established by the purchaser.
All fuel element materials shall be traceable.
Any materials or fuel element components that are fabricated using equipment, personnel, or processes that are not in accordance with approvals as previously granted by the purchaser are subject to rejection (see def.). A report of any such incident must be submitted in accordance with Section 6.3.7.
4.2 Core DensityThe density of the fuel cores required in Section 3.4.1.3 shall be determined bythe Archimedes principle.
Fuel element inspection for shipment or rejection will be made by the on-site purchaser's representative at the supplier's plant. Final fuel element acceptance will be made by the purchaser at the User's facility.
During qualification of the fuel plate core void densityrequired by Section 3.4.1.3 shall be determined on all qualification fuel platessubmitted.
4.1      Materials Compliance with the material requirements of Section 3.2 shall be established by supplier certification. A "Certification of Chemical Analysis" or a certified mill test report shall be supplied to the purchaser for each lot of material used in the fabrication of fuel elements. This certificate shall give the results of the chemical analysis for the material. All fuel element materials shall be traceable.
After the particular plate type has been qualified, 100% inspection forvoid density is not required for production lots of fuel plates. For production lots,three randomly selected fuel plates from each lot shall be inspected for voidvolume density.
4.2      Core Density The density of the fuel cores required in Section 3.4.1.3 shall be determined by the Archimedes principle. During qualification of the fuel plate core void density required by Section 3.4.1.3 shall be determined on all qualification fuel plates submitted. After the particular plate type has been qualified, 100% inspection for void density is not required for production lots of fuel plates. For production lots, three randomly selected fuel plates from each lot shall be inspected for void volume density. Should any one of these plates be discrepant, the entire lot must then be inspected for void volume density. If void density discrepancies appear regularly in the process, the purchaser may request 100% inspection.
Should any one of these plates be discrepant, the entire lot mustthen be inspected for void volume density.
PUR-1 SAR                                          Appendix 3-27                              PUR-SARAppedix
If void density discrepancies appearregularly in the process, the purchaser may request 100% inspection.
                                                                                                    -27Rev
PUR-1 SARAppendix 3-27PUR- SARAppedix
: 2. July  23, 2015
-27Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
 
SPC-382STANDARD AND CONTROL FUEL Revision:
Form 412.09 (Rev. 09)
1ELEMENTS
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                          SPC-382 STANDARD AND CONTROL FUEL                          Revision:      1 ELEMENTS - ASSEMBLED FOR THE                        Effective Date: 01/24/07    Page: 23 of 57 PURDUE UNIVERSITY REACTOR The actual core volume shall be calculated by the following formula where:
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 23 of 57PURDUE UNIVERSITY REACTORThe actual core volume shall be calculated by the following formula where:weight units are in grams and volumes in cubic centimeters.
weight units are in grams and volumes in cubic centimeters.
PALwhere:Voimmersion volume of fuel plate coreVp volume of fuel plateAL= density of aluminum used for fuel plate cladding2.715 gins/ccWp = weight of plateWc = deburred weight of fuel plate core compactPUR-1 SARAppendix 3-28PUR- SARAppedix
PAL where:
-28Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Vo          immersion volume of fuel plate core Vp      volume of fuel plate AL=    density of aluminum used for fuel plate cladding 2.715 gins/cc Wp =    weight of plate Wc =    deburred weight of fuel plate core compact PUR-1 SAR                                        Appendix 3-28                        PUR-SARAppedix
SPC-3 82STANDARD AND CONTROL FUEL Revision:
                                                                                            -28Rev
1ELEMENTS
: 2. July 23, 2015
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 24 of 57PURDUE UNIVERSITY REACTORThe theoretical core volume shall be calculated by the following formulas:
 
_ ( WU3Si2 + ( WA/1Vet --pA---TJwhere:Vct= calculated theoretical core volumeWU3Si2 = weight of U3Si2 powder in coreWal weight of aluminum matrix powder in corepU3Si2= density of U3Si2powder as measuredPAl= density of aluminum powder used for core matrix= 2.710 gms/ccThe void percent in the core shall be calculated using the following formula:V&deg;%=v V-vCt(10000)Vcwhere:V% = percent voids in the fuel plate core4.3 Fuel LoadingVerification of the fuel loading as specified in Section 3.4.1.2 shall be inconformance to the supplier's procedure required in Section 6.3.1.In order to determine compliance with the fuel density requirements ofSection 4.4, the U-235 loading of the fuel plate, as determined in accordance withthe procedures of Section 6.3.1, will be divided by the core volume (Vc) ascalculated by the method described in the second paragraph of Section 4.2.4.4 Fuel Homogeneity Fuel core homogeneity requirements shall be complied with by a one-piece radiograph of all fuel plates from each fuel plate lot and evaluation of theradiograph by calibrated densitometer measurements.
Form 412.09 (Rev. 09)
Purchaser approved densitystandards may be used by the supplier.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                               SPC-3 82 STANDARD AND CONTROL FUEL                           Revision:         1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07         Page: 24 of 57 PURDUE UNIVERSITY REACTOR The theoretical core volume shall be calculated by the following formulas:
Fuel plates and density standards shall bePUR-1 SARAppendix 3-29FUR- SARAppedix
Vet --
-29Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
_ **)
SPC-382STANDARD AND CONTROL FUEL Revision:
( WU3Si2  * + *x pA---TJ
1ELEMENTS
( WA/1 where:
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 25 of 57PURDUE UNIVERSITY REACTORexposed simultaneously.
Vct        =    calculated theoretical core volume WU 3Si2  =      weight of U3 Si2 powder in core Wal              weight of aluminum matrix powder in core pU 3 Si 2 =      density of U3 Si2 powder as measured PAl      =      density of aluminum powder used for core matrix
Fuel plate density variations shall be determined bycomparison of fuel plate areas to corresponding areas of the standard.
                                        =      2.710 gms/cc The void percent in the core shall be calculated using the following formula:
All fuel plates shall be inspected for homogeneity.
V&deg;%=v  V-vCt(    10 0 00)
Homogeneity of the fuel platecore shall be determined by radiograph film density measurements with adensitometer having a 0.080 inch aperture.
Vc where:
When determining fuel core density from plate radiographs, the brighter theimage on the radiograph, the more dense is the uranium and the lower the numberindicated on the densitometer.
V%        =      percent voids in the fuel plate core 4.3    Fuel Loading Verification of the fuel loading as specified in Section 3.4.1.2 shall be in conformance to the supplier's procedure required in Section 6.3.1.
The darker the image on the radiograph, the lessdense is the uranium and the larger the number indicated on the densitometer.
In order to determine compliance with the fuel density requirements of Section 4.4, the U-235 loading of the fuel plate, as determined in accordance with the procedures of Section 6.3.1, will be divided by the core volume (Vc) as calculated by the method described in the second paragraph of Section 4.2.
A+30% fuel core density and a +20% fuel core density is indicated by thedensitometer readings in the suspect area being 30% or 20% lower than theaverage densitometer readings for all core locations.
4.4    Fuel Homogeneity Fuel core homogeneity requirements shall be complied with by a one-piece radiograph of all fuel plates from each fuel plate lot and evaluation of the radiograph by calibrated densitometer measurements. Purchaser approved density standards may be used by the supplier. Fuel plates and density standards shall be PUR-1 SAR                                          Appendix 3-29                            FUR-SARAppedix
A -30% or a -20% fuel coredensity is indicated by the densitometer readings in the suspect area being 30% or20% higher than the average densitometer readings for all fuel core locations.
                                                                                                  -29Rev
Any one-half inch diameter or greater spot in the plate fuel core area, other thanthe dogbone area shall not be less in fuel density than -20% of the average fueldensity for all fuel core locations.
: 2. July  23, 2015
To determine the low density of a one-half inchdiameter area, the film is maneuvered under the densitometer in the low-density area until the highest number possible is obtained on the densitometer.
 
Thisnumber is recorded.
Form 412.09 (Rev. 09)
Then four readings are taken one-fourth inch from this spotand symmetrical around it. The average of these five readings is compared to theaverage densitometer readings for all fuel core locations.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                            SPC-382 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS - ASSEMBLED FOR THE                          Effective Date: 01/24/07      Page: 25 of 57 PURDUE UNIVERSITY REACTOR exposed simultaneously. Fuel plate density variations shall be determined by comparison of fuel plate areas to corresponding areas of the standard.
If density standards are used, the average densitometer readings of all fuel corelocations will be replaced by the nominal density standard and comparisons willbe determined between the suspect spot on the radiograph and the -30% and-20% standards.
All fuel plates shall be inspected for homogeneity. Homogeneity of the fuel plate core shall be determined by radiograph film density measurements with a densitometer having a 0.080 inch aperture.
For the +30% and +20% homogeneity overload inspection, compare the nominal density standard to the suspect area. In this casedensitometer units from nominal of the fuel plate represent the following percentages:
When determining fuel core density from plate radiographs, the brighter the image on the radiograph, the more dense is the uranium and the lower the number indicated on the densitometer. The darker the image on the radiograph, the less dense is the uranium and the larger the number indicated on the densitometer. A
-0.15 = +30%; -0.10 = +20%. Fuel plates exceeding these limits arediscrepant.
              +30% fuel core density and a +20% fuel core density is indicated by the densitometer readings in the suspect area being 30% or 20% lower than the average densitometer readings for all core locations. A -30% or a -20% fuel core density is indicated by the densitometer readings in the suspect area being 30% or 20% higher than the average densitometer readings for all fuel core locations.
For rectangular shaped, suspected discrepant areas that are evaluated to the one-half inch criteria, orient the four symmetrical readings such that worst casereadings will be taken.Between the minimum and maximum permissible fuel core length boundary, fuelunderload condition shall not be evaluated.
Any one-half inch diameter or greater spot in the plate fuel core area, other than the dogbone area shall not be less in fuel density than -20% of the average fuel density for all fuel core locations. To determine the low density of a one-half inch diameter area, the film is maneuvered under the densitometer in the low-density area until the highest number possible is obtained on the densitometer. This number is recorded. Then four readings are taken one-fourth inch from this spot and symmetrical around it. The average of these five readings is compared to the average densitometer readings for all fuel core locations.
Any indication of un-alloyed uranium as determined by radiography shall because for rejection.
If density standards are used, the average densitometer readings of all fuel core locations will be replaced by the nominal density standard and comparisons will be determined between the suspect spot on the radiograph and the -30% and
PUR-1 SARAppendix 3-30PUR1 SR Apenix -30Rev2.  
              -20% standards. For the +30% and +20% homogeneity overload inspection, compare the nominal density standard to the suspect area. In this case densitometer units from nominal of the fuel plate represent the following percentages: -0.15 = +30%; -0.10 = +20%. Fuel plates exceeding these limits are discrepant.
,July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
For rectangular shaped, suspected discrepant areas that are evaluated to the one-half inch criteria, orient the four symmetrical readings such that worst case readings will be taken.
SPC-382STANDARD AND CONTROL FUEL Revision:
Between the minimum and maximum permissible fuel core length boundary, fuel underload condition shall not be evaluated.
1ELEMENTSuRU U VEST- ASSEMBLEDRE oFOR THE Effective Date: 01/24/07 Page: 26 of 57Any 0.080 inch diameter spot in the fuel plate dogbone area (area within one inchof each fuel core end) shall not be greater in fuel density than +30% of theaverage fuel density for all core locations.
Any indication of un-alloyed uranium as determined by radiography shall be cause for rejection.
Any one-half inch diameter area in thedogbone area shall not be less in fuel density than -30% of the average fueldensity for all fuel core locations.
PUR-1 SAR                                          Appendix 3-30                          PUR1 SR ,July Apenix
The actual dogbone shall not be more than one-half inch in the longitudinal direction.
                                                                                                    -30Rev2.
Other than the dogbone areas near ends of fuel core, any one-half inch diameterarea shall not be greater in fuel density than +20% of the average fuel density forall fuel core locations.
23,  2015
To determine the high density of a one-half inch diameterarea, the film is maneuvered under the densitometer in the high-density area untilthe lowest number possible is obtained on the densitometer.
 
This number isrecorded.
Form 412.09 (Rev. 09)
Then four readings are taken one-fourth inch from this spot andsymmetrically around it. The average of these five readings is compared to theaverage densitometer readings for all fuel core locations.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                              SPC-382 STANDARD AND CONTROL FUEL                              Revision:      1 ELEMENTSuRU U ASSEMBLEDRE VEST-                  oFOR THE          Effective Date: 01/24/07          Page: 26 of 57 Any 0.080 inch diameter spot in the fuel plate dogbone area (area within one inch of each fuel core end) shall not be greater in fuel density than +30% of the average fuel density for all core locations. Any one-half inch diameter area in the dogbone area shall not be less in fuel density than -30% of the average fuel density for all fuel core locations. The actual dogbone shall not be more than one-half inch in the longitudinal direction.
Unless otherwise specified, purchaser approval of all radiographs is required priorto assembly of fuel plates into elements.
Other than the dogbone areas near ends of fuel core, any one-half inch diameter area shall not be greater in fuel density than +20% of the average fuel density for all fuel core locations. To determine the high density of a one-half inch diameter area, the film is maneuvered under the densitometer in the high-density area until the lowest number possible is obtained on the densitometer. This number is recorded. Then four readings are taken one-fourth inch from this spot and symmetrically around it. The average of these five readings is compared to the average densitometer readings for all fuel core locations.
4.5 Core Configuration Each finish-cut flat fuel plate shall be radiographed in accordance withAppendix A and evaluated for compliance with Section 3.3.1.2.Visual radiograph inspections will be performed without magnification on a lighttable having a light intensity of 450 to 600 ft-candles at the table surface and thearea darkened to give a light range of 5 to 15 ft-candles 18 in. above the lighttable with radiograph film in place on the table.4.6 Bond Integrity 4.6.1 Blister Anneal:After the fuel plate has been hot rolled, it shall be heated to 9000F+130F,held at that temperature for a period of 2 hours, -15 minutes,
Unless otherwise specified, purchaser approval of all radiographs is required prior to assembly of fuel plates into elements.
+30 minutes,removed from furnace, and allowed to air cool.Any blisters, in the fuel core region larger than a 0.060 in. diameter or anyblister in the frame region of the fuel plate larger than 0.120 in. diametershall result in rejection of the associated fuel plate. A maximum of twoblisters less than 0.060 in. diameter is allowed in the fuel core area,provided they are more than 0.25 0 in. apart. A maximum of two blisters inany of the four sides of the picture frame (see def.)(a maximum of eight)region smaller than 0.120 in. can be tolerated providing that no blister isPUR-1 SARAppendix 3-31PUR- SARAppedix
4.5    Core Configuration Each finish-cut flat fuel plate shall be radiographed in accordance with Appendix A and evaluated for compliance with Section 3.3.1.2.
-31Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Visual radiograph inspections will be performed without magnification on a light table having a light intensity of 450 to 600 ft-candles at the table surface and the area darkened to give a light range of 5 to 15 ft-candles 18 in. above the light table with radiograph film in place on the table.
SPC-382STANDARD AND CONTROL FUEL Revision:
4.6     Bond Integrity 4.6.1      Blister Anneal:
1ELEMENTS
After the fuel plate has been hot rolled, it shall be heated to 900 0 F+13 0 F, held at that temperature for a period of 2 hours, -15 minutes, +30 minutes, removed from furnace, and allowed to air cool.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 27 of 57PURDUE UNhIVERSITY REACTORany closer to the plate edge or end or to another blister than the majordimension of the blister and no blister is closer to the plate edge or endthan 0.050 inch. When there is question as to size or location of theblisters, the acceptance or rejection of the plate shall be determined in theultrasonic inspection of Section 4.6.2.4.6.2 Ultrasonic Scanning:
Any blisters, in the fuel core region larger than a 0.060 in. diameter or any blister in the frame region of the fuel plate larger than 0.120 in. diameter shall result in rejection of the associated fuel plate. A maximum of two blisters less than 0.060 in. diameter is allowed in the fuel core area, provided they are more than 0.25 0 in. apart. A maximum of two blisters in any of the four sides of the pictureframe (see def.)(a maximum of eight) region smaller than 0.120 in. can be tolerated providing that no blister is PUR-1 SAR                                            Appendix 3-31                            PUR-SARAppedix
The finished fuel plate area shall be ultrasonically inspected incompliance with ASME Boiler and Pressure Vessel Code, Section V,Article 5, Paragraphs T-ll0, T-5 10, T-520, T-521, T-522-a, b, c, e, g, i,j, k, 1, o, T-523, T-523-1, and T-534. Any indication of discontinuity inthe fuel core region equivalent to that indicated by a 0.060 in. diameterstandard or any indication of a discontinuity in the frame region of thefuel plate equivalent to that indicated by a 0.120 in. diameter standardshall result in rejection of the associated fuel plate. Acceptance criteriafor number of blisters revealed by ultrasonic scanning are perSection 4.6.1. Any discontinuities, inside the fuel plate, other thanblisters and for which acceptance criterion is not already stated, shall bedescribed by the supplier and evaluated by the purchaser.
                                                                                                      -31Rev
4.6.3 Metallo~raphic Examination.
: 2. July 23, 2015
During qualification, one fuel plate per lot selected for qualification perSection 3.1.1 will be sectioned per Figure 1, polished and etched, andexamined at 50x or above for bond and clad-core-clad dimensions perthe requirements of Sections 3.3.1.3 and 3.3.1.4, and Drawing 635463,respectively.
 
If the fuel plate fails the metallographic examination for grain growth,voids, laminations, core cracking or separation, or foreign particles ormaterials, then randomly selected another plate in the lot formetallographic examination.
Form 412.09 (Rev. 09)
If this plate fails the examination, reject thelot.Fuel plates selected for destruction tests may be rejected fuel plates,providing the attribute to be tested for is not affected by the cause forrejection.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                              SPC-382 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS - ASSEMBLED FOR THE                            Effective Date: 01/24/07        Page: 27 of 57 PURDUE UNhIVERSITY REACTOR any closer to the plate edge or end or to another blister than the major dimension of the blister and no blister is closer to the plate edge or end than 0.050 inch. When there is question as to size or location of the blisters, the acceptance or rejection of the plate shall be determined in the ultrasonic inspection of Section 4.6.2.
Reject fuel plates so used must have purchaser approval beforedestruct tests are performed.
4.6.2    Ultrasonic Scanning:
4.7 Internal DefectsAny internal defect in excess of the requirement of Section 3.3.1.3 in the fuelcore, including voids, laminations, U3Si2segregation,  
The finished fuel plate area shall be ultrasonically inspected in compliance with ASME Boiler and Pressure Vessel Code, Section V, Article 5, Paragraphs T-ll0, T-5 10, T-520, T-521, T-522-a, b, c, e, g, i, j, k, 1,o, T-523, T-523-1, and T-534. Any indication of discontinuity in the fuel core region equivalent to that indicated by a 0.060 in. diameter standard or any indication of a discontinuity in the frame region of the fuel plate equivalent to that indicated by a 0.120 in. diameter standard shall result in rejection of the associated fuel plate. Acceptance criteria for number of blisters revealed by ultrasonic scanning are per Section 4.6.1. Any discontinuities, inside the fuel plate, other than blisters and for which acceptance criterion is not already stated, shall be described by the supplier and evaluated by the purchaser.
: clumping, core cracking orPUR-1 SARAppendix 3-32PUR- SARAppedix
4.6.3    Metallo~raphic Examination.
-32Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
During qualification, one fuel plate per lot selected for qualification per Section 3.1.1 will be sectioned per Figure 1, polished and etched, and examined at 50x or above for bond and clad-core-clad dimensions per the requirements of Sections 3.3.1.3 and 3.3.1.4, and Drawing 635463, respectively.
SPC-382 5STANDARD AND CONTROL FUEL Revision:
If the fuel plate fails the metallographic examination for grain growth, voids, laminations, core cracking or separation, or foreign particles or materials, then randomly selected another plate in the lot for metallographic examination. If this plate fails the examination, reject the lot.
1ELEMENTS
Fuel plates selected for destruction tests may be rejected fuel plates, providing the attribute to be tested for is not affected by the cause for rejection. Reject fuel plates so used must have purchaser approval before destruct tests are performed.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 28 of 5PURDUE UNIVERSITY REACTORseparation, or foreign particles or materials, which is identified by anymeasurement technique, including radiography per Section 4.4, ultrasonic scanning per Section 4.6.2, or metallography per Section 4.6.3, shall be cause forrejection of the fuel plate.4.8 Surface Finish and DefectsCompliance with requirements of Section 3.5 shall be established by visualinspection of all fuel plates and fuel elements.
4.7    Internal Defects Any internal defect in excess of the requirement of Section 3.3.1.3 in the fuel core, including voids, laminations, U3 Si2 segregation, clumping, core cracking or PUR-1 SAR                                          Appendix 3-32                          PUR-SARAppedix
Out-of-specification defects shallbe measured for size and depth and reported to the purchaser.
                                                                                                    -32Rev
4.9 Clad-Core-Clad Dimensions Fuel Plate Qualification requirements of section 3.1.1 shall be established byultrasonic techniques using the purchaser-supplied, min-clad inspection gage. Allfuel plates will be subjected to ultrasonic mmn-clad inspection with the fuel coreregion scanned for each plate. Ultrasonic mmn-clad inspection shall beaccomplished by calibration of the mmn-clad gage, using the Advanced TestReactor (ATR) Standard (8E0777) scanned at the normal mode of 0.008 inches.The mmn-clad gage will then be adjusted and the fuel plates will be scanned at adepth of 0.010 inches. Ultrasonic Test (UT) traces showing fuel at the 0.010 inchdepth will be compared to the 0.008 inch standard to determine plateacceptability.
: 2. July  23, 2015
If the density of indications from fuel plate exceeds the ATRstandard density of indications, the plate is rejectable.
 
NOTE: The ATR standard is a small piece of an A TR fuel plate that has fuelparticles near the surface.
Form 412.09 (Rev. 09)
It is used on the UT mmn-clad machine toindicate mmi-clad indications and compare the density of theseindications to any indications noted from a fuel plate being inspected by UT.During the fuel plate qualification
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                            SPC-382                        5 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS - ASSEMBLED FOR THE                          Effective Date: 01/24/07        Page: 28 of 5 PURDUE UNIVERSITY REACTOR separation, or foreign particles or materials, which is identified by any measurement technique, including radiography per Section 4.4, ultrasonic scanning per Section 4.6.2, or metallography per Section 4.6.3, shall be cause for rejection of the fuel plate.
: process, compliance with the requirements ofSection 3.3.1.4 shall be established by destructive analysis of one fuel plate per lotin accordance with Figure 1.After fuel plate qualification, all production plates shall be mmi-clad ultrasonic inspected at a depth of 0.010 inches. Those plates discrepant at 0.010 inches shallbe rescanned at 0.008 inches. Plates which are acceptable when re-scanned at0.008 inches shall be submitted on Information/Change Request (Form 540.33) tothe purchaser.
4.8    Surface Finish and Defects Compliance with requirements of Section 3.5 shall be established by visual inspection of all fuel plates and fuel elements. Out-of-specification defects shall be measured for size and depth and reported to the purchaser.
PUR-1 SARAppendix 3-33PUR1 SR Apenix -33Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laborator SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
4.9    Clad-Core-Clad Dimensions Fuel Plate Qualification requirements of section 3.1.1 shall be established by ultrasonic techniques using the purchaser-supplied, min-clad inspection gage. All fuel plates will be subjected to ultrasonic mmn-clad inspection with the fuel core region scanned for each plate. Ultrasonic mmn-clad inspection shall be accomplished by calibration of the mmn-clad gage, using the Advanced Test Reactor (ATR) Standard (8E0777) scanned at the normal mode of 0.008 inches.
SPC-382STANDARD AND CONTROL FUEL Revision:
The mmn-clad gage will then be adjusted and the fuel plates will be scanned at a depth of 0.010 inches. Ultrasonic Test (UT) traces showing fuel at the 0.010 inch depth will be compared to the 0.008 inch standard to determine plate acceptability. If the density of indications from fuel plate exceeds the ATR standard density of indications, the plate is rejectable.
1ELEMENTS
NOTE:        The ATR standardis a smallpiece of an A TR fuel plate that has fuel particles near the surface. It is used on the UT mmn-clad machine to indicate mmi-clad indicationsand compare the density of these indicationsto any indicationsnotedfrom a fuel plate being inspected by UT.
-ASSEMBLED FOR THE Effective Date: 01/24/07PURDUE UNIVERSITY REACTORPage: 29 of 574.10 Cleanliness Fuel plate, fuel assembly, and fuel element container cleanliness requirements ofSection 3.5.2 shall be established by visual inspection without magnification of allfuel plates, fuel assemblies, and fuel element containers.
During the fuel plate qualification process, compliance with the requirements of Section 3.3.1.4 shall be established by destructive analysis of one fuel plate per lot in accordance with Figure 1.
4.11 Contamination The surfaces of each fuel plate and fuel assembly shall be counted or smeared andcounted for alpha-beta-ganmma contamination and meet the requirements ofSection 3.5.3.4.12 Dimensional It shall be the supplier's responsibility to assure that fabrication is performed inaccordance with all dimensions delineated in the Drawings referenced in Section2.1.2. Noncomplying design dimensions on fuel plates, fuel assemblies, and fuelelement containers (actual measurements) shall be submitted to the purchaser forreview and approval.
After fuel plate qualification, all production plates shall be mmi-clad ultrasonic inspected at a depth of 0.010 inches. Those plates discrepant at 0.010 inches shall be rescanned at 0.008 inches. Plates which are acceptable when re-scanned at 0.008 inches shall be submitted on Information/Change Request (Form 540.33) to the purchaser.
Any discrepant component shall not be used in a fuelelement assembly unless approved.
PUR-1 SAR                                          Appendix 3-33                          PUR1 SR 2. July Apenix
The supplier is to certify to compliance with the design dimensional requirements delineated in the Drawings referenced in Section 2.1.2.All dimensions of finished fuel plates, fuel assemblies and fuel element containers apply at 75&deg;F+5&deg;F.
                                                                                                        -33Rev 23, 2015
4.12.1 Final Dimensional Inspection.
 
Dimensions required by this specification and drawings of Section 2.1.2shall be inspected using a purchaser approved sample plan and recordedon an inspection sheet with "in specification" dimensions recorded bycheck mark, "O, or actual measurements and ''out of specification''
Form 412.09 (Rev. 09)
Idaho National Laborator SPECIFICATION FOR PURDUE UNIVERSITY                        Identifier:    SPC-382 STANDARD AND CONTROL FUEL                            Revision:      1 ELEMENTS        -  ASSEMBLED FOR THE                    Effective Date: 01/24/07          Page: 29 of 57 PURDUE UNIVERSITY REACTOR 4.10 Cleanliness Fuel plate, fuel assembly, and fuel element container cleanliness requirements of Section 3.5.2 shall be established by visual inspection without magnification of all fuel plates, fuel assemblies, and fuel element containers.
4.11 Contamination The surfaces of each fuel plate and fuel assembly shall be counted or smeared and counted for alpha-beta-ganmma contamination and meet the requirements of Section 3.5.3.
4.12 Dimensional It shall be the supplier's responsibility to assure that fabrication is performed in accordance with all dimensions delineated in the Drawings referenced in Section 2.1.2. Noncomplying design dimensions on fuel plates, fuel assemblies, and fuel element containers (actual measurements) shall be submitted to the purchaser for review and approval. Any discrepant component shall not be used in a fuel element assembly unless approved.
The supplier is to certify to compliance with the design dimensional requirements delineated in the Drawings referenced in Section 2.1.2.
All dimensions of finished fuel plates, fuel assemblies and fuel element containers apply at 75&deg;F+5&deg;F.
4.12.1    Final Dimensional Inspection.
Dimensions required by this specification and drawings of Section 2.1.2 shall be inspected using a purchaser approved sample plan and recorded on an inspection sheet with "in specification" dimensions recorded by check mark, "O, or actual measurements and ''out of specification''
dimensions recorded as actual measurements.
dimensions recorded as actual measurements.
4.13 Reactor Components and Spare Fuel Element PartsReactor components and spare fuel element parts not assembled into fuel elementassemblies are required to be certified.
4.13 Reactor Components and Spare Fuel Element Parts Reactor components and spare fuel element parts not assembled into fuel element assemblies are required to be certified. The certification shall consist of material certification, fabrication verification, and supplier certificate of compliance to the specification and drawing requirements. The certification documents shall be submitted to the purchaser and user.
The certification shall consist of materialcertification, fabrication verification, and supplier certificate of compliance to thespecification and drawing requirements.
PUR-1 SAR                                          Appendix 3-34                            PUR-SARAppedix
The certification documents shall besubmitted to the purchaser and user.PUR-1 SARAppendix 3-34PUR- SARAppedix  
                                                                                                    -34Rev
-34Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: 2. July 23, 2015
SPC-382STANDARD AND CONTROL FUEL Revision:
 
1ELEMENTS
Form 412.09 (Rev. 09)
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 30 of 57PURDUE UNIVERSITY REACTOR5. PACKAGING AND SHIPPINGPackaging and shipping of the fuel elements shall be performed using a Purchaser approved procedure in compliance with this section.*The purchaser shall provide shipping containers to protect the fuel elements from damage duringshipment and which conform to the applicable requirements of the Departments of Energy andTransportation, and other regulatory agencies having jurisdiction of the shipment of radioactive materials.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                               SPC-382 STANDARD AND CONTROL FUEL                             Revision:       1 ELEMENTS - ASSEMBLED FOR THE                             Effective Date: 01/24/07           Page: 30 of 57 PURDUE UNIVERSITY REACTOR
Re-useable shipping containers will be returned to the Supplier by the User at thePurchaser's expense.*The Supplier is responsible for loading the fuel elements into shipping containers in a sealedpolyethylene sleeve in a cleaned dry condition and free of extraneous materials.
: 5.     PACKAGING AND SHIPPING Packaging and shipping of the fuel elements shall be performed using a Purchaser approved procedure in compliance with this section.
*The Supplier shall take necessary precautions during pack~aging to prevent damage to the fuelelements during shipment.
      *The purchaser shall provide shipping containers to protect the fuel elements from damage during shipment and which conform to the applicable requirements of the Departments of Energy and Transportation, and other regulatory agencies having jurisdiction of the shipment of radioactive materials. Re-useable shipping containers will be returned to the Supplier by the User at the Purchaser's expense.
Each container shall be provided with a tamper-proof seal. Loadingand shipping documents for the container shall be prepared in accordance with the applicable regulatory requirements.
      *The Supplier is responsible for loading the fuel elements into shipping containers in a sealed polyethylene sleeve in a cleaned dry condition and free of extraneous materials.
*The Supplier shall make arrangements for shipment to the User.6. NOTES6.1 Definitions For the purpose of this specification, the following terms are identified:
      *The Supplier shall take necessary precautions during pack~aging to prevent damage to the fuel elements during shipment. Each container shall be provided with a tamper-proof seal. Loading and shipping documents for the container shall be prepared in accordance with the applicable regulatory requirements.
Batch. The amount of sulicide powder mixture which is handled as a unit ortraceable to a common step.Blended.
      *The Supplier shall make arrangements for shipment to the User.
To mix or mingle constituents of a batch.Certification.
: 6.     NOTES 6.1     Definitions For the purpose of this specification, the following terms are identified:
The action of determining, verifying and attesting in writing (signedby a qualified party) to the qualifications of personnel and material.
Batch. The amount of sulicide powder mixture which is handled as a unit or traceable to a common step.
Cladding.
Blended. To mix or mingle constituents of a batch.
The aluminum covers bonded to the fuel core and the picture frame.Control Fuel Element Assembly.
Certification. The action of determining, verifying and attesting in writing (signed by a qualified party) to the qualifications of personnel and material.
An assembly consisting of the control fuelelement container with eight fuel plates.Controlled Work Area. A work area to which access of personnel, tools, andmaterials is limited and physically controlled.
Cladding. The aluminum covers bonded to the fuel core and the picture frame.
Temporary enclosures may be usedwhere adjacent activities produce contamination which is detrimental to the job.PUR-1 SARAppendix 3-35PUR1 SR Apenix -35Rev2.
Control Fuel Element Assembly. An assembly consisting of the control fuel element container with eight fuel plates.
July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Controlled Work Area. A work area to which access of personnel, tools, and materials is limited and physically controlled. Temporary enclosures may be used where adjacent activities produce contamination which is detrimental to the job.
SPC-382STANDARD AND CONTROL FUEL Revision:
PUR-1 SAR                                            Appendix 3-35                              PUR1 SR     Apenix July -35Rev2.
1ELEMENTS
23, 2015
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 31 of 57PURDUE UNIVERSITY REACTORDevelopment.
 
A determination of processes, equipment, and parameters requiredto produce a product in compliance with this specification.
Form 412.09 (Rev. 09)
Dogbone Area. Thickening of the fuel core usually in the last 1/2 in. of the core,which may result in clad thinning in those areas.Dummy Fuel Element Assembly.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                         Effective Date: 01/24/07       Page: 31 of 57 PURDUE UNIVERSITY REACTOR Development. A determination of processes, equipment, and parameters required to produce a product in compliance with this specification.
An assembly consisting of a fuel elementcontainer with unfueled simulated dummy fuel plates.Dummy Fuel Plate. A non-fueled plate made entirely from the aluminum materialspecified in this document.
Dogbone Area. Thickening of the fuel core usually in the last 1/2 in. of the core, which may result in clad thinning in those areas.
Edge Clad. The distance between the edge of the fuel core and the edge of thefinished fuel plate, before any stray particles are removed, in the width direction as determined by radiography of a flat fuel plate.Failure.
Dummy Fuel Element Assembly. An assembly consisting of a fuel element container with unfueled simulated dummy fuel plates.
A condition where the fabrication process appears to be out of control ora breakdown or damage to equipment creates excessive costs and/or scheduledelays.Fuel Compact.
Dummy Fuel Plate. A non-fueled plate made entirely from the aluminum material specified in this document.
A quantity of uranium silicide powder and aluminum powder, coldcompacted by pressing into a solid block for assembly into packs for hot roll andcold roll into fuel plates. The compacts are encased in frames and cover plates toform the pack.Fuel Assembly.
Edge Clad. The distance between the edge of the fuel core and the edge of the finished fuel plate, before any stray particles are removed, in the width direction as determined by radiography of a flat fuel plate.
An assembly of fuel plates and hardware components.
Failure. A condition where the fabrication process appears to be out of control or a breakdown or damage to equipment creates excessive costs and/or schedule delays.
Thisincludes both the standard and control fuel elements.
Fuel Compact. A quantity of uranium silicide powder and aluminum powder, cold compacted by pressing into a solid block for assembly into packs for hot roll and cold roll into fuel plates. The compacts are encased in frames and cover plates to form the pack.
Fuel Core. The uranium-bearing region of each Fuel Plate.Fuel Plate. The Fuel Core complete with aluminum frame and cladding.
FuelAssembly. An assembly of fuel plates and hardware components. This includes both the standard and control fuel elements.
Graphite Reflector Assemblies.
Fuel Core. The uranium-bearing region of each Fuel Plate.
A component consisting of a graphite container assembly with a graphite blockc inside.In-Process Controls.
Fuel Plate. The Fuel Core complete with aluminum frame and cladding.
Inspections and tests made during production to ensure thatthe manufacturing processes, equipment, and personnel are producing a productmeeting specified requirements.
Graphite Reflector Assemblies. A component consisting of a graphite container assembly with a graphite blockc inside.
Irradiation Facility Assemblies.
In-Process Controls. Inspections and tests made during production to ensure that the manufacturing processes, equipment, and personnel are producing a product meeting specified requirements.
A component consisting of a round tube attachedinside a graphite container assembly with graphite blocks filling the annulusbetween the tube and container.
IrradiationFacilityAssemblies. A component consisting of a round tube attached inside a graphite container assembly with graphite blocks filling the annulus between the tube and container. Inserted within the tube is the isotope capsule assemblies.
Inserted within the tube is the isotope capsuleassemblies.
PUR-1 SAR                                        Appendix 3-36                          PUR-SARAppedix
PUR-1 SARAppendix 3-36PUR- SARAppedix  
                                                                                                  -36Rev
-36Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: 2. July 23, 2015
SPC-382STANDARD AND CONTROL FUEL Revision:
 
1ELEMENTS
Form 412.09 (Rev. 09)
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 32 of 57PURDUE UNIVERSITY REACTORLot. A group of pieces handled as a unit or material traceable to a commonprocessing step.Manufacture(ing).
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY                         Identifier:     SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07       Page: 32 of 57 PURDUE UNIVERSITY REACTOR Lot. A group of pieces handled as a unit     or material traceable to a common processing step.
All fabrication,  
Manufacture(ing). All fabrication, assembly, test, inspection and quality control processes. Fabrication is a synonym for Manufacture.
: assembly, test, inspection and quality controlprocesses.
Pack. The fuel compact, picture frame, and cover plates, assembled together for hot rolling.
Fabrication is a synonym for Manufacture.
Picture Frame. The window shaped aluminum frame, which holds the fuel compact.
Pack. The fuel compact, picture frame, and cover plates, assembled together forhot rolling.Picture Frame. The window shaped aluminum frame, which holds the fuelcompact.Plates. See Fuel Plates.Procedure.
Plates. See Fuel Plates.
The detailed description of the series of processes during manufacture and inspection, which follow a regular definite order (not to be construed as anoutline).
Procedure. The detailed description of the series of processes during manufacture and inspection, which follow a regular definite order (not to be construed as an outline).
Production.
Production.That phase of the program, following Qualification, during which the product is in Manufacture.
That phase of the program, following Qualification, during which theproduct is in Manufacture.
Purchaser.Idaho National Laboratory (INL).
Purchaser.
Qualification. A demonstration that the Manufacturing process, equipment and personnel can produce a Product in compliance with this Specification.
Idaho National Laboratory (INL).Qualification.
Quality Control. The sampling plans, inspections, tests and records required and used during Production to assure that the Product is in compliance with this Specification.
A demonstration that the Manufacturing  
Rejection. Materials, parts, components, or assembly products, which will not be accepted as fulfilling the contract requirements because of noncompliance with this Specification.
: process, equipment andpersonnel can produce a Product in compliance with this Specification.
Requalification. A demonstration that a single or group of manufacturing processes, equipment and personnel can produce a product in compliance with this specification after the original qualification has been completed and becomes invalid.
Quality Control.
Silicide. Uranium metal alloyed with silicon and fabricated per the requirements of Specification TRTR-14. The word "fuel" is a synonym for Silicide.
The sampling plans, inspections, tests and records required andused during Production to assure that the Product is in compliance with thisSpecification.
Specification. All parts and appendixes to this document, its references, drawings, and standards, as may be modified from time to time by contractual document.
Rejection.
StandardFuel Element Assembly. An assembly consisting of the fuel element container with fourteen (14) fuel plates.
Materials, parts, components, or assembly  
PUR-1 SAR                                          Appendix 3-37                            PUR-SARAppedix
: products, which will not beaccepted as fulfilling the contract requirements because of noncompliance withthis Specification.
                                                                                                    -37Rev
Requalification.
: 2. July 23, 2015
A demonstration that a single or group of manufacturing processes, equipment and personnel can produce a product in compliance withthis specification after the original qualification has been completed and becomesinvalid.Silicide.
 
