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=Text=
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          .            ,
                               "                                                      1 Washington 1                                              StateUniversity w
                               "                                                      1 Washington 1                                              StateUniversity w
Nuclear Radiation Center, Pullman, Washington 99164 1300 / 509-335-8641
Nuclear Radiation Center, Pullman, Washington 99164 1300 / 509-335-8641
[
[
..'
f' ' r LNovember 21,:1989 l
f' ' r
                                                                            '
                '
                    ,
LNovember 21,:1989 l
Documentation Control Desk-U.S. Nuclear. Regulatory Commission
Documentation Control Desk-U.S. Nuclear. Regulatory Commission
;,                                      ,        Washington, DC 20555
;,                                      ,        Washington, DC 20555
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                         "                    t cations to facility license R-76, the attached Safety Analysis is herewith
                         "                    t cations to facility license R-76, the attached Safety Analysis is herewith
{                                                submitted..
{                                                submitted..
            ,
Sinberely,
Sinberely,
: l.                                            Wf.W LW. E. Wilson
: l.                                            Wf.W LW. E. Wilson l Associate Director
              '
l Associate Director
                  *
                                                 ' Enclosures : ' (4) .
                                                 ' Enclosures : ' (4) .
WEW: crc'-
WEW: crc'-
    "
_
                          ,
'
            .
      .
!
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!n u
p?
p?
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0 Y
0 Y
:                8
:                8
                                  <
                                                               $00?($$ff g.
                                                               $00?($$ff g.
n                              -          --                . :- _
n                              -          --                . :- _
                                                                                        -


         #p** **euq UNITED STATES
         #p** **euq UNITED STATES jyqf.%  g              NUCLEAR REGULATORY COMMISSION WASHINGT ON, D. C,20555
      .!
           %                                          October 26, 1989 Docket No. 50-27 n
      ;; .
jyqf.%  g              NUCLEAR REGULATORY COMMISSION WASHINGT ON, D. C,20555
           %                                          October 26, 1989
  !
Docket No. 50-27 n
S 3          Mr. W. E. Wilson Associate Director Nuclear Raciation Center Washington State University Pullman, Washington 99164-1300
S 3          Mr. W. E. Wilson Associate Director Nuclear Raciation Center Washington State University Pullman, Washington 99164-1300


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==SUBJECT:==
==SUBJECT:==
REQUEST FOR ADDITIONAL INFORMATION We are continuing our review of the documentation submitted in support of your application for amendment of Operating License No. R-76 for the Washington State University Modified TRIGA Research Reactor that was submitted on September 6, 1989. During our review of your submittal, questions have arisen for which we require acditional information and clar111 cation. . Please provide a r6sponse to the enclosed Request for Additional Information within 45 days of the date of this letter. Following receipt of the additional information,
REQUEST FOR ADDITIONAL INFORMATION We are continuing our review of the documentation submitted in support of your application for amendment of Operating License No. R-76 for the Washington State University Modified TRIGA Research Reactor that was submitted on September 6, 1989. During our review of your submittal, questions have arisen for which we require acditional information and clar111 cation. . Please provide a r6sponse to the enclosed Request for Additional Information within 45 days of the date of this letter. Following receipt of the additional information, we will continue our evaluation of your amendment application. If you have any questions regarding this review, please contact me at (301) 492-1121.
'
we will continue our evaluation of your amendment application. If you have any questions regarding this review, please contact me at (301) 492-1121.
             -The reporting and/or recordkeeping requirenants contained in this letter                              i af fect fewer than ten respondents; therefore, OMC clearance is ~not reouireo                        ;
             -The reporting and/or recordkeeping requirenants contained in this letter                              i af fect fewer than ten respondents; therefore, OMC clearance is ~not reouireo                        ;
under P. L. 96-511.
under P. L. 96-511.
                                                                                                               ,q. .
                                                                                                               ,q. .
,                                                            Sincerely.                                    .
,                                                            Sincerely.                                    .
                                                                                                              '
                                                                                                                  ;
ghfdth            (Gu      ,
ghfdth            (Gu      ,
Alexander Adams, Jr., Pr ect Manager Non-Power Reactor, Detshatssioning and Environmental Project Directorate Division of Reactor Projects - Ill,                  ;
Alexander Adams, Jr., Pr ect Manager Non-Power Reactor, Detshatssioning and Environmental Project Directorate Division of Reactor Projects - Ill,                  ;
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==Enclosure:==
==Enclosure:==
                                                                                            !
    "
As stated ccw/ enclosure:
As stated ccw/ enclosure:
See next page
See next page
/
/
!
                                                                                                                  -
l:                                                                                                                ;
l:                                                                                                                ;
;                                                                                                                  e
;                                                                                                                  e
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in        ,
in        ,
c;      ''~,;
c;      ''~,;
                      -
ot        .,;                                                                                        ;
ot        .,;                                                                                        ;
                                                                                                        ,
ENCLOSURE      <
ENCLOSURE      <
:
:
                                                                                                        '
RE00EST FOR ADDITIONAL INFORMATION WASHINGTON STATE UNIVERSITY DOCKET NO. 50-27
RE00EST FOR ADDITIONAL INFORMATION WASHINGTON STATE UNIVERSITY DOCKET NO. 50-27
                                                                                                        .
                                                                                                        .
                   -1. Please provide a safety analysis to support your request for amendment.
                   -1. Please provide a safety analysis to support your request for amendment.
in your safety analysis make a determination if the amendment' involves a    ,
in your safety analysis make a determination if the amendment' involves a    ,
                                                                                                        !
   -".                    significant hazards consideration. Provice information to justify changing pulse mook limits from reactivity irsertion to peak fuel temperature. What uncertainties are involved in the calculation of the
   -".                    significant hazards consideration. Provice information to justify changing pulse mook limits from reactivity irsertion to peak fuel
              ,
temperature. What uncertainties are involved in the calculation of the
                         . maximum reactivity insertion? What is the maxiir.um allowable time span allowed between calculations?
                         . maximum reactivity insertion? What is the maxiir.um allowable time span allowed between calculations?
                                                                                                    .
l
l
  ..
                                                                                                      .


