ML20070P388

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Theoretical Manual & User'S Manual for Axial Shape Analyzer for SIMULATE-3 (Asas).
ML20070P388
Person / Time
Site: Fort Calhoun Omaha Public Power District icon.png
Issue date: 04/19/1994
From:
YANKEE ATOMIC ELECTRIC CO.
To:
Shared Package
ML19304C106 List:
References
NUDOCS 9405110277
Download: ML20070P388 (119)
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l ASAS (AXIAL SHAPE ANALYZER FOR SIMl] LATE 3)

THEORETICAL MANUAL AND USER'S MANUAL April 19,1994 9

Yankee Atomic Electric Company i

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- ASAS Manual Revision 0 April 19,1994

1 TABLE OF CONTENTS i

DESCRIPTION PAGE LIST OF FIGURES . . . . . . . . . . ..... ..... . . . . . . . . . . . . . . . . . . . . . iii THEORETICAL MANUAL ..... . . . . . . . . . , . . . . ... 1 Abstract . . . ... ....... ........ . . . . . . . . . . . . . . . . . ..... 1 Type of Problem Solved . . . ...... . . . . . . . . . . . . . . . . . . . . . . .. . 1 User Support . . . . . - .. .. ....... . . . . . . . . . . . . . . . . . . . . .... 1 ,

Computer Code Description . . . . . . . . . . . . . . . . . . .. . 2 Equations . . . . . . . .. . ... ...... . . . . . . . . . 5 USER'S MANUAL . . ...... .. . .. ....... . . . . . . . . . . . . . . 12  ;

Input Instructions - SIMUIATE-3 Pin Power File . . . . . . . . . . . . . . . 12 Input Instructions - Detector View Factor File . . . . . . . . . . . . . . . . . . . . 13 Input Instructions - User Input File .. .... . . . . . . . . . . . . . . . . .... 14 File Interface Names . . . ..... . . . . . . . . . . . .... 22 Output File Descriptions . . . .. . . . . . . . . . . . . .. 24 REFERENCES . . . .. .. ... .. .. . . . . . . . . . . . . . ... 115 i

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LIST OF FIGURES FIGURE NUMBER DESCRIPTION PAGE 1 ASAS and SIMULATE-3 Assembly Numbering Schemes . . . ... ....... 27 2 SIMULATE-3 Input File for Cycle 15 As-Built Depletion ..... . ...... 28 3 SIMULATE-3 Input File for Cycle 15 BOC Xenon Oscillation . . . . ..... 29 4 Axial Shape Index Versus Oscillation Time for Sample SIMULATE-3 Xenon Oscillation Case . .......... ..... 30 5 SIMULATE-3 Input File for 3D Pin Power File Generation for the ASAS Sample Case . . . . . . ... . .. . .. .. .. 31 6 Suggested SIMUIATE-3 CEA Insertion Cases for Setpoint Analysis . . . .. 33 7 Sample View Factor File . . . . . . . .. . . . . .. ... ... .... 34 ,

8 Sample ASAS User Input File . . . .. . .. . ........ . .. .... 40 9 Sample Procedure to Execute ASAS on a HP/UX UNIX Computer . . 41 10 Sample Procedure to Generate SIMULATE.3 and ASAS Input Files and Execute the Codes for the Flyspeck Analysis .. 42 11 Sample Script File to Execute Flyproc for 100 Timepoints .. . . .... 48 12 CONCAT.F - Sample Code to Concatenate and Sort Multiple CTS and ATS Files . . . ..... .. . . . .. .. . .... 50 13 Sample User Output File ... . .. . . .. . ... . 54 l 14 Sample CTS Output File . ... . . . ...... .. . . .. . 91 15 Sample ATS Output File . . . . . .... . .... .... 92 16 Sample POSTSCRIPT Plots .. . . .. . .... . .. 108 17 POSTER. TOP - File Added to Top of ASAS Plot File . . .... . 110 Prior to Frinting ASAS Manual Revision 0 iii April 19,1994

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TIIEORETICAL MANUAL The theoretical manual contains an abstract which provides a summary of the ASAS code's capabilities, a description of the type of problem solved, a description of the computer code functions and subroutines, and a description of significant equations and numerical manipulations used.

Abstract t ASAS (Axial Shape Analyzer for S_IMULATE-3)(pronounced ' ACES') is a FORTRAN 77 computer code which provides a link between the SIMULATE-3 advanced nodal theory computer code (Reference 1) and thermal-hydraulic and setpoint computer codes, ASAS adjusts SIMULATE-3 powers to accommodate user-supplied uncertainty factors, and writes select information to a user output file, a Core Transient Summary (CTS) file, an Axial Transient Summary (ATS) file, and a plot file (on option).

ASAS reads a user input file, a file containing pin-wise ex-core detector view factors, and a SIMULATE-3 3D pin power file. It calculates core average power related data and determines which assemblics from the SIMULATE-3 pin file to process based on options from the user input file. For each assembly processed, ASAS calculates additional data. The data produced by ASAS include axial shape, power peaking, and power-to-fuel-design-limit data, and are described in the Equations portion of the Theoretical Manual.

Type of Problem Solved ASAS will process a 3D SIMULATE-3 pin power file containing up to 50 cases. The code was written explicitly for Fort Calhoun modelled in SIMULATE-3 as a quarter core.

User Support Support for the ASAS code can be obtained by calling Yankee Atomic Electric Company at (508) 779-6711 X2039.

l ASAS Manual Revision 0 1 April 19.1994

Computer Code Description The subroutines and functions in ASAS are described in this section.

PROGRAM ASAS The main portion of the code calls the system date and time subroutines, opens the user input and all the output files, and calls subroutines INP'I', SPLSET, and MAIN.

SUBitOUTINE INPT This subroutine reads the user input file and the ex-core detector view factor file. It echos the user input and provides an edit of the data used in the run. Range and error checking of the input data is performed here as well. Subroutine INPT is called from PROGRAM ASAS.

SUBROUTINE SPLSET This subroutine calculates the axial plane boundary interface locations as a fraction of core height, sets the 2 array (defined in the Equations section of this manual) by calling subroutine ASET, and calls LUDCMP to perform a portion of the matrix solution of the equation 2+0=5 Subroutine SPLSET is called from PROGRAM ASAS.

SUBROUTINE MAIN -

This subroutine reads the SIMULATE-3 pin power file and calculates the core average parameters (see the Equations section of this manual for a description of these data). The >

core average axial shape is determined via a call to subroutine FITSUB. Subroutine MAIN then calls subroutines SELECT, CALC 2D, and/or CALC 3D to select the assemblics to be processed (based on user input options). For each assembly to be processed, subroutine MAIN calls subroutine PROCESS. Subroutine MAIN is called from PROGRAM ASAS.

SUBROUTINE SELECT 4

This subroutine is called from subroutine MAIN. It assigns the user-selected assemblies to be processed (entered via the SEL. ASS card in the User Input file) to their appropriate fuel -

types. These assemblies are also called the ' winning' assemblies. ASAS processes the winning '

assemblies by fuel type, then by assembly within that fuel type. For example, if assemblies 1, 10, and 30 are selected by via the SEL. ASS card, and the fuel types assigned to these assemblies via the LAY.DWN card are 2,2, and 1, respectively, then the assemblies will be processed in the order 39,1, then 10. Subroutine SELECT is called only if NSEL (entered via the SEL. ASS card) is greater than zero.

SUBROUTINE CALC 2D This subroutine is called from subroutine MAIN. IfICALC (entered via the CONTROL card) is equal to 2, then subroutine CALC 2D determines assemblies to be processed in addition to those selected via subroutine SELECT. These assemblies are those which contain the maximum 2D pin and channel powers for each fuel type. Therefore for each fuel type, one or ASAS Manual hvision 0 2 April 19,1994

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I two assemblies will be selected, depending on whether the maximum channel assembly is also the maximum 2D pin assembly. ,

l SUBROUTINE CALC 3D j 1

This subroutine is called from subroutine MAIN. IfICALC (entered via the CONTROL card) is equal to 3, then subroutine CALC 3D determines assemblies to be processed in addition to those selected via subroutine SELECT. These assemblies are those which contain the maximum pin and channel powers for each fuel type at each of the NPLANE axial planes, where NPLANE is set to 16 for the Fort Calhoun model in a data statement in the code. ,

Therefore for each fuel type, from one to up to 2*NPLANE assemblies will be selected, depending on how many different assemblies contain these limiting locations.

SUBROUTINE FITSUB ,

This subroutine calculates the 5 vector in the equation 2 *b=5 by calling subroutine BSET for the area-preserving natural spline fit of the core average axial shape and the axial shape of each winning assembly. It then completes the solution of these equations for the vector U by calling subroutine LUBKSB. The coefficients 5 are then used to calculate the axial power shape over NFLFIT (entered via the CONTROL card) uniform axial planes.

FITSUB then generates a plot of the input axial shape in histogram form, a smooth curve of the axial shape as determined from the fit coeflicients b , and the resulting output axial shape in histogram form. 'rhis subroutine is called from subroutine MAIN for the core average axial shape and from PROCESS for each winning assembly average axial shape.

SUBROUTINE PROCESS This subroutine calculates all the winning assembly data described in the Equations section of this manual, and writes this data to the User Output file, the CTS file, and the ATS file. The axial data fit to NPLFIT planes is determined via a call to subroutine FITSUB. Subroutine PROCESS is called from subroutine MAIN.

SUBROUTINE ASET Subroutine ASET determines the elements in the I array from the NPLANE axial node boundaries. Subroutine ASET is called from subroutine SPLSET.

SUBROUTINE BSET Subroutine BSET is called from subroutine FITSUB. It determines the elements in the 5 vector for either the core average axial shape or a winning assembly average axial shape.

SUBROUTINE LUDCMP This subroutine is called from subroutine SPLSET. It decomposes a matrix 2 into a lower triangular and an upper triangular matrix (called an LU decomposition). The matrix to be ASAS Manual Revision o 3 April 19,1994  :

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decomposed is 3 , and the decomposed matrices are returned in the 5 matrix.

This subroutine is used together with the LUBKSF, subroutine to solve the matrix equation 2 *U=5 . This subroutine is taken from Chapter 2.3 of Reference 2.

SUBROUTINE LUBKSB This subroutine is called from subroutine FITSUB. It finds a d vector that solves the matrix equation N

  • 0=5 , with a decomposed lower triangular and upper triangular matrix,'

decomposed from an original 3 matrix by the subroutine LUDCMP.

This subroutine is used together with the LUDCMP subroutine to solve the matrix equation 2

  • U=5 This subroutine is taken from Chapter 2.3 of Reference 2.

SUBROUTINE HEADING This subroutine prints a heading to the user output file. It calls subroutine IIEAD1 and adds case specific data after the HEADI heading info. ,

SUBROUTINE IIEAD1 This subroutine prints a heading to the user output file. This heading contains the program title, date, time, and page number.

SUBROUTINE POWPRN This subroutine prints an assembly power distribution to the user output file.

FUNCTION LLEN This function determines the length of a character string. ,

ASAS Manual Revision 0 4- April 19,1994

l Equations Note: In the theoretical and user's manual, and in the code itself, the indices I, J, K, L, M, and N mean the pin row number, pin column number, axial plane number, case number, fuel type number, and assembly number, respectively, unless noted otherwise in the manual or the computer code.

ASAS reads a user input file and a SIMULATE-3 3D pin power file containing from 1 to 50 cases. A select list of data which is read from the user input file follows.

  • CAkWFP The core average linear heat generation rate (LHGR) in kW/ft.

MLIMu The SAFDL on LIIGR for fuel type M.

  • FCALC The calculational uncertainty factor.
  • FTILT The core tilt uncertainty factor.
  • FGRID The grid dip factor.
  • FE The engineering (i.e. fabrication) uncertainty factor.
  • FCALOR The plant calorimetric uncertainty factor.
  • FDEP The fuel deposition factor (fraction of energy deposited in fuel).
  • FfRIP The trip overshoot power uncertainty factor.
  • FASI The axial shape index (ASI) uncertainty factor.
  • FRTt The radial peaking factor for case L.

ASAS reads a view factor file (the name of this file is defined in the user input file) for the pinwise ex-core detector view factors.

  • VUFACv,n The ex-core detector view factor for pin row I, column J, assembly N.

ASAS reads the following information from the SIMULATE-3 pin power file for each case:

  • XPO The cycle average exposure in GWd/MtU (for xenon oscillation cases, this is the oscillation time in hours).
  • EI3AR The core average exposure in GWd/MtU.
  • PERCTP The percent rated core power.
  • PERCWT The percent rated core flow.
  • NOTWT The number of notches of control rods inserted into core.

FQ The maximum 3D pin power including intranodal axial peaking (equal to the 4-pin edit in the SIMULATE-3 output file)(this ,

does not include the grid dip factor FGRID).

  • F DELTA-II The 2D radial pin peaking factor (this does not include the grid dip factor FGRID).
  • A-O The core average axial offset (the ASI is the negative of this).
  • PINPAVv y The 2D pin powers for assembly N.
  • PINPOW u.x,s The 3D pin powers for assembly N.

SERIAlm The 6 digit serial number for assembly N.

NHPINs The number of fuel rods in assembly N.

ASAS determines the following core average parameters for each case:

CORAXx The normalized core average axial power shape (NPLANE values).

  • FZCORE The core average axial peaking factor (determined as the maximum of the CORAXx values).
  • KFZCOR The axial plane of FZCORE.
  • ASICOR The core ASI (this is the negative of the axial offset read from the SIMULATE-3 pin file).

ASAS Manual Revision o 5 April 19,1994 l

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  • ASIPER The peripheral ex-core ASI.
  • EXCORE The ex-core response.

CORFITx The normalized core average axial power shape fit to NPLFIT uniform axial planes.

  • FZCFIT The axial peaking factor from CORFIT (determined as the maximum of the CORFITx values).
  • KZCFIT The axial plane of FZCFIT.
  • ASICUN The core average ASI with the ASI uncertainty factor FASI.
  • ASIPUN The peripheral ex-core ASI with the ASI uncertainty factor FASL For each case, the winning assemblies are selected via the SEL. ASS card and/or the ICALC =

2 or 3 option from the CONTROL card. For each winning assembly N, ASAS determines:

  • ASSAXgy The normalized assembly average axial power shape.

FZASSu The assembly axial peaking factor (determined as the maximum of the ASSAXg,x values for assembly N).

  • KFZASSy The axial plane of FZASSs.
  • ASIASS 3 The assembly average ASI.

ASIAUNs The assembly average ASI with the ASI uncertainty factor FASL

  • PINADJ un The 2D pin powers, adjusted by the ratio of the local pin axial peak to the assembly axial peak, This is done so that use of the assembly peaking factor preserves the maximum 3D peak for each pin. PINADJ also includes the grid dip factor FORID.
  • FDilASS 3 The maximum 2D pin peaking in the assembly, including the grid dip factor FGRID (determined as the maximum over I and J of PINADJg 7 ul
  • 12DASSs, J2DASSu The location of the maximum 2D pin power in the assembly.

CHAMAXs The maximum 2D channel power in the ass'embly, including the grid dip factor FGRID (determined as the maximum 4-pin average power over I and J of PINADJt t s).

  • IC2Ds, JC2Dy The location of the maximum 2D channel power in assembly N.

FQASSu The maximum 3D peaking in the assembly, including the grid  ;

dip factor FGRID,

  • IFQASSu, JFQASSs The location within the assembly of the 3D peak.

KFQASSs

  • LHRASSy The maximum LHGR in the assembly (kW/ft), including the grid dip factor FGRID.
  • PLASSy The power-to-fuel design limit (PFDL) for the assembly (w/o ,

uncertainties), including the grid dip factor FGRID and the energy deposition factor FDEP.-

FDlIUNCu The maximum 2D pin peaking in the assembly, including the grid dip factor FGRID, the calculational uncertainty factor FCALC, and the azimuthal tilt uncertainty factor FTILT. -

  • FQUNCy The maximum 3D peaking in the assembly, including the grid -

dip factor FGRID, the calculational uncertainty factor FCALC, and the azimuthal tilt uncertainty factor FTILT. .

  • LIIRUNCy The maximum LHGR in the assembly, including the grid dip factor FGRID, the calculational uncertainty factor FCALC, the azimuthal tilt uncertainty factor FTILT, the engineering uncertainty factor FE, and the calorimetric power uncertainty factor FCALOR.

PLUNCs The PFDL, for the assembly, including the grid dip factor FGRID,.

the calculational uncertainty factor FCALC, the azimuthal tilt ASAS Manual itevision 0 6 April 19,1994

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uncertainty factor FTILT, the engineering uncertainty factor FE, the calorimetric power uncertainty factor FCALOR, the energy deposition factor FDEP, and the trip overshoot power uncertainty <

factor FTRIP.

ASIAUNu The assembly average ASI with the ASI uncertainty factor FASI.

  • ASSFITx, The normalized axial power shape fit to NPLFIT uniform axial planes.

FZAFITs The assembly axial peaking factor from ASSFITx,(determined as the maximum of the ASSFITx3 values for assembly N)

KZAFITs The axial plane of FZAFITu.

The equations used to calculate the above parameters are defined below.

1 CORAX g NPLANE*[,,, PINPOW,,,, WEIGHTy CORAX,= (I)

[,,,, PINPOW,,,,* WEIGHTg Where:

WEIGIITu is the assembly weighting factor contained in a data statement in ASAS. This factor is unity for all assemblies, except the quadrant boundary assemblies. The weighting factor for these assemblies is 0.5 and 0.25 for the core center assembly.

ASIPER g9y ASIPER= BOT-M BOT + 70P Where:

BOT =[,,,,,, PINPOW,,,,

  • VUFA C,,pe WEIGHTg (3y and 7OP =[,,, , PINPO W,,,,* VUFA C,,,pe WEIGHTu (4y EXCORE 2

(BOT + 7DP) .[gNROD . WEIGHTg EXCORE=

(0)

NFLANE<[gNHPIN y* WEIGHTg Where NROD is the number of rods along one side of an assembly. It is set equal to 14 for Fort Calhoun in a data statement of the code.

CORFIT The NPLFIT values of CORFITx are determined from a natural spline fit of the CORAXg data (NPLANE values). The spline fit is determined using equations which preserve the average value over the interval, rather than forcing the curve through the input data coordinates, i This is necessary to fit the normalized SIMULATE-3 axial power distributions because the ,

axial powers are defined in SIMULATE-3 as the average powers over the axial intervals, not ASAS Manual Revision 0 7 April 19,1994 1

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the powers at the midpoint of the intervals. The conventional natural spline and the modified area-preserving natural spline fit processes are defined below.

I Conventional Natural Spline A conventional natural spline fit requires as input a set of coupled vectors X and E . It then generates a set of second order polynomial coeflicients for a range surrounding each ordered data pair which define the curve in that range. The conditions required of these coefficients are defined below.

Condition # 1 F(Xg)# Y, or C,,,<C ,*X 2 y <3,.$ ug Condition #2 The curve is continuous over its entire range, or F(Xg ig)=F(X g,i. i,2) or C ,, + C2y .Xr .tr2 + 3C ,

  • Xx! in <if,i + C25.i 'X x.tr2 ' C 3 A. i 3 . itz (9)

Where:

Xx.1,2 represents the top boundary of node K, and

.Xn.iie2 represents the bottom boundary of node K+1.

Note also that Xx,in = Xx.i.3,2 . (10) i i

Condition #3 The slope is continuous throughout its entire range, or the derivative at Xxin = We derivative at .Xxi y2, or C2f + 2 . C3 ,g . rX . it242x.1 + 2.C ,y,3

  • Xr.t/2 3

in order to provide sufficient conditions to solve the matrix of equations, two additional equations must be supplied. These are defined as a zero second derivative in the first and last intervals (known as a natural spline), or

2. C3,3-0.0 (12) and 2.C3 ,.g0 0 (13)

The above equations define a matrix of equations which can be written as:

ASAS Manual llevision o 8 April 19,1994

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(14)

Ned=5 i

Where:

1 is a maLix of 3*NPLANE by 3*NPLANE elements defined by the X coordinate data,-

5 is a vector containing the constants in each equation which are defined from the f data for the appropriate equations, and C is a vector of 3*NPLANE elements containing the three quadratic fit coe1Ticients for each of the NPLANE intervals. This vector is determined by standard matrix solution techniques Gleference 2).

Area-Preserving Natural Spline The defining equations for the area-preseiving natural spline fit are identical to those for the conventional natural spline, with one exception. The first condition is replaced with:

Condition #1 The average value from Xx-v2 to Xx.ir2 = Yx, or

['"'"*'*C,,4 2,

  • b C,, . X dX

=YK x &

fx,a.wgy e

or Cif.(X,,in-X r-i/2) + @ <2.r

  • N.1/2-N-it2h W 3'C ,.d.3,2d_if2) (16)

= Y' Xx ig-Xx-nn

}

The elements of 2 are determined in subroutine ASET, and the elements of 5 are determined ,

in subroutine BSET. The elements of d are determined using the matrix solution subroutines LUDCMP and LUBKSB, which were obtained from Reference 2.

The coeflicient vector d is used in subroutine FITSUB to calculate the average values of CORFITxover tlie NPLFIT uniform axial planes using equation 16 to de n i the average value. Note that the boundaries of the NPLFIT uniform axial planes do not necessarily line up exactly with the boundaries of the input NPLANE axial planes. Therefore subroutine FITSUB has logic to use the correct interval's coefficients, even if this means breaking the integration into two or more segments.

ASSAX u NFL4NE*[uPINPO H'y,, ($qy ASSA X,,=

Eux PINPO H'u,,

ASAS Manual Revision 0 9 April 19,1994 I

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ASIASS ASIASSu=

BOTg -1DP" (18)

BOTg+7DPg Where:

(AU)

BOTg =[,,,,,, PINPOW,,pp and (E0}

IDPy =[y,,,, PINPOWupp PINAD.1 PINPA Vup*FZPINy ,*FGRID p,

FZASSg Where:

UJB (22)

FZPINyp=hfAX,,, , ,

ExPINPOW y ,p FDHASS INOI FDHASS y =hiAX_, a ,,,,,,(PINADJyp}

i CHAMAX CHAbfAXy =hiAX,,,,,,,s ,[0.25 *(PINADJup + PINADJ,, up + PINADJy ,,p + PINA DJ,,y ,,p)} g24y

'l FQASS

( 0)

FQASSg= hfA X,,, ,,, ,, , ,,g , [PINPO Wup eFGRID}

LHRASS (26)

LHRASSu =FQASSg *CAKWFT PLASS 100.0

  • AfUhf" (27)

PLASSp=

LHRASSy *FDEP FDHUNC I28)

FDHUNCy cFDHASSg *FCALC FTILT ASAS Enual Revision 0 10 April 19,1994

FOUNC FQUNCg=FQASSg eFCALCeFTILT LIIRUNC LHRUNCg=FQUNCgeCAKWFTeFE*FCAL PLUNC 100.0 *MLIM" (31)

PLUNCg= -FTRIP LHRUNCg *FDEP ASIAUN if ASIASS, is less than FASI and greater than -FASI: ASIUNCy r U.0 (02) if ASIASS, is greater than FASI: ASIUNCy = ASIASS, - FASI If ASIASS, is less than -FASI: ASIUNCg = ASIASS, + FASI ASSFIT The NPLFIT values of ASSFITxy are determined from the NPLANE values of ASSAXxy using the same area-preserving natural spline fit process that was used to determine CORFITx, 11 April 19,1994 ASAS Manual Revision 0

USER'S MANUAL .

' l The User's Manual provides input instructions for all input files to the code, describes the file linking names, and provides a description of the files generated by the code. A series of SIMULATE-3 input and ASAS input and output f.les is provided for one sample case.

INPUTINSTRUCTIONS Three files are required for input to the ASAS code. These are a SIMULATE-3 pin power file, a detector view factor file, and a user input file. These are described below.

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INPUTINSTRUCTIONS SIMULATE-3 PIN POWER FILE This file is generated by a SIMULATE-3 case. It must be a three-dimensional file containing pin powers only. Pin exposures must not exist on the file. This file may contain up to 50 cases. It is generated via the following SIMULATE-3 input card:

'PI N. FI L','ON','fil e n n m e',' ADD','3 D'/

Where filename is a user-selected name for the file.

Four files were used to generate the 3D SIMULATE-3 pin power file s30 test.p, which was used in the ASAS sample case. These files are as follows:

830c15s.i This input file is the BOC 15 model setup. This input file is not shown due to its large size. It is identical to the file C1511FP-BOC which was provided to Yankee by OPPD, with the following modifications:

- The CRD. SEQ card was modified to provide spaces between the values for NOTCll(IGROUP, pass).

The CRD.POS card was modified to provide spaces between the values for NPCR(ir,jr).

- The STA card was changed from STA 1 to STA.

s30e15d.i This input file is the Cycle 15 as-built depletion, and is shown in Figure 2. This file is identical to the file C15-DEP which was provided to Yankee by OPPD, with the following modifications:

The RES card was modified to accommodate the name of the restart file.

A WRE card was added to create a restart at 500 mwd /MtU.

s30ABos.1 This input file is the BOC 15 (500 mwd /MtU) oscillation and is shown in Figure 3. This file generates a restart every hour from 1 to 8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br /> and every half hour from 8 through 80 hours9.259259e-4 days <br />0.0222 hours <br />1.322751e-4 weeks <br />3.044e-5 months <br />. A xenon oscillation is induced by turning off doppler feedback via the SEG.TFU and TAB.TFU cards, and Bank 4 is inserted 40% at 75% power for 8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br />. At 8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br />, Bank 4 is withdrawn and power is returned to 100%. The axial shape index versus oscillation time resulting from this run is shown in Figure 4.

830 test.1 This input file is the CEA insertion run which generates the SIMULATE-3 3D pin power file, and is shown in Figure 5. Two CEA insertion cases are selected from the 12 suggested CEA insertion cases shown in Figure 6. These cases were developed from the Power Dependent Insertion Limit (Figure 2 of the Cycle 15 Core Operating Limits Report) transmitted to Yankee from OPPD.

ASAS Manual Revision 0 12 April 19,1994  ;

h INPUT INSTRUCTIONS - DETECTOR VIEW FACTOR FILE This file contains data for the relative contribution of each pin to the ex-core neutron detector, i.e. the view factor data. The format of this file is:

l'arameter Description Card 1: Format (I3)

IASS Assembly number, This must be in the ASAS numerical order according to the Fort Calhoun ASAS numbering scheme, which is shown in Figure 1.

1 Card 2: Format (14F7.4)

VUFAC ng,my.i n Pinwise ex-core detector view factors for row 1 of assembly IASS VUFACa;3ma,i,a Pinwise ex-core detector view factors for row 2 of assembly IASS VUFAC,u ussu,i,n Pinwise ex-core detector view factors for row 3 of assembly IASS VUFACu;.assu-i.a Pinwise ex-core detector view factors for row 4 of assembly IASS VUFAC,v,assy i,a Pinwise ex-core detector view factors for row 5 of assembly LASS VUFAC,uussa,tn Pinwise ex-core detector view factors for row 6 of assembly IASS VUFAC njawy,i,a Pinwise ex-core detector view factors for row 7 of assembly IASS VUFAC,qassy,tn Pinwise ex-core detector view factors for row 8 of assembly IASS VUFAC,uussu i.n Pinwise ex-core detector view factors for row 9 of assembly IASS VUFACoo mssv.t.u Pinwise ex-core detector view factors for row 10 of assembly IASS >

VUFAC o uussa.i n Pinwise ex-core detector view factors for row 11 of assembly IASS VUFAC ov.tw u tu Pinwise ex-core detector view factors for row 12 of assembly IASS i VUFAC ouassa,i,n Pinwise ex-core detector view factors for row 13 of assembly IASS VUFAC ouussu t.u Pinwise ex-core detector view factors for row 14 of assembly IASS Card 2 is therefore entered 14 times for each assembly, and Card 1 and the 14 Cards 2 are I entered 39 times, one set for each assembly, i i

A sample detector view factor file is shown in Figure 7. This file contains view factors for the safety channel detectors located at 21". They have a flat weighting within each assembly, and were developed from data transmitted to Yankee from OPPD.

ASAS Manual Revision 0 13 April 19,1994 ,

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. . - = . . _.._. = -

- . _ = - - -

= - - -

INPUT INSTRUCTIONS - USER INPUT FILE The user input file is entered using free format, except where noted. The input cards are identified by a seven character string at the left-most position of the card. The cards may be entered in any order except for the EXECUTE card, which terminates the input phase of the code and begins execution.

A sample user input file is shown in Figure 8. This file was used together with the files in Figures 2,3,5, and 7 to generate the sample output files in Figures 13 through 16.

The input cards and their default values are listed below:

TIT.RUN - Run Title

Description:

Maximum 80 character title for the run Card format:

TIT.RUN TITLE Default: Blank title CONTROL - Control Parameters

Description:

This card contains selected integer control parameters for the run.

Card format:

CONTROL NFT,NCASE,1 CALC,NPLFIT,10UT,lPLT,IATS NFT Number of fuel types (limit 9). ASAS determines the limiting assemblies for each fuel type if ICALC is 2 or 3, and groups the printing of the results according to fuel type.

NCASE Number of cases in the run (limit 50). This must equal the number of cases on the SIMULATE-3 pin file.

ICALC Limiting assembly selection option. This is performed in addition to the SEL. ASS assemblies.

=2 Select the assembly containing the limiting 3D pin power and the assembly containing the limiting 2D channel power from each fuel type. The limiting channel is determined as the maximum average four pin channel.

=3 Select the assembly containing the limiting pin power and the-assembly containing the limiting channel power at each axial plane in the SIMULATE-3 pin file from each fuel type. The limiting channelis determined as the maximum average four pin channel integrated from the bottom of the core to the plane of interest.

  • 2, the only selection of assemblies is via the SEL. ASS card.

x3 NPLFIT Number of axial planes to fit the axial power shapes for printing to the CTS file (limit 50).

IOUT Option to print standard / expanded data to the output file.

=0 Print the input echo, the input data used in the run, selected ASAS Manual Revision 0 14 April 19,1994

l 1

l assembly edits, and for each selected assembly the following.

' Header information:

  • XPO - cycle exposure, I
  • EBAR - core average exposure,
  • POWER - power level in percent,
  • FLOW - core flow in percent,
  • NOTWT - total control rod steps inserted into the core,
  • FQ - 3D pin peaking from the GIMULATE-3 pin file, which includes the axial intranodal peaking (this is also called the 4 PIN edit in SIMULATE-3),

a F-DELTA-II - 2D radial pin peaking factor,

  • INCORE ASI - In-core average axial shape index, _
  • PERIPHERAL ASI - Ex-core weighted axial shape index,
  • TOTAL RELATIVE EXCORE SIGNAL,
  • FUEL TYPE,
  • ASSEMBLY NUMBER, and
  • ' ASSEMBLY SERIAL NUMBER.

Adiusted 2D Pin Powers:

i

  • 2D PIN POWERS. These are adjusted by the ratio of the l

assembly average axial peaking factor to the pin axial peaking factor in order to preserve the peak LHGR for each pin when using the core average axial shape. Also the grid dip factor FGRID is applied to these 2D pin powers.

Assembly Information:

  • MAXIMUM 2D ONE PIN POWER

= MAXIMUM CHANNEL POWER

= MAXIMUM 3D ONE PIN POWER

= MAXIMUM LHGR

  • MAXIMUM LHGR WITH UNCERTAINTY
  • PL TO FUEL DESIGN SAFDL WITH UNCERTAINTIES
  • ASSEMBLY AXIAL SHAPE INDEX
  • ASSEMBLY AXIAL SHAPE INDEX WITH UNCERTAINTY

=1 In addition to the above data, print the following for each selected assembly:

  • PIN POWERS FOR THE LIMITING AXIAL PLANE
  • FZ FACTORS - axial peaking factors for each pin in the assembly
  • ASSEMBLY AVERAGE PEAKING FACTOR. *
  • 2D PIN POWERS - as read from the SIMULATE-3 pin file.

IPIII' =0 _ Don't generate the POSTSCRIPT plot file

=1 Generate the POSTSCRIPT plot file. This file contains a plot of '

three sets of data for the core average and each assembly processed. These three sets of data are:

  • The SIMULATE-3 NPLANE plane normalized axial power distributions in histogram form,
  • The axial power distribution reallocated to the NPLFIT ,

axial planes in histogram form, and i-

  • A smooth curve of the axial power distribution calculated from the area preserving natural spline fit coeflicients.

l IATS =0 Generate ID core average axial power data only for the ATS file.

l This consists of the core average axial power in NPLFIT axial I

ASAS Manual Revision 0 15 April 19,1994 l

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l planes.

=1 Generate ID and 3D power data for the ATS file. This consists of the core average and assembly average axial power in NPLFIT axial planes, and the adjusted 2D pin powers for the limiting assembly. One set of data is printed for each winning assembly of each case.

Default:

CONTROL 1,1,1,40,0,0,0 FUE. LIM . Fuel Type Name nnd LIIGH SAFDL

Description:

This card contains the fuel design limit on linear heat generation rate and the corresponding fuel type name. One FUE. LIM card is entered for each fuel type, and the card should be entered NFT times; once for each fuel type.

Card format:

FUE. LIM M,MLIMu,ATYPEu M Fuel type number.

MLIMu LHGR SAFDL (kW/ft) for fuel type M.

ATYPEu Maximum 5 character name for fuel type M.

Default:

MLIM = 21 kW/ft for all fuel types, ATYPE = 'ALL ' for all fuel types.

LAY.DWN - Fuel Type by Assembly Laydown

Description:

This card specifies the fuel type by assembly laydown according to the ASAS quarter core assembly numbering scheme shown in Figure 1.

Card Format:

LAY.DWN 26x,2i4/

16x,5i4/ Note that this format is an 12x,6i4/ upper left quarter core laydown 12x,6i4/

12x,6i4/

8x,7i4/

8x,7i4 IAFT(i),i=1,39 Assembly fuel type by assembly position Default: IAFT = 1 for all assemblies ASAS Manual Revision 0 16 April 19,1994 l

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VUE.FIL - Ex-core Detector Pin View Factor File Name  ;

1

Description:

This card contains the name of the file which has the ex-core neutron detector view factors by pin. This name must include the path name if the file does not exist on the working directory of the run.