Uranium metal alloyed with silicon and fabricated per the requirements of Specification TRTR-14.
Form 412.09 (Rev. 09)
The word "fuel" is a synonym for Silicide.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                               SPC-382 STANDARD AND CONTROL FUEL                             Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07           Page: 33 of 57 PURDUE UNIVERSITY REACTOR Stray Fuel Particles. Isolated fuel particles lying outside the maximum fuel core outline defined on Drawing 635463.
Specification.
Supplier. The primary vendor selected by INL to manufacture the product.
All parts and appendixes to this document, its references,  
User. Purdue University, at West Lafayette, Indiana.
: drawings, and standards, as may be modified from time to time by contractual document.
6.2     Purchaser Tests None 6.3   Submittals The following data and records shall be supplied to the purchaser in the quantities stated. The purchaser's approval, prior to implementation, is required on those marked with an asterisk. All records and data shall be maintained by the supplier for the duration of the Purdue University fuel element contract.
Standard Fuel Element Assembly.
The granting of approval by the purchaser of design, working drawings, specifications, requests, and other technical data submitted by the supplier under the provisions of the subcontract or specification shall not affect or relieve the supplier from such responsibility as the supplier has with respect to adequacy or correctness of the design, working drawings specifications, reports, and other technical data.
An assembly consisting of the fuel elementcontainer with fourteen (14) fuel plates.PUR-1 SARAppendix 3-37PUR- SARAppedix  
 
-37Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
====6.3.1 Preproduction====
SPC-382STANDARD AND CONTROL FUEL Revision:
Documents requiring approval must be submitted prior to production use. The number of copies shall be as specified by the Vendor Data Schedule. These documents include:
1ELEMENTS
                            -   *A detailed description as to the weighing procedure by which the supplier proposes to assign Plate U-235 content as required in Section 4.3.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 33 of 57PURDUE UNIVERSITY REACTORStray Fuel Particles.
                            -   Included in the description must be sampling, analytical, and quality control procedures; a statement as to the established accuracy and precision of the assigned fuel plate and fuel element U-23 5 content; developmental and production data in support of the accuracy and precision estimate; and data which at the 95% confidence level, shows that the method used to assign U-235 values has a bias which is less than 0.2% relative
Isolated fuel particles lying outside the maximum fuel coreoutline defined on Drawing 635463.Supplier.
                            -   *A detailed description as to the manner the supplier will use to verify' the fuel Plate U-235 value as required by Section 4.3 PUR-1 SAR                                          Appendix 3-38                              FUR-SARAppedix
The primary vendor selected by INL to manufacture the product.User. Purdue University, at West Lafayette, Indiana.6.2 Purchaser TestsNone6.3 Submittals The following data and records shall be supplied to the purchaser in the quantities stated. The purchaser's  
                                                                                                      -38Rev
: approval, prior to implementation, is required on thosemarked with an asterisk.
: 2. July 23, 2015
All records and data shall be maintained by the supplierfor the duration of the Purdue University fuel element contract.
 
The granting of approval by the purchaser of design, working drawings, specifications,  
Form 412.09 (Rev. 09)
: requests, and other technical data submitted by the supplier underthe provisions of the subcontract or specification shall not affect or relieve thesupplier from such responsibility as the supplier has with respect to adequacy orcorrectness of the design, working drawings specifications,  
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                                 SPC-382 STANDARD AND CONTROL FUEL                             Revision:         1 ELEMENTS - ASSEMBLED FOR THE                             Effective Date: 01/24/07             Page: 34 of 57 PURDUE UNIVERSITY REACTOR
: reports, and othertechnical data.6.3.1 Preproduction:
                            -   *AlI fabrication, assembly, cleaning, surface treating, handling, and decontamination procedures (not to be construed as an outline)
Documents requiring approval must be submitted prior to production use. The number of copies shall be as specified by the Vendor DataSchedule.
                                *AlI production test, inspection, and quality control procedures, including all nondestructive and destructive tests and all standards and sampling section drawings. All data from these tests, including but not limited to: radiographs, metallographic samples, ultrasonic testing traces, and qualification yield rates
These documents include:-*A detailed description as to the weighing procedure by which thesupplier proposes to assign Plate U-235 content as required inSection 4.3.-Included in the description must be sampling, analytical, and qualitycontrol procedures; a statement as to the established accuracy andprecision of the assigned fuel plate and fuel element U-23 5 content;developmental and production data in support of the accuracy andprecision estimate; and data which at the 95% confidence level, showsthat the method used to assign U-235 values has a bias which is lessthan 0.2% relative-*A detailed description as to the manner the supplier will use to verify'the fuel Plate U-235 value as required by Section 4.3PUR-1 SARAppendix 3-38FUR- SARAppedix  
                            -   *All packaging, storage and shipping procedures
-38Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
 
SPC-382STANDARD AND CONTROL FUEL Revision:
====6.3.2 Pre-repair====
1ELEMENTS
                        *All repair programs and procedures prior to use.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 34 of 57PURDUE UNIVERSITY REACTOR-*AlI fabrication,  
6.3.3   Manufacturinu Schedule:
: assembly, cleaning, surface treating,  
                        *A schedule using a purchaser approved technique.
: handling, anddecontamination procedures (not to be construed as an outline)*AlI production test, inspection, and quality control procedures, including all nondestructive and destructive tests and all standards andsampling section drawings.
6.3.3.1        Reports.
All data from these tests, including but notlimited to: radiographs, metallographic  
: 1. Biweekly qualifications phase summary status report. The first such report shall be initiated 1 month after date of contract award.
: samples, ultrasonic testingtraces, and qualification yield rates-*All packaging, storage and shipping procedures 6.3.2 Pre-repair:
: 2. Three (3) copies of a monthly report detailing program~
*All repair programs and procedures prior to use.6.3.3 Manufacturinu Schedule:
progress against a previously submitted schedule shall be supplied by the supplier to the purchaser. Report type, format and submittal schedule shall be as agreed upon between the purchaser and supplier.
*A schedule using a purchaser approved technique.
6.3.4   Delivery Submittals:
6.3.3.1Reports.1. Biweekly qualifications phase summary status report. Thefirst such report shall be initiated 1 month after date ofcontract award.2. Three (3) copies of a monthly report detailing program~progress against a previously submitted schedule shall besupplied by the supplier to the purchaser.
Three copies (except as noted) of the following data and records shall be sent prior to or accompany the shipments. The supplier shall maintain copies of these records for at least 10 years and until the supplier has received written approval from the purchaser for disposition or disposal:
Report type,format and submittal schedule shall be as agreed uponbetween the purchaser and supplier.
                            -   Certification of product compliance to the requirements of this specification to include any test data pertaining thereto
6.3.4 Delivery Submittals:
                            -   Supplier's core compact data sheets, with individual fuel plate uranium composition data including:
Three copies (except as noted) of the following data and records shall besent prior to or accompany the shipments.
                        -       Serial number with batch (see def.) identification PUR-1 SAR                                            Appendix 3-39                                PUR-SARAppedix
The supplier shall maintaincopies of these records for at least 10 years and until the supplier hasreceived written approval from the purchaser for disposition or disposal:
                                                                                                          -39Rev
-Certification of product compliance to the requirements of thisspecification to include any test data pertaining thereto-Supplier's core compact data sheets, with individual fuel plate uraniumcomposition data including:
: 2. July 23, 2015
-Serial number with batch (see def.) identification PUR-1 SARAppendix 3-39PUR- SARAppedix  
 
-39Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Form 412.09 (Rev. 09)
SPC-382STANDARD AND CONTROL FUEL Revision:
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                               SPC-382 STANDARD AND CONTROL FUEL                             Revision:       1 ELEMENTSpRU UIEST-ASSEMBLEDRECoFOR THE                   Effective Date: 01/24/07           Page: 35 of 57 Uranium content Fuel plate core weight U-23 5 enrichment Total quantity U-235 content Core void density data
1ELEMENTSpRU UIEST- ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 35 of 57Uranium contentFuel plate core weightU-23 5 enrichment Total quantity U-235 contentCore void density data-Individual fuel element composition data, including:
                            -   Individual fuel element composition data, including:
Uranium contentU-235 contentSerial number of each plate in the element-Radiation count from fuel plate and fuel element exterior as required bySection 3.5.3 and 4.11. The counting period, counter, background, efficiency, and type of counter used shall be reported-List of all applicable waivers and deviations and related fuel plates orfuel elements-If performed, documented evidence of the performance and test resultsof the boehimite formation from the fuel element surface treatment perSection 3.8.6.3.5 Fuel Plate Radiographs:
Uranium content U-235 content Serial number of each plate in the element
Fuel plate radiographs of all accepted fuel plates required by Sections 4.4and 4.5 and Appendix A shall be sent to the user.6.3.6 Core Compact Data Sheets:Supplier's fuel core compact data sheets shall be supplied to the INLQuality Assurance Representative as they are generated.
                            -   Radiation count from fuel plate and fuel element exterior as required by Section 3.5.3 and 4.11. The counting period, counter, background, efficiency, and type of counter used shall be reported
6.3.7 Report of Production by Unapproved Process:Whenever the supplier's previously submitted and approved processcontrol limits are exceeded, or any material or fuel element components are fabricated using equipment, personnel, or processes which are notpurchaser
                            -   List of all applicable waivers and deviations and related fuel plates or fuel elements
: approved, the time, nature, description, corrective action to betaken, and proposed further corrective action shall be reportedimmediately by the supplier, with a written report to the purchaser tofollow within 10 working days.PUR-1 SARAppendix 3-40PUR- SARAppedix  
                            -   If performed, documented evidence of the performance and test results of the boehimite formation from the fuel element surface treatment per Section 3.8.
-40Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
6.3.5   Fuel Plate Radiographs:
SPC-382STANDARD AND CONTROL FUEL Revision:
Fuel plate radiographs of all accepted fuel plates required by Sections 4.4 and 4.5 and Appendix A shall be sent to the user.
1ELEMENTS
6.3.6   Core Compact Data Sheets:
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 36 of 57PURDUE UNIVERSITY REACTOR1. T Samples.
Supplier's fuel core compact data sheets shall be supplied to the INL Quality Assurance Representative as they are generated.
Transverse to be taken equally space along Fuel Core length.2. L Samples.
6.3.7   Report of Production by Unapproved Process:
Longitudinal to be taken at centerline and to include the Dogbone Area.TilT34I JLiT[- II I+/- +I IL11LL 1I I-I-I IFigure 1. Purdue University Fuel Plate Sampling Procedures For Destructive Tests.PUR-1 SARAppendix 3-41PUR- SARAppedix  
Whenever the supplier's previously submitted and approved process control limits are exceeded, or any material or fuel element components are fabricated using equipment, personnel, or processes which are not purchaser approved, the time, nature, description, corrective action to be taken, and proposed further corrective action shall be reported immediately by the supplier, with a written report to the purchaser to follow within 10 working days.
-41Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
PUR-1 SAR                                            Appendix 3-40                              PUR-SARAppedix
SPC-382STANDARD AND CONTROL FUEL Revision:
                                                                                                        -40Rev
1ELEMENTSpR E UIEST- ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 37 of 57APPENDIX ARequirements for Radiography of Purdue University Fuel Plates1. ScopeThis specification provides requirements for radiography of Purdue University reactorfuel plates, acceptable film quality and film identification.
: 2. July 23, 2015
: 2. Requirements A procedure must be writt en to specify the details for achieving acceptable fuel plateradiographs.
 
The procedure must include the requirements given in this specification.
Form 412.09 (Rev. 09)
2.1 Equipment SetupThe voltage shall be 100 k.v.p. with a focal spot size of 5 mm maximum.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                             SPC-382 STANDARD AND CONTROL FUEL                           Revision:         1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date:   01/24/07       Page: 36 of 57 PURDUE UNIVERSITY REACTOR
Thedistance between the focal point and the plate shall be at least twice the length ofthe plate. The focal point shall be centered laterally and longitudinally over theplate or group of plates.2.2 Film2.2.1 The image outline shall be clear and sharp; the film shall be free of runs,streaks, scratches, blurs, and cassette defect that will affect the areacovered by the fuel plates.2.2.2 The film density of all points of the radiograph that correspond to thefuel plate border locations outside the plate core shall providedensitometer readings between 1.5 and 2.7. Film density as read over thenominal density standards shall provide densitometer readings between0.9 and 1.5.2.2.3 The film shall be extreme sensitivity, extra fine grain, high contrast, double emulsion, industrial x-ray type, (Kodak type M or equal) which isacceptable to the purchaser.
: 1.     T Samples. Transverse to be taken equally space along Fuel Core length.
Development of the film shall be inaccordance with the manufacturer's recommendation.
: 2.     L Samples. Longitudinal to be taken at centerline and to include the Dogbone Area.
2.2.4 Film Identification Appendix APUR-1 SAR Appendix 3-42 Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Til                        T3            4 I                                        J
SPC-382STANDARD AND CONTROL FUEL Revision:
[-                                                   I I                                                                     I
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                            +/-                                       +
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 38 of 57PURDUE UNIVERSITY REACTOR2.2.5 A system of identification of the film shall be provided by the supplier, which shall show as a minimum:A. Plate lot numberB. Plate type and serial numberC. Orientation of density standardD. Density standard identification E. Date of radiography.
LiT I                                                                     I L11LL                                                                  1 I            I-I-I                       I Figure 1. Purdue University Fuel Plate Sampling Procedures For Destructive Tests.
Appendix APUR-1 SARRevA2.pJuyi23,3201 PUR-1 SANRev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
PUR-1 SAR                                          Appendix 3-41                            PUR-SARAppedix
SPC-382STANDARD AND CONTROL FUEL Revision:
                                                                                                    -41Rev
1ELEMENTS
: 2. July 23, 2015
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 39 of 57PURDUE UNIVERSITY REACTORAPPENDIX BWelding Requirements and Qualification for Purdue University FuelElements1. ScopeThe requirements for welding and for the evaluation of welds applicable to the PurdueUniversity Fuel Element Container and components are established by this Appendix.
 
1.1 Application.
Form 412.09 (Rev. 09)
This document defines requirements for the following:
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                               SPC-382 STANDARD AND CONTROL FUEL                             Revision:       1 ELEMENTSpR E UIEST-ASSEMBLEDRECoFOR THE                   Effective Date: 01/24/07         Page: 37 of 57 APPENDIX A Requirements for Radiography of Purdue University Fuel Plates
1.1.1 Welding procedure qualification.
: 1. Scope This specification provides requirements for radiography of Purdue University reactor fuel plates, acceptable film quality and film identification.
1.1.2 Performance qualification of welders, welding equipment, and specialfixturing.
: 2.     Requirements A procedure must be writt en to specify the details for achieving acceptable fuel plate radiographs. The procedure must include the requirements given in this specification.
1.1.3 Information to be included in welding procedure specifications.
2.1     Equipment Setup The voltage shall be 100 k.v.p. with a focal spot size of 5 mm maximum. The distance between the focal point and the plate shall be at least twice the length of the plate. The focal point shall be centered laterally and longitudinally over the plate or group of plates.
1.1.4 Application of qualified procedures to production welding.1.1.5 Destructive testing and nondestructive examination for qualification andfor production welding.1.2 Special Limitations for Applicability.
2.2     Film 2.2.1     The image outline shall be clear and sharp; the film shall be free of runs, streaks, scratches, blurs, and cassette defect that will affect the area covered by the fuel plates.
The requirements contained in thisappendix are to some degree based on RDT F6-2T. Those requirements applicable to Manual, GTAW, single pass, welding of Plug Joint welds, CornerJoint welds, and Partial Penetration Butt Joint welds have been included in thisappendix.
2.2.2     The film density of all points of the radiograph that correspond to the fuel plate border locations outside the plate core shall provide densitometer readings between 1.5 and 2.7. Film density as read over the nominal density standards shall provide densitometer readings between 0.9 and 1.5.
The introduction of a new weld design or weld process requiring achange in these limited parameters would require an appropriate review of RDTF6-2T for requirements applicable to the new parameters.
2.2.3     The film shall be extreme sensitivity, extra fine grain, high contrast, double emulsion, industrial x-ray type, (Kodak type M or equal) which is acceptable to the purchaser. Development of the film shall be in accordance with the manufacturer's recommendation.
1.3 Definitions.
2.2.4     Film Identification Appendix A PUR-1 SAR                                           Appendix 3-42                             Rev 2. July 23, 2015
Arc Strike. Any localized  
 
: melting, heat affected zones, or change in the contour ofthe surface of the finished weld or adjacent base metal resulting from an arc orheat generated by the passage of electrical energy between the weld or base metaland a current source; such as welding electrodes, electron beams, ground clamps,high frequency arc, etc.Automatic Welding.
Form 412.09 (Rev. 09)
Welding with equipment which performs the entire weldingoperation without constant observation and adjustment of controls by an operator.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY                     Identifier:     SPC-382 STANDARD AND CONTROL FUEL                       Revision:       1 ELEMENTS      - ASSEMBLED FOR THE                 Effective Date: 01/24/07         Page: 38 of 57 PURDUE UNIVERSITY REACTOR 2.2.5   A system of identification of the film shall be provided by the supplier, which shall show as a minimum:
The equipment may or may not perform the loading and unloading of the work.Appendix BPUR-1 SAR Appendix 3-44 Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
A.     Plate lot number B.     Plate type and serial number C.     Orientation of density standard D.     Density standard identification E.     Date of radiography.
SPC-382STANDARD AND CONTROL FUEL Revision:
Appendix A PUR-1     SARRevA2.pJuyi23,3201 PUR-1 SAN                                                                                Rev 2. July 23, 2015
1ELEMENTS
 
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 40 of 57PURDUE UNIVERSITY REACTORFace of Weld. The exposed surface of a weld on the side from which welding wasdone.Face Reinforcement.
Form 412.09 (Rev. 09)
Reinforcement of weld at the side of the joint from whichwelding was done.Heat. A single homogeneous melt of metal or alloy.Joint Penetration.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                         Revision:       1 ELEMENTS - ASSEMBLED FOR THE                         Effective Date: 01/24/07       Page: 39 of 57 PURDUE UNIVERSITY REACTOR APPENDIX B Welding Requirements and Qualification for Purdue University Fuel Elements
The minimum depth a groove or flange weld extends from itsface into a joint, exclusive of reinforcement.
: 1. Scope The requirements for welding and for the evaluation of welds applicable to the Purdue University Fuel Element Container and components are established by this Appendix.
Machine Welding.
1.1   Application. This document defines requirements for the following:
Welding with equipment which performs the weldingoperations under the constant observation and control of an operator.
1.1.1     Welding procedure qualification.
Theequipment may or may not perform the loading and unloading of the work.Position of Welding.
1.1.2     Performance qualification of welders, welding equipment, and special fixturing.
The terms related to positions of welding for joint types andwelding processes and the position limits are defined in Section IX, ASME Boilerand Pressure Vessel Code.Repair. The process of restoring a nonconforming item characteristic to anacceptable condition, although it does not conform to a specified requirement.
1.1.3     Information to be included in welding procedure specifications.
Rework. The process by which a nonconforming item is made to conform tospecified requirements.
1.1.4   Application of qualified procedures to production welding.
Root of a Joint. That portion of a joint to be welded where the members approachclosest to each other. In cross section the root of the joint may be a point, a lineor an area.Root of a Weld. The points, as shown in cross section, at which the back of theweld intersects the base metal surfaces.
1.1.5     Destructive testing and nondestructive examination for qualification and for production welding.
Root Penetration.
1.2   Special Limitations for Applicability. The requirements contained in this appendix are to some degree based on RDT F6-2T. Those requirements applicable to Manual, GTAW, single pass, welding of Plug Joint welds, Corner Joint welds, and Partial Penetration Butt Joint welds have been included in this appendix. The introduction of a new weld design or weld process requiring a change in these limited parameters would require an appropriate review of RDT F6-2T for requirements applicable to the new parameters.
The depth a groove weld extends into the root of a jointmeasured on the centerline of the root cross section.Root Reinforcement.
1.3   Definitions.
Reinforcement of weld at the side opposite that from whichwelding was done.Root Surface.
Arc Strike. Any localized melting, heat affected zones, or change in the contour of the surface of the finished weld or adjacent base metal resulting from an arc or heat generated by the passage of electrical energy between the weld or base metal and a current source; such as welding electrodes, electron beams, ground clamps, high frequency arc, etc.
The exposed surface of a weld on the side opposite that from whichwelding was done.Size of a Groove Weld. The joint penetration (depth of chamfering plus rootpenetration when specified).
Automatic Welding. Welding with equipment which performs the entire welding operation without constant observation and adjustment of controls by an operator.
Appendix BAppendix 3-45 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
The equipment may or may not perform the loading and unloading of the work.
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
Appendix B PUR-1 SAR                                       Appendix 3-44                           Rev 2. July 23, 2015
1ELEMENTS
 
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 41of5PURDUE UNIVERSITY REACTORUndercut.
Form 412.09 (Rev. 09)
A groove melted into the base metal adjacent to the toe or root of aweld and left unfilled by weld metal.Underfill.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07         Page: 40 of 57 PURDUE UNIVERSITY REACTOR Face of Weld. The exposed surface of a weld on the side from which welding was done.
A depression on the face of the weld or root surface extending belowthe surface of the adjacent base metal.Welder and Welding Operator Performance Qualification.
Face Reinforcement. Reinforcement of weld at the side of the joint from which welding was done.
The tests todemonstrate a welder's or welding operator's ability to produce welds meetingprescribed standards.
Heat. A single homogeneous melt of metal or alloy.
Welder. One who is capable of performing a manual or semiautomatic weldingoperation (sometimes erroneously used to denote a welding machine).
Joint Penetration.The minimum depth a groove or flange weld extends from its face into a joint, exclusive of reinforcement.
Welding Operator.
Machine Welding. Welding with equipment which performs the welding operations under the constant observation and control of an operator. The equipment may or may not perform the loading and unloading of the work.
One who operates machine or automatic welding equipment.
Position of Welding. The terms related to positions of welding for joint types and welding processes and the position limits are defined in Section IX, ASME Boiler and Pressure Vessel Code.
Welding Procedure Qualification.
Repair. The process of restoring a nonconforming item characteristic to an acceptable condition, although it does not conform to a specified requirement.
The test to demonstrate that welds made by aspecified procedure can meet prescribed standards.
Rework. The process by which a nonconforming item is made to conform to specified requirements.
Welding Procedure Specifcation.
Root of a Joint. That portion of a joint to be welded where the members approach closest to each other. In cross section the root of the joint may be a point, a line or an area.
A written welding procedure which specifies the detailed methods and practices to be used in the production of a weldment andhow they shall be carried out. A specification includes all elements of aprocedure necessary to produce a satisfactory weldment.
Root of a Weld. The points, as shown in cross section, at which the back of the weld intersects the base metal surfaces.
Examples of some ofthe elements included in a specification are: material used, preparation of basematerials, preheat and postheat  
Root Penetration.The depth a groove weld extends into the root of a joint measured on the centerline of the root cross section.
: cleaning, assembly method and sequence, fixturing, heat treatments, joint welding procedures, preweld and postweldnondestructive examinations, repair, rework, etc.Welding Procedure.
Root Reinforcement. Reinforcement of weld at the side opposite that from which welding was done.
The detailed methods and practices including all jointwelding procedures.
Root Surface. The exposed surface of a weld on the side opposite that from which welding was done.
: 2. Reference DocumentThe following documents are a part of this appendix to the extent specified herein. Theissue of a document in effect on the date of the invitation to bid, including anyamendments also in effect on that date, shall apply unless otherwise specified.
Size of a Groove Weld. The joint penetration (depth of chamfering plus root penetration when specified).
Wherethis appendix appears to conflict with the requirements of a reference  
Appendix B PUR-1 SAR                                          Appendix 3-45                           Rev 2. July 23, 2015
: document, suchconflict shall be brought to the attention of the purchaser for resolution.
 
Appendix BPUR-1 SAR Appendix 3-46 Rev 2. July 23, 2015.
Form 412.09 (Rev. 09)
Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                             SPC-382of5 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07         Page: 41of5 PURDUE UNIVERSITY REACTOR Undercut. A groove melted into the base metal adjacent     to the toe or root of a weld and left unfilled by weld metal.
SPC-382STANDARD AND CONTROL FUEL Revision:
Underfill. A depression on the face of the weld or root surface extending below the surface of the adjacent base metal.
1ELEMENTS
Welder and Welding OperatorPerformance Qualification. The tests to demonstrate a welder's or welding operator's ability to produce welds meeting prescribed standards.
-ASSEMBLED FOR TILE Effective Date: 01/24/07 Page: 42 of 57PURDUE UNIVERSITY REACTOR2.1 American Society for Testing and Materials (ASTM) Standards 2.1.1 ASTM E2, Preparation of Micrograplis of Metals and Alloys2.1.2 ASTM E3, Preparation of Metallographic Specimen2.2 American Society of Mechanical Engineers (ASME) Codes2.2.1 ASME Boiler and Pressure Vessel Code, Section IX, WeldingQualifications 2.3 American Welding Society (AWS) Standards 2.3.1 AWS A2.2, Nondestructive Testing Symbols2.3.2 AWS A3.0, Terms and Definitions
Welder. One who is capable of performing a manual or semiautomatic welding operation (sometimes erroneously used to denote a welding machine).
: 3. Weld Qualification Requirements 3.1 General Reqiuirements Appendix BPUR-1 SARRevA2.pJuyi23,3201 PUR-1 SARRev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Welding Operator. One who operates machine or automatic welding equipment.
SPC-382STANDARD AND CONTROL FUEL Revision:
Welding Procedure Qualification. The test to demonstrate that welds made by a specified procedure can meet prescribed standards.
1ELEMENTS
Welding ProcedureSpecifcation. A written welding procedure which specifies the detailed methods and practices to be used in the production of a weldment and how they shall be carried out. A specification includes all elements of a procedure necessary to produce a satisfactory weldment. Examples of some of the elements included in a specification are: material used, preparation of base materials, preheat and postheat cleaning, assembly method and sequence, fixturing, heat treatments, joint welding procedures, preweld and postweld nondestructive examinations, repair, rework, etc.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 43 of 57PURDUE UNIVERSITY REACTOR3.1.1 All welding procedures,  
Welding Procedure.The detailed methods and practices including all joint welding procedures.
: welders, or welding machine operators shall bequalified in accordance with the provisions identified in this Appendix.
: 2.     Reference Document The following documents are a part of this appendix to the extent specified herein. The issue of a document in effect on the date of the invitation to bid, including any amendments also in effect on that date, shall apply unless otherwise specified. Where this appendix appears to conflict with the requirements of a reference document, such conflict shall be brought to the attention of the purchaser for resolution.
3.1.2 Weld Procedure and Performance Qualification Testing previously qualified to these requirements under other contracts may be used.Existing records to support previously qualified procedures andpersonnel are subject to review by the purchaser.
Appendix B PUR-1 SAR                                         Appendix 3-46                               Rev 2. July 23, 2015.
3.1.3 Base materials and filler material shall comply with the requirements ofthe drawings.
 
3.1.4 Welding processes which satisfy the specified requirements and producethe quality required by this Appendix are permissible.
Form 412.09 (Rev. 09)
Weldingprocedures which utilize fluxes and coatings shall not be used.3.1.5 Fixtures:
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                         SPC-382 STANDARD AND CONTROL FUEL                       Revision:       1 ELEMENTS - ASSEMBLED FOR TILE                     Effective Date: 01/24/07       Page: 42 of 57 PURDUE UNIVERSITY REACTOR 2.1   American Society for Testing and Materials (ASTM) Standards 2.1.1   ASTM E2,     Preparation of Micrograplis of Metals and Alloys 2.1.2   ASTM E3,     Preparation of Metallographic Specimen 2.2   American Society of Mechanical Engineers (ASME) Codes 2.2.1   ASME Boiler and Pressure Vessel Code, Section IX, Welding Qualifications 2.3   American Welding Society (AWS) Standards 2.3.1   AWS A2.2, Nondestructive Testing Symbols 2.3.2   AWS A3.0, Terms and Definitions
The capability of fixtures for aligning parts shall bedemonstrated before welding of production parts is initiated.
: 3.     Weld Qualification Requirements 3.1   General Reqiuirements Appendix B PUR-1 SARRevA2.pJuyi23,3201 PUR-1 SAR                                                                              Rev 2. July 23, 2015
If chill barsor blocks are used, the type of material and their location with respect tothe joint shall be included in the procedure specification.
 
3.1.6 Position of Qualification Welds. All procedure and performance qualification test welds shall be made in the same positions as forproduction welds.3.1.7 Special Conditions for Qualification Welds: All procedure andperformance qualification test welds shall be made under conditions which simulate the actual production welding conditions.
Form 412.09 (Rev. 09)
Theseconditions shall include space limitations, joint accessibility, degree ofcomfort due to heat, position and other handicaps or environmental factors which the welder or welding operator will endure during actualproduction welding.3.1.8 Heat Treatment.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                         Effective Date: 01/24/07         Page: 43 of 57 PURDUE UNIVERSITY REACTOR 3.1.1   All welding procedures, welders, or welding machine operators shall be qualified in accordance with the provisions identified in this Appendix.
Weld preheat and postheat treatments shall not be usedwithout prior approval by the purchaser.
3.1.2   Weld Procedure and Performance Qualification Testing previously qualified to these requirements under other contracts may be used.
3.1.9 Interpass Temperature.
Existing records to support previously qualified procedures and personnel are subject to review by the purchaser.
For multi-pass weld, the weld interpass temperature shall not be less than 60&deg; F or greater than 3500 F withoutprior approval by the purchaser.
3.1.3   Base materials and filler material shall comply with the requirements of the drawings.
3.1.10 Records.
3.1.4   Welding processes which satisfy the specified requirements and produce the quality required by this Appendix are permissible. Welding procedures which utilize fluxes and coatings shall not be used.
Records of welding, associated processing, and inspection shall be maintained for all welds. Complete records may consist ofinspection forms, routings, or reference to Operating Procedures or otherdocuments.
 
These records shall include at least the following:
====3.1.5 Fixtures====
Appendix BAppendix 3-48 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
The capability of fixtures for aligning parts shall be demonstrated before welding of production parts is initiated. If chill bars or blocks are used, the type of material and their location with respect to the joint shall be included in the procedure specification.
SPC-382STANDARD AND CONTROL FUEL Revision:
3.1.6   Position of Qualification Welds. All procedure and performance qualification test welds shall be made in the same positions as for production welds.
1ELEMENTS
3.1.7   Special Conditions for Qualification Welds: All procedure and performance qualification test welds shall be made under conditions which simulate the actual production welding conditions. These conditions shall include space limitations, joint accessibility, degree of comfort due to heat, position and other handicaps or environmental factors which the welder or welding operator will endure during actual production welding.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 44 of 57PURDUE UNIVERSITY REACTOR1. Base Material (Type, material specification, heat or lot number).2. Filler Material (Type, material specification, heat or lot number).3. Cleaning procedures.
3.1.8   Heat Treatment. Weld preheat and postheat treatments shall not be used without prior approval by the purchaser.
3.1.9   Interpass Temperature. For multi-pass weld, the weld interpass temperature shall not be less than 60&deg; F or greater than 3500 F without prior approval by the purchaser.
3.1.10   Records. Records of welding, associated processing, and inspection shall be maintained for all welds. Complete records may consist of inspection forms, routings, or reference to Operating Procedures or other documents. These records shall include at least the following:
Appendix B Appendix 3-48                           Rev 2. July 23, 2015 PUR-1 SAR
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                         Revision:       1 ELEMENTS - ASSEMBLED FOR THE                       Effective Date: 01/24/07           Page: 44 of 57 PURDUE UNIVERSITY REACTOR
: 1. Base Material (Type, material specification, heat or lot number).
: 2. Filler Material (Type, material specification, heat or lot number).
: 3. Cleaning procedures.
: 4. Joint identification and weld maps when applicable.
: 4. Joint identification and weld maps when applicable.
: 5. Welding machine type and identification.
: 5. Welding machine type and identification.
Line 774: Line 787:
: 7. Welder or welding operator qualification.
: 7. Welder or welding operator qualification.
: 8. Procedure and performance qualification.
: 8. Procedure and performance qualification.
: 9. Current-voltage data for machine or automatic welding.10. Date welds are made.11. Inert gas mixture, when applicable.
: 9. Current-voltage data for machine or automatic welding.
: 10. Date welds are made.
: 11. Inert gas mixture, when applicable.
: 12. Nondestructive examination procedure.
: 12. Nondestructive examination procedure.
: 13. Nondestructive examination personnel identification.
: 13. Nondestructive examination personnel identification.
: 14. Examinations and tests (nondestructive and destructive) and theresults.15. Photomacro graphs and photomicrographs.
: 14. Examinations and tests (nondestructive and destructive) and the results.
: 15. Photomacro graphs and photomicrographs.
: 16. Metallographic specimens.
: 16. Metallographic specimens.
: 17. If applicable, rework and repair of welds.18. Disposition of welds.3.2 Welding Procedure Specification 3.2.1 The welding procedure specification shall meet the requirements of thisAppendix, and shall be submitted to the purchaser for information.
: 17. If applicable, rework and repair of welds.
3.2.2 The welding procedure specification shall include all essential elementsand details, as required by this section, to cover each joint to be weldedby the supplier.
: 18. Disposition of welds.
Each joint shall be identified in the welding procedure specification.
3.2   Welding Procedure Specification 3.2.1   The welding procedure specification shall meet the requirements of this Appendix, and shall be submitted to the purchaser for information.
The specification shall include a joint design sketch forAppendix BPUR-1 SARRevA2.pJuyi23,3201 PUR-1 SARRev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UN~IVERSITY Identifier:
3.2.2   The welding procedure specification shall include all essential elements and details, as required by this section, to cover each joint to be welded by the supplier. Each joint shall be identified in the welding procedure specification. The specification shall include a joint design sketch for Appendix B SARRevA2.pJuyi23,3201 PUR-1 PUR-1 SAR                                                                                  Rev 2. July 23, 2015
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
 
1ELEMENTS
Form 412.09 (Rev. 09)
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 45of5PURDUE UNIVERSITY REACTOReach joint welding procedure even if the specification references drawingnumbers.3.2.3 The following basic information and essential variables shall be includedin sufficient detail to assure that compliance with the requirements of thespecification can be verified:
Idaho National Laboratory SPECIFICATION FOR PURDUE UN~IVERSITY Identifier:                           SPC-382of5 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07         Page: 45of5 PURDUE UNIVERSITY REACTOR each joint welding procedure even if the specification references drawing numbers.
3.2.3   The following basic information and essential variables shall be included in sufficient detail to assure that compliance with the requirements of the specification can be verified:
: 1. Basic Information
: 1. Basic Information
: a. Joint Design: (the joint geometry, fit-up, and other requireddimensions of the welded j oint) tolerances and materialthickness.
: a. Joint Design: (the joint geometry, fit-up, and other required dimensions of the welded j oint) tolerances and material thickness.
: b. Method of arc initiation
: b. Method of arc initiation
: c. Electrode size (for gas tungsten arc welding)d. Gas type and flow rate (shielding and backing gas)e. Welding current range for manual weldingf. Whether tack welds or fixtures are used for assembly of thejoint for weldingg. Method and frequency of cleaningh. Number of weld layers and passesi. Whether stringer beads or weave beads are used2. Essential Variables
: c. Electrode size (for gas tungsten arc welding)
: d. Gas type and flow rate (shielding and backing gas)
: e. Welding current range for manual welding
: f. Whether tack welds or fixtures are used for assembly of the joint for welding
: g. Method and frequency of cleaning
: h. Number of weld layers and passes
: i. Whether stringer beads or weave beads are used
: 2. Essential Variables
: a. General, All Welding Processes.
: a. General, All Welding Processes.
i.A change from a base material type or grade(materials of the same nominal chemical analysisand mechanical property range, even though adifferent product form) to any other base materialtype or grade. When joints are made between twodifferent types or grades of base material, aprocedure qualification shall be made for theapplicable combinations of materials, even thoughprocedure qualification tests have been made foreach of the two base materials welded to itself.Appendix BAppendix 3-50 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
i.A change from a base material type or grade (materials of the same nominal chemical analysis and mechanical property range, even though a different product form) to any other base material type or grade. When joints are made between two different types or grades of base material, a procedure qualification shall be made for the applicable combinations of materials, even though procedure qualification tests have been made for each of the two base materials welded to itself.
SPC-382STANDARD AND CONTROL FUEL Revision:
Appendix B Appendix 3-50                             Rev 2. July 23, 2015 PUR-1 SAR
1ELEMENTSpRU U VEST- ASSEMBLEDRE oFOR THE Effective Date: 01/24/07 Page: 46 of 57ii. A change of filler metal type or classification to anyother type of classification iii. A change in welding position.
 
iv. A change in vertical welding direction, i.e., fromupward to downward or vice versa.v. The addition or omission of integral backing (e.g.,"butt-lap" type joint).vi. The addition or omission of nonfusing metalretainers.
Form 412.09 (Rev. 09)
vii. The addition or omission of filler metal to the joint.viii. Any change in the method by which filler is added,such as preplaced shims, preplaced wire, preplaced consumable  
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                     SPC-382 STANDARD AND CONTROL FUEL                     Revision:       1 ELEMENTSpRU U ASSEMBLEDRE VEST-           oFOR THE           Effective Date: 01/24/07         Page: 46 of 57 ii. A change of filler metal type or classification to any other type of classification iii. A change in welding position.
: inserts, wire feed, or prior weld metalsurfacing
iv. A change in vertical welding direction, i.e., from upward to downward or vice versa.
("buttering")
: v. The addition or omission of integral backing (e.g.,
of one or both joint faces.ix. The addition or omission or any type of preplaced consumable inserts or joint surfacing.
                                        "butt-lap" type joint).
vi. The addition or omission of nonfusing metal retainers.
vii. The addition or omission of filler metal to the joint.
viii. Any change in the method by which filler is added, such as preplaced shims, preplaced wire, preplaced consumable inserts, wire feed, or prior weld metal surfacing ("buttering") of one or both joint faces.
ix. The addition or omission or any type of preplaced consumable inserts or joint surfacing.
: x. A change in the shape or size of preplaced consumable inserts or joint surfacing.
: x. A change in the shape or size of preplaced consumable inserts or joint surfacing.
xi. A change from multiple pass welds to single passwelds.xii. The omission of inert gas backing during welding,except that requalification is not required where aqualified welding procedure is changed to omit theinert gas backing and then is used only for a singlewelded butt joint with a backing strip, or a filletweld. For multiple pass welding, the omission ofinert gas backing during welding until three layersor 3/16 of weld metal thickness has been deposited, whichever is greatest.
xi. A change from multiple pass welds to single pass welds.
xiii. A change from one welding process to any otherprocess or combination of welding processes.
xii. The omission of inert gas backing during welding, except that requalification is not required where a qualified welding procedure is changed to omit the inert gas backing and then is used only for a single welded butt joint with a backing strip, or a fillet weld. For multiple pass welding, the omission of inert gas backing during welding until three layers or 3/16 of weld metal thickness has been deposited, whichever is greatest.
xiii. A change from one welding process to any other process or combination of welding processes.
: b. Manual Welding, All Welding Processes.
: b. Manual Welding, All Welding Processes.
Appendix BAppendix 3-51 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Appendix B PUR-1 SAR                                  Appendix 3-51                             Rev 2. July 23, 2015
SPC-382STANDARD AND CONTROL FUEL Revision:
 