b        _
b        _
                                                                                                    ,
: u.        .                                                                                      l
: u.        .                                                                                      l
    ,. .      .
               '    NEW SAFETY ANALYSIS FOR PULSING OF THE WSU MODIFIED TRIGA e
               '    NEW SAFETY ANALYSIS FOR PULSING OF THE WSU MODIFIED TRIGA e
REACTOR - November. 1989 Introduction                                                                      >
REACTOR - November. 1989 Introduction                                                                      >
                       'The present Technical Specifications for the WSU Triga reactor were approved on August 11, 1982, as part of the                          <
                       'The present Technical Specifications for the WSU Triga reactor were approved on August 11, 1982, as part of the                          <
: relicensing          process. Section  3.3    of        these      Technical s
: relicensing          process. Section  3.3    of        these      Technical s
Specifications established a pulsing limit of $2.50 for the WSU reactor based on the information that was available at the time    the proposed Technical        Specifications were              submitted during the relicensing process.          Subsequent to the application for renewal of the reactor facility license,                      a FLIP fuel damage problem occurred at the Texas A&M TRIGA reactor.                          On September 27,          1976 (1), Texas A&M University discovered the fact that some of the FLIP fuel rods adjacent to the transient rod were severely damaged in the form of swollen cladding and bent and bowed fuel rods. The damage was limited to the four fuel rods surrounding the transient rod.                The exact cause of
Specifications established a pulsing limit of $2.50 for the WSU reactor based on the information that was available at the time    the proposed Technical        Specifications were              submitted during the relicensing process.          Subsequent to the application for renewal of the reactor facility license,                      a FLIP fuel damage problem occurred at the Texas A&M TRIGA reactor.                          On September 27,          1976 (1), Texas A&M University discovered the fact that some of the FLIP fuel rods adjacent to the transient rod were severely damaged in the form of swollen cladding and bent and bowed fuel rods. The damage was limited to the four fuel rods surrounding the transient rod.                The exact cause of the    FLIP fuel        damage was not apparent in            1976 since      no existing safety limit had been exceeded.                      The cause of the damage has only more recently been determined af ter detailed i
                                                                                                    ,
the    FLIP fuel        damage was not apparent in            1976 since      no existing safety limit had been exceeded.                      The cause of the damage has only more recently been determined af ter detailed i
metalurgical examination of sections taken from the damaged FLIP fuel.          The WSU modified TRIGA reactor is similar to the Texas A& M reactor and is also fueled with a mixture of                                i Standard and FLIP fuel'.          Accordingly, in order to preclude the              l possibility of a similar FLIP fuel damage problem occurring at WSU, WSU administrative 1y limited all pulsing to $2.00 after the problem at Texas A&M became known.
metalurgical examination of sections taken from the damaged FLIP fuel.          The WSU modified TRIGA reactor is similar to the Texas A& M reactor and is also fueled with a mixture of                                i Standard and FLIP fuel'.          Accordingly, in order to preclude the              l possibility of a similar FLIP fuel damage problem occurring at WSU, WSU administrative 1y limited all pulsing to $2.00 after the problem at Texas A&M became known.
__      __ _ _ _
                                                                    - - _
_        _ __


Y
Y l
  .    ..
l
      .    ,,
                  *
: i. -    ,.
: i. -    ,.
Cause of the FLIP Fuel Damace in the Texas A&M Reactor Extensive cooperative research by the people at Texas A&M, Argonne National Lab West and General Atomics led to a resolution of the damage mechanism as described below: (2)
Cause of the FLIP Fuel Damace in the Texas A&M Reactor Extensive cooperative research by the people at Texas A&M, Argonne National Lab West and General Atomics led to a resolution of the damage mechanism as described below: (2)
  ,
TRIGA fuel    is fabricated with a nominal        hydrogen to l
TRIGA fuel    is fabricated with a nominal        hydrogen to l
i zirconium ratio of 1. 6 for FLIP fuel and 1.65 for Standard.
i zirconium ratio of 1. 6 for FLIP fuel and 1.65 for Standard.
This yields delta phase zirconium hydride which has a high              l
This yields delta phase zirconium hydride which has a high              l creep strength and undergoes no phase changes at temperatures over 1000 0C (3).        However, after extensive steady ' state      J operation at 1 Mw,      the high temperature gradient        created during steady . state operation will cause the hydrogen to redistribute from the central high temperature regions of the fuel' to the cooler outer regions. When the fuel is pulsed, the instantaneous temperature distribution is such that the highest values occur at the surface of the element and the lowest values occur at the center.          The higher temperatures in the outer regions occur in fuel with a hydrogen to zirconium ratio that has now substantially increased above the nominal value. This produces hydrogen gas pressures considerably in excess of that expected for ZrH              (2) l .6'
              .
creep strength and undergoes no phase changes at temperatures over 1000 0C (3).        However, after extensive steady ' state      J operation at 1 Mw,      the high temperature gradient        created during steady . state operation will cause the hydrogen to redistribute from the central high temperature regions of the fuel' to the cooler outer regions. When the fuel is pulsed, the instantaneous temperature distribution is such that the highest values occur at the surface of the element and the lowest values occur at the center.          The higher temperatures in the outer regions occur in fuel with a hydrogen to zirconium ratio that has now substantially increased above the nominal value. This produces hydrogen gas pressures considerably in excess of that expected for ZrH              (2) l .6'
: j.                    Figure 1 on the next page of this report shows the relationship between maximum fuel temperature during pulsing 1
: j.                    Figure 1 on the next page of this report shows the relationship between maximum fuel temperature during pulsing 1
versus FLIP fuel damage that was observed in the Texas A&M
versus FLIP fuel damage that was observed in the Texas A&M TRIGA reactor.      A detailed analysis of the failed FLIP fuel and extensive consideration of the properties of zirconium hydride fuel (4) by General Atomics established the fact (2)
                              '
TRIGA reactor.      A detailed analysis of the failed FLIP fuel and extensive consideration of the properties of zirconium hydride fuel (4) by General Atomics established the fact (2)
                                                          .-.