Card Format:

VUE.FIL DETFIL DETFIL Maximum 80 character name of file containing the ex-core neutron detector view factors Default:

VUE.FIL VUFAC UNC.FAC - Uncertainty Factors

Description:

This card contains the uncertainty factors.

Card Format:

UNC.FAC FCALC,FTILT,FGRID,FE,FCALOR,FDEP,FTRIP,FASI FCAL,C Calculational uncertainty factor FTILT Azimuthal tilt uncertainty factor FGRID Grid dip axial shape penalty factor FE Engineering (i.e. fabrication) uncertainty factor FCALOR Calorimetric power uncertainty factor FDEP Fuel deposition factor (fraction of energy deposited in the fuel)

FTRIP Trip overshoot power uncertainty factor (% power)

FASI Axial shape uncertainty factor (%)

Default:

UNC.FAC 1.0,1.0,1,0,1.0,L O,1.0,0.0,0.0 COR.LIIR - Core Average Linear IIcat Generation Rate

Description:

This card contains the core average linear heat generation rate (kW/ft). This is used to calculate the maximum LHGR and the FFDL. CAkWFT should include an appropriate axial fuel densification factor,if applicable.

Card Format:

COR.LHR CAkWFT CAkWFT Core average linear heat generation rate (kW/ft) i Default:

COR.LHR 6.0 ASAS Manual Revision 0 17 April 19,1994

TIT.CAS Radial Peaking Limit and Case Title

Description:

This card contains the radial peaking limit and the case title.

Card Format:

TIT.CAS L,FRTt,CASEID o L Case number (limit 50)

FRTt Itadial peaking limit for case L (this can be printed to the CTS file)

CASEID o Maximum 60 character title of case L. The first 8 characters of CASEID(L) are used as part of the case identifier in the CTS file along with the 1 digit fuel type number and the 1 digit sequence number for that assembly.

Default:

FRT = 1.5 for all cases CASEID is blank for all cases SEL. ASS - User Selected Assemblies l l

l

Description:

This card contains up to ten user-selected assemblies to be processed, in addition  !

to those determined from the ICALC=2 and ICALC=3 options. ,

I Card ' Format SEL. ASS NSEL,ISELuy 33sn, )

NSEL Number of user-selected assemblies (limit 10). Note, a limit of 9 assemblies per fuel type exists in order to accommodate the printing of the CASEID to the CTS file.

ISEL33.i3sa User-selected assembly numbers Default:

SEL. ASS 0 SIM.FIL - SIMULATE 3 Pin File Name

Description:

This card contains the name of the SIMULATE-3 3D pin power file. This name must include the path name if the file does not exist on the working directory of the run.

Card Format:

SIM.FIL SIMPIN

' SIMPIN Maximum 80 character name of SIMULATE-3 3D pin power file.

Default:

SIM.FIL PINFILE ASAS Manual Revision 0 18 April 19,1994

EDT. REQ CTS File Edit Hequests

Description:

This card contains the parameters to be written to the CTS file. The case aumber and case ID are written to the first two fields. This card provides the user the flexibility to derme additional edits.

Card Format:

EDT. REQ AREQuaxq AREQggeq 10 character edit request enclosed in quotes EDT. REQ is entered up to 12 times, once for each edit request. NREQ is incremented for each entry of EDT. REQ. The allowable values for AREQ are:

Core Average Edits

" POWER Power level (%)

"FZ-FISS "

Axial peaking factor of the core or "FZ-THRM "FZLOC-FISS* Plane of axial peaking factor of the core or "FZLOC-THRM" "ASI-FISS "

In-core average axial shape index or "ASI-CORE "

"ASI-PER "

Peripheral ex-core axial shape index "EXCORE RES" Ex-core detector response

  • ASI-COR-UN" In-core average axial shape index - includes the uncertainty factor FASI  !

"ASI-PER-UN" Peripheral ex-core average axial shape index - includes the uncertainty

, factor FASI l

l. Winnine Assembly Edits

" ASSEMIiLY # " Assembly number.

I i "ASI-ASS

  • Axial shape index of the assembly.

"FZ-ASS "

Axial peaking factor of the assembly.

"FZLOC-ASS "

Plane of axial peaking factor of the assembly.

"F-DELH "

Maximum 2-D power in the assembly includes the factor FGRID.

"F-DELH LOC" Location of F-DEL.Il - This is a 6 digit integer XXYYZZ, where XX is the ASAS Manual Revision 0 19 April 19,1994

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row, YY is the column, and ZZ is the assembly.

"FQ-FISS "

. Peak 3D power in the assembly, includes the factor FGRID.

or "FQ-THRM "LHGR "

Maximum linear heat generation rate in the assembly, includes the factor FGRID.

"PFDL-NO UN" Power fraction to design limit with no uncertainty factors (only factors FGRID and FDEP are applied).

"ASI-ASS-UN" Axial shape index of the assembly - includes the uncertainty factor FASI.

"F-DELH UNC" Maximum 2 D power in the assembly with the factor FGRID, and unecrtainty factors FCALC and FTILT.

"FQ W/UNC "

Peak 3D power in the assembly with the factor FGRID, and the uncertainty factors FCALC and FTILT, "Luca W/UNC" Maximum linear heat generation rate in the assembly with the factor FGRID, and the uncertainty factors FCALC, FTILT, FE, and FCALOR.

"PFDL "

Power fraction-to-design limit with the factor FGRID, and the or uncertainty factors FCALC, FTILT, FE, and FCALOR.

"PFDL W/UNC" Default:

NREQ=G, and EDT. REQ " POWER EDT. REQ ." ASI-FISS EDT. REQ "PFDL EDT. REQ "FZ-FISS "

EDT. REQ

  • FZLOC-FISS" EDT. REQ "FQ-FISS EXECUTE - Execute Case

Description:

Upon reading this card, the code terminates the reading of data from the input file and executes the run.

1

' Format: l EXECUTE 'l Default:

None ASAS Manua Revision 0 20 April 19,1994 l

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COMMENT . Comment Card

Description:

This card allows for comments to be included in the input file. They are not processed by the code, Format:

COMMEN'I' STRING STRING A character string of any length Default:

None 1

l I

ASAS Manual Revision 0 21 April 19,1994 l I

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FILE INTERFACE NAMES AND SCRIPT FILES File Interface Names The file interfaces for the ASAS code are listed below. ASAS is executed by typing tim name of the executable, and appropriate manipulation of the ASAS file narnes.

ASAS File interfares INPUT / ASAS ASAS File Name Description OliTPUT Fil.E UNIT #

USEl(IN User input file Input 1 DETFll' View factor file Input 9 SIM PlN' SIMUI. ATE-3 3D pin power file Input 8 USEltOT User output file Output 2 CTSFIL CTS file Output 3 ATSFil, ATS file Output 1 Pl!!'FHf POSTEH7 plot file Output 10

' These names are variables in the code. The names of these files are defined via the user input file cards VUE.FIL and SIM.FIL 2 This file is generated only if IPl!!'= 1 in the CONTHOL card of the user input file.

Script Files Two script files are available to execute the ASAS code. The first such script file is ASAPHOC, and is shown in Figure 9. It executes the code in a stand alone fashion. The script file is executed with the conunand ASAPHOC $1<er>, where $1 is a user supplied ID, and <er> is a carriage return.

For example, in the sample case, $1 is TEST 1. Therefore the user input file is ASATEST1.IN, and the output files are ASATESTI.OUT, ASATESTI. CTS, ASATEST1.ATS, and ASATEST1. PLT.

The second script file in FLYPHOC, and is shown in Figure 10. This script file generates a SIMULATE-3 CEA insertion input file, calls the script file to execute SIMULATE.3, then generates an AFAS input file and executes ASAS for that case. FLYPitOC is set up to generate a ID ATS file, and processes only one user-selected assena>ly. It was developed by Yankee and OPPD to execute on the OPPD llP DOMAIN workstation, and execute the SlMULATE-3 case on the OPPD lHM computer.

FLYPROC is executed with the command FLYPItOC $1 $2 $3 $4 $5ccr>

where:

$1 is the loading pattern identifier,

$2 is the time in cycle life (H for BOC, in which case COR.llOR is net to 95G ppm; M for MOC, n which case Colt.llOR is set to 586 ppm; and E for EOC, in which case COR.UOH is set to

-88 ppmh

$3 is the two digit serluence number of the run (typically starting at 00 and ending at 99),

$4 is the oscillation time in hours (for the purposes of selecting the appropriate restart), and

$5 is the cycle number.

FLYPHOC is submitted for 100 time points by the script file Aboesub, which is shown in Figure 11. These time points were selected from the axial shape index plot shown in Figure 4.

ASAS mnual llevu, ion o 22 Apnl 19,1994

Auxiliary Code An auxiliary computer code CONCAT.F is shown in Figure 12. This code concatenates multiple CTS and ATS files into a master CTS and ATS file, sorts the cases, and changes the Case ID's for use by OPPD'c safety analysis codes. This code was developed by OPPD.

l ASAS Manual Itensmn 0 23 April 19,1994

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OUTPUT FILE DESCRIPTIONS l l

The four output files are described below. Three of these files are shown in Figures 13 through 15 for the sample case, and Figure 16 shows several of the plots generated with the ASAS output plot file.

User Output File This file is in a format for readability by the user. The contents of this file are controlled by the IOUT option. The following information is printed if IOUT is 0 or 1: i The input echo, the input data used in the run, selected assembly edits, and for each selected assembly the following: ,

  • XPO - cycle exposure,
  • EBAR - core average exposure,
  • POWER - power level in percent,
  • FLOW - core flow in percent,
  • NOTWT - total control rod steps inserted into the core,
  • FQ - 3D pin peaking from the SIMULATE-3 pin file, which includes the axial intranodal peaking (this is also called the 4 PIN edit in SIMULATE-3),
  • INCORE ASI - In-core average axial shape index,
  • PERIPIIERAL ASI - Ex-core weighted axial shape index, '
  • TOTAL RELATIVE EXCORE SIGNAL,
  • FUEL TYPE,
  • ASSEMBLY NUMBER, and
  • ASSEMBLY SERIAL NUMBER.

Adiusted 2D Pin Powers:

  • 2D PIN POWERS. These are adjusted by the ratio of the assembly average axial peaking factor to the pin axial peaking factor in order to preserve the peak LHGR for each pin when using the core average axial shape. Also the grid dip factor FGRID is ,

applied to these 2D pin powers.

Assembly Information:

  • MAXIMUM 2D ONE PIN POWER
  • MAXIMUM 2D ONE PIN POWER WITH UNCERTAINTIES
  • MAXIMUM CHANNEL POWER
  • MAXIMUM 3D ONE PIN POWER
  • MAXIMUM 3D ONE PIN POWER WITH UNCERTAINTIES
  • MAXIMUM LHGR WITH UNCERTAINTY
  • PL TO FUEL DESIGN SAFDL WITH UNCERTAINTIES
  • ASSEMBLY AXIAL SHAPE INDEX
  • ASSEMBLY AXIAL SHAPE INDEX WITH UNCERTAINTY IfIOUT is equal to 1, then the following additional data are printed for each winning assembly:
  • PIN POWERS FOR THE LIMITING AXIAL PLANE ,

a FZ FACTORS - axial peaking factors for each pin in the assembly

  • ASSEMBLY AVERAGE PEAKING FACTOR.
  • 2D PIN POWERS - as read from the SIMULATE-3 pin file.

ASAS Manual Redsion 0 24 April 19,1994 -

y I

l The sample case user output file is shown in Figure 13.

Core Transient Output File (CTS File) l This file contains one header card and a card of data for each winning assembly in each case.  :

The format of the file is determined by the user via the EDT. REQ input cards.

The first field provides the case number, and the second field provides a 10 character CASEID delimited by double o"otes ("). The first 8 characters of the CASEID is the first 8 characters of the case title provided by the user via the TIT,CAS card; the ninth character is the fuel type of the winning assembly number (1 thus the limit on 9 for NFT in the CONTROL card); and the tenth character is the winning assembly sequence number (hopefully less than 9, or ASAS will terminate execution with an error message). P Subsequent fields, from 1 to 12 additional fields, are defined via the EDT. REQ cards. The allowable edit requests are provided in the Input Instructions - User Input File section of this ,

manual.

The format of this file is (15,3X,A12,1X,NE15.0), where N is the number of data requests.

For edit requests "FZLOC-FISS", "FZLOC-THRM", "ASSEMIlLY #", or "F-DELH LOC", the field is written in (19,6X) format instead of(E15.6) format.

The CTS output file for the sample case is shown in Figure 14.

Axial Transient Output File FATS File)

This file contains one set of data for each winning assembly of each case. This data consists of the following: ,

  • The number of axial nodes written in format (15). ,
  • The number of fields on file written in format (15). IfIATS=0, this is 1. IfIATS=1, this is 2.
  • The case number written in format (15).
  • The 10 digit Case ID delimited by double quotes ("). The first 8 characters of the Case 1 ID is the first 8 characters of the case title provided by the user via the TIT.CAS card; the ninth character is the fuel type of the winning assembly number (1 thus the
  • limit on 9 for NFT in the CONTROL card); and the tenth character is the winning assembly sequence number (hopefully less than 9, or ASAS will terminate execution with an error message). This is written in format (1X,A12).
  • The percent full power written in format (F11.3).
  • The Core Average ASI written in format (E15.5). ,
  • The Radial Peaking Factor (read from User Input via the TIT.CAS card). This is written in format (F11.5).

ASAS Manual Revision o 25 April 19,1994 l

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  • The Axial Peaking Factor determined as the maximum plane of the core average axial shape fit to NPLFIT planes. This is written in format (F11.5).

l

  • The Assembly Peaking Factor determined as the maximum plane of the assembly j average axial shape fit to NPLFIT planes. This is written in format (F11.5). l
  • The assembly number (according to the Figure I numbering scheme), written in format ,

(I5). -

  • The reason for selection of the assembly, delimited in double quotes and written in format (1X,A16).
  • The header card for the axial power shape data.

If IATS=1, it reads:

"K" "RPOW-IIPTII " " ASS-AXIAL" '

If IATS=0, it reads:

"K" "RPOW-IIPTII "

These character strings are delimited in double quotes and written in format (1X,A3,2X,A12,2X,A12)

  • The axial plane and the core average axial power shape (and the assembly average  :

axial power shape if IATS=1) fit to NPLFIT axial planes, written in format (14,2F12.5),

with axial plane 1 the bottom, and axial plane NPLFIT the top.

  • IfIATS=1, the header card for the 2D radial pin powers for the winning assembly.

This card is: >

ASSEMBLY 2D PIN POWERS and is written in format (A22). i

  • IfIATS=1, the 2D radial pin powers, written format (14F8.4).

The ATS output file for the sample case is shown in Figure 15. .

Plot File i

This file contains POSTSCRIPT plot commands to generate one plot for the core average axial shape and each winning assembly for each case run. Each plot contains a histogram of the NPIANE axial plane data, a smooth fit generated from the area-preserving natural spline fit coeflicients, and a histogram of the resulting NPLFIT axial plane data. This file is generated )

on option (IPIll'=1 in the CONTROL card of the user input file). In order to plot this, a l POSTSCRIPT plot file is required, and the file POSTER. TOP must be added to the top of the '

plot file. Two of the plots from the sample case are shown in Figure 16 and POSTER. TOP is ,

shown in Figure 17. l l

i I l ASAS Mnual Revision 0 26 April 19,1994

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l 1

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Figure 1 i

' ASAS and SIMULATE-3 Assembly Numbering Schemes 1 ASAS Assembly Number..... ........ 1 2 l SIMULATE-3 Assembly Number.. . . . . 39 38 ,

?

3 4 5 6 7 37 36 35 34 33 ,

8 9 10 11 12 23

)

32 31 30 29 28 27 14 15 16 17 18 19 s

26 25 24 23 22 21 p_ .

20 21 22 23 24 25 19 18 17 16 15 14 l 26 20 27 28 29 30 31 32 12 11 10 9 8 7 33 l-13 34 35 36 37 38 39 6 5 4 3 2 1 I

P P

ASAS Manual Revision 0 27 April 19,1994 ,

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Figure 2 SIMUIATE-3 Input File for Cycle 15 As-Built Depletion

  • LTM' THis is A 3-0 DtPLEff 0N FOR CYCLE 13 Af ftJILT

' TIT.CA$' ' CYCLE IS ASBUl!.T DEPLETION'/

' PES' ' / P PG3 / Sp /OPPD/ aloelte , c' . 0. 0 /

'ITE.Bom',850 0/ I s

l 'OEP.sTA' ' AVE' O 0.0 25,0,50,-o.S.1.0.-o.S.12.0, o.5.14.0.14.2/

l 'CVR.0FE' 100./

l

} 'PRI.stA' 50** '/

i 'PRI.5TA' '2RPF' '2RPD' '2FXP' '2KINP'/ ]

j

' PIN.EDT' 50* 't

' PIN.EI4' 'ON' 'SUMM' '2 PIN' '2kWF"

  • 2 Pli) * '2P/N' '2NPO'/

' PIN. BUM' '3PP2' ')PPF' '3 FIN' ')EXP'/

'ITE. LIM',1.0000.1,0.0000005.0.000005....,40/

' WF R ' , ' /P PG)/sp/0 PPD / sloc1'>d. r * ,0. 50. 6. 00.14. 20/

' ET A' /

'END'/

1

(<

.l ASAS Manual Rem %n 0 28 April 19,1994

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Figure 3 SIMUIATE-3 Input File for Cycle 15 BOC Xenon Oscillation

'717.RUN' 'SJOABos"/

' DIM. CAL' 16 2 3 1/

'COR.SYM',*MIR'/

  • TIT.CAS'.'C15 500 Mwo/trr 1000 PPM. BANK 4 INSERTED 404 NO IUPPLEN 75% KMTR' f

' 9 ES * , - / R PG j /Sp/OPPD / 3 )OCl 5d . t ' ,0. $ 00 /

'COR.0FE',73.0/

'COR.BOR',1000 /

' IT E . KEF * /

'COR. TIN',541.00/

'DEP.HR$*.' AVE' 0.0 -1.0 8.0/

  • CED.5EC' 4. 756/* BANK 4 40% inserted (60% of 1260
  • 756)

'5EG.T7V'.0.850.00,0.0,0.0/

'TAs .Tru' 1 0 ' EXP' 10 ' POW' 1 0.0 2.0 5.0 10.0 15.0 20.0 30.0 40.0 S0.0 60.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0 0.c 0.0 0.0 0.0/

'PRI,STA' $0* */

' P1N . ELfr * ' Ort'/

' PRI . ET A' , ' OFF ' /

' PIN . StfM ' 50* 'I

' BAT . EITf ' , ' CFF ' /

' EPM.CHF','PFPMIT'/

' WPE' , ' / PUB /ept ratiemp /OFFD/ s30ADoa . : * , 8. 0 /

'STA'/

' TIT.CAS','C15 BOC 1500 mwd /MTl 1000 PPM. ANO, 1004 Kurn 8 50 HOl?R OSCILt.AT3ON' /

'COM.0FE'.100.0/

'COR. TIN'.54).00/

'DEP.MPS',* AVE

  • 8.0. 0.S 50.0/

'CFD. SEQ' 4, 12 f,0 /

  • B ANK 4 100% wit hdI nwn

'WRE ' , ' / pun ispinriesp /CPt pt a 30A50s . r ' to,C/

  • STA'/

' TIT.CAS* 'C3% DOC 1500 MWD /MTl 1000 PrM, ARo, 1004 P(MER 50-80 HOUR osCILI.ATION' /

't'EP.HPS' ' AVE' $0.0,-0.5.90.0/

' WP E ' , / PUB /8finnesp/OPPD/s30Abos.r' -60.0/

'STA'/

  • END'/

ASAS Manual itevision 0 29 April 19,1994 ,

i l

1 l

l i

Figure 4 l Axial Shape Index Versus Oscillation Time for Sample SIMULATE-3 Xenon Oscillation Case 8

f

-8

.a -8 W o )0 9

o 2 .) < o o f- 0

..oc Z 'vy r R O

F 5 '

=! ^oc , en o -

C

- g cc w o D O '3 C oo g0- @

i u) b e

  1. 4.

_ .ge w i -Z

> / 9 H

l x

w oC O o O )e d n U o0 Z v

+

4 to

,o w p0 0 0

<C -

,f., '

I ((

O J

k- Uo o n

1 g C o X 0 '-. O ,C D

<C Oc g ,

Oo

'oC 3oC o O

(51

. -l O

c

, , , o 9 9 9 h 9 9 9 9 4 9 9 N O 9 9 9 h 9 9 o e o o o o o o o o.o" o 9o 999o 9 o 9i X3ONI 3dVHS 7VlXV 3 BOON!

ASAS Planual Revision 0 30 Apnl 19,1994 - 1 l

l

Figure 5 SIMULATE-3 Input File for 3D Pin Power File Generation for the ASAS Sample Case Page 1 of 2

' TIT.RUN' ' S3MEST' /

' TIT.CAS' 'C15 500 mwd /MT 1000 PPM. 10.5 HOURS. 2004 POWER. ARO. PDII. A'/

' F ES * . * / PUB / spi nnesp/OPPD/ s 30ABos . r ' ,10. 5 /

'DEP.FFD*,0/

' COB.CFr*,100.0/

'cCR. BOP'.1000./

'JTE.EEF'/

'COR. TIN',543.00/

'EEG TFU' 1 .000000E+00 324.93 -29.21 /

'SEG.TFU' 2 ,000D00E+00 324.93 -29.21 /

'SEG.TFU' 3 .000000E+00 324.9) -29.21 /

'SEG.TFU' 4 .000000E+00 324.93 29.21 /

'$EG.TFU' 5 .000000E400 324.93 $29.21 /

'SEG,TFU' 6 .000000F+00 324.93 -29.21 /

'sEG.TFU' 7 .000000E*00 324.93 -29.21 /

'SEG.TFU' 8 .000000E+00 324.93 -29.21 /

  • BEG.TFU' 9 .000000t+00 324.93 -29.21 /

'sEG.TFU' 10 .000000E+00 283.74 -25.96 /

'SEG.TFU' 11 .000000E+00 283.74 -25.96 /

'SEG.TFU' 12 .00000cE+00 283.74 -25.96 /

'SEG.TFU' 13 .000000E+00 283.74 -25.96 /

"EEG.TFU' 14 .000000E+00 283.74 -25.96 /

'SEO.TFU' 15 .000000E+00 283.74 -25.96 /

' S F:G . TFU" 16 .000000E+00 283.74 -25.96 /

'SEG.TFU' 17 .000000E+00 324.93 -29.21 /

'SEG.TFU' 18 .000000E+00 324.93 -29.21 t "SEG,TFU" 19 .000000E*UD 324.93 -29.21 /

'SEG.TFU' 20 .000000E+00 J20.1 -24.73 /

'SEG.TFU' 21 .000000E 00 320.1 -24.73 /

' SEG.TFtJ* 22 .000000E+00 320.1 -24.73 /

  • SEG.TFU* 23 .000000E+00 320.1 -24.73 /

'SEG.TFU' 24 .000000E+00 320.1 -24.73 /

i *SEG.TFU' 25 .000000E*00 320.1 -24.73 /

'SEG.TPU' 26 .000000E*00 320.1 -24.73 /

  • SEG.TFU' 27 .000000Ee00 320.1 -24.?3 /

'SEO.TFU' 28 .000000E+00 320.1 -24.7J /

'SFG.TFU' 29 .000000E+00 283.74 -25.96 /

'SEG.TFU' 30 .000000E+00 283.74 -25.96 /

'SEG.TFU' 31 .000000E+00 283.74 -25.96 /

'SEG.TFU' 32 .000D00E*00 283.74 -25.96 /

  • EEG.TPU' 33 .000000E+00 283.74 -25.96 /

'SEG.TFU' 34 .000000E+00 281.74 -25.96 /

'5EG.TFU' n .000000E+00 28).74 -25.96 /

'SEG.TFU' 36 .000000E+00 283.74 -25.96 /

'$EG.TFU' 37 000000E*00 263.74 -25.96 /

' S EG . T FU' 38 .000000E+00 324.93 -29.21 / e

'SEG.TFU' 39 .000000E+00 324.93 -29.21 /

'SEG,TFU" 40 .000000E+00 324.93 -29.21 /

' TAB.TFU' i1 *EXP' 10 ' Pow 1 ,

.000000E*00 2.0 5.0 10.0 15.0 20.0 30.0 40.0 50.0 60.0 1.0 61.27 54.04 53.87 33.07 16.16 .45 -28.39 -57.29 -70.43 -70.62 /

'TAS.TFU" 1 2/

' TAB.TFU' 1 3/ '

' TAB.TFU' 1 4/ '

' TAB.TFU' 1 5/

' TAD.TFU' 1 6/

' TAD.TFU* 17/

'TAS TFU' 1 8/

' TAB tFU' I 9/

' TAR.TFU' 1 17!

' TAD.TFV* 1 18/

'T.b..FU' 1 19/

' TAB.TFU' 1 38/

' TAB . T FU ' 1 39/

' TAD.TFU' 1 40/

' TAB.TFv' 2 20 'EXP+ 10 ' Pow' 1

.000000E+00 2.0 5 0 10.0 15.0 20.0 30.0 40.0 50.0 60.0 1.0 49.02 56.15 50.65 15.32 22.3 10.78 -9,67 -29.48 -42.75 -43.56 /

' TAB .T FO ' 2 21/

' TAB.TFU' 2 22/

' TAB.TPU- 2 23/

' TAB .*f rU' 2 24/

' TAB.TFU' 2 25/

' T Ap .TFU' 2 26/

' TAB.TFU' 2 27/

' TAB.TFU' 2 20/

' TAB.Trud 3 10 ExF' 10 ' PCW ' 1

.000000r+00 2.0 5.0 10.0 15.0 20.0 30.0 40.0 '>0.0 60.0 1.0 60.14 53.91 63.7 31.47 8.16 -17.51 -52.77 -57.87 -59.28 -57.4 /

' TAB.TFU* 3 11/

  • T AB .TFU' 3 12/

' TAD.TFU' 3 13/

' TAB.TFU" 3 14.'

' TAB.TFU' 3 15/

' TAB.TFU' 3 16/

' TAB.TFU" 3 29/

' TAB.TFU' 3 30/

' TAB.TFU' 3 31/

' TAB.TFU' 3 32/

  • TAB.TFU 3 33/

' TAB.TFU' 3 34/

' TAB.TFU' 3 35i

  • TAB.TFU' 3 361 ASAS Manual Revision 0 31 April 19,1994

+ -

l 1

1 Figure 5 SIMULATE-3 Input File for 3D Pin Power File Generation >

for the ASAS Sample Case Page 2 of 2

  • TAs.TFU' 3 31/

' COM '.

'CoM' Pass 1 2 3 4 5 6 7 8 9 10 11

  • CPD. SEQ
  • 1. 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260/* BANK 1
  • cRD.szo* 2, 12601260 1260126012601260126012601260 12601260/* BANK 2
  • CRD, SEQ' 3, 1260 1260 1260 1260 1218 1057 896 715 574 413 268/* BANK 3

'CRD SEQ' 4, 1260 945 784 623 462 301 140 0 0 0 0/* BANr 4

'CRD. 8EQ' 5, 12 60 1260 126 0 1260 12 60 12 60 1260 1760 12 60 12 60 1260/

  • BANK A

'CRD. 5EQ' 6, 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260/* BANK B

'CRD. SEQ' 7, 1260 1260 1260 1260 1260 1260 1260 1760 1260 1260 1260/* BANK N

'CRD. SEQ' 8, 1260 1360 1260 1260 1260 1260 1260 1260 1260 1260 1260 /* HATN1UM RODS

'CRD. PAS' 8.1/

'P3N.FIL','ON','PINFILE',' ADD *,*3*D'/

'PPI.sTA', 50* */

' PIN . EIff ' 'ON',,'2 PIN'/

'STA'/

' TIT.CAS','C15 $00 mwd /NT 1000 PPM, 10.$ HOURS, 20% POWER. BANK ) AT $74, PDIL J'/

' CDP. OPE', 20.0/

'COR. TIN'.635.10/

'CRD. PAS',8,9/

'STA"/

'END'/

I t

S ASAS Manual Revision o 32 April 19,1994 -

_2 _ _ _ , . . _ _ . _ - ,2-

Figure 6 Suggested SIMULATE-3 CEA Insertion Cases For Setpoint Analysis PDIL Inlet Case Power Level Temp (*F) CEA Positions A 100 543.0 ARO B 100' 543.0 Bank 4 at 945 C 90 543.0 Bank 4 at 945 D 80 543.0- Bank 4 at 784 E 70 543.0 Bank 4 at 623 F 60 541.4 Bank 4 at 462 Bank 3 at 1218 G 50 539.9 Bank 4 at 301, Bank 3 at 1057 11 40 538.3 Bank 4 at 140, Bank 3 at 896 I 30 536.7 Bank 3 at 735 J 20 535.1 Bank 3 at 574 K 10 533.6 Bank 3 at 413 L 1 532.16 Bank 3 at 268

- 0 532.0 Bank 3 at 252 i

ASAS Manuni llevision o 33 April 19,1994

, ~. _

Figure 7 Sample View Factor File I)ouge 1 of 6 1

0014306 .0014306 .0014306 .0014306 0014306 .0014106 .0014106 ,0014306 .0014306 .0014)06 .0014304 0014306

.0014106 .0014306 .0014306 ,0014306 .0014306 .0014306 .0014306 .0014304 .0014306 .0014306 0014306 0014306 .0014306 .0014306

.0014306 .0014306 .0014306 0014306 .0014306 .0014106 0014306 .0014306 .0034306 .0014306 .0014306 .0014306 .0014306,0014306

.0014)D6 .0014304

,0014306 .0014306 .0014306 .0014306 .0014306 0014306 ,0034306 .0014306 0014306 .0014306 .0014306 .0014306 .0014306 .0014306 .;

.0014306 0014306 .0014306 .0014306 .0014306 .0014306 .0014306 .0034306 .0014306 .0014306 .0014306 .0014306 ,0014306 .0014306

.0014306 .0014306 0014306 .0014306 .0014306

.0014306 .0014306 .0014306 .0014306 .0014306 .0014306.^014106

.0014306.0014106 .0014306

.0014306 .0014306 .0014306

.0014306 .0014304

.0014306 .0014306

.0014306 0014306 .0014306

.0014306 .0014306 .0014306

.0014306 .0014306 .0014306 0014306 .0014306 .0014306 .0014306 .0014304 .0014306 .0014306 .0014306 .0014306 .0014306 . 0014306

.0014306 .0014306 0014306 .0014)06 .0014306 .0014306 .0014306 .0014306 .0014)06 .0014306 .0014306 ,0014306 .0034306 .0014306

.0014306 .0014306 .0014306 .0014306 .0014306 .0014306 .0014506 .0014306 .0034306 .0014306 .0014306 .0014306 .0014306 .0014306

.0014306 0014306 0014106 .0014306 .0014306 .0014306 .0014306 .0014106 .0014306 .0014306 .0014306 0014306 .0014306 .0014306

.0014306 0014106 .0014306 .0014306 .0014306 .0014306 .0014306 .0014304 001410e .0014306-.0014306 .0014304 .001430s .0014306 0014306 0014306 .0014306 .0014306 .0014306 .0014306 .0014306 0014306 .0014306 .0014306 .0014306 .0014306 .0014)06 .0014306

.0014306 .0014306 .0014306 .0014306 0034306 .0014306 .0014306 .0014306 .0014306 .0014306 ,0014306 .0014306 .0014306 .0014306 3

.0001500 .0007500 .0007500 .0007500 .000'500 .0007500 0007500 .0001500 0007500 .0001500 .0007500 .0007500 .0007500 .0007500

.0007300 0007500 .0007500 .0007500 .0007500 .0007500 .0001500 .0007500 .000?S00 ,0007500 .0007500 .0007S00 .0007500 .0007500

.0007500 0001??0 0007500 0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0091500 .0007500 .0007500 .0001500

.0007500 .0007500 .0001500 .0001500 .0007500 .0007500 .0007500 .0001500 .0007500 .0007S00 .0007500 .0001%00 0007500 .0001500

.0007500 .0007500 0007500 .0007500 .0007S00 .0007500 .0007500 .0007t00 .0007500 .0007500 .0007500 0007300 .0007500 .0007500

.0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0007500 .0001500 .0007500 40007500 .0007500

.0007500 .0007500 .0007500 .0007500 .0001$00 .0007%00 .0007500 .0007500 .0007500 .000?500 .0007S00 .0007500 .0001500 0007500

.0007500 .0007$00 .0007500 .0007500 .0007500 ,0007S00 .0007500 .0007500 .0001500 .0007500 .0001500 .0007500 .0007500 .0007S00

,0007500 .0007507 .0007$00 .0007S00 .0007500 .0007S00 .0007500 .0007%00 .0007%00 0007$00 .0007500 .0007900 . 0007500 .0007S00

.0007500 .0007500 .0007500 .0007500 .0007500 .0007500 0007500 .0007500 0007500 .0007500 .0007$00 .0007500 i .0607S00 .0001500 .0001500 .00D7500 .0007500 .0007%DO .0007500 .0007500 .0007500 .0007500 .0007500 .0007400 0007%00 .0007500.0001300 .0007500

.b007500 .0007S00 .0007500 .0007500 .0007S00 ,0007500 .0007500 .0007500 .000'500 .0007500 .0001500 .000'500 .0007500 0007500 0007600 .0007500 ,0007500 0001500 0007500 0007500 ,0007S00 .000?$00 0007500 .0007500 .0007S00 .0007500 0001S00 .0007300

,0007500 .0007500 0007$00 0007500 0007500 .0007500 0007300 .000?$00 .0007300 .0007500 0007500 .0007500 .0007500 0007S00 1

0009974 .0009974 0009914 ,0009974 .0009974 .0009974 .0009914 .0009974 .0009974 .0009974 0009974 .0009974

.0009914 .0009974 0009974 .0009974 .0009974 0009974 .0009974 0009974 .0009974 .0009974 .0009914 0009974 .0009974 .0009974 0009974 .0009974