1ELEMENTS
Form 412.09 (Rev. 09)
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 47 of 57PURDUE UNIVERSITY REACTOR1. An increase in the standard size of filler metal fromthat stated and qualified in the procedure specification.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                 SPC-382 STANDARD AND CONTROL FUEL                 Revision:       1 ELEMENTS - ASSEMBLED FOR THE               Effective Date: 01/24/07       Page: 47 of 57 PURDUE UNIVERSITY REACTOR
ii. A change in joint geometry which violates thetolerances given for the joint geometry elementslisted below:Bevel Angle: State in procedure specification.
: 1. An increase in the standard size of filler metal from that stated and qualified in the procedure specification.
Tolerance:-
ii. A change in joint geometry which violates the tolerances given for the joint geometry elements listed below:
Minus 5%.Groove Angle: State in procedure specification.
Bevel Angle: State in procedure specification.
Tolerance:
Tolerance:- Minus 5%.
Minus 5%Alignment Tolerance:
Groove Angle: State in procedure specification.
Assign value inprocedure specification.
Tolerance: Minus 5%
Qualify procedure forsingle welded joints using maximumpermissible misalignment in a portion of thejoint.c. Gas Tungsten Arc Process.1. A change of electrode material type.ii. A change in arc starting methods.iii. A change from a single shielding gas to any othershielding gas or to a mixture of shielding gases or achange in specified composition of gas mixture.iv. A decrease in shielded gas flow rate of more thanten percent.Appendix BAppendix 3-52 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Alignment Tolerance: Assign value in procedure specification. Qualify procedure for single welded joints using maximum permissible misalignment in a portion of the joint.
SPC-382STANDARD AND CONTROL FUEL Revision:
: c. Gas Tungsten Arc Process.
1ELEMENTS
: 1. A change of electrode material type.
-ASSEMBLED FOR THE Effective Date: 01/24/07PURDUE UNIVERSITY REACTOR3.3 Welding Procedure Qualification Page: 48 of 573.3.1 The welding procedure shall be qualified to the requirements of thissection.3.3.2 All welding used in qualifying a welding procedure shall be performed in accordance with a welding procedure specification.
ii. A change in arc starting methods.
3.3.3 Before any welding is performed on production components, the suppliershall qualify each proposed welding procedure by:1. Recording all essential elements of the welding procedure in awelding procedure specification (see Section 3.2)2. Verifying the welding procedure specification by welding testspecimens representing each joint to be welded in production andperforming nondestructive examination and destructive tests inaccordance with the requirements of this Appendix.
iii. A change from a single shielding gas to any other shielding gas or to a mixture of shielding gases or a change in specified composition of gas mixture.
: 3. Submitting to the purchaser, for information, the weldingprocedure specification and a certified copy of the detailed resultsobtained from the tests performed on the test welds. Themetallographic sections required by this Appendix shall also besubmitted to the purchaser.
iv. A decrease in shielded gas flow rate of more than ten percent.
Appendix BAppendix 3-53 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Appendix B PUR-1 SAR                              Appendix 3-52                           Rev 2. July 23, 2015
SPC-382STANDARD AND CONTROL FUEL Revision:
 
1ELEMENTS
Form 412.09 (Rev. 09)
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 49 of 57PURDUE UNIVERSITY REACTOR3.3.4 Essential Variables.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY                       Identifier:     SPC-382 STANDARD AND CONTROL FUEL                         Revision:       1 ELEMENTS      - ASSEMBLED FOR THE                   Effective Date: 01/24/07        Page: 48 of 57 PURDUE UNIVERSITY REACTOR 3.3   Welding Procedure Qualification 3.3.1   The welding procedure shall be qualified to the requirements of this section.
The welding procedure shall be set us as a newwelding procedure specification and shall be completely re-qualified when any of the changes listed in Section 3.2.3.2 are made in theprocedure.
3.3.2   All welding used in qualifying a welding procedure shall be performed in accordance with a welding procedure specification.
3.3.5 Chart Recordings.
3.3.3   Before any welding is performed on production components, the supplier shall qualify each proposed welding procedure by:
Current-voltage-time charts shall be used for eachprocedure qualification weld for automatic or machine welding.Calibrated current and voltage indicating meters may be substituted fortrace chart type equipment for manual welding.
: 1. Recording all essential elements of the welding procedure in a welding procedure specification (see Section 3.2)
The current and voltageranges shall be recorded for manual welding.3.4 Welder Performance Qualification 3.4.1 Performance qualification weld tests shall meet the requirements of thissection, except that any welder used to qualify the welding procedure shall also be considered qualified and additional performance weld testsare not required.
: 2. Verifying the welding procedure specification by welding test specimens representing each joint to be welded in production and performing nondestructive examination and destructive tests in accordance with the requirements of this Appendix.
3.4.2 General.1. The performance qualification tests are intended to determine theability of welders to make sound welds.2. The performance test may be terminated at any stage of the testingprocedure whenever it becomes apparent to the supervisor conducting the tests that the welder does not have skill required toproduce satisfactory results.
: 3. Submitting to the purchaser, for information, the welding procedure specification and a certified copy of the detailed results obtained from the tests performed on the test welds. The metallographic sections required by this Appendix shall also be submitted to the purchaser.
In this event, the welder may be re-tested at the discretion of the supplier in accordance with 3.4.3.3. Each supplier shall maintain a record of the procedures, including the essential variables, under which welders are examined and theresults of the examinations.
Appendix B Appendix 3-53                           Rev 2. July 23, 2015 PUR-1 SAR
3.4.3 Qualification of Welders.1. Each welder shall pass the tests prescribed for procedure qualification except that tensile tests are not required.
 
Theessential variables and the test results obtained by each weldershall be recorded in a Performance Qualification Test Report. Anywelder who performs acceptable welding procedure qualification tests shall be considered qualified.
Form 412.09 (Rev. 09)
: 2. Renewal of Qualification.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                             SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07       Page: 49 of 57 PURDUE UNIVERSITY REACTOR 3.3.4   Essential Variables. The welding procedure shall be set us as a new welding procedure specification and shall be completely re-qualified when any of the changes listed in Section 3.2.3.2 are made in the procedure.
Requalification of a welder is requiredwhen:Appendix BAppendix 3-54 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
3.3.5   Chart Recordings. Current-voltage-time charts shall be used for each procedure qualification weld for automatic or machine welding.
SPC-3 82STANDARD AND CONTROL FUEL Revision:
Calibrated current and voltage indicating meters may be substituted for trace chart type equipment for manual welding. The current and voltage ranges shall be recorded for manual welding.
1ELEMENTS
3.4   Welder Performance Qualification 3.4.1   Performance qualification weld tests shall meet the requirements of this section, except that any welder used to qualify the welding procedure shall also be considered qualified and additional performance weld tests are not required.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 50 of 57PURDUE UNIVERSITY REACTORa. 90 or more days have elapsed since he last producedacceptable welds using the specific welding process, orb. He has not performed acceptable welds using theproduction welding procedure.
3.4.2   General.
: c. Any time there is a specific reason to question a welder'sability to make welds meeting the requirements of thisAppendix, requalification shall be required.
: 1. The performance qualification tests are intended to determine the ability of welders to make sound welds.
Only one testweld shall be required for renewal of qualification.
: 2. The performance test may be terminated at any stage of the testing procedure whenever it becomes apparent to the supervisor conducting the tests that the welder does not have skill required to produce satisfactory results. In this event, the welder may be re-tested at the discretion of the supplier in accordance with 3.4.3.
If thistest weld fails to meet all of the original requirements, thena complete performance requalification shall be required.
: 3. Each supplier shall maintain a record of the procedures, including the essential variables, under which welders are examined and the results of the examinations.
3.4.4 Chart Recordings.
3.4.3   Qualification of Welders.
Current-voltage-time charts shall be used for eachprocedure and performance qualification weld for automatic or machinewelding.
: 1. Each welder shall pass the tests prescribed for procedure qualification except that tensile tests are not required. The essential variables and the test results obtained by each welder shall be recorded in a Performance Qualification Test Report. Any welder who performs acceptable welding procedure qualification tests shall be considered qualified.
Calibrated current and voltage indicating meters may besubstituted for trace chart type equipment for manual welding.
: 2. Renewal of Qualification. Requalification of a welder is required when:
Thecurrent and voltage ranges shall be recorded for manual welding.3.5 Welding Machine Qualification 3.5.1 Performance qualification weld tests shall meet the requirements of thissection, except that any welding machine used to qualify the weldingprocedure shall also be considered qualified and additional performance weld tests are not required.
Appendix B PUR-1 SAR                                          Appendix 3-54                           Rev 2. July 23, 2015
: 1. The performance qualification tests are intended to determine theability of welding machines to make sound welds.2. Any time there is a specific reason to question a weldingmachine's ability to make welds meeting the requirements of thisAppendix, requalification shall be required.
 
Only one test weldshall be required for renewal of qualification.
Form 412.09 (Rev. 09)
If this test weld failsto meet all of the original requirements, then a completeperformance requalification shall be required.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                             SPC-3 82 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                           Effective Date: 01/24/07         Page: 50 of 57 PURDUE UNIVERSITY REACTOR
Welding machinesused for the manual welding of any successful procedure or welderqualification tests shall be considered qualified for manual weldingof all core components covered in this Appendix.
: a. 90 or more days have elapsed since he last produced acceptable welds using the specific welding process, or
Appendix BAR Appendix 3-55 Rev 2. July 2PUR-1 SI3, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: b. He has not performed acceptable welds using the production welding procedure.
SPC-382 5STANDARD AND CONTROL FUEL Revision:
: c. Any time there is a specific reason to question a welder's ability to make welds meeting the requirements of this Appendix, requalification shall be required. Only one test weld shall be required for renewal of qualification. If this test weld fails to meet all of the original requirements, then a complete performance requalification shall be required.
1ELEMENTSpRU UIEST- ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 51 of 53.5.2 Welding machines used for the manual welding of any successful welderperformance qualification tests shall be considered qualified for manualwelding of all components covered in this session.3.6 Examination  
3.4.4   Chart Recordings. Current-voltage-time charts shall be used for each procedure and performance qualification weld for automatic or machine welding. Calibrated current and voltage indicating meters may be substituted for trace chart type equipment for manual welding. The current and voltage ranges shall be recorded for manual welding.
& Tests3.6.1 Type of Test Required.
3.5   Welding Machine Qualification 3.5.1   Performance qualification weld tests shall meet the requirements of this section, except that any welding machine used to qualify the welding procedure shall also be considered qualified and additional performance weld tests are not required.
The following tests shall be used for thequalification of welding procedures and / or welders as applicable:
: 1. The performance qualification tests are intended to determine the ability of welding machines to make sound welds.
: 1. Nondestructive examination by a liquid penetrant method.2. Nondestructive examination by Visual to test for soundness andsurface characteristics of the weld.3. Destructive examination by sectioning for metallo graphicexamination of weld joints and adjacent areas to test for fusion,weld geometry, weld reinforcement, and soundness of the weld.4. When the purchaser has reason to believe that the quality of anyweldment is doubtful, he may require additional inspection.
: 2. Any time there is a specific reason to question a welding machine's ability to make welds meeting the requirements of this Appendix, requalification shall be required. Only one test weld shall be required for renewal of qualification. If this test weld fails to meet all of the original requirements, then a complete performance requalification shall be required. Welding machines used for the manual welding of any successful procedure or welder qualification tests shall be considered qualified for manual welding of all core components covered in this Appendix.
: 5. Nondestructive Examination and Testsa. Visual. The test weld shall be examined visually prior towelding and after welding in accordance with Section 5.1b. Liquid Penetrant.
Appendix B AR                                          Appendix 3-55                             Rev 2. July 2 PUR-1 SI                                                                                                  3, 2015
The test weld shall be examined after the.final layer in accordance with Section 3.6.2.2 using a colorcontrast method.c. Unless otherwise specified, inspection of procedure andperformance qualification welds shall be performed in thefinal surface condition.
 
: 6. Destructive Examination.
Form 412.09 (Rev. 09)
Each test weld shall be sectioned transversely to metallographically examine a minimum of:a. Three section faces for welds on cylindrical components less than 1 'A inch in diameter or for welds that are one tofour inches long on non-cylindrical components.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                             SPC-382                           5 STANDARD AND CONTROL FUEL                         Revision:         1 ELEMENTSpRU UIEST-ASSEMBLEDRECoFOR THE                 Effective Date: 01/24/07           Page: 51 of 5 3.5.2   Welding machines used for the manual welding of any successful welder performance qualification tests shall be considered qualified for manual welding of all components covered in this session.
: b. Four sections faces for welds in cylindrical components that are greater than 11/4'/ inch in diameter or for welds thatare greater than four inches long on non-cylindrical components.
3.6   Examination & Tests 3.6.1   Type of Test Required. The following tests shall be used for the qualification of welding procedures and / or welders as applicable:
Appendix BARAppendix 3-56 Rev 2. July2PUR-1 St.33, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: 1. Nondestructive examination by a liquid penetrant method.
SPC-382STANDARD AND CONTROL FUEL Revision:
: 2. Nondestructive examination by Visual to test for soundness and surface characteristics of the weld.
1ELEMENTS
: 3. Destructive examination by sectioning for metallo graphic examination of weld joints and adjacent areas to test for fusion, weld geometry, weld reinforcement, and soundness of the weld.
-. ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 52 of 57PURDUE UNIVERSITY REACTORc. One section face for plug welds, arc spot welds, and weldsthat are less than one inch long on non-cylindrical components.
: 4. When the purchaser has reason to believe that the quality of any weldment is doubtful, he may require additional inspection.
: d. The cross section shall be polished and etched to provideclear definition of the structure in the fusion zone and theheat-affected zones.e. For welds in (a) and (b) of this paragraph, one cross sectionshall be made through a weld start and a weld stop area andthe remaining sections shall be made at random. For welddescribed in (c) of this paragraph, the cross section shall bemade at the approximate centerline of the weld.Examination of the welds shall be in accordance withSection 3.6.2.3.3.6.2 Acceptance Criteria for Qualification Test Welds1. Visual Examination.
: 5. Nondestructive Examination and Tests
Visual examination shall be in accordance with Section 5.1.2. Liquid Penetrant Examination.
: a. Visual. The test weld shall be examined visually prior to welding and after welding in accordance with Section 5.1
Unless otherwise specified, finalweld surfaces shall be examined using a color contrast method.a. For welded joints in materials less than 1/8 inch thick thefollowing relevant indications are unacceptable.
: b. Liquid Penetrant. The test weld shall be examined after the.
: 1. Any cracks.ii. Linear indications.
final layer in accordance with Section 3.6.2.2 using a color contrast method.
iii. Indications with dimensions exceeding 1/64 inch.iv. Rounded indication separated by 1/44 inch or lessedge-to-edge.
: c. Unless otherwise specified, inspection of procedure and performance qualification welds shall be performed in the final surface condition.
: v. Five or more rounded indications in any six squareinches of weld surface with the maj or dimension ofthis area not to exceed six inches with the areabeing taken in the most unfavorable locationrelative to the indication being evaluated.
: 6. Destructive Examination. Each test weld shall be sectioned transversely to metallographically examine a minimum of:
: b. For all welds in materials 1/8 inch thick or greater, thefollowing relevant indications are unacceptable.  
: a. Three section faces for welds on cylindrical components less than 1'A inch in diameter or for welds that are one to four inches long on non-cylindrical components.
(OnlyAppendix BAppendix 3-57 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: b. Four sections faces for welds in cylindrical components that are greater than 11/4'/ inch in diameter or for welds that are greater than four inches long on non-cylindrical components.
SPC-382of5 STANDARD AND CONTROL FUEL Revision:
Appendix B ARAppendix                              3-56                               Rev 2. July2 .33,2015 PUR-1 St
1ELEMENTS
 
-ASSEMBLED FOR THlE Effective Date: 01/24/07 Page: 53of5PURDUE UNIVERSITY REACTORthose indications with maj or dimensions greater than 1/64inch are considered relevant for item (iii).)1. Any cracks.ii. Any linear indications.
Form 412.09 (Rev. 09)
iii. Rounded indications with dimensions exceeding 10percent of the nominal weld thickness or 1/8 inch,whichever is smaller.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY                       Identifier:     SPC-382 STANDARD AND CONTROL FUEL                         Revision:       1 ELEMENTS -. ASSEMBLED FOR THE                       Effective Date: 01/24/07         Page: 52 of 57 PURDUE UNIVERSITY REACTOR
Rounded indications separated by 1/16 or less edge-to-edge shall beevaluated as a single indication.
: c. One section face     for plug welds, arc spot welds, and welds that are less than   one inch long on non-cylindrical components.
: d. The cross section shall be polished and etched to provide clear definition of the structure in the fusion zone and the heat-affected zones.
: e. For welds in (a) and (b) of this paragraph, one cross section shall be made through a weld start and a weld stop area and the remaining sections shall be made at random. For weld described in (c) of this paragraph, the cross section shall be made at the approximate centerline of the weld.
Examination of the welds shall be in accordance with Section 3.6.2.3.
3.6.2   Acceptance Criteria for Qualification Test Welds
: 1. Visual Examination. Visual examination shall be in accordance with Section 5.1.
: 2. Liquid Penetrant Examination. Unless otherwise specified, final weld surfaces shall be examined using a color contrast method.
: a. For welded joints in materials less than 1/8 inch thick the following relevant indications are unacceptable.
: 1. Any cracks.
ii. Linear indications.
iii. Indications with dimensions exceeding 1/64 inch.
iv. Rounded indication separated by 1/44 inch or less edge-to-edge.
: v. Five or more rounded indications in any six square inches of weld surface with the maj or dimension of this area not to exceed six inches with the area being taken in the most unfavorable location relative to the indication being evaluated.
: b. For all welds in materials 1/8 inch thick or greater, the following relevant indications are unacceptable. (Only Appendix B PUR-1 SAR                                        Appendix 3-57                             Rev 2. July 23, 2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382of5 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THlE                         Effective Date: 01/24/07       Page: 53of5 PURDUE UNIVERSITY REACTOR those indications with maj or dimensions greater than 1/64 inch are considered relevant for item (iii).)
: 1. Any cracks.
ii. Any linear indications.
iii. Rounded indications with dimensions exceeding 10 percent of the nominal weld thickness or 1/8 inch, whichever is smaller. Rounded indications separated by 1/16 or less edge-to-edge shall be evaluated as a single indication.
iv. Four or more rounded indications in a line separated by 1/16 inch or less edge-to-edge.
iv. Four or more rounded indications in a line separated by 1/16 inch or less edge-to-edge.
: v. Six or more indications in any six square inches ofweld surface with the major dimension of this areanot to exceed six inches with the area taken in themost unfavorable location relative to the indications being evaluated.
: v. Six or more indications in any six square inches of weld surface with the major dimension of this area not to exceed six inches with the area taken in the most unfavorable location relative to the indications being evaluated.
vi. Aligned indications in which the average of thecenter-to-center distance between any oneindication and the two adjacent indications in astraight line is less than 3/16 inch.3. Metallo graphic Examination Metallographic examinations shall beperformed on qualification test welds at not less than 50X on testwelds as required in this Section in accordance with ASTM E.2.Any cross section which is shown by metallographic examination to contain any of the following relevant defects shall be cause forrejection of the test welds.a. Any cracks.b. Incomplete fusion, or insufficient joint or root penetration.
vi. Aligned indications in which the average of the center-to-center distance between any one indication and the two adjacent indications in a straight line is less than 3/16 inch.
: c. Any tungsten inclusions, slag inclusions, or porosity havinga maximum dimension greater than 20 percent of the weldthickness or 1/32 inch, whichever is smaller.d. More than four tungsten inclusions or pores which have a~maximum dimension less than in (c) above.Appendix BAppendix 3-58 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: 3. Metallo graphic Examination Metallographic examinations shall be performed on qualification test welds at not less than 50X on test welds as required in this Section in accordance with ASTM E.2.
SPC-382STANDARD AND CONTROL FUEL Revision:
Any cross section which is shown by metallographic examination to contain any of the following relevant defects shall be cause for rejection of the test welds.
1ELEMENTS
: a. Any cracks.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 54 of 57PURDUE UNIVERSITY REACTORe. Any deviation from specified weld geometry or weldreinforcement.
: b. Incomplete fusion, or insufficient joint or root penetration.
3.6.3 Test Welds.1. Procedure and / or welder performance qualification shall be madeon test welds which duplicate the production weld joint type andwhich simulate the conditions to be used in production with respectto orientation, the essential variables listed in Section 3.2.3.2, andthe dimensions of the parts to be joined to the extent that theyaffect heat requirements, relative  
: c. Any tungsten inclusions, slag inclusions, or porosity having a maximum dimension greater than 20 percent of the weld thickness or 1/32 inch, whichever is smaller.
: motions, and distortions.
: d. More than four tungsten inclusions or pores which have a~
Allwelding used in qualifying a welding procedure and / or welderperformance shall be performed in accordance with the procedure specification.
maximum dimension less than in (c) above.
: 2. For manual welding, two consecutive test welds shall be madewhen the weld joint is less than six inches in length. Only one testweld shall be required when the weld joint is 6 inches or greater inlength.3. All test welds shall be tested using the required tests listed inSection 3.6.1. To qualify the procedure specification used inmaking the test welds, each Weld shall pass the required tests.4. Repair of procedure or performance qualification test weld(s) isprohibited.
Appendix B Appendix 3-58                           Rev 2. July 23, 2015 PUR-1 SAR
: 4. Production WeldingAll production welding shall be accomplished using approved welding procedure specifications and qualified welders and/or welding operators.
 
: 5. Quality Acceptance of Production Welds5.1 All completed production welds shall be visually examined in accordance withthe following requirements:
Form 412.09 (Rev. 09)
5.1.1 General Visual Inspection Requirements.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                             SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                         Effective Date: 01/24/07           Page: 54 of 57 PURDUE UNIVERSITY REACTOR
All visual examinations shallcomply with the following:
: e. Any deviation from specified weld geometry or weld reinforcement.
: 1. Visual examination shall be made under direct daylight-type fluorescent lighting of at least 100 foot-candles at the workexamination area.Appendix BPUR-1 SAR Appendix 3-59 Rev 2. July 23, 2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
3.6.3     Test Welds.
SPC-382STANDARD AND CONTROL FUEL Revision:
: 1. Procedure and / or welder performance qualification shall be made on test welds which duplicate the production weld joint type and which simulate the conditions to be used in production with respect to orientation, the essential variables listed in Section 3.2.3.2, and the dimensions of the parts to be joined to the extent that they affect heat requirements, relative motions, and distortions. All welding used in qualifying a welding procedure and / or welder performance shall be performed in accordance with the procedure specification.
1ELEMENTS
: 2. For manual welding, two consecutive test welds shall be made when the weld joint is less than six inches in length. Only one test weld shall be required when the weld joint is 6 inches or greater in length.
-ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 55 of 57PURDUE UNIVERSITY REACTOR2. Visual examination shall be performed with the aid of a 5x(minimum) magnifying glass.3. The inspection required by this standard shall not be performed bythe welder who made the welds. However, if the welder isqualified in accordance with this standard, he may visually inspecthis own welds prior to the inspections required by this standard.
: 3. All test welds shall be tested using the required tests listed in Section 3.6.1. To qualify the procedure specification used in making the test welds, each Weld shall pass the required tests.
: 4. Personnel performing visual inspection shall have 20-20 vision,natural or corrected, stereo acuity, and shall not be color-blind.
: 4. Repair of procedure or performance qualification test weld(s) is prohibited.
5.1.2 Visual Acceptance Criteria (except for porosity).
: 4.     Production Welding All production welding shall be accomplished using approved welding procedure specifications and qualified welders and/or welding operators.
Visual examination ofweld joint preparations and welds shall be performed in accordance withthe following requirements to verify conformance to the written weldingprocedure, the design requirements, and the requirements of thisstandard:
: 5.     Quality Acceptance of Production Welds 5.1     All completed production welds shall be visually examined in accordance with the following requirements:
: 1. Prior to welding, the weld joint edges and adjacent surfaces shallbe examined for:a. Proper edge preparation, dimensions, and finish.b. Alignment and fitup of the pieces being welded.c. Verification of correct material by check of records.d. Verification of the cleanliness requirements.
5.1.1   General Visual Inspection Requirements. All visual examinations shall comply with the following:
: 2. After welding, the joint shall be examined in the final surfacecondition for:a. Contour, reinforcement and surface finish of welds.b. Degree of underfill,  
: 1. Visual examination shall be made under direct daylight-type fluorescent lighting of at least 100 foot-candles at the work examination area.
: undercut, and overlap.c. Arc strikes, weld spatter and impression marking.d. Burn-through and fuse-through
Appendix B PUR-1 SAR                                         Appendix 3-59                             Rev 2. July 23, 2015
: 3. Weld joints and surfaces which are shown by visual examination tohave any of the following defects or areas of nonconformance areunacceptable:
 
: a. Any nonconformance revealed by 5.1.2.1.Appendix BAppendix 3-60 Rev 2. July 23, 2015PUR-1 SAR Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
Form 412.09 (Rev. 09)
SPC-382STAN7DARD AND CONTROL FUEL Revision:
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                           Revision:       1 ELEMENTS - ASSEMBLED FOR THE                         Effective Date: 01/24/07         Page: 55 of 57 PURDUE UNIVERSITY REACTOR
1ELEMENTS
: 2. Visual examination shall be performed with the aid of a 5x (minimum) magnifying glass.
-ASSEMBLED FOR THlE Effective Date: 01/24/07 Page: 56 of 57PURDUE UNTIVERSITY REACTORb. Any zone of incomplete fusion.c. Insufficient joint or root penetration.
: 3. The inspection required by this standard shall not be performed by the welder who made the welds. However, if the welder is qualified in accordance with this standard, he may visually inspect his own welds prior to the inspections required by this standard.
: d. Any undercutting, underfill, or burn through.e. Any concavity on the face side of groove welds.f. Any arc strikes, weld spatter, and impression marking.g. Any visible inclusions,  
: 4. Personnel performing visual inspection shall have 20-20 vision, natural or corrected, stereo acuity, and shall not be color-blind.
: porosity, cracks, and unfilledcraters.4. Machined welds shall meet the drawing requirements.
5.1.2   Visual Acceptance Criteria (except for porosity). Visual examination of weld joint preparations and welds shall be performed in accordance with the following requirements to verify conformance to the written welding procedure, the design requirements, and the requirements of this standard:
: 5. All welds shall be free from surface markings resulting frommishandling,  
: 1. Prior to welding, the weld joint edges and adjacent surfaces shall be examined for:
: punching, scratching, etc., which exceed the specified surface requirements.
: a. Proper edge preparation, dimensions, and finish.
: 6. All welds shall be fiee of dross, or slag.7. All welds shall be free of oxidation due to improper shfielding andoverheating which produce black or gray spalling or looseparticles.
: b. Alignment and fitup of the pieces being welded.
Iridescent temper films and the dark metallic vapordeposits which may occur adjacent to the welds are acceptable.
: c. Verification of correct material by check of records.
These films and deposits shall be removed by approved cleaningprocedures when accessible.
: d. Verification of the cleanliness requirements.
5.1.3 Visible unacceptable porosity is as follows:1. Four or more pores with a major dimension of 0.048 inches ormore randomly positioned.
: 2. After welding, the joint shall be examined in the final surface condition for:
: 2. A single pore with a major dimension of 0.064 inches or more.3. Six or more pores with a major dimension of 0.016 inches orgreater in one weld.4. Four or more porosity with a major dimension of 0.016 inches orgreater, in line separated by less than 0.063 inches from edge toedge.5.2 Repair of a defective weld by welding shall be limited to two attempts.
: a. Contour, reinforcement and surface finish of welds.
Unacceptable defects shall be removed and re-examination made using liquidpenetrant color contrast method to assure complete removal of the defect. If theAppendix BANAppendix 3-61 Rev 2. July2PUR-1 Sa3,2015 Form 412.09 (Rev. 09)Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:
: b. Degree of underfill, undercut, and overlap.
SPC-382STANDARD AND CONTROL FUEL Revision:
: c. Arc strikes, weld spatter and impression marking.
1ELEMENTS
: d. Burn-through and fuse-through
-. ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 57 of 57PURDUE UNIVERSITY REACTORremoval of the defects results in reducing the thickness of the weld metal belowthe thickness of the base metal, the area shall be rewelded using a welding repairprocedure which has been approved by the Purchaser.
: 3. Weld joints and surfaces which are shown by visual examination to have any of the following defects or areas of nonconformance are unacceptable:
Whenever a defect isremoved and subsequent repair by welding is not required, the excavated areashall be blended into the surrounding surface to remove any sharp notches,crevices or corners.
: a. Any nonconformance revealed by 5.1.2.1.
Completed repairs shall be visually re-examined per Section5.1. Records shall be maintained on all repairs and shall include the following:
Appendix B PUR-1 SAR                                        Appendix 3-60                             Rev 2. July 23, 2015
5.2.1 Location ofj oint.5.2.2 Location of defect.5.2.3 Description of defect, including type and size.5.2.4 Reference to approved repair procedure.
 
5.2.5 Inspections before and after repair and the results thereof.5.2.6 Identification of repair welders or welding operators.
Form 412.09 (Rev. 09)
Appendix BPUR-1 SARRevA2.pJuyi23,3201 PUR-1 SARRev2. July 23, 2015 1RA.J4I 2 I 1SNOTES:1. PROCURE.
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STAN7DARD AND CONTROL FUEL                       Revision:       1 ELEMENTS - ASSEMBLED FOR THlE                       Effective Date: 01/24/07         Page: 56 of 57 PURDUE UNTIVERSITY REACTOR
FABRICATE, AND INSPECT PER SPECIFICATION SPC-382.L2MARK ASSEMBLY ISENTFItC.BT82 PER SPECIFICATION SPO-SA2.3. REMOVE AUL BURRS HAS SHARP ESGES.2 1 SHEET REV STATUS PTA 0 PHYSIS2 E LESHEETS REVISED DESCRIPTION OF ITEM 3ASSES SHEET 2;I SEEOSAR-RADE ESS2 ,&8NY1C M ~t I1/2SA/ST2 ASSES ITEM S. CHANGES MATEREAL ITEM?CHANGES ITEMS. SEE SAA-RTA7VT A/ASSDC4 CU PAILLPS, 100" 3I6 SST OR 304SST 91 635457.5 SOURCE DRIVE TOP B .A S CU PHILUPS, T00O 315 SST 7B-SB SAC-2A S I/S LU1 635482-3 SOURCE DRIVE CONTAINERA 1 5 35465-1 GRAPHITE BLOCK1 R 35462-1 GRAPHITE CONTAINER3 ASSEMBLYSC .5 SOURCE ERRSE SUPPORTASSEMBLY2 sc 1 GRAPHITE REFLECTOR ASSEMBLY1 Br-1 SECTIONED ISOMETRIC REFERENCE ONLYSCALE: NONE-2 FINAL-t FINALsncsoa= REOURNTR:
: b. Any zone of incomplete fusion.
T, VINNOU.NHARRIK 3SIG S. MORRELL PURSUE UNIVERSITYN OUDRAM TEST RESEARCH AND TRAINING REACTORTA/SM-T S.,t PROJECT SEO. IGRAPHITE REFLECTOR ASSEMBLY ANDSPA.'USS SOURCE DRIVE ASSEMBL.Y PROR I PHIRSCAAPPARH ARTUI/ES 5 A FFECTAR IVTE: A/1iO NOTES ISHEET 1 OF 2I 21 SORE0VAPURS- 1 OAR Arniendix 3-63 Rev' 2, Iulv 23, 2015[ APPLE~ATUN U/bb4 7517 ''2"1Y I ' I V I "." W
: c. Insufficient joint or root penetration.
* I V I I IIDIB (2953)AX 7I2.95(3 AXC-2 ASSEMBLYSCALE: 111BVA-2 SECTIONED ISOMETRIC SCALE: NONEPUR-1 SAR Appendls*
: d. Any undercutting, underfill, or burn through.
3-64 Rev 2, July 23, 2013D OIMF3 DWG-635454 20 I i., I I CA E AII A I/I&D4:j1 8765~J74I I T INOTES:1. PROCURE.
: e. Any concavity on the face side of groove welds.
: f. Any arc strikes, weld spatter, and impression marking.
: g. Any visible inclusions, porosity, cracks, and unfilled craters.
: 4. Machined welds shall meet the drawing requirements.
: 5. All welds shall be free from surface markings resulting from mishandling, punching, scratching, etc., which exceed the specified surface requirements.
: 6. All welds shall be fiee of dross, or slag.
: 7. All welds shall be free of oxidation due to improper shfielding and overheating which produce black or gray spalling or loose particles. Iridescent temper films and the dark metallic vapor deposits which may occur adjacent to the welds are acceptable.
These films and deposits shall be removed by approved cleaning procedures when accessible.
5.1.3   Visible unacceptable porosity is as follows:
: 1. Four or more pores with a major dimension of 0.048 inches or more randomly positioned.
: 2. A single pore with a major dimension of 0.064 inches or more.
: 3. Six or more pores with a major dimension of 0.016 inches or greater in one weld.
: 4. Four or more porosity with a major dimension of 0.016 inches or greater, in line separated by less than 0.063 inches from edge to edge.
5.2   Repair of a defective weld by welding shall be limited to two attempts.
Unacceptable defects shall be removed and re-examination made using liquid penetrant color contrast method to assure complete removal of the defect. If the Appendix B PUR-1 Sa        ANAppendix                              3-61                             Rev 2. July2 3,2015
 
Form 412.09 (Rev. 09)
Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier:                           SPC-382 STANDARD AND CONTROL FUEL                         Revision:       1 ELEMENTS -. ASSEMBLED FOR THE                       Effective Date: 01/24/07         Page: 57 of 57 PURDUE UNIVERSITY REACTOR removal of the defects results in reducing the thickness of the weld metal below the thickness of the base metal, the area shall be rewelded using a welding repair procedure which has been approved by the Purchaser. Whenever a defect is removed and subsequent repair by welding is not required, the excavated area shall be blended into the surrounding surface to remove any sharp notches, crevices or corners. Completed repairs shall be visually re-examined per Section 5.1. Records shall be maintained on all repairs and shall include the following:
5.2.1     Location ofj oint.
5.2.2     Location of defect.
5.2.3     Description of defect, including type and size.
5.2.4     Reference to approved repair procedure.
5.2.5     Inspections before and after repair and the results thereof.
5.2.6     Identification of repair welders or welding operators.
Appendix B PUR-1 SAR      PUR-1          SARRevA2.pJuyi23,3201 Rev2. July 23, 2015
 
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: 1. PROCURE.        ANDINSPECT FABRICATE,          PERSPECIFICATION SNOTES:
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: 3. REMOVEAUL BURRSHASSHARPESGES.
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                                                                                                                -2  FINAL                ae* *N: N OUDRAM                   TESTRESEARCH    ANDTRAINING REACTOR TA/SM-TS.,t     PROJECTSEO.IGRAPHITE                       REFLECTOR ASSEMBLY AND
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* PURS-1OAR Arniendix 3-63 Rev' 2, Iulv 23, 2015
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NOTES:
: 1. PROCURE. FABRICATE.ANDINSPECT  PERSPECIFICATION SPC-3R2.
LIADDED          A -3ASSY;        TITLES L1UICHNG
/&#x17d;MARKE ASSEMBLY    IDENT1FICATIONPERSPECIFICATIONSPC-TBZ                                                                                                                                1CHANGED NOTE TO 3 SHOW        REVISED NEWFUEL  PLATE  DESIGN;    140
  /.OUANTn~f OF ITEM 5 (FUELPlATES)ANADITEMN(DUMMY FUELPLATES) USEDIN-UASSEMULY                                                                                                            SEDADD    UGUUUED ITEM B. CHARGED  MATERIAL  ITEMA,          HHD (PARTIAL FUEL ASSEMBLY)
A\CHANNE L SPACING TO REDETERMINED BYTHEUSER.
I;SO'TRO*" BYSIDEPLATEGROOVE      LOCATIONS ANDWIDTHS. AND ITEM..  ,NOTEA,,SEEO  ..
A....          I    ....
FUELPLATE  THICKNESS.DIRECT MEASUREMENT IS NOTREQUIRED.
S. REMOVE AU.BURRS  ANDSHARPEDGES.                                                                        ___________-(-I                                                      %
D K
It            VA C
                                                                                                        ~-1                              A*
                                                                                                                                      -2 A*
45              B-3MA                                                      MACHINE  SCREW,  FLATHD.
PHIWPS,1W0'3B                          TO    ST 8-3UUNC-UA X lI2LG --          3!6 SST OR*SST B
MAHN
                                                                                                                                                                                                *EFLAT HD, A    4  4  EG              PHIWPU.I1DO"                    31 SSTOR DR4  UST              H 14 AH              A 6.35A3-3  DUMMY  FUELPLATE                                              B AR 14          A35463-1  FUELPLATEASSEMBLY                                              5 1    1  1        635454-1  STANDARD  FUELCONTAINER4 SC        -D    DUMMY  FUELELEMENT3 SC        -2    PARTIAL  FUEL ELEMENT SC      -I    STIANDARD  FUELELEMEN'T
                                                                                                                                                                  -ASSEMMESBATRIOLY                    T                                              S1IAEATTCETK CAT  EUNTEY*NSA            DRUESCBPT0H                    0RHEI*RRA            AG
    -1 SECTIONED SCALE:NONE ISOMETRIC          REFERENCE ONLY                                                                                                VWIRFSRRT    RESSEUSTER:
T. VINNOLA am~o*        L*DeIG2DMOREL                          PURDUEUNIVERSITY TESTRESEARCH    ANDTRAINING  REACTOR
                                                                                                                                            .. IFNA                                                              STANDARD    FUEL.PARTIAL U DUMMY  ELEMENT  ASSEMBUES FUR-I SAR    AppendixE 3-65 Rev 2, July 23, 2015                                                                    in~i                          DwMFG.'*635455  IP*V R                    I7                                    I                    I                                                    PLIAWT  I            ,TSORP            -                                            EE. O I                          U T                                                          2                                            1      SD*2
 