{{         .1                                                                                !
((         .1                                                                                !
      ...
            .    ,                                                                          ,
                                                                                               +
                                                                                               +
  .-          ,
1 FUEL DAMAGE VERSUS FUEL TEMPERATURE IN F N'5 ^ 5 M TRIGA REACTOR, 1976 500  -
1
                ,
                *
            .                                                                          .
                                                                                              .
FUEL DAMAGE VERSUS FUEL TEMPERATURE IN F N'5 ^ 5 M TRIGA REACTOR, 1976
                                                                                          .
                                                                                              &
500  -
                                                                                            .
400 e                              I                            .
400 e                              I                            .
CNSC CF    l CAMAGE N:
CNSC CF    l CAMAGE N:
Line 186: Line 108:
                       $ 300 -                                %_,
                       $ 300 -                                %_,
t y
t y
G
G 01                                      ,,      o ,
                    ,
01                                      ,,      o ,
e                                        ,.
e                                        ,.
g ace -
g ace -
I l
I l
I 83C*    I  "    %$ 3R DAMAcgp 10 0 -      CAMAGE FRr                      ' MC3I TEMFERATtjj          f L:MIT o
I 83C*    I  "    %$ 3R DAMAcgp 10 0 -      CAMAGE FRr                      ' MC3I TEMFERATtjj          f L:MIT o
                          .
i                '              '
i                '              '
O 7C0              800            900            ICCO
O 7C0              800            900            ICCO TEMPERATURE (*C)
      -
TEMPERATURE (*C)
Figure 1
Figure 1
                                    ,
                        .


>
that the - onset of FLIP damage occurred at a temperature of about;8740 C 'during pulsing. That is, in a FLIP fueled core with extensive steady state operation, if the temperature of a FLIP fuel rod during subsequent pulsing exceeds 874 0C, FLIP fuel rod damage is very likely to occur in that rod.
  .    .
    ..
that the - onset of FLIP damage occurred at a temperature of about;8740 C 'during pulsing. That is, in a FLIP fueled core
                                                                                  >
with extensive steady state operation, if the temperature of a FLIP fuel rod during subsequent pulsing exceeds 874 0C, FLIP fuel rod damage is very likely to occur in that rod.
The failure mechanism is associated with the fact that 0
The failure mechanism is associated with the fact that 0
above 874    C the hydrogen disassociation pressure in a FLIP          '
above 874    C the hydrogen disassociation pressure in a FLIP          '
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These microscopic holes . grow larger and proliferate with each pulse that produces a FLIP fuel rod temperature above 874 0C.
These microscopic holes . grow larger and proliferate with each pulse that produces a FLIP fuel rod temperature above 874 0C.
The microscopic holes eventually caused the FLIP fuel rod material to fracture, swell and distort.                The damaged FLIP fuel rod material, in turn, created distorted, bent and bowed FLIP fuel rods.
The microscopic holes eventually caused the FLIP fuel rod material to fracture, swell and distort.                The damaged FLIP fuel rod material, in turn, created distorted, bent and bowed FLIP fuel rods.
Fuel TemDerature Limit for Pulsina of a - FLIP Fueled TRIGA Reactp,I Extensive studies conducted in the aftermath of the FLIP fuel damage problem that occurred at Texas A&M as discussed in the previous section of this report revealed the fact that FLIP fuel damage occurs when the FLIP fuel temperature exceeds 8740 C during pulsing. The FLIP fuel damage was discovered at
Fuel TemDerature Limit for Pulsina of a - FLIP Fueled TRIGA Reactp,I Extensive studies conducted in the aftermath of the FLIP fuel damage problem that occurred at Texas A&M as discussed in the previous section of this report revealed the fact that FLIP fuel damage occurs when the FLIP fuel temperature exceeds 8740 C during pulsing. The FLIP fuel damage was discovered at Texas    A&M  before  a  cladding      failure      occurred  with  an associated release of fission products.            However, if the FLIP fuel damage had not been discovered, a cladding failure would l
                                                                                    ,
Texas    A&M  before  a  cladding      failure      occurred  with  an associated release of fission products.            However, if the FLIP fuel damage had not been discovered, a cladding failure would l
l l
l l
l l
l l
l
l
                                              . .      - . -


F                                            ,                                                                      ;
F                                            ,                                                                      ;
& :;-        ,
r-                                                                                      >
r-                                                                                      >
t/l          9, '
t/l          9, '
                                                                                                                    ,
1 i
1 i
        .            ..
e            10,000.    -
              *
                        ..
* e            10,000.    -
a 1
a 1
                                           ~                                                  '
                                           ~                                                  '
                                                                                                                        ,,
1 l
1
i                                    .                                                                            ;
                                          -
i 1000.
                                                                                                                      .
l i                                    .                                                                            ;
                                                                                                                        ,
i
                                          .
                                                                                                                      .
                                          -
1000.
                                          .
  '                                      .
                              -
m                                                                                        '
m                                                                                        '
A
A I
                                          .
w                                                                                        ,
I w                                                                                        ,
5 m
5 m
m          -                                                                            ,
m          -                                                                            ,
Line 263: Line 153:
                                         =
                                         =
                               .D                                                                          ,
                               .D                                                                          ,
                                                                                                                  ,
1 E'  .
1
                            .
E'  .
                                          ,,
a:
a:
                               .m.
                               .m.
                                                                                                                      '
a m          .
a
                                .
m          .
cr w
cr w
                                          -
10.
10.
                                           ~
                                           ~
      -
l J
l J
                                           .                                                                          i
                                           .                                                                          i i
'
d i,o                                                                              i 700      800      300        1000    1100    1200        1300    1400    l ZrH        M E M RE  'C l.65 1
i d
Equilibrium hydrogen pressure over ZrH 1.65    versus temperature Figure 2 7
                                                    ,        ,          .        .      ,          ,
i,o                                                                              i 700      800      300        1000    1100    1200        1300    1400    l ZrH        M E M RE  'C l.65
                                                                                                                      ,
1
                                            -
Equilibrium hydrogen pressure over ZrH 1.65    versus temperature Figure 2
          ,
7


          ,
i
i
       *T probably have occurred eventually which is a much more-severe          ;
       *T probably have occurred eventually which is a much more-severe          ;
Line 306: Line 178:
l I          '
l I          '
l -- .
l -- .
,
: p.                  ,
: p.                  ,
  '
         .          .                      Peak Pcwer and Energy Release vs. Reactivity Insertion
                .                                                                                                          .
         .          .                      Peak Pcwer and Energy
                          ,
                '
Release vs. Reactivity Insertion
                     -                                                                                      ~
                     -                                                                                      ~
2000                                Core 32A
2000                                Core 32A
                                                                                                        '
             ,1750  -                                                                                      -
             ,1750  -                                                                                      -
                                                                                                            -
1500, -
1500, -
                                                                                                           .                -r c'
                                                                                                           .                -r c'
1250:-                                                                                        - 25  4 4          l x
1250:-                                                                                        - 25  4 4          l x
2                                                                                                              a
2                                                                                                              a 5                                                                                                            N          '
    -                                                                                                              -
      -.                                                                                                            .
5                                                                                                            N          '
     .3        _100:* -                                                                                        - 20  -          -
     .3        _100:* -                                                                                        - 20  -          -
: c.                                                                                                            -
: c.                                                                                                            -
Line 333: Line 194:
: c.                                                                                                            n
: c.                                                                                                            n
               - 750'-                                                /                                      - 15    . ,
               - 750'-                                                /                                      - 15    . ,
                                                                                                                              .
                                                                                                                              '
500  -
500  -
                                                          .
                                                                                                               - 10 r.
                                                                                                               - 10
250                                                                                            5 1.25        1.50        1.75        2.00                          2.25    2.50 l
          .
                            .
                                                            .
r.
          .
                        -        '
                                                                                                              -
250                                                                                            5
                                ,            .            ,          ,                            ,
,
1.25        1.50        1.75        2.00                          2.25    2.50 l
Reactivity Inserpion ($)
Reactivity Inserpion ($)
                                    ,
Figure 3
Figure 3
  -
                                                                          . . - . . _ _ _ , _ _ _ _