,00099?4 .0009974 .0009974 00099's .0009974 .00099't .0009974 .0009974 0009974 .0009974 .0009974 .0009974 .0009974 .0009974 0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974 0009474 0009974 .0009974 .0009974 .0009974

.0009974 0009974 .0009974 .0009914 .0009974 .00t9914 .0009974 .0009974 .00C9974 .0009914 0009974 .0039974 .0009974 .0009314

.0009974 0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009914 0009974 ,0009974 .00099'4.0009974

.0009974 .0009974 0009974 .0009974 .0009974 .00099'4 0009974 .0009974 .0009914 .0009974 .0009974 .0009974 .0009974 .00099'4 .0009914 .0009974 0009914 .0009974 .0009974 0009974 .0009974 0009974 0009974 .00099'd .0009974 .0009974 .0009974 .0009974 .0009974 .0009974 0009974 0009974 .0009974 .0009974 .00099'4 .0009974 .0009974 0009974 .0009974 .0009974 0009974 .0009974 .0009974 .0009914

.0009974 .0009914 .0009974 .0009914 .0009974 .0009974 00099?4 .0009974 .0009974 .0009974 .00099'd .0009974

.00099'd .0009974 .0009974 .0009974 .0009974 .0009974 ,0009994 .0009974 .0009974 .0009974 .0009974 .0009914 .0009974 .0009974.0009974 00099?4

.0009974 .0009974 .0009914 .0009974 .0009914 .0009914 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974  ;

.0009974 0009974 .0009974 0009974 .0009974 .0009974 .0009974 0009974 .0009974 .0009974 .0009974 .0009974 .0009974 .0009974

.0009974 .00099'4 .000vv14 ,0009974 .0009974 .0009974 .0009974 .0009974 .0009914 .0009974 .0009914 .0009974 .0009974 .00099?4 4

.0007357 0601351 .0007)S7 .0007357 0007357 .0007357 .0007357 .0001357 .0007357 .0007357 .0001357 .0007357 0001357 .0007357

.0007357 0001357 0007357 .0001357 ,0007357 .0007357 .0007357 .0007351 .0007357 .0007357 .0007357 ,0007357 .0007357 .0007357

.0007357 .0001357 0007357 0007357 0007357 .0001357 .0007357 .0007351 .0007357 .0001357 .0007357 .0007357 .0097357 0007357 0001357 0007357 0001351 .0007357 .0007357 0007357 .0007357 .0007151 .0007351 .0007357 .0D07357 .0007357 0001357 .0007351

.0007357 ,0007.357 0007357 .000?)S7 .0001357 .0007151 ,0007357 .00073t? .0007351 .0001357 0007357 .0007357 ,0007357 .0007357 0001357 0007)57 000?357 .0007357 .0007357 0007357 0007557 .0007157 .0007357 .0007357 ,0007357 .0007357 .0007357 .0007357 0007357 .0007357 .0007351 .0007357 .0001357 .0007357 ,0007357 .0007357 000735* .0007357 .0007357 ,0007357 0007357 .0007357

.0007357 .0007357 .00073%7 0007357 .0007351 .0007357 .0001357 0007357 .0007357 .0007357 .0007357 .0007357 .0007351 .0007357

.00D7357 .0007357 .0007357 .000735? .0907357 .0007357 .0007357 ,D007351 0007357 .0001357 .0007351 .0007357 0007157 .0007351

.0007351 .0007357 .0001357 .0007357 .0007357 .0007351 ,0007357 .0001357 .0007357 .0001357 .0007357 .0007357 .0007J57 .0007357

.0007357 .0001357 .0007357 .0007)ST .0001357 ,0007357 .0001357 .0007397 .0007351 .0001357 .00073f? .0007357 .0007351 .0007357

.0007357 .0001357 0007357 .0007357 .0007357 0007357 .0007157 .0007357 .0007357 .0001357 .000 " 57 .0001351 .0007357 ,0007357 0007357 0007357 .0007357 ,0007357 0007351 .000?357 .0007357 .0007357 ,0007357 .0001357 .0007357 .0007357 0007351 .0007351 0007357 .0001357 0001357 .0001357 .0001357 .0007357 .0007357 .0007357 .0007357 .0007357 .0007351 .0007357 .0007357 .0007357 5

0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 0003959 .0003959 .0003959 .0003959 .0003959 .0003959 0003959

.0003959 .0003959 0003959 0003959 ,0003959 .0003959 ,0003959 ,0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 0003959 .0003959 .0003959 .000)959 .0003959 ,0003959 .0003959 .0003959 000!959 .0003'359 .0003959 .0003959 .0003959 .0003959

.000Tw59 ,000395# 00D3959 .0001959 0003959 .0003959 .0003959 .0003959 ,0003959 .0003959 .000)959 .0003959 .0003959 .0003959

.0003959 0003959 .0C03959 .D00t959 .0003959 0003959 .0003959 0003959 0003959 .0003959 0001959 ,0003959 ,0003959 .0003959

.0003959 0003959 0003959 0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 ,0003959 .0003959 .0003959 .0003959

.0003959 .0003t?9 ,0003959 .0003959 .0003959 .0003959 0003959 .0003959 .0003959 .0003959 .000J959 .0003959 .0003959 0003959

.0003559 0001959 .0003959 0003959 00039t9 0003959 0003959 .0003959 0003959 .0003959 .0003959 .0003959 .0003959 .0003959

.0003959 0003959 0003959 0003959 .0003959 .0003959 .0003959 .0003959 0003959 .0001959 .0003959 0003959 .0003959 .0003959

.000J959 .0003159 0001959 .0003959 Oc03959 .0003959 .0003959 .0003959 .0003959 .0003959 ,0003959 .0003959 .0003959 .0003959

.0001959 0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0003959 .0001959 0003959 ,0001959 0003959 .0003959 0003959 ,0003959

.0003959C003959

.000)959 .0003959.0003959

.0003959.0003759

.0003959 .0003959

.0003959 0003959 .0003959.0003959

.0D03959.0003959 0003959 .0003959

.0003959 ,0003959

.0003959 .0003959

.0003959,0003959

.0003959

.0003959 0003959

.0003959

. .0003959

.000)959 .0003959 .0003959 0003959 ,000.3959 0003959 .0003959 0003959 8

.0001857 .0001857 .000185? 0001857 0001857 00C1857 0001857 .0001857 .0001857 0001857 .0001857 .0001857 .0001857 .0001857

.00018t7 .0001851 .0001857 .0001857 0001857 0001857 0001857 .0001857 0001857 .0001857 .0001857 .0001857 .0001851 .0001851

.0001857 .0001857 .0003657 00018t* .0001857 0001857 40001857 .0001857 .0001857 0001857 .0001857 ,0001857 .0001857 .0001857

.0001857 .0001857 .0001857 00n1851 .0001857 .0001857 0001851 .0001851 0001857 .0001857 .0001857 .0001851 .0001857 .0001k57 0001857 ,0001857 .0D01857 ,0001857 .0001857 .0001857 0001851 0001851 .0001854 .0001857 .0001851 .0001857 ,0001851 .0001851 0001857 0001857 0001857 .u001857 .0001857 .0001851 .0001857 .0001851 .0001857 .0001857 .0001857 .0001857

.0001851 .0001857 0001857 .0001851 .0001851 0001857 0001857 .0001857 .0001857 .0001857 .0001857 .0001857 .0D01857 .0001857

.0001858 .0001851

.0001851 .0001851

.0001857 .0001857 .0001R57

.0001857 .0001857 .0001851

,0001857 .0001857 .0001851 .0001851 .0001857 0003851 .0001857.0001857

.0001857 .0001857

.0001857 .0001857 00n1857 .0001857 ,0001857 0001857 .0001857 .0001857.0001857

.0001857 .0001857

.0001851 .0001857 0001857 .0001857

.0001857 .0001857 .0001857.0001851

.0001857 00C1851 .0001857 0001851 0001857 0001851 .0003851 .C001457 .0001857 .000185? .0001857 .0001857 .0001857 .0001857 .0001857 . .0001851 .0001857 0001857 .D001857 .0001851 .0001857 .0001857 .0001857 .0001857 .0001857 .0001857 .0001857 .0001851 .0001821 .C001857 .0001857 0001851 .0001851

.0001857 .0001857 0001851 00cIB57 ,0001851 .0001857 .0001857

.0003857 ,0001857

.00018570001857 .0001857.0001857

.0001857.0001857

.0001857 .0001851 0001857.0001851

.0001857.0001851

.0001857.0001857

.0001857..0001857 .0001857 7

.0001388 0001388 .0001388 .0001381 .0001388 .0001188 .0001388 .0001388 .0001388 .0001388 0001388 0001388 0001388 .000138a

.0001388 0001388 0001398 .0001388 .0001388 .0001388 -0001388 .0001388 .0001388 .0001388 ,0001388 0001388 ..000.1398 .0001388

.0J01388 0001388 00D1384 .0001388 .0001388 .0001388 .0001388 0001388 .0001388 .0001388 .0001388 ,0001388 .0001388 0001388 0001386 .0001188 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388 .0001388

.0001388 .0001388 .0001388 .0001138 .0001388 .0001388 .0001388 .0001388 .0001368 .0001388 .0001368 .0001388 <0001388 0001388

.000L388 .0001388 .0001388 000138e .0001388 .0001388 .0001388 .0001388 .0001388 .0001188 .0001388 .0001388 .0001384 .0001388 0001198 .00G1388 .0001.188 .0001388 0001388 .00013d8 0001388 .0001388 0001389 0001389 .0001388 .0001388 .0001388 .0002388 0001188 .0001388 .0001386 0001388 0001388 .000138# .0001388 0001388 0001386 .0001388 0001388 .0001386 . 0001388 .0001388 0001389 0001388 .0001388 .0D01388 .0003388 ,0001388 0001388 .00c1388 .00D1388 _00C1388 0001388 .0001188 .0001388 .0001388 0001398 0001388 0001388 .DD01385 .0001388 ,00013P8

' .00C3388 0001388 .0001388 .0001388 .0001388 0001188 .0001398 .c301198 ,0001388 0001348 .0001388 .0001388 0001389 .0001388 D001188 .0001388 0001388 .0001388 0001388 .0001386 0001388 .0001388

.0001388 0001388

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.0001388 0001388 .00c1388 .0001388 ASAS Manual Revision o 34 April 19,1994

i Figure 7 Sample View Factor File ,i I) age 2 crf (3 l 0001388 .0001388 .0001388 .0001388 .0001388 .0001388 ,0001388 .0001388 .0001388 ,0001388 .0001388 .0001388 .0001388 .0001388 l

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.0000000 .0030000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .00;rogo .0000000 .0000000 .0000000 .0000000 3 ASAS Manual Revision o 35 April 19,1994

Figure 7

, Sample View Factor File Page 3 of 6

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.0000000 .0000000 ASAS mnual Revision o 3G Apnl 19,1994

- - . . - - . = . . -. - -. . - -- . - . - - - -- . -

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.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 0000000

.0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .00000t0 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000090 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 34 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000'0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000C00 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000010 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 20000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .00000c0 .0000000 .0000000 0000000 0000000 .0000000 .0000000 ,0000000

.0000000 .0000000 .0000000 0000000 .0000000 .000G000 ,0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000.0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 2%

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 <0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 6

.0300000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000C00 0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000

.0000000 .0000000 .0000000 0000000 .0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000

.0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 36

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.00000bo .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 ,0000000 ,0000000 .0000000 .0000000 00D0000 .0000000 0000000 0000000 0000000 ,0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .00D0000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .000D000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .00C0000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 ,0000000 .0000000 ,0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 27

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 ,0000000 .0000000 i

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000004 .0000000 0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000'

.0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000-

.0000000 .0000000 .D000000 .0000000 .0000000 .000C000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 29 0000000 .0000000 0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0003000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000D00 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 ASAS Manual hvision o 37 April 19,1994

_ _ _ _ .~ _ _ - _ . . ._ _

1 l

l l

l F'igrure 7 l Sample View Factor File Page 5 of 6

.0000000 10000000 .0000000 .000000u .0000000 .0000000 .0000000 .0000000 0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 l

.0000000 .0000000 .000000t .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 l 0000000 ,0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0D00000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 40000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 29 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000

.0000000 .0000000

.0000000 .0000000 .0000000

.0000000 .0000000

.0000000 .0000000 0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000

.0000000 .0000000 .0000000 .0000000 ,0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 ,0000000 0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

,0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 ,0000000 0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 10000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 30

.0000000 0000000 0000000 .0000000 0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .00000E0 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000

.0000000 0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000.0000000

.0000000.0000000 .0000000.0000000

.0000000 .0000000 .0000000 0000000

.0000000 0000000 .0000000

.0000000

.0000000 0000000 0000000 0000P00 .0000000 .0000000 6000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 ,0000000 .0000000 .0000000 .0000000 ,0000000 ,0000000 ,0000000 .0000000 0000000 .0000000 .0000000

.0000000 0000000 .0000000 00000.0 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000

_0000000 0000000 0000000 .0001000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .00D0000 .0000000 .000w000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

,0000000 .0000000 0000000 .000dOOw .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 31

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 .000^000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .000e000 .0000000 ,0000000 .0000000

.0000000 .0000000 .0000000 .00an000 .0000000 0000000 .0000000 .0000000

.00000ev .0000000

.J"00000 .0000000 0000000 .0000000

.0000000 0000000

.0000000 .0000000

.0000000 .0000000

.0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .000F000 .0t00000 .0000000 .0000000 .0000000 .0000000 0000000

.0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 . 0030000 ,0(00000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .r000000 .b4^0000 0000000 .0000000 ,0000000 .0000000 .0000000

.000000D .D000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .00006:0 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 0000000 ,0000000 .0000000 ,0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 ,0000000 0000000 .000J000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0c00000 .0000000 .0000000 .0000000 .0000000 .0000000 32

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .00000s0

.00000t0 .0000000

.0000000 0000000

,0000000 .0000000

.0000000 .0000000

.0000000 .0000000

.0000000 .0000000 0000000

.0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,000000. .0000000 .0000000 .0000000 _0000000 0000000 .0000000

.0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0C00000 .C000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 0000000 0000000 .0000000 0000000 0000000 .0000000 0000000 .0000CJO 0000000 000D000 .0000000 .0000000 .0000000 .0000000 20000000 .0000000 .0000000 .0000000 .0000000 0000000 .000C000 .00000vo .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 00n0000 ,0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .000D000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 0000000 .0000000 .0000000

.0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000s00 0000000 0000000 .0000000 .0000000 .00D0000 ,0000000 .0000000 0000000 0000000 0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 33

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 ,0000000 0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 0000000 .0000000 .0000000

,0000000 0000000 0000000 .0000000 ;0000000 0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 D000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 .0000000 .0000000 .0000000 .000D000 D000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 34

.0000000 .0000000 0000000 .0000000 ,00D0000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .00000D0 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 I'

.0000000 .0000000 ,0000000 .0000000 0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 ,0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0D00000 0000000 .0000000 .0000000 "000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000

.0000900 .0000000 .0000000 .00"0000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 ,0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 0000000 ,0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 ,0300000 .0000000 ,0000000 0000000 .0000000 .0000099 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .000D000 0000000 0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 ASAS Manual Revision 0 38 April 19,1994

l Figure 7 Sample View Factor File 1)oy;e 6 ctf 6  ;

)

25

.0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .00000D0 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 36

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0u00000 .0000000 0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .000000D .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0900000 .000000J 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 31

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .000000D .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

,0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0030000

.0000000 0000000 .0000000 .0000000 .0000000 ,0000000 ,0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 30

.0000000 .0000000 .00000D0 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0u00000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 i .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 t

.0000000 .0000000 .0000000 .0000000 .C000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .3500000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 39

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000

! ,0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000

( .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 i .0000000 0000000 .0000000 .0000000 .0000000 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000

,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 ,0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000 0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .00000C0 .0000000 ,0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000

.0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 .0000000 The sam of the view f actor s is .9999983 ASAS Enual Revision 0 39 April 19,1994

Figure 8 ,

Sample ASAS User Input File  !

' TIT.RUN Fort Calhoun Cycle 15 B X 10.5 Hours a asetest CONTROL 22340111 FUE. LIM 1 15.0 ' TYPE 1'  ?

l FUE. LIM 2 16.0

  • TYPE 2' LAY.DWN 1 2 1 2 1 2 1 2 1 2 1 1 2 1 2 1 2 2 1 2 1 2 1 1 2 1 2 1 2 1 2 1 2 1 2. 1 2 WE.FIL f acgent .out COMMDff f cale f tilt ferid fe fealer fdep ftrip fasi UNC.FAC 1.10 1.03 1.0075 1,03 1.02 0.915 3.0 .C4 COR.LHR 6.00 .

TIT.CA5 1 1. 77 00 's 10. 5- A PDIL CAS2 100% POWER, AR0" TIT.CAS 2 2.3320 's-10.5-J PDIL CAir 2C% POWER, BANK 3 AT 574' 8EL. Ass 3 1 10 39 )

81M.FIL / PPG) /Ep/OPPD/s 30t est.p ],

EM. REQ 'ASI. ASS EM.P EQ ' AS!- PER ' l E M.PEQ 'ASI-COPE

- EM.PEQ ' FFDL EM . P EQ ' LHOR W/UNC' KDT.PEQ 'FZLOC-FISS' EM NEQ ' ASSEMBLY 9' EM. P E0 ' EXCOPE PES

  • EX ECVTL l

4

)

ASAS Manual Revision 0 40 April 19,1994 1

')1

, I

_ _ _ ._ -~ _. -- _. ., -

I 1

l Figure 9 l Sample Procedure to Execute ASAS on a HP/UX UNIX Computer i

ft / bin /ksh e I t ASAPROC 5

0 Script file to execute the ASAS code 0

0 This script file is executed by typing the following: -)

i e asaproc $1 <cr> '

0 where 8 $1 is a user supplied ID for the run (for example. 001), and e *cr> is carriage return, e

e The files associated with the run are therefore 8 asall.in - user input file (e.q, ara 001.in)

O asa$1.out - user output file (e.g. asa001.out) ,

e asa$1. cts - CTS output file (e.g. asa001. cts)

  1. asa$1.ats - ATS output file fe.g. asa001.ats) 8 asa$1. pit - POSTSCRIPT plot file (e.g. asa001. pit) 01D=*pwd' day =$0LD/anall day
  • out="$0LD/asa$1.out' in= * $0LD /a sa $ 1. in
  • ct a= " $0LD/ asa $1. ct s " ,

ats=*$0LD/asa$1.ats' pit =*$0LD/asa$1. pit

  • test -f $ day && rm $ day echo '1' >$ day 2 $ day echo ***********************************************************>>$ day 2>>$ day echo * * >>$ day 2n$ day echo * * >>$ day 22>$ day echo * * >>$ day 2n$ day e echo * * >> $d.ay 2n $ day echo
  • Script File to Run ASAS version O' >>$ day 2*>$ day echo * * > > $ day 2 => $ day echo
  • The start date and time is 'date'* >>$ day 2n$ day echo *
  • n$ day 2n$ day 9 echo
  • The username is ' uname -n' * > > $ day 2n$ day e:bo * * >>$ day 2>>$ day echo
  • The input flie is $1n* >>$ day 2=>$ day echo * * >>$ day 2*>$ day echo
  • The user output file is Sout* >>$ day 2>>$ day echo n$ day 2*>$ day echo
  • The output ete file is $ cts' n$ day 2 n$ day eche *
  • n$ day 2>*$ day echo
  • The output ats file is $ ate" >>$ day 2>>$da',

echo n$ day 2 n$ day 9

8 test -f Sout && tm Sout n$ day 2n$ day test -f CTEFIL && rm CTEFIL n$ day ?>>$ day test - f ATSFIL && tm ATSFIL >>$ day 2>>$ day a

9 run job under tmp space on HF workstation 4

9 RUNDIR= * / t mp/ ASA. $ $

  • n$ day 2*>$ day 9 mkdir $RUNDIR p $ day 2 n$ day ,

PUMD1P='pwd' n$ day 2>>$ day echo

  • The run time directory is $PUfD17" n$ day 2n$ day a
  • echo n$ day 2 n$ day ezho *
  • n$ day 2n$ day ed SRtmD1R >>$ day 2=>$ day cp sin USERIN n$ day 2n$ day in -s out,$1 USERCT >>$ day 2=>$ day in -s $ cts CTEFIL n$ day 2n$ day ,

In -s $at e ATSFIL n$ day 2n $ day '

in -s $ pit PLTFIL n$ day 2n$ day s

8 execute ASAS 9

asas 2 n$ day 9

9 normal termination

! t 9 cd SotD >>$ day 2n$ day rm USEROf n$ day 2n$ day rm CTSFIL n$ day 2>>$ day tw ATSFIL >>$ day 2*>$dey re PLTFIL n$ day 2n$ day echo

  • The finish date and tinte is 'date'* >>$ day 2=>$ day echo * * >>$ day 2=>$ day echo ********************************************************* n$ day 2 $ day cat out 81 $ day >$out 2 n$ day rs out.$1 l

l

[

l' I

i ASAS Manual Revision 0 41 April 19,1994 l

, - _ =-. . -. . - ..

Figure 10 Sample Procedure to Generate SIMULATE-3 and ASAS Input Files And Execute the Codes for the Flyspeck Analysis Page1of6 ff / bin /Itsh t

  1. TITLE:

tetti flyproe v1.0 Executes EIMULATE-3 ond ASAS Codes IAuth: 03/15/94 MEC, 03/23/94 RBS 0 Modified by TAH f or Fort Calhoun Cy:le ib 4 /12/94 9

4 COPYRIGiff 1994 YANKEE ATOMIC ELECTRIC COMPANY

  1. Script file to create user input files for SIMULATE-3 and ASAS 8 and execute the codes f or the flyspeck analysis e

i This script file le executed by typing the following:

  1. flyproc $1 $2 $3 $4 $5 <cr*

6 wheret

  1. $1 - $5 are explained below.

O <cr> 1s carriage return.

4

  1. The SIMULATE-3 files associated with the run are those '

9 generated by the a3v402b script file, and are

  1. s30$1$2$3.1 - Input file te.g. s30AB00.il e s30$1$2$3.o - Output file te.g. s30AB00.o)
  1. m30$1$2$3sp- Pin Power file (e.g. s10AB00.pl
  1. m3081$2$3.d - Dayfile te.g. a30AP00.d) a 9 The ASAS files associated with the run are thereforet e asa$182$3.in - user input file le.g. asaAB00. Ar.)
  1. asa$182$3,out - user output flie (e.g. asaAB00.out) e esa$1$2$3 ets - CTS output file (e.g. asaAB00. Cts) e asa$1$2$3.ats - ATS output file (e.g. asaAa00.ats) 9 asa$1$253. pit POSTSCRIPT plot file (e.g. asaAB00. pit)
  1. asa$1$2$3. day - Dayfile (e.g. asaAB00 day!

8 fthe above examples correspond to loading pattern A. h0C,

  1. sequence 00) e 8 MINOR Script File e

4 CESCRIPTIONt 9

e C:entes user input files for and Executes SIMULATE-3 and ASAS 8 for the flyspeck analysis e

e VARI ABLh:$ USEDt 5 INLINE V?.RIABLES:

  1. GLOBAL:
  1. LOCALi 9 $1 - Loading Pattern Case Identifierr ($LPCI) 9 'A' shcrt grevious cycle length e "B nominal previous cycle length 9 *C* long previous cycle length 8

9 $2

  • Time in Cycle Life (Alphabetic) ($ATICL) 8 *B* for BOC: $ BOP = 956 ppm i *M* for MOC; $90P = 586 ppm
  1. *E' for EOC: $BOR = -BA ppte t
  1. $3 - Sequence Numt.er ($ SEQ) 8 00 through 99 0

8 $4 - Oscillation Time in Hours ($03CH) 8 $$ - cycle number ($CYC) .

0 9 EXTERNAL SUBROUTINES CALLED:

$ INITIALIEATION/EETUP:

Seet -x orrfig*0 0

t HELP:

8 if ( *$1' = 'h* ) ll 1 *$1* =

  • h* J l{ t *$1' = *]

then mort *k2 << EOF HELP FOR PROCEDUPE/SCP1PT FILE $0 WHO: Osiaha Public Power District - Fort Calhoun WHAT$ Creat es user input files for SIMULATE-3 and ASAS and executes the codes for the flyspeck ar.alysis WHY:

WHEN; For the Flyspeck analysts WHtPEr From any directory where the user has twx permission.

HOW: $4 LPC2 ATICL SEQ OSCH CYC LPCI - Loading Fattern Case identifier

'A' short previous cycle length

  • m* nominal previous cycle length
  • C' long previous cycle length ASAS Manual llevision 0 '42 April 19,1994

. . . . _- - - - - - . - - , . . .. - . . - . ~

l l

i Figure 10 Sample Procedure to Generate SIMULATE-3 and ASAS Input Files And Execute the Codes for the Flyspeck Analysis Page 2 of 6 ATICL - Time in Cycle Life (Alphabetic)

  • B* for DOC / BOR = 956 ppmg prrICL = 1
  • M* for MOCs BOR = 586 ppe; HTICL e 2
  • E' for EOC; BON a -88 ppm; NTICL = 3 SEQ - Sequence Nusd>er 00 through 99 OSCH - Cecillation Time in Hours ICYC
  • Cycle number EOF exit 1 ft i t i Set variables LPCIs$1 ATICL*$(2)OC TIL=$2 SEQ =$1 OSCH"$4 CYC=55 j . If i $ATICL e *BOC* j i then BOP = 9 %

alif f $ATICL = *McC* 1 then DOPA $R6 elif 1 $ATICL = *EOC' } s then BOPa+88 tb a

i PtJN Sf:CTION:

0 ASASDIRs*/ top /ASAS.$$*

IFMOlff = * / net liten / User / tom /aSaa/simdlate/ output

  • IBMINa*/ net /$bm/userItcr/asas/ simulate / input
  • OLD='pwj' day *$OLD/asa$LPCI$TIL$SEC. day test -f $ day && rm $ day outa * $0LD/ asaSLPCI$71L$$EQ .out
  • In=*$0LD/asaSLPCI$TILSSEC.an*

cts **$0LD/asa$LPCI$TIL$ SEQ cts

  • at s**$0LD/asa$LPCISTIL$5EQ ats*

pit **$OLD/asA$LPCISTIL$5EQ. pit

  • 9 0 Generste Header Information 9

9 Initialise veslables e

if 1 $ ADMIN _ NODE a **

] J then ADMIN, NODE = * / / t oomis*

ti ban.dira'$ ADMIN _ NODE /usertstudsv)k/ bin

  • SCI 1 pts _dir=*$ ADMIN.NODF/ user /atudavtk/ scripts
  • Igstdat**dete' PIDe* echo $$'

HOSTNAME= / bire/ hc s t name '

grpe'/ Led 4,3/usr/ucb> groups' JoeID=' $(scripts da r l/jobad I t r A-Z a-t '

JOBNAME=SJOBID ver syss.3 uname .n > _t enr 1 ver sysS.3 uname -m = temp 2 NODEID=' cat ___ tempi' NODETYFEm' cat ___ temp 2' E1s _t empi _, t emp2 9

9 Setup the header e

cat $ scripts dir/ Logo > $ day echo * * >> $ day 2=>$ day echo *1* >> $ day 2*> $ day a echo * * >= $ day 2*> Sday scho

  • Date/ Time $1gstdat* >> $ day 2=> $ day echo * *>> $dsey 2*> $ day echo
  • User $USEP* ** $ day 2>= $ day 9 a ho
  • Group $grpil)* >> $ day 2 m > $ day I

O echo

  • Organiset ion $ ORGANI 7.AT I DN * => $ day 2** $ day ocho * >> $ day 2m> $$ay echo
  • Jcb Id 4 SJOSID* >> $ day 23= $ day echo * *>> . Sday 2>> $ day echo
  • Node Name //'/etc/hostnee" >> $ day 2>* $ day erbo
  • Node Id CNODEID* wm $ day 2s> $ day echo
  • Cpu type s $NDDETYPE' ** $ day 2s> $ day echo
  • Operating * >= $ day 2m> $3ey echo
  • System  : 'bidt l / bod 4.3/ bin /grep revision'a >> $ day 2>= $ day echo *
  • 3D $ day 2** $ day echo
  • Prucess ID $11D* km $ day 2> > $ day echo * * > > - $ day 2 => $ day

?

ASAS %nual Revision 0 43 April 19,1994 i

e , , - ,

i i

I i

Figure 10 Sample Procedure to Generate SIMULATE-3 and ASAS Input Files And Execute the Codes for the Flyspeck Analysis Page 3 of G echo

  • Submit Node //$HOSTNAME" >> $ day.2>> $ day ocho
  • Directory i $ FWD * >> $ day 2** $ day echo * * >> $ day 2>> $ day echo * * >> $ day 2*> $ day echo *
  • n $ day 2=* $ day 0

echo

  • The ASAS run time directory le $ASASDIR* n$ day 2* >$doy echo * * >=$ day 2s>$ day echo
  • The input file is $in' > > $ day 2 *>$ day echo
  • The user output file le $out' "$ day 2*>$ day echo
  • The out put cts file is $ cts
  • n$ day 2n$ day echo
  • The out put ets file is sats* ==$ day 23.$ day scho
  • The out put plot file as Spit * 'Sday 2>>$ day acho *
  • > > $da y 2n $ day 6

8 Remove any old files e

test f $0ut && sm Sout m e$ day 2n$da/

test -f CTZFJL && re CTSFIL >>$ day 2>*$ day test f ATSTIL && re ATSFIL >>$ day 2*>$ day test - f PLTFIL && rm PLTFIL n$ day 2n$ day test -f $1n && im $1n "$ day 2 "$ day test -f $out && tm Sout >> $ day 2 n $ day test -f $ cts && rm $ cts >>$ day 2**$ day test -f $at s && tm $ats >>$ day 2*>$ day test -f $out && rm $ pit >>$ day 2n $ day tent f $1n.2 && rm $1n.Z >>$dey 2>*$ day test +f $out.1 && rm Sout.2 n $ day 2n$ day tett -t $ cts.1 && rm $ct s. 2 >> $ day 2 > > $ day test -f $ats.1 && rm $ats.2 n$ day 2n$ day test f Sout.2 && rm Spit.2 **$ day 2n$ day t est. -f m30$LPCISTILSDEO.d && rm s30$LPCI$TIL$5EC d n$ day 2ntby test -f s30$LPCI$71L$$EQ.d.2 && rm $10$LPCJ STILSSEC.d 2 "$ day 2n $ day test -f $(IBMIN)/s30$LPCIST1L$5EQ.1 && rm $(It4 MIN) / s33$LPCI$TIL$5E2. i n$ day 2n $dsy ,

test -f $ {IBMIN) /s30$LPCISTIL$5EQ. l .E && tm $(IBMINp/m30$LPcISTIL$5EO.i 2 " $ day 2 n$ day ,

sikdir $ASASpik *n$ day 2*>$ day cat a f.071 * $(IBMIN)/s30$LPCICTIL$(SFQ).1 2n=$ day

  • TIT. PUN ' . * $30$ LPCI $TILS ( SEQ 3 ' /

' DIM. CAL' 16 2 2 1/

'COR.FYM*,"MtR'/ 6

' TIT.CAsd.'CSCYC LP $ LPCI . $ ATICL $ bOR PFM. $O9CH ftBS, 1004 POb1P, APO FriL A'/

' PE3 ' . 'alD$LPCI $ (Tillos . T * , $0SCH t

' PEP FPt" ,01 '

'COR.0FE'.100.0/

'C DR . ICR ' . $ ( B3P ) /

'1TE . F.EF ' /

' CDP. TIN'.543.00/  !

  • EFG.TFU' 1 .000000E.00 324,93 -29.21 / ,

' SFG , Tf'LP 2 .000000E+00 324.9) -29.21 /

' S Fi3. TFU ' 3 .000000E+00 ')24.93 -29.21 /

'SEG TFU' 4 .000000E*00 3J4.53 -29.21 /

' E FG . TFU' 5 .000000E*00 324.9) -29.21 / .

'SFG TTV' 6 .000000E*00 324.53 -29.21 i

' 5EG . T FU ' 7 .000000E+00 324.93 -29.21 /

  • sEG.TFU' B 1000000E+0D 324.93 ~29.21 !

'SEG.TTU* 9 .000000E*00 324.93 -29.21 /

' Sr.o . trV ' 10 .000000E+00 283.74 -25.96 /

'SEG TFU 11 ,000000E+00 203.74 -25.96 i

' Sr.G TN' 12 ,0000001 00 283.74 -25.96 /

'6EG.TFU' 13 .000000E+00 283.74 -25.96 /

' SEG. TFU' 14 .00GC00E+00 283.74 -25.96 /

  • FEG . TN' 15 .000000E400 283,74 25.96 /

'sEG . TN' 16 .000900E+00 283.74 -25.96 / 1

'SEG.TFU' 17 ,000000E+00 324.9) -29.21 /

'SEG.TFU+ 18 .000000E*00 324.93 -29.21 /

' 6EG . TFU' 19 .000000E400 324.93 -29.21 /

'5EA TFU' 20 .000000F+00 320.1 -2 4.7.3 /

' S Er2. TFU ' 21 ,0000D0Ee00 320.1 24,73 /

'SEG.T7U' 22 ,000000E+00 320.1 -24.73 /

'SEG.TFU' 23 .000000E+00 320.1 -24.*l3 /

'SEG.TFU' 24 .000D00E.00 320.1 -24.73 /

' FEG . T FU ' 25 .000000E*00 320,1 -24.73 /

'SEG.TFU' 26 .000000E+00 320.1 -24.73 /

'SEG.TFU' 27 000000E*00 320.1 -24.73 /

' FEG.TW' 28 . 000000E + 00 3 20.1 -24,73 /

'SEG.TFV' 29 .000000r+00 283.74 -25.96 /

'SEG.TFU' 30 .000000E+00 283.74 -25.96 /

'SEG.TFU* 31 .000000E+00 283.74 -25.96 /

'SEG.TFU' 32 .000000E+00 283.74 -2*>.96 /

'SEG.TFU' 33 .000000E+00 283.74 -25.96 / I 34 .000000E*00 283.74 -25.96 / j

. 8EG SEG. .TFU' TFU'35 .000000E+00 283.74 25.96 /

'SFO.TFU' 36 .000000E+00 283.74 -25,96 /

'SEG.TFU' 37 .000000E+00 2B3.74 -25.96 *'

' S EG , TrU' 38 ,000000E* 00 324. 93 -29 21 /

  • SEG.TFU' 39 .000000E+00 324.93 -29.21 / '

'$EG.tFU 4D .000000E+00 324.93 -29.21 *

' TAB TFU* 11 'EXP*

.000000E+00 2.0 5.0 10

  • Pow'.1 10.0 15 0 20.0 30.0 40.0 50.0 60.0 ASAS Manual Revirdon 0 44 April 19,1994

- . , . - ~ -- - . . . _ . - - .- - . - . .