8                                  7                  6                              5                                4        3                            I 1
                                                                                                                                                                                                    .........
NOTES:                                                                                                                                                                    RAY                I*sMCHIO                      EFRFIN DATA.
: 1. PROCURE,FABRICATE, ANDINSPECT              SPC-.382.
PERSPECIFICATION 2                                                                                                                                                                            CHANGED  TO SHOWNEWFUELPLATEDESION:
LXA      ASEMLY  DNIFCTO PE DRSECFID;CAINSC-B          ..... T...                                                                                                          I  ADDED -2 ASSEMBLY.
SEESAR-N3094D0 SECTION  A-A.B ITEM6;          1524/07 CHANGED  MEATERIAL ITEM?7CHANGED    MOTE 3.
FUELPLATETHICKNESS.
DIRECTMEASUREMENTIS NOTREOUIRED.
: 4. REMOVEALLBURRSANDSHARPEDGED.
IC A
                                                                                                                          -1 ASSEMBLY                                                                                                      B
                                                                                                                          -2 ASSEMBLY MACAWNE  SCREW.FLATAS.                  O~
S  B  CG                PHILWPS,SB0                  316SETON34SST                  7 S-3D UNO-DA A5/11LU A
                                                                                        --SECHANNELSUPACNG .156 8
1  1 535AA3.3  DUMMY S3SH6A=11I CONTROL FUELPLATE TOP 6
5 B        635463-I  FUELPLATE  ASSEMBLY                                          A 1 I            34B      CONTROL  FUELCONTAINER ASSEMBSLY SC        *D      DUMMY  CONTROL  FUELELEMENT ASSEMBLY2 SC        *t    CONTROL  FUELELEMENT S-T    ASSEMBLY1 CAT. BERTPYPTIOG          0S TESPTE0M CA                            OSEBANBAB            AU
  -1 SECTIONED SCALE:
NONE ISOMETRIC      BEFERENCEONLY A
mua= e..7    RAOLESISR:
T. VINMOLA SECTION SCALE.1/1 A-A                                                                                                                    PURDUEUNIVERSrITY
                                                                                                                                      -2 FINAL                                                TESTRESEACRH    ANDTRAINING REACTOR CONTROL  FUELELEMENT    ASSEMBLY AND
                                                                                                                                      -1 FINAL                                              DUMMY CONATROL    FUELELEMENT  ASSEMBLY PUR-1 SAR    Appendix 3-66  Rev 2, July 23, 2015 DI01MF3                    DwO-635456        2~
C                I                7                I                  I                                                          A, L I                                                                                                                                Z U
T T        *.+      O                                                                            1      *a*
 
R                                  7                                                              5                                    4          3                                    2                                        1 NOTES:
: 1. PROCURE, FABRICATE,ANDINSPECT PER SPECIFICATION                                                                                                                                                    REVISE  TO SHOWNEWFUELPLATEDESGN; SPC-382.
1 REMOVED    iTEMS2,4A&7REVIESEDTITLE; L~MARK  ASSEMBLY IDENTIFICATION PERSPECIFICATION SPC-382,                                                                                                                                                  2 SEE DA-514751 BEEDAR-SURAUR HEIVISiNS              1/2407
                                                                                                                                                                                                                                                            /40 3CHANNELSPACING IS CNROLDBY SIDEPLATEGROOVELOCATIONS ANDWIDTHS,AND                                                                                                                              REVISED  NOTESB&  MATERIAL ONITEM B 4
FUELPLATETHICTINESS.
DIRECTMEASUREMENTIS NOTREQUIRED.
4a REMOVE ALLBURRS  ANDSHARPEDGES.
0 A
                                                                                                                                        -1 ASSEMBLY SCALE:11' B
MACHINE  SCREW. FLATRD.
CDPHILLIPS.              ITS'                  316SSTOR[504SST              B B-32UNC.DA  X 5/16LG B*
35468-?    FISSIONCHAMBER    TOP                                        A 635463-1    PUEL PLATE  ASSEMBLY                                        S 515458-1    STANDARD  FUELCONTAINER ASSEMRBLV (DXCHANNEL A
SPACING
                                                                                            .120)                        -ISNNEL SPACING  .130(
                                                                                                                                                                                              -U      REMOVED                                                      S DC          -1      EEMNTFISSION CRAMBER ASML FUEL
      -1 SECTIONED ISOMETRIC                                                                          SECTION A-A SCALE:HONE                                                                                SCALE.1/
REFERENCEONLY                                                                                                                                                                                                LIST PUTSUSI P*T*
A RAT D*IS
* RHAURSTER:
T.VINNOLA ottaRR          AESRGNa MORRELL                        PURDUE UNISERSITY
                                                                                                                                                                                        ,  ,=,WN N.OLOHAM                  TEATRESEARCH ANDTRAINIMO  REACTON FISSIONCRAMBERFUELELEMENT  ASSEMBLY i  FINALTR StUR- l SAR  AppendixE 367  Rev 2, July 23. 2015 I.!I.                                                                                                                                                        I            1
                                                                                                                                                                                                                                                  *&deg;*635457 I'*
APLICATMB              -                                                      1I          I. ElF  1.
8                                  77                            6b                                                    AlA          4 4
SORRY I.
1        ..
SD*o*
 
NOTES:
: 1. PROCURE,FABRICATE.
ANTINSPECT  PERSPECIFICATION SPC-352.
2r REMOVED
: 3. REMOVED
: 4. REMOVE ALLRIURRS ANDSHARP  EDGES.
: 5. WELDPERSPECIRCEATION SPC-352APPENODD B.USINGITEM 7 (WELD FILLERMETAL).
S. AUL CORNER ANDFILLETRADII
                            ,U30UNLESS OTHERWISE  NOTED.
SCRUTICAL INTERFACEDIMENSIONSSHALL BEADHERED  TO.
ANVERIFY RECTANGULAR GAUGE.DFEPROVIDED CAVITYANDSLOTSIZEWITH GO-NO-GO GAUGE SHALL GO-NO-GO SLIDE FREELY THROUGHOUT ENTIREDESIGNATED CAVITY(OR SLOT)LENGTH  FOR ALLULOTSW*IrHUIUT HANG-UP,STICEING.
OR DISENGAGEMENT  FROM SLOT.
                                                                  -1 ASSEMBLY                                                -1 ISOMETRIC VIEW REFERENCE ONLY SCALE:
1/1                                                    SCALE:
NONE VIEW B DEALE:4:1                      VIEW C    AU SCALE.
4/1 VIEW A SCALE: 2/1 PUR-I1SAR    Appendix 3-68    Rev 2, July 23, 2015
 
NOTES:
: 1. PROCURE.FABRICATE.
ANDINSPECT PERSPECIFICATIONSPC-382.
: 2. REMOVED
: 3. REMOVED B. REMOVE ALLBURRSANDSHARPEDGES.
U. WlELD PERSPECIFICATION SPC.382APPENDIX B. USING ITEM7 (WELD FILLERMETAL).
THROUGHOUT ENTIREDESIGNATEDCAVITY(ORSLOT)LENGTH  FOR ALLSLOTSWITHOUTHANG-UP, STICKING,ONDISENGAGEMENT  FROM SLOT,
                                                                -1 ASSEMBLY SCALE:1/1
                                                                                                                        -1 ISOMETRIC SCALA:
NONE VIEW REFERENCE ONLY jz~~
VIEW SCALE:
B 4/1 VIEW C 4x
                                                                                                              ,SCALE:
4/l VIEW    A SCALE:E1 PUR-1 SAR    Appendix 3-69    Rev 2, July 23,2015
 
NOTES:
: 1. PROCURE.FABRICATE.
ANDINSPECT PERSPECIFICATION  SPO-,3A2.
: 2. REMOVED
: 3. REMOVE ALLBURRSAWD SRARPEDGES.
A. WELDpERSPECIFICATIONSEC-UB2 APPENODIXB, USINGITEM 7 (WELDFILLERMETAL). _
: 5. REMOVED.
GAUGE.OFFPROVIDED GO-MO-GOGAUGE SHALL        FREELY S LIIDE TH*ROUGAGUTENTIREDESIGNATESCAVITY(ORSLOT)tLENGTH  FON ALLSLOTSPATAGUTHANG-UP.STICKING.
ORDISENGAGEMENT FROMSLOT.
                                                                                          ,167/
                                                            -1 ASSEMBLY SEALE III
                                                                                                -1 ISOMETRIC SCALE:
NONE VIEW REFERENCE ONLY i"
(,060)*'1-3 WIEWA UCALE:Dli                  VIEW SCALE:
C A/l AU
 
7                                        S                47  4 R                                                                                                                          3                                      2                    I                    1 NOTES:                                                                                                                                                                  REVl04100                                      I  EFECTNEATE SEEDAR-514751      REVINIONS              440
: 1. PROCURE.TABRRCATE, ANDINSPECTPERSPECIFICATION SPC-382.                                                                                                                      REVISED THEDESCRIPTION  SFRTEM  3                /47 1SEE DAR-5UH425                                    /40 Z/2*\MARK ASSEMRLY IDENTFIfCATION PERSPECIFICATION SPO-3E2.
2CHANGED  MATERIAL ITEM7                        4AU
: 3. REMOVE ALLBURRSANDSHARPEDGES.
D
                                                                          .4                    1      F
                                                                                            *mL
                                                                                                                  -1 ASSEMBLY SCALE:1,1 B
MACHINE SCREW,FLAT HD, A CAPHILUIPS,              TOO                    316 SSTOR3U4 SOT              7 R*.32, UNC-2A 0172LU                      __
1            835461.2    CAPSULE INSERT ASSEMBLY 1          635451.1    CAPSULE HOLDERHASSEMBLVY 1          63S462-I    GRAPHITE CONTAINER3 ASSEMBLY DC          -1        IRRADIATION FACILITY ASSEMELY                                  I
                                                                                                                                                  -1 SAFETI    PARTOB              IIOAIELtISERE                UHIE RIE,/PECFECATEH    ITEI 510011                  (1SFTI                                                                                                        CA*
T. EIEqNTEMTI                ECAET.,'P'                URAE,.SRMA          o..
A
        -1 SECTIONED ISOMETRIC                REFERENCEONLY SCALE:NONE                                                                                                                      05TN400          BEASlN U.MORRELL                          PURDUEUNt~fERSITY ETORiroOR TNAN OLOHAM                      TESTRESEARCH    ANDTRAINING  REACTOR L*    FINAL    TOOTNTA U,      0      so 004C                          IRRADIATION FACILITYASSEMBLY
                                                                                                                                *F  NEXT AS*              .. ......          .....          1M                        owG.635460      2"*
PI16.1 CAD    Ann,.HSiY 3-71  A.RT I/O/Rh  101IS                                                NEBOTI    505051            1F
~TI                                                                                                                            F  STBACUB/OE                                  2                                        1      S2EU32 66                                                    4 8                                  77                                                          'P  4                                                            2,                                        1      SD8032
 
I
                                              -7 P
12 4,
4                                    3                                                2                      I                    1 I.I.,ll                I REV                                          REASONS STATES NOTES:                                                                                                                                                                                    ITITI1IREV            IDESl.ETSj REVISEDTOLERANCES              ONlITEM
: 1. REMOVEALLBURRSANDSHARPEDGSES.
: 2. pROCURE.
FABRICATE.
FABRICATE.
AND INSPECT PER SPECIFICATION SPC-3R2./MARKE ASSEMBLY IDENT1FICATION PER SPECIFICATION SPC-TBZ/.OUANTn~f OF ITEM 5 (FUEL PlATES) ANAD ITEM N (DUMMY FUE L PLATES) USED IN -U ASSE MULY(PARTIAL FUEL ASSEMBLY)
ANDINSPECT  PERSPECIFICATION SPC-382.
TO RE DETERMINED BY THE USER.A\CHANNE L SPACING BY SIDE PLATE GROOVE LOCATIONS AND WIDTHS. ANDFUEL PLATE THICKNESS.
I    I ..............
DIRECT MEASUREMENT IS NOT REQUIRED.
1%o?
S. REMOVE AU. BURRS AND SHARP EDGES.i T
I
* c I{ LIADDED NOTE 3 A -3 ASSY; REVISED TITLES1CHANGED TO SHOW NEW FUEL PLATE DESIGN; 140SEDADD UGUUUED ITEM B. CHARGED MATERIAL ITEM A, HHDL1UICHNGE ITEM.. ,NOTEA,,SEEO
: 3. WELDPERSPECIFICATION SP0-322APPENDIXR.USING ITEM17{WE  LDFILLERMETAL).
..A.... I ....___________
4.ALLCORNERANDFILLET RAD*II.O3OUNLESS OTIIERISSENOTED.
-(-ID%KItVAC~-1 -2 45 B-3MAMACHINE SCREW, FLAT HD.PHIWPS, 1W0'3B TO ST8-3UUNC-UA X lI2LG --3! 6 SST BMAHN HD,A 4 4 EG PHIWPU.I1DO" 31 SST OR DR4 UST H14 AH A 6.35A3-3 DUMMY FUEL PLATE BAR 14 A 35463-1 FUELPLATEASSEMBLY 51 1 1 635454-1 STANDARD FUEL CONTAINER4 SC -D DUMMY FUEL ELEMENT3SC -2 PARTIAL FUEL ELEMENTSC -I STIANDARD FUEL ELEMEN'T-ASSEMMESBAT RIOLY T 1IAEATTCETK SCAT DRUESCBPT0H AG-1 SECTIONED ISOMETRIC REFERENCE ONLYSCALE: NONE..IFNAVWIRFSRRT RESSEUSTER:
D I-
T. VINNOLAam~o PURDUE UNIVERSITY TEST RESEARCH AND TRAINING REACTORSTANDARD FUEL. PARTIALU DUMMY ELEMENT ASSEMBUES FUR-I SAR AppendixE 3-65 Rev 2, July 23, 2015in~i R I7 I I PLIAWT I ,TSORP -EE. OIUT21 8765431I .........
                                                                                                                                              ...........................                                               J    -O              SEEDETAIL
NOTES:1. PROCURE, FABRICATE, AND INSPECT PER SPECIFICATION SPC-.382.
_(2.755) 3 SEE  ASS C
L2XA ASEMLY DNIFCTO PE DRSECFID;CAINSC-B
                                                                                                                              -1 ASSEMBLY SCALE Ill AR AR AR AR SC                            ELILRMTL                          ER4043            AWDA5AD 17 AR          SC                                                        BAR.01/)2          ASTMB211    IN ALSON61.TNST AR          SC                                                        BA*R.
.....T ...FUEL PLATE THICKNESS.
0114          ASTMB2TT IS AL6021-T05 1 AR                SC                                                        002101t18          ASTMB211    14 TB51 ALBAAI.
DIRECT MEASUREMENT IS NOT REOUIRED.
AR          SC                                                        TUBING,1 TI8ODX D05WALL        12 AL.DEI-TE          ASTM B21D AR              SC iTUBING,1*314005X.,25                                                      WALL      Il ALBAA61.TB        ASTM8212 1  C10          PLGpLATE,                                1127115      ASTMBUS    ID AL 661 T-5 I        SC        -B         CAPSULE      UPPERTUBE              BAR,01 31          ASTM8211    9 t      S          -8        CAPSUIEHOLDER          TOP          PLATE.I THE        ASTI,BUSS 8 45 .D535A5\
: 4. REMOVE ALL BURRS AND SHARP EDGED.RAY EFRFIN DATA.CHANGED TO SHOW NEW FUEL PLATE DESION:I ADDED -2 ASSEMBLY.
                                                                                        *    "4-1            7F 5THR..                                                                             tSC          -7        CAPSULE      HOLDE*R  BOTTOM        PLATE.54114TK      P.5748209    7 3XHRU                                                                    1           535405-2      GRAPHT CAPSULE          HOLDER                                    S SC         *4        CAPSULE      HOLDER    TOPPLATE4 1  SC .3          CAPSULE      HOLDER    WELDMENT3 275 5
SECTION A-A. B ITEM 6; 1524/07SEE SAR-N3094D0 CHANGED MEATERIAL ITEM?7 CHANGED MOTE 3.ICA-1 ASSEMBLY-2 ASSEMBLYBA--SE CHANNELSUPACNG
ASSEMBLY SC         -2        CAPSULE      RNSERT  ASSEMBLY
.156MACAWNE SCREW. FLAT AS. O~S B CG PHILWPS, SB0 316 SET ON34SST 7S-3D UNO-DA A 5/11 LU8 5 35AA3.3 DUMMY FUEL PLATE 61 1 S 3SH6A=11I CONTROL TOP 5B 635463- I FUEL PLATE ASSEMBLY A1 I 34B CONTROL FUEL CONTAINER ASSEMBSLY SC *D DUMMY CONTROL FUEL ELEMENTASSEMBLY2 SC CONTROL FUEL ELEMENTS -T ASSEMBLY1 CAT. BERTPYPTIOG CA 0S TESPTE0M OS EBANBAB AU-1 SECTIONED ISOMETRIC BEFERENCEONLY SCALE: NONESECTION A-ASCALE. 1/1PUR-1 SAR Appendix 3-66 Rev 2, July 23, 2015-2 FINAL-1 FINALmua= e..7 RAOLESISR:
                                                                                                                                -LK                                                                                                                                                            2 SC        .1        CAPSULE      HIOLDER  ASSEMBLY P0279                          IBEREIELFATIO            TO WOE/BOOtlN                                                  SSAEIOUHRNB          AT
T. VINMOLAPURDUE UNIVERSrITY TEST RESEACRH AND TRAINING REACTORCONTROL FUEL ELEMENT ASSEMBLY ANDDUMMY CONATROL FUEL ELEMENT ASSEMBLYDI01MF3 DwO-635456 2~AC I 7 I I LT A,IUTOZ1 R754321NOTES:1. PROCURE, FABRICATE, AND INSPECT PER SPECIFICATION SPC-382.L~MARK ASSEMBLY IDENTIFICATION PER SPECIFICATION SPC-382,43CHANNEL SPACING IS CNROLDBY SIDE PLATE GROOVE LOCATIONS AND WIDTHS, ANDFUEL PLATE THICTINESS.
      -1 ISOMETRIC         REFERENEONLY NONE SCALE:
DIRECT MEASUREMENT IS NOT REQUIRED.
oDETAIL SCALE: U11 P4415SIL$
4a REMOVE ALL BURRS AND SHARP EDGES.2 SEE DA-514751 HEIVISiNS
                                                                                                                                                                                              -   B.B,m 5y    BEALBASl*T.RINOLA mIInt*          CF.*N DEBAMORREL                                  PURDUEUSIVERSITY TESTRESEARCH  4245TRAINING REACTOR
/40REVISE TO SHOW NEW FUEL PLATE DESGN;1 REMOVED iTEMS 2,4A &7REVIESEDTITLE; 1/2407BEE DAR-SURAUR REVISED NOTE SB& MATERIAL ON ITEM B0A-1 ASSEMBLYSCALE: 11'BSECTION A-ASCALE. 1/MACHINE SCREW. FLAT RD.CDPHILLIPS.
                                                                                                                                                                          -2  635460                                                                  CAPSULE HOLDER ANDCAPSULE    INSERT
ITS' 316SST OR[504SST BB-32 UNC.DA X 5/16LGB* 35468-? FISSION CHAMBER TOP A635463-1 PUEL PLATE ASSEMBLY S515458-1 STANDARD FUEL CONTAINER ASS EMRBLV-U REMOVED SDC -1 EEMNTFISSION CRAMBER FUEL ASMLA(DX CHANNEL SPACING .120)-ISNNEL SPACING .130(-1 SECTIONED ISOMETRIC SCALE: HONEREFERENCE ONLYPUTSUSIi FINALTRRAT D*IS RHAURSTER:
                                                                                                                                                                          -I  635460            IBRBB          FOR*IB*4,92 O        IDAI                      ASSAMBUES  ANDDETAILA 0 9911 c    550 N*x**SV PUJR- I SAR Appendix 3-72      ReP 2. July 23, 2015                                                                                                                                                             1 I*'*
T. VINNOLAottaRR AESRGN a MORRELL, ,= ,WN N.OLOHAMLISTPURDUE UNISERSITY TEAT RESEARCH AND TRAINIMO REACTONFISSION CRAMBER FUEL ELEMENT ASSEMBLYAStUR- l SAR AppendixE 367 Rev 2, July 23. 2015I.!I. I APLICATMB 1 -AlA8 7 b 41 SORRY I ElF 18764I I .... .1 NOTES:1. PROCURE, FABRICATE.
95115*1     8R                                                          :_=='
ANT INSPECT PER SPECIFICATION SPC-352.2r REMOVED3. REMOVED4. REMOVE ALL RIURRS AND SHARP EDGES.5. WELD PER SPECIRCEATION SPC-352 APPENODD B. USING ITEM 7 (WELDFILLER METAL).S. AUL CORNER AND FILLET RADII ,U30 UNLESS OTHERWISE NOTED.SCRUTICAL INTERFACE DIMENSIONS SHALL BE ADHERED TO.ANVERIFY RECTANGULAR CAVITY AND SLOT SIZE WITH GO-NO-GOGAUGE. DFE PROVIDED GO-NO-GO GAUGE SHALL SLIDE FREELYTHROUGHOUT ENTIRE DESIGNATED CAVITY (OR SLOT) LENGTH FORALL ULOTS HANG-UP, STICEING.
OF 3
OR DISENGAGEMENT FROMSLOT.-1 ASSEMBLYSCALE: 1/1-1 ISOMETRIC VIEW REFERENCE ONLYSCALE: NONEVIEW BDEALE: 4:1VIEW C AUSCALE. 4/1VIEW ASCALE: 2/1PUR-I1 SAR Appendix 3-68 Rev 2, July 23, 2015 NOTES:1. PROCURE.
                            *                  -               ,^  b                              31                                    '8                                                                                                                                  1 8                                    7                                                       0                                                                                                                                                                          1       Su*o*
 
a              7            6                          5                                4          3                          2                       1 D
z5.1*                                                        "4"4 "1
                                                        -3 ASSEMBLY SCALE:   lt
                                                                                                                                                  -02.6
                                                                                                                                                          .0065X45" 8  ESDETA SECTION  A-A                  SECTION  B-B SCALE LI                      SCALEIII B
(255) 20 14 000
                    ~1                                   '4-                               ABC
  -4 ASSEMBLY BVVB~I
[0]
                                                                                                                    -8 ISOMETRIC R*EERECE ONL SCALE:
NONE A
0* DETAIL SCALE:il1 PUR-i SAR AppendLx 3-73  Roy 2, July 23. 201.5                                                  D O1MF3            ow3.635461      1 1      008032
[0 U              /I           b t5                                                          44                                    2                      1       so*
 
Q a
                          "7
                          -7 R                                                J,            ,l A
1 0
                    -u-i C
          '1
                                                                                  -2 ASSEMBLY SCALE:
Oit IR 0110 2.750
                                                                                                    -0
                                                                                                    - -H01(.
f 01.040 B
C) DETAIL C) DETAIL SCALE.211 A
-2 ISOMETRIC  FIEFNENCE OLY PUR-1 SAR AppendLx 3-74  Re'," 2. July 23.2015                                0 IO1MF3' ow-356 SCALENONE B
8                    7/
PUR-i SAR Appendix 3-74  Rev 2. July23. 2015  'P            4 4
:3 3
2 2                  1    SDE*2
 
                                                  .7                        IV                                                4,       A                                                  9                                    1 NOTES:
REMOVEDPRIORREVHISTORY                      IO
: 1. REMOVEALLBURRSANDSHARPEDGES.                                                                                                                                                            4SEE ECR-55V8)R72/0
: 2. PROCURE.
FABRICATE.
FABRICATE.
AND INSPECT PER SPECIFICATION SPC-382.2. REMOVED3. REMOVEDB. REMOVE ALL BURRS AND SHARP EDGES.U. WlELD PER SPECIFICATION SPC.382 APPENDIX B. USING ITEM 7 (WELDFILLER METAL).THROUGHOUT ENTIRE DESIGNATED CAVITY (OR SLOT) LENGTH FORALL SLOTS WITHOUT HANG-UP,
ANDINSPECT  PERSPECIFICATION SP-32.                                                                                                                                       REVIVED DIMENSIONS                            BSl
: STICKING, ON DISENGAGEMENT FROMSLOT,-1 ASSEMBLYSCALE: 1/1-1 ISOMETRIC VIEW REFERENCE ONLYSCALA: NONEjz~~VIEW C 4x,SCALE: 4/lVIEW BSCALE: 4/1VIEW ASCALE: E1PUR-1 SAR Appendix 3-69 Rev 2, July 23,2015 NOTES:1. PROCURE.
: 3. WELDPERSPECIFICATION SPC-SJA2 APPENDSXB. USINGITEMB WEhLD   F'iLLERMETAL).
FABRICATE.
A. ALLCORNERANDFILLET RADII.232 UNLESS OTHERWISE   NOTED.
AND INSPECT PER SPECIFICATION SPO-,3A2.
4CRITICAL INTERFACE DRMENSIONSSHALL READHERED  TO, D
: 2. REMOVED3. REMOVE ALL BURRS AWD SRARP EDGES.A. WELD pER SPECIFICATION SEC-UB2 APPENODIX B, USING ITEM 7(WELD FILLER METAL). _5. REMOVED.GAUGE. OFF PROVIDED GO-MO-GO GAUGE SHALL S LIIDE FREELY ENTIRE DESIGNATES CAVITY (OR SLOT) tLENGTH FONALL SLOTS PATAGUT HANG-UP.
  /~VERIFYRECTAN*G ULARCAVITY ANDSLOTSIZEWITH  GO-NO-GO   DAUGE. DIV PROVIDED GO-NO-GO GAUGESHALLSLIDEFREE  LYTHIROUGHOUT ENTIRE   DESIGNATED CAVITY(OR SLOT)
STICKING.
LENGTHFORALLSLOTSWITHOUTY HANG-UP. STICKING. ORDISENGAGEMENT  FROM SLOT.
OR DISENGAGEMENT FROM SLOT.,167/-1 ASSEMBLYSEALE III-1 ISOMETRIC VIEW REFERENCE ONLYSCALE: NONEi" WIEW AUCALE: DliVIEW C AUSCALE: A/l R7S4743NOTES:1. PROCURE.
                                                                                                                                                                                                                    .---.---.J, m
TABRRCATE, AND INSPECT PER SPECIFICATION SPC-382.
                                                                                                                                                                                                            -1 ISOMETRIC           REFERENCE ONLY SCALE: NONE
ASSEMRLY IDENTFIfCATION PER SPECIFICATION SPO-3E2.3. REMOVE ALL BURRS AND SHARP EDGES.2 I 1SEE DAR-514751 REVINIONS 440REVl04100 I EFECTNEATE REVISED THE DESCRIPTION SF RTEM 3 /471SEE DAR-5UH425
                                                                                    -1,ASSEMBLY     IsHOw
/402CHANGED MATERIAL ITEM 7 4AUD.4 1 F-1 ASSEMBLYSCALE: 1,1BMACHINE SCREW, FLAT HD,A CAPHILUIPS, TOO 316 SST OR3U4 SOT 7UNC-2A 0172 LU __1 8 35461.2 CAPSULE INSERT ASSEMBLY1 635451.1 CAPSULE HOLDERHASSEMBLVY 1 63S462-I GRAPHITE CONTAINER3 ASSEMBLYDC -1 IRRADIATION FACILITY ASSEMELY I-1 SAFETI PART OB IIOAIELtISERE UHIE RIE,/PECFECATEH ITEIT. EIEqNTEMTI ECAET.,'P' URAE,.SRMA o..510011(1SFTI-1 SECTIONED ISOMETRIC REFERENCEONLY SCALE: NONEFINALNEXT 05TN400 B EASlN U. MORRELL PURDUE UNt~fERSITY ETORiroOR TNAN OLOHAM TEST RESEARCH AND TRAINING REACTORTOOT , NTA U 0 004C so IRRADIATION FACILITY ASSEMBLY.. ...... ..... 1M owG.635460 N EBOTI 505051 1FAPI16.1 C AD Ann,.HSiY 3-71 A.RT I/O/Rh 101IS~TI F STBACUB/OE 7 6 4 2 1 S2EU32876'P42,1 SD8032
                                                                                    -3 ASSEMBLY     (SIMILR)                                             AR AR SC                       WELDFILLERMETAL           ER4043           AWEANS)   BS 1                  -T*       SOUIRCEDRIVE NOZZLE         MK   RMASU-ASSEMBLY                 MK   RM656-I   "'         -H       NOZZLE                   MANE FROGM B3SAHT-3         B IINCONTAINER                                        MN   RMBNS-1     N1       -       TUNE ASSEMBLY             MK   RM656*
-712432I1I P 4, I.I.,ll I REASONSREV STATESNOTES:1. REMOVE ALL BURRS AND SHARP EDGSES.2. pROCURE.
SCS3.OURCE               DRIVE CONTAINER3 S-3       ASSEMBLY3
FABRICATE.
                                                                                                                                                                                  -2       REMOVED2 S-,       GRAPHITECONTAINER ASSEMBLY1 PA*I*
AND INSPECT PER SPECIFICATION SPC-382.3. WELD PER SPECIFICATION SP0-322 APPENDIX R. USING ITEM 17 {WE LD FILLER METAL).4.ALL CORNER AND FILLET OTIIERISSE NOTED.ITITI1IREV IDESl.ETSj REVISED TOLERANCES ONl ITEM1%o?I I ..............
4-NEAGA*S!"ENT.VINNOLA                 PUDUE UNIVERSAITY HAHN)S, NORRELL               TESTRESEARCH ANAD TRAININGREACTOR
IDI-_(2.755)...........................
                                                                                                                                                                    *m        5)3.1 N. GIGISAM               GRAPHITECONTAINER ASSEMBLY ISSAA            ENAWJANA.                   ANDSOURCE DRIVECONTAINER  ASSEMBLY
J-O SEE DETAIL3 SEE ASSC-1 ASSEMBLYSCALE IllAR AR AR AR SC ELILRMTL ER4043 AWDA5AD 17AR SC BAR. 01/)2 ASTM B211 INAL SON61.TNST AR SC 0114 ASTM B2TT ISAL 6021-T05 1AR SC 002101t18 ASTM B211 14ALBAAI. TB51AR SC TUBING, 1 TI8OD X D05 WALL 12AL. DEI-TE ASTM B21DAR SC WALL IlALBAA61.TB ASTM 82121 C 10 PLGpLATE, 1127115 ASTM BUS IDAL 661 T-5I SC -B CAPSULE UPPER TUBE BAR, 01 31 ASTM 8211 9t S -8 CAPSUIE HOLDER TOP PLATE. I THE ASTI, BUSS 8tSC -7 CAPSULE BOTTOM PLATE. 54114TK P.574 8209 71 5 35405-2 GRAPHT CAPSULE HOLDER SSC *4 CAPSULE HOLDER TOP PLATE41 SC .3 CAPSULE HOLDER WELDMENT3 ASSEMBLYSC -2 CAPSULE RNSERT ASSEMBLY 2SC .1 CAPSULE HIOLDER ASSEMBLYP0279 IBEREIELFATIO TO45 .D535A5\* "4-1 7F 5 THR..2753XH RU-LK5WOE/BOOtlN SSAEIOUHRNB AT-1 ISOMETRIC REFERENEONLY SCALE: NONEoDETAILSCALE: U11P4415SIL$
                                                                                                                                            -HASNAG)5ANN
-2 635460-I 635460-B.B,m 5y T.RINOLADEBA MORRELIBRBB IB*4,92 O IDA I0 c 9911 55095115*1 8RPURDUE USIVERSITY TEST RESEARCH 4245 TRAINING REACTORCAPSULE HOLDER AND CAPSULE INSERTASSAMBUES AND DETAILA1 I*'*PUJR- I SAR Appendix 3-72 ReP 2. July 23, 2015:_=='OF 3* -,^ b 31 '8 18701 a7654321D"4"4"1-3 ASSEMBLYSCALE: lt-02.6.0065 X45"8 ESDETA(255)SECTION A-ASCALE LISECTION B-BSCALE IIIB20 14-4-000~1'4- ABCBVVB~I[0]-4 ASSEMBLY-8 ISOMETRIC ONLSCALE: NONEADETAILSCALE: il1PUR-i SAR AppendLx 3-73 Roy 2, July 23. 201.5D O1MF3 ow3.635461 1[0 I b 4 1 008032U/t5421 J, ,lQ"7R1a -7 A0-u-iC'1-2 ASSEMBLYSCALE: Oit0110 IR2.750f-0 -01.040 -H01(.1O)
                                                                                                                                            -IA5NI                      rnAO3    OENNWA)P)NANLSNAV)NS                             t'NCE'P VIEW A                                                                                                                                              SAD6354621M3ISW SCALE:*I                            FUR-I1SAR Appendix 3-75     Rev 2, July23, 2015  VIEW B 4              .1.
C) DETAILBC) DETAILSCALE. 211A-2 ISOMETRIC FIEFNENCE OLYPUR-1 SAR AppendLx 3-74 Re'," 2. July 23.20150 IO1MF3' ow-356SCALE NONE PUR-i SAR Appendix 3-74 Rev 2. July 23. 2015B / 'P 4 :3 2874321 4,.7IVA91NOTES:1. REMOVE ALL BURRS AND SHARP EDGES.2. PROCURE.
                                                    /I                         b t*                          b9                            4         :J
FABRICATE.
 