                                                                                                                                                                          -      - --
   .g.. .,
   .g.. .,
                                                                                                                                                                                        .,
                                                                                                                                                                                            '
N~
N~
  -                > .
   .'{ ' k.:          . .
   .'{ ' k.:          . .
                      '' '
5
5
     '^- ,' q                                  >
     '^- ,' q                                  >
                .
  .                        .
b',
b',
a, *
a,
  ,.
* WSU TRIGA CORE 32A 4
                                                                                                  ,
                  ,
                                                                                                                                                                                          ;
WSU TRIGA CORE 32A
                                '.
                                                                                                                                                                                          .
4
                        '
p                                                                                                                                                                                      .i
p                                                                                                                                                                                      .i
:4
:4
      ,
                 - '-              IC gWww
                 - '-              IC gWww
                                       .mc. P g,              -
                                       .mc. P g,              -
8-
8-
                                             ~i
                                             ~i t-p                                                                                                                                          ,
                                                                                                                                                                                          ,
t-p                                                                                                                                          ,
6-4 5
6-4 5
4-l-
4-l-
Line 393: Line 220:
r                  I
r                  I
                               <              2-
                               <              2-
                              >
                              --                                                                                                                                                            ,
                              <        .
: e.          . s.1 -
: e.          . s.1 -
                           -W
                           -W
Line 401: Line 225:
C- = l .,. w, ,,.  ,
C- = l .,. w, ,,.  ,
W                9-
W                9-
                            >
                           . -              e-' t i
                           . -              e-' t i
                           - C-              I I c                6-I x                5-
                           - C-              I I c                6-I x                5-l:
                            <                                                                        -
l:
                           -W C.,
                           -W C.,
4 l-
4 l-3-
; ..
L i
-
3-L i
2.sll-2-                                                                                                                                            '
2.sll-2-                                                                                                                                            '
i t.5    -
i t.5    -
!
E ICC t  t  t t          t        t  f f !!                      t              I  t t        t        t tii 1
E
'
ICC t  t  t t          t        t  f f !!                      t              I  t t        t        t tii 1
                                                                 !.4 2 2.5 3        4 56743                              1.5                22.53        4 56739
                                                                 !.4 2 2.5 3        4 56743                              1.5                22.53        4 56739
                                                                                   ,                    10 10 0
                                                                                   ,                    10 10 0
            -
                                               ,            FULL W!CTH AT HAL: FEAK PCWE?, MILL!SECONCS Figure 4 a
                                               ,            FULL W!CTH AT HAL: FEAK PCWE?, MILL!SECONCS
;
Figure 4 a
!
,,            ,                .                  _ _ . . _          _    _ .. _ . . . . _ . .        . _ . . . . . _ . _ _ . . . . . . _  _    . _ . . . _ . .    -    - _      _


                     =                                  .y
                     =                                  .y 77
                  -
                              -
77
        .,.
                                                   ' TABLE-1 0 2. '      .
                                                   ' TABLE-1 0 2. '      .
      '
CORE 32A PULSING CHARACTERISTICS XL =' 24.usec.            Tc = -0.0145 $/*C N = 102 TRIGA! rods      To = 35'C-Reactivity.            max;        Tp                E                E7cm
:
        "'
CORE 32A PULSING CHARACTERISTICS XL =' 24.usec.            Tc = -0.0145 $/*C N = 102 TRIGA! rods      To = 35'C-
  .
  ".
Reactivity.            max;        Tp                E                E7cm
($)        (Megawatts)        (*C)        (Megawatt-Sec)      (Watt-Sec/cc) 1.25-              51            69-            5.9                  159 1.50              205          103-            9.0                  243 1.75              467          136            12.2                  330 i
($)        (Megawatts)        (*C)        (Megawatt-Sec)      (Watt-Sec/cc) 1.25-              51            69-            5.9                  159 1.50              205          103-            9.0                  243 1.75              467          136            12.2                  330 i
12.00              839          168            15.6                  420
12.00              839          168            15.6                  420 2.25-        -1324            200            19.0                  513 2.5C          ~ 1926          232            22.5                  609 2.75            2648          263            26.2                  708
                                                                                                  !
2.25-        -1324            200            19.0                  513
    '
2.5C          ~ 1926          232            22.5                  609 2.75            2648          263            26.2                  708
                         $      = reactivity inserted in dollars I
                         $      = reactivity inserted in dollars I
lGi/    = average peak core temperature in,'C E      = energy released in megawatt-sec 5/cm = average energy per em        3 of fuel in watt-sec/cm 3
lGi/    = average peak core temperature in,'C E      = energy released in megawatt-sec 5/cm = average energy per em        3 of fuel in watt-sec/cm 3
                                  '
                                                                                                  !
                                                                                                 .i 1
                                                                                                 .i 1
:l
:l
Line 456: Line 251:
i l
i l
l 1
l 1
                                                                                                  !
1
1
                 ~
                 ~