Figure 10 Sample Procedure to Generate SIMULATE-3 and ASAS Input Files And Execute the Codes for the Flyspeck Analysis Page 4 of 6 1.0 61.27 54.04 53.a7 33.07 16.16 .45 -28.39 -57.29 70.43 -70.62 /

' T AB . TFt/ ' 12/

' TAB.TFU' 1 3/

' TAB.TFU' 14/

  • TAB.TFU" 1 5/ b

' TAB.TFU' 14/

' TAB.TFU' 17/

' TAB.TFU* 1 8/

' TAB.TFU' 1 9/

' TAB . T FU ' 1 17/

' TAB.TFU* 1 18/

' TAB.TFU' 1 19/ ,

  • TAB.TFU$ 1 38/

' TAB.TFU' 1 39/

' TAB.TFU' 1 40/

' TAB.TFU' 2 20 'EXP' 10 ' Pow' 1 000000E 00 2.0 5.0 10,0 15.0 20.0 30.0 40 0 50.0 60.0 1.0 49.02 56.15 50 65 35.32 22.3 10.78 -9.67 -29.48 -42.75 -43.56 i

' TAB.TFU' 2 21/

' T AB . TW' 2 22/

' TAB.TFU' 2 23/

' TAB.TFU' 2 24/

' TAB.TFU'-2 25/

' TAB.TFU' 2 26/

' TAD.TFU' 2 27/

  • TAB,TFU* 2 28/

' T AB . T FU" 3 10 ' E.X P ' 10 ' Pow' 1

.000000E+00 2.0 5.0 10.0 15.0 20.0 30.0 40.0 50.0 60.0 1.0 60.74 51.91 63.7 31.47 8,16 -17.51 -52.77 -57.87 59.28 -57,4 /

'TAS TFU' 3 11/

' T AB . TW " 3 12/

' TAB.TFU* 3 13/

  • TAB.TFU* 3 14/

' T AR . T FU ' 3 15/

  • TAB.TFU' 3 16/

' TAB.TFU' 3 29/

' TAB.TFU' 3 30/

' TAB.TFU' 3 31/

' TAB.TFU' 3 32/

' TAB.TFU' 3 33/

' TAB,TFU' 3 34/

' TAB.TFU' 3 35/ r

  • TAB.TFU' 3 36/

' TAB TFU' 3 37/

,coM

'COM' PASS 1 2 3 4 5 6 7 8 9 10 11

'CkD, SEQ' 1, 1260 126 0 1260 1260 12 60 1260 12 60 126 0 1J 60 1260 1260/

  • BANK 1

'CPp. SEQ' 2, 1260 1260 1260 1760 1260 1260 1260 1260 1260 1260 1260/* BANK 2

'CED.EFo* 3, 1260 1260 1260 1260 1218 1057 896 735 574 413 368/* BANF 3

'CRD. SEQ

  • 4. 1260 945 784 623 462 301 140 0 0 0 0'* BANK 4

'CRD. SEQ' 5, 1260 1260 1260 126 0 1260 1260 1260 1240 1260 1260 1260 /

  • BANK A

'CRD.EEg' 6 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260/* BANK B

'CRD. SEQ' 7, 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260 1260/* BANK N 0 0 0 0 0 0 0 0 0 0 0/* HAFNIUM RODS

'CFD. SEQ',9,8.1/

'CBD. PAS'

'PINFILE',' ADD'.*3+D'/

' FIN.FIL','ON'

'PRI.STA' 50** '! >

' PIN.ELT' 'ON',,'2 PIN'/

' ERR .CHW ' , ' FEFMIT ' /

' PIN. SUM' 50* 't

' ETA'i

' TIT . CAE ' , ' C$CYC LP $ LPCI, $ATICL $ BON PPM. $0SCH HRS, Ps1001, B4 AT 945, PDIL B'/ i

'COR. OPE',100.0/

'CCR. TIN'354),00/

  • CPD, PAS",8,2/ t

'STA'/

' TIT . CAS ' , ' C$CYC LP E LPCI . $ATICL IBOR PPM, $0SCH HRS, P= 904, B4 AT 945, PDIL C'/

  • COR. OPE', 90.0/

'COR. TIN *,543,00/

'CRD.PA3',8,2/

' ETA'/

  • TIT.CAS* 'CSCYC LP $LPCI. $AT!CL SBOP PPM. $0SCH HPS, P= 865, B4 AT 784, PDIL D*/ .S

'i

'COR.0PE . 80.0/

'COR.TJN'.543.00/ I

'CED. PAS' 8,3/ ]

'9TA*/

' TIT,CAA' 'CSCYC LP $LPC1, SATICL $ DOR PPM, $0SCH HR5, Pa 704, B4 AT 623, FD7L E'/

'COR.OPR'. 70.0/

'COR. TIN",543.00/

  • CR D. PAS * ,8,4 /

'STA'/

' TIT.CAS' 'CSCYC LP $LPCI, $ATICL $50R PPM, $O5CH HRS, Pe 60%, B4 AT 462. B3 AT 1218, PDIL F'/

'COR. OPE', 60.0/

'COR. TIN'.541,40/

' CP.D. PAS " . 8. 5 /

'STA'/

'TTT.CAS' 'CSCYC LP $LPCI, SATICL $BOR FPM, $0SCH HPS, Fe 50%. B4 AT 301 B3 AT 1057, PDIL G'/ )

'COR. OPE *. 50 0/

'COR. TIN'.539.90/

'CRD, PAS',8,6/ l l

ASAS Manual Revision 0 45 April 19,1994

Figure 10 Sample Procedure to Generate SIMULATE-3 and ASAS Input Files And Execute the Codes for the Flyspeck Analysis Page 5 of G

'9TA'/

  • T!T.CA8','C$CYC LP $LPC1, SATICL $ DOR PPM, $0SCH HRS, P. 40%. B4 AT 140, b) AT $96, PDIL H'/

' COP, OPE', 40,0/

'COR TIN',538.30/

' CRD PAS' ,8,7 /

'KTA'/ '

  • TIT,CAS* 'CCCYC LP $LPC1, $ATICL $ROR PPM, $09CH HP2, P= 30%, B1 AT 735, PDIL l'i
  • COR,OFE*, 30.0/

'COR. TIN',$3$.70/

'CRD,PA$',4,8/

'8TA'/

' TIT.CAS','C$CYC LP $LPC1, $ATICL $BOR PPM, $0$CH HRS, P* 20%, B1 AT $74, PDIL J'/

' CDP. OPE', 20.0/

'COR. TIN',$35.10/

' CR D . PAS ' ,8. 9 /

'STA'/

' TIT.CAS','C$CYC LP SLPCI, SAT 3CL $soR PFM, $0SCH HR$. P= 10%, B 3 AT 413, PDIL K /

  • COR, OPE'. 10.0/

' Cop.71N',533.60/

'CPD. PAS',8,10/

'STA'/

' T17.CAS' , ' C$CYC LP $LPCI, $ATiCL $BOF FPM, $COCH HRS, P= 14 D3 AT 252, PDIL L'/

'COR.0FR', 1.0/

' CDP TIN'.$)2.16/

'CPD. PAS *,B,1)/

  • STA'/

'END'/

KOF1 e

e Emerute SIMULATE 3 0

e e3v402b -b m30$LPCI$11L$ SEQ -t / PPG 3/Sp/OPPDvDppd/t30 ppd $CYC.l -1 t -c n -r all >>$ day 2*>$ day a sh bigblue / user /tce/com/eJasas s30$LPCI$TILS(SEQ). i s30$LPCJ4(TIL) cia r n$ day 2n$ day a

e copy files f rom IBM to HP and rename to script names mv $(3DMIN)/s30$LPCISTIL$(SEO),i s30$LPCISTIL$(SEQl .1 n$ day 2ntday ev $11BMOUT)/s30$LPCI$7IL$(SrQ).A.out a30$LPCISTIL$(SrQ).o n& day 2 n$ day mv ${IP.MOUT)/s30$LPCI$7IL$(SEQ).i. sum s30$LPCl$TIL${ SEQ).s n$ day 2 n$ day e

  1. Cr eat e Mengrios input 8

0 0 f un jc b under tmp space on HP Wr kstation e ,

ed SASASDIP in -s $1n USFPIN n$ day 2n$ day In -s out .$LPCI$TIL$$EQ UMROT >>$ day 2n$ day in -s $ cts CTSFIL n$dey 2n$ day in -s $ata ATSFIL **$dgy 2*=$ day jn -s $ pit PLTFIL n$ day 2 *>$dny mv $ (IBMOU*) /m30$LPCI$71LS (SEQ) . l . pin s30$LPC1$TIL$ { SEQ) .p n$ day 2n$ day cat av EOF 2 > Sin 2e*$ day TIT.RUN C$CYC LP $LPCI, $ATICL $ BOP PPH, $0SCH HMS + Pun esa$LPC!$71LSSEQ CONTROL 112340000 rDE.LIH 1 22,0 'ALL' WE.FIL $CLD/ f argen) .out COMMENT frele ftilt fgrid fe feel fdep fttip fast UNC.FAC 1.038 1.030 1.0075 1.00 3.c0 0.975 0.0 .00 COR.LHR 6.Q$7 TIT.CAs 1 1,7700 '$TIL-$0SCH-A MIL CASE A - 100% POWER, ARO' TIT.CAS 2 1.9400 'fTIL-50SCH-B PDIL CASE B - 1004 POWER, BMm 4 AT 945' TIT CAS 3 1,9500 '$TIL-$O5CH-C FDIL CASE C - 90% POWEP, BAIN,4 AT 94%* '

T17.C AS 4 1,9500 '$TIL-$0SCH-D PDIL CASE D - 404 NWER, BANK 4 AT 784' TIT,CAS $ 1.9500 *$TIL-$OSCH-E PDIL CASE E - 70% PWER, P.AMK 4 AT 423' TIT.CA3 5 2.0700 '$71La$0SCH-F PDIL CASE F - 60% P NER, BANK 4 AT 462, PANK 3 AT 1218' TIT.CAA 7 2,1900 * $7IL-$0SCH G PDIL CASE G - 506 POWER, BANK 4 AT 301, bANN 3 AT 10$7' TIT.CAS 8 2.2300 '$TIL $OSL'H-M P03L CASE H - 40% POWER, bANY 4 AT 140, RANK 3 AT 8 91i' TIT.CAS 9 2,2500 'STIL-80SCH41 PDIL CASE I - 309 POWER, BMW 3 AT 735' .

TIT CAS 10 2.2600 '6TIL-$0SCH-J PDIL CASE J

  • 20% POWER. PANK 3 AT $74' TIT.CAS 11 2.2900 '$TIL-$0SCH K PDIL CASE F - 10% POWER, BANK 3 AT 413' T37,CAS 12 2 2900 '$7IL-50SCH L PPIL CASE L 14 POWER, BMW 3 AT 268' KEL. ASS 1 28 SIM.FIL m 30$LPCI$72L$ f SEQ) .p EM . REQ ' POWER FDT.P2Q 'ASI-F195 EM , P EQ ' Pf'DL EM . R EQ ' FZ-FISS RDT . P EC ' FT.!MC FISS '

EM. MFQ ' FQ-FISS EM . R EO ' FE-THRM KUT. reg 'FZLOC-THPN EDT. REQ ' F;)-THF.M

  • EARCUTE ASAS Manual Revision 0 46 April 19,1994

1 1

1 1

l Figure 10 i Sample Procedure to Generate SIMULATE-3 and ASAS Input Files 1 And Execute the Codes for the Flyspeck Analysis i Page 6 of 6 EOF 2 0

0 Execute ASAS S

// tom / user / tom /ases/Rev1/asas >> $ day 2>>$ day f

. l 0 Pemove SIMULATE-3 pin file l test -f 630$LPCI$TIL$(SFQ).p && rm e30$LPCI$TIL$(StQ) .p >> 3 day 2n$ day 0

e normal termination e

test -f USEROT && rm USEROT >>$ day 2m>$ day test -f CTSFIL && rm CTSFIL >>$ day 2n$ day test -f ATSFIL && tm ATSFIL >>$ day 2>>$ day test. -f PLTFIL && rm PLTFIL >>$ day 2*>$ day j echo

  • The finish date and time is 'date'* n$ day 2>>$. lay l a a echo
  • * * " * ' ' * * * * * * * " ' " * * * * ' * " ' " * * * * * * ' * * * * ' * " * " *
  • n$ day 2n$ day j scho cat out.$LPCICTILCSr0 $ day >$out 2 n$ day i l

test -f out.$LFCI$71L$(SEQ) && rm out,$LPCISTILS(SEQ) cd 80LD rm *r $ASASDIP O

I Check that files exist and then compress 4 tieleted Spit file because it isn't being generat ed for each in 1

$oot \

Gate \

$ cts \

$ day \

s10SLPCICTIL$ SEQ.1 \

s 30$ LPC1 $71L$ SEQ .o da ,

test -f $each af I *$7' += 'O' ) , then I echo *ERP.OR: FILE Seach NOT FOUND* 3 ocho *flyptoc ADOPTED

  • i exit else compress $each fi donc

$ KKIT:

5 exit 0 l

ASAS Manual Revision 0 47 April 19,1994

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Figure 11 Sample Script File to Execute Flyproc for 100 Timepoints Page 1 of 2 I

- flyproc A B 00 10.5 15 flyproe A B 01 11.0 15 flyproc A B 02 11.5 15 flyproc A B D1 12.0 15 flyptoc A B 04 12.5 15 flyproc A B 05 13.0 15 flyproc A B 06 13.5 15 flyproc A B 07 14.0 it flyproc A B 08 14.5 15 flyproc A B 09 15.0 15 flyproc A B 10 15.5 15 flyproc A B 11 16.0 15 flyproe A B 12 16.5 15 ,

flyproc A B 11 17.0 15 flyproc A B 14 17.5 15 flypsoc A B 15 18.0 15 flyproc A B 16 18.5 15 flyproc A h 17 19.0 15 flyproc A D 18 27.5 15 flyproc A B 19 24.0 15 flyptoc A B 20 24.5 15 flyproc A B 21 25.0 15 flyproc A B 22 25,5 15 flyproc A B 23 26.0 15 flyproc A B 24 26.5 15 flyproc A B 25 27.0 15 flyproc A B 26 27.5 15 flypro9 A B 27 24.0 15 flyproc A B 28 28.5 15 flyproc B 29 29.0 15 flyproc s B 30 29.5 15 flypree A B 11 30.0 15 flyproc 4 B 12 30.5 15 flyproc A B 3) 31.0 15 flyproc A B 34 31.5 15 flyproc A B 35 31.0 15 flyproc A B 36 32.5 15 flyproc A B 37 33.0 15 flyproe A B 38 39.0 15 flyproc A B 19 39,5 15 flyproc A B 40 40.0 15 +

flyproc A B 41 40.5 15 flyproc A B 42 41.0 15 flyproc A B 43 41.5 15 flyproc A B 44 62.0 15 flyproc A B 45 42.5 15 flyproc A B 46 43.0 lb flyproe A B 47 41.5 15 flyproc A B 46 44.0 15 flyproe A B 49 44.5 15 flyproc A B 50 45.0 15 flyproc A B 51 45.5 15 flyproc A B 52 46.0 15 flyproc A B 53 46.5 15 flyproc A B 54 47.0 15 flyptoc A B 55 47.5 15 flyproc A B 56 48.0 15 '

flyproc A B $7 48,5 15 flyproc A B 58 49.0 15 flyproc A B 59 54.5 15 flypree A B 60 55.0 15 flyproc A B 61 55.5 15 .

flyproc A B 62 56.0 15 flyproc A B 63 56.5 15 flyproc A B 64 57.0 15 flyproc A B 65 57.5 15 flyproc A B 66 58,0 15 flyproc A B 67 54.5 15 flyproc A B 68 59.0 15 flyproc A B 69 59.5 15 i flyproc 4 B 70 40.015 -)

flyproc A B 71 60.5 15 flyproc A B 72 61.0 15 flyproc A B 73 61.5 15 flyproc A B 14 62,0 15 flyproc A B 75 62.5 15 i flyproc A B 14 63.0 15 flyproc A B 77 63.5 15 flyproc A B 78 64.0 15 j flyproc A B 79 64.5 15 flyproc A B 60 65.0 15 i flyproc A B 81 65.5 15 flyproc A B 82 66,0 15 flyproc A B 83 72.0 15 flyproc A B 84 72.5 15 flyproc A B 65 73.0 15 flyproc A B 86 73.5 15 flyprov A e 87 74.0 15 ASAS Wnual llevision 0 48 April 19,1994

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1 Figure 11 Sample Script File to Execute Flyproc for 100 Timepoints Page 2 of 2 flyproc A B 88 74.5 15 flyproc A B 89 75.0 15 flyproc A B 90 75,5 15 flyproe A B 91 76.0 15 flyproc A B 92 76.5 15 flyproc A B 93 77,0 15 flyproc A B 94 77.5 15 flyproc A B 95 18,0 15 flyproc A B 96 78.5 15 flyproc A B 97 79,0 15 flyptoc A B 98 79.5 15 flyproc A B 99 80.0 15 1

ASAS Manual itevision 0 49 April 19,1994

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Figure 12 Sample Code to Concatenate and Sort Multiple CTS and ATS Files Page 1 of 4 progias concat integer *4 ISHCST,getpid_,getuid_. process _id flag (haracter*0 NAME TTIME character *10 TDATE characto *32 HNAME char ac t er

  • 4 durwy character *3 opt charact er *1 separator charseter*6 casolabel,casetest character *132 inputdar, output file, input file currentdir char act e r *12 columnl abe l (15 ) , rodeon f igur at ionlabe l ( 2 00, 201 cha ract er
  • 12 r ndnewc on f igurat ionlabe142 0 l , f il ename char act er *132 header record (20 ) . output et s f 11e, out put at a file integer case.confaguration, column,locationt2,20,2001 int eger numbe rof header recor de ,3, j , k, start ing filenumber integer endirwf11enum be r , filenumber , blank . blank 2 integer aviairades, fields.camenumber, cases integer *4 readstatus real data 115.20,2006,percentpower(200.20e,axialshapeindex(200,20) real radialg+akingf actor (200,20),axialpeatingf actor (2 00. 20; real axialdata[200.20.50) write f* *4a.$1-)
  • Enter the directory containing the files to pro

' cess:

reai (*,'(a80)-) inputdir 2000 write (*,'ta.5I') "Is this an ats or ets file concatanation: -

read (*,' fall') opt write (*.'(a,$)')

  • Enter t he starting file numt+r to process:
  • r ead (* , ' (121 ' ) startingfilenumber i~

write (* ' d a, $i ')

  • Enter the ending file number to process: =

read * .'1121') endingfilenumber write (*,*ta.$)')

  • Enter the name of t he output file (evtensions w
  • 1ll be addedii reeS (*,-(aB03') outputfile blank =index(outputfile. 'i d w yr . cts' out put et a f ile=out put f ile (1 s blank -1) / /dumy dom:vy s .ats' outputatsfile*outputfile(l' blank-1)// dummy C Deen Initialisation separators'/*

centigurationel frienumberustartingfilenumber DATA r odnewconf ig ur a t i ori t ette l / '

'4-25-RDC *

  • *d.3$. goc - , = g .3 8.BT *"', "4-51-BOC
  • , *4-O-DOC *
      • 4-76 Boc **3-41-Bot '*3-54-Boc -
    • =3.p.poc ,
  • "4-89

'=3 79. BoC Bot *

,8* '/

if (opt.eq 'ats') goto 10000 if fort.ne.'ets*) then wr i t e ( * '(al*) "Ceneatanation option not ats or ets please rest aart-goto 2000 endif C Open the output file open (uni t all *il es cut put e t e fil e . stat us= ' UNTHOWN'

  • tostats- uadstatus,etr=1200)

C Construct the name of the file to process for ets files 10 filenamet):5)='asaAB*

write I f 11er,are i6 :7),'(12.2)') filenumber filename (8:113e . cts' if (inputdir.eq. ') then flagsgetcwd (currentdir) $

blank elndex t eur rent dir . *)

input di r (i t blank- 1)

  • cur r entdi r endi$

t-lank =i ndex q inputdi r , ' 'l I inputfile(1: blank-11=inputdir inputfile(blank:blankleseparator input file (blank *1 :13 2 ) = f 11erame C write ( % *) ' Pr oc es sing filename * ,inputfile C opening the data file to read ir, data open (unit = 10. fil e= 1hput f ile , st at us= ' OLF , lost at'readst atus , err =11

+00)

C Pea $ the header r ecords until a CASE stateeer.t is reache; 20 read (10,'{1x a6)',end=10001 caselabel -[

if (caselabel.ne."' CASE *') goto 20 C Pead the cata labelt on the CASE st atement line backspace (10t seed 110, ' (1x , a6,1x .10 f a12,3x.11 * ) canelabel,(columnlabelti).1=1,1C

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ASAS Manual Revision o 50 April 19,1994 i

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Figure 12 j Sample Code to Concatenate and Sort Multiple CTS and ATS Files i Page 2 of 4 C pead in the data records until the end-cf file is reached 30 read (10,'(15,3x.n12,3x f9.3,4x,1p.3e15.6,19,6x,2e15,6,19,6x,

  • e15.6)',end=10001
  • con figur at ion, rodeonf igur at ionlabel ( filenumber . conf igur at ion ) ,
  • (dat a (co lumn, con f iguration, f il enumber +11, column =1,41,
  • locationll, configuration,filenamber*1),
  • (data (column, configuration,filenumber+1), column.5,6),
  • location (2, configuration,filenumberell, adot a (7, conf igur at ion , f ilentunbe r 41 )

configuration = configuration.1 goto 30 1000 filenumber.filenumber*1 close (10) if (filenumber.le,endingfilenumber) goto 10 C"'*'*'***"'"*******"'*

C End of files reached printout file C***********************************

C Write the Header Records write (11,'(al') '

' Header Records

  • B' write (11,'fal')
  • File Version Number
  • Ja blask indexIinputdir,* 'I blank 2*index(outputfAle,* ')

write (11,'fa.a.a,a,al') *0riginal Fath Name' * ,

  • inputdir(1: blank-1),*/',outputfile(1: blank 2-11, l'

l process td.getpid_t)

(- ISHOST e hos t nm_ (HNAME )

CALL getlog.INAME) blank =index(HNAME, ')

write (11,'(a,a,al's

  • Machine' ** HNAME(1: blank-1),

blanksindex(NAME, ')

  • write (11,'fa,a,al*l '

' User * * ,NAME(1: blank-1),

write (11,'(a,15.al') '

'JOBID* * . process _id,'**

CALL XDATE(TDATE)

CALL XTIMEtTTIME) write (11,'(a a.al') '

'Date' * ,TDATE,

write (11, ' (a , a , a l ' ) *

  • Time' * ,TTIML**

write (11, '

  • Program * 'ASAS 1.0 MOD l

mrite (11,'(al') *lal*) 11

  • Names' write (11,
  • I15.13 x, a7 ) ' ) cor.f i g ur a t i on- 1,
  • Files
  • do 60 i=1. configuration-1 write (11,*(15,13x,a12)') endingfilenumber-startingfilenumber41,
  • *Timepoints" write 111,'(1x.m6,1x.10ta12,3x) *) caselabel,(columniabelth),k=1
  • ,101 do 50 jel endingfilenumber to write (11,'(15,3x,a12,3x,f9.3,4x,1p,3e15.6,19,6x,2e15.6.19,6x, e15.61')
  • j,rodeonfiguratlonlabel(j,i6,
  • (datalcolumn,1,j), column =1,4).
  • location (1,i,jl,
  • (dataleolumn,1,ji. column.5,6),
  • location (2,1,j),
  • data (7,1.j) 60 write (11,*(15,3r a12,3x,f9.3,4x,lp,3415.6.19,h ,
  • 2e15,6,19,6x,e15.61')
  • 3,rodnewconfigurationlabelii),
  • (da ta (c olumn,1, j ) , co lumn= 1, 4 ) ,
  • locationII,1.j1,
  • (datateolumn,2,j),colurn=5,6),

location (2,1.j),

  • da t a ( 7,1, j )

close illi goto 9999 1100 blank =index(inputfile, ')

write (*,*)

  • Error cpening A riput file: *

,inputfileilsblank-1), ..

    • check filename
  • j goto 9999 '

1200 llank*index(outputetsfile, *)

write (*,*)

  • Error cpening CTS output file: *,
  • out put et s fli e (1. blank-1) , " chec k filename' gato 9999 1300 blank =index f outputatsfile,' ')

write (*,*)

  • Err or opening ATS output file: *
  • outputatsfile11: blank-1)," check filename' goto 9999 c........................................

C.T.h. i s. . i s. .t. h.e. . A. T.S. .. . .. f i l. e. .g r o.c..e...

s. s. i n.g t...a c t. 2 o.n.

e . . .

ASAS Manual Revision 0 51 April 19,1994 1

1 Figure 12 Sample Code to Concatenate and Sort Multiple CTS and ATS Files Page 3 of 4 C Open the output file )

10000 open tunit=11.flie=outputatsfile.statuss'UNT.NOWN*,

  • iostatsreadstatus,ers 1300)

C Constrr:t the name of the file to process for ets files

  1. 41 enumbere st ar ting filemunber 110 filename (1:Sle'asaAn*

write (filename (4:7),'(12'21') filencaber filename (8:11).'.ats' ,

if finputdir.aq,) then flagsgetcwd_(currentdirl blank eindex (cur rent dir. *I inputdir(1 blank-1)=currentdir endif blank =index(inputdir,' 'l inputfile(1 blank.11einputdir inputfilethlank:blanklaseparator inputfile(blank +1:132)= filename C write (*,*) ' Processing filename = ',inputfile C opening the data file to read in data ,

open f unit =10. f ile= inpot tile, status 'OLD' ,iostato readstatus , er r=1'. .

  • 00)

C Pead the hander records 120 read (10, ' (15) * ,end=3000) aximinodes a read (10 '(151',end=30001 fields read (10,'(15t*,end=30001 casenumber r

read (10,'(1x a12)',end=30001 .

  • rodeon f agur at ionlabel I f 11enumber . ca senumber i read (10,*(fil.31',end*3000) percent power ( f il enumbe r . ca senumber )

read fl0,*(e15.5)*.end=3000) axialshapeindextfilenumber,

  • casenumber) read (10,*(f11,5)'.ende3000i e adialpeaking f act or ( f 11enumber ,
  • casenumber) read (10,'(fil.51'.end=3000) axialpea king f act or ( f il enumbe r, casenumeer) read 110.'fa'132)'.end*30001 headerrecordial C Fead in the data records until tne end-et-file is reached do 130 1 1 axialnodes t 110 read (10.'(4x,f12.5)',end=3000) axialdatalfilenumber,casenumber,1) goto 120 3000 filenumberafilenumber+1 if (filenumber.le.endingfilenumberi goto 110 6 C Write out the ats file wr2te (11 'ta)*l * ' Header Pecords* 4' write (11 *(a)') *
  • File Version Number
  • l' blankaindextinputdir.' 'l .

blank 2*index(outputfile.# *) I writa (11,'(a.a,a,a,al'l

  • Original Path Name' ,

inputdir(1: blank-11,*/',outputfile(1: blank 2-1).

process _idsgetpad_()

1$HOSTshostnm.(HNAMEl cat.L getlog_lNAMEl blank =index(MNAME,' *)

write (11,'(a.a.al') *

  • Machine' * ,HNAMF(1tblank-1), * .7 blank =index(NAME ' ')

write ill,'(a.a.a)')

  • User * ,NAME41tblank-1),'

write (11,'la,15.a)') *

  • JOBID* ' , pr oc es s_id, ' '

CALL XDATELTDATEl j Call XTIME(TTIME) write (11, ' 'Date* **,TDATE. '

writ e (11, ' ta . a , al ' )

'(a,a.al'1 *

  • T ime ' * . TT IM E, ' '*
  • write (ll.*(al')
  • Program * *ASAS 1.0 MOD 1*'

write (11,'ti5,15x,a13)'l axialnodes,'* Axial Nodes

  • write (11,'li$.151.a161*l fields.** Fields on File **

cas e s send ing f ilenabe r- s t a; 51 ng f i lenumber +1 do 200 j 1,casenumber do 200 i=1. cases f11enumbereatartingfilenumber+1+1 write (11,*(15,15x.a13)') (j -il

  • cases +1,
  • Case Numbet* t write 111.*t1x,a12,7x.a9)')
  • . rodnewcor.figurationlabeltjl,'* Case Ip*

wr it e (11. ' ( f11. 3. 9x. a201 * ) pe r cent powe r ( filenumber . j ) .

  • ** Percent Full Power *'

write til,'f2x,e13.6,5x,a181') axials hapeindex t illenusnbe r . j ) .

  • ** Core Average ASI*

write ill."(3x,f8,5.9x.a18)*)

  • r adia lpea king f act or ( f il enumbe r, j l ,
  • ** Radial Feaka.ng Factor (FR)*

write ill, ' (3x. f 8. 5. 9x. a22) ' l ASAS Manttal Revision 0 52 April 19,1994

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1 Figure 12 Sample Code to Concatenate and Sort Multiple CTS and ATS Files Page 4 of 4

  • axialpeakingfactortfilenumber,j),
  • ** Axial Peaking Factor **

write (11,'(a132)') headerrecord(1) do 200 k'1,axialnodes 200 write (11,'(14,4x,f8.61') k,axialdatatfilenumber.j,k) 9999 close (11) end C

C'**********************************************************************

SUBitOMINE XDATE( ADATE)

CHARACT D*10 ADATE,3D DIMENSION TM(3)

CALL IDATE (!DT I1) ,IM (2 ) , TDT (31 )

WRITE (ID. ' (12.2. I2. 2.14. 4 I

  • IT M l2 ) ,1DT (1) IDT (3 )

WRITEIADATE a(A4, */' ,A2,*'/,A21') 3D(5:8),IDII:21,Ir(3:4)

RETURN END C

C***********************************************************************

SUBROlffINE XTIME(ATIMEl CHARACTD *8 ATIME DIMENSION ITM(3)

CALL ITIME t ITMill ,TTM (2) . ITM ( 3) )

WRITEIATIME.10lITMill,1TM(2),ITM(3) 10 FORMATl!2.2,' .32.2,'i',I2.2)

PETURN T.ND a

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ASAS Manual Revision 0 53 April 19,1994

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- . l Figure 13 l Sample User Output File i Page 1 of 37 i 1

l 1 Ph0GPAM ASAS VERSION 1, PEV DATE 4/12/94. TODAY'S DATE IS 04/12/94, THE TIME IS 08:19:49 PAGE 1 A CODE TO CREATE WJT CMANNEL DATA FILES FROM A SIM'J1 ATE-3 PIN FILE e....... I N PW ECHO * * * * * * * *

  • TIT.RUN Fort ralhoun Cycle 15 BOC 10.5 Hours - asetest CGiftHOL 22340111 FUE. LIM 1 15.0 ' TYPE 1' FUE. LIM 2 16,0 ' TYPE 2' LAY. LMN 1 2 1 2 1 2 1

'2 1 2 1 2 1 1 2 1 2 1 2 2 1 2 1 2 1 1 2 1 2 1 2 1 2 1 2 1 2 1 2 VUE.FIL fargen1.cmL Cf.*9tDft feele f t ilt ferid fe feelcr fder ftrip fasi UNO.FAC 1.10 1.03 1.007$ 1.03 1.02 0.915 30 .04 CCR.1.HR 6.00 TIT.CAS 1 1.7700 'B 10.$-A PDIL CASE A

  • 1004 POWFP. ARO' TIT.r%s 2 2.3320 's-10.5-J FDIL CASE J - 20% POWER, BAN # 3 AT $74*

SEL. ASS 3 1 10 39 BIN.FII. /RPG3 /fip!OFPD/o30 test.p EDT PEQ 'ASI-ASS EPT. REQ 'ASI-PER EDT.FEQ 'AS1-COPE EDT.FE's 'PFDL '

EDT. REQ *LHGP W/UNC EM . PEO ' FZLOC-FIS9' EDt. PEQ

  • ASSD4BLY 8' EM . REQ ' EXCOP E PES' EXECWE

........ two or rnrut Ecso *********

F T

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l ASAS Manual Revision 0 54 April 19,1994

Figure 13 Sample User Output File Page 2 of 37 1 PROGRAM ASAS VERSION 1, PEV DATE 4/12/94. TODAY'S DATE IS 04/12/94, THE TIME IS 08:19:49 PACE 2 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE LISTING OF DATA 10 WE USED FOR THIS RUNT RUN TTTLE = Fort Calhoun Cycle 15 Doc 10.$ Hours - amatest CONT 90L PAPAMETERSi NUMBER OF FUEL TYPES = 2 NUMBER OF CASES IN RUN = 2 ASSEMBLY SELECTION OPTION e 3 FUMBER OF P1. ANES FOR AX1AL FIT = 40 SHORT/14NG Ot7tPUT OPTION = 1 CD4ERATE PLCrt FILE f 0/11 e 1 1D/3D ATS OtfrPUT OFTION 10/1)

  • 1 FUEL LIMITS IATA; FUEL LHGN TYPE SAFDL M1EL 8 (KW/FT) TYPE I 15.00 TYPE 1 2 16.00 TYPE 2 FUEL TYPE NUMBER 1.AYDCMN DATA:

1 1 1 2 1 2 1 2 1 2 1 2 1 1 2 1 2 1 2 2 1 2 I 2 1 1 2 1 2 1 2 1 2 1 2 1 2 1 2 NAME OF FILE CONTAINING DETECTOR VIEW FACTORS = facgeni.out UNCEPTAINTY FACTOR DATA:

CALCULA710NAL UNCERTAINTY FACTOR IFCALC) = 1.1000 AZIMirTHAL TILT UNCERTAINTY FACTOR tFTILT) = 1.0300 GDID DIP FACTOR fFGRIDI = 1.0075 EN3INEERING (FABRICATION) FACTOR fFE) = 1.0300 CALOPIMETRIC POWER UNCERTIfffY FACTOR (FCALOR) a 1,0200 FUEL ENERGY DEPOSITION FACTOR (FDEP) = .9750 TRIP OVERSHOOT POWER UNCERTAINTY FACTOR (FTRI P) = 3.0000 t PCWER PERIPMERAL ASI UNCERTAINTY FACTOR (FASI) = .0400 DELTA ASI CORE AVERAOE LHGR = 6.0000 KW/FT CASE TITLES AND RACI AL PEAKING FACTORS PADIAL CASE PEAEING 4 FA N R CASE TITLE 1 1.7700 B-10.5-A PDIL CASE A - 100% POWER, ARO 1 2 2.1320 B-10.5-J FDIL CASE J - 2C4 POWER, SANK 3 AT 574 i USER-SELECTED ASSEMBL1ES = 11039 I

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l ASAS Manual Revision 0 55 April 19,1994 l

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Figure 13 Sample User Output File Page 3 of 37 1 PROGRAM Af.AS VERSION 1. PEV DATE 4/12/94. TODAY'S LATE IS 04112/94, THE TIME !$ 09:19:49 PAGE 3 A CCCE TO CREATE MOT CHANNEL DATA fit.E9 FROM A SIMULATE-3 PIN FILE LISTING OF DATA TO BE USED FOP THIS PUN (CCHTINUED):

SIH'11 ATE 1 PIN FILE l&AME o /RPG3/Sp/OPPD/m30 test.p 7871ESTED EDITS FOR THE CT9 FILE ASI-ASS ASI-PEN ASI-CORE PFDI, LHGR W/UNC FZLit~F188 ASSEMBLY 6 EXCORE PES FLAT-WEIGHTED ASSEMBLY-AVERAGE VIEW FACTOR $r

.28040 .14700

.19549 .14420 .07760 .03640 .02720

.03959 .02911 .02230 .01431 .00000 00000

.00000 .00000 .00000 .00000 .00000 .00000

.00000 .00000 .00000 .00000 . 00000 00000

.00000 .00000 00000 .00000 .00000 00000 .00000

.00000 .00000 .00000 .00000 .00000 .00000 .00000 WEIGHTED StlM OF FACTORS e .99999 MAXRFC.MAXSTA.MAXPIN.MAXHED !AFUL

  • 1419 2 254 1$ 13 e

b f

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1 ASAS Manual Revision 0 -56 April 19,1994

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Figure 13 Sample User Output File Page 4 of 37 TODAY'S DATE IS 04/12/94, THE TIME IS 08:19:49 PAGE 4 1 PROGRAM ASAS VERSION 1 PEV DATE 4/12/94.