AND INSPECT PER SPECIFICATION SP-32.3. WELD PER SPECIFICATION SPC-SJA2 APPENDSX B. USING ITEM B WEhLD F'iLLER METAL).A. ALL CORNER AND FILLET RADII .232 UNLESS OTHERWISE NOTED.4CRITICAL INTERFACE DRMENSIONS SHALL RE ADHERED TO,/~VERIFY ULAR CAVITY AND SLOT SIZE WITH GO-NO-GO DAUGE. DIV PROVIDEDGO-NO-GO GAUGE SHALL SLIDE FREE LY THIROUGHOUT ENTIRE DESIGNATED CAVITY (ORSLOT) LENGTH FOR ALL SLOTS WITHOUTY HANG-UP.
8                 I                 7                 I             I4                                           I                               I             2                                   I NOTES:                                                                                                                                             I   I       I   I..
STICKING.
: 1. REMOVE ALL.
OR DISENGAGEMENT FROMSLOT.REMOVED PRIOR REV HISTORY IO4SEE ECR-55V8)R72/0 REVIVED DIMENSIONS BSlD.---.---.
BURRS ANDSHARP  EDGES.SE                                                                                                                                             c.583720
J, m-1 ISOMETRIC REFERENCE ONLYSCALE: NONE-1, ASSEMBLY IsHOw-3 ASSEMBLY (SIMILR)AR AR SC WELDFILLERMETAL ER4043 AWEANS) BS1 -T* SOUIRCE DRIVE NOZZLE MK RMASU-ASSEMBLY MK RM656-I "' -H NOZZLE MANE FROGM B3SAHT-3 BIINCONTAINER MN RMBNS-1 N1 -TUNE ASSEMBLY MK RM656*SCS3.OURCE DRIVE CONTAINER3 S -3 ASSEMBLY3
: 2. PROCURE. FABRICATE.
-2 REMOVED2S -, GRAPHITE CONTAINER ASSEMBLY14--HASN AG)5ANN-IA5NINEAGA* S!"EN T. VINNOLA PUDUE UNIVERSAITY HAHN) S, NORRELL TEST RESEARCH ANAD TRAINING REACTOR5)3.1 N. GIGISAM GRAPHITE CONTAINER ASSEMBLYISSAA E N AWJAN A. AND SOURCE DRIVE CONTAINER ASSEMBLYrnAO 3 OENNWA)P)NANLSNAV)NS t'NCE'PSAD6354621M3ISW VIEW ASCALE: FUR-I1 SAR Appendix 3-75 Rev 2, July 23, 2015VIEW B.1.I b 9 4/b4:J 8 I 7 I I4 I I 2 INOTES: I I I I..1. REMOVE ALL. BURRS AND SHARP EDGES.SE c.5837202. PROCURE.
ANDINSPECT  PERSPECIFICATTON SPC-382,                                                                                                                       SEEECR.652525                             811507 I/3ALL GROOVE   LOCATIONING DIMENSIONS ARE*8802ANDTOLERANCE  SHALL NOTSEACCUMULATIHE UNLESSOTHERWISE  SPECIFIES.                                                                                                                           8SEER53R L+/-&#x17d;WELDPREPASNECESSARY.
FABRICATE.
AND INSPECT PER SPECIFICATTON SPC-382, SEE ECR.652525 811507I/3ALL GROOVE LOCATIONING DIMENSIONS ARE *8802 AND TOLERANCE SHALLNOT SE ACCUMULATIHE UNLESS OTHERWISE SPECIFIES.
8SEER53RL+/-WELD PREP AS NECESSARY.
5.REMOVEDD
5.REMOVEDD
/Z\TOLERANCE XXX 1.041-2RV8X.005 MAD 255722 .28_D -.1883 CZ-:2.AA cm.]oE0 .-.8 (Cm TNDR IEPLT HE O LTjBT 211C ETILL8THND8HW  
/Z\TOLERANCE XXX 1.041
-0 EMVE 1-2284 __ __H__ET-1DEAI 098 N________-__PARPT__L,-E AT ~ -.84 __ ____ ___.21 ,, *622STANDARD SIDE PLATE SHEET OR PLATE ATMB2SC -1 ERGT SAND ALNIT 85361221T6 G DEALETADSHSRI-IT REMOVES ID-3 GTOrRLSDETAIL RIGHTE ANS06 OPOSTE) SCMB21 -5 SPCRPLATED 82417(I) UT ASTIM 8209 5uSLEFT HND5Al.8881-T 1-C 635STANDARD SIDE PDLN E.MEETEOR PLATE ANSVER 8221*6 3548 R/ LEFTDU HANDT RESEARC1.DTP8 GRfC-.3 REMOVED548 o~&#xa2;CONTROLSII 5 PLT SETDPAE STI 2213 21IREMOVED 7 4 9D6-C) DETAIL LEFT HANI SO VsowlDETAIL rnGHTIIANO(oPPosITE PUR- I SAR Appendix 3-77 Rev' 2, July 23, 2015I : &L. I 2i ZI- 2 1 Seib/00Z I.0fl.010J/-> 040045I/ .00420 4( 2260.9451242xx20 .,77.1701 2 1.3155.DETAILI //I nlnl l00.T 3400270F OX .255fo20 .25045 -'2~I. _______ I40, 2.0100)DETAILPUR-i SAR Appendix 1-70 Rev 2, July 23, 2015 1a"7R'I,2tI f I V I v * ! V I I iD-.355AL(TOP) (BOTTOM}A-AE PARALLEL WITHIN .005-11 ISOMETRIC ONLSCALE: NONECBA) DETAIL/ASCALE: 111OUR-I OAR Appendix 3-79 Rev 2, July 23, 2015D OJMF3 00S~ 63 46 6EA3EE ROTED OE0f l 0I .'"PR I ' i2. .../I::).Z,Z O"7'S55',,A5-111111 7NOTES:1. REMOVE Alt BURRS AND SHARP EDGES.2. PROCURE, FABRICATE, AND WNSPECT PER SPECIFICATION SPC-3BZ.3. WELD PER SPECIFICATION SPC-3B2 APPENDIX B USING ITEM 8 (WELD FILLER METALI.A ALL CORNER AND FILLET RADII .230 UNLESS OTHERWISE NOTED.S. REMOVEDATOLERANCE:
                              -2RV8X.005MAD                                                              2557 22 .28_D -                                                                                                                                                         CZ                      .1883
A. IIAXCERNE I IR H NID FCNTIE0UE SY53.A-LL1LLLIZLIJREVXTATU 12~ ~ FSREVISED TITLE; REVISED ITEM 3; ADDED NOTE A;ADDED SHEET 2 & 3; ADDED ITEM 2:SEE DAR-SSBA4VX 1/TAX?7TOTALLY REVISED SHEET 2C REMOVE D CHAMFER 440FROM DETAIL U. ADDED RADIUJS DIMENSION TO AlSITEM 3, REMOVED MOTE S. SEE DAR-D14751 3SEE ECX-551R72 T/2/07ADDED NOTE 7.ID-1 ISOMETRIC REFERENCEONLY SCALE: NOSESE .... SEE DETAIL(SSSTU = II2.i.IS .13..B1313 SEE DETAIL E1I~CI (2.5531-1 ASSEMBLYSALE: /1SR SC WELS FILLER METAL ER 4543 AWS A5.10 8_WOVEN WIRE CLOTH.SLUSC -V MESH TN16 B6MESH PER NACH, BAL ASTM E 2UISSC -3 NOZZLE PITEUMINA1Y MACHINED ALRXST. T6 ORAL 60A1-TN511 OR 3AL NXNI-TS5l SC -2 SOURCE DRIVE TOP AP L RUST-TENTf ASTM B20XASC -I SOURCE DRIVE NOZZLEASSEMBLY-T I/ST PAETISH NA'TURI.PXGCEEAIB(
                        -     :2.AA                                                                                                     cm.]oE0             .
I7512CVI. REBFIPITIC UHSSCXVER XEHRANNE I2mi.7PM IS UST-XN1 635TARTEBBIa y 5 REOUENTRH.
                      -   .8                                                                           (Cm                                                                   TNDR   IEPLT           HE O   LTjBT         211 C
T. AINMOLAAXSIVIN D. MORRELLgqITIR DRAWN AS.LHAt IcL oEAV IPURDUE UNIVERISITY TEST RESEARCH AND TRAINING REACTORSOURCE DRIVE NOZZLE ASSEMBLYAND SOURCE DRT/E TOPn
                                                                              -2284    __  __H__ET ETILL8THND8HW                                                 -0       EMVE                                               1
] 4IAO) DETAILSCALE: 1It0DETAILSCALE; litruE- I TAIlS A[T~ERUIX 55V WET 1. IXJ~ 1.1, ~AIT APREARRA I I~EC~X~EIDIART j1c118 NOTES SUET 1 OF 3B / B A'S 4 1 SURESA87(5,1=4 7 R "7 4DX11/4-28 UNF *.381, .375(FOP){8OTTOMA)
                                                    - 1DEAI 098                                                   N________-__PARPT__L,-E                                                                           '.T.*
Ct 2.52*, 01 _" [ '-2 ISOMETRIC REFERENC.'E 084,VSCALE: NONET22 ~.... :_/t (.25).-2X .219.284BOX ROE'C) ETAIL L/\APUJR- I 04AR Appendix 3-81 Rev 2. July 23. 2015SSF41. NOTED 2d 3 2+ '5/00q.Z 7417 N17I IID-1 ISOMETRIC REFERENCEONLY SCALE: NONEB0 DETAIL/AAPUR- 1 SAR Appendix 3-82 Rev 2, July 23, 2015D OJMF3 owci-635467 4nolAn ati / b 9 4 1 ..... I 0-- 9/bb41 NOTES:1. REMOVE ALL BURRS AND SI-ARP EDGES.2. PROCURE, FABRICATE.
AT         ~__  -. ____
AND INSPECT PER SPECIFICATION SPC-382.A AILLCORNER AND FILLET RADII D030 UN LESS OTHERWISE NOTED.4. REMOVED,/ TOLERANCE:
84       ___
.0031 ABA5-1 ISOMETRIC REFERENCE ONLYSCALE NONEo DETAILAPUR-l SAR Appendix 3-83 Rev 2, Jully 23, 2015 7,1,A,0O"t0DX1)4-28 UNF.- 3B 7.375(TOP) (BOTTOM)-2 ISOMETRIC SCALE: NONE-- 2X .07BC) DETAIL A\SCALE: 11PUR- I SAP. Appendix 3-84 Rev 2, July 23, 2015O OJMF3 owe.635468 48A~EE NOTED EEl 2I 1 S08183A-a T -, "r 'I02}}
                                                                  .21   ,,                                                                                             *622STANDARDSIDE  PLATE       SHEET ORPLATE    ATMB2 SC
                                                                                                                                                                      -1       ERGTSAND                ALNIT           85361221T6 G DEALETADSHSRI-IT                                         REMOVES                                             ID
                                                                                              -3 GTOrRLSDETAILRIGHTE ANS06 OPOSTE)                                 SCMB21 -5     SPCRPLATED               82417 (I)     UT                                                                                                         ASTIM 8209   5uS LEFT HND5Al.8881-T 1-C 635STANDARD                             SIDEPDLNE.MEETEOR       PLATE ANSVER   8221
                                                                                                                                                  *6 3548 11111m*    R/     LEFTDU HANDT               RESEARC1.DTP8 GRfC
                                                                                                                                      -.                         o~&#xa2;   3    REMOVED548                                            3*
5     CONTROLSIIPLT        SETDPAE       STI 2213                                     21IREMOVED
 
7                                                 4                               9 D
6-C) DETAIL LEFT HANISOVsowl c*) DETAIL rnGHTIIANO(oPPosITE PUR- I SAR Appendix 3-77   Rev'2, July23, 2015 I  :
                                                                                        &L. I Is*.ee  2 ZI-                                         2       i        1     Seib
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      .945 124 20.,77.1            701 2 1.315 0* DETAIL 2x              5.
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                                                                                                            -11 ISOMETRIC SCALE:
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            ) DETAIL/A SCALE:111 OUR-I OAR   Appendix 3-79     Rev 2, July 23, 2015 ROTED EA3EE  OE 6346 DOJMF3 00S~     6 0f  l             0I
                    *    .                                                               '"PR   I '             i2.                                 . ..
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O                                     "7                                 'S                                55                ',,             A                                                      5-1 11111                            7 NOTES:                                                                                                                                                                    LL1LLLIZLIJREVXTATU              12~                            ~                    F
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ADDED SREVISEDSHEET TITLE;  2REVISED
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Latest revision as of 09:42, 31 October 2019

Purdue University - Request for Additional Information Regarding the Purdue University Reactor License Renewal Application (TAC No. ME1594), Responses to Letter Dated August 29, 2014 (ML14115A221). Part 5 of 5
ML15210A288
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Text

APPENDIX 2: NATCON INFORMATION Hot Channel Factors in the NATCON Code Version 1.0 The NATOON code version 1.0 [Ref. ANL/RERTR/TM-12] uses three hot channel factors (FQ, FW, FH). Using the source code and documentation, the factor FH used in NATCON is found to be the same as the factor FNUSLT used by E. E. Feldman. Table 1 shows the tolerances and uncertainties included in each of the six hot channel factors used by E. E. Feldman. The correspondence between the NATCON hot channel factors and E. E. Feldman's six hot channel factors is as follows.

Feldman's Hot Channel FactorNC CNInu Variable System-wide Factors:

FFLOW a factor to account for the uncertainty in total reactor FW (approximately) flow FPOWER a factor to account for the uncertainty in total reactor FQ power FNUSLT a factor to account for the uncertainty in Nu number FH correlation Local Factors:

FBULK a hot channel factor for local bulk coolant FBULK (new input) temperature rise FFILM a hot channel factor for local temperature rise across FFILM (new input) the coolant film FFLUX a hot channel factor for local heat flux from cladding FFLUX (new input) surface Hot Channel Factors in the NATCON Code Version 2.0 PUR-1 SAR Appendix 2-1 PUR-SARAppndix2-1Rev 2, July 23, 2015

Sections 2.1 and 2.2 develop, for laminar natural convection, two thermal-hydraulic relationships that are used in section 2.3 to obtain formulas for the hot channel factors from user-supplied manufacturing tolerances and measurement uncertainties. The results of section 2.3 are summarized here for convenience. The first three are local/random hot channel factors, and the last three are system-wide. An example of the use of these hot channel factors is given in section 4, with NATCON running instructions in section 3, and the new input description in section 5.

FBULK- 1 +j{(1+ u)2a+(1+ u 2 )2+-r-:U1 2--* +u62 FBULK is higher (conservative) if the temperature dependence of water viscosity is ignored.

FFILM = 11u 1 2+/-+u 2 2+/-+u 3 2 +u4 2+/-+u 5 2 FFLUX -- l*u 2 +u 2 +/-+u2 +u4 1 2 3 FQ = 1 +u-FW = 1 + u8 FH = 1 +- u9 where ul= Fractional uncertainty in neiitronics calculation of power in a plate u2= Fractional uncertainty in U-235 mass per plate =Am/_M u3 Fractional uncertainty in local (at an axial position) fuel meat thickness u4= Fractional uncertainty in U-235 local (at an axial position) homogeneity u5 = Fractional uncertainty in coolant channel thickness = (tnc - thc) / tn u6 = Fractional uncertainty in flow distribution among channels u7= Fractional uncertainty in reactor power measurement u8= Fractional uncertainty in flow due to uncertainty in friction factor Ug = Fractional uncertainty in convective heat transfer coefficient, or in the Nu number correlation M = Nominal mass of U-235 per plate, gram Am = Tolerance allowed in U-235 mass per plate, gram PUR-1 SAR Appendix 2-2 PUR-SARAppndix2-2Rev 2, July 23, 2015

The code obtains, for an input nominal reactor power CPWR, a thermal-hydraulic solution using the three systematic hot channel factors FW, EQ and FH. If the user-input reactor power is zero, then the code itself chooses the nominal power from a series of power levels (10 kW, 100 kW, 200 kW, and so on increasing in steps of 100 kW). This thermal-hydraulic calculation is done for a hot plate power of CPWR*FQ*(Radial power peaking factor RPEAK)/(Total number of fuel plates in standard and control assemblies). Also, the frictional resistance to flow is multiplied by FW 2 , and the convective heat transfer coefficient found for laminar flow in a rectangular channel is divided by FH. The random hot channel factors FBULK, FFILM and FFLUX are not used in this solution.

Having obtained the above solution, the random hot channel factors FBULK, FFILM and FFLUX are applied to the temperatures obtained, using the following equations. The temperatures calculated with all six hot channel factors are printed after the above solution. The onset of nucleate boiling ratio, ONBR, is computed using the temperatures with all six hot channel factors applied (using the equation below). If the user-input nominal power is zero, then the last nominal power for which the code prints a solution is that at which the ONBR is 1.0.

Ti,6hcf = To + (Ti- To)*FBULK Twalj,i,6hcf = Ti,6hcf + (TwaiiUi- Ti)*FFILM Tmax,j,6hcf = TwaII,i,6hcf + (Tmax~i - TwaIlU)*FFLUX where To = Bulk water temperature at the coolant channel inlet, i.e., the pool temperature, T* = Bulk water temperature in node i of the channel with only systematic hot channel factors applied, 00 Twai,i Cladding surface temperature in node i with only systematic hot channel factors applied, °C Tmax,i =Fuel meat centerline temperature in node i with only systematic hot channel factors applied, °C TI,6hof = Bulk water temperature in node i of the channel with all six hot channel factors,

°C TwaII,i,6hcf = Cladding surface temperature in node i with all six hot channel factors, 0C Tmax,i,6hcf = Fuel meat centerline temperature in node i with all six hot channel factors, C T~o, = Incipient boiling temperature in node i with only systematic hot channel factors applied, C PUR-1 SAR Appendix 2-3 PuR-SARAppndix2-3Rev 2, July 23, 2015

Flow Rate in a Coolant Channel versus Power of a Fuel Plate NATCON is a laminar natural circulation code. The flow rate is calculated in the code by balancing the buoyancy pressure force to the laminar friction pressure drop. Following this concept, an analytical relationship is developed here (with some approximation) for the coolant flow rate in a single coolant channel in terms of the power generated in a fuel plate and the channel geometrical dimensions. The analytical relationship is needed for obtaining hot channel factors.

The hot channel factor FW used in the code to account for the uncertainty in coolant flow rate is actually applied to the laminar friction factor in the code, that is, the laminar friction factor is multiplied by FW 2. It is not applied directly to the flow rate. The relationship developed here explains how this technique works.

p1 , T1 at channel outlet IL = Channel height containing hot coolant (hotter than pool), m IP = Power in a single fuel plate or the two half plates, W IW=Upward flow rate in a single channel, kg/s po, To at channel inlet Schematic of what the code analyses, that is, a single rectangular coolant channel heated by a half of a fuel plate on each side (right and left sides).

The above schematic shows what the code analyses, that is, a single rectangular coolant channel heated by a half of a fuel plate on each side (right and left sides). See Fig. 1 for details.

The buoyancy pressure force is caused by the decrease in water density due to heating in the channel. The temperature dependence of water density can be written as

,p(T)=po - ,p0 ,8 (T -To ) (I) where T1= Bulk water temperature at channel outlet, C AT = T1 - To = Temperature rise in channel from inlet to outlet, C PUR-1 SAR Appendix 2-4 PUR-SARAppndix2-4Rev 2, July 23, 2015

p0 = Water density at channel inlet, i.e., the water density in the pool, kg/rn 3 I? = Volumetric expansion coefficient of water, per C

,p = Average coolant density in the channel, kg/rn 3 L= Channel height that contains hotter coolant (hotter than pool), m. It is the sum of heat generating length of fuel plate, non-heat generating fuel plate length at top, and the assembly duct length above the top of fuel plate g = Acceleration due to gravity, 9.8 m/s 2 The buoyancy pressure force is given by BuoyancyAp =(po -p)gL (2)

The average coolant density p is given by p =O0.5 (po+p,) = p0 -0.5,po /J(T 1-To )= p 0 - 0.5,Op0 fAT (3)

Buoyancy Ap = 0.5 p 0 ,/1 AT g L (4)

The coolant temperature rise AT can be written in terms of the input power P generated in a fuel plate, as shown by Eq. (5) below, and then the buoyancy A p of Eq. (4) can be written in terms of the input power P, as shown by Eq. (6).

AT = P/ (W Cp) (5)

_ 0o/gLP BuoyancyAp - WC(6)

Ignoring the minor losses at channel inlet and outlet, the laminar frictional pressure drop in the channel is written below as Eq. (9) after using the laminar friction factor given by Eq. (7), and after replacing the coolant velOcity by mass flow rate using Eq. (8). The parameter C in Eq. (7) is a constant for a given channel cross section, but it depends upon the channel cross section aspect ratio width/thickness, and varies from 57 for aspect ratio 1.0 (square channel) to 96 for an infinite aspect ratio (infinitely wide channel).

f =C /Re (7)

W= pAV (8)

PUR-1 SAR Appendix 2-5 PUR-SARAppndix2-5Rev 2, July 23, 2015

2 = C ULcW(9 Fritioal Fritioal P p_ *'k-'V 2D 24p AD 2 9 where f - Moody friction factor for laminar flow in the channel Re - Reynolds number in the channel = ,oVD/,u A = Flow area of the channel cross section, m2 D = Equivalent hydraulic diameter of the channel cross section, m Lc = Total coolant channel length causing frictional pressure drop, m.

V = Coolant velocity averaged over the channel cross section, m/s W = Coolant mass flow rate in the channel, kg/s 11 = Average coolant dynamic viscosity in the channel, N-s/rn 2

/u (T) = Temperature-dependent dynamic viscosity of water, N-s/rn 2

/-Uo =1, (To) = Coolant dynamic viscosity at the channel inlet temperature To For the PUR-1 reactor, the temperature dependence of the dynamic viscosity of water over the temperature range 27 00 < T < 50 °0 can be approximated as follows.

pz(T)= ,p(To)(1+T-T) )- 0 (10) where a = 0.12, To = 2700C, , ( To) = 0.875x10 -3N-s/in 2 The average coolant dynamic viscosity ,p used in Eq. (9) can be set equal to the viscosity at the average coolant temperature (To + 0.5AT) in the channel. Putting this temperature in Eq.

(10), the average viscosity ,u is found to be p* = ,p(To)(1 +0.5AT) -.0 (11 )

Equation (11) indicates that the average viscosity 41 can be set equal to ,p ( To) if AT is just a few 00 (this is the case for the PUR-1 reactor at the operating power of 1 kW). If AT is greater than a few 00, i.e., 1 <<0.5AT (this is the case for the PUR-1 reactor at an ONB power of about 100 kW), then Eq. (11) simplifies to the following.

PUR-1 SAR Appendix 2-6 PUR-SARAppndix2-6Rev 2, July 23, 20i5

,u= ,u ( To) (0.5AT)- 0 ifi ATT>> 22 0°C 1a (12a)

/ 1u /u(To) if AT<<2 °C (12b)

Substituting Eq. (12a) into Eq. (9), the frictional Ap becomes Frictional Ap = Cui°(AT)-*LcW=- C'U°LcW (-'W-p' (13) 21-a p AD 2 21-° 7 AD 2 \ /-,

P Equating the frictional A p of Eq. (13) to the buoyancy A p of Eq. (6) to find the steady-state coolant flow rate W in the channel, one obtains Eq. (14) below. Equation (14) can be rewritten as Eq. (15).

P0 flgLP-_ C 'u-----°L-W-- (-W " (14) 2WCp 21-a p AD 2 )

W -+ p0poAD2 /3gLPl+a 15 2' CltoLc C* 15 Equation (15) relates the fuel plate power to the channel flow rate in natural circulation. It is used to find the dependence of the flow rate on the parameter C in the laminar friction factor (at constant power). All parameters in this equation are constant (p* is also practically constant) except the parameter C in the laminar friction factor. Based on Eq.(15), the relationship between the flow rate W and the parameter C is given by Eq. (16) below.

Wcc I (16)

Equation (16) shows that the friction factor parameter C is multiplied by a factor (FW) 2, the 2

coolant flow rate W will be reduced by the factor (FW) 2+a,. This has been verified by actually running the NATCON code for the PUR-1 reactor. Since a is small (a = 0.12 for the PUR-1 reactor), 21(2+a) is nearly 1.0, and the flow rate W is reduced approximately by the factor FW.

Bulk Coolant Temperature Rise versus Power of a Fuel Plate Equation (5) expresses, for laminar natural circulation, the bulk coolant temperature rise in terms of fuel plate power, coolant flow rate and specific heat. Putting the value of flow rate obtained in Eq. (15) into Eq. (5), the bulk coolant temperature rise is given by Eq. (17) below, purely in terms of power and the geometrical dimensions of the channel. The right hand side of Eq. (17) is rearranged into two factors in Eq. (18), such that the second factor is sensitive to power and channel geometrical dimensions that usually have manufacturing tolerances and PUR-1 SAR Appendix 2-7 PUR-SARAppndix2-7Rev 2, July 23, 2015

measurement uncertainties, and the first factor is insensitive to power and channel geometrical dimensions.

AT =::" 2;Q ---°c;-]*P j2÷ (17)'

AT[C~p~po/gL .A (18)

The nominal flow area and hydraulic diameter of a rectangular coolant channel are given by A = tnc Wn (1 9)

Pw= 2 (tnc+ W~c) (20)

D = 4 A/ P~, = 2 tnc Who / (tnc + Wnc) (21) where to = Channel thickness (spacing between fuel plates), m to = Nominal channel thickness (spacing between fuel plates), m thc = Minimum channel thickness in hot channel (spacing between fuel plates), m Wc =Channel width, assumed not to change from its nominal value, m Pw = Wetted perimeter of the nominal channel, m Pc = Power generated in a fuel plate, without applying manufacturing tolerances, W Phc = Power generated in a fuel plate, after applying manufacturing tolerances, W Because the channel thickness to, is much smaller than the channel width Wc in most experimental reactors, Eq. (21) reduces to o ,* 2 tc, (22)

Using the channel area and hydraulic diameter given by Eqs. (19) and (22) into Eq. (18), the bulk coolant temperature rise can be written in terms of power, channel thickness, and channel width. This is the desired relationship for use in finding hot channel factors.

PUR-1 SAP, Appendix 2-8 PUR-SARAppndix2-8Rev 2, July 23, 2015

CfOL

-- -- -7_- 1 (23)

C /o3afgL'* 4w~t3 Formulas for Hot Channel Factors For use in the NATCON version 2.0, six hot channel factors (three global/systemic and three local/random) are obtained from 9 manufacturing tolerances and measurement uncertainties u1 ,

u=,..., u 9 that are defined below. These are fractional uncertainties rather than percent. Of these nine uncertainties, those affecting a particular hot channel factor are indicated in Table 1. The systemic hot channel factors are given by Eqs. (24) through (26), and the random hot channel factors are given by Eqs. (27) through (29). A utility Fortran computer program NATCON_HCF and a Microsoft spreadsheet NATCON.HotChanFactors.xls have also been developed to compute the hot channel factors using these formulas.

EQ = 1 + u7 (24)

FW =1 + u8 (25)

FH = 1 + u9 (26)

The ratio of the power generated in hot plate to its nominal power, caused by the uncertainties in neutronics-computed power and in U-235 mass per plate, can be written as Ph...._c(1 +u1 )(1+/-+u 2) (27) nPo The ratio of bulk coolant temperature rise in hot channel to the temperature rise in the nominal Channel, caused by the uncertainties in neutronics-computed power, U-235 mass per plate, and channel thickness, is obtained from Eq. (23). Only the quantity in the second parentheses is important here because the quantity in the first parentheses is insensitive to these uncertainties.

~h 1 (28)

The uncertainty in flow distribution is assumed to reduce the channel flow to (1- U6 ) times the flow without this uncertainty, and therefore the bulk coolant temperature rise is increased by the factor (1+ u 6 ). This uncertainty in bulk coolant temperature rise is statistically combined with that given by Eq. (28) to obtain the following formula for the hot channel factor FBULK for input to the NATOON version 2.0.

FBULK= 1 +, lu)*g'~22T 1. -1+u2 (29)

PUR-1 SAR Appendix 2-9 PuR-SARAppndix2-9Rev 2, July 23, 2015

The temperature drop across coolant2 film on the cladding surface at an axial location is given by Eq. (30). Here the heat flux q" (W/m ) on the cladding surface is replaced by tf q'"/2 in terms of the volumetric power density q"'" (W/m 3 ) in the fuel meat.

Aflh 2h (0 The convective heat transfer coefficient h (W/m 2 -C) is given by Eq. (31). Here the laminar Nusselt number Nu is independent of flow rate, and varies only slowly with the aspect ratio (width/thickness) of coolant channel. The main variation of the heat transfer coefficient with channel thickness is due to the denominator of Eq. (31). The numerator of Eq. (31) is considered to be constant.

h - NKc°° - N"IKC°°! (31)

D 2tc Using Eq. (31) for the heat transfer coefficient, the temperature drop across coolant film can be written as Eq. (32).

fil~m - Nco (32)

Equation (32) states that ATift,~is directly proportional to the fuel meat thickness (having uncertainty u3 ), the channel thickness (having uncertainty u5 ), and the power density in meat.

The uncertainty in power density is caused by three uncertainties, that is, u1 , u2 and u4 .

Statistically combining these five uncertainties gives the following formula for the hot channel factor FFILM for input to the NATCON version 2.0.

FFILM =1+4Ul2+/-+u 2 2+/-+u 3 2+/-u-/

4 2+/-*U5 2 (33)

The uncertainty in the heat flux at the cladding surface is included in the hot channel factor FFILM given by Eq. (33). A hot channel factor FFLUX for the heat flux alone can be found from Eq. (34) for heat flux in terms of the power density q"'" in the fuel meat and the thickness of the meat. The fractional uncertainty in heat flux is the sum of fractional uncertainties in power density and meat thickness, as given by Eq. (35).

q" t- (34) 2 Sq"_ Sq '" Ste

__ +/- fe (35) q,, q,, tfuel In Eq. (35), the uncertainty in power density is caused by three uncertainties, that is, u1 , u 2 and u4 . The uncertainty in the meat thickness is given by u3 . Statistically combining these four uncertainties gives the following formula for the hot channel factor FFLUX for input to the NATCON version 2.0.

PUR-1 SAR Appendix 2-10 PUR-SARAppedix

-10Rev 2, July 23, 2015

FFLUX= 1+ */~u1 2 +//2 -+/-u32 +u 42 (6 (36)

The uncertainty in the temperature drop ATmetal from fuel meat centerline to cladding surface is not important in the case of the PUR-1 reactor because ATmetai is very small compared to ATritm.

For example, ATmetai is 0.05 00 and ATfilm is 34.5 00 at 100 kW without any hot channel factors.

Table A2-1. Uncertainties Included in the Six Hot Channel Factors Used in NATCON Version 2.0 (X implies that an uncertainty affects a hot channel factor)

Uncertainty Fraction FQ FW {FH FBULK FFILM FFLUX Local or random uncertainties I Neutronics calculation ofXXX power in a plate, u1 2 U-235 mass per plate, u 2 X X X 3 Local fuel meat thickness,XX u3 4 U-235 axial homogeneity,XX 5 Coolant channel thickness,XX u5 6 Flow distribution amongXX channels, u6 System-wide uncertainties 7 Reactor power measurement uncertainty, X 8 Flow uncertainty due to X

___uncertainty in friction_____

PUR-1 SAR Appendix 2-11 PUR-SARAppedix

-11Rev 2, July 23, 2015

factor, u 8 9 Heat transfer coefficient uncertainty due to uncertainty in Nu number correlation, u9 The following information was presented as answers to Requests for Additional Information (RAIs) during the conversion process. This information is not presented in the SAR chapters on thermal hydraulics.

Question 28

28. Appendix 1. From the information in Appendix 1 it is not clear how insignificant are the channel inlet and outlet losses when compared to the wall shear. Please clarify.

Response

The information in Appendix 1 was used only to obtain hot channel factors for input to a more detailed thermal-hydraulic calculation using the NATCON code [Ref. 8 of the conversion proposal]. Therefore, Appendix 1 is a simplified modeling of what is calculated in detail in NATCON, and it is used only for the purpose of obtaining closed-form equations from which hot channel factors could be found. Appendix 1 does not include the minor losses. The minor losses calculated by NATCON are reported below, and found to be about 16% of the total frictional pressure drop in the HEU core, and 14% of the total frictional pressure drop in the LEU core (see Table 027-1 ).

The pressure drop due to inlet and outlet losses were calculated (by the NATCON code) using loss coefficients of 0.5 and 1.0 respectively. The pressure drop due to wall shear along the channel length is found by summing the pressure drop for each axial mesh which is calculated using temperature-dependent coolant viscosity and density for the axial mesh (14 mesh intervals were used over the channel length in all calculations). The pressure drops are calculated by NATCON assuming fully developed laminar flow in a rectangular cross-section channel, and then multiplied by a factor FW 2 (FW squared) where FW is an input which may be used to account for the increased pressure drop due to hydrodynamically developing laminar flow. In the calculations presented in the conversion proposal, FW was always set to 1.0, and thus the increased pressure drop due to developing laminar flow was not included. It is included in the calculations presented here (Table 027-1). The method used is described below.

For the most limiting fuel plate in Table 4-27 of the conversion proposal for each core (HEU and LEU), a comparison of the pressure drops due to inlet plus outlet loss and wall shear, with and without the effect of developing laminar flow, are tabulated in Table 027-1.

NATCON calculates the Darcy-Weisbach friction factor f = C/Re for laminar flow, using a built-in table of the parameter C for different aspect ratios of the rectangular channel cross section PUR-1 SAR Appendix 2-12 PUR-SARAppedix

-12Rev 2, July 23, 2015

(values of parameter C are given in the response to Question number 29). An apparent value of the parameter C averaged over the channel length, called Capp, was calculated using Eq. (576) of Shah and London [Ref. 2 listed at the end of all responses] to account for the increased pressure drop due to hydrodynamically developing laminar flow in the channel. The ratio Capp/C was found to be 1.1105 for the 207 mil HEU channel, 1.0985 for the 197 mil LEU channel. Since the NATOON code multiplies the fully developed friction factor by FW 2 as mentioned above, the input FW equals 1.054 and 1.048 for the HEU and LEU channels respectively. NATCON calculations were done using these values of FW, and the pressure drops due to inlet plus outlet loss and wall shear are compared in Table Q27-1 (column B for the HEU channel, and column F for the LEU channel).

Table Q27-1 shows that the pressure drops due to wall shear and minor losses are 84% and 16%, respectively, of the total pressure drop in the HEU channel at its ONB power; and the pressure drops due to wall shear and inlet plus outlet loss are 86% and 14%, respectively, of the total pressure drop in the LEU channel at its ONB power.

Question 29

29. Appendix 1. From the information in Appendix 1 it is not clear what is the functional dependency of the laminar friction parameter C to the channel cross-section dimensions.

Provide a reference for the evaluation of C.

Response

The following values (rows 1 and 2 of Table Q29-1) of the parameter C for fully developed laminar flow in a channel of rectangularcross section versus the width-to-thickness aspect ratio (Wc/tc) of the channel are used in the NATCON code that was used in the thermal-hydraulics calculations. The table starts from the square cross section (aspect ratio = 1.0) and goes to the infinite value of the aspect ratio (parallel plates). In order to find the parameter C for the aspect ratio of the PUR-1 reactor, the NATCON code simply interpolates between the tabulated values.

The original author of the code obtained these values from an old Reference [E. R. G. Eckert and T. F. Irvine, Heat Transfer Laboratory, University of Minnesota (1957)] but these values are also given in a textbook by Frank Incropera [Ref. 3]. These values are obtained from the closed-form analytical solution for the fully developed laminar velocity distribution in a rectangular channel summarized by R. K. Shah and A. L. London [Ref. 2]. Equation (341) in [Ref. 2] is a fitted equation to easily find the parameter C. It should be noted that the aspect ratio used in

[Ref. 2] is channel thickness-to-width ratio (the reciprocal of that used in NATOON and shown below in Table A2-2), and the friction factor in [Ref. 2] should be multiplied by 4 to get the Darcy-Weisbach friction factor that is used in NATCON and tabulated below.

Table A2-2. Friction Parameter C Used in the NATCON Code wtc 1.0 2.0 3.0 4.0 5.0 6.3 8.0 11.0 15.0 18.0 100.0 C in 58.0 63.0 69.0 72.5 77.0 80.0 83.0 85.0 88.0 89.0 96.0 NATCON PUR-1 SAR Appendix 2-13 PUR-SARAppedix

-13Rev 2, July 23, 2015

C in 57.0 62.0 69.0 73.0 82.0 96.0 Ref. 3 C in 56.9 62.2 68.4 72.9 76.3 79.5 82.4 85.6 88.1 89.3 94.7 Ref. 2 Question 30

30. Appendix 1. From the information in Appendix 1 in both the calculation of the channel flow and the calculation of the bulk coolant temperature rise the ratio of the coolant kinematic viscosity to density (pip) was assumed to be insensitive to temperature. Please demonstrate the validity of this assumption.

Response

The information in Appendix 1 was used only to obtain hot channel factors for input to a more detailed thermal-hydraulic calculation using the NATCON code [Ref. 8 of the conversion proposal]. NATCON does account for the temperature dependence of coolant viscosity and density in the calculation of the channel flow and the calculation of the bulk coolant temperature rise. Therefore, Appendix 1 is a simplified modeling of what is calculated in detail in NATCON, for the purpose of obtaining closed-form equations from which hot channel factors could be found.

As suggested in the question, water viscosity is temperature-dependent, i.e., it decreases with rising temperature. Appendix 1 was revised to account for the effect of temperature dependence of viscosity on hot channel factors, and the revised Appendix 1 is enclosed herewith. The temperature dependence of the dynamic viscosity of water over the temperature range 27 00 <

T < 50 00 (adequate for the PUR-1 reactor) can be written as follows.

/()= /z(T 0 ) (1+T-T 0 )-0 (Al) where a=0.12 To= 27 00 = Pool temperature of PUR-1

,u ( To) = 0.875x10 -3 N-s/rn 2

,p (T) = Temperature-dependent dynamic viscosity of water, N-s/in 2 As shown in the revised Appendix 1, the revised relationship between the flow rate W in a channel and the friction parameter C is given by Eq. (A2). The revised formula for hot channel factor FBULK for bulk coolant temperature rise is given by Eq. (A3).

(A2 PUR-1 SAR Appendix 2-14 PuR-SARAppedix

-14Rev 2, July 23, 2015

FRUlLu )=+,(l+u9 )2+- lJ l -1} u (A3)

The exponent on the right hand side of Eq. (A2) changed from 0.5 (in the conversion proposal ignoring temperature dependence of p) to the revised value 1/2.12 = 0.4717. There exponents in Eq. (A3) for EBULK also changed, e.g., from 3/2 to 3/2.12 =1.415. As a result of this revision, the hot channel factor FBULK decreased from 1.312 (in the conversion proposal) to 1.301 for the most limiting fuel plate 262 in the HEU core. Similarly, FBULK decreased from 1.321 (in the conversion proposal) to 1.308 for the most limiting fuel plate 1348 in the LEU core. The effect of ignoring the temperature dependence of viscosity is conservative.

NATCON calculations were done with these revised values of EBULK along with a value of FW

> 1.0 to account for the increased friction due to developing laminar flow (in response to Question number 33). The results are shown in Table Q27-1 (column C for the HEU core, and column G for the LEU core).

As a consequence of the two effects (i.e., increased friction due to developing laminar flow and the temperature dependence of viscosity) on hot channel factors FW and EBULK, the ONB power of the HEU core changes from 76.3 kW (reported in the conversion proposal) to 75.9 kW, and the ONB power of the LEU core changes from 96.1 kW (reported in the conversion proposal) to 95.8 kW. The effect is small for the PUR-1 reactor.

Question 32

32. Appendix 1. Equation (30) has two terms and the conversion proposal states that the expression within the parenthesis on the right hand side of the equation varies slowly compared to the heat flux tfuel q'"/2. Demonstrate the validity of the statement with reference to the PUR-1 fuel plate.

Response

Equation (30) of Appendix 1 is for finding a hot channel factor for the temperature drop from the meat mid-plane to cladding surface (ATmetai). This temperature drop is very small compared to the temperature drop from the cladding surface to bulk coolant (ATflrn). For example, in the PUR-1 HEU fuel plate 262 without hot channel factors, Ammetai iS 0.07 °C and ATfi~m is 46.98 °C (at meat mid-height) at a high power of 100 kW. Similarly, in the PUR-1 LEU fuel plate 1348 without hot channel factors, Ammetai is 0.05 °C and ATfi m is 34.5 °C at a power of 100 kW.

Therefore, the hot channel factor for Ammetai iS not important for PUR-1. The important hot channel factor is the factor FFILM for ATf, m. In the case of PUR-1, ATtim is the bigger component (bigger than the bulk coolant temperature rise) in the total temperature rise from the inlet temperature to the cladding surface temperature at the axial level experiencing the onset of nucleate boiling. The hot channel factor FFILM found by Eq. (29) of Appendix 1 in the conversion proposal remains unchanged. It depends on the uncertainties in q'"tfuel and channel thickness (as shown in Eq. 28), but not on the uncertainty in [tfuel/( 4 KfueI) + tcdad/Kclad].

In short, PUR-1 is not limited by the fuel peak temperature, but by the onset of nucleate boiling, and the uncertainty in [tfuel/( 4 KfueI) + tclad/Kclad] is not important for PUR-1. We believe that the hot channel factor FFILM has been determined accurately.

PUR-1 SAR Appendix 2-15 PUR-SARAppedix

-15Rev 2, July 23, 2015

Question 33

33. Section 4.7.2. According to Appendix 1 the systematic uncertainty in flow rate is accounted for by applying the hot channel factor Fw to the laminar friction factor C. Explain the reason for the value of the flow friction factor Fw being unity in Tables 4-25 and 4-26.

Response

As suggested in the question, a value of FW (hot channel factor for flow) greater than 1.0 should be used to account for the increased frictional pressure drop due to the hydrodynamically developing laminar flow in the entrance region of the coolant channel, otherwise the code (NATCON) accounts only for the fully developed frictional pressure drop. This has been done now and the results are presented in Table Q27-1. Since each coolant channel creates its own buoyancy to drive its own coolant flow, there is no uncertainty due to redistribution of a total reactor flow rate. The loss coefficients of 0.5 and 1.0 at channel inlet and outlet are used in the calculations. To account for the reduction in flow rate due to the hydrodynamically developing laminar flow in the channel, the values of FW were calculated for the most limiting channels in the HEU and LEU cores as follows.

NATOON calculates the Darcy-Weisbach friction factor f = C/Re using a built-in table of the parameter C for different aspect ratios of the rectangular channel cross section (values of parameter C are given in the answer to Question number 29). These values of parameter C are for the fully developed laminar flow in a rectangular cross-section channel. An apparent value of the parameter C averaged over the channel length, called Capp, was calculated using Eq. (576) of Shah and London [Ref. 2] to account for the increased pressure drop due to hydrodynamically developing laminar flow in the channel. The ratio Capp/C was found to be 1.1105 for the 207 rail HEU channel, and 1.0985 for the 197 mil LEU channel. Since the NATCON code multiplies the fully developed frictional factor by FW 2 , the input FW equals 1.054 and 1.048 for the HEU and LEU channels respectively. The flow reduction factor is input factor FW or more accurately FW2/( 2+a) FW°'94 34 (noting that a = 0.12 for the PUR-1 reactor as mentioned in the revised Appendix 1 enclosed herewith).

The results of using these values of FW in NATCON calculations (excluding the effect of temperature dependence of p on hot channel factors) are shown in Table Q27-1. The ONB power of the HEU core changes to 75.8 kW from 76.3 kW reported in the conversion proposal.

The ONB power of the LEU core changes to 95.7 kW from 96.1 kW reported in the conversion proposal.

The channel flow indeed gets reduced by the factor FW0 9434 " as expected. For the HEU plate 262, the flow reduces from 0.02083 kg/s to 0.01 989 kg/s (see Table Q27-1) when the input hot channel factor FW is changed from 1.0 to 1.054. The expected reduced flow should be 0.02083/(1.054)0"9434 = 0.01982 kg/s which is close to the NATCON-calculated value of 0.01 989 kg/s. For the LEU plate 1348, the flow reduces from 0.01 912 kg/s to 0.01834 kg/s (see Table Q27-1) when the input FW is changed from 1.0 to 1.048. The expected reduced flow should be 0.01 912/(1 .048)0.9434 = 0.01 829 kg/s which is close to the NATCON-calculated value of 0.01834 kg/s.