k p    .                                                                        .:
k p    .                                                                        .:
      *
           ;      Watts-sec = 2.08 x 10~ 3 ( AT) 2 - 2. 09 A T - 53. 6 cm'                                                          ,
           ;      Watts-sec = 2.08 x 10~ 3 ( AT) 2 - 2. 09 A T - 53. 6
        '
cm'                                                          ,
i
i
           .where - 6 T is the average core temperature rise in degrees
           .where - 6 T is the average core temperature rise in degrees centigrade. . Using the limiting fuel temperature of 830 C established in    the previous section of this report which corresponds- to a AT of 795 0 C above ambient, we calculate a i
                                                                                    !
maximum' allowable power density during a pulse of 2923 watts-sec/cm3 . This value represents the worst case condition and        i thus we must make 'a correction for heterogeneous effects in.
centigrade. . Using the limiting fuel temperature of 830 C established in    the previous section of this report which corresponds- to a AT of 795 0 C above ambient, we calculate a i
maximum' allowable power density during a pulse of 2923 watts-
                                                                                    ,
sec/cm3 . This value represents the worst case condition and        i thus we must make 'a correction for heterogeneous effects in.
the real core.      The total ' peaking factor for the WSU TRIGA reactor calculates cut to be 5.91 using the data developed at General Atomics (6).      That is, the ratio between the average temperature in the core ' to the highest temperature point in          i the core due to heterogeneous effects is 5.91.              Thus, the average power density in the core should not exceed 2923/5.91.
the real core.      The total ' peaking factor for the WSU TRIGA reactor calculates cut to be 5.91 using the data developed at General Atomics (6).      That is, the ratio between the average temperature in the core ' to the highest temperature point in          i the core due to heterogeneous effects is 5.91.              Thus, the average power density in the core should not exceed 2923/5.91.
           =
           =
Line 484: Line 271:


k in                      ,
k in                      ,
                            ..
                                    ,
                                  .
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             / 'r ..' s ';
                               -'    s r.-
                               -'    s r.-
  -
w.,
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TEXAS _Afd!h!IXED CORE III A
TEXAS _Afd!h!IXED CORE III A t                  .
        .
t                  .
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                                          -
O
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                                                                                                          ,
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* W                                        -
* W                                        -
                                           .E 300 -
                                           .E 300 -
                                          >
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                                         .W
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W Q.
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830 C_
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W                                                            -.
W                                                            -.
W<t                                                            1
W<t                                                            1
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                                         -
                                         -
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* 3CC -
:'
                                         .U a
                                         .U a
                                        -<
                                         ; u.
                                         ; u.
                                                                                                            ,
                                                          ' ,      ,          ,  '
                                               -750                        ,
                                               -750                        ,
                                                                                       '  '  i  '
                                                                                       '  '  i  '
2.'*' *^      2:28
2.'*' *^      2:28 2.50              'O        j L-
.
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:                                                            REDITY INSERTICN (s) u                  ,
:                                                            REDITY INSERTICN (s) u                  ,
1 la 1.
1 la 1.
Figure 5
Figure 5 5
                                                                                                    .
a l
5 a
l
                                                                                            .
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1 i .
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                                                                      ,
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m.
m.
                                                                                           )
                                                                                           )
  '- . , ,    ,
                ;                                                                        '
1 Hazards Evaluatiori of Present WSU Reactor Pulsino Litgit Retaining the present . technical specification limit for          l the WSU TRIGA reactor with a pulsing          limit of    $2.50  is
1 Hazards Evaluatiori of Present WSU Reactor Pulsino Litgit Retaining the present . technical specification limit for          l the WSU TRIGA reactor with a pulsing          limit of    $2.50  is
                 . inconsistent  with  reactor  safety  methodology    since  the analysis upon which that limit was set now turns out to be less than conservative. The most likely result from pulsing the WSU TRIGA reactor at the $2.50 level would be a FLIP fuel
                 . inconsistent  with  reactor  safety  methodology    since  the analysis upon which that limit was set now turns out to be less than conservative. The most likely result from pulsing the WSU TRIGA reactor at the $2.50 level would be a FLIP fuel
                 -problem like the one that occurred at Texas A&M and the
                 -problem like the one that occurred at Texas A&M and the possibility of a fuel cladding rupture with the release of fission products into the reactor pool room.      The Design Basis Accident in the SAR for the WSU TRIGA reactor is the failure of one fuel rod and the release of the contained fission products into the pool room.        The SAR analysis demonstrates that    this  postulated  accident    would  not    constitute. a significant safety hazard to the general public.            Thus, the present non-conservative      pulsing  limit  of  $2.50  does  not involve a significant safety hazard.
                                                                                        ,
The requested change in the technical specification for the WSU TRIGA reactor from the present $2.50 pulsing limit to one related to the maximum allowable fuel temperature during a
possibility of a fuel cladding rupture with the release of fission products into the reactor pool room.      The Design Basis Accident in the SAR for the WSU TRIGA reactor is the failure of one fuel rod and the release of the contained fission products into the pool room.        The SAR analysis demonstrates that    this  postulated  accident    would  not    constitute. a significant safety hazard to the general public.            Thus, the present non-conservative      pulsing  limit  of  $2.50  does  not involve a significant safety hazard.
The requested change in the technical specification for
!
the WSU TRIGA reactor from the present $2.50 pulsing limit to one related to the maximum allowable fuel temperature during a
                 -pulse    does  not    involve  a    significant    safety    hazard consideration on the basis of the considerations listed above.
                 -pulse    does  not    involve  a    significant    safety    hazard consideration on the basis of the considerations listed above.
The change involves shifting to a more conservative limit based on the results of the analysis of the cause of the FLIP fuel damage problem that occurred at Texas A&M.        The requested change is also consistent with the technical specification
The change involves shifting to a more conservative limit based on the results of the analysis of the cause of the FLIP fuel damage problem that occurred at Texas A&M.        The requested change is also consistent with the technical specification
Line 565: Line 316:
fh          ,                                                                      ,
fh          ,                                                                      ,
l
l
    .
   ~
   ~
       't .,
       't .,
            -"-
                 ' established for the Texas A &M reactor as a result of the        ,
                 ' established for the Texas A &M reactor as a result of the        ,
                             ~
                             ~
FLIP fuel damage problem that occurred at that facility.
FLIP fuel damage problem that occurred at that facility.
                                                                      .
Uncertainties in the Pulsina Limit Based on Fuel Temoerature The. primary uncertainties associated with the calculation of  the  maximum  allowable  polse  insertion  based  on  fuel temperature by the method outlined in this report fall- into      '
Uncertainties in the Pulsina Limit Based on Fuel Temoerature The. primary uncertainties associated with the calculation of  the  maximum  allowable  polse  insertion  based  on  fuel temperature by the method outlined in this report fall- into      '
two areas.      These areas are 1) the accuracy of the Fuchs-Nordheim pulsing model, and 2) calculation of the average core temperature and the core temperature peaking factor.          The Fuchs-Nordheim variable heat capacity mode is known to be conservative - (7) and thus the actual average power density will be slightly less than predicted by this model.            The conservative nature of this model primarily stems from the fact that the model assumes a constant negative temperature coefficient whereas the real temperature coefficient of.a FLIP fueled reactor increases with increasing temperature. At WSU,
two areas.      These areas are 1) the accuracy of the Fuchs-Nordheim pulsing model, and 2) calculation of the average core temperature and the core temperature peaking factor.          The Fuchs-Nordheim variable heat capacity mode is known to be conservative - (7) and thus the actual average power density will be slightly less than predicted by this model.            The conservative nature of this model primarily stems from the fact that the model assumes a constant negative temperature coefficient whereas the real temperature coefficient of.a FLIP fueled reactor increases with increasing temperature. At WSU, core temperature calculations,are based on the fuel rod power density as calculated using the two dimensional EXTERMINATOR-2 diffusion code. (8) This code has been used at WSU and Texas A&M for a number of years and has been found to be quite accurate. The peaking factors used to make the average to peak-temperature calculation are a small modification of those reported in report GA-9350 (5) that are as accurate as one can calculate. The small modification used at WSU increases the total    peaking  factor  and  thus  makes  the  analysis  more
                                                                                  ,
core temperature calculations,are based on the fuel rod power density as calculated using the two dimensional EXTERMINATOR-2 diffusion code. (8) This code has been used at WSU and Texas A&M for a number of years and has been found to be quite accurate. The peaking factors used to make the average to peak-temperature calculation are a small modification of those reported in report GA-9350 (5) that are as accurate as one can calculate. The small modification used at WSU increases the total    peaking  factor  and  thus  makes  the  analysis  more