A CODE M CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 FIN FILE PIN FILE NAME /RPG1/Sp/OPPD/s30 test.p RUN TITLE  : Fort Calhoun Cycle 15 BoC 10.5 Mours - amatest CASE 3D 9-10.5-A PDIL CAS8 A

  • 100% POWER, ARO XPO = 10.500 GWD/MT, EBAR s 16.119 GWD/MT. POWER = 100.004, FIDW = 100.004 PKrNT = 19120. STEPS INSERTED, FQ = 2.000, F-DELTA-H e 1.651. INCOPE ASI = .0078, PERIPHERAL ASI = .002)

TMAL RELATIVE EXCOR5 SIGNAL = .4425 TOTAL FtIEL PINS IN QUARTER CORE = 5804.0 MTAL OF A1.L PINS IN QUARTER CORE = 6517.0 EDIT OF ASSEMBLY NUMBERS TO BE PROCESSED (AND REASONS POR EELECTIONI FOR FUEL TYPE:

TYPE 1 TYPE 2 1 10 USER SELECT USER SELECT 18 39 rQ-PLANE 1 USER SELECT 14 35 FQ-PLANI 2 FQ-PLANE 1 25 19 FQ-FLANE 16 FQ-PLANE 16 t

?

ASAS Manual Revision 0 57 April 19,1994 i

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Figure 13 Sample User Output File Page 5 of 37 1 PROGRAM ASAS VERSION 1, REV DATE 4/12/94. TODAY* $ DATE IS 04/12/94 THE TIME 18 08:19t49 PAGE 5 A CDLE TO CREATE HOT CHANNE1 DATA FILES FROM A SIMULATE 3 PIN FILE PIN FILE NAME / R PG 3 / Sp /OPPD/ a 30t en t .p RlfN T!TLE s Fort Calhoun Cycle 15 B3C 10.5 Hours

  • asetest CASE ID t B-10.5-A PD1L CASE A - 100% POWER, ARO 1P0 e 10.500 cwD/wr, EBAR = 16.119 GWD/MT, POWER = 100.009 FLOW = 100.00%

N7FWT

  • 1.653, INCORE ASI * .0078, PERIPHERAL AS1 * .0023 TVTAL RELATIVE EXCORE SIGNAL * .4425 FUEL TYFE TYPE 1 PIN POWERS FOR LIMITING LNGR PLANE 8 FOR ASSEMBLY 1,$ERIAL NUMBEN OMN012 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 ,0565 .0591 .0630 .0669 .0704 .0144 .0804 .0825 .0814 .0826 .0845 .0862 .0879 .0918 2 .0644 .0709 .0780 .0828 .0849 .0865 .0888 ,0910 .0938 .0981 .1025 .1043 .3039- .1054 3 .0757 .0854 ---- ---- .1021 .1014 .1020 .1045 1095 .1169 ---- ---- .1230 .2219 4 0892 .3000 ---- ---- .1186 .1176 .1181 .1208 .3266 .1350 ---- ---- .3412 .1393 5 .3052 .1137 .1239 .1307 .1333 .1354 .1174 .1405 .1456 .3513 .3574 .1593 .1571 .1572 6 .1259 .1293 .1364 .1431 .1493 .3563 .1633 .2672 .1685 .1697 .1721 .1737 .1741 .1163 7 .1559 .1495 .1527 .1588 .1668 .1793 +--- ---- ,1957 .1920 .1924 .1936 .1945 .1973 8 .1900 .1724 .1754 .1817 .1901 .2046 ---- ---- .2219 .2162 .2164 .2177 .3194 .2242 9 .1964 .1987 .2073 .2155 .2225 .2305 .2370 .2416 .2441 .2455 .2485 .2504 .2507 .2544 10 .2253 .3349 2509 .2600 .2600 2595 .2580 .2617 .2721 .2831 ,2952 .2978 .2916 .2911 il .2636 .2795 ---- ----

.3040 .2942 .2899 .2939 .3080 .3296 ---- ---- .3412 .3340 12 3085 .3232 ---- ---, .3437 . 3324 ,3294 .3347 .3489 ,3731 ---- -+-- .3879 .3813 13 .3592 .3628 .3766 .381E .3767 .3738 .3185 .3865 .3956 .4118 ,4302 .4361 .4303 .4344 14 _4228 .4128 .4143 .4166 .4195 .4279 .4495 .4633 .4603 .4667 .4761 .4835 4894 .5053 FZ FACTORS FOR ASSEMBLY 1, SERIAL NUMBER OMN012 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1460 1.1412 1.1380 1.1363 1.1359 1.1363 1.1375 1.1362 1.1331 1.1306 1.1286 1.1276 1.1276 1,1277 2 1.1440 1.1389 1.1345 1.1334 1.1355 1.1363 1.1361 1.1349 1.1329 1.1300 1.1256 1.1246 1.1269 1.1270 3 1.1435 1.1366 - - - . ---- 1.1333 1.1362 1.1364 1.1352 1.1329 1.1276 ---- ---- 1.1242 1.1265 4 1.1445 1.1376 - - -

1.1340 1 1371 1.1368 1.1357 1.1335 1.1283 ---- ---- 1.1251 1.1274 5 1.1469 1.1426 1.1376 1.1361 1.1380 1.1380 1.1365 1.1354 1.1345 1.1322 1.1284 1.1276 1.1297 1.1300 6 1.1503 1.1467 1.1443 1.1424 1.1406 1.1373 1.1326 1.1313 1.1342 1.1353 1.1349 1.1343 1.1339 1.1328 7 1,1548 1.1498 1.1473 1.1449 1.1416 1.1347 ---- ---- 1.1322 1.1373 1.1382 1.1381 1.1370 1.1353 8 1.1565 1.1518 1.1497 1.1475 1.1445 1.1376 ---- - -- 1.1347 1.1399 1.1409 1.1409 1.1401 1.1391 9 1.1553 1.1525 1.1503 1.1486 1.1472 1.1439 1.1384 1.1372 1.1408 1.1422 1.1419 1.1416 1.1415 1.1405 10 1.1548 1.1520 1.1468 1.1456 1.1483 1.1484 1.1467 1.1456 1.1453 1.1435 1.1390 1.1384 1.1417 1.1422 11 1.1558 1.2499 -- -

1.1469 1.1511 1.1511 1.1502 1.1485 1.1425 ---- - -- 1.1404 1.1446 12 1.1581 1,1523 - - - -

1.1493 1.1541 1.1547 1.1541 1.1519 1.1456 ---- ---- 1.1439 1.1482 13 1.1613 1,1589 1.1537 1.1526 1.1560 1.1577 1.1578 1.1576 1.1560 1.1530 1.1482 1.1478 1.1511 1.1528 14 1.164) 2.1630 1.1613 1.1602 1.1603 1.1601 1.1611 1.1617 1.1596 1.1578 1.1564 1.1562 1.1568 1.1572 ASSEMBLY AXI AL PEAKING FACTOR

  • 1.146) (FROM 16 PLANE DATAI ASAS Manual Revision 0 '58 April 19,1994 l

Figure 13 Sample User Output File Page 6 of 37 PROGFAM ASAS VERSION 1, REY DATE 4/12/94. TODAY'E DATE IS 04/12/94. THE TIME IS 08:19:49 PAGE 6 1

A CODE TO CFEATE HOT CHANNEL DATA FILES FROM A SIMU1 ATE-3 FIN FILE PIN FILE NAME 1 /RPG3/Sp/OPPD/s30 test.p RUN TITLE t Fort Calhoun Cycle 15 BOC 10,5 Hours - asatest CASE ID i B-10.5-A PD1L CASE A

  • 1004 POWER. ARO XPO = 10.500 GWD/MT. EBAR
  • 16.119 GWD/MT. POWER = 100.00%. FLOW = 100.004 NOWf a 15120. ETEPS INSERTED, FQ = 2.000, F-DELTA-H = 1.653. INCORE ASI = .0078. PER1PHERAL ASI = .0023 TOTAL PELATIVE EXCORE SIGNAL * .4425 FUEL TYPE : TYPE) 2D PIN POWERS FOR ASSEMBLY 1, SERIAL NLHBER OMN012 1 2 3 4 5 6 7 8 9 10 11 12 13 14 a 1 .0496 . .0519 0556 .0590 .0621 .0656 .0708 .0727 .0720 .0732 .0751 .0767 .0782 .0816 2 .0565 .0623 .0688 .0732 .0748 .0761 .0782 .0802 .0829 .0869 .0913 .0930 .0923 .0937 3 .0664 .0751 ---- ---- .0902 .0892 .0898 .0920 .0964 .1039 +--- ---- .1096 .3082 4 .0781 0879 ---- ---- .1047 .3034 .1039 .3064 .1117 .1198 ---- --- .1257 .2236 5 .0918 .0995 .3089 .1151 .1172 .1190 ,12C9 .3237 .1283 .1337 .1396 .1414 .1391 .1391 6 .1095 .3127 .1192 .2253 1309 .1375 .1441 .1478 .1486 >1495 .1516 .1531 .1535 .1556 7 .1352 #1300 .1331 .3397 .1461 .1500 ---+ ---- .1729 .2688 .1690 ,1701 .1710 ,1737 .

$ .1559 .1497 .3526 .1583 .1661 .1798 ---- ---- .1955 .1897 .1894 .1908 .1924 .1968 9 .3702 .3724 .1802 .1876 .1940 .2015 .2082 .2124 .2140 .2149 .2176 .2193 .2196 .2231 10 .1951 .2039 .2188 e2270 .2265 .2260 .2250 .2284 2376 .2476 .2591 .2616 .2554 .2549 il .2281 .2431 ---- ---- .2651 .2556 .2519 .2555 .2681 .2885 ---- ---- .2992 .2918 12 .2664 .2805 - -- ---- .2990 .2880 .2853 .2900 .3029 .3256 ---- -+ - .3391 .3321-13 .3093 .3131 .3265 .3313 .3259 .3229 .3269 .3339 .3422 .3571 ,3747 ,3799 .3736 .3768 14 .3632 .3550 .3567 .3591 .3615 .3686 .3871 .3988 .3970 .4031 .4117 .4182 .4231 .4367 FUEL TYPE i TYFE!

ADJUSTED 2D PIN POWEPS FOR ASSEMBLY 1. SERIAL NUMBER OMN012 (INCLUDES GRID DIP FACTOR OF 1.007$)

1 2 3 4 5 6 7 8 9 10 Il 12 13 14 1 .0500 .C521 .0556 .0589 .0620 .0655 .0708 .0726 .0717 .0728 .0745 .0760 .0775 .0809 2 .0568 .0624 .0686 .0729 .0747 .0760 .0781 .0800 .0825 .0863 .0903 .0919 .0914 .0928 3 .0667 .0752 ---- ~~-- .0898 .0891 .0897 .0918 .0962 .1029 ---- ---- .1083 .3072 4 .0786 ,0879 ---- ---- .1043 .1034 .1038 .1062 ,1112 .1188 -- - .--- .1243 .1224 5 .0926 .0999 .1089 .1149 1172 .1190 .1207 .1235 .1279 .1330 .1385 .1402 .1381 .1381 6 ,1107 .1136 .3198 .1358 .1312 .1374 .1435 .1469 1481 .1492 .1512 .1527 .1530 .1550 1 .1373 .1314 .1342 .1396 .1466 .1576 ---- ----

.1720 .1687 .1691 .1701 .1709 .1734 8 1584 .1515 .1542 .1597 .1671 .1798 ---- - - - .1950 .1900 .1902 .1914 .1928 ,1970 9 .3728 .2747 1822 .1894 .1956 2026 .3083 .2123 .2146 .2157 .2164 .2201 .2203 .2236 10 .1981 .2064 .2206 .2285 .22P6 2281 .2268 .2300 .2392 .2488 .2594 ,2617 .2563 .2558 il ,2317 .2457 ---- ---- .2672 .2586 .2548 .2583 .2707 .2897 ---- --- .2998 .2933 12 .2712 .2840 ---- ---- .3020 .2922 .2895 .2942 .3067 .3279 ---- ---- .3410 .3351 13 43157 .3189 .3310 .3356 .3311 .3286 .3326 .3397 .3477 .3619 ,3781 3833 .3782 .3818 14 .3716 .3628 .3641 .3662 .3687 .3761 .3950 .4072 .4046 .4102 .4185 .4250 .4302 .4441 MAX 1WJM 2D ONE FIN POWER e .4441 AT ROW 14 CCLUMN 14 MAXIMLH 2D ONE PIN POWER W/UNC = .5032 ( .4441 X 1.1000 X 1.0300)

  • HAX1WJM CHANNEL POWER = .4086 AT RCW 13 COLUMN 13 MAXIMUM 3D ONE PIN POWER * .5051 AT ROW 14 COLUMN 14 (!NCLUDES GRID DIP FACTOR OF 1.0075l MAXIMUM 3D ONE PIN POWER W/UNC = .5768 ( .5091 X 1.1000 X 1.03001 r MAXIWJM LNGR = 3.0548 KW/FT ( .5091 X 6.00001 MAXIKJM LMGR W/UNCERTA1NTY = 3.6362 FW/FT ( .5768 I 6.0000 X 1.0300 X 1.02001 PL TO 15.00 FW/PT W/O UNC e 503.6236 ( 15.00 X 100.00 It 3.0548 X .9750))

PL TO 15.00 FW1FT W/ UNCERTAINTY = 420.0959 1 15.00 X 100.00 /( 3.6362 X .97501 - 3.0000)

ASS D" Y AX1AL SHAPE INDEX = .0155 ASSE/ .LY AX1 AL SMAFE INDEX W/UNC= .0000 NORMAL!I.ED ASSEMBLY AXIAL POWER SHAPE:

NODE 1 2 3 4 5 6 7 8 AX1AL POWER .6720 8292 .9307 1.0109 1.0583 1.1052 1.1232 1.146)

NODE 9 10 11 12 13 14 15 16 AXIAL POWER 1.1402 1.1417 1.1145 1.0947 1.0435 9873 .8778 7244 ASAS Manual Revision 0 59 April 19,1994

_ . _ __ ~_ ._.

Figure 13 Sample User Output. File Page 7 of 37 1 PROGRAM ASAS VER$1DN 1. REV DATE 4/12/94. TODAY's DATE is 04/12/94, THE TIME IS 08:19:49 PACE 7 A CODE '19 CREATE NOT CHANNEL DATA Fil.ES FROM A 51MU1A7E-3 PIN FILE FIN FILE NAME' /RPG3/sp/0 PPD /s30 test.p BUN TITLE .t Fort Calhoun Cycle 15 soc 10.5 Hours - esatest CASE ID i B-10.5-A PDIL CASE A - 1004 POWER. ARO XPO = 10.500 CWD/MT. EBAR + 16.119 GWD/MT, POWER = 100.00%. FLOW = 100.001 NO1vr o 15120. STEP 8 2NSERTED. FQ

  • 1.653, INCORE A S1 = .0078 PERIPHERAL ASI e .0023 TOTAL PELATIVE EXCOPE SIGNAL * .4425 FUEL TYPE TYPE 1 P!N POWEPS FOR LIMITING LHGA PLANE 8 FOR ASSFMBLY 18. SERIAL NUMBER oms 027 1 2 3 4 5 6 7 8 9 10 11 12 11 14 1 1.5R77 1.4293 1.7106 1.5957 1.7028 1.7207 1 7110 1.7154 1.7318 1.7184 1.4119 1.1317 1.4454 1.5940 1 1.E578 ' 7e45 1,5732 1.6924 1.4531 1.7220 1.7177 1.7214 1.7322 1.6684 1.7124 1.5941 1.7644 1.4607 1 **14 1.5910 - -- ---- 1.7357 1.7797 1.7488 1.7523 1.7908 1.1535 ---- ---- 1.6113 1,7710 4 1.6572 1.7237 - -- ---- 1.6269 1.7920 1.7775 1.7811 1.8043 1.64;6 ---- - ---* 1.7530 1.6691 5 1.7754 1.6915 1.7566 1.6348 1.8423 1.8156 1.8086 1.8123 1.8289 1.8656 136632 1.7924 1.7253 1.7947 6 1.7956 1.7670 1.8074 1.8076 1.8225 1.8555 1 6395 1.6429 1.8691 1,8460 1.8402 1.8469 1.8066 1.8234 7 1.7775 1.7638 1.7811 1.7994 1.8225 1.6459 ---- --- 1.6563 1.8438 1.8303 1,8202 1.6073 1.8174-8 1.7789 1.7664 1.7847 1.8018 1.8277 1.6518 ---- ---- 1.6630 1.8501 1.8361 1.8254 1.8119 1.4211 9 1.8031 1.1781 1.8215 1.8238 1,8406 1.8'55 1.6587 1.6631 1.8914 1.8675 1.8609 1.8667 1.8244 1.8388 10 1.7901 1.7112 1.7808 1.6610 1.8743 1.8492 1.8438 1.8486 1.8659 1.9011 1.6964 1.8261' 1.7561 1.8224 11 1.6789 1.7526 - -- - -- 1.6677 1.8396 1.8269 1,8317 1.8563 1.6936 -+-- ---- 1.7974 1.7077 12 1.1963 1.6270 ---- - - - 1.7922 1.8415 1.8121 1.8167 1.8578 1.8190 ---- ---- 1.6673 1.8253 13 1.4943 1.7940 1.6247 1.7542 1.7196 1.7955 1.7934 1.7979 1.8108 1,7446 1.7885 1.6629 1.8366 1,5186 14 1.6421 1.4797 1.7761 1.6638 1.7815 1.8051 1.7962 1.800', 1.8199 1.8059 1.6951 1.8160 1.5149 1,6725 F1 FACTORS FOR AASEMBLY 18. SEFIAL NUMBER OMSC27 1 2 3 4 5 6 7 8- 9 10 11 12 13 14 1 1.1956 1.1903 1.1931 1.1896 1.1941 1.1957 1.1958 1,1958 1.1954 1.1936 1.1886 1.1918 1.1887 1.1939 2 1.1904 1.1924 1.1901 1.1939 1.1901 1.1947 1.1954 1.1953 1.1944 1.1894 1,1929 1.1888 1.1909- 1.1887 3 1.1934 1.1903 ~~-- -- - 1.1948 1.1949 1.1954 1.1953 1.1945 1.1942 --- +--- 1.1989 1.1920 4 1.1900 1.1942 ---- ---+ 1.1907 1.1943 1.1952 1.1951 1.1939 1.1902 --- ---a 1.1931 1.1688 5 1.1947 1.1905 1.195D 1.1908 1.1937 -1.1943 1.1939 1.1938 1.1941 1.1933 1.1902 1.1943 1.1896 1,1937 6 1.1962 1.1951 1.1951 1.1943 1.1943 1.1935 1.1896 1.1895 1.1933 1.1940 1.1939 1,1946 1.1945 1.1955 7 1,1962 1.1957 1.1955 1.1952 1,1938 1.1895 ---- ---- 1.1895 1.1937 1.1950 1.1952 1.1953 1.1954 8 1.1959 1.1954 1.1951 1.1950 1.1937 1.1894 ---- - -- 1.1895 1,1936 1.1949 1.1952 1.1952 1.1956 9 1.1952 1.1942 1.1943 1.1937 1.1918 1.1930 1.1892 1.1893 1,1910 1.1938 1.1937 1.1943 1.1942 1.1951 10 1.1929 1.1889 1.1937 1.1897 1.1927 1.1935 1.1932 1.1912 1.1935 1.1927 1.1890 1.1938 1,1891 1.1932 11 1.1875 1.1920 ---- --- 1.1893 1.1931 1.1942 1.1942 1.1931 1.1895 ---- ---- 1.1924 1.1840 12 1.1902 1.1875 ---

1.1910 1.1933 1.1940 1.1941 1.1934 1.1932 ---

1.1880 1.1908 13 1.1866 1.1890 1.1872 1.1914 1.1879 1.1928 1.1937 1.1938 1.1930 1.1982 1.1918 1.1977 1.1895 1.1872 14 1.1916 1.1865 1,1897 1.18E7 1.1917 1,1935 1.1938 1.1939 1,1937 3.1920 1.1871 1.1902 1.1870 1.1918 A53DtBLY AX1AL PEAlt1N3 FAC*rOR = 1.1926 (FROM 16 PLANE DATA)

T ASAS Manual Revision 0 60 Apnl 19,1994

~ - - - , . -. - . . - . . . - . - . - . -- - .

Figure 13 Sample User Output File Page 8 of 37 1 PROGRAM ASAS VERSION 1, REV DATE 4/12/94. TODAY'S DATE 15 04/12/94. THE TIME IS 08:19:49 PAGE 8 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME /RPC1/Sp/OPPD/a30 test.p RUN TITLE  : Fort Calhoun Cycle 15 BOC 10.5 Hours - asatest CASE ID  : B-10.5-A PDIL CASE A - 2004 POWER, ARO ,

XPO e 10.500 CWD/MT, EBAR

  • 16.119 GWD/NT. POWER = 100.009. FI4W = 100.004 NOTw!' = 15120. STEPS INSERTED, FQ s 2.000. F-DELTA-H = 1.653, INCORE ASI = .0078. PERIPMERAL ASI = .0023 TOTAL RELATIVE EXCORE E!GNA1. * .4425 FUEL TYPE : TYPE 1 2D P!N POWERS FOR ASSENSLY 18, SERI AL NUMBER OMS 027 1 2 3 4 5 '6 7 8 9 10 11 12 13 14 1 1.3279 1.2009 1.4337 1.3415 1.4259 1.4391 1.4308 1.4345 1.4481 1.4391 1.3576 1.4530 1.2160 1.3351 2 1.2246 1.4630 1.3218 1.4176 1.3891 1.4413 1.4369 1,4401 1.4503 1,4028 1.4355 1.3409 1.4816 1.2288 3 1.4784 1.3366 *--- ---- 1.4527 1.4894 1.4629 1.4660 1.4992 1.4684 ---- ,--- 1.3569 1.4858 4 1.3926 1.4434 ---- ---- 1.3663 1.5005 1.4872 1.4903 1.5112 1.3829 ---- ---- 1.4692 1,4040 5 1.4861 1.4209 1.4699 1.3729 1.5434 1.5202 1.5149 1.5181 1.5317 .1.5634 1.3975 1.5008 1.4504 1.5035 6 1.5011 1,4785 1.5124 1.5134 1.5260 1.5547 1.3782 1.3811 1.5663 1.5460 1.5413 1.5461 1.5125 1.5253 7 1.4859 1.4752 1.4898 1.5055 1.5267 1.3837 ---- **-- 1.3925 1.5446 1.5317 1.5229 1.5121 1.5201-8 1.4875 1.4777 1.4931 1.5095 1.5312 1.3887 ---- ---- 1.3981 1,5500 1.5366 1.5273 1.5159 1.5233 9 1.5087 1.4889 1.5252 1,5279 1.5419 1.5721 1.3947 1.3984 1.5853 1.5644 1.5590 1.5630 1.5278 1.5386 10 1.5006 1.4393 1.4919 1.3962 1.5714 1.5494 1.5452 1.5493 1.5634 1,5956 1.4258 1.5296 1.4768 1,5274 11 1.4138 1.4703 ---- ---- 1.4023 1.5419 1.5298 1.5338 1,5558 1.4239 ---- ---- 1.5074 1.4375 12 1.5092 1.3701 + -- ---+ 1.5023 1.5432 1.5176 1.5214 1.5567 1.5244 ---- ---- 1,4035 1.5328 13 1.2593 1.5089 1.3685 1.4724 1.4476 1.5052 1.5023 1.5060 1.5179 1.4683 1.5007 1.4001 1.5439 1.2792 14 1.3781 1.2471 1.4928 1.4021 1.4950 1.5125 1.5046 1.5083 1.5246 1.5150 1.4279 1.5257 1.2763 1.4033 FUEL TYPE . TYPE 1 ANUSTED 2D PIN POWERS FOR ASSEMBLY 18, SERIAL FJMBER OMS 027 (INCLUDES GRID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3413 1.2075 1.4451 1.3481 1.4385 1.4537 1.4455 1.4491 1,4630 1.4517 1.3634 1.4630 1.2211 1.3466 2 1.2316 1.4738 1.3290 1.4298 1.3965 1.4548 1.4511 1.4542 1.4634 1.4095 1.4467 1.3467 1,4905 1.2340 3 1.4906 1.3441 ---- ---- 1.4664 1.5035 1.4774 1.4804 1.5129 1.4814 *- - ---a 1.3629 1.4961 4 1.4001 1.4562 ---- ---- 1.3744 1.5139 1.5016 1.5047 1.5243 1.3904 ---- ---- 1.4809 1.4101 5 1.4999 1.4290 1.4840 1,3811 1.5564 1.5338 1.5280 1.5310 1.5451 1.5761 1.4051 1,5143 1.4576 1.5162 6 1.5169 1.4927 1.5269 1.5271 1.5397 1.5675 1.3851 1.3879 1.5790 1.5595 1.5546 1.5603 1.5263 1.5405 7 1.5017 1.4901 1.5047 1.5202 1.5397 1.3905 ----

1.3993 1.5577 1.5463 1.5378 1.5269 1.5354 8 1.5028 4.4923 1,5077 1.5239 1.5441 1.3934 ---- ---- 1.4049 1.5630 1.5512 1.5421 1.5307 1.5385 9 1.5233 1.5021 1.5388 1.5407 1.5550 1.5844 1.4013 1.4050 1.5978 1.5771 1.5721 1.5770 1.5413 1.5534 10 1.5123 1.4457 1.5044 1.4032 1.5834 1.5622 1.5576 1.5617 1.5763 1.6078 1.4331 1 5427 1.4836 1.5396 11 1.4184 1,4806 ---- ---- 1.4089 1.5541 1.5434 1.5474 1.5632 1.4308 ---- ---- - 1.5184 1.4427 12 1.5175 1.3745 ---- ---- 1.5141 1.$551 1,5309 1.5348 1.5695 1.5367 ----

1.4986 1.5420 13 1.2624 1.5156 1.3725 1.4820 1.4528 1.5168 1.5151 1.5189 1.5298 1.4739 1.5109 1.4048 1.5516 1.2829 14 1.3872 1.2500 1.5004 1.4056 1.5051 1.5250 1.5174 1.5212 1.5375 1.5256 1.4320 1.5341 1.2798 1.4129 MAXIM"M 20 ONE P1H POWER e 1.6078 AT ROW 10 COLUMN 10 MAXIMUM 2D ONE FIN POWER W/UNC a 1.8216 (1.6078 X 1.1000 X 1.0300)

MAXIMUM CHANNEL POWER = 1.5899 AT ROW 9 COLUMN 9 MAXIMUM 3D ONE PIN POWER = 1.9174 AT ROW 10 COLUMN 10 (INCLUDES GRID CIP FACTOR OF 1.0015)

MAXIMUM 3D ONE PIN POWER W/UNC e 2.1724 11.9174 X 1.1000 X 1.0300)

MAXIMUM LHCR e 11.5042 FW/FT 11.9174 X 6.0000}

MAXIMUM LHCR W/UNCEPTAINTY = 13.6938 KW/FT (2.1724 X 6.0000 X 1.0300 X 1.0200)  !

PL TO 15.00 FW/ PT W/O UNC = 133.7298 ( 15.00 X 100.00 /t11.5042 X .9750))

PL TO 15.00 KW/FT W/ UNCERTAINTY = 109.3469 ( 15.00 X 100.00 /f13.6938 X .9750) - 3.0000)

ASSENBLY AX1AL SHAPE INDEX e .0151 ASS 104BLY AXIAL SRATE INDEX W/UNC* .0000 NORMALIZED AS$fMBLY AX1AL POWER SHAPEi NODE 1 2 3 4 5 6 7 8 AX1AL POWER .5505 .8389 .9876 1.0830 1.1245 1.1700 1.1738 1.1924 NCDE 9 10 11 12 13 14 15 16 ARIAL POWER 1.1703 1,1662 1.1225 1.0941 1.0232 9475 7916 .5636 ASAS Manual ikvision 0 61 April 19,1994

- -- - - - -- -- .- =- , - - . . - - - -. _ - . - .

Figure 13 Sample User Output File Page 9 of 37 1 PROGRAM ASAS VERSION 1. REV DATE 4/12/94. TODAY'S DATE 15 04/12/94 THE TIME IS 08:19:49 PAGE 9 A CODE TO CREATE NOT CHANNEL DATA Fil.ES FPOM A SIMU1 ATE-3 PIN FILE PIN FILR NAME r /RPG3 / Sp/0PFD/s 30t est .p RUN TITLE i Fort Calhoun Cycle 15 SOC 10.5 Housa + amatest CANE ID B 10.5-A PDIL CASE A - 100% POhER, ARO XPo a 10.500 GWD/prf. EBAR s 16.119 GWD/MT. POWER = 100.004 FLOW = 100.004 NOWf a 15120. STEPS INSERTED. FD e 2,000 F-DELTA-M = 1,653, INCORE ASI = .0078, PERIPHEBAL ASI = .0033 TOTAL PELATIV8 EXCORE SIGNAL e ,4425 l

FUBL TYPE , TYPE 1 PIN POWERS FOR LIMITING LHGR PLANE 8 FOR ASSEMBLY 16, SERIAL NUMBER OM5019 1 2 3 4 5 6 7 8 9 10 11 11 13 14 1 1.4140 1.3226 1.6547 1.7210 1.7129 1.7199 1.1209 1.7321 1,7608 1.7866 1.8311 1.7998 1.4766 1.6314 '

2 1,3176 1.6398 1.5223 1.6896 1.6610 1.7342 1.7375 1,7471 1.7700 1.7237 1.7831 1.6393 1.8088 1.5057 3 1.6433 1.5178 ---- -+-- 1.7748 1.8100 1.7776 1.7854 1.8408 1.8300 ---- ---- 1.6530 1,8500 4 1.7047 1.6805 ---- ---- 1.8273 1.8566 1,8177 1,8237 1.8825 1.8737 ---- --- 1.8062 1.8918 5 1.6931 1.6489 1.1676 1.8243 1.9275 1.8622 1.8919 1.8965 1.8833 1.9675 1.8814 1.8459 1.7533 1.8527 6 1.6976 1.7194 1.8008 1.8519 1.8606 1.7975 1 8856 1.8899 1.8165 1.8934 1.9005 1.8669 1,8093 1.8317 7 1.6979 1.7219 1.7679 1.8128 1.8902 1.8857 ---- ---- 1.9052 1.9223 1.8561 1.8246 1.7964- 1.8030 8 1.7097 1.7324 1.7770 1.8204 1.8966 1.8912 ---- ---- 1.9101 1.9260 1.8588 1.8264 1.7974 1.0032 9 1.7381 1.1563 1.8343 1.8820 1.8866 1.8206 1.9062 1,9095 1.8323 1.9062 1.9105 1.8742 1.8142 1.8344..