Question 36

36. Table 4-28. Define the parameter "margin to incipient boiling."

PUR-1 SAR Appendix 2-16 PuR-SARAppedix

-16Rev 2, July 23, 2015

Response

The margin to incipient boiling shown in Table 4-28 was calculated at the nominal operating power of PUR-1 (i.e., 1 kW), and it is the smallest value of the temperature difference (ToNg -

Tw) over the coolant channel length in the hottest channel where Tw is cladding surface temperature with all hot channel factors applied, and TONB is the local onset-of-nucleate-boiling temperature. This basically gives an idea of how far below the onset of nucleate boiling condition the reactor is operating. This definition can be written as an equation as follows:

where T(z) = Bulk coolant temperature at axial position z in the channel heated by the plate power of PopFr EQ/N and applying the global hot channel factors for flow and Nusselt number of Fw and Fh Twani(Z) = Cladding surface temperature at axial position z in the channel heated by a plate power of Pop~r EQ/N and applying the global hot channel factors for flow and Nusselt number of Fw and Fh q"(z) = Heat flux at position z for the plate power of Pop~r EQ/N and applying the global hot channel factors for flow and Nusselt number of Fw and Fh p(z) = Absolute pressure in the channel at axial position z T~nop(p(z), q"(z)Fnux) = Onset of nucleate boiling temperature at absolute pressure p(z) and heat flux q"(z)Fflux Pop = Operating power of the reactor (e.g., 1 kW for PUR-1)

N = Number of fuel plates in the core (e.g., 190 for PUR-1 LEU core)

To = Coolant temperature at the channel inlet Fr = RPEAK = Radial power factor of the plate cooled by the channel Fw = Hot channel factor for flow in the channel EQ = Hot channel factor for reactor power Fh =Hot channel factor for Nusselt number Fflrn = FFILM = Hot channel factor for temperature drop across the coolant film on cladding surface EFlux - FFLUX = Hot channel factor for heat flux FbuIk = FBULK = Hot channel factor for bulk coolant temperature rise in the channel PUR-1 SAR Appendix 2-17 PUR-SARAppedix

-17Rev 2, July 23, 2015

APPENDIX 3: FUEL SPECIFICATIONS Pages Appendix 3-2 through Appendix 3-62 are the specification document Specification for Purdue University Standard and Control Fuel Elements - Assembled for the Purdue University Reactor, idaho NationalLaboratory, SPC-382, Rev 1, January 27, 2007..

Pages Appendix 3-63 through Appendix 3-84 are engineering drawings of the PUR-1 fuei assemblies.

PUR-1 SAR Appendix 3-1 PuR-SARAppndix3-1Rev 2, July 23, 2015

Document ID: SPC-382 Revision ID: I Effective Date: 01/24/07 Specification Specification for Purdue University Standard and Control Fuel Elements -

Assem bled for the Purdue University Reactor The INL is a U.S. Department of Energy National Laboratory operated by Battelle Energy Alliance.

Idaho National Laboratory PUR-1 SAR Appendix 3-2 FUR-SARAppndix3-2Rev

2. July 23, 2015

INTENTIONALLY BLANK PUR-1 SAR Appendix 3-3 PUR-SARAppndix3-3Rev

2. July 23, 2015

Form 412.09 CRe'. 09)

.F.'* *dhl*AO:PRDEUIEST Idenifir:IPCa82r U- OR*VE*[IDN PUNRDUE FUNIERITY00 Ideniie.r: ENGIE-RNG N

U SI IMWDCNRLFESHO

  • ELEMENTS - ASSEMBLED FOR THE Effective Date:

NIERN 01/24/07 Page: i of ii PURDUE UNIVERSITY REACTOR .

Document Project File No. Revision

1. Identifier: SPC-382 2. (optional): ________3. No.: 1 Specification for Purdue University Standard and Control Fuel Elements - Assembled for the
4. Document Title: Purdue University Reactor Comments
5. : .All review and approval signatures for this specification are located on DAR Number 511249.
  • SIGNATURES. ......... ii ,:
6. 7.i 8.

Type or Printed Name JSignature Organization!

Signature I Code Date Discipline See DAR Number 506184.

See DAR Number 511249.

Document Control Release / . -. *

9. Signature: 7*f **Date: ]' LE. o07
10. Is this a Construction Specification? Yes [] No [] 11. NCR Related? Yes Lii No []

Does document contain sensitive, unclassified information? [] Yes [] No If Yes, what

12. category: __________
13. Can document be externally distributed? Yes [] No Li Area Index
14. Code: Area______ Type______ SSC ID)

Review annually. Cutoff when Record superseded, obsolete or Uniform File Disposition Retention cancelled. Destroy 75 years

15. Code: 0250 16. Authority: ENVl-b-4-a Period: after cutoff.
17. For QA Records Classification Only: Lifetime [-i, Nonpermanent LI-, Permanent LI Item or activity to which the QA Records apply: _____________________________

Periodic Review Frequency: N/A Li, 5 years [], or

18. Other___________________ ____

Nuclear Engineering Building [] 400 Central Drive ta West Lafayette, IN 47907-2017 PUR-I SAR (765) 494-5739 m Fax: (765) 494-9570 [] https:/lengineerin~dplj.N4E Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Ida ho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: ii of ii PURDUE UNIVERSITY REACTOR INTENTIONALLY BLANK PUR-1 SAR Appendix 3-5 PUR-SARAppndix3-5Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 1 of 57 PURDUE UNIVERSITY REACTOR

[Purdue University Reactor [Specification [ DAR Number: 511249 [

REVISION LOG Rev. Date Affected Pages Revision Description 0 05/31/06 All New Document.

1 0 1/24/07 All Revised to add Program Anneal requirements and

_____ ________ ____________update Drawing Titles 1 4

-I- + I I- 4 F + I.

I. + I-PUR-1 SAR Appendix 3-6 FUR-SARAppndix3-6Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 2 of 57 PURDUE UNIVERSITY REACTOR CONTENTS

1.

SUMMARY

............................................................................................... 5 1.1 General .............................................................................................. 5

2. APPLICABLE CODES, PROCEDURES, AND REFERENCES...................................... 5 2.1 Standards, Specifications, Drawings and Attachments.......................................... 5 2.1.1 Specifications and Standards ......................................................... 5 2.1.2 Drawings (INL)........................................................................ 8
3. TECHNICAL REQUIREMENTS.......................................................................... 9 3.1 Production Qualification.................. ......................................................... 9 3.1.1 Fuel Plate Qualification: .............................................................. 9 3.1.2 Fuel Element Qualification:......................................................... 10

3.1.3 Requalification

...................................................................... 10 3.1.4 Operator Qualification:........................................... 11 3.2 Materials ........................................................................................... 12 3.2.1 Fuel Bearing Plates .................................................................. 12 3.2.2 Aluminum Weld Filler Metal: ...................................................... 12 3.2.3 Dummy (Non-Fueled) Plate:........................................................ 12 3.2.4 Material Requirements .............................................................. 13 3.3 Mechanical Requirements........................................................................ 13 3.3.1 Fuel Plate Requirements ............................................................ 13 3.3.2 Non-fueled (dummy) plates:........................................................ 15 3.3.3 Fuel Element Requirements......................................................... 15 3.4 Physical Properties................................................................................ 15 3.4.1 Fuel Plate Requirements ............................................................ 15 3.5 Surface Condition ................................................................................. 17 3.5.1 Surface Defects ...................................................................... 17

3.5.2 Cleanliness

.......................................................................... 17

3.5.3 Contamination

....................................................................... 18 3.6 Marking............................................................................................ 18 3.6.1 Fuel Plate Identification: ............................................................ 18 3.6.2 Fuel Assembly Identification:....................................................... 18 3.6.3 Dummy Element Identification: .................................................... 19 3.7 Storage ............................................................................................. 19 3.8 Fuel Element Surface Treatment ................................................................ 19 PUR-1 SAR Appendix 3-7 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 3 of 57 PURDUE UNIVERSITY REACTOR 3.8.1............................................................................................ 19 3.8.2............................................................................................ 20 3.8.3............................................................................................ 20 3.9 Graphite Reflectors and Graphite Radiation Baskets .......................................... 20

3.9.1 Material

.............................................................................. 20 3.9.2 Assembly:............................................................................. 20

3.9.3 Welding

.............................................................................. 20

3.9.4 Identification

........................................................................ 20 3.9.5 Dimensional Inspection:............................................................. 21 3.9.6 Surface Finish and Defects: ......................................................... 21

3.9.7 Storage

............................................................................... 21

4. QUALITY ASSURANCE................................................................................. 21 4.1 Materials ........................................................................................... 22 4.2 Core Density....................................................................................... 22 4.3 Fuel Loading....................................................................................... 24 4.4 Fuel Homogeneity ................................................................................ 24 4.5 Core Configuration................................................................................ 26 4.6 Bond Integrity ..................................................................................... 26 4.6.1 Blister Anneal: ....................................................................... 26 4.6.2 Ultrasonic Scanning: ................................................................ 27 4.6.3 Metallographic Examination........................................................ 27 4.7 Internal Defects ................................................................................... 27 4.8 Surface Finish and Defects....................................................................... 28 4.9 Clad-Core-Clad Dimensions..................................................................... 28 4.10 Cleanliness......................................................................................... 29 4.11 Contamination..................................................................................... 29 4.12 Dimensional ....................................................................................... 29 4.12.1 Final Dimensional Inspection....................................................... 29 4.13 Reactor Components and Spare Fuel Element Parts........................................... 29
5. PACKAGING AND SHIPPING.......................................................................... 30
6. NOTES ...................................................................................................... 30 PUR-1 SAR Appendix 3-8 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY !Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 4 of 57 PURDUE UNIVERSITY REACTOR 6.1 Definitions......................................................................................... 30 6.2 Purchaser Tests.................................................................................... 33 6.3 Submittals.......................................................................................... 33 6.3.1 Preproduction:........................................................................ 33 6.3.2 Pre-repair:............................................................................. 34 6.3.3 Manufacturing Schedule: ........................................................... 34 6.3.4 Delivery Submittals: ................................................................. 34 6.3.5 Fuel Plate Radiographs:............................................................. 35 6.3.6 Core Compact Data Sheets: ......................................................... 35 6.3.7 Report of Production by Unapproved Process:.................................... 35 APPENDIX A ...................................................................................................... 37 APPENDIX B...................................................................................................... 39 FIGURES

1. Purdue University Fuel Plate Sampling Procedures For Destructive Tests....................... 36 PUR-1 SAR Appendix 3-9 PUR-SARAppndix3-9Rev
2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 5 of 57 PURDUE UNIVERSITY REACTOR 1.

SUMMARY

1.1 General This specification (see def.) defines the materials, components, testing, inspection, certain processes, quality control (see def.) requirements and acceptance criteria for the fabrication of standard and controlfuel elements (see def.) and fuel element containers for the Purdue University Reactor at Purdue University at West Lafayette, Indiana.

2. APPLICABLE CODES, PROCEDURES, AND REFERENCES 2.1 Standards, Specifications, Drawings and Attachments The applicable portions of the following documents as defined herein, form a part of this specification. Where there is a conflict between the documents cited and the latest revision thereof, the supplier (see def.) shall notify the purchaser (see def.) of the conflict and use the latest revision in effect at the signing of the contract, unless otherwise directed by the purchaser.

2.1 .1 Specifications and Standards National Codes and Standards ASTM E 1742-00 Standard Practice for Radiograph Examination ASTM E 1417-99 Standard Practice for Liquid Penetrant Examination MIL-C-45 662 Calibration System Requirements RDT F6-2T Welding of Reactor Core Components, Sections 1,2,3 and 6 American Society for Testing and Materials (ASTM)

ASTM B 209-00 Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate ASTM B 210-04 Aluminum and Aluminum-Alloy Drawn Seamless Tubes ASTM B 211-00 Standard Specification for Aluminum and Aluminum-Alloy Bar, Rod and Wire ASTM B 214-99 Standard Test Method for Sieve Analysis of Granular Metal Powders ASTM B 221-00 Standard Specification for Aluminum PUR-1 SAR SAR ~~~Appendix PUR-1 3-10 2 uy2,21

2. July 23,2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 6 of 5 PURDUE UNIVERSITY REACTOR and Aluminum-Alloy Extruded Bars, Rods, Wires, Profiles and Tubes ASTM B 24 1-02 Aluminum and Aluminum-Alloy Seamless Pipe and Seamless Extruded Tube ASTM E 8-00 Methods of Tension Testing of Metallic Materials ASTM E 29-93 a (1999) Recommended Practice for Indicating Which Places of Figures are to be Considered Significant in Specified Limiting Values ASTM E 2016-99 Standard Specification for Industrial Woven Wire Cloth American Welding Society (AWS')

AWS A5.10-1995 Aluminum and Aluminum Alloy Welding Rod and Bare Electrodes American National Standards Institute (ANSI)

ANSI B46.1-1994 Surface Texture ANSI Y14.5-1994 Dimensioning and Tolerancing for Engineering Drawings American Society of Mechanical Engineers (ASME)

ASME Section V - 2001, Boiler and Pressure Vessel Code without addendum Section V ASME Section IX - 2001 Boiler and Pressure Vessel Code Section IX ASME NQA- 1-1997 Quality Assurance Requirements for Nuclear Facility Applications PUR-1 SAR ~~~Appendix PUR-1 SAR 3-11 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 7 of 5 PURDUE UNIVERSITY REACTOR Idaho National Laboratory (INL)

TRTR- 11 Specification for Low Enriched Uranium Metal in Test Reactor Fuel TRTR- 14 Specification for Reactor Grade Low Enriched Uranium Silicide Fuel Powder IN-F-4-TRA Specification for Aluminum Powder for Matrix Material in Test Reactor Fuel STD 7022A Cleanliness Acceptance Levels for Nuclear or Non-Nuclear Service Components American Society for Nondestructive Test (ASNT)

SNT-TC-lA (1996 or later) American Society For Nondestructive Testing (ASNT) Recommended Practice PUR-1 SAR SAR ~~~Appendix PUR-1 3-12 2 uy2,21

2. July 23,2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 8 of 57 PURDUE UNIVERSITY REACTOR 2.1.2 Drawings (JNL) 635454 Purdue University Test Research and Training Reactor Graphite Reflector Assembly and Source Drive Assembly 635455 Purdue University Test Research and Training Reactor Standard Fuel, Partial,

& Dummy Element Assemblies 635456 Purdue University Test Research and Training Reactor Control Fuel Element Assembly and Dummy Control Fuel Element Assembly 635457 Purdue University Test Research and Training Reactor Fission Chamber Fuel Element Assembly 635458 Purdue University Test Research and Training Reactor Standard Fuel Container Assembly 635459 Purdue University Test Research and Training Reactor Control Fuel Container Assembly 635460 Purdue University Test Research and Training Reactor Irradiation Facility Assembly 635461 Purdue University Test Research and.

Training Reactor Capsule Holder and Capsule Insert Assemblies and Details 635462 Purdue University Test Research and Training Reactor Graphite Container Assembly, and Source Drive Container Assembly 635463 Purdue University Test Research and Training Reactor Fuel Plate Assembly and Dummy Fuel Plate Detail 635464 Purdue University Test Research and Training Reactor Container Tube Assembly and Details 635465 Purdue University Test Research and PUR-1 SAR SAR ~~~Appendix PUR-1 3-13 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1of5 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 9of5 PURDUE UNIVERSITY REACTOR Training Reactor Graphite Block Detail And Graphite Capsule Holder Detail 635466 Purdue University Test Research and Training Reactor Miscellaneous Details 635467 Purdue University Test Research and Training Reactor Source Drive Nozzle Assembly and Source Drive Top 635468 Purdue University Test Research and Training Reactor Nozzle Preliminary Machined and Fission Chamber Top

3. TECHNICAL REQUIREMENTS 3.1 Production Qualification The supplier is required to qualify the processes or portions of the process or be exempt from same by written approval of the purchaser. In qualifcation (see def.), only materials that comply with this specification shall be used.

Qualification processes, equipment, and operator qualificationltraining programs shall be identical to those used during production (see def.). To qualify, the supplier must demonstrate, to the satisfaction of the purchaser, that the process is capable of producing a product, which satisfies all the requirements of the specifications. Assembly of production fuel elements shall not be initiated until:

(1) all required data, to assure compliance with the qualification requirements, has been submitted to the purchaser; (2) data and records required by Section 6.3 have been submitted; and (3) written approval of qualification has been received by the supplier from the purchaser.

3.1.1 Fuel Plate Qualification:

Fuelplate (see def.) qualification shall be satisfied by supplier production of a minimum of two consecutively produced plate lots (see def.), in lot quantities of 24 plates (see def.). The plates shall be made using low enriched uranium in the form of Silicide (see def.) powder, which have a yield of no less than 65% acceptable fuel plates meeting all applicable requirements of this specification. The supplier may combine the results of two consecutive lots into a production run in determining the 65% yield requirement provided that there have been no changes in the manufacturing (see def.) procedure (see def.) between lots which would require requalifcation(see def.) in accordance with Section 3.1.3.

PUR-1 SAR ~~~Appendix PUR-1 SAR 3-14 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 10of5 PURDUE UNIVERSITY REACTOR In the event that fuel plate qualification has been performed by the supplier meeting all the requirements of this specification during the past twelve months, and qualified operators are performing the fabrication, fuel plate qualification requirements listed above will be waived.

Fuel plates made in development (see def.) (prior to and including qualification runs that fail to meet the 65% yield requirements) will not be used in fabricating production fuel elements without prior approval of the purchaser.

3.1.2 Fuel Element Qualification:

The supplier shall fabricate 1 dummy standardfuel element assembly (see def.), which shall meet the requirements of this specification.

3.1.3 Requalification

The supplier shall notify the purchaser of any proposed process change.

A changed process may not be used in production until the supplier has met all the requirements of Section 3.1.3, submits the results and data of the requalification effort, and receives written approval from the purchaser.

Requalification for any fuel plate attribute to the requirements of the specification will be required when the processes, materials, fuel loadings, equipment or equipment operators (welding and rolling) which have been previously qualified are changed, unless the supplier can demonstrate to the satisfaction of the purchaser by engineering explanation or proof test that such changes will have no detrimental effect on the product.

Requalification for compacting, pack (see def.) assembly, and rolling mill operators can be less than qualification basis, since the procedure has already been established. Candidate operators who are not qualified for compacting operations, pack assembly operations, and hot/cold rolling mill operations must demonstrate their abilities in performing the individual operations they are assigned.

An operator must qualify by processing two lots of fuel plates with minimum lot size of 24, for the operation he is assigned to qualify, before performing any production operation independently. Each lot of fuel plates shall be processed through final inspection, with a minimum yield rate of 90% acceptable fuel plates required for the operator to be termed qualified.

PUR-1 SAR SAR ~~~Appendix PUR-1 3-15 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 11of5 PURDUE UNIVERSITY REACTOR NOTE: Failure of an operatorto qualify', because offuel piate deviations, must be based on deviations related to the operation being qualified.

The purchaser on a case-by-case basis will determine the quantities and sizes of requali~ficationfuel plates selected to be destructively examined.

3.1.4 Operator Qualification:

Operator qualification will be accomplished via an approved supplier internal qualification program for the following operations:

A. Arc melting B. Compacting C. Pack assembly D. Hot rolling B. Cold rolling F. Final machining.

3.1.4.1 In addition to the operations specified above, the supplier shall also show evidence of the training and competency of those individuals who perform any of the following fuel element fabrication and inspection activities:

A. Powder sieving, weighing, and testing B. Compact weighing, visual and dimensional inspection C. Fuel plate/element and component cleaning D. Fuel plate annealing operations B. Dimensional inspection of plates, elements, and subcomponents F. Metallographic sample preparation and inspection

0. Visual inspection of plates, elements, and subcomponents H. Void volume inspection I. Fluoroscope inspection of fuel plates PUR-1 SAR ~~~Appendix PUR-1 SAR 3-16 2 uy2,21
2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 12 of 57 PURDUE UNIVERSITY REACTOR J. Radiography and inspection of fuel plate radiographs K. Ultrasonic testing and interpretation.

The individuals performing these operations shall have specific requirements imposed on them that will demonstrate their knowledge and ability to perform their respective assignments. Documented evidence of the training of these individuals shall be maintained and shall be made available to the purchaser upon request.

3.2 Materials The material requirements for the components comprising the fuel element are as specified on Drawings per Section 2.1.2 and requirements of this section.

3.2.1 Fuel Bearin2 Plates 3.2.1.1 Fuel Cores: The fuel cores (see def.) of the fuel plates shall be uranium silicide powder dispersed in aluminum alloy powder which meet the requirements of IN.-F-4-TRA and TRTR- 14, per Section 2.1.1 of this specification.

3.2.1.2 Frames and Covers: Aluminum for the frames and cover plates shall conform to ASTM B209, Alloy 606 1-0. The aluminum plate stock used for frame and cover plates shall be certified by the supplier to contain less than 30 PPM boron, 80 PPM cadmium, and 80 PPM lithium.

The subcontractor shall furnish certified physical properties and chemical analyses of ingots or plates of the 6061 materials to INL.

3.2.2 Aluminum Weld Filler Metal:

All aluminum weld filler metal shall be ER4043 as required by Specification AWS A5.10-1995.

3.2.3 Dummy (Non-Fueled) Plate:

Dummy (non-fueled) plates (see def.) shall be fabricated from aluminum Type 6061-0, that meets the requirements of Section 3.2.1.2.

PUR-1 SAR SAR ~~~Appendix PUR-1 3-17 2 uy2,21

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSuRU UIEST-ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 13 of 57 3.2.4 Material Reqiuirements All material used or contained in the product shall comply with all the requirements of this specification and Drawings per Section 2.1.2 unless exempted by written document by the purchaser.

3.3 Mechanical Requirements 3.3.1 Fuel Plate Requirements 3.3.1.1 Fabrication: The supplier shall furnish the details of his fuel plate rolling schedule and component cleaning process to the purchaser for approval prior to use in production per 6.3.1.

Compacting details shall include silicide - aluminum compacting pressure and compacting press dwell time.

After hot rolling, each fuel plate shall be blister annealed per Section 4.6.1 and then cold rolled to final thickness at room temperature. After cold rolling operation, the fuel plates shall be subjected to program annealing. The rolling schedule shall contain, at a minimum, the following:

A. Nominal plate reduction B. Minimum number of hot roll passes C. Nominal inter-pass reduction and target thickness D. Hot rolling furnace temperature E. Preheat time for all hot roll passes F. Final hot roll plate thickness G. Type and frequency of roll lubricant utilized H. Nominal cold roll reduction.

I. Final cold roll thickness.

Fuel plate cladding (see def.) thickness required by Section 3.3.1.4 and fuel core homogeneity requirements of Section 4.4 are independent requirements that must be met.

PUR-I SAR Appendix 3-18 PUR-SARAppedix July -152.

23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 14 of 57 PURDUE UNIVERSITY REACTOR 3.3.1.2 Core Configuration: No fuel particles are allowed within the fuel free zones located at the ends of the plates as shown on Drawing 635463.

The nominally unfueled area of each fuel plate as defined by Drawing 635463 may contain random fuel particles defined as flaking and limited in size, location, and spacing per this Section, as determined by Section 4.5.

The presence of fuel particles detected between the maximum fuel core outline and fuel plate edges and ends is allowed provided they do not violate the following restrictions:

- One or more fuel particles, which fit in a rectangle whose area is not more than 4x1 0-4 in2 is acceptable AND

- The fuel particle(s) are no closer than 0.080 in. to any other particle edge to edge AND

- No particle is closer to the plate edge or end than the major dimension of the particle.

Stray fuel particles (see def.) that violate the above requirements may be removed from fuel plate edges by filing, provided the following:

- The filed out area is no deeper into the edge of the plate than 0.050 in., no longer than 0.250 in.

AND Each filed area is at least 1.0 in. apart Filing of fuel plate ends, for the removal of stray particles, is not allowed, unless previously approved by the purchaser.

3.3.1.3 Internal Defects and Bond Integrity: Metallurgical bond, as determined by Section 4.6 is required at interface areas of the finished fuel plates, specifically fuel core-to-clad and clad-to-frame. The presence of grain growth across the fuel PUR-1 SAR SAR ~~~Appendix PUR-1 3-19 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 15 of 57 PURDUE UNIVERSITY REACTOR matrix-cladding interface and across the aluminum frame-cladding interface of at least 50% is required. Fuel core defects in excess of 0.06 in. in any dimension as determined by Section 4.7 are not allowed.

3.3.1.4 Cladding Thickness: During production, all plates will be subjected to UT mmn-clad inspection. The standard will be calibrated at the nominal 0.008-inch scan depth. The gage will then be adjusted to a 0.010 inch scanning depth and the fuel plates will be scanned at 0.0 10 inch. Fuel plate UT traces, which display mmi-clad indications at the 0.010-inch depth, shall be visually compared with the 0.008-inch Standard trace. Fuel plates for which the UT reports show a comparable density of indications, or worse, than the indications displayed on the standard UT report are unacceptable. Fuel plates, which fail the 0.010-inch UT scan, shall be rescanned at 0.008 inch. Only fuel plates which are acceptable when rescanned at 0.008 inch shall be submitted to the Purchaser and User for evaluation.

3.3.2 Non-fueled (dummy) plates:

The supplier shall use a cold rolling method to obtain plate thickness.

Non-fueled (dummy) plates shall be subjected to program anneal.

3.3.3 Fuel Element Reqiuirements 3.3.3.1 Weldinp: All welding shall be performed using procedures and welding personnel qualified in accordance with ASME Section IX or the criteria defined in Appendix B. Quality acceptance of production welds shall be in accordance with Appendix B, Section 5.

3.4 Physical Properties Fuel plates shall have a core of U3 Si2 and aluminum and completed fuel plates and fuel elements shall have fuel loadings per Sections 3.4.1.2, and 3.4.1.5.

3.4.1 Fuel Plate Requirements 3.4.1.1 Fuel Core: The fuel core shall consist of 19.75 "0.2 weight

% enriched uranium silicide powder dispersed in aluminum powder. The uranium silicide powder shall be -100, +325 U.S. standard mesh particles. However, a blend may PUR-1 SAR SAR ~~~Appendix PUR-1 3-20 22. July uy2,21 23,2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 16 of 57 PURDUE UNIVERSITY REACTOR contain up to 35 weight percent of -325 U.S. standard mesh particles. Any powder particles greater than 100 mesh particles shall be reground such that they will go thru the 100 mesh sieve. The fuel core shall be fabricated according to standard powder-metallurgical and roll-bonding techniques. The supplier shall provide to the purchaser, a written procedure for pack assembly and the initial rolling step which describes the method used to prevent excessive oxidation that causes non-bond of fuel core to the cladding.

3.4.1.2 Fuel Loading: By using the approved supplier's method of assigning U-23 5 content, per a detailed description as to the weighing procedure by which the supplier proposes to assign fuel plate U-235 content. Each fuel plate shall contain 12.5 "0.35 grams U-235. The weight of each core shall be measured and recorded to within 0.01 gram U-235 based upon weight of the final compact and chemical and isotopic analysis of the constituents.

3.4.1.3 Fuel Homogeneity: Fuel homogeneity requirements are located in section 4.4.

3.4.1.4 Void Volume: In the qualification process, all fuel plates shall be inspected for void volume using the method described in Section 4.2. The percent voids in the fuel cores of all fuel plates shall be determined by the inspection procedure developed by the supplier. The percent voids in the fuel cores shall be at least 3.0% and not more than 11.0%.

3.4.1.5 Fuel Element Requirements 3.4.1.6 Fuel Loading: Assigned fuel loading for each fuel element shall be 175.006-4.90 grams of U-235. Each Control Fuel Element shall contain 100 *2.80 grams of U-235. Control limits for the method used to measure this weight are established at the 95% confidence level for a significant population of measurements of a particular standard. The U-235 enrichment shall be 19.75 '-0.2 weight % of total uranium per specification TRTR- 11.

PUR-1 SAR PUR-1 SAR ~~Appendix 3-212.Jl3,01 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 17of5 PURDUE UNIVERSITY REACTOR 3.5 Surface Condition Fuel plates and completed fuel elements must comply with the surface condition requirements of Section 3.5.1, 3.5.2, and 3.5.3 and drawings of Section 2.1.2, per ANSI B46. 1. Sanding, or any other finishing procedure that will smear the aluminum surface, will not be allowed on fuel plates unless approved by the purchaser.

3.5.1 Surface Defects 3.5.1.1 Compliance with surface finish and defect requirements shall be established by 100% visual inspection of all fuel plates and elements. The surface of the finished fuel plates shall be smooth and free of gouges, scratches, pits, or removal of metal in excess of 0.005 inch in depth. Dents in the fuel plate shall not exceed 0.0 12 inch in depth or 0.25 inch in diameter. If there is evidence of dogboning in the plates, surface defects in the dogbone (see def.) area shall not exceed 0.003 inch in depth. No degradation of the fuel plates beyond these limits shall be permitted.

3.5.1.2 Fuel Plates shall be free of stringiness, scabs, or cracks.

Surface finish shall be as required by Drawing 635463.

Compliance with requirements of this section shall be accomplished by visual inspection of all fuel plates and fuel elements.

3.5.1.3 Defects on fuel plate edges or ends are permissible provided they are evaluated and acceptable to the requirements of Paragraph 3.3.1.2.

3.5.1.4 Compliance with surface finish and defect requirements shall be established by 100% visual inspection of all fuel element containers. Fuel element containers shall be free of surface defects such as pits, dents, or scratches in excess of 0.0 10 inch in depth and 0.12 inch in diameter or equivalent area.

3.5.2 Cleanliness

The suppliers fabrication, assembly, and storage areas used for the production of Purdue University fuel elements and/or components shall conform to the requirements of "controlledwork area" (see def.) as defined in Paragraph 1.3.6 of INL Standard 7022A. Cleanliness shall be PUR-1 SAR ~~~Appendix PUR-1 SAR 3-22 22. July uy2,21 23, 2015

Form 4l2.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 18 of 57 PURDUE UNIVERSITY REACTOR in compliance with INL Standard 7022A, Paragraphs 1.1, 1.2.3, 3.1, 3.2-b, d, i, 3.3 - d, e, 4.1.3, 4.2, and 4.3. Freon shall not be used to clean fuel elements or components.

As determined by Section 4.10 of this specification, there shall be no foreign materials on the finished fuel plates or surfaces of the finished fuel elements. All oil, metal chips, turnings, dusts, abrasives and spatter, scale, and other particles shall be removed from the fuel surfaces by procedures which assure that the minimum cladding thickness has not been violated. All components shall be cleaned by a method approved by the purchaser.

3.5.3 Contamination

The surfaces of each fuel plate shall be counted or smeared and counted for alpha-beta-gamma contamination. The alpha count shall be less than five dpm per 100 cm 2, and the beta-gamma count shall be less than 200 dpm per 100 cm2.

Each fuel element shall be smeared and counted for radioactive contamination. The alpha count shall be less than five dpm per 100 cm 2 ,

and the beta-gamma count shall be less than 200 dpm per 100 cm2 3.6 Marking NOTE: All/fuel plates, fuel assemblies, andfuel element containers will be markedper this section.

3.6.1 Fuel Plate Identification:

Each finished fuel plate shall be identified, as shown on Drawing 635463, by a combination of numbers and/or letters that will maintain positive identification relative to the complete traceability to the supplier fabrication history, including the basic material lots, heat or metal, manufacturing cycle, and quality control phases. The identification number shall be stamped, etched or vibro-peened at the location specified by Drawing 635463. The depth of the identification characters shall not exceed 0.010 in.

3.6.2 Fuel Assembly Identification:

r Each fuel assembly shall have an identifying number such as 07-XX (07 signifying year of fabrication). The number shall be placed on the container assembly as shown on Drawings 635455, 635456 and 635457.

PUR-I EAR SAR~~~Appendix PUR-l 3-23 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 19 of 57 PURDUE UNIVERSITY REACTOR The identification shall be stamped or entered by a method approved by the purchaser, with two inch block characters not in excess of 0.010 inches in depth. Standard assemblies should be labeled: E2, F2, G2, H2, F3, H3, E4, F4, G4, H4, F5, H5. Control assemblies should be labeled: E3, G3, and E5. The fission chamber assembly should be labeled as G5. The source assembly shall be labeled as C3. The spare Standard Assemblies should be labeled: SP-1, SP-2, SP-3. The spare Control Assembly should be labeled as SP-4.

3.6.3 Dummy Element Identification:

The dummy standard fuel element assembly shall have the identifyring number DUM-1. The number shall be placed on the container assembly as shown on Drawing 635455. The identification shall be stamped or entered by a method approved by the purchaser, with two inch block characters not in excess of 0.010 inches in depth.

3.7 Storage All fuel plates, fuel assemblies, and fuel element containers that have received final cleaning per Section 3.5.2 shall be protected in clean polyethylene containers or other containers approved by the purchaser while (1) awaiting final assembly, (2) being transferred into or being maintained in storage, or (3) being prepared for packaging or shipment. Any material exposed to contamination shall be reinspected to the requirements of Section 3.5.

3.8 Fuel Element Surface Treatment If boehnmite treatment is required during fuel element fabrication, the following shall apply. After fuel elements are assembled and inspected they shall be subjected to an environment that will cause an evenly distributed boehmite layer of 0.00006 to 0.0003 in. thickness (averaged over the surface using eddy current instrumentation) to form on all surfaces of the entire assembly. The treatment process shall be performed under controlled conditions, which shall require the supplier to maintain a record of the thermal history of the autoclave. The records shall include heat charts of recorded time and temperature. Documented evidence of the controls placed on the autoclave shall be maintained by the supplier.

3.8.1 After the boehmite process has been qualified, one fuel element from every 2n autoclave run shall be inspected following a procedure approved by the Purchaser.

PUR-1 SAR SAR ~~~Appendix PUR-1 3-24 22. July uy2,21 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 20of5 PURDUE UNIVERSITY REACTOR 3.8.2 Each fuel element shall have a corresponding aluminum plate coupon, made from fuel plate end crops, placed near the fuel element during the boehmite formation process. The aluminum plate coupon shall be subjected to the same environment as the fuel elements and each coupon measured for boehmite thickness.

3.8.3 Fuel elements and aluminum plate coupons subjected to the boehmite formation process must be carefully handled to preclude scratches, dents, and gouges that would cause removal of boehmite.

3.9 Graphite Reflectors and Graphite Radiation Baskets Graphite reflector assemblies (see def.) and irradiationfacility assemblies (see def.) shall be fabricated as per requirements contained in this section and in drawings 635454, 635460, 635461, and 635465.

3.9.1 Material

All materials used shall comply with all the requirements of this specification and applicable drawings.

3.9.2 Assembly

The assembly of the graphite reflector assemblies and irradiation facility assemblies shall be as shown on the applicable drawings.

3.9.3 Welding

All welding shall be performed using procedures and welding personnel qualified in accordance with ASME Section IX or the criteria defined in Appendix B. Quality acceptance of production welds shall be in accordance with Appendix B, Section 5.

3.9.4 Identification

The graphite reflector assemblies shall have identifying numbers such as GR-X placed on the side of the assembly as shown drawing 635454.

The graphite reflector shall be labeled as follows: Dl, D2, D3, D4, D5, El, Fl, G1, Hl, I1, 12, 13, 14, and I5. The irradiation facility assemblies shall have identifying numbers such as IF-X placed on the side of the assembly as shown on drawing 635460. The irradiation facility assemblies shall be labeled as follows: D6, E6, F6, G6, H6, and 16. The identification shall be stamped or entered by a method approved by the purchaser, with two inch block not in excess of 0.0 10 inches in depth.

PUR-1 SAR SAR ~~~Appendix PUR-1 3-25 2 uy2,21

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSuRU U ASSEMBLED VEST- ECoFOR THE Effective Date: 01/24/07 Page: 21 of 57 3.9.5 Dimensional Inspection:

Verification of all external dimensions of the graphite reflector assemblies and irradiation facility assemblies shall be by 100%

inspection, in accordance with drawings 635454 and 635460. All dimensions of this specification shall apply at a temperature of 75°F+/-

5°"

3.9.6 Surface Finish and Defects:

The graphite reflector assemblies and irradiation facility assemblies shall be free of surface defects such as pits, dents, scratches in excess of 0.010 inch deep and 0.12 inch diameter or equivalent area.

3.9.7 Storage

All graphite reflector assemblies and irradiation facility assemblies shall have received final cleaning and shall be protected in clean polyethylene containers or other containers approved by the purchaser while (a) being transferred into storage, (b) being maintained in storage, or (c) being prepared for shipment or packaging.

4. QUALITY ASSURANCE The supplier shall document, implement, and maintain a quality program in compliance with ASME NQA-1-1997.

The supplier shall permit the purchaser to conduct pre-award and continuing evaluation of the Quality Program.

Personnel performing NDE examinations, specifically radiographic, ultrasonic, liquid penetrant, and visual shall be certified to American Society for Nondestructive Testing (ASNT) Number SNT-TC-1A and certification documentation shall be made available to the purchaser.

Unless otherwise specified, the supplier shall be responsible for the performance of all tests and inspections required prior to submission to the purchaser of any fuel element for acceptance. Provided, however, that the performance of such tests and inspections is in addition to, and does not limit, the right of the purchaser to conduct such other tests and inspections as the purchaser deems necessary to assure that all fuel elements are in-conformance with all requirements of this specification. Except as otherwise specified, the supplier may use for inspection purposes either his own or any commercial laboratory acceptable to the purchaser. Records of all tests and examinations shall be kept complete PUR-1 SAR PUR-1 SAR ~~Appendix 3-262.Jl3,01 2. July 23, 2015

Forn 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 22 of 57 PURDUE UNIVERSITY REACTOR and available to the purchaser. All test and measuring equipment shall be calibrated per the requirements of Standard MIL-C-45 662.

The following applies to specified limits for requirements on core density per Section 3.4.1.1 and 4.2 and all dimensional requirements of this specification. For purposes of determining conformance with this specification an observed value or a calculated value shall be rounded off to the nearest unit in the last right hand place of figures used in expressing the limiting value in accordance with the rounding-off method of the Recommended Practices for Designating Significant Places in Specified Limiting Values (ASTM E29).

The supplier shall prepare for his use and the purchaser's approval an integrated manufacturing and inspection test plan. The plan shall include all manufacturing operations, equipment and tooling used, inspection requirements and gaging used, and mandatory hold points established by the purchaser.

Any materials or fuel element components that are fabricated using equipment, personnel, or processes that are not in accordance with approvals as previously granted by the purchaser are subject to rejection (see def.). A report of any such incident must be submitted in accordance with Section 6.3.7.