         = ..
         = ..
,,--
     .51 Iconsetvative. In general, all the uncertainties are such-that lead-to the setting of a conservative limit.
     .51
          -
Iconsetvative. In general, all the uncertainties are such-that lead-to the setting of a conservative limit.
Recommended Precuency of Pulsina Limit Evaluation The two. primary parameters that . cause a change in a core's performance that necessitate a recalculation of the temperature related pulsing limit are: 1)      core changes and-
Recommended Precuency of Pulsina Limit Evaluation The two. primary parameters that . cause a change in a core's performance that necessitate a recalculation of the temperature related pulsing limit are: 1)      core changes and-
: 2) fuel burnup. Accordingly, a new calculation must be made sach time the core is rearranged including just moving fuel rods around- in the core. Also, the temperature limit should be calculated annually to take into account the effects of burnup and' of the buildup of fission products in the core.
: 2) fuel burnup. Accordingly, a new calculation must be made sach time the core is rearranged including just moving fuel rods around- in the core. Also, the temperature limit should be calculated annually to take into account the effects of burnup and' of the buildup of fission products in the core.
Line 588: Line 331:
i
i
                                                                                 ?
                                                                                 ?
                                      .


_
{.' is 7
{.' is 7
i
i
  ,,5.,    .
  ,,5.,    .
            *'
        ,
N REFERENCES
N REFERENCES
                                                                                 )
                                                                                 )
: 1. . Status Report on Damaged FLIP Fuel During Operation of
: 1. . Status Report on Damaged FLIP Fuel During Operation of
                                                                                .
                       ~the NSCR at Texas A & .M University, Letter to the USAEC of November 1,      1976, from John  D. Ronald, Director, Texas A & M University, Nuclear Science      -3 Center.
                       ~the NSCR at Texas A & .M University, Letter to the USAEC of November 1,      1976, from John  D. Ronald, Director, Texas A & M University, Nuclear Science      -3 Center.
: 2. Supplement I to the 1979 Safety Analysis Report for the Texas A & M Nuclear. Science Center Reactor,- 30        ,
: 2. Supplement I to the 1979 Safety Analysis Report for the Texas A & M Nuclear. Science Center Reactor,- 30        ,

Latest revision as of 12:21, 27 February 2020

Forwards Safety Analysis Re Licensee 890906 Request to Modify License R-76,per NRC 891026 Request
ML19332C721
Person / Time
Site: Washington State University
Issue date: 11/21/1989
From: Wilson W
WASHINGTON STATE UNIV., PULLMAN, WA
To:
NRC OFFICE OF INFORMATION RESOURCES MANAGEMENT (IRM)
References
NUDOCS 8911280468
Download: ML19332C721 (16)


Text

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" 1 Washington 1 StateUniversity w

Nuclear Radiation Center, Pullman, Washington 99164 1300 / 509-335-8641

[

f' ' r LNovember 21,:1989 l

Documentation Control Desk-U.S. Nuclear. Regulatory Commission

, , Washington, DC 20555

.) Gentlemeni-

[

-In accordance with the letter of October 26, 1989 from Mr. A.: Adams to

(;;,. Mr. W.E.: Wilson requesting additional information on Washington State K :r University's request of: September 6,1989 to modify the technical'specifi-

!:n

" t cations to facility license R-76, the attached Safety Analysis is herewith

{ submitted..

Sinberely,

l. Wf.W LW. E. Wilson l Associate Director

' Enclosures : ' (4) .

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  1. p** **euq UNITED STATES jyqf.% g NUCLEAR REGULATORY COMMISSION WASHINGT ON, D. C,20555

% October 26, 1989 Docket No. 50-27 n

S 3 Mr. W. E. Wilson Associate Director Nuclear Raciation Center Washington State University Pullman, Washington 99164-1300

Dear Mr. Wilson:

SUBJECT:

REQUEST FOR ADDITIONAL INFORMATION We are continuing our review of the documentation submitted in support of your application for amendment of Operating License No. R-76 for the Washington State University Modified TRIGA Research Reactor that was submitted on September 6, 1989. During our review of your submittal, questions have arisen for which we require acditional information and clar111 cation. . Please provide a r6sponse to the enclosed Request for Additional Information within 45 days of the date of this letter. Following receipt of the additional information, we will continue our evaluation of your amendment application. If you have any questions regarding this review, please contact me at (301) 492-1121.

-The reporting and/or recordkeeping requirenants contained in this letter i af fect fewer than ten respondents; therefore, OMC clearance is ~not reouireo  ;

under P. L.96-511.

,q. .