10 1.7640 1.1116 1.8260 1.8767 1.9755 1.9024 1.9276 1.9293 1.9101 1.9902 1.8984 1.8586 1.7621 1.8583 11 1.8084 1.7718 ---- ---- 1.8933 1.9145 1.866? 1.8676 1.9200 1,9040 ---- ---- 1.8190 1.9007 12 1.7766 1.E281 ---- ---- 1.8598 1.8840 1,8395 1.8399 1.8876 1,8679 ---- - -- 1.6690 1.8639 13 1.4543 1.7857 1.6450 1.8073 1.7616 1.8228 1.8115 1.8113 1.8249 1,7678 1.8193 1.6658 1.8318 1.5219 14 1,5950 1.4718 1.8170 1.8673 1.8381 1.8257 1.8068 1.8057 1.8258 1.8417 1.8771 1.8367 1,5026 1.6591 FZ FACTOPS FOR ASSEMBLY 16. SE91AL NUMBER CMS 019 1 2 3 4 b 6 7 8 9 10 11 12 13 14 1 1.2083 1.2016 1.2080 1.2092 1.2094 1.2100 1.2095 1.2093 1.2094 1.2083 1,2075 1.2058 1.2010 1.2055 2 1.2036 1 2070 1.2052 1.2094 1.2056 1,2095 1.2099 1.2096 1.2087 1,2042 1.2075 1.2027 1.2040 1.2006 3 1.2081 1.2054 ---- - - - 1.2106 1.2097 1.2100 1.2097 1.2087 1.2090 ---- ---- 1.2017 1.2045 4 1.2095 1.2098 ---* ---- 1.2110 1.2100 1.2099 1.2096 1.2089 1 2091 ----

1.2055 1.2052 5 1 2099 1.2061 1.2110 1.2113 1.2101 1.2090 1.2093 1,2008 1.2076 1.2078 1.2080 1.2068 1.2011 1,2049 6 1.2106 1.2101 1.2103 1.2105 1.2092 1.2056 1.2095 1,2091 1.2041 1.2066 1.2067 1.2055 1.2046 1.2051 7 1.2102 1,2108 1.2108 1.2106 1.2097 1.2098 ----

1.2081 1.2068 1.2065 1.2056 1.2048 1.2043 8 1.2103 1.2107 1.2106 1.2104 1.2095 1 2095 ---- --- 1.2078 1.2064 1.2061 1.2052 1,2044 1.2038 9 1.2105 1 2099 1,2099 1.2099 1.2085 1.2048 1.2086 1.2081 1.2029 1.2053 1.-2054 1.2041 1.2031 1.2036 10 1.2096 1.2056 1.2103 1.2104 1.2089 1.2016 1.2076 1.2071 1.2057 1.2057 1.2057 1.2044 1.1985 1.2022 11 1.2090 1.2091 ----

.1.2094 1.2080 1.2077 1.20?1 1,2061 1.2061 ---- --- 1.2018 1.2013 12 1.2075 1.2045 ---- ---- 1.2085 1.2072 1.2671 1.2066 1.2052 1.2051 s-* - -- 1.1970 1.1996 13 1.2028 1.2060 1.2039 1.2076 1,2032 1.2066 1.2066 1.2060 1.2046 1.1997 1.2026 1.1974 1.1984 1.1947 14 1.2074 1.2027 1.2067 1 2074 1.2071 1.2072 1.2061 1,2055 1.2052 1.2036 1.2024 1,2002 1.1950 141994 ASSEMBLY AX1AL PEAKING FACTOR

  • 1.2067 WROM 16 PLANE DATA)

E ASAS Manual Revision 0 62 April 19,1994

Figure 13 i Sample User Output File Page 10 of 37

-1 PROGRAM ASAS VERSION 1, REV DATE 4/12/94. TODAY'S DATE IS 04/12/94 THE TIME IS 08:19:49 PAGE 10 A CODE M CREATE MOT CHANNEL DATA FILES FROM A SIMUIATE-3 FIN FILE PIN FILE NAME : /RPO3/Sp/OPPD/s30 test.p RUN TITLE s Port Calhoun Cycle 15 BOC 10.5 H wss a esatest CASE ID t 8-10.5-A PD1b CASE A - 1005 90WER. ARG XPo e 10.500 GWD/MT. EBAR = 16.119 GWD/Pfr POWER = 100.009 rLOW = 100.004 NOTwf = 15120. ETEPS INSERTED. FQ = 2.000, F-DELTA-H e 1.653, INCORE AS! = .0078, PERIPMERAL ASI = .0023 TOTAL RELAT3VE EXCORE SIGNAL = .4425 FUEL TYPE TYPE 1 2D FIN POWERS FON ASSEM8LY 16. SERIAL NUMBER OMS 019 1 2 3 4 5 6 7 8 9 to 11 12 13 14 1 1.1702 1.0989 1.1698 1.4233 1.4163 1.4214 1.4228 1.4323 1.4560 1.4787 1.5164 1.4926 1.2295 1.3532 2 1.0948 1.3587 1.2631 1.3910 1.3778 1,4339 1.4361 1.4443 1.4644 1.4314 1.4767 1.3631 1.5024 1,2542 3 1.3603 1.2592 ---- ---- 1.4661 1.4963 1.4692 1.4759 1.5229 1.5137 ++-- ---- 1.3755 1.5366 4 1.4095 1.3891 ---- +--- 1.5089 1.5343 1.5023 1.5077 1.5572 1.5497 ---- ---- 1.4983 1.5697 5 1.3994 1.3672 1.4597 1.5061 1.5928 1.5403 1.5645 1.5609 1 5595 1.6290 1.5574 1.5296. 1.4598 1.5376 6 1.4023 1.4208 1.4879 1.5299 1.5387 1.4909 1.5589 1.5631 1.5087 1.5692 1.5749 1.5486 1.5020 1.5199 7 1.4029 1.4222 1.4602 1.4974 1.5625 1.5587 ---- ---- 1.5770 1.5929 1.5385 1.5134 1.4909 1.4971

1.5815 1,5965 1,5411 -1.5154 8 1.4127 1.4109 1.4678 1.5040 1.5681 1.5636 ---- 1.4923 1.4979 9 1.4158 1.4516 1.5161 1 5555 1.5611 1.5111 1.5771 1.5806 1.5232 1.5815 1 5P50 1.5564 1.5079 1.5241 10 1.4584 1.4197 1.5087 1.5505 1.6341 1.5754 1.5962 1.5983 1.5843 1.6507 1.5745 1.5432 1.4703 1.5457 11 1.4958 1.4654 ---+ ---- 1.5655 1.5848 1.5457 1.5471 1.5919 1.5786 ---- ---- 1.5135 1.5822 12 1.4715 1.3517 ---- --- 1.5388 1.5606 1.5239 1.5249 1.5662 1.5500 - - - ---- 1.3943 1.5538 13 1.2091 1.4840 1.3664 1.4966 1.4641 1.5107 1.5013 1.5019 1.5150 1,4736 1.5128 1.3912 1.5285 1.2738 14 1.3210 1.2237 1.5058 1.5465 1.5227 1.5123 1.4980 1.4979 1.5150 1.5302 1.5612 1.5303 1.2574 1.3833 FUEL TYFE TYPE 1 AnJUSTED 2D PIN POWERS FOR ASSEMBLY 16 SERIAL NUMBER OMS 019 (INCLUDES GRID CIP FACMR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1806 1,1043 1.3916 1.4370 1.4302 1.4360 1.4368 1.4462 1.4702 1.4917 1.5289 1.5*27 1.2329 1.3621 t 2 1.1002 1.3692 1.2711 1.4107 1.3869 1.4480 1.4508 1.4588 1.4779 1.4392 1.4888 1.3681 1.5102 1.2572 3 1.3721 1.2673 ---- ---- 1.4818 1.5113 1.4842 1.4907 1.5370 1.5279 ---- ---- 1.3802 1.5453 4 1.4234 1.4031 --~~ ---- 1.5257 1.5502 1,5177 1.5227 1.5718 1.5644 ----

1.5081 1.5795 5 1.4137 1.3768 1.4759 1.5232 1.6094 1 5548 1.5796 1.5835 1.5724 1.6427 1.5708 1.5412 1.4639 1.5469 6 1.4174 1.4356 1.5035 1.5462 1.5535 1.5008 1.5744 1.5780 1.5167 1.5809 1.5868 1.5588 1.5107 1.5294 7 1.4176 1.4377 1.4761 1.5136 1.5762 1.5744 ---- ---- 1.5908 - 1.6050 1.5498 1.5235 1.4999 1.5054.

8 3.4275 1.4465 1.4837 1.5199 1.5836 1.5790 ---- ---- 1.5948 1.6081 1.5520 1.5249 1.5007 1.5056 9 1.4512 1.4664 1 5315 1.5713 1.5752 1.5201 1.5915 1.5944 1.5299 1.5916 1.5952 1.5648 1.5148 1.5316 to 1.4729 1.4291 1.5246 1.5669 1.6494 1.5884 1,6095 1.6109 1.5948 1.6617 1.5851 1.5518 1.4713 1.5515 -

11 1.5099 1.4794 ---* ---- 1.5808 1.5985 1.5586 1.5591 1.6031 1.5897 ---- ---- 1.5188 1.5870 12 1.4835 1.3594 ---- ---- 1.5528 1.5730 1.5359 1.5362 1.5761 1.5596 ---- --~~ 1.3935 1.5563 13 '1.2142 1.4943 1.3735 1.5090 1.4709 1.5219 1.5125 1.5121 1.5237 1.4160 1.5190 1.3908 1.5294 1.2707 14 1.3318 1.2288 1.5171 1.5591 1.5347 1.5244 1.5086 1,5077 1.5245 1.5377 1.5673 1.5335 1.2546 1.3852 MAXIMUM 2D ONE PIN POWER s 1.6617 AT R0W 10 COLUMN 10 MAKIMUM 2D ONE PIN POWER W/UNC o 1.8827 (1.(617 X 1.1000 X 1.0100)

MAXIM'.!M CHANNEL POWER = 1.6123 AT ROW 10 COLUMN 9 MAXIMUM 3D ONE PIN POWER = 2.0051 AT pow 10 COLUMN 10 (INCLUDES GRID D1P FACTOR OF 1.0075)

MAXIMUM 3D CNB PIN POWER W/UNC = 2.2718 (2,0051 1 1.1000 X 1.0300)

  • MAXIMUM LMGR = 12.0305 FW/FT (2.0051 X 6.0000)

MAXIMUM LMGR W/ UNCERTAINTY = 14.3203 KW/FT (2.2718 A 4.0000 1 1.0300 X 1.02001 PL 70 15.00 FW/FT W/O VNC

  • 127.9799 ( 15.00 X 100.00 r (12.0305 X .9750))

PL TO 15.00 KW/FT W/UTCEPTAINTY = 104 4323 ( 15.00 3: 100.00 /(14,3203 x .97501 - 3.0000)

ASSEMBLY AX1AL SRAPE INDEX s .0273 ASSEXBLY AXIAL SHAPE 1NDEX W/ UNCO .0000 NORMALIZED ASSEMBLY AX1AL Wa'ER $HAFEs NODE 1 2 3 4 5 6 7 8 AX1AL POWER .5199 .8407 1.0066 1.1088 1.1500 1.1932 1.1922 1.2067 -

NorE 9 10 11 12 13 14 15 16 AX1AL POWER 1.1790 1.1707 1.1216 1.08P9 1.0123 ,9301 7639 .5154 [

4 i

t I

?

ASAS Manual Revision 0 63 April 19,1994

- --.- m , , y

. .ew;. __,.,

,i.+- e , . - . . - J 433 4- .A. A:: 4- W--.-m..+a.4-i'l

-.Ji+ni4- --vi4--A JMa'.e A.# .--- .M,_ A- . _ . ,a .u__

l l

Figure 13 l

. Sample User Output File Page 11 of 37 i

l 1 PROG 8AM AGAE VER$10N 1. REV CATE 4 /12 /94. TODAY'S DATE 18 04/12/94 THE TIME 15 04:19:49 PAGE 11 A CODE TO CREATE WM CHANNEL DATA FILES FHOM A SIMULATE 3 FIN FILE PIN FILE NAME : /RPG3/Sp/OPPD/s30 test.p RUN TITLE s Fort Calhoun Cycle 15 DOC 10.5 Hours - asetest CASE ID B-10.5-A PDIL CASE A - 100% POWER. ARO XPO

  • 10.500 CWD/Kr. EBAR e 16.119 GWD/MT. POWER e 100.00%. Plow = 100.004 NOTWP e 15120. ETEPs INSERTED, FQ = 2.000 F-DELTA-H e 1.653, INCORR ASE = .0078. PER1PHERAL ASI e .0023 TOTAL RELATIVE EXC' ORE SIGNAL e .4(25 PUEL TYPE . TYPE 1 PIN POWERS FOR LIMITING LNGR PLANE 8 FOR AS$DiBLY 25, SERIAL NUK8ER OM3034

' 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.6673 .1.5157 1.8169 1.6909 1.7974 1.7761 1.5991 1.5991 1.7761 1.7974 1.6909 1.8169 1.5157 1.6613 2 1.5097 1.8222 1.6460 1.7626 1.6914 1.7616 1.7347 1.7347 1.7616 1.6934 1.7626 1.6460 1,8222 1.5097 3 1,7995 1.6370 ---- ---- 1.6152 1.7868 1.7705 1,7705 1.7868 1.6152 ----

1.6370 1.1995 4 1.6638 1.7417 ---- ---- 1.6258 1.7986 1.1834 1.1834 1,7986 1.6258 ---* - - - 1.7417 1.6638 5 1.7560 1.6617 1.5940 1.6148 1.8366 1.6109 1.1990 1.7990 1.8109 1.8366 1.6148 1.5940 1.6617 1.7560 6 1.7214 1.7159 1.7507 1.7737 1.7982 1.8309 1.6161 1.6161 1.8309 1.7982 1.7737 1.7507 1,7159 1.7214 7 1.5341 1.6766 1.7222 1.746t 1.7741 1.6051 ----

1.6051 1.7741 1.7465 1.7222 1.6766 1.5361 8 1.5246 1.6664 1.7124 1.7371 1.7645 1.5947 ---- ---- 1.5947 1.7645 1.7371 1.7124 1.6664 1.5246 9 1 6829 1.6188 1.7141 1.7377 1.7620 1.7939 1.5819 1.5819 1.7939 1.7620 1.7377 1.7141 1,6788 1.6829 to 1.6883 1.5986 1.5346 1.5558 1.7719 1.7477 1.7362 1.7362 1.7477 1.7719 1.5558 1,5346 1.5986 1.6883 11 1.5727 1.6497 ---- ---- 1.5434 1.7099 1.6957 1.6957 1.7099 1.5434 ----

1.6497 1.5727 12 1.6764 1 5261 ---- ---- 1.5109 1.6741 1,6594 1.6594 1.6741 1.5109 ---- ---- 1,5261 1 6764 13 1.3885 1.6772 1.5160 1.62E5 1.5636 1.6292 1.6050 1.6030 1.6292 1.5636 1.6265 1.5160 1.6772 1.3885 '

14 1.5277 1.3824 1.6579 1.5437 1.6443 1.6267 1.4636 1.4636 1.6267 1.6443 1.5417 1.6579 1.3824 1.5277 F3 FACTOP9 FOR ASSEMBLY 25. SERIAL NUMBER OMS 014 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1906 1.1857 1.1889 1.1854 1.1932 1.1909 1.1860 1,1860 1.1909 1.1902 1.1854 1.1889 1.1857 1.1906 2 1.1853 1.1873 1.1850 1.1888 1.1841 1.1895 1.1897 1.1897 1.1895 1.1841 1,1938 1.1850 1.1873 1.1853 3 1.1980 1.1845 ----

1.1840 1.1884 1.1900 1.1900 1.1884 1.1840 ----

1.1845 1.1880 '

4 1 1839 1.1877 ----

3.1837 1.1877 1.1893 1.1893 1.1877 1.1837 ---- ---- 1.1877 1.1839 5 1.1880 1.1823 1,1827 1.1830 1,1866 1.1876 1.1875 1.1875 1.1876 1.1866 1.1830 1.1817 1.1823 1.1880 6 1.1879 1.1869 1.1864 1.1863 1.1868 1.1860 1.1825 1.1825 1.1960 1.1868 1.1863 1.1844 1.1869 1.1879 7 1.1821 1.1863 1.1872 1.1871 1.1860 1.1818 ---- ---- 1.1818 1.1860 1.1871 1.1872 1.1863 1.1822 8 1.1811 1.1855 1.1864 1.1864 1.1853 1.1808 ----

1.1808 1.1853 1.1864 1.1864 1.1855 1.1811 9 1.1854 1.1845 1.1940 1.1840 1.1846 1.1837 1.1800 1.1800 1.1817 1.1846 1.1940 1.1840 1.1845 1.1854 10 1,1818 1.1780 1.1784 1.1788 1.1821 1.1830 1.1837 1.1P37 1,1836 1.1827 1,1788 1.1784 1.1783 1.1838 >

11 1.1778 1.1818 - - - -

1 1781 1.1825 1.1840 1.1840 1.1825 1.1781 ---- ---* 1.1818 1.1778  :

12 1.1805 1.1769 -- - ---- 1.1768 1.1817 t.1833 1.1833 1.1817 1.1768 ---- ---- 1.1769 1.1805 13 1.1763 1.1784 1.1761 1.1803 1.1757 1 1814 1.1817 1,1817 1.1814 1.1757 1.1803 1.1761 1.1784 1.1763 14 1.1809 1.1755 1.1790 1.1755 1.1807 1.1814 1.1765 1.1765 1.1816 1.1807 1.1755 1.1790 1.1755 1.1809 ASSEMBLY AX1AL PEAF.ING PACTOR = 1.1839 (FROM 16 PLANE DATA) 6 I

9 i

' ASAS Manual Revision 0 64 April 19,1994 '

l

l l

l Figure 13 Sample User Output File 7

Page 12 of 37 1 PROGRAM ASAS VERSION 1. REV DATE 4/12/94, TODAY'S DATE 25 04/12/94 THE TIME IS 08:19:49 PAGE 12 -

A COLE 70 CREATE MOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE 'j PIN FILE NAME /RPG3/Sp/OPPD/s30 test.p 1 RUN TITLE i Fort Calhoun cycle 15 BOC 10.5 Hours - asetest i CASE in i B-10.5-A PD1L CASE A

  • 100% POWER. ARO XPO e 10.500 GWD/MT. EBAR s- 16.119 GWD/MT. POWER e 100.006 F1hw e 100.008 NOTWT . 15120. STEPS INSERTED. FQ = 2.000, F-DELTA-H
  • 1.6$3. INCORE ASI = .0078 PERIPHERAL ASI = .0023 TOTAL RELATIVE EXCOPE SIGNAL = .4425 FUEL TYPE TYPE 1 l

2D PIN POWERS FOR ASSD(SLY 25. SERIAL NUMBER OMS 034 l 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.4004 1.2784 1.5282 1.4264 1.5102 1.4915 1.3483 1.3483 1.4915 1.5102 1.4264 1.5282 1.2784 1.4004 2 1.2736 1.5348 1.3891 1.4826 1.4301 1.4809 1.4581 1.4581 1.4809 1.4301 1.4826 1.3891 1.5348 1.2736-3 1.5147 1.3820 ---- ---* 1.3643 1.5035 1.4978 1.4878 1.5035 1.3643 ---- ---- 1.3820 1.5147 4 1.4054 1.4665 ---- ---- 1.3735 1.5143 1.4996 1.4996 1.5143 1.3735 ---- ---- 1.4665 1.4054 5 1.4781 1.4055 1.3478 1.3650 1.5478 1.5249 1.5150 1.5150 4.5249 1.5478 1 3650 1.3478 1.4055 1.4781 6 1.4491 1.4456 1.4756 1.4952 1.5151 1.5438 1.3667 1.3667 1.5438 1.5151 1.4952 1.4756 1.4456 1.4491 7 1.2994 1.4133 1.4506 1.4712 1.4959 1.3582 ---- ---+ 1.3582 1.4959 1.4712 1.4506 1.4133 1.2994 I I

8 1.2908 1.4057 1.4433 1.4642 1.4887 1.3505 ---- ---- 1.3505 1.4887 1.4642 1.4413 1.4057 1.2908 9 1.4197 1.4174 1.4477 1.4476 1.4874 1.5155 1.3406 1.3406 1.5155 1.4874 1.4616 1.4477 1.4174 1.4197 10 1.4262 1.3571 1.3023 1/3198 1.4961 1.4763 1.4668 1.4668 1.4763 1.4981 1.3198 1.3023 1.3571 1.4262 11 1.3353 1.3959 -- - ---- 1.3101 1.4460 1.4321 1.4321 1.4460 1.3101 ---- ---- 1.3959 1.3353 12 1.4201 1.2967 ---- ---- 1.2834 1.4167 1.4023 1.4023 1.4167 1.2838 ---- ---- 1.2967 1.4201 13 1.1804 1.4233 1.2889 1.3780 1.3300 1.3790 1.3582 1.3582 1.3790 1.3300 1.3780 1.2889 1.4233 1.1804 14 1.2937 1.1760 1.4063 1.3132 1.3926 1.3767 1.2440 1.2440 1.3767 1.3926 1.3132 1.4063 1.1760 1.2937 FUEL TYPE : TYPE 1 ADJUSTED 2D PIN POWERS FOR ASSEMBLY 25, SERI AL NUMBER OMS 034 (INCLUDES GRID D1P FACTOR OF 1.00751 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.4188 1.2899 1.5461 1.4389 1.5296 1.5115 1.3608 1.3608 1.5115 1.5296 1.4389 1.5461 1.2899 1.4188 2 1.2847 1.5506 1.4007 1.4999 1.4411 1.4991 1.4762 1.4762 1.4991 1.4411 1.4999 1.4007 1.5506 1.2847 3 1.5314 1,3930 ---- ---+ 1.3746 1.5205 1.5066 1.5066 1.5205 1.3746 ---- ---- 1.3930 1.5314 4 1.4159 1.4821 ---- ---- 1.3835 1.5306 1.5176 1.5176 1.5306 1.3835 ~*-- ---- 1.4821 1.4159 5 1.4943 1.4141 1.3565 1.3741 1.5629 1.5410 1.5309 1.5309 1.5410 1.5629 1.3741 1.3565 1 4141 1.4943 6 1.4649 1.4602 1.4898 1.5094 1.5302 1.5581 1.3753 1.3753 1.5581 1.5302 1.5094 1.4898 1.4602 1.4649 7 1.3072 1.4267 1.4656 1.4862 1.5097 1.3659 --+- ---- 1.3659 1.5097 1.4862 1.4656 1.4267 1.3072 8 1.2974 1.4181 1.4573 1.4782 1.5016 1.3571 ---- ---- 1.3571 1.5016 1.4782 1.4513 1.4181 1.2974 9 1.4321 1.4287 1.4587 1.4787 1.4994 1.5266 1.3462 1.3462 1.5266 1.4994 1.4787 1.4587 1.4287 1.4321 to 1.4367 1.3604 1.3059 1.3239 1.5079 1.4873 1.4775 1.4775 1.4873 1.5079 1.3239 1.3059 1.3604 1.4367 11 1,3383 1.4039 ---- ---- 1.3134 1.4551 1.4430 1.4430 1.4551 1.3134 - -- ---- 1.4039 1.3383 12 1.4266 1.2987 ---- ---- 1,2857 1.4241 1.4121 1.4121 1.4247 1 2857 ---- ---- 1.2987 1.4266 13 1.1816 1.4273 1.2901 1.3841 1.3306 1.3864 1.3658 1,3658 1.3864 1.3306 1.3841 1.2901 1.4273 1.1816 14 1.3000 1.1764 1.4109 1.3137 1.3993 1.3843 1.2455 1.2455 1.3843 1.3993 1.3137 1.4109 1.1764 1.3000 MAXIMUM 2D ONE FIN POWER s 1.5629 AT ROW 5 COLUMN 5 MAXIMUM 2D ONE PIN POWER W/UNC . 1.7708 11.5629 x 1.1000 K 1.0300)

MAXIMUM CHANNEL POWED = 1.5481 AT ROW 5 COLUMN 5 MAXIMUM 3D ONE FIN POWER . 1.8503 AT ROW 5 COLL 901 5 (!NCLUDES GRID DIP FACTOR OF 1.00751 MAXIM'fM 3D ONE FIN POWER W/UNC e 2.0964 11.8503 X 1.1000 X 1.0300)

MAX 1 MUM LHGR = 11.1021 FW/FT (1.8503 X 6.0000)

MAXIMUM LNGR W/ UNCERTAINTY = 13.2151 FW/FT (2.0964 X 6.0000 X 1.0300 X 1.0200)

PL TO 15.00 FW/FT W/O UNC = 138.5741 i 15.00 X 100.00 /f11.1021 X .9750))

PL TO 15. 00 FWr FT W/UNCEPTAINTY e 113.4165 ( 15.00 X 100.00 /(13.2151 X .9750) - 3.0000)

AS$EMBLY AX1AL SRAPE INDEX = .0055 ASSEMBLY AXIAL SMAPE INDEX W/LHC= .0000 NORMAL 11ED ASSEMBLY AXIAL POWER SHAPE:

NccE 1 2 3 4 5 6 7 8 AX1AL POWER .5610 .8314 .9746 1.0672 1.1086 1.1554 1.1621 1.1819 NODE 9 10 11 12 13 14 15 16 AX1AL POWEP 1.1654 1.1648 1.1253 1.1015 1.0347 .9626 .8094 .5922 ASAS Manual Revision o 65 April 19,1994

Figure 13 Sample User Output File Page 13 of 37 ,

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l 1 PROGRAM ASAS VERSIC-N 1. REV DATE 4/12 /94. TODAY'S DATE IS 04/12/98 THE TIME IS 08:19:49 PAGE 13 j A CODE TO CRI. ATE HOT CHANNEL DATA FILES PROM A SIMULATE-3 PIN FILE PIN FILE NAME a / RPG3 /Sp ROP PD / s 30t ee t . g:

RUN TITLE a Fort Calhoun Cycle 15 BOC 10.5 Hours - asetest CASE ID  : 0-10.5-A PDIL CASE A - 1009 POWER. ARO KPo = 10.500 GWD/MT+ EBAR

  • 16.119 GWDiMT. POWER e 100.00%. FLOW = 100.009 N7f'#1' = 15120 STEPS INSERTED. PQ = 2.000. F-DELTA-M e 1.653. INCORE ASI e .0078. PERIPHERA1. AS! . .0023 TOTAL RELAT3VE EACOP.E SIGNAL s .4425 FUEL TYPE TYPE 2 PIN POWERS FOR LIMITING LHGR PLANE 8 FOR ASSEMBLY 10. SERIAL NUMitER OMR013 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 .1.0085 1.0313 1.1565 1.1937 1.2144 1.2297 1.2520 1.2756 1.3227 1.3906 1.4356 1.4678 1.3656 1.4016 2 1 G077 1.1409 1.1528 1.2006 1.2441 1.2366 1.2450 1.2661 1.1272 1 4104 1.4440 1.4615 1.5230 1.3971 3 1.1131 f.1350 ---- - + - 1.2580 1.2739 1,2717 1.2935 1.3669 1.4289 -~~- ---- 1.5090 1.5509 4 1.1376 1.1697 ---- ---- 1.2888 1.3090 1,3114 1.3328 1.4025 1.4596 +--- ---- 1.5470 1.5750 5 1,1503 1,2043 1.2359 1.2795 1.3432 1.3464 1.3765 1.4013 1.4361 1.5131 1.5174 1.5414 1.5124 1.5782 6 1.1609 1.1924 1.2464 1.2939 1.3404 1.4084 1.4250 1.4558 1.4957 3.4933 1.5166 1.5350 1.5425 1.5801 7 1.1796 1.1990 1.2425 1.2942 1.3677 1.4221 ---- - - - 1.5099 1.5119 1.4969 1.5111 1.5349 1.5974 8 1.2116 1.2269 1.2695 1.3194 1.3942 1.4517 - - -

1.5442 1.5418 1.5223 1.5337 1.5561 1.6196 9 1.264) 1.2914 1.3445 1.3902 1.4322 1.4977 1.5128 1.5477 1.5817 .1.5797 1.5997 1.6146 1.6164 1.4537 10 1.3304 1.3817 1.4107 1.4507 1.5117 1.4997 1,5220 1.5493 1.5836 1.6646 1.6643 1.6820 1.7011 1.7079 11 1.3979 1.4245 ----

1.5237 1.5297 1.5149 1.5357 1.6095 1.6701 ---- ---- 1.7377 1.7618 12 1.4492 1.4607 ----

1.5607 1.5595 1.5391 1.5564 1.6338 1.6972 ---- ---- 1,7451 1.7906 11 1.2777 1.5413 1.5420 1.5837 1.6151 1.5849 1.5784 1.5948 1.6511 1.7324 1,7630 1.7608 1.8253 1.65;9 14 1.4432 1.4598 1.6212 1.6479 1.6510 1.6515 1.6673 1.6853 1.7172 1.7683 1.8171 1.8344 1.6758 1.7390 FZ FACTORS FOR ASSEMBLY 10, SERIAL NUMBER OMRC13 l

1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1917 1.1930 1.1914 1.1923 1.1941 1.19$6 1.1967 1,1971 1.1974 1.1973 1.1975 1.1980 1.2012 1.1996 2 1.1923 1.1905 1.1904 1.1916 1.1937 1.1960 1.1970 1.1966 1.1975 1.1976 1.1975 1.1986 1.1986 1.2012 3 1.1296 1.1894 -- - ---- 1.1926 1.1953 1.1969 1.1966 1,1967 1.1965 ---- ---- 1.1990 1,1985 4 1.1897 1.1897 --- --+- 1.1925 1.1950 1.1968 1,19E0 1.1964 1.1961 *--- ---- 1.1985 1.1985 5 1.1908 1.1911 1.1910 1.1917 1.1930 1.1954 1.1957 1.1953 1.1962 1.1964 1.1968 1.1979 1.1994 1.1991 6 1.1916 1.1929 1.1930 1.1916 1.1948 1.1947 1.1938 1.1946 1.1961 1.1970 1.1981 1.1989 1.2001 1.1998 1 1.1924 1.1935 1.1944 1.1951 121948 1.1934 ---- ---- 1.1954 1.1970 1.1984 1.1996 1.1998 1.1999 8 1.1934 1.1940 1.1948 1.1952 1.1952 1.1946 ---+

1.1964 1.1976 1.1986 1.1996 1.1998 1.2002 9 1.1937 1.1945 1,1945 1.1951 1.1959 1.1961 1.1957 1.1962 1.1979 1.1980 1.1986 1.1993 1.2005 1.2000 10 1.1940 1.1944 1.1940 1.1945 1.1955 1.1972 1.1975 1.1973 1.1978 1.1978 1,1988 1,1992 1.2008'1,2000 11 1.1944 1.1944 ----

-- - 1.1958 1.1971 1.1989 1.1982 1.1982 1.1987 ---

+--- 1.2000 1.1993 12 1.1951 1.1952 ---- -- . 1.1966 1.1983 1.1997 1.1991 1.1988 1.1989 ---- -- - 1.2009 1.1997 13 1.1983 1.1959 1.1962 1.1966 1.1980 1.1993 1.1998 1.1993 1.2000 1.2004 1.1998 1.2009 1.1999 1.2019 14 1.1972 1.1986 1.1965 1.1969 1,1979 1.1928 1.1995 1.1999 1.1996 1.1997 1.1991 1.1936 1.2019 1.2003 ASSEMBLY AX1AL PR.ANING FACTOR = 1.1969 (FROM 16 PLANE DATAl l

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ASAS Manual Revision 0 66 April 19.1994

Figure 13 Sample User Output File Page 14 of 37 1 PROGRAM ASAS VER$10N 1. REV DATR 4/12/94. TOLAf*S DATE IS 04/12/94, THE TIME !$ 08:19:49 PAGE 14 A CODE TO CFEATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME s /RPG3/Sp/OFPD/s30 test.p PUN TITLE i Port Calhoun Cycle 15 BOC 10.5 Hours - saatest CAbE ID i B-10.5-A PD11, CASE A - 1004 POWER, ARO XPO e 10.500 GWD/MT. ESAR

  • 16.119 GWD/Mr. POWER = 100.004. FLOW e 100.004 NO7wf = 15120. STEPS INSERTED. FO e 2.000. F-DELTA-H e 1.653. INCORE ASI e .0078, FER1PHERAL ASI e .0023 TOTAL RELAT1VE E'XCORE SIGNAL

. = .4425 FUEL TYPE s TYPE 2 2D PIM POWERS FOR ASSEMlfLY 10, STRI AL NUMBER OMRQ13 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 .8462 .8644 .9708 1.0011 1.0169 1.0286 1.0462 1.0656 1.1046 1.1530 1.1988 1.2251 1.1369 1.1684 2 .8452 .9583 .9684 1.0075 1.0424 1.0339 1.0401 1.0581 1.1083 1.1776 1.2059 1.2193 1.2706 1.1631 3 .9357 .9542 ---- ---- 1.0548 1.0658 1.0(25 1.0810 1.1423 1.1943 -+-- ---- 1.2585 1.2941 4 .9562 .9832 ---- ---- 1.0808 1.0954 1.0958 1.1144 1.1722 1.2204 ---- +--- 1.2908 1.3141 5 .9660 1.0111 1.0377 1.0736 1.1260 1.1263 1.1511 1.1723 1.2006 1.2647 1.2678 1.2867 1.3109 1.3162 6 .9742 .9996 1.0447 1.0840 1.1219 1.1789 1.1917 1.2187 1.2504 1.2475 1.2659 1.2803 1.2853 1.3170 7 .9892 1.0046 1.0403 1.0829 1.1447 1.1916 ---- --~~ 1.2631 1.2631 1.2491 1.2597 1.2793 1.3313 8 1.0152 1.0276 1.0625 1.1039 1.1665 1.2152 ---- ---- 1.2908 1.2874 1.2700 1,2785 1.2974 1.3494 9 1.0591 1.0811 1.1257 1.1633 1.1975 1.2521 1.2652 1.2939 1.3204 1.3186 1.3347 1.3463 1.3465 1.3781 10 1.1142 1.1567 1.1815 1.2145 1.2645 1.2526 1.2710 1.2940 1.3220 1.3898 1.3883 1.4025 1.4166 1.4232 11 1.1704 1.1926 ---- ---- 1,2742 1.2772 1.2636 1.2817 1.3432 1.3933 ---- ---- 1,4481 1.4690 12 1.2126 1.2222 ---- ---- 1.3043 1.3014 1.2828 1.2980 1.3628 1,4156 ---- ---- 1.4531 1.4925 13 1.1497 1.2939 1.2891 1.3235 1.3482 1.3215 1,3155 1.3297 1,3759 1.4431 1.4695 1.4663 1.5212 1.3743 14 1.2056 1,2179 1.3550 1.3767 1.3783 1.3776 1.3900 1.4045 1.4316 1.4740 1.5153 1.5308 1.3968 1.4405 FUEL TYPB . TYPE 2 ALMUSTED 2D PIN POWERS FOR ASSEMPLY 10/ SEPIAL NUMBER OMRO13 (INCLUDES GRID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 .8489 .8681 .9735 1.0048 1.0222 1.0351 1.0538 1.0737 1.1133 1.1621 1.2084 1.2355 1.1495 1.1798 2 .8483 ,9603 .9703 1.0106 1.0414 1.0409 1.0480 1.0658 1.1172 1.1972 1.2155 1.2302 1.2820 1.1760 3 .9370 .9553 ----

1.0589 1.0723 1.0705 1.0888 1.1506 1.2028 ---- ---- 1.2702 1.3055 4 .9576 .9846 ---- ---- 1.0848 1.1019 1.1039 1.1219 1 1805 1.2286 - ---- ---- 1.1022. 1.3258 +

5 .9683 1.0137 1.0403 1.0770 1.1307 1.1333 1,1546 1.1795 1.2088 1.2737 1.2773 1.2974 1.3235 1.3284 6 .9772 1.0037 1.0491 .1.0892 1.1283 1.1855 1.1995 1.2254 1.2590 1.2570 1.2766 1.2921 1.2983 1.3301 7 .9929 1.0092 1.0459 1.0894 1.1513 1.1971 ---- ---- 1.2710 1.2727 1.2600 1.2719 1.2920 1.1446 8 1,0198 1.0327 1.0686 1.1106 1.1735 1.2220 ---- ---- 1.2998 1.2978 1.2814 1.2910 1.3103 1.3632 4 9 1.0642 1.0870 1.1318 1.1702 1.2055 1.2607 1.2734 1.3028 1.3313 1.3297 1.3465 1.3591 1.3606 1.3920 1 10 1.1198 1.1630 1.1875 1.2211 1.2725 1.2624 1.2812 1.3041 1.3329 1.4012 1.4009 1.4158 1.4318 1.4376 al 1,1766 1.1990 ---- - - - 1.2826 1,2876 1.2752 1 2927 1.3548 1.4058 ---+ ---a 1.4627 1.4830 12 1.2198 1.2295 ----

1.3137 1.3127 1.2955 1.3101 1.3752 1.4286 ---- ---- 1.4689 1.5072 13 1.1596 1.3025 1.2979 1.3331 1.3595 .1.3341 1.3286 1.3424 1.3898 1.4582 1.4840 1.4822 1.5365 1.3904 14 1.2148 1.2288 1.3647 1.3871 1,3897 1.3901 1.4034 1.4186 1.4455 1.4885 1.5295 1.5458 1.4131 1.4554 MAXIMUM 2D ONE PIN POWER s 1.5458 AT POW 14 COLIMN 12 MAXIMUM 2D ONE FIN POWER W/UNC = 1.7514 l1.5458 X 1.1000 X 1.0300) .