Fuel element inspection for shipment or rejection will be made by the on-site purchaser's representative at the supplier's plant. Final fuel element acceptance will be made by the purchaser at the User's facility.

4.1 Materials Compliance with the material requirements of Section 3.2 shall be established by supplier certification. A "Certification of Chemical Analysis" or a certified mill test report shall be supplied to the purchaser for each lot of material used in the fabrication of fuel elements. This certificate shall give the results of the chemical analysis for the material. All fuel element materials shall be traceable.

4.2 Core Density The density of the fuel cores required in Section 3.4.1.3 shall be determined by the Archimedes principle. During qualification of the fuel plate core void density required by Section 3.4.1.3 shall be determined on all qualification fuel plates submitted. After the particular plate type has been qualified, 100% inspection for void density is not required for production lots of fuel plates. For production lots, three randomly selected fuel plates from each lot shall be inspected for void volume density. Should any one of these plates be discrepant, the entire lot must then be inspected for void volume density. If void density discrepancies appear regularly in the process, the purchaser may request 100% inspection.

PUR-1 SAR Appendix 3-27 PUR-SARAppedix

-27Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 23 of 57 PURDUE UNIVERSITY REACTOR The actual core volume shall be calculated by the following formula where:

weight units are in grams and volumes in cubic centimeters.

PAL where:

Vo immersion volume of fuel plate core Vp volume of fuel plate AL= density of aluminum used for fuel plate cladding 2.715 gins/cc Wp = weight of plate Wc = deburred weight of fuel plate core compact PUR-1 SAR Appendix 3-28 PUR-SARAppedix

-28Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-3 82 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 24 of 57 PURDUE UNIVERSITY REACTOR The theoretical core volume shall be calculated by the following formulas:

Vet --

_ **)

( WU3Si2 * + *x pA---TJ

( WA/1 where:

Vct = calculated theoretical core volume WU 3Si2 = weight of U3 Si2 powder in core Wal weight of aluminum matrix powder in core pU 3 Si 2 = density of U3 Si2 powder as measured PAl = density of aluminum powder used for core matrix

= 2.710 gms/cc The void percent in the core shall be calculated using the following formula:

V°%=v V-vCt( 10 0 00)

Vc where:

V% = percent voids in the fuel plate core 4.3 Fuel Loading Verification of the fuel loading as specified in Section 3.4.1.2 shall be in conformance to the supplier's procedure required in Section 6.3.1.

In order to determine compliance with the fuel density requirements of Section 4.4, the U-235 loading of the fuel plate, as determined in accordance with the procedures of Section 6.3.1, will be divided by the core volume (Vc) as calculated by the method described in the second paragraph of Section 4.2.

4.4 Fuel Homogeneity Fuel core homogeneity requirements shall be complied with by a one-piece radiograph of all fuel plates from each fuel plate lot and evaluation of the radiograph by calibrated densitometer measurements. Purchaser approved density standards may be used by the supplier. Fuel plates and density standards shall be PUR-1 SAR Appendix 3-29 FUR-SARAppedix

-29Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 25 of 57 PURDUE UNIVERSITY REACTOR exposed simultaneously. Fuel plate density variations shall be determined by comparison of fuel plate areas to corresponding areas of the standard.

All fuel plates shall be inspected for homogeneity. Homogeneity of the fuel plate core shall be determined by radiograph film density measurements with a densitometer having a 0.080 inch aperture.

When determining fuel core density from plate radiographs, the brighter the image on the radiograph, the more dense is the uranium and the lower the number indicated on the densitometer. The darker the image on the radiograph, the less dense is the uranium and the larger the number indicated on the densitometer. A

+30% fuel core density and a +20% fuel core density is indicated by the densitometer readings in the suspect area being 30% or 20% lower than the average densitometer readings for all core locations. A -30% or a -20% fuel core density is indicated by the densitometer readings in the suspect area being 30% or 20% higher than the average densitometer readings for all fuel core locations.

Any one-half inch diameter or greater spot in the plate fuel core area, other than the dogbone area shall not be less in fuel density than -20% of the average fuel density for all fuel core locations. To determine the low density of a one-half inch diameter area, the film is maneuvered under the densitometer in the low-density area until the highest number possible is obtained on the densitometer. This number is recorded. Then four readings are taken one-fourth inch from this spot and symmetrical around it. The average of these five readings is compared to the average densitometer readings for all fuel core locations.

If density standards are used, the average densitometer readings of all fuel core locations will be replaced by the nominal density standard and comparisons will be determined between the suspect spot on the radiograph and the -30% and

-20% standards. For the +30% and +20% homogeneity overload inspection, compare the nominal density standard to the suspect area. In this case densitometer units from nominal of the fuel plate represent the following percentages: -0.15 = +30%; -0.10 = +20%. Fuel plates exceeding these limits are discrepant.

For rectangular shaped, suspected discrepant areas that are evaluated to the one-half inch criteria, orient the four symmetrical readings such that worst case readings will be taken.

Between the minimum and maximum permissible fuel core length boundary, fuel underload condition shall not be evaluated.

Any indication of un-alloyed uranium as determined by radiography shall be cause for rejection.

PUR-1 SAR Appendix 3-30 PUR1 SR ,July Apenix

-30Rev2.

23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSuRU U ASSEMBLEDRE VEST- oFOR THE Effective Date: 01/24/07 Page: 26 of 57 Any 0.080 inch diameter spot in the fuel plate dogbone area (area within one inch of each fuel core end) shall not be greater in fuel density than +30% of the average fuel density for all core locations. Any one-half inch diameter area in the dogbone area shall not be less in fuel density than -30% of the average fuel density for all fuel core locations. The actual dogbone shall not be more than one-half inch in the longitudinal direction.

Other than the dogbone areas near ends of fuel core, any one-half inch diameter area shall not be greater in fuel density than +20% of the average fuel density for all fuel core locations. To determine the high density of a one-half inch diameter area, the film is maneuvered under the densitometer in the high-density area until the lowest number possible is obtained on the densitometer. This number is recorded. Then four readings are taken one-fourth inch from this spot and symmetrically around it. The average of these five readings is compared to the average densitometer readings for all fuel core locations.

Unless otherwise specified, purchaser approval of all radiographs is required prior to assembly of fuel plates into elements.

4.5 Core Configuration Each finish-cut flat fuel plate shall be radiographed in accordance with Appendix A and evaluated for compliance with Section 3.3.1.2.

Visual radiograph inspections will be performed without magnification on a light table having a light intensity of 450 to 600 ft-candles at the table surface and the area darkened to give a light range of 5 to 15 ft-candles 18 in. above the light table with radiograph film in place on the table.

4.6 Bond Integrity 4.6.1 Blister Anneal:

After the fuel plate has been hot rolled, it shall be heated to 900 0 F+13 0 F, held at that temperature for a period of 2 hours2.314815e-5 days <br />5.555556e-4 hours <br />3.306878e-6 weeks <br />7.61e-7 months <br />, -15 minutes, +30 minutes, removed from furnace, and allowed to air cool.

Any blisters, in the fuel core region larger than a 0.060 in. diameter or any blister in the frame region of the fuel plate larger than 0.120 in. diameter shall result in rejection of the associated fuel plate. A maximum of two blisters less than 0.060 in. diameter is allowed in the fuel core area, provided they are more than 0.25 0 in. apart. A maximum of two blisters in any of the four sides of the pictureframe (see def.)(a maximum of eight) region smaller than 0.120 in. can be tolerated providing that no blister is PUR-1 SAR Appendix 3-31 PUR-SARAppedix

-31Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 27 of 57 PURDUE UNhIVERSITY REACTOR any closer to the plate edge or end or to another blister than the major dimension of the blister and no blister is closer to the plate edge or end than 0.050 inch. When there is question as to size or location of the blisters, the acceptance or rejection of the plate shall be determined in the ultrasonic inspection of Section 4.6.2.

4.6.2 Ultrasonic Scanning:

The finished fuel plate area shall be ultrasonically inspected in compliance with ASME Boiler and Pressure Vessel Code,Section V, Article 5, Paragraphs T-ll0, T-5 10, T-520, T-521, T-522-a, b, c, e, g, i, j, k, 1,o, T-523, T-523-1, and T-534. Any indication of discontinuity in the fuel core region equivalent to that indicated by a 0.060 in. diameter standard or any indication of a discontinuity in the frame region of the fuel plate equivalent to that indicated by a 0.120 in. diameter standard shall result in rejection of the associated fuel plate. Acceptance criteria for number of blisters revealed by ultrasonic scanning are per Section 4.6.1. Any discontinuities, inside the fuel plate, other than blisters and for which acceptance criterion is not already stated, shall be described by the supplier and evaluated by the purchaser.

4.6.3 Metallo~raphic Examination.

During qualification, one fuel plate per lot selected for qualification per Section 3.1.1 will be sectioned per Figure 1, polished and etched, and examined at 50x or above for bond and clad-core-clad dimensions per the requirements of Sections 3.3.1.3 and 3.3.1.4, and Drawing 635463, respectively.

If the fuel plate fails the metallographic examination for grain growth, voids, laminations, core cracking or separation, or foreign particles or materials, then randomly selected another plate in the lot for metallographic examination. If this plate fails the examination, reject the lot.

Fuel plates selected for destruction tests may be rejected fuel plates, providing the attribute to be tested for is not affected by the cause for rejection. Reject fuel plates so used must have purchaser approval before destruct tests are performed.

4.7 Internal Defects Any internal defect in excess of the requirement of Section 3.3.1.3 in the fuel core, including voids, laminations, U3 Si2 segregation, clumping, core cracking or PUR-1 SAR Appendix 3-32 PUR-SARAppedix

-32Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 28 of 5 PURDUE UNIVERSITY REACTOR separation, or foreign particles or materials, which is identified by any measurement technique, including radiography per Section 4.4, ultrasonic scanning per Section 4.6.2, or metallography per Section 4.6.3, shall be cause for rejection of the fuel plate.

4.8 Surface Finish and Defects Compliance with requirements of Section 3.5 shall be established by visual inspection of all fuel plates and fuel elements. Out-of-specification defects shall be measured for size and depth and reported to the purchaser.

4.9 Clad-Core-Clad Dimensions Fuel Plate Qualification requirements of section 3.1.1 shall be established by ultrasonic techniques using the purchaser-supplied, min-clad inspection gage. All fuel plates will be subjected to ultrasonic mmn-clad inspection with the fuel core region scanned for each plate. Ultrasonic mmn-clad inspection shall be accomplished by calibration of the mmn-clad gage, using the Advanced Test Reactor (ATR) Standard (8E0777) scanned at the normal mode of 0.008 inches.

The mmn-clad gage will then be adjusted and the fuel plates will be scanned at a depth of 0.010 inches. Ultrasonic Test (UT) traces showing fuel at the 0.010 inch depth will be compared to the 0.008 inch standard to determine plate acceptability. If the density of indications from fuel plate exceeds the ATR standard density of indications, the plate is rejectable.

NOTE: The ATR standardis a smallpiece of an A TR fuel plate that has fuel particles near the surface. It is used on the UT mmn-clad machine to indicate mmi-clad indicationsand compare the density of these indicationsto any indicationsnotedfrom a fuel plate being inspected by UT.

During the fuel plate qualification process, compliance with the requirements of Section 3.3.1.4 shall be established by destructive analysis of one fuel plate per lot in accordance with Figure 1.

After fuel plate qualification, all production plates shall be mmi-clad ultrasonic inspected at a depth of 0.010 inches. Those plates discrepant at 0.010 inches shall be rescanned at 0.008 inches. Plates which are acceptable when re-scanned at 0.008 inches shall be submitted on Information/Change Request (Form 540.33) to the purchaser.

PUR-1 SAR Appendix 3-33 PUR1 SR 2. July Apenix

-33Rev 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laborator SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 29 of 57 PURDUE UNIVERSITY REACTOR 4.10 Cleanliness Fuel plate, fuel assembly, and fuel element container cleanliness requirements of Section 3.5.2 shall be established by visual inspection without magnification of all fuel plates, fuel assemblies, and fuel element containers.

4.11 Contamination The surfaces of each fuel plate and fuel assembly shall be counted or smeared and counted for alpha-beta-ganmma contamination and meet the requirements of Section 3.5.3.

4.12 Dimensional It shall be the supplier's responsibility to assure that fabrication is performed in accordance with all dimensions delineated in the Drawings referenced in Section 2.1.2. Noncomplying design dimensions on fuel plates, fuel assemblies, and fuel element containers (actual measurements) shall be submitted to the purchaser for review and approval. Any discrepant component shall not be used in a fuel element assembly unless approved.

The supplier is to certify to compliance with the design dimensional requirements delineated in the Drawings referenced in Section 2.1.2.

All dimensions of finished fuel plates, fuel assemblies and fuel element containers apply at 75°F+5°F.

4.12.1 Final Dimensional Inspection.

Dimensions required by this specification and drawings of Section 2.1.2 shall be inspected using a purchaser approved sample plan and recorded on an inspection sheet with "in specification" dimensions recorded by check mark, "O, or actual measurements and out of specification

dimensions recorded as actual measurements.

4.13 Reactor Components and Spare Fuel Element Parts Reactor components and spare fuel element parts not assembled into fuel element assemblies are required to be certified. The certification shall consist of material certification, fabrication verification, and supplier certificate of compliance to the specification and drawing requirements. The certification documents shall be submitted to the purchaser and user.

PUR-1 SAR Appendix 3-34 PUR-SARAppedix

-34Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 30 of 57 PURDUE UNIVERSITY REACTOR

5. PACKAGING AND SHIPPING Packaging and shipping of the fuel elements shall be performed using a Purchaser approved procedure in compliance with this section.
  • The purchaser shall provide shipping containers to protect the fuel elements from damage during shipment and which conform to the applicable requirements of the Departments of Energy and Transportation, and other regulatory agencies having jurisdiction of the shipment of radioactive materials. Re-useable shipping containers will be returned to the Supplier by the User at the Purchaser's expense.
  • The Supplier is responsible for loading the fuel elements into shipping containers in a sealed polyethylene sleeve in a cleaned dry condition and free of extraneous materials.
  • The Supplier shall take necessary precautions during pack~aging to prevent damage to the fuel elements during shipment. Each container shall be provided with a tamper-proof seal. Loading and shipping documents for the container shall be prepared in accordance with the applicable regulatory requirements.
  • The Supplier shall make arrangements for shipment to the User.
6. NOTES 6.1 Definitions For the purpose of this specification, the following terms are identified:

Batch. The amount of sulicide powder mixture which is handled as a unit or traceable to a common step.

Blended. To mix or mingle constituents of a batch.

Certification. The action of determining, verifying and attesting in writing (signed by a qualified party) to the qualifications of personnel and material.

Cladding. The aluminum covers bonded to the fuel core and the picture frame.

Control Fuel Element Assembly. An assembly consisting of the control fuel element container with eight fuel plates.

Controlled Work Area. A work area to which access of personnel, tools, and materials is limited and physically controlled. Temporary enclosures may be used where adjacent activities produce contamination which is detrimental to the job.

PUR-1 SAR Appendix 3-35 PUR1 SR Apenix July -35Rev2.

23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 31 of 57 PURDUE UNIVERSITY REACTOR Development. A determination of processes, equipment, and parameters required to produce a product in compliance with this specification.

Dogbone Area. Thickening of the fuel core usually in the last 1/2 in. of the core, which may result in clad thinning in those areas.

Dummy Fuel Element Assembly. An assembly consisting of a fuel element container with unfueled simulated dummy fuel plates.

Dummy Fuel Plate. A non-fueled plate made entirely from the aluminum material specified in this document.

Edge Clad. The distance between the edge of the fuel core and the edge of the finished fuel plate, before any stray particles are removed, in the width direction as determined by radiography of a flat fuel plate.

Failure. A condition where the fabrication process appears to be out of control or a breakdown or damage to equipment creates excessive costs and/or schedule delays.

Fuel Compact. A quantity of uranium silicide powder and aluminum powder, cold compacted by pressing into a solid block for assembly into packs for hot roll and cold roll into fuel plates. The compacts are encased in frames and cover plates to form the pack.

FuelAssembly. An assembly of fuel plates and hardware components. This includes both the standard and control fuel elements.

Fuel Core. The uranium-bearing region of each Fuel Plate.

Fuel Plate. The Fuel Core complete with aluminum frame and cladding.

Graphite Reflector Assemblies. A component consisting of a graphite container assembly with a graphite blockc inside.

In-Process Controls. Inspections and tests made during production to ensure that the manufacturing processes, equipment, and personnel are producing a product meeting specified requirements.

IrradiationFacilityAssemblies. A component consisting of a round tube attached inside a graphite container assembly with graphite blocks filling the annulus between the tube and container. Inserted within the tube is the isotope capsule assemblies.

PUR-1 SAR Appendix 3-36 PUR-SARAppedix

-36Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 32 of 57 PURDUE UNIVERSITY REACTOR Lot. A group of pieces handled as a unit or material traceable to a common processing step.

Manufacture(ing). All fabrication, assembly, test, inspection and quality control processes. Fabrication is a synonym for Manufacture.

Pack. The fuel compact, picture frame, and cover plates, assembled together for hot rolling.

Picture Frame. The window shaped aluminum frame, which holds the fuel compact.

Plates. See Fuel Plates.

Procedure. The detailed description of the series of processes during manufacture and inspection, which follow a regular definite order (not to be construed as an outline).

Production.That phase of the program, following Qualification, during which the product is in Manufacture.

Purchaser.Idaho National Laboratory (INL).

Qualification. A demonstration that the Manufacturing process, equipment and personnel can produce a Product in compliance with this Specification.

Quality Control. The sampling plans, inspections, tests and records required and used during Production to assure that the Product is in compliance with this Specification.

Rejection. Materials, parts, components, or assembly products, which will not be accepted as fulfilling the contract requirements because of noncompliance with this Specification.

Requalification. A demonstration that a single or group of manufacturing processes, equipment and personnel can produce a product in compliance with this specification after the original qualification has been completed and becomes invalid.

Silicide. Uranium metal alloyed with silicon and fabricated per the requirements of Specification TRTR-14. The word "fuel" is a synonym for Silicide.

Specification. All parts and appendixes to this document, its references, drawings, and standards, as may be modified from time to time by contractual document.

StandardFuel Element Assembly. An assembly consisting of the fuel element container with fourteen (14) fuel plates.

PUR-1 SAR Appendix 3-37 PUR-SARAppedix

-37Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 33 of 57 PURDUE UNIVERSITY REACTOR Stray Fuel Particles. Isolated fuel particles lying outside the maximum fuel core outline defined on Drawing 635463.

Supplier. The primary vendor selected by INL to manufacture the product.

User. Purdue University, at West Lafayette, Indiana.

6.2 Purchaser Tests None 6.3 Submittals The following data and records shall be supplied to the purchaser in the quantities stated. The purchaser's approval, prior to implementation, is required on those marked with an asterisk. All records and data shall be maintained by the supplier for the duration of the Purdue University fuel element contract.

The granting of approval by the purchaser of design, working drawings, specifications, requests, and other technical data submitted by the supplier under the provisions of the subcontract or specification shall not affect or relieve the supplier from such responsibility as the supplier has with respect to adequacy or correctness of the design, working drawings specifications, reports, and other technical data.

6.3.1 Preproduction

Documents requiring approval must be submitted prior to production use. The number of copies shall be as specified by the Vendor Data Schedule. These documents include:

- *A detailed description as to the weighing procedure by which the supplier proposes to assign Plate U-235 content as required in Section 4.3.

- Included in the description must be sampling, analytical, and quality control procedures; a statement as to the established accuracy and precision of the assigned fuel plate and fuel element U-23 5 content; developmental and production data in support of the accuracy and precision estimate; and data which at the 95% confidence level, shows that the method used to assign U-235 values has a bias which is less than 0.2% relative

- *A detailed description as to the manner the supplier will use to verify' the fuel Plate U-235 value as required by Section 4.3 PUR-1 SAR Appendix 3-38 FUR-SARAppedix

-38Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 34 of 57 PURDUE UNIVERSITY REACTOR

- *AlI fabrication, assembly, cleaning, surface treating, handling, and decontamination procedures (not to be construed as an outline)

  • AlI production test, inspection, and quality control procedures, including all nondestructive and destructive tests and all standards and sampling section drawings. All data from these tests, including but not limited to: radiographs, metallographic samples, ultrasonic testing traces, and qualification yield rates

- *All packaging, storage and shipping procedures

6.3.2 Pre-repair

  • All repair programs and procedures prior to use.

6.3.3 Manufacturinu Schedule:

  • A schedule using a purchaser approved technique.

6.3.3.1 Reports.

1. Biweekly qualifications phase summary status report. The first such report shall be initiated 1 month after date of contract award.
2. Three (3) copies of a monthly report detailing program~

progress against a previously submitted schedule shall be supplied by the supplier to the purchaser. Report type, format and submittal schedule shall be as agreed upon between the purchaser and supplier.

6.3.4 Delivery Submittals:

Three copies (except as noted) of the following data and records shall be sent prior to or accompany the shipments. The supplier shall maintain copies of these records for at least 10 years and until the supplier has received written approval from the purchaser for disposition or disposal:

- Certification of product compliance to the requirements of this specification to include any test data pertaining thereto

- Supplier's core compact data sheets, with individual fuel plate uranium composition data including:

- Serial number with batch (see def.) identification PUR-1 SAR Appendix 3-39 PUR-SARAppedix

-39Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSpRU UIEST-ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 35 of 57 Uranium content Fuel plate core weight U-23 5 enrichment Total quantity U-235 content Core void density data

- Individual fuel element composition data, including:

Uranium content U-235 content Serial number of each plate in the element

- Radiation count from fuel plate and fuel element exterior as required by Section 3.5.3 and 4.11. The counting period, counter, background, efficiency, and type of counter used shall be reported

- List of all applicable waivers and deviations and related fuel plates or fuel elements

- If performed, documented evidence of the performance and test results of the boehimite formation from the fuel element surface treatment per Section 3.8.

6.3.5 Fuel Plate Radiographs:

Fuel plate radiographs of all accepted fuel plates required by Sections 4.4 and 4.5 and Appendix A shall be sent to the user.

6.3.6 Core Compact Data Sheets:

Supplier's fuel core compact data sheets shall be supplied to the INL Quality Assurance Representative as they are generated.

6.3.7 Report of Production by Unapproved Process:

Whenever the supplier's previously submitted and approved process control limits are exceeded, or any material or fuel element components are fabricated using equipment, personnel, or processes which are not purchaser approved, the time, nature, description, corrective action to be taken, and proposed further corrective action shall be reported immediately by the supplier, with a written report to the purchaser to follow within 10 working days.

PUR-1 SAR Appendix 3-40 PUR-SARAppedix

-40Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 36 of 57 PURDUE UNIVERSITY REACTOR

1. T Samples. Transverse to be taken equally space along Fuel Core length.
2. L Samples. Longitudinal to be taken at centerline and to include the Dogbone Area.

Til T3 4 I J

[- I I I

+/- +

LiT I I L11LL 1 I I-I-I I Figure 1. Purdue University Fuel Plate Sampling Procedures For Destructive Tests.

PUR-1 SAR Appendix 3-41 PUR-SARAppedix

-41Rev

2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSpR E UIEST-ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 37 of 57 APPENDIX A Requirements for Radiography of Purdue University Fuel Plates

1. Scope This specification provides requirements for radiography of Purdue University reactor fuel plates, acceptable film quality and film identification.
2. Requirements A procedure must be writt en to specify the details for achieving acceptable fuel plate radiographs. The procedure must include the requirements given in this specification.

2.1 Equipment Setup The voltage shall be 100 k.v.p. with a focal spot size of 5 mm maximum. The distance between the focal point and the plate shall be at least twice the length of the plate. The focal point shall be centered laterally and longitudinally over the plate or group of plates.

2.2 Film 2.2.1 The image outline shall be clear and sharp; the film shall be free of runs, streaks, scratches, blurs, and cassette defect that will affect the area covered by the fuel plates.

2.2.2 The film density of all points of the radiograph that correspond to the fuel plate border locations outside the plate core shall provide densitometer readings between 1.5 and 2.7. Film density as read over the nominal density standards shall provide densitometer readings between 0.9 and 1.5.

2.2.3 The film shall be extreme sensitivity, extra fine grain, high contrast, double emulsion, industrial x-ray type, (Kodak type M or equal) which is acceptable to the purchaser. Development of the film shall be in accordance with the manufacturer's recommendation.

2.2.4 Film Identification Appendix A PUR-1 SAR Appendix 3-42 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 38 of 57 PURDUE UNIVERSITY REACTOR 2.2.5 A system of identification of the film shall be provided by the supplier, which shall show as a minimum:

A. Plate lot number B. Plate type and serial number C. Orientation of density standard D. Density standard identification E. Date of radiography.

Appendix A PUR-1 SARRevA2.pJuyi23,3201 PUR-1 SAN Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 39 of 57 PURDUE UNIVERSITY REACTOR APPENDIX B Welding Requirements and Qualification for Purdue University Fuel Elements

1. Scope The requirements for welding and for the evaluation of welds applicable to the Purdue University Fuel Element Container and components are established by this Appendix.

1.1 Application. This document defines requirements for the following:

1.1.1 Welding procedure qualification.

1.1.2 Performance qualification of welders, welding equipment, and special fixturing.

1.1.3 Information to be included in welding procedure specifications.

1.1.4 Application of qualified procedures to production welding.

1.1.5 Destructive testing and nondestructive examination for qualification and for production welding.

1.2 Special Limitations for Applicability. The requirements contained in this appendix are to some degree based on RDT F6-2T. Those requirements applicable to Manual, GTAW, single pass, welding of Plug Joint welds, Corner Joint welds, and Partial Penetration Butt Joint welds have been included in this appendix. The introduction of a new weld design or weld process requiring a change in these limited parameters would require an appropriate review of RDT F6-2T for requirements applicable to the new parameters.

1.3 Definitions.

Arc Strike. Any localized melting, heat affected zones, or change in the contour of the surface of the finished weld or adjacent base metal resulting from an arc or heat generated by the passage of electrical energy between the weld or base metal and a current source; such as welding electrodes, electron beams, ground clamps, high frequency arc, etc.

Automatic Welding. Welding with equipment which performs the entire welding operation without constant observation and adjustment of controls by an operator.

The equipment may or may not perform the loading and unloading of the work.

Appendix B PUR-1 SAR Appendix 3-44 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 40 of 57 PURDUE UNIVERSITY REACTOR Face of Weld. The exposed surface of a weld on the side from which welding was done.

Face Reinforcement. Reinforcement of weld at the side of the joint from which welding was done.

Heat. A single homogeneous melt of metal or alloy.

Joint Penetration.The minimum depth a groove or flange weld extends from its face into a joint, exclusive of reinforcement.

Machine Welding. Welding with equipment which performs the welding operations under the constant observation and control of an operator. The equipment may or may not perform the loading and unloading of the work.

Position of Welding. The terms related to positions of welding for joint types and welding processes and the position limits are defined in Section IX, ASME Boiler and Pressure Vessel Code.

Repair. The process of restoring a nonconforming item characteristic to an acceptable condition, although it does not conform to a specified requirement.

Rework. The process by which a nonconforming item is made to conform to specified requirements.

Root of a Joint. That portion of a joint to be welded where the members approach closest to each other. In cross section the root of the joint may be a point, a line or an area.

Root of a Weld. The points, as shown in cross section, at which the back of the weld intersects the base metal surfaces.

Root Penetration.The depth a groove weld extends into the root of a joint measured on the centerline of the root cross section.

Root Reinforcement. Reinforcement of weld at the side opposite that from which welding was done.

Root Surface. The exposed surface of a weld on the side opposite that from which welding was done.

Size of a Groove Weld. The joint penetration (depth of chamfering plus root penetration when specified).

Appendix B PUR-1 SAR Appendix 3-45 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 41of5 PURDUE UNIVERSITY REACTOR Undercut. A groove melted into the base metal adjacent to the toe or root of a weld and left unfilled by weld metal.

Underfill. A depression on the face of the weld or root surface extending below the surface of the adjacent base metal.

Welder and Welding OperatorPerformance Qualification. The tests to demonstrate a welder's or welding operator's ability to produce welds meeting prescribed standards.

Welder. One who is capable of performing a manual or semiautomatic welding operation (sometimes erroneously used to denote a welding machine).

Welding Operator. One who operates machine or automatic welding equipment.

Welding Procedure Qualification. The test to demonstrate that welds made by a specified procedure can meet prescribed standards.

Welding ProcedureSpecifcation. A written welding procedure which specifies the detailed methods and practices to be used in the production of a weldment and how they shall be carried out. A specification includes all elements of a procedure necessary to produce a satisfactory weldment. Examples of some of the elements included in a specification are: material used, preparation of base materials, preheat and postheat cleaning, assembly method and sequence, fixturing, heat treatments, joint welding procedures, preweld and postweld nondestructive examinations, repair, rework, etc.

Welding Procedure.The detailed methods and practices including all joint welding procedures.

2. Reference Document The following documents are a part of this appendix to the extent specified herein. The issue of a document in effect on the date of the invitation to bid, including any amendments also in effect on that date, shall apply unless otherwise specified. Where this appendix appears to conflict with the requirements of a reference document, such conflict shall be brought to the attention of the purchaser for resolution.

Appendix B PUR-1 SAR Appendix 3-46 Rev 2. July 23, 2015.

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR TILE Effective Date: 01/24/07 Page: 42 of 57 PURDUE UNIVERSITY REACTOR 2.1 American Society for Testing and Materials (ASTM) Standards 2.1.1 ASTM E2, Preparation of Micrograplis of Metals and Alloys 2.1.2 ASTM E3, Preparation of Metallographic Specimen 2.2 American Society of Mechanical Engineers (ASME) Codes 2.2.1 ASME Boiler and Pressure Vessel Code,Section IX, Welding Qualifications 2.3 American Welding Society (AWS) Standards 2.3.1 AWS A2.2, Nondestructive Testing Symbols 2.3.2 AWS A3.0, Terms and Definitions

3. Weld Qualification Requirements 3.1 General Reqiuirements Appendix B PUR-1 SARRevA2.pJuyi23,3201 PUR-1 SAR Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 43 of 57 PURDUE UNIVERSITY REACTOR 3.1.1 All welding procedures, welders, or welding machine operators shall be qualified in accordance with the provisions identified in this Appendix.

3.1.2 Weld Procedure and Performance Qualification Testing previously qualified to these requirements under other contracts may be used.

Existing records to support previously qualified procedures and personnel are subject to review by the purchaser.

3.1.3 Base materials and filler material shall comply with the requirements of the drawings.

3.1.4 Welding processes which satisfy the specified requirements and produce the quality required by this Appendix are permissible. Welding procedures which utilize fluxes and coatings shall not be used.

3.1.5 Fixtures

The capability of fixtures for aligning parts shall be demonstrated before welding of production parts is initiated. If chill bars or blocks are used, the type of material and their location with respect to the joint shall be included in the procedure specification.

3.1.6 Position of Qualification Welds. All procedure and performance qualification test welds shall be made in the same positions as for production welds.

3.1.7 Special Conditions for Qualification Welds: All procedure and performance qualification test welds shall be made under conditions which simulate the actual production welding conditions. These conditions shall include space limitations, joint accessibility, degree of comfort due to heat, position and other handicaps or environmental factors which the welder or welding operator will endure during actual production welding.

3.1.8 Heat Treatment. Weld preheat and postheat treatments shall not be used without prior approval by the purchaser.

3.1.9 Interpass Temperature. For multi-pass weld, the weld interpass temperature shall not be less than 60° F or greater than 3500 F without prior approval by the purchaser.

3.1.10 Records. Records of welding, associated processing, and inspection shall be maintained for all welds. Complete records may consist of inspection forms, routings, or reference to Operating Procedures or other documents. These records shall include at least the following:

Appendix B Appendix 3-48 Rev 2. July 23, 2015 PUR-1 SAR

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 44 of 57 PURDUE UNIVERSITY REACTOR

1. Base Material (Type, material specification, heat or lot number).
2. Filler Material (Type, material specification, heat or lot number).
3. Cleaning procedures.
4. Joint identification and weld maps when applicable.
5. Welding machine type and identification.
6. Welding procedure specification.
7. Welder or welding operator qualification.
8. Procedure and performance qualification.
9. Current-voltage data for machine or automatic welding.
10. Date welds are made.
11. Inert gas mixture, when applicable.
12. Nondestructive examination procedure.
13. Nondestructive examination personnel identification.
14. Examinations and tests (nondestructive and destructive) and the results.
15. Photomacro graphs and photomicrographs.
16. Metallographic specimens.
17. If applicable, rework and repair of welds.
18. Disposition of welds.

3.2 Welding Procedure Specification 3.2.1 The welding procedure specification shall meet the requirements of this Appendix, and shall be submitted to the purchaser for information.

3.2.2 The welding procedure specification shall include all essential elements and details, as required by this section, to cover each joint to be welded by the supplier. Each joint shall be identified in the welding procedure specification. The specification shall include a joint design sketch for Appendix B SARRevA2.pJuyi23,3201 PUR-1 PUR-1 SAR Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UN~IVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 45of5 PURDUE UNIVERSITY REACTOR each joint welding procedure even if the specification references drawing numbers.

3.2.3 The following basic information and essential variables shall be included in sufficient detail to assure that compliance with the requirements of the specification can be verified:

1. Basic Information
a. Joint Design: (the joint geometry, fit-up, and other required dimensions of the welded j oint) tolerances and material thickness.
b. Method of arc initiation
c. Electrode size (for gas tungsten arc welding)
d. Gas type and flow rate (shielding and backing gas)
e. Welding current range for manual welding
f. Whether tack welds or fixtures are used for assembly of the joint for welding
g. Method and frequency of cleaning
h. Number of weld layers and passes
i. Whether stringer beads or weave beads are used
2. Essential Variables
a. General, All Welding Processes.

i.A change from a base material type or grade (materials of the same nominal chemical analysis and mechanical property range, even though a different product form) to any other base material type or grade. When joints are made between two different types or grades of base material, a procedure qualification shall be made for the applicable combinations of materials, even though procedure qualification tests have been made for each of the two base materials welded to itself.

Appendix B Appendix 3-50 Rev 2. July 23, 2015 PUR-1 SAR

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSpRU U ASSEMBLEDRE VEST- oFOR THE Effective Date: 01/24/07 Page: 46 of 57 ii. A change of filler metal type or classification to any other type of classification iii. A change in welding position.

iv. A change in vertical welding direction, i.e., from upward to downward or vice versa.

v. The addition or omission of integral backing (e.g.,

"butt-lap" type joint).

vi. The addition or omission of nonfusing metal retainers.

vii. The addition or omission of filler metal to the joint.

viii. Any change in the method by which filler is added, such as preplaced shims, preplaced wire, preplaced consumable inserts, wire feed, or prior weld metal surfacing ("buttering") of one or both joint faces.

ix. The addition or omission or any type of preplaced consumable inserts or joint surfacing.

x. A change in the shape or size of preplaced consumable inserts or joint surfacing.

xi. A change from multiple pass welds to single pass welds.

xii. The omission of inert gas backing during welding, except that requalification is not required where a qualified welding procedure is changed to omit the inert gas backing and then is used only for a single welded butt joint with a backing strip, or a fillet weld. For multiple pass welding, the omission of inert gas backing during welding until three layers or 3/16 of weld metal thickness has been deposited, whichever is greatest.

xiii. A change from one welding process to any other process or combination of welding processes.

b. Manual Welding, All Welding Processes.

Appendix B PUR-1 SAR Appendix 3-51 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 47 of 57 PURDUE UNIVERSITY REACTOR

1. An increase in the standard size of filler metal from that stated and qualified in the procedure specification.

ii. A change in joint geometry which violates the tolerances given for the joint geometry elements listed below:

Bevel Angle: State in procedure specification.

Tolerance:- Minus 5%.

Groove Angle: State in procedure specification.

Tolerance: Minus 5%

Alignment Tolerance: Assign value in procedure specification. Qualify procedure for single welded joints using maximum permissible misalignment in a portion of the joint.

c. Gas Tungsten Arc Process.
1. A change of electrode material type.

ii. A change in arc starting methods.

iii. A change from a single shielding gas to any other shielding gas or to a mixture of shielding gases or a change in specified composition of gas mixture.

iv. A decrease in shielded gas flow rate of more than ten percent.

Appendix B PUR-1 SAR Appendix 3-52 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 48 of 57 PURDUE UNIVERSITY REACTOR 3.3 Welding Procedure Qualification 3.3.1 The welding procedure shall be qualified to the requirements of this section.

3.3.2 All welding used in qualifying a welding procedure shall be performed in accordance with a welding procedure specification.

3.3.3 Before any welding is performed on production components, the supplier shall qualify each proposed welding procedure by:

1. Recording all essential elements of the welding procedure in a welding procedure specification (see Section 3.2)
2. Verifying the welding procedure specification by welding test specimens representing each joint to be welded in production and performing nondestructive examination and destructive tests in accordance with the requirements of this Appendix.
3. Submitting to the purchaser, for information, the welding procedure specification and a certified copy of the detailed results obtained from the tests performed on the test welds. The metallographic sections required by this Appendix shall also be submitted to the purchaser.

Appendix B Appendix 3-53 Rev 2. July 23, 2015 PUR-1 SAR

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 49 of 57 PURDUE UNIVERSITY REACTOR 3.3.4 Essential Variables. The welding procedure shall be set us as a new welding procedure specification and shall be completely re-qualified when any of the changes listed in Section 3.2.3.2 are made in the procedure.

3.3.5 Chart Recordings. Current-voltage-time charts shall be used for each procedure qualification weld for automatic or machine welding.

Calibrated current and voltage indicating meters may be substituted for trace chart type equipment for manual welding. The current and voltage ranges shall be recorded for manual welding.

3.4 Welder Performance Qualification 3.4.1 Performance qualification weld tests shall meet the requirements of this section, except that any welder used to qualify the welding procedure shall also be considered qualified and additional performance weld tests are not required.

3.4.2 General.

1. The performance qualification tests are intended to determine the ability of welders to make sound welds.
2. The performance test may be terminated at any stage of the testing procedure whenever it becomes apparent to the supervisor conducting the tests that the welder does not have skill required to produce satisfactory results. In this event, the welder may be re-tested at the discretion of the supplier in accordance with 3.4.3.
3. Each supplier shall maintain a record of the procedures, including the essential variables, under which welders are examined and the results of the examinations.

3.4.3 Qualification of Welders.

1. Each welder shall pass the tests prescribed for procedure qualification except that tensile tests are not required. The essential variables and the test results obtained by each welder shall be recorded in a Performance Qualification Test Report. Any welder who performs acceptable welding procedure qualification tests shall be considered qualified.
2. Renewal of Qualification. Requalification of a welder is required when:

Appendix B PUR-1 SAR Appendix 3-54 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-3 82 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 50 of 57 PURDUE UNIVERSITY REACTOR

a. 90 or more days have elapsed since he last produced acceptable welds using the specific welding process, or
b. He has not performed acceptable welds using the production welding procedure.
c. Any time there is a specific reason to question a welder's ability to make welds meeting the requirements of this Appendix, requalification shall be required. Only one test weld shall be required for renewal of qualification. If this test weld fails to meet all of the original requirements, then a complete performance requalification shall be required.