, Sincerely. .

ghfdth (Gu ,

Alexander Adams, Jr., Pr ect Manager Non-Power Reactor, Detshatssioning and Environmental Project Directorate Division of Reactor Projects - Ill,  ;

IV, Y and Special Projects Office of Nuclear Reactor Regulation

Enclosure:

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ENCLOSURE <

RE00EST FOR ADDITIONAL INFORMATION WASHINGTON STATE UNIVERSITY DOCKET NO. 50-27

-1. Please provide a safety analysis to support your request for amendment.

in your safety analysis make a determination if the amendment' involves a ,

-". significant hazards consideration. Provice information to justify changing pulse mook limits from reactivity irsertion to peak fuel temperature. What uncertainties are involved in the calculation of the

. maximum reactivity insertion? What is the maxiir.um allowable time span allowed between calculations?

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' NEW SAFETY ANALYSIS FOR PULSING OF THE WSU MODIFIED TRIGA e

REACTOR - November. 1989 Introduction >

'The present Technical Specifications for the WSU Triga reactor were approved on August 11, 1982, as part of the <

relicensing process. Section 3.3 of these Technical s

Specifications established a pulsing limit of $2.50 for the WSU reactor based on the information that was available at the time the proposed Technical Specifications were submitted during the relicensing process. Subsequent to the application for renewal of the reactor facility license, a FLIP fuel damage problem occurred at the Texas A&M TRIGA reactor. On September 27, 1976 (1), Texas A&M University discovered the fact that some of the FLIP fuel rods adjacent to the transient rod were severely damaged in the form of swollen cladding and bent and bowed fuel rods. The damage was limited to the four fuel rods surrounding the transient rod. The exact cause of the FLIP fuel damage was not apparent in 1976 since no existing safety limit had been exceeded. The cause of the damage has only more recently been determined af ter detailed i

metalurgical examination of sections taken from the damaged FLIP fuel. The WSU modified TRIGA reactor is similar to the Texas A& M reactor and is also fueled with a mixture of i Standard and FLIP fuel'. Accordingly, in order to preclude the l possibility of a similar FLIP fuel damage problem occurring at WSU, WSU administrative 1y limited all pulsing to $2.00 after the problem at Texas A&M became known.

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Cause of the FLIP Fuel Damace in the Texas A&M Reactor Extensive cooperative research by the people at Texas A&M, Argonne National Lab West and General Atomics led to a resolution of the damage mechanism as described below: (2)

TRIGA fuel is fabricated with a nominal hydrogen to l

i zirconium ratio of 1. 6 for FLIP fuel and 1.65 for Standard.

This yields delta phase zirconium hydride which has a high l creep strength and undergoes no phase changes at temperatures over 1000 0C (3). However, after extensive steady ' state J operation at 1 Mw, the high temperature gradient created during steady . state operation will cause the hydrogen to redistribute from the central high temperature regions of the fuel' to the cooler outer regions. When the fuel is pulsed, the instantaneous temperature distribution is such that the highest values occur at the surface of the element and the lowest values occur at the center. The higher temperatures in the outer regions occur in fuel with a hydrogen to zirconium ratio that has now substantially increased above the nominal value. This produces hydrogen gas pressures considerably in excess of that expected for ZrH (2) l .6'

j. Figure 1 on the next page of this report shows the relationship between maximum fuel temperature during pulsing 1

versus FLIP fuel damage that was observed in the Texas A&M TRIGA reactor. A detailed analysis of the failed FLIP fuel and extensive consideration of the properties of zirconium hydride fuel (4) by General Atomics established the fact (2)

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1 FUEL DAMAGE VERSUS FUEL TEMPERATURE IN F N'5 ^ 5 M TRIGA REACTOR, 1976 500 -

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that the - onset of FLIP damage occurred at a temperature of about;8740 C 'during pulsing. That is, in a FLIP fueled core with extensive steady state operation, if the temperature of a FLIP fuel rod during subsequent pulsing exceeds 874 0C, FLIP fuel rod damage is very likely to occur in that rod.

The failure mechanism is associated with the fact that 0

above 874 C the hydrogen disassociation pressure in a FLIP '

fuel rod with extensive- steady state operation and the associated hydrogen redistribution effect is sufficient to cause small microscopic holes to develop in the FLIP fuel.

These microscopic holes . grow larger and proliferate with each pulse that produces a FLIP fuel rod temperature above 874 0C.

The microscopic holes eventually caused the FLIP fuel rod material to fracture, swell and distort. The damaged FLIP fuel rod material, in turn, created distorted, bent and bowed FLIP fuel rods.

Fuel TemDerature Limit for Pulsina of a - FLIP Fueled TRIGA Reactp,I Extensive studies conducted in the aftermath of the FLIP fuel damage problem that occurred at Texas A&M as discussed in the previous section of this report revealed the fact that FLIP fuel damage occurs when the FLIP fuel temperature exceeds 8740 C during pulsing. The FLIP fuel damage was discovered at Texas A&M before a cladding failure occurred with an associated release of fission products. However, if the FLIP fuel damage had not been discovered, a cladding failure would l

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Equilibrium hydrogen pressure over ZrH 1.65 versus temperature Figure 2 7

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problem than just bent and bowed fuel rods.

i Figure 2 on the following page shows the equilibrium  :

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hydrogen pressure over ZrHl .65 versus temperature. These pressures are not actually achieved during pulsing because the-  :

pressure is more a function of the average temperature of the ,

fuel than the peak temeprature during a pulse. However, the curve may be used to compare relative values for comparison purposes. At a fuel temperature of 874 C, 0 this curve predicts an equilibrium hydrogen pressure of about 70 psi. If we select a safety margin factor of two, then the allowable equilibrium hydrogen pressure would be set at 35 psi.

Referring to the graph in Figure 2, we see that this corresponds to a fuel temperature of 830 0C. Accordingly, if the maximum allowable FLIP fuel temperature during a pulse is limited to 830 0C, this temperature limic should preclude the development of damage in the FLIP fuel rods of the type that occurred at Texas A&M. This limit is consistent with observed results shown in Figure 1.