MAXIMUM CHANNEL POWER = 1.5104 AT ROW 13 COLUMN 11 MAXIMUM 3D ONE PIN POWER = 1.8502 AT ROW 14 COLUMN 12 (INCLUDES GRID DIP FACTOR OF 1,0075)

MAX.IMUM 3D ON8 PIN PCWEP W/UNC = 2.0962 (1.8502 X 1.2000 X 1.0300)

MAXIMUM LHGP = 11.1010 FWIFT (1.8502 X 6.0000)

MAXIM'JM LNGR W/ UNCERTAINTY = 13.2139 FW/FT (2.0962 I 6.0000 X 1.0300 1 1.0200)

FL TO 16.00 KW/F"r W/O UNC

  • 147.8264 ( 16.00 X 100.00 /(11.1010 X .975011 PL TO 16.00 FWiFT W/ UNCERTAINTY , 121.1895 ( 16.00 X 100.00 /t13.2139 X .97501 - 3,00006 ASSEMBLY AX1AL SHAPE INDEX = .0206 ASSEMBLY AXIAL SKAFE JNDEX W/UNCs .0000 NOPMALIZED ASSEMBLY AX1AL POWER SHAFE; NOLE 1 2 3 4 5 6 7 8 AXIAL POWER .5271 .8446 ,9996 1.0960 1.1376 1.1803 1.1822 1,1969 NOCE 9 10 31 12 13 14 15 lb AXI AI, VJWER 1.1729 1.1653 1.1208 1.0911 1.0209 .9445 7870 .5328 ,

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ASAS Manual Revision 0 67 April 19,1994 l l

i I?igiare 13 Sample User Output File Page 15 of 37 '

1 PROGRAM ASAS VRPSIDN 1, PEV DATE 4 /12 /94. TODAY'S DATE IS 04/12/94. THE TIME IS 08:19:49 FAGE 15 A CODE TO CREATI HOT CHANNEL DATA FILES PROM A B1MULATE*1 PIN FILE 6 PIN FILE NAME /RPG1/Sp/OPPD/e30 test.p RUN T171.E t Fort Calhoun Cycle 15 poc 10.5 Hours - esatsst CASE 10 m p-10.5-A PDIL CASE A - 1009 POWER. ARO XPO = 10.500 GWD/Kr. EBAR e 16.119 GWD/MT. POWER e 100.004, F14W

  • 100.004 NOTWT
  • 15120. ETEP8 ' ASSERTED. FQ = 2.000. F-DELTA H = 1.65). INCORE ASI . .0078, PERIPHERAL ASI = 0023 TOTAL PELA71V8 EXCORE SIGNAL e .4425 FUEL TYPE TYPE 2 P1H POWERS FOR LIMITING LH3R PLANE 8 FOR ASSEMBLY 39, SERIAL NUMBER OM5026 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.4752 1.3313 1.6026 1.5001 1.6077 1.6270 1.6156 1.6156 1.6270 1.6077 1.5001 1.6026 1.3313 1.4752 2 1.3120 1,6123 1.4622 1.581) 1.5466 1.6138 1.6072 1.6072 1.6138 1.5466 1.5813 1.4622 1.6123 1,3320 3 1.6041 1.4629 ----

1.6153 1.6558 1.6238 1.6238 1.6558 1.6151 ~+-- ---- 1.4629 1.6041 4 1.5021 1.5827 - -- ---- 1.5040 1,6569 1.6396 1.6396 1.6569 1.5040 ----

1.5827 1.5021

  • 5 1.6102 1.5485 1.6165 1.5045 1.6964 1.6695 1.6592 1.6592 1.6695 1.6964 1.5045 1.4165 1.5485 1.6102 ,

6 1.6297 1 6160 1.6573 1.6579 1.6699 1.6968 1.4987 1.4947 1.6968 1.6699 1.6579 1,6573 1.6160 1.6297 7 1.6181 1.6094 1.6254 1,6407 1.6599 1.4950 ----

1.4950 1.6599 1.6407 1.6254 1.6094 1.6181 8 1.6181 1.6094 1.6254 1.6407 1.6599 1.4950 ----

1.4950 1.6599 1.6407 1.6254 1.6094 1.6181 9 1.6297 1.6160 1.6573 1.6579 1.6699 1.6968 1.4947 1.4947 1.6968 1.6699 1.6579 1.6573 1.6160 1.6297 '

10 1.6102 1.5485 1.6165 1.5045 1.6964 1.6695 1.6592 1.4592 1.6695 1.6964 1.5045 1.6165 1.5485 1.6102 il 1.5021 1,5827 ---- ---- 1.5040 1.6569 1.6396 1.6196 1.6569 1.5040 --- ---* 1.5821 1.5021 12 1.6041 1 4629 -- -

1.6153 1.6558 1.6238 1.6238 1.6558 1.6153 ----

1.4629 1.6041 13 1.3320 1.6123 1 4622 1.5811 1.5466 1.6136 1.6072 1.6072 1.6138 1.5466 1.5813 1.4622 1.6123 1.3320 14 1.4752 1.3313 1.6026 1.5001 1.6077 1.6270 1.6156 1.6156 1.6270 1.6077 1.5001 1.6026 1.3333 1.4752 i

FZ FACTOPS FOR ASSEMBLY 39 EERI AL NUMBER OM3026 i

~

1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1779 1.1722 1.1760 1.1728 1.1783 1,15J3 1.1807 1.1807 1.180) 1.1783 1.1728 1.1760 1.1722 1.1779 2 1.1123 1.1749 1.1728 1.1775 1.1739 1.1794 1.1803 1.1803 1.1794 1.1739 1.1775 1.1728 1.1749 1.1723 3 1.1761 1.1729 ----

3.1791 1.1796 1.1804 1.1804 1.1796 1.1791 ----

- - - - - 1.1729 1.1761 6 4 1.1729 1.1776 --- ---- 1,1148 1.1791 1.1802 1.1802 1.1791 1.1748 ----

1.1776 1.1729 #

5 1.1785 1.1741 1.1791 1.1748 1.1784 1.1793 1.1790 1.1790 1.1793 1.1784 1.1748 1,1791 1,1741 1.1785 6 1.1805 1.1795 1.1797 1,1792 1.1793 1.1785 1.1743 1.1743 1.1785 1.1793 1.1792 1.1797 1.1795 1.1805 7 1.1808 1,1805 1.1805 1.1803 1.1791 1.1741 ---- --- 1.1741 1.1791 1,1803 1.1805 1.1805 1.1808 8 1.1808 1.1805 1.1805 1.1801 1.1791 1.1743 ----

1.1743 1.1791 1.1803 1.1805 1.1805 1.1808 9 1.1805 1 1795 1.1797 1.1792 1.1793 1.17P5 1.1743 1.1743 1.1185 1.1793 1.1792 1.1797 1.1795 1.1805 l 10 1.1785 1.1741 1.1791 1.1748 1.1784 1.1793 1.1790 1.1790 1.1791 1.1784 .1148 1.1791 1.1741 1 1785

=

11 1.1129 1.1776 ----

1.1748 1.1791. 1.1802 1.1802 1.1791 1.1748 ----

1.1776 1.1729 12 1.1761 1.1729 ---+ +--- 1.1791 1.1796 1.1804 1.1804 1,1796 1.1791 - - - - ---- 1.1729 1.1761 13 1.1723 1.1749 1 1728 1.1775 1.1739 1.1794 1.1803 1.1803 1.1794 1.1739 1.1775 1.1728 1.1749 1.1723 14 1.1779 1.1722 1.1760 1.1728 1 1183 1.1803 1 1807 1.1807 1.1603 1.1781 1.1728 1.1760 1.1722 1.1779 ASSEMBLY AX1AL PEAKING FACTOR

  • 1.1776 t FROM 16 PLANE DATA)

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l ASAS Manual Revision 0 68 April 19,1994

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Figure 13 l Sample User Output File Page 16 of 37 1 PROGRAM AEAS VERSIGH 1 REV DATE 4/12/94 TODAY'S DATE 15 04/12/94. THE TIME 15 08:19 49 PAOE 16 A CODE TO CREATE HOT CHANNEL DATA FILF.S FROM A SIMULATE-3 PIN FILE PIN FILE NAM i / PPG 3/Sp/OPPD/s30 test.p DUN TITLE i Port Calhoun Cycle 15 BOC 10.5 Hours - asatest CASE 1D B-10.5 A PDIL CASE A - 2004 POWEP. ARO XPO a 10.500 GWD/wf. EBAR = 16.119 GWD/MT. FOWER e 100.004. F1/W e 100.004 N(rrwr . 15120. STEPS INSEPTED. FQ a 2.000. F-DELTA-M = 1.653, INCORE ASI e .0078 PERIPHERAL ASI a .0023 TOTAL kELATIVE EXCORE SIGNAL * .4425 l FUEL TYFE a TYPE 2 2D PIN POWERS FOP ASSEMBLY 39 SERIAL NUMBER CM5026 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.2524 1,1357 1.3624 1.2791 1.3644 1.3784 1.3684 1,3684 1.3784 1.3444 1.2791 1.3628 1,1357 1.2524 2 1.3362 1.3723 1.2467 1.3429 1.3175 1.3684 1.3617 1.3617 1,3684 1.3175 1.3429 1.2467 1.3723 1.1362 3 1.3640 1.2473 ---- --- 1.3700 1.4037 1.3756 1.3756 1.4037 1.3700 ---- - -- 1.2473 1.3640 4 1.2807 1.3440 - -- -~~. 1.2802 1.4053 1.3892 1.3892 1.4053 1.2802 ---- ---- 1.3440 1.2807

  • 5 1.3664 1.3189 1.3709 1.2806 1.4396 1.4151 1.407) 1.4073 1.4157 1.4396 1.2806 1.3709 1.3189 1.3664

( 1.3805 1.3700 1.4049 1.4060 1.4160 1.4398 1.2729 1.2729 1.4398 1.4160 -1.4060 1.4049 1.3700 1.3805 7 1.3703 1.3633 1.3769 1.3901 1.4078 1.2731 ---- ---- 1.2731 1.4078 1.3901 1.3169 1.3633 1.3703 8 1.3703 1.3633 1.3769 1.3901 1.4378 1.2731 --*- --~~ 1.2731 1.4078 1.3901 1.3769 1,3633 1.3703 9 1.3805 1.3700 1.4049 1.4060 1.4160 1.4398 1.2729 1.2729 1.4398 1.4160 1.4060 1.4049 1.3700 1.3805 10 1.3664 1.3189 1.3709 1.2806 1.4396 1.4157 1.4073 1.4073 1.4157 1.4396 1.2806 1.3709 1.3189 1.3664 11 1.2807 1.3440 ---- ---- 1.2802 1.4053 1.3892 1.3892 1.4053 1.2802 ----

1.3440 1.2807 12 1.3640 1.2473 ---- ---- 1.3700 1.4037 1.3756 1.3756 1.4037 1.3700 - -- ---- 1.2413 1.3640 13 1.1362 1.3723 1.2467 1.3429 1.3175 1.3684 1.3617 1.3617 1.3684 1.3175. 1.3429 1.2467 1.3723 1.1362 14 1.2524 1.1357 1.3628 1.2791 1.3644 1.3784 1.3684 1.3684 1.3784 1.3644 1.2791 1.3628 1.1157 1.2524 ,

r FUEL TYPE i TYPE 2 ADJUSTED 2D PIN POWERS FOR ASSEMBLY 39. SERIAL NUMBER OMS 026 (INCLUDES GRID D1P FACTOR OF 1,0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.2621 1.1389 1.3710 1.2833 1.3754 1.3919 1.3822 1.1822 1.3919 1.3754 1.2833 1.3710 1.1389 1.2621 2 1.1395 1.3793 1.2509 1.3528 1.3232 1.3806 1.3750 1.3750 1.3806 1.3232 1.3528 1,2509 1.3793 1.1395 3 1.3724 1.2515 ---- ---- 1.3819 1.4165 1.3892 1.3892 1.4165 1.3819 ---- ---- 1.2515 1.3724 4 1.2831 1.3540 ---- --- 1.2867 1.4175 1,4027 1.4027 1.4175 1.2867 ---- ---- 1.3540 1.2851 5 1.3776 1.3247 1.3827 1,2872 1.4513 1,4283 1.4195 1.4195 1.4283 1.4513 1.2872 1.3829 1.3247 1.3776 6 1,3942 1.3825 1.4179 1.4184 1.4287 1.4517 1.2786 1.2788 1.4517 1.4287 1.4184 1.4179 1.3825 1.3942 7 1.3843 1,3768 1.3906 1.4037 1.4201 1.2790 -+-- ---- 1.2790 1.4201 1.4037 1.3906 1.3768 1.3843 8 1.3843 1.3768 1.3906 1.4037 1.4201 1.2790 ---- ---- 1.2790 1.4201 1.4037 1.3906 1.3168 1,3843 -

9 1,3942 1.3525 1 4179 1.4184 1.4287 1.4517 1.2788 1.2788 1.4517 1.4287 1.4384 1.4179 1.3825 1.3942 10 1.3776 1.3247 1.3829 1.3872 1.4513 1 4283 1.4195 1.4195 1.4283 1.4513 1.2872 1.3829 1.3247 1,3776 11 1.2851 1.3540 ---- -- - 1.2867 1.4175 1.4027 1.4027 1.4175 1.2867 ---- ~~- 1.3540 1.2851 12 1.3724 1.2515 ---- 4--- 1.3819 1.4165 1.3892 1.3892 1.4165 1,3819 ---- ---- 1.2515 1.3724 13 1.1395 1.3793 1.2509 1.3528 1.1232 1.3806 1.3750 1.3750 1.3806 1.3232 1.3528 1.2509 1.3793 1.1395 '

14' 2.2611 1.1389 1.3710 1.2833 1.3754 1.3919 1.3822 1.3822 1.3919 1.3754 1.2833 1.3710 1.1389 1.2621 MAX 1 MUM 2D OM PIN POWER = 1.4517 AT ROW 6 COLUMN 6 MAKIMUM 2D ONE FIN POWER W/UNC = 1.6447 (1.4517 K 1.1000 X 1.0300)

MAX 1MtM CHANNEL POWER

  • 1.4400 At ROW 5 COLUMN 5 MAXIMUM 3D ONE PIN POWER
  • 1.7095 AT ROW 6 COLtHN 6 (INCLLT/ES CRID DIP FACTOR OF 1.0075)

MAX 1 MUM 30 ONE PIN POWER W/UNC e 1.9369 11.7095 1 1.1000 X 1.0300)

MAX 1 MUM LNGR = 10,2573 Fw FT (1.7095 K 6.0000)

MAXIMUM LMGR W/ UNCERTAINTY = 12.2096 itwrFT (1.9369 K 6.0000 X 1.0300 x 1.02001 PL TO 16.00 EW/FT W/O tmc a 159.9862 ( 16.00 2 100.00 /(10.2573 K .9750))

PL TO 16400 FW/FT W/ UNCERTAINTY

  • 131.4050 ( 16.00 x 100.00 /(12.2096 X .97501 - 3.0000)

ASSEMBLY AX1AL EhAPE INDEX e .0046 '

ASSEMBLY A11AL SMAFE INDEX WitHC= .0000 HOkMAL17.ED ASSEMBLY A11 AL PCWER SHAPE NOLE . 1 2 3 4 5 6 7 8 AX!AL POWEN .5446 .8278 .9676 1.0551 1.0950 1.1429 1.1524 1.1776 NOr.E 9 10 11 12 13 14 15 16 AXIAL POWER 1.1629 1.1660 1.1296 1.1116 1.0507 .9860 .8337 5964 i L

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ASAS Manual Revision 0 69 April 19,1994 1

_ __ __. _ _ . _ _ _ __ _ _ . _ . . . _ _ . _ _ _ . . _ . . _ _ _ __. _ _. _ . _ _ _ _ _ _ _ ~~

- .- . - -- ~, . . . - . . . . - -. . . . ..

Figure 13 Sample User Output File Page 17 of 37 1 PHOGFAM ASAS VERSION 1. ROV DATE 4 /12 /94. TODAY'S DATE 18 04/12/94 THE TIME 15 08519:49 PAGE 17 A CODE TO CRfATE HOT CHAhNEL DATA FILES FROM A $1MULATS-3 FIN P1LE PIN FILE NAMP. t / PPG 3/Sp/OPPD/s30 test.p RUN TITLE Fort callwun Cyca,15 BOC 10.5 Houn s - amatest CASE ID i S 10. % A PD1L CASE A - 1009 MNER, Ako XPO e 10.500 GWD/Kr. EEAR e 16.119 GWDINT. PCWER = 100,00%. FIDW e 100.006 NCrrwt = 15120. STEPS INSEP'f ED. FQ = 2.000 P-DELTA-H e 1.653, INCORE ASI e .0078 PER1PHERAL AS1 = .0023 TOTAL RELATIVE EXCORE SI.GNAL e .4425 FUE1. TYPE t TYPK2 PIN POWERS FOR LIMITING LHCR PLANE 8 POR ASSEMBLY 35. SERIAL NUMBKP OM3020 1 . 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.5076 1.3957 1.7272 1.1779 1.7531 1.7468 1.7373 1.7451 1.7736 1.1996 1.8459 1.8164 1.4896 1.6349 2 1,1836 1.704? 1.5685 1.7269 1.6865 1.7515 '1.7488 1.7563 1.7783 1.7325 1.7945 1.6518 1.8199 1.4997 3 1.7023 1.5592 ---- ---- 1.7924 1.8223 1,7871 1.7945 1.8504 1.8419 ---- ---- 1.6674 1.8459 4 1.7443 1.7086 ---- ---- 1.8375 1.8643 1.8255 1.8330 1.8942 1.8897 ---- ---- 1.8290 1.8938 5 1.7132 1.6614 1.7756 1.8288 1.9302 1.8646 1.8967 1.9047 1.8954 1,9867 1.9070 1.8767 1 7815 1.0625

  • 6 1.7002 1.7178 1.7965 1.8464 1.8551. 1.7939 1.8853 1.8938 1,8256 1.9107 1.9267 1.8999 1.8424 1.8495 7 1.6442 1,7611 1.77.28 1.79'? 1 #162 1.8143 - - - ---- 1.9068 1.9330 1.0165 1.8540 1.8307 18UD i '

8 1.6842 1.7011 1.1528 1.7979 1.8762 1.8741 ---- --- 1.9c68 1.9330 1.8765 1,8540 1.8307 1.8318 9 1.7002 1.7178 1.7965 1.8464 1.855' 3.7939 1.8853 1.8938 1.8256 1.9107 1.9267 1.8999 1.8424 1.8495 10 1.7132 1.6614 1.1756 1 8288 1.9302 1.8646 1.8967 1.9047 1.8954 1.9867 1.9070 1.8167 1.7815 1.8625 11 1.7443 1.7086 ---- ---- 1.8175 1.8643 1.8255 1.8330 1.8942 1.8897 ---- ---- 1.8290 1.8938 12 1.7023 1.5592 - - ---

1.7924 1.8223 1.7871 1.7945 1.8504 1.8419 ---- ---- 1.6674 1,8459 13 1.1836 1.1047 1.5685 1.7269 1.6865 1.7535 1.7488 1.7561 1.7783 1.7325 1.7945 1,6518 1.8399 1.4997 14 1,5076 1.3957 1.7272 1,7779 1.7533 1.7468 1.7313 1.1451 1.7736 1.7996 1.8459 1.8144 1.4896 1.6349 FZ FACTORS FOR ASSEMBLY 35. SER1AL NUMBER OMS 020 1 2 3 4 5 6 7 8 9 10 11 12 13 14 ,

1 1.2024 3.1973 1.2015 1.2024 1.2023 1.2028 1.2023 1.2022 1.2023 1.2011 1.2004 1.1988 1,1918 1.1984

[

2 1.1975 1.2003 1.1981 1.2022 1.1980 1.2020 1.2025 1.2023 1.2012 1.1966 1.2002 1.1954 1.1970 1.1935 3 1,2021 1.1985 - - - ---- 1.2D33 1,2024 1.2027 1.2025 1.2016 1,2019 --+- ---- 1.1953 1.1983

. e 1.20)4 1.2031 ---- --- 1.2040 1.2C30 1.2010 1.2028 1.2022 1.2027 ---- ---- 1.2000 1.1998 1

3 1.2038 1.1993 1.2042 1.2045 1.2034 1.2023 1.2028 1.2025 1.2015 1.2020 1.2026 1.2018 1.1962 1.2003 6 1.2046 1.2017 1.2037 1.2019 1.2027 1.1991 1.2034 1.2032 1.1983 1.2014 1.2020 1.2012 1.2006 1.2012 7 1.2043 1.2044 1.204) 1.2042 1.2035 1.2037 - - - ---- 1.2030 1.2022 1.2023 1.2019 1.2014 1.2009 8 1.204) 1.2044 1.204) 1.2042 1.2035 1.2017 ---- -- - 1.2030 1.2022 1.2023 1.2019 1,2014 1.2009 9 1.2046 1.2037 1.2037 1.2039 1.2027 1.1991 1.2034 1.2032 1.1983 1.2014 1.2020 1.2012 1.2006 1.2012 10 1.2038 1.1993 1.2042 1. 2045 1.2034 1.2023 1.2028 1.2025 1.2015 1.2020 1.2026 1,2018 1,1962 1.2003 Il 1.2034 1.2031 -+-- +--- 1.2040 1.2030 1.2030 1.2028 1.2022 1.2027 ---- ---- 1.2000 1.1998 12 1.2021 1.1985 ---- ---- 1.2033 1.2024 1.2027 1.2025 1.2016 1.2019 ---- ---- 1.1953 1.1983 13 1,1975 1.2003 1.1981 1.2022 1.1980 1.2020 1.2025 1.2023 1.2012 1,1966 1.2002 1.1954 1.1970 1.1935 14 1.2024 1.1973 1.2015 1.2024 1.2023 1,2028 1.2023 1.2022 1.2023 1.2011 1.2004 1.1988 1.1938 1.1984 ASSEMBLY AXIAL PEAKING FACTOR . 1.2014 (PROM 16 PLANE DATA) l l

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i ASAS Manual Revision 0 70 April 19,1994 i

Figure 13 Sample User Output File Page 18 of 37 1 'PROGPAM ASAS VERSION 1, P.EV DATE 4/12/94. TODAY'S DATE IS 04/12/94 THE TIME IS CBs19:49 PAGE 18 A CODE TO CPI. ATE HOT CHANNEL D4TA FILES FROM A $7MULATE-3 PIN FILE PIN FILE NAME / PPG 3/Sp/OPPD/s30 test.p RtM TITLE Fort Calhoun cycle 15 BOC 10.5 Hours - asatest t CASE ID B-10.5-A PDIL CA3E A - 100% POWER. ARO XPO = 10.500 CWD/M. EBAR e 16.119 CWD/M. POWER = 100,00t. FLOW = 100.004 Naqwr = 15120. STEPS INSERTED. FO = 2.000 F-DELh -H = 1.65), INCOkE AS! = .0078. PER1PHERAL ASI = .0023 TOTAL RELATIVI EXCORS SIGNAL = .4425 FUEL TYPE r * 'E2 2D PIN POWEW CR ASSEMBLY 35. SERIAL NUMBER OM3020 1 2 3 4 5 6 7 8 9 10 11 12 13 14 I 1.2538 1.1657 1.4376 1.4787 1.4582 1.4522 1.4450 1.4516 1.4752 1.4982 1.5377 1.5152 1.2477 1.3642.

2 1.1555 1.4202 1.3091 1.4364 1.4078 1.4572 1.4544 1.4608 1.4804 1.4479 1,4951 1.3818 1.5101 1.3566 - i 3 1.4162 1.3010 ---- +--- 1.4896 1.5155 1.4859 1.4923 1.540s 1.5324 ---- ---- 1.3950 1.5404 4 3.4495 1.4202 ---- -~~- 1.5261 1.5497 1 8176 s.5240 1.5756 1.5712 - - - - - ---- 1.5241 1.5784 5 1.4232 1.3852 1.4745 1.5181 1.6040 1.5508 1.5770 1.5840 1.5775 1.6529 -1.5857 1.5616 1.4892 1.5517 3 6 1.4114 2.4272 1.4945 1.5337 1.5424 1.4961 1.5664 1.5740 1.5235 1.5905 1.6030 1.5817 1.5345 1.5397 7 1.3985 1.4174 1.4554 1.4930 1.5590 1.5570 ---- - -- 1.5850 1.6079 1.5608 1.5426 1.5238 1.5253 8 1.3985 1.4174 1.4554 1.4930 1.5590 1.5570 ---- ---- 1.5850 1.6079 1.5608 1.5426 1.5338 1.5253 9 1.4114 1.4272 1.4925 1.5337- 1.5424 1.4961 1.5666 1.5740 1.5235 1.5905 1,6030 1.5817 1.5345 1.5397 -

10 1.4232 1.3852 1.4745 1.5183 1.6040 1.5504 1,5770 1.5840 1.5775 1.f.529 1.5657 1.5616 1.4892 1.5517 11 1.4495 1.4202 ---- ---- 1.5261 1.5497 1.5174 1.5240 1.5756 1.5712 ---- ---- 1.5241 1.5784 12 1.4162 1.3010 ---- ---- 1.6896 1.5355 1.4859 1.4923 1.5400 1.5324 ---- ---- 1.3950 1.5404 13 1.1555 1.4302 1.3091 1.4364 1.4078 1.4572 1.4544 1.4608 1.4804 1.4479 1.4951 1.3818 1,5203 1.2566 14 1.2538 1.1657 1.4316 1.4787 1.4582 1.4522 1.4450 1.4516 1.4752 1.4982 1.5377 1.5152 1.2477 1.3642 FVEL TYPE : TYPE 2 AELJUSTED 2D PIN POWERS FOR ASSEM1;LY 35, SERI AL NUMBER OM3020 IINCLUDES GRID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.2642 1.1704 1.4484 1.4909 1.4702 1.4648 1.4569 1.4634 1.4873 1.5091 1.5479 1.5232 1.2491 1.3710 2 1.1603 1,4295 1.3153 1,4481 1.4143 1.4688 1.4665 1.4728 1.4912 1.4529 1.5048 1.3951- 1.5261 1.2576 3 1.4275 1.3075 ---- ---- 1.5031 1.5181 1.4987 1,5049 1.5517 1.5446 ---- ---- 1.3982 1.5480 4 1.4628 1.4338 ---- ---- 1.5409 1.5634 1.5308 1.5371 1.5885 1.5647 ---- ---- 1.5337 1.5881 5 1.4367 1.3932 1.4890 1.5336 1,6186 1.5636 1.5905 1.5972 1.5894 1.6660 . 1.5991 1.5737 1.4939 1.5618 6 1.4258 3.4405 1.5065 1.5483 1.5557 1.5041 1.5810 1.5881 1.5309 1.6023 1.6157 1.5933 1.5450 1.5510 7 1.4124 1.4316 1.4699 1.5077 1.5734 1.5717 ---- ---- 1.5990 1.6209 1.5736 1.5547 1.5352 1.5361 8 1.4124 1.4316 1.4699 1.5077 1.5734 1.5717 ---- --- 1.5990 1.6209 1.5736 1.5547 1.5352 1.5361 9 1.4258 1.4405 145065 1.5483 1.5557 1.5043 1.5810 1.5881 1.5309 1.6023 1.6157 1.5933 1.5450 1.5510 10 1.4361 1.3932 1.4890 1.5336 1.6186 1.5636 1.5905 1.5972 1.5894 1.6660 1.5991 1,5737 1.4939 1.5618 11 1.4628 1.4328 - - - ---- 1.5409 1.5634 1.5308 1.5371 1.5885 1.5847 ---- ---- 1.5337 1.5881 12 1.4275 1.3075 ---- --- 1.5031 1.5281 1.4987 1.5049 1.5517 1.5446 ---- ---- 1.3982t 1.5480 13 1.1603 1.4295 1.3153 1.4481 1.4143 1.4688 1.4665 1.4728 1.4912 1.4529 1.5048 1.3851 1.5261 1.2576 14 1.2642 1.1704 1.4484 1.4909 1.4702 1.4648 1.4569 1.4634 1,4873 1.5091 1.5479 1.5232 .1,2491 1.3710 MAXIM'.M 2D ONE PIN POWEH = 1.6660 AT ROW 5 COLUMN 10 MAXIMUM 2D ONE FIN POWER W/UNC = 1.8876 (1.6660 X 1.1000 X 1.0300)

MAXIMON CHANNEL POWER a 1.6208 AT ROW 5 COLUMN 10 MAXIMUM 3D ONE PIN BOWER = 2.0016 AT ROW 5 COLUMN 10 (INCLUDE 8 GRID DIP FACTOR OF 1.0075n MAXIMUM 3D ONE FIN POWER W/UNC = 2.2679 (2.0016 X 1.1000 X 1.03001 MAXIMUM LHGR = 12.0099 FW/FT (2.0016 X 6.00001 MAXIM'JM t. HOR W/ UNCERTAINTY = 14.2957 KW/PT (2.2679 X 6.0000 X 1.0300 X 1.0200)

PL TO 16.00 FW/FT W!O UNC = 136.6398 t 16.00 X 100.00 /412.0099 X .97501)

PL TO 16.00 KW/FT W/ UNCERTAINTY = 111.7916 1 16.00 X 100.00 /(14.2957 I .97506 - 3.0000)

ASSEMBLY AXIAL SHAfE INDEX = .0239

  • ASSEMBLY AX1AL SHAPE INDEX W/UNCs .0000 NORMAL 1tED ASSEMBLY AXIAL POWER SHAPE:

NOCE 1 2 3 4 5 6 7 8 AXIAL FOWER .5314 8453 1.0015 1.0997 1.1409 1.1850 1.1856' 1.2014 NODE 9 10 11 12 13 14 15 16 '

AXIAL POWER 1.1753 1.1680 1.1203 1.0886 1.0140 .9355 .7762 .5312 I

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l ASAS Manual Revision 0 71 April 19,1994 3

Figure 13 Sample User Output File Page 19 of 37 1 PROGRAM ASA8 VERS!CN 1, PEV DATE 4/12/94. TODAY'S DATE 22 04/12/94 THE TIME IS 08:19:49 PAGE 19 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A SIMULATE.3 FIN FILE PIN FILE NAME : /RPG3/Sp/OPPD/s30 test.p RUN TITLE  : Fort Calhoun Cycle 15 BOC 10.5 Hours - asatest CASE 1D s 9-10.5-A PDIL CASE A - 100% POWER, ARO

.X PO e 10.500 GWD/MT, EnAR = 16.119 CWD/MP, POWER = 100.00%. F1hW

  • 100.006 l Ncr!wr = 15120. BTEPS INSERTED. FQ = 2.000; F-DELTA-H e 1.653. INCORE ASI = .0078. PERIPHERAL ASI = .0023  !