3.4.4 Chart Recordings. Current-voltage-time charts shall be used for each procedure and performance qualification weld for automatic or machine welding. Calibrated current and voltage indicating meters may be substituted for trace chart type equipment for manual welding. The current and voltage ranges shall be recorded for manual welding.

3.5 Welding Machine Qualification 3.5.1 Performance qualification weld tests shall meet the requirements of this section, except that any welding machine used to qualify the welding procedure shall also be considered qualified and additional performance weld tests are not required.

1. The performance qualification tests are intended to determine the ability of welding machines to make sound welds.
2. Any time there is a specific reason to question a welding machine's ability to make welds meeting the requirements of this Appendix, requalification shall be required. Only one test weld shall be required for renewal of qualification. If this test weld fails to meet all of the original requirements, then a complete performance requalification shall be required. Welding machines used for the manual welding of any successful procedure or welder qualification tests shall be considered qualified for manual welding of all core components covered in this Appendix.

Appendix B AR Appendix 3-55 Rev 2. July 2 PUR-1 SI 3, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTSpRU UIEST-ASSEMBLEDRECoFOR THE Effective Date: 01/24/07 Page: 51 of 5 3.5.2 Welding machines used for the manual welding of any successful welder performance qualification tests shall be considered qualified for manual welding of all components covered in this session.

3.6 Examination & Tests 3.6.1 Type of Test Required. The following tests shall be used for the qualification of welding procedures and / or welders as applicable:

1. Nondestructive examination by a liquid penetrant method.
2. Nondestructive examination by Visual to test for soundness and surface characteristics of the weld.
3. Destructive examination by sectioning for metallo graphic examination of weld joints and adjacent areas to test for fusion, weld geometry, weld reinforcement, and soundness of the weld.
4. When the purchaser has reason to believe that the quality of any weldment is doubtful, he may require additional inspection.
5. Nondestructive Examination and Tests
a. Visual. The test weld shall be examined visually prior to welding and after welding in accordance with Section 5.1
b. Liquid Penetrant. The test weld shall be examined after the.

final layer in accordance with Section 3.6.2.2 using a color contrast method.

c. Unless otherwise specified, inspection of procedure and performance qualification welds shall be performed in the final surface condition.
6. Destructive Examination. Each test weld shall be sectioned transversely to metallographically examine a minimum of:
a. Three section faces for welds on cylindrical components less than 1'A inch in diameter or for welds that are one to four inches long on non-cylindrical components.
b. Four sections faces for welds in cylindrical components that are greater than 11/4'/ inch in diameter or for welds that are greater than four inches long on non-cylindrical components.

Appendix B ARAppendix 3-56 Rev 2. July2 .33,2015 PUR-1 St

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS -. ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 52 of 57 PURDUE UNIVERSITY REACTOR

c. One section face for plug welds, arc spot welds, and welds that are less than one inch long on non-cylindrical components.
d. The cross section shall be polished and etched to provide clear definition of the structure in the fusion zone and the heat-affected zones.
e. For welds in (a) and (b) of this paragraph, one cross section shall be made through a weld start and a weld stop area and the remaining sections shall be made at random. For weld described in (c) of this paragraph, the cross section shall be made at the approximate centerline of the weld.

Examination of the welds shall be in accordance with Section 3.6.2.3.

3.6.2 Acceptance Criteria for Qualification Test Welds

1. Visual Examination. Visual examination shall be in accordance with Section 5.1.
2. Liquid Penetrant Examination. Unless otherwise specified, final weld surfaces shall be examined using a color contrast method.
a. For welded joints in materials less than 1/8 inch thick the following relevant indications are unacceptable.
1. Any cracks.

ii. Linear indications.

iii. Indications with dimensions exceeding 1/64 inch.

iv. Rounded indication separated by 1/44 inch or less edge-to-edge.

v. Five or more rounded indications in any six square inches of weld surface with the maj or dimension of this area not to exceed six inches with the area being taken in the most unfavorable location relative to the indication being evaluated.
b. For all welds in materials 1/8 inch thick or greater, the following relevant indications are unacceptable. (Only Appendix B PUR-1 SAR Appendix 3-57 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382of5 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THlE Effective Date: 01/24/07 Page: 53of5 PURDUE UNIVERSITY REACTOR those indications with maj or dimensions greater than 1/64 inch are considered relevant for item (iii).)

1. Any cracks.

ii. Any linear indications.

iii. Rounded indications with dimensions exceeding 10 percent of the nominal weld thickness or 1/8 inch, whichever is smaller. Rounded indications separated by 1/16 or less edge-to-edge shall be evaluated as a single indication.

iv. Four or more rounded indications in a line separated by 1/16 inch or less edge-to-edge.

v. Six or more indications in any six square inches of weld surface with the major dimension of this area not to exceed six inches with the area taken in the most unfavorable location relative to the indications being evaluated.

vi. Aligned indications in which the average of the center-to-center distance between any one indication and the two adjacent indications in a straight line is less than 3/16 inch.

3. Metallo graphic Examination Metallographic examinations shall be performed on qualification test welds at not less than 50X on test welds as required in this Section in accordance with ASTM E.2.

Any cross section which is shown by metallographic examination to contain any of the following relevant defects shall be cause for rejection of the test welds.

a. Any cracks.
b. Incomplete fusion, or insufficient joint or root penetration.
c. Any tungsten inclusions, slag inclusions, or porosity having a maximum dimension greater than 20 percent of the weld thickness or 1/32 inch, whichever is smaller.
d. More than four tungsten inclusions or pores which have a~

maximum dimension less than in (c) above.

Appendix B Appendix 3-58 Rev 2. July 23, 2015 PUR-1 SAR

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 54 of 57 PURDUE UNIVERSITY REACTOR

e. Any deviation from specified weld geometry or weld reinforcement.

3.6.3 Test Welds.

1. Procedure and / or welder performance qualification shall be made on test welds which duplicate the production weld joint type and which simulate the conditions to be used in production with respect to orientation, the essential variables listed in Section 3.2.3.2, and the dimensions of the parts to be joined to the extent that they affect heat requirements, relative motions, and distortions. All welding used in qualifying a welding procedure and / or welder performance shall be performed in accordance with the procedure specification.
2. For manual welding, two consecutive test welds shall be made when the weld joint is less than six inches in length. Only one test weld shall be required when the weld joint is 6 inches or greater in length.
3. All test welds shall be tested using the required tests listed in Section 3.6.1. To qualify the procedure specification used in making the test welds, each Weld shall pass the required tests.
4. Repair of procedure or performance qualification test weld(s) is prohibited.
4. Production Welding All production welding shall be accomplished using approved welding procedure specifications and qualified welders and/or welding operators.
5. Quality Acceptance of Production Welds 5.1 All completed production welds shall be visually examined in accordance with the following requirements:

5.1.1 General Visual Inspection Requirements. All visual examinations shall comply with the following:

1. Visual examination shall be made under direct daylight-type fluorescent lighting of at least 100 foot-candles at the work examination area.

Appendix B PUR-1 SAR Appendix 3-59 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 55 of 57 PURDUE UNIVERSITY REACTOR

2. Visual examination shall be performed with the aid of a 5x (minimum) magnifying glass.
3. The inspection required by this standard shall not be performed by the welder who made the welds. However, if the welder is qualified in accordance with this standard, he may visually inspect his own welds prior to the inspections required by this standard.
4. Personnel performing visual inspection shall have 20-20 vision, natural or corrected, stereo acuity, and shall not be color-blind.

5.1.2 Visual Acceptance Criteria (except for porosity). Visual examination of weld joint preparations and welds shall be performed in accordance with the following requirements to verify conformance to the written welding procedure, the design requirements, and the requirements of this standard:

1. Prior to welding, the weld joint edges and adjacent surfaces shall be examined for:
a. Proper edge preparation, dimensions, and finish.
b. Alignment and fitup of the pieces being welded.
c. Verification of correct material by check of records.
d. Verification of the cleanliness requirements.
2. After welding, the joint shall be examined in the final surface condition for:
a. Contour, reinforcement and surface finish of welds.
b. Degree of underfill, undercut, and overlap.
c. Arc strikes, weld spatter and impression marking.
d. Burn-through and fuse-through
3. Weld joints and surfaces which are shown by visual examination to have any of the following defects or areas of nonconformance are unacceptable:
a. Any nonconformance revealed by 5.1.2.1.

Appendix B PUR-1 SAR Appendix 3-60 Rev 2. July 23, 2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STAN7DARD AND CONTROL FUEL Revision: 1 ELEMENTS - ASSEMBLED FOR THlE Effective Date: 01/24/07 Page: 56 of 57 PURDUE UNTIVERSITY REACTOR

b. Any zone of incomplete fusion.
c. Insufficient joint or root penetration.
d. Any undercutting, underfill, or burn through.
e. Any concavity on the face side of groove welds.
f. Any arc strikes, weld spatter, and impression marking.
g. Any visible inclusions, porosity, cracks, and unfilled craters.
4. Machined welds shall meet the drawing requirements.
5. All welds shall be free from surface markings resulting from mishandling, punching, scratching, etc., which exceed the specified surface requirements.
6. All welds shall be fiee of dross, or slag.
7. All welds shall be free of oxidation due to improper shfielding and overheating which produce black or gray spalling or loose particles. Iridescent temper films and the dark metallic vapor deposits which may occur adjacent to the welds are acceptable.

These films and deposits shall be removed by approved cleaning procedures when accessible.

5.1.3 Visible unacceptable porosity is as follows:

1. Four or more pores with a major dimension of 0.048 inches or more randomly positioned.
2. A single pore with a major dimension of 0.064 inches or more.
3. Six or more pores with a major dimension of 0.016 inches or greater in one weld.
4. Four or more porosity with a major dimension of 0.016 inches or greater, in line separated by less than 0.063 inches from edge to edge.

5.2 Repair of a defective weld by welding shall be limited to two attempts.

Unacceptable defects shall be removed and re-examination made using liquid penetrant color contrast method to assure complete removal of the defect. If the Appendix B PUR-1 Sa ANAppendix 3-61 Rev 2. July2 3,2015

Form 412.09 (Rev. 09)

Idaho National Laboratory SPECIFICATION FOR PURDUE UNIVERSITY Identifier: SPC-382 STANDARD AND CONTROL FUEL Revision: 1 ELEMENTS -. ASSEMBLED FOR THE Effective Date: 01/24/07 Page: 57 of 57 PURDUE UNIVERSITY REACTOR removal of the defects results in reducing the thickness of the weld metal below the thickness of the base metal, the area shall be rewelded using a welding repair procedure which has been approved by the Purchaser. Whenever a defect is removed and subsequent repair by welding is not required, the excavated area shall be blended into the surrounding surface to remove any sharp notches, crevices or corners. Completed repairs shall be visually re-examined per Section 5.1. Records shall be maintained on all repairs and shall include the following:

5.2.1 Location ofj oint.

5.2.2 Location of defect.

5.2.3 Description of defect, including type and size.

5.2.4 Reference to approved repair procedure.

5.2.5 Inspections before and after repair and the results thereof.

5.2.6 Identification of repair welders or welding operators.

Appendix B PUR-1 SAR PUR-1 SARRevA2.pJuyi23,3201 Rev2. July 23, 2015

1 R A .J 4 I 2 I 1 2

21 SHEET REVSTATUS E

PTA LESHEETS REVISED 0

DESCRIPTION PHYSIS OF ITEM 3 NY1C M ~tI ASSESSHEET2;

1. PROCURE. ANDINSPECT FABRICATE, PERSPECIFICATION SNOTES:

2 SPC-382.

L ŽMARK ASSEMBLY ISENTFItC.BT82 PER SPECIFICATION SPO-SA2. I SEEOSAR-RADE ESS2 ,&8 1/2SA/ST

3. REMOVEAUL BURRSHASSHARPESGES.

2 ASSESITEMS. CHANGES MATEREAL ITEM?

CHANGES ITEMS.SEESAA-RTA7VT A/ASS D

C 4 CU PAILLPS,100" 3I6 SSTOR304SST 9 1 635457.5 SOURCEDRIVE TOP .

  • B B

A S CU PHILUPS,T00O 315SST OR~f*SST 7 B-SBSAC-2A S I/SLU 1 635482-3 SOURCE DRIVE CONTAINERA 1 535465-1 GRAPHITE BLOCK 1 R35462-1 GRAPHITE CONTAINER3 ASSEMBLY SC .5 SOURCE ERRSE SUPPORT ASSEMBLY2 sc1 GRAPHITE REFLECTOR ASSEMBLY1 r

-1 SECTIONED ISOMETRIC REFERENCE ONLY A

sncsoa= REOURNTR: T,VINNOU.N SCALE:NONE HARRIK 3SIG S. MORRELL PURSUEUNIVERSITY

-2 FINAL ae* *N: N OUDRAM TESTRESEARCH ANDTRAINING REACTOR TA/SM-TS.,t PROJECTSEO.IGRAPHITE REFLECTOR ASSEMBLY AND

-t FINAL SPA.'USS SOURCEDRIVE ASSEMBL.Y PROR I PHIRSCAAPPARH ARTUI/ES G* 5

  • PURS-1OAR Arniendix 3-63 Rev' 2, Iulv 23, 2015

[ APPLE~ATUN AFFECTARIVTE:A/1iO S*aH NOTES 1 OF 2 ISHEET U / b b 4 L*

I 21 SORE0V

Y I 7

' I V I "."

517 W

'* I V I

'2

  • I "1

I ID I

B (2953) AX 7 I2.95 (3 AX C

-2 ASSEMBLY SCALE:

111 B

V A

-2 SECTIONED SCALE:

NONE ISOMETRIC PUR-1 SAR Appendls 3-64 Rev 2, July 23, 2013 D OIMF3 DWG-635454 2 0 I i., I I*" I CAE AII A I

/ I& D 4 :j 1 sDso:*

8I 7T 6 5 ~J7 I I i T

  • 4 c I *w*s

{

NOTES:

1. PROCURE. FABRICATE.ANDINSPECT PERSPECIFICATION SPC-3R2.

LIADDED A -3ASSY; TITLES L1UICHNG

/ŽMARKE ASSEMBLY IDENT1FICATIONPERSPECIFICATIONSPC-TBZ 1CHANGED NOTE TO 3 SHOW REVISED NEWFUEL PLATE DESIGN; 140

/.OUANTn~f OF ITEM 5 (FUELPlATES)ANADITEMN(DUMMY FUELPLATES) USEDIN-UASSEMULY SEDADD UGUUUED ITEM B. CHARGED MATERIAL ITEMA, HHD (PARTIAL FUEL ASSEMBLY)

A\CHANNE L SPACING TO REDETERMINED BYTHEUSER.

I;SO'TRO*" BYSIDEPLATEGROOVE LOCATIONS ANDWIDTHS. AND ITEM.. ,NOTEA,,SEEO ..

A.... I ....

FUELPLATE THICKNESS.DIRECT MEASUREMENT IS NOTREQUIRED.

S. REMOVE AU.BURRS ANDSHARPEDGES. ___________-(-I  %

D K

It VA C

~-1 A*

-2 A*

45 B-3MA MACHINE SCREW, FLATHD.

PHIWPS,1W0'3B TO ST 8-3UUNC-UA X lI2LG -- 3!6 SST OR*SST B

MAHN

  • EFLAT HD, A 4 4 EG PHIWPU.I1DO" 31 SSTOR DR4 UST H 14 AH A 6.35A3-3 DUMMY FUELPLATE B AR 14 A35463-1 FUELPLATEASSEMBLY 5 1 1 1 635454-1 STANDARD FUELCONTAINER4 SC -D DUMMY FUELELEMENT3 SC -2 PARTIAL FUEL ELEMENT SC -I STIANDARD FUELELEMEN'T

-ASSEMMESBATRIOLY T S1IAEATTCETK CAT EUNTEY*NSA DRUESCBPT0H 0RHEI*RRA AG

-1 SECTIONED SCALE:NONE ISOMETRIC REFERENCE ONLY VWIRFSRRT RESSEUSTER:

T. VINNOLA am~o* L*DeIG2DMOREL PURDUEUNIVERSITY TESTRESEARCH ANDTRAINING REACTOR

.. IFNA STANDARD FUEL.PARTIAL U DUMMY ELEMENT ASSEMBUES FUR-I SAR AppendixE 3-65 Rev 2, July 23, 2015 in~i DwMFG.'*635455 IP*V R I7 I I PLIAWT I ,TSORP - EE. O I U T 2 1 SD*2

8 7 6 5 4 3 I 1

.........

NOTES: RAY I*sMCHIO EFRFIN DATA.

1. PROCURE,FABRICATE, ANDINSPECT SPC-.382.

PERSPECIFICATION 2 CHANGED TO SHOWNEWFUELPLATEDESION:

LXA ASEMLY DNIFCTO PE DRSECFID;CAINSC-B ..... T... I ADDED -2 ASSEMBLY.

SEESAR-N3094D0 SECTION A-A.B ITEM6; 1524/07 CHANGED MEATERIAL ITEM?7CHANGED MOTE 3.

FUELPLATETHICKNESS.

DIRECTMEASUREMENTIS NOTREOUIRED.

4. REMOVEALLBURRSANDSHARPEDGED.

IC A

-1 ASSEMBLY B

-2 ASSEMBLY MACAWNE SCREW.FLATAS. O~

S B CG PHILWPS,SB0 316SETON34SST 7 S-3D UNO-DA A5/11LU A

--SECHANNELSUPACNG .156 8

1 1 535AA3.3 DUMMY S3SH6A=11I CONTROL FUELPLATE TOP 6

5 B 635463-I FUELPLATE ASSEMBLY A 1 I 34B CONTROL FUELCONTAINER ASSEMBSLY SC *D DUMMY CONTROL FUELELEMENT ASSEMBLY2 SC *t CONTROL FUELELEMENT S-T ASSEMBLY1 CAT. BERTPYPTIOG 0S TESPTE0M CA OSEBANBAB AU

-1 SECTIONED SCALE:

NONE ISOMETRIC BEFERENCEONLY A

mua= e..7 RAOLESISR:

T. VINMOLA SECTION SCALE.1/1 A-A PURDUEUNIVERSrITY

-2 FINAL TESTRESEACRH ANDTRAINING REACTOR CONTROL FUELELEMENT ASSEMBLY AND

-1 FINAL DUMMY CONATROL FUELELEMENT ASSEMBLY PUR-1 SAR Appendix 3-66 Rev 2, July 23, 2015 DI01MF3 DwO-635456 2~

C I 7 I I A, L I Z U

T T *.+ O 1 *a*

R 7 5 4 3 2 1 NOTES:

1. PROCURE, FABRICATE,ANDINSPECT PER SPECIFICATION REVISE TO SHOWNEWFUELPLATEDESGN; SPC-382.

1 REMOVED iTEMS2,4A&7REVIESEDTITLE; L~MARK ASSEMBLY IDENTIFICATION PERSPECIFICATION SPC-382, 2 SEE DA-514751 BEEDAR-SURAUR HEIVISiNS 1/2407

/40 3CHANNELSPACING IS CNROLDBY SIDEPLATEGROOVELOCATIONS ANDWIDTHS,AND REVISED NOTESB& MATERIAL ONITEM B 4

FUELPLATETHICTINESS.

DIRECTMEASUREMENTIS NOTREQUIRED.

4a REMOVE ALLBURRS ANDSHARPEDGES.

0 A

-1 ASSEMBLY SCALE:11' B

MACHINE SCREW. FLATRD.

CDPHILLIPS. ITS' 316SSTOR[504SST B B-32UNC.DA X 5/16LG B*

35468-? FISSIONCHAMBER TOP A 635463-1 PUEL PLATE ASSEMBLY S 515458-1 STANDARD FUELCONTAINER ASSEMRBLV (DXCHANNEL A

SPACING

.120) -ISNNEL SPACING .130(

-U REMOVED S DC -1 EEMNTFISSION CRAMBER ASML FUEL

-1 SECTIONED ISOMETRIC SECTION A-A SCALE:HONE SCALE.1/

REFERENCEONLY LIST PUTSUSI P*T*

A RAT D*IS

  • RHAURSTER:

T.VINNOLA ottaRR AESRGNa MORRELL PURDUE UNISERSITY

, ,=,WN N.OLOHAM TEATRESEARCH ANDTRAINIMO REACTON FISSIONCRAMBERFUELELEMENT ASSEMBLY i FINALTR StUR- l SAR AppendixE 367 Rev 2, July 23. 2015 I.!I. I 1

  • °*635457 I'*

APLICATMB - 1I I. ElF 1.

8 77 6b AlA 4 4

SORRY I.

1 ..

SD*o*

NOTES:

1. PROCURE,FABRICATE.

ANTINSPECT PERSPECIFICATION SPC-352.

2r REMOVED

3. REMOVED
4. REMOVE ALLRIURRS ANDSHARP EDGES.
5. WELDPERSPECIRCEATION SPC-352APPENODD B.USINGITEM 7 (WELD FILLERMETAL).

S. AUL CORNER ANDFILLETRADII

,U30UNLESS OTHERWISE NOTED.

SCRUTICAL INTERFACEDIMENSIONSSHALL BEADHERED TO.

ANVERIFY RECTANGULAR GAUGE.DFEPROVIDED CAVITYANDSLOTSIZEWITH GO-NO-GO GAUGE SHALL GO-NO-GO SLIDE FREELY THROUGHOUT ENTIREDESIGNATED CAVITY(OR SLOT)LENGTH FOR ALLULOTSW*IrHUIUT HANG-UP,STICEING.

OR DISENGAGEMENT FROM SLOT.

-1 ASSEMBLY -1 ISOMETRIC VIEW REFERENCE ONLY SCALE:

1/1 SCALE:

NONE VIEW B DEALE:4:1 VIEW C AU SCALE.

4/1 VIEW A SCALE: 2/1 PUR-I1SAR Appendix 3-68 Rev 2, July 23, 2015

NOTES:

1. PROCURE.FABRICATE.

ANDINSPECT PERSPECIFICATIONSPC-382.

2. REMOVED
3. REMOVED B. REMOVE ALLBURRSANDSHARPEDGES.

U. WlELD PERSPECIFICATION SPC.382APPENDIX B. USING ITEM7 (WELD FILLERMETAL).

THROUGHOUT ENTIREDESIGNATEDCAVITY(ORSLOT)LENGTH FOR ALLSLOTSWITHOUTHANG-UP, STICKING,ONDISENGAGEMENT FROM SLOT,

-1 ASSEMBLY SCALE:1/1

-1 ISOMETRIC SCALA:

NONE VIEW REFERENCE ONLY jz~~

VIEW SCALE:

B 4/1 VIEW C 4x

,SCALE:

4/l VIEW A SCALE:E1 PUR-1 SAR Appendix 3-69 Rev 2, July 23,2015

NOTES:

1. PROCURE.FABRICATE.

ANDINSPECT PERSPECIFICATION SPO-,3A2.

2. REMOVED
3. REMOVE ALLBURRSAWD SRARPEDGES.

A. WELDpERSPECIFICATIONSEC-UB2 APPENODIXB, USINGITEM 7 (WELDFILLERMETAL). _

5. REMOVED.

GAUGE.OFFPROVIDED GO-MO-GOGAUGE SHALL FREELY S LIIDE TH*ROUGAGUTENTIREDESIGNATESCAVITY(ORSLOT)tLENGTH FON ALLSLOTSPATAGUTHANG-UP.STICKING.

ORDISENGAGEMENT FROMSLOT.

,167/

-1 ASSEMBLY SEALE III

-1 ISOMETRIC SCALE:

NONE VIEW REFERENCE ONLY i"

(,060)*'1-3 WIEWA UCALE:Dli VIEW SCALE:

C A/l AU

7 S 47 4 R 3 2 I 1 NOTES: REVl04100 I EFECTNEATE SEEDAR-514751 REVINIONS 440

1. PROCURE.TABRRCATE, ANDINSPECTPERSPECIFICATION SPC-382. REVISED THEDESCRIPTION SFRTEM 3 /47 1SEE DAR-5UH425 /40 Z/2*\MARK ASSEMRLY IDENTFIfCATION PERSPECIFICATION SPO-3E2.

2CHANGED MATERIAL ITEM7 4AU

3. REMOVE ALLBURRSANDSHARPEDGES.

D

.4 1 F

  • mL

-1 ASSEMBLY SCALE:1,1 B

MACHINE SCREW,FLAT HD, A CAPHILUIPS, TOO 316 SSTOR3U4 SOT 7 R*.32, UNC-2A 0172LU __

1 835461.2 CAPSULE INSERT ASSEMBLY 1 635451.1 CAPSULE HOLDERHASSEMBLVY 1 63S462-I GRAPHITE CONTAINER3 ASSEMBLY DC -1 IRRADIATION FACILITY ASSEMELY I

-1 SAFETI PARTOB IIOAIELtISERE UHIE RIE,/PECFECATEH ITEI 510011 (1SFTI CA*

T. EIEqNTEMTI ECAET.,'P' URAE,.SRMA o..

A

-1 SECTIONED ISOMETRIC REFERENCEONLY SCALE:NONE 05TN400 BEASlN U.MORRELL PURDUEUNt~fERSITY ETORiroOR TNAN OLOHAM TESTRESEARCH ANDTRAINING REACTOR L* FINAL TOOTNTA U, 0 so 004C IRRADIATION FACILITYASSEMBLY

  • F NEXT AS* .. ...... ..... 1M owG.635460 2"*

PI16.1 CAD Ann,.HSiY 3-71 A.RT I/O/Rh 101IS NEBOTI 505051 1F

~TI F STBACUB/OE 2 1 S2EU32 66 4 8 77 'P 4 2, 1 SD8032

I

-7 P

12 4,

4 3 2 I 1 I.I.,ll I REV REASONS STATES NOTES: ITITI1IREV IDESl.ETSj REVISEDTOLERANCES ONlITEM

1. REMOVEALLBURRSANDSHARPEDGSES.
2. pROCURE.

FABRICATE.

ANDINSPECT PERSPECIFICATION SPC-382.

I I ..............

1%o?

I

3. WELDPERSPECIFICATION SP0-322APPENDIXR.USING ITEM17{WE LDFILLERMETAL).

4.ALLCORNERANDFILLET RAD*II.O3OUNLESS OTIIERISSENOTED.

D I-

........................... J -O SEEDETAIL

_(2.755) 3 SEE ASS C

-1 ASSEMBLY SCALE Ill AR AR AR AR SC ELILRMTL ER4043 AWDA5AD 17 AR SC BAR.01/)2 ASTMB211 IN ALSON61.TNST AR SC BA*R.

0114 ASTMB2TT IS AL6021-T05 1 AR SC 002101t18 ASTMB211 14 TB51 ALBAAI.

AR SC TUBING,1 TI8ODX D05WALL 12 AL.DEI-TE ASTM B21D AR SC iTUBING,1*314005X.,25 WALL Il ALBAA61.TB ASTM8212 1 C10 PLGpLATE, 1127115 ASTMBUS ID AL 661 T-5 I SC -B CAPSULE UPPERTUBE BAR,01 31 ASTM8211 9 t S -8 CAPSUIEHOLDER TOP PLATE.I THE ASTI,BUSS 8 45 .D535A5\

  • "4-1 7F 5THR.. tSC -7 CAPSULE HOLDE*R BOTTOM PLATE.54114TK P.5748209 7 3XHRU 1 535405-2 GRAPHT CAPSULE HOLDER S SC *4 CAPSULE HOLDER TOPPLATE4 1 SC .3 CAPSULE HOLDER WELDMENT3 275 5

ASSEMBLY SC -2 CAPSULE RNSERT ASSEMBLY

-LK 2 SC .1 CAPSULE HIOLDER ASSEMBLY P0279 IBEREIELFATIO TO WOE/BOOtlN SSAEIOUHRNB AT

-1 ISOMETRIC REFERENEONLY NONE SCALE:

oDETAIL SCALE: U11 P4415SIL$

- B.B,m 5y BEALBASl*T.RINOLA mIInt* CF.*N DEBAMORREL PURDUEUSIVERSITY TESTRESEARCH 4245TRAINING REACTOR

-2 635460 CAPSULE HOLDER ANDCAPSULE INSERT

-I 635460 IBRBB FOR*IB*4,92 O IDAI ASSAMBUES ANDDETAILA 0 9911 c 550 N*x**SV PUJR- I SAR Appendix 3-72 ReP 2. July 23, 2015 1 I*'*

95115*1 8R :_=='

OF 3

  • - ,^ b 31 '8 1 8 7 0 1 Su*o*

a 7 6 5 4 3 2 1 D

z5.1* "4"4 "1

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-02.6

.0065X45" 8 ESDETA SECTION A-A SECTION B-B SCALE LI SCALEIII B

(255) 20 14 000

~1 '4- ABC

-4 ASSEMBLY BVVB~I

[0]

-8 ISOMETRIC R*EERECE ONL SCALE:

NONE A

0* DETAIL SCALE:il1 PUR-i SAR AppendLx 3-73 Roy 2, July 23. 201.5 D O1MF3 ow3.635461 1 1 008032

[0 U /I b t5 44 2 1 so*

Q a

"7

-7 R J, ,l A

1 0

-u-i C

'1

-2 ASSEMBLY SCALE:

Oit IR 0110 2.750

-0

- -H01(.

f 01.040 B

C) DETAIL C) DETAIL SCALE.211 A

-2 ISOMETRIC FIEFNENCE OLY PUR-1 SAR AppendLx 3-74 Re'," 2. July 23.2015 0 IO1MF3' ow-356 SCALENONE B

8 7/

PUR-i SAR Appendix 3-74 Rev 2. July23. 2015 'P 4 4

3 3

2 2 1 SDE*2

.7 IV 4, A 9 1 NOTES:

REMOVEDPRIORREVHISTORY IO

1. REMOVEALLBURRSANDSHARPEDGES. 4SEE ECR-55V8)R72/0
2. PROCURE.

FABRICATE.

ANDINSPECT PERSPECIFICATION SP-32. REVIVED DIMENSIONS BSl

3. WELDPERSPECIFICATION SPC-SJA2 APPENDSXB. USINGITEMB WEhLD F'iLLERMETAL).

A. ALLCORNERANDFILLET RADII.232 UNLESS OTHERWISE NOTED.

4CRITICAL INTERFACE DRMENSIONSSHALL READHERED TO, D

/~VERIFYRECTAN*G ULARCAVITY ANDSLOTSIZEWITH GO-NO-GO DAUGE. DIV PROVIDED GO-NO-GO GAUGESHALLSLIDEFREE LYTHIROUGHOUT ENTIRE DESIGNATED CAVITY(OR SLOT)

LENGTHFORALLSLOTSWITHOUTY HANG-UP. STICKING. ORDISENGAGEMENT FROM SLOT.

.---.---.J, m

-1 ISOMETRIC REFERENCE ONLY SCALE: NONE

-1,ASSEMBLY IsHOw

-3 ASSEMBLY (SIMILR) AR AR SC WELDFILLERMETAL ER4043 AWEANS) BS 1 -T* SOUIRCEDRIVE NOZZLE MK RMASU-ASSEMBLY MK RM656-I "' -H NOZZLE MANE FROGM B3SAHT-3 B IINCONTAINER MN RMBNS-1 N1 - TUNE ASSEMBLY MK RM656*

SCS3.OURCE DRIVE CONTAINER3 S-3 ASSEMBLY3

-2 REMOVED2 S-, GRAPHITECONTAINER ASSEMBLY1 PA*I*

4-NEAGA*S!"ENT.VINNOLA PUDUE UNIVERSAITY HAHN)S, NORRELL TESTRESEARCH ANAD TRAININGREACTOR

  • m 5)3.1 N. GIGISAM GRAPHITECONTAINER ASSEMBLY ISSAA ENAWJANA. ANDSOURCE DRIVECONTAINER ASSEMBLY

-HASNAG)5ANN

-IA5NI rnAO3 OENNWA)P)NANLSNAV)NS t'NCE'P VIEW A SAD6354621M3ISW SCALE:*I FUR-I1SAR Appendix 3-75 Rev 2, July23, 2015 VIEW B 4 .1.

/I b t* b9 4 :J

8 I 7 I I4 I I 2 I NOTES: I I I I..

1. REMOVE ALL.

BURRS ANDSHARP EDGES.SE c.583720

2. PROCURE. FABRICATE.

ANDINSPECT PERSPECIFICATTON SPC-382, SEEECR.652525 811507 I/3ALL GROOVE LOCATIONING DIMENSIONS ARE*8802ANDTOLERANCE SHALL NOTSEACCUMULATIHE UNLESSOTHERWISE SPECIFIES. 8SEER53R L+/-ŽWELDPREPASNECESSARY.

5.REMOVEDD

/Z\TOLERANCE XXX 1.041

-2RV8X.005MAD 2557 22 .28_D - CZ .1883

- :2.AA cm.]oE0 .

- .8 (Cm TNDR IEPLT HE O LTjBT 211 C

-2284 __ __H__ET ETILL8THND8HW -0 EMVE 1

- 1DEAI 098 N________-__PARPT__L,-E '.T.*

AT ~__ -. ____

84 ___

.21 ,, *622STANDARDSIDE PLATE SHEET ORPLATE ATMB2 SC

-1 ERGTSAND ALNIT 85361221T6 G DEALETADSHSRI-IT REMOVES ID

-3 GTOrRLSDETAILRIGHTE ANS06 OPOSTE) SCMB21 -5 SPCRPLATED 82417 (I) UT ASTIM 8209 5uS LEFT HND5Al.8881-T 1-C 635STANDARD SIDEPDLNE.MEETEOR PLATE ANSVER 8221

  • 6 3548 11111m* R/ LEFTDU HANDT RESEARC1.DTP8 GRfC

-. o~¢ 3 REMOVED548 3*

5 CONTROLSIIPLT SETDPAE STI 2213 21IREMOVED

7 4 9 D

6-C) DETAIL LEFT HANISOVsowl c*) DETAIL rnGHTIIANO(oPPosITE PUR- I SAR Appendix 3-77 Rev'2, July23, 2015 I  :

&L. I Is*.ee 2 ZI- 2 i 1 Seib

/ 0 0 Z

.010 I.0fl J

/-> 040045 I/ .004 20 4( 2 260

.945 124 20.,77.1 701 2 1.315 0* DETAIL 2x 5.

//I *[

I nlnl l 00.T 34 00270 F OX.255 fo 20.25045 - '2~I. _______ I 40,2.010 0)DETAIL PUR-i SAR Appendix 1-70 Rev 2, July23, 2015

a

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f I R

V I v

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  • 2 I

t i

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- .355 AL (TOP) (BOTTOM}

EPARALLEL WITHIN.005 SEC*lON A-A

-11 ISOMETRIC SCALE:

NONE REF*ERECE ONL C

B A

) DETAIL/A SCALE:111 OUR-I OAR Appendix 3-79 Rev 2, July 23, 2015 ROTED EA3EE OE 6346 DOJMF3 00S~ 6 0f l 0I

  • . '"PR I ' i2. . ..

/ I::) .Z, Z

O "7 'S 55 ',, A 5-1 11111 7 NOTES: LL1LLLIZLIJREVXTATU 12~ ~ F

1. REMOVE Alt BURRS ANDSHARP EDGES.

ADDED SREVISEDSHEET TITLE; 2REVISED

& 3;ADDED ITEM ITEM 2:

3;ADDED NOTEA; 1/TAX?7

2. PROCURE, AND WNSPECT FABRICATE, PERSPECIFICATION SPC-3BZ. SEEDAR-SSBA4VX
3. WELD A PERSPECIFICATION ALLCORNER ANDFILLET SPC-3B2APPENDIX

.230UNLESS RADII BUSINGITEM OTHERWISE 8 (WELD NOTED.

FILLERMETALI. TOTALLY REVISED FROMDETAIL ITEM3, REMOVED SHEET2CREMOVE U.ADDED MOTE RADIUJS D CHAMFER DIMENSION S.SEEDAR-D14751 TO 440 AlS S. REMOVED ATOLERANCE:

3SEEECX-551R72 T/2/07 ID ADDED NOTE7.

A. IIAXCERNE I IR H NID FCNTIE0UE SY53.A-

-1 ISOMETRIC REFERENCEONLY SCALE: NOSE SE

.... L(>-* //-'* SEEDETAIL (SSSTU =I 3 SEEDETAIL E1I~ C

.IS .13..B I2.i 131 SR SC WELSFILLER METAL ER 4543 AWSA5.10 8_

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SLUSC -V MESH TN16 B6MESHPERNACH, B

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-T I/ST SC

-3

-2

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NA'TURI.PXGCEEAIB( I7512 XEHRANNE I PM ISUST IA EBBIa 5y T. AINMOLA REOUENTRH.

II*.a AXSIVIN D. MORRELL PURDUE UNIVERISITY gqITIRA*1 DRAWN AS.LHA TESTRESEARCH ANDTRAINING REACTOR O) DETAIL SCALE:1It 0DETAIL SCALE;lit 1*,* IcL t oEAV I SOURCEDRIVE NOZZLEASSEMBLY ANDSOURCEDRT/ETOP

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  • 2.52 SCALE:NONE
  • , 01 [ _" '

T2 2 ~

....

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.- 2X .219

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OXROE' C) ETAILL/\ A PUJR-I 04AR Appendix 3-81 Rev 2. July 23. 2015 SSF41.NOTED A8*'EET2

'5 03 2+

d / 0 q. Z

7 4 1 7 N17I II D

-1 ISOMETRIC SCALE:

NONE REFERENCEONLY B

0 DETAIL/A A

PUR- 1 SAR Appendix 3-82 Rev 2, July 23, 2015 D OJMF3 nolAn owci-635467a 4 ti / b 9 4 ..... I1 0-- 9

/ b b 4 1 so*

NOTES:

1. REMOVE ALLBURRSANDSI-ARPEDGES.

A 2. PROCURE,FABRICATE.

AILLCORNER ANDINSPECT ANDFILLET RADIID030 PERSPECIFICATION UNLESSOTHERWISE SPC-382.

NOTED.

4. REMOVED

,/ TOLERANCE:

.0031 ABA5

-1 ISOMETRIC REFERENCE ONLY SCALENONE o DETAILA PUR-l SAR Appendix 3-83 Rev 2, Jully23, 2015

7 ,1, A, 0 O "t 0

D UNF.-3B 7.375 X1)4-28 (TOP) (BOTTOM)

-2 ISOMETRIC SCALE:

NONE

-- 2X.07 B

C) DETAIL SCALE: 11 A\

A PUR- I SAP. Appendix 3-84 Rev 2, July 23, 2015 O OJMF3 owe.635468 4

- a T -, "r I-r* ' NOTED 8A~EE EEl 2 I 0 *D 2 I 1 S08183