Pulsina Performance of the WSU Modified TRIGA Reactor y The pulsing performance of the WSU modified TRIGA reactor with the present mixed fuel core No. 32A is shown in Figures 3 and 4 and Table I. Core 32A is composed of 75% FLIP fuel in l the center of the core and 25% Standard fuel around the edges of the core. This core has a fuel temperature to power

(- density relationship (3) of:

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CORE 32A PULSING CHARACTERISTICS XL =' 24.usec. Tc = -0.0145 $/*C N = 102 TRIGA! rods To = 35'C-Reactivity. max; Tp E E7cm

($) (Megawatts) (*C) (Megawatt-Sec) (Watt-Sec/cc) 1.25- 51 69- 5.9 159 1.50 205 103- 9.0 243 1.75 467 136 12.2 330 i

12.00 839 168 15.6 420 2.25- -1324 200 19.0 513 2.5C ~ 1926 232 22.5 609 2.75 2648 263 26.2 708

$ = reactivity inserted in dollars I

lGi/ = average peak core temperature in,'C E = energy released in megawatt-sec 5/cm = average energy per em 3 of fuel in watt-sec/cm 3

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.where - 6 T is the average core temperature rise in degrees centigrade. . Using the limiting fuel temperature of 830 C established in the previous section of this report which corresponds- to a AT of 795 0 C above ambient, we calculate a i

maximum' allowable power density during a pulse of 2923 watts-sec/cm3 . This value represents the worst case condition and i thus we must make 'a correction for heterogeneous effects in.

the real core. The total ' peaking factor for the WSU TRIGA reactor calculates cut to be 5.91 using the data developed at General Atomics (6). That is, the ratio between the average temperature in the core ' to the highest temperature point in i the core due to heterogeneous effects is 5.91. Thus, the average power density in the core should not exceed 2923/5.91.

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495' watts-sec/cm3 in order to limit the temperature in the hottest spot to'830 0C.

L Referring to Table I which depicts the performance of L core 32A using the Fuchs-Nordheim variable heat capacity model (6); we see that the safe pulsing limit for this core . is between $2.00 and $2.25. Interpolation of data in Table I yields a safe ' pulsing limit of $2.20. Figure 5 shows the l

l performance of the Texas A&M reactor during pulsing and the

. pulsing limit of $2.28 that was established for the core l represented by Figure 1. The cores in the Texas A&M and WSU l

L reactors are quite similar and thus one would expect the pulsing limits to be similar even though the calculations were

l. done by somewhat different methods.

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1 Hazards Evaluatiori of Present WSU Reactor Pulsino Litgit Retaining the present . technical specification limit for l the WSU TRIGA reactor with a pulsing limit of $2.50 is

. inconsistent with reactor safety methodology since the analysis upon which that limit was set now turns out to be less than conservative. The most likely result from pulsing the WSU TRIGA reactor at the $2.50 level would be a FLIP fuel

-problem like the one that occurred at Texas A&M and the possibility of a fuel cladding rupture with the release of fission products into the reactor pool room. The Design Basis Accident in the SAR for the WSU TRIGA reactor is the failure of one fuel rod and the release of the contained fission products into the pool room. The SAR analysis demonstrates that this postulated accident would not constitute. a significant safety hazard to the general public. Thus, the present non-conservative pulsing limit of $2.50 does not involve a significant safety hazard.

The requested change in the technical specification for the WSU TRIGA reactor from the present $2.50 pulsing limit to one related to the maximum allowable fuel temperature during a

-pulse does not involve a significant safety hazard consideration on the basis of the considerations listed above.

The change involves shifting to a more conservative limit based on the results of the analysis of the cause of the FLIP fuel damage problem that occurred at Texas A&M. The requested change is also consistent with the technical specification

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FLIP fuel damage problem that occurred at that facility.

Uncertainties in the Pulsina Limit Based on Fuel Temoerature The. primary uncertainties associated with the calculation of the maximum allowable polse insertion based on fuel temperature by the method outlined in this report fall- into '

two areas. These areas are 1) the accuracy of the Fuchs-Nordheim pulsing model, and 2) calculation of the average core temperature and the core temperature peaking factor. The Fuchs-Nordheim variable heat capacity mode is known to be conservative - (7) and thus the actual average power density will be slightly less than predicted by this model. The conservative nature of this model primarily stems from the fact that the model assumes a constant negative temperature coefficient whereas the real temperature coefficient of.a FLIP fueled reactor increases with increasing temperature. At WSU, core temperature calculations,are based on the fuel rod power density as calculated using the two dimensional EXTERMINATOR-2 diffusion code. (8) This code has been used at WSU and Texas A&M for a number of years and has been found to be quite accurate. The peaking factors used to make the average to peak-temperature calculation are a small modification of those reported in report GA-9350 (5) that are as accurate as one can calculate. The small modification used at WSU increases the total peaking factor and thus makes the analysis more

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.51 Iconsetvative. In general, all the uncertainties are such-that lead-to the setting of a conservative limit.

Recommended Precuency of Pulsina Limit Evaluation The two. primary parameters that . cause a change in a core's performance that necessitate a recalculation of the temperature related pulsing limit are: 1) core changes and-

2) fuel burnup. Accordingly, a new calculation must be made sach time the core is rearranged including just moving fuel rods around- in the core. Also, the temperature limit should be calculated annually to take into account the effects of burnup and' of the buildup of fission products in the core.

Due. to the fact that the highest burnup is in the center of-the core, the power density in the hottest rod decreases with burnup thereby making a previously calculated temperature i related pulsing limit more conservative. Accordingly, annual calculations on an unchanged core is conservative.

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N REFERENCES

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1. . Status Report on Damaged FLIP Fuel During Operation of

~the NSCR at Texas A & .M University, Letter to the USAEC of November 1, 1976, from John D. Ronald, Director, Texas A & M University, Nuclear Science -3 Center.

2. Supplement I to the 1979 Safety Analysis Report for the Texas A & M Nuclear. Science Center Reactor,- 30 ,

March, 1982.

3. Safeguards Summary Report for the TRIGA-FLIP Reactor at the Puerto Rico Nuclear Center, PRNC-123, Revision C,-November 11, 1969.
4. The U-ZrH Alloy: Its Properties and Use in TRIGA Fuel, G. A. x Report E-117-833 of February 1980 by M. T.

Simnad.

5. Experimental Results from Tests of 18 TRIGA-FLIP Fuel Elements in the Torrey Pines Marte F Reactor, G.A.

report GA-9350 by G. B. West and J. R. Shoptaugh.

6.

The Fuchs-Nordheim Model with variable Heat Capacity, NS'

& E, Vol 16,-No. 4, August 1963, R. Scaleter.

7.

Safety Analysis Report for the I311nois Advanced TRIGA,

-University of Illinois, August 1967.

8.

-EXTERMINATOR-2: A Fortran-IV Code for Solium, Multigroup Neutron Diffusion Equations in Two Dimensions, ORNL-4078, April 1967, J. B. Fowler et al.

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