TOTAL RELATIVE EXCORE SIGNAL = .4425 l

FUEL TYPE : TYPE 2 PIN POWERS FOR LIMITING LHGR PLANE 8 FOR ASSEMBLY 19. SERIAL NUMBER OMR021 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.5404 1.5144 1.6273 1.6132 1.5988 1.5765 1.5768 1.5768 1.5765 1.5988 1.6132 1.6273 1.5144 1.5404 l 2 1.5486 1.6703 1.6235 1.6292 1.6371 1.5648 1.5563 1.5563 1.5848 1.6171 1.6292 1.6235 1.6703 1.5486 3 1.6875 1.6464 ---- ---- 1.6365 1.6116 1.5680 1.5680 1.6116 1,6365 ---- ---- 1.6464 1.6875 4 1.6896 1.6688 ---- ---- 1.6409 1,6115 1.5892 1.5892 1.6315 1.6409 ---- ---- 1.6688 1.6896 5 1.6871 1.6897 1.6656 1.6535 1.6913 1.6454 1.6367 1.6367 1.6454 1.6913 1.6535 1.6656 1.6897 1.6873 6 1.6731 1.6452 1.6494 1.6533 1.6547 1.6948 1.6495 1.6495 1,6948 1.6547 1.6531 1.6496 1.6452 1.6733 7 1.6794 1.6211 1.6103 1.6156 1.6511 1.6547 ----

1.6547 1.6511 1.6156 1.6103 1.6211 1.6794 0 1.6841 1.62C9 1.6081 1.6128 1.6518 1.6594 ---- ---- 1.6594 1.6518 1.6128 1.6081 1.6209 1.6841 9 1.6907 1.6587 1.6618 1.6657 1.6679 1.7124 1.6743 1.6743 1,7124 .1.6619 1.6657 1.6618 1.6587 1.6907

  • 10 1.7227 1.7222 1.6961 1.6835 1.7215 1.6740 1.6741 1.6741 1.6760 1.7215 1.6835 1.6961 1.7222 1.7227 11 1.7451 1.7215 ---- ++-- 1.6872 1.6768 1.6351 1.6357 1.6768 1.6872 ---- ---- 1.7215 1.7451 12 1.7664 1.7205 ----

1.6994 1.6706 1.6253 1.6253 1.6706 1.6994 - --

1.7205 1.7664 13 1.6414 1.7711 1.7176 1.7182 1.7201 1.6587 1.6222 1.6222 1.6587 1.7201 1.7182 1.7176 1.7711 1.6414 14 1.6649 1.6348 1.7556 1.7322 1.7076 1.6706 1.4505 1.6505 1.6706 1.7076 1.7122 1.7556 1.6348 1.6649 L

FZ FACTORS FOR ASSEHaLY 19 SERI AL N'JMBER OMR021 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1749 1.1758 1.1741 1.1750 1.1757 1.1765 1.1777 1.1777 1.1765 1.1757 1.1750 1.1743 1.1758 1.1749 2 1.1766 1.1752 1.1751 1.1757 1.1770 1.1789 1.1795 1.1795 1.1789 1.1770 1.1757 1.1751 1.1752 1.1766 3 1.1755 1.1756 ---- ---- 1.1774 1.1793 1.1803 1.1803 1.1791 1.1774 ----

1.1756 1.1755 4 1.1766 1.1766 -- -

1.1776 1.1795 1.1804 1.1804 1.1795 1.1776 ---- ----.1.1766 1.1766 5 1.1775 1.1781 1,1780 1.1778 1.1786 1.1796 1.1794 1.1794 1.1796 1.1786 1.1778 1,1780 1.1781 1.1775 6 1.1784 1.1802 1.2001 1.1799 1.1797 1.1784 1.1774 1.1774 1.1784 1.1797 1.1799 1.1801 1.1802 1.1784 7 1.1795 1.1806 1.1810 1.1807 1.1795 1.1773 ---- ---- 1.1773 1.1795 1.1807 1.1810 1.1806 1.1795 8 1.1796 1.1802 1.1805 1.1801 1.1794 1.1774 ---- ---- 1.1774 1.1794 1.1801 1.1805 1.1802 .1.1796 9 1.1783 1,1800 1.1797 1.1798 1.1794 1.1782 1.1777 1.1777 1.1782 1.1794 1.1798 1.1797 1.1800 1.1783 10 1.1778 1.1782 1.1780 1.1781 1,1784 1.1795 1.1797 1.1797 1.1795 1.1784 1.1781 1.1780 1.1782 1.1778 11 1.1771 1.1769 ----

1.1779 1.1796 1.1802 1.1802 1.1796 1.1779 ----

1.1769 1.1771 12 1.1762 1.1765 ----

- - - - 1.1775 1.1792 1.1801 1.1801 1.1792 1.1775 - --

1.1765 1.1762 13 1.1774 1.176D 1.1760 1.1762 1.1772 1.1789 1.1789 1.1789 1.1789 1.1772 1.1762 1.1760^ 1,1760 1.1774 14 1.1760 1.1767 1.1751 1.1755 1.1739 1.1760 1.1767 1.1767 1.1760 1.1759 1.1755 1.1751 1.1767 1.1760 ASSEMBLY ARIAL PEAKING FACTOR e 1.1780 (FROM 16 PLANE DATA) b ASAS Manual Revision 0 72 April 19,1994

Figure 13 Sample User Output File Page 20 of 37 1 PROGRAM ASAS VERSION 1. REV DATE 4/12/94. TODAY'S DATE IS 04/12/94, THE TIM 8 38 08:19:49 PAGE 20 A CODE 'N) CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME s /RPG3/Sp/OPPD/a30 test.p RUN TITLE Fort Calhoun Cycle 15 BOC 10.5 Hours - asetest CASE ID s B-10.5-A PD3L CASE A - 1004 POWER, ARO XPO e 10.500 GWD/MT. EBAR = '16.119 GWD/MT. POWER = 100.004. FLOW = 100.004 Nt71WP = 15120. FTEPS INSERTED, FQ = 2.000, F-DELTA-H e 1.653 INCORE AS3 e .0078 PERIPHERAL ASI = .0023 TOTAL RELATIVE EXCORE SIGNAL * ,4425 FUEL TYPE t TYPE 2 2D PIN POWERS FOR ASSEMBLY 19, SERIAL NUMBER OMR021 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3111 1.2879 1.2858 1.3730 1.3599 1.3400 1.3389 1.3389 1.3400 1.3599 1.3730 1.3858 1.2879 1.3111 2 1.3162 1.4212 1.3816 1.3857 1.3909 1.3443 1.3195 1.3195 1.3443 1.3909 1.3857 1.3816 1.4212 1.3162 3 1.4356 1.4005 ---- ---- 1.3899 1.3666 1.3285 1.3285 1.3664 1.3899 ---- ---- 1.4005 1.4356 4 1.4361 1.4183 ---- ---- 1.3935 1.3832 1.3463 1.3463 1.3832 1.3935 ---- ---- 1.4183 1.4361 5 1.4329 1.4343 1.4139 1.4038 1.4350 1.3949 1.3877 1.3877 1.3949 1.4350 1.4038 1.4139 1.4343 1.4329 6 1.4200 1.3940 1.3979 1.4012 1.4026 1.4382 1.4010 1.4010 1.4382 1.4026 1.4012 1.3979 1.3940 1.4200 7 1.4239 1.3731 1.3635 1.1683 1.3999 1.4055 ---- ---- 1.4055 1.3999 1.3683 1.3635 1.3731 1.4239 8 1.4277 1.3735 1.3623 1.3647 1.4006 1.4094 ----

1.4094 1.4006 1.3667 1.3623 1.3735 7.4277 9 1.4349 1.4057 1.4086 1.4119 1.4142 1.4535 1.4217 1.4217 1.4535 1.4142 1.4119 1.4086 1.4057 't.4349 10 1.4627 1,4617 1.4399 1.4290 1.4609 1.4210 1.4191 1.4191 1.4210 1.4609 1.4290 1.4399 1.4617 1.4627 11 1.4826 1.4627 ---- ---- 1.4324 1.4214 1.1860 1.3860 '1.4214 1.4324 ----

1.4627 1.4826-12 - 1,5018 1,4625 ----

1.4432 1.4167 1.3772 1.3773 1.4167 1.4432 ---- ---- 1.4625 1.5018 13 1.3941 1.5060 1.4605 1.4608 1.4611 1.4070 1.3760 1.3760 1.4070 1.4611 1.4608 1.4605 1.5060 1.3941 14 1.4157 1.3893 1.4940 1.4735 1.4521 1.4205 1.4027 1.4027 1.4205 1.4521 1.4735 1.4940 1.3893 1.4157 FUEL TYPE r TYPE 2 AIVUSTED 2D PIN POWERS FOS ASSEMBLY 19, SERIAL NUMBER OMR031 (INCLUDES GRID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3175 1.2952 1.3918 1.3798 1.3674 1.3484 1.3487 1.3487 1.3484 1.3674 1.3798 1.3918 3.2952 1.3175 2 1.3245 1.4285 1.3885 1.3934 1.4002 1.3555 1.3311 1.3311 1.3555 1.4002 1.3934 1.3885 1.4285 1.3245 3 1.4433 1.4082 ---- ---- 1.3996 1,3784 1.3411 1.3411 1.3784 1.3996 ---- ---- '1.4082 1.4433 4 1.4451 1.4273 ----

1.4035 1.3954 1.3592 1.3592 1.3954 1.4035 ----

1.4273 1.4451 5 1.4431 1.4452 1.4246 1.4142 1.4466 1.4073 1.3998 1,3998 1.4073 1.4466 1.4142 1.4246 -1.4452 1.4431 6 1.4311 1.4071 1.4109 1.4141 1.4153 1.4495 1.4108 1.4108 1.4495 1.4153 1.4141 1.4109 1.4071 1,4311 7 1.4364 1.3865 1.3773 1.3818 1.4122 1.4152 - --

1.4152 1.4122 1.3818 1.3773 1.3865 1.4364 8 1.4404 1.3843 1.3754 1.3794 1.4128 1.4192 ----

1.4192 1.4128 1.3794 1.3754 1.3863 1.4404 9 1.4461 1.4387 1.4213 1.4247 1.4265 1.4646 1.4321 1.4321 1.4646 1.4265 1.4247 1.4213 1.4187 1.4461 10 1.4734 1,4730 1.4507 1.4399 1.4724 1.4335 1.4319 1.4319 1.4335 1.4724 1.4399 1.4507 1.4730 1.4734 11 1,4925 1.4724 ---- ---- 1.4431 1.4341 1.3990 1.3990 1,4341 1,4431 ---- ---- 1.4724 1.4925 12 1.5108 1.4716 ---- ---- 1.4535 1.4288 1.3901 1.3901 1.4288 1.4535 ---- ---- 1.4716 1.5108 13 1.4039 1.5148 1.4690 1.4695 1.4711 1.4186 1.3874 1.3874 1.4186 1.4711 1.4695 1.4690 1.5148 1.4039 14 1.4240 1.3983 1.5015 1.4815 1.4605 1.4288 1.4117 1.4117 1.4288 1.4605 1.4815 1.5015 1.3983 1.4240 MAXIMUM 2D ONE PIN POWER = 1 $144 AT ROW 13 COLUMN 2 MAXIMUM 2D ONE PIN POWER W/UNC = 1.7162 (1.5148 X 1.1000 X 1.0300)

MAXIMUM CHANNEL POWER e 1.4868 AT ROW 11 COLtNN 13 l MAXIMUM 3D ONE PIN POWER = 1.7844 AT ROW 13 COLIIMN 2 {INCLUCES GRID DIP FACTOP. OF 1.0075) i MAX 1 MUM 3D ONE PIN POWER W/UNC e 2.0217 (1.7844 X 3.1000 X 1.0300)

MAXIMUM LHGR = 10.7061 FW/FT (1.7844 X 6.0000)

MAXIM'!M LNGR W/ UNCERTAINTY a 12.7438 FW/FT (2.0217 X 6.0000 X 1.0300 X 1.02001 PL TO 16.00 KW/FT W/O UNC = 153.2793 ( 16.00 X 100.00 /(10,7061 X .9750))

PL TO 16.00 EW/PT W/ UNCERTAINTY = 125.7704 1 16.00 1 100.00 /(12.7438 x .9750) + 3.0000)

ASSEMELY AX1AL SHAPE IEEX e .0074 ASSEMBLY AX1AL SHAFE INDEX W/UNC= .0000 NORMAL 11ED ASSEMBLY AXIAL POWER SHAPER NODE 1 2 3 4 5 6 7 8 AXIAL POWER .5675 .8509 .9797 1.0655 1.1071 1.1514 1.1592 1.1780 N3DE 9 10 11 12 13 14 15 16 AX1AL POWER 1.1608 1.1573 1.1154 1.0938 1.0307 .9634 .8242 .5932 E

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l- ASAS Manual Revision o 73 April 19,1994 i

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l Figure 13  !

Sample User Output File Page 21 of 37 1 PROGRAM ASAS VERSION 1 REV DATE 4 /12 /94. TODAY'S DATE IS 04/12/94. THE TIME IS 08:19:49 PAGE 21 A CODE TO CREATE NOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME i /R PG3 / Sp /OPPD/ s 30t est .p PUN TITI.E e Fort Calhoun Cycle 15 bOC 16.$ Hours - asatest CASE ID i B-10.5-J PDIL CASE J - 244 POWER, BANK 3 AT $74 X PO

  • 10,500 GWD/MT, EBAR = 16.119 GWDiMT, POWER = 20.004 FLhW = 100.004 NOTWT = 24164. ETEPS INSERTED, FQ e 2.624 F-DELTA-H = 1,990, INCORE ASI = .3058, PERIPHERAL ASI a .1549 TOTAL PELATIVE EXCORE SIGNAL a .4147 TOTAL FUEL PINS IN QUARTER CORE a 5804.0
  • TOTAL OF ALL PINS IN QUARTER CORE . 6517.0-EDIT OF ASSEMBLY NUMBERS TO BE PROCESSED (AND REASONS FOR SELECTION) FOR FUEL TYPE:

4 TYPE 1 TYPE 2 i

1 10 USER SELECT USER SELECT 11 39 FO-PLANE 1 USEP. SELECT 16 3$

FQ-PLANE 1 FQ-PLANE 1 Il PQ-PLANE 16 18 CN-PLANE 2 v

t b

A$AS Manual Revision 0 74 April 19,1994

_ m . - _ _ _ ._. . _- . - _ _ . _ _ _ _ . _ _ - _-

Figure 13 Sample User Output File Page 22 of 37 1 PROGRAM ASAS VERSION 1. REV DATE 4/12/94. TOLAY'S DATE IS 04/12/94, THE TIME IS 08:19:49 PAGE 22 A CODE TO CREATE HCT CHANNEL DATA FILES FROM A $1MULATE-3 PIN FILE PIN FILE NAME t (RPG3/Sp/CPPD/s30 test.p  :

Port Calhoun Cycle 15 BOC 10,5 Hours - esatest '

SUN TITLE CASE ID h-10.5-J PDIL CA5E J - 20s POWER. BANK 3 AT 574 KPO e 10.500 GWD/MT, ESAR a 16.119 GWD/N1', POWER = 20.00s. rLOW = 100.004 - .

NO7Wr a 24164. STEPS INSERTED. FQ s 2.628 F-DELTA-H = 1.890, INCCRE AS1 = .3058. PERIPHERA1,AS1 e .1549 TOTA 1. ItELATIVE EXCORE SIGNAL e ,4347 FUEL TYPE : TYPE 1 PIN POWERS FOR LIMITING LNGR PLANE 6 FOR ASSDfBLY 1. SERIAL NUM8ER OMN012 .

1 2 3 4 5 6 7 8 9 to 11 12 13 14 1 .0634 .0666 .0714 .0760 .0801 .0848 .0917 .0942 .0932 .0947 .0971 .0992 .1013 .1058 2 .0724 .0803 .0896 .0944 .C970 .0990 .1019 .1046 .1080 .1130 .1383 ,1204 .1202 .1222 3 .0853 .0969 ---- ----

.1168 .1164 .1174 .1204 .2264 .1351 ---- ---- .3427 .1416 4 .1007 ,1136 ---- ---- .1359 1352 .1361 .1395 .1464 .1563 ---+ -+-- 1642 ,1622 5 .3188 .1292 .1414 .1496 .3531 .1558 .1585 .1625 .1686 .1755 .1827 .3852 ..1830 .1834 6 .1422 .1471 .1559 .1641 .1716 .1801 .1884 .1935 .1955 .1972 .2003 .2025 .2032 .2061 '

7 .1762 .17C2 .1747 .1824 .1920 .2069 ---- -- - .2274 .2215 .2244 .2262 .2275 .2310 8 .2036 .1967 .2014 .2094 .219.9 .2372 ---- ---- .2590 .2529 .2535 .2555 .2577 .2636 9 .2224 .2272 .2395 .2484 .2578 .2678 .2760 .2820 .2857 .2878 .2918 .2945 .2952 .2999 10 .2556 ,2689 .2890 .3007 .3017 .3019 .3010 .3061 .3190 .3326 .3472 ,3510 .3441 .3439 11 .2998 .3207 ---- ---- .3531 .3428 .3387 .3443 .3616 .3877 ---- ---- .4034 .3954 12 .3516 .3713 ---- ---- .3998 3879 .3854 .3927 .4104 .4396 ---- ----

.4596 .4523 13 .4102 .4176 .4358 .4436 .4190 .4368 .4433 .4541 .4658 .4859 .5088 .5167 .5106 .5162 14 ,4844 .4762 4805 .4852 .4900 .5012 .5275 .5453 .5429 .5516 5641 .5739 .5818 .6018 F3 PACTORS FOR ASSEMBLY 1, SERIAL IFJH8ER CHN012 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.2512 1.2492 1.2471 1.2463 1.2467 1.2479 1.2491 1.2476 1.2442 1.2412 1.2389 1.2381- 1.2387 1.2393 2 1.2518 1.2506 1.2447 1.2437 1.2482 1.2502 1.2507 1.2496 1.2468 1.2426 1.2358 1.2350 1.2399 1.2413 3 1.2531 1.2476 ---- ---- 1.2447 1.2513 1.2521 1.2511 1.2479 1.2389 --+- ---- 1.2364 1.2422 4 1.2558 1.2494 ---- ---- 1.2462 1.2526 1.2530 1.2520 1.2494 1.2406 ---- ---- 1.2385 1.2443 5 1.2600 1.2576 1.2509 1.2493 1.2533 1.2540 1.2528 1.2518 1.2511 1.2483 1.2420 1.2416 1.2466 1.2478 6 1.2648 1.2630 1.2607 1.2588 1.2571 1.2532 1.2472 1.2461 1.2506 1.2527 1.2526 .1,2523 1.2524 1.2518 7 1.2694 1.2671 1.2648 1.2623 1.2588 1.2500 ---, ---- 1.2481 1.2555 1.2572 1.3575 1.2568 1.2552 8 1.2721 1.2700 1.2683 1.2661 1.2628 1.2541 ---- +--- 1.2519 1.2593 1.2612 1.2616 1.2610 1.2602 9 1.2716 1.2708 1.2690 1.2674 1.2661 1.2623 1.2556 1.2547 1.2599 1,2623 1.2623 1.2625 1.2629 1.2623 10 1.2723 1.2702 1.2640 1.2631 1.2674 1.2681 1.2666 1.2658 1.2659 1.2640 1.2584 1.2582 1.2633 1.2647 11 1.2741 1.2675 ---- ---- 1.2652 1.2717 1.2724 1.2718 1,2700 1.2625 ---- ---- 1.2618 1.2680 12 1.2773 1.2706 ----

1.2685 1.2757 1.2771 1.2749 1.2746 1.2667 ---- -+-- 1.2664 1.2729 13 1.2812 1.2792 1.2731 1.2724 1.2714 1.2803 1.2811 1.2815 1.2798 1.2764 1.2708 1.2709 1.2767 1.2787 14 1.2851 1.2845 1.2832 1.2825 1,2831 1.2844 1.2851 1,2865 1.2844 1.2826 1.2816 1.2820 1.2831 1.2843 ASSEMBLY AXIAL PF.AKING FACTOR e 1.2662 (FRCH 16 PIANE DATA)

E h

ASAS Woual Revisip 0 75 April 19.1994

<~ . ---a - - - == , . - . - > , , , , e ,-we- 4 , -

i l

Figure 13 '

l Sample User Output File Page 23 of 37 l

1 PPOGIULM AEAS VERSION 1, &EV DATE 4/12 /94. TODAY'S DATE 15 04/12/%4. THE TIME 25 08:19:49 PAGE 23 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME : /RPG3/SP/OPPD/s30 test.p PUN TITLE Fort Cs1houn cycle 15 BOC 10.5 Hours - asatest CASE ID B-10.5-J FDIL CASE J - 20% POWER. SANN 3 AT 574 XPO e 10.500 GMD/Fr. EBAR a 16.119 CWD/Kr. POWER = 20.004. Flow e 100.004 N7!WT e 24164. STEPS INSERTED. FQ = 2.628. F-DELTA-H = 1.890. INCORE ASI e .2058. PEDIPMERAL ASI e .3549 'j TOTAL RELA 11VS EXCOPE SIGNAL a .4347  ;

FUEL TYPE e TYPE 1 2D PIN POWERS FOR ASSEMBLY 1. SERIAL NUMBER Cool 012 1 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 .0507 .0533 .0572 .0609 ,0442 .0679 .0734 .0754 .0749 .0763 .0784 .0801 .0817 .0853 l 2 .0578 .0642 0712 .0759 .0777 .0792 .0814 .0837 .0866 .0910 .0957 .0976 .0970 .0984 i 3 .06R1 .0777 ---- ---- .0939 .0930 .0937 .0961 .1011 .1090 ---- ---- ,1154 .1140 4 4 .0802 .0909 ---- ---- .1090 .1079 .3086 .1114 .1172 .1260 ---- --- .3326 .3304 5 ,0941 .1028 .1130 .3197 .1221 .1243 .1265 .1298 .1348 .1406 .1471 .1492 .1468 .1470 i 6 .1124 .1165 .3236 .3304 .1365 .1437 .1511 .1553 .1563 .3574 .1599 ,1617 .1623 .1646 -

7 .1388 .1343 .1382 .1445 .1526 ,1655 ---- ---- .1822 .1780 .1785 1794 .1810 .1841 8 .1600 .1549 .1588 .1654 .1741 .1891 ---- ---- .2069 .2008 .2010 .3025 .2044 .2092 9 ,1749 .3788 .1979 .1963 .2036 .2122 ,2199 .2248 .2267 .2280 .2311 .2333 .2337 .2376 10 42009 .3117 .2287 .2380 .2380 .2381 .2316 .2418 .2520 .2631 .2759 .2789 .2724 .2719 11 .2353 .3530 --- - --

.2791 .2695 .2662 .2708 .2847 .3071 - - - --- .3197 .3119 12 .2753 2923 ---- - - . - .3152 .3041 .3018 3076 .3220 .3411 ---- --- .3629 .3554 13 .3202 .3264 .3423 .3487 .1436 .3412 .3460 .3544 .3639 .3807 .4004 .4568 .3999 .403) 14 .3769 3708 .3745 .3784 .3819 .3902 .4105 .4239 .4226 .4300 .4401 .4477 .4535 .4684 FUEL TYFE i TYPE 1 ACJUSTED 2D P!N POWERS FOR ASSfMbLY 1. SEP1AL NUMBER OMN012 l!NCLUDES CR1D DIP F AC1cp OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 .0505 .0530 .0568 .0604 .0637 .0675 .0730 .0750 .0742 .0754 .0773 .0789 .0806 .0842 2 .0576 .0639 .0705 .0751 .0772 .0788 .0810 .0032 .0859 .0899 .0941 .0959 .0957 .0972 3 .0679 .0771 --- ---- .0930 .0926 .0934 .0958 .1005 .1075 ---- - - - - .3136 .1127 4 .0801 .0904 ---- ---- .1081 .3076 ,1083 .1110 .1165 .1243 ---- -- .1306 .3291 5 .0945 10s8 .3125 .1190 .3218 .1240 .3261 .1293 .1341 .1397 .1454 .1474 .2456 .1459 4 .1132 .1171 .1240 .1306 .1366 .1433 .1499 .1540 .1556 .1569 .1593 .1611 .1617 .1640 7 .3402 .1354 .1390 1451 .1528 .1646 ---- ---- .3809 .1779 .1786 .1799 .1810 1818 8 .1620 .3565 .1602 .1666 .1749 .1887 ---- ---- .3061 .3012 .2017 .2033 .20$1 ..2098 9 .3769 .1807 ,1898 .1980 .2051 .2131 .2196 .2244 .2273 .2290 .2321 ,2343 .2348 .2386 10 .2013 .2140 2300 .2392 .2401 .2402 .2395 .2436 .2539 .2646 .2763 .2792 .2738 ,2736 11 .2385 .2552 ---- ---- .2809 .2727 .2695 .2740 .2877 .3085 ---- ---- 3210 .3147 12 .2791 .2955 ---- ---- .3181 .3087 .3066 .3125 .3265 .3498 ---- ----

.3657 .3599 13 .3264 .3322 .3468 .3530 .3493 .3476 .3527 .3613 .3706 .3866 .4049 .4111 ,4063 .4107 14 .3854 .378) .3823 .3861 .3899 ,3988 .4197 .4339 .4319 .4389 .4488 .4566 .4629 .4788 MAXIMUM 2D ONE P!N POWER = ,4788 AT ROW 14 COLUMN 14 MAXIMUM 2D ONE PIN PCWER W/UNC = .5425 ( .4788 X 1.1000 X 1.0300)

MAXIMUM CHANNEL POWER * .4191 AT ROW 13 COLUMN 13 MAXIMUM 3D ONE PIN PCWER e 6C63 AT POW 14 CCLL'HN 14 (!N^LUDES GRID DIP FACTOR OF 1,0075)

MAXIMUM 3D ONE PIN POWER W/UNC * .6870 t 6063 X 1.1000 X 1.0300)

MAXIMUM LMCD = 3.6379 FW/FT ( .6063 X 6.0000)

MAXIMUM LNGR W/UNCEPTAINTY = 4 3304 FW/FT ( ,6870 X 6.0000 K 1.0300 X 1.0200)

PL TO 15,00 FW/FT W/O UNC = 422.8934 ( 15.00 X 100.00 /( 3.6379 x .9750)')

PL 1V 15. 00 FW/ FT W/UNCERTA!NTY e 352.2741 1 15.00 X 100.00 /t 4,3304 X .9750) - 3.0000)

ASSEMBLY AKIAL EMAPE INDEX = .1500 ASSEMPLY AX1AL SMAPE INDEX W/UNC= 1108 NOFMALIZF:D ASSEMBLY AX1AL POWER SMAFE:

NOCF 1 2 3 4 5 6 7 8 AX1A!. POWER .8452 1.0410 1.1582 1.2373 1.2603 1.2662 1.2229 1.1754 NOCE 9 10 11 12 13 14 15 16 AXI:1 POTP 1,0959 1.C310 .9525 .8955 .8272 .7677 .6750 .5486 J

i l

l i

ASAS Manual Revhion 0 76 April 19,1994

'I i

_ , _ . __ _J

Irignani 13 Sample User Output File Page 24 of 37 1 PROGRAM AFAS VERSION 1, PFV CATE 4/12/94. TODAY'S DATE 18 04/12/94, TWE TIME 19 08:19:49 PAGE 24 A CODE TO CRF. ATE HOT CHANNEL DATA FILES FROM A SIM'JLATE-3 PIN FILE PIN FILE NAME : /PPGl/Sp/OPPD/s30 test.p RUN TITLE  : Fort Calhoun Cycle 15 BOC 10.5 Hours - asatest CASE ID .i B-10.5-J PDIL CAEE J - 20% POWER. BANK 3 AT 574 XPO s 10.500 GWD/MT, ERAR = 16.119 GWD/MT. POWER = 204009. PIDW e 100,004 N97WT e 24164. STEPS INSFFTED, FQ e 2.628. F-DELTA-M = 1.890, INCOPmE ASI = .2058 PERIPHERAL ASI e .1549 TOTAL kELATIVE KKCOP.E SIGMAL e .4347 FUEL TYPE TYPE 1-PIN POWERS FOR LIMITING LHOR PLANE 5 FOR ASSEMBLY 13.EERI AL NUMBER OMS 013 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.7593 1.5845 1 8858 1.7638 1.8985 1.9193 .1,9051 1.9052 1.9193 1.8985 1,7638 1.8858 1.5845 1.7593 2 1.6146 1.9237 1.7816 1.9391 1.8461 1,9231 1.9178 1,9178 1.9231 1.8461 1.9391 1.7816 1.9237 1.6166 3 1.9528 1.8085 ---- ---- 2.0134 2.0098 1.9672 1.9672 2.0098 2.0134 ---- ---- 1.8085 1.9528 4 1.8507 1.9947 ---- ---- 1.8975 2.0456 2.0201 2.0201 2.0456 1.8975 ---- ---- 1.9947 1,8507 5 2.0176 1.9240 2.0674 1.9226 2.1287 2.0931 2,C824 2.0824 2.0931 2.1287 1.9226 2.0674 1.9240 2.0176 6 2,0661 2.0311 2.0916 2.1009 2.1218 2.1673 1.9521 1.9521 2.1673 2.1218 2.1009 2.0916 2.0311 2,0661 7 2.0777 2.0536 2.0766 2.1047 2.1416 1.9807 ---- ---- 1,9807 2.1416 2.1047 2.0766 2.0536 2.0777 8 2.1049 2.0802 2.1034 2.1317 2.1698 2.0103 ---- ---- 2.0103 2.1698 2.1317 2.1034 2.0802 2,1049 9_ 2.1532 2.1177 2.1808 2.1910 2.2127 2.2614 2.0404 2.0404 2.2614 2.2127 2.1910 2.4808 2.1177 2.1532 10 2.1656 2.0689 2.2215 2.0678 2.286) 2.2480 2.2373 2.2373 2.2480 2.2863 2.0678

2.1023 2,2628 2.2343 2.2343 2 2628 2.1021 ----

2.2215 2.0689 2.1656

2.2091 2.0485 11 2.0485 2.2091 ----

12 2.2260 2.0665 - --*~ ---- 2.2962 2.2899 2.2413 2.2413 2.2899 2.2962 ---- ---- 2.0665 2.2260 13 1,9019 2.2448 2.0993 2,2817 2.1723 2.2589 2.2517 2.2517 2,2589 2.1723 2.2817 2.0993 2.2648 1.9019 14 2.1343 1.9264 2.2902 2.1426 2.3024 2.3257 2.3077 2,3077 2.3257 2.3024 2.1426 2.2902 1.9264 2.1343 F2 FACTORS FOR ASSEMBLY 13. SERIAL NUMBER OM3013 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1426 1.3363 1.3412 1.3376 1.3445 1.3470 1.3476 1.3476 1.34?0 1.3445 1,3376 1.3412 1.3363 1.3426 2 1.3386 1.3417 1.3382 1.3442 1.'3406 1.3474 1.3489 1.3489 1.3474 1.3406 1.3442 1.3382 1.3417 1.3386 3 1.3452 1.3399 ---- ---- 1.3478 1.3491 1.3513 1.3513 1,3497 1,3478 ---- .--- 1.3399 1.3452 4 1.3431 1.3475 ~~-- -+-- 1,3449 1.3515 1.3529 1.3529 1.3515 1.3449 --- ---+ 1.3475 1.3431 5 1.3517 1.3457 1.3513 1.3468 1.3522 1.3541 1.3540 1.3540 1.3541 1,3522 1.3468 1.2513 1.3457 1,3517 6 1.3564 1.3547 1.3554 1,3556 1.3563 1.1553 1.3500 1.3500 1.3553 1.3563 1.3556 1.3554 1.3547 1,3564 7 1.3599 1.3592 1.3602 1.3601 1.3594 1.3527 ---- ---- 1.3527 1.3594 1.3601 1.3602 1.3592 1.3599 8 1.3634 1 3627 1.3638 1.3637 1.3630 1.3559 ---- ---- 1.3559 1 3630 1.3637 1.3638 1.3627 1.3634 9 1.3667 1.3650 1.3659 1,3661 1.3668 1,3658 1.3599 1.3599 1.3658 1.3668 1.3661 1.3659 1.3650 1.3667 10 1.3680 1.3617 1.3681 1.3631 1.3695 1.3715 1.3718 1,3718 1.3715 1.3695 1.3631 1.3681 1.3617 1.3680 11 1.3650 1.3705 ---- ---- 1.3682 1.3458 1.3775 1.3775 1,3758 1.3682 *--- ---- 1.3705 1.3650 12 1,3141 1.3692 -- --- 1.3789 1.3813 1.3831 1.3831 1 3813 1.3789 ---- ---- 1.3692 1.3741 13 1.3736 1.3785 1.3751 1.3821 1,3784 1.3862 1.3880 1.3880 1.3862 1.3784 1.3821 1.3751 1.3785 1.3736 14 1.3859 1.3797 1.3862 1.3826 1.3907 1.3939 1.3946 1.3946 1.3939 1,3907 1.3826 1.3862 1.3197 1.1859 ASSENBLY AX1AL FEAKING FACTOR e 4.3613 (PRCM 16 PLANE 1)ATA) i I

l ASAS Manual Revision 0 77 April 19,1994 l

l

  • __s= a -g- +.d+ . .u. . .i.e-m ,i. -an. e- t r-. s

5 Figure 13 Sample User Output File Page 25 of 37 1 PMBAM ASAE VERSION 1. REV 1 SATE 4/12/94, TODAY'S DATE IC 04/12/94. THE TIME IE 08419:49 PAGE 25 A COLE TO CREATE MOT CHAHEE1. DATA FILES FROM A SIMULATE-3 FIN FILE PIN FILE NAME t /PPC3/Sp/OPPDIs30 test.p RUN TITLE a Port Calhoun Cycle 15 BOC 10.5 Hours

  • asetest CASE ID s 5 10.5-J PD1L CASE J - 20% POWER, BANK 3 AT 574 ,

XPO e 10.500 OWD / MT. - ESAR

  • 16.119 CWD/Kr. POWER e 20.fW FIon' = 100.00t NO7wr a 24164. BTEPS INSEPTED. FQ
  • 2.628 F-DELTA-H e 1.890, NICOPE A$1 * .3058 PERIPNERAL ASI e. .1549 I TOTAL PELATIVE F.XCORE SIGNAL * .4347 FUEL TYPE : TYPE 1 2D PIN POWERS FOR ASSEMBLY 13. SERIAL NUMBER OM5013 .

1 2 3 4 5 6 7 e s 10 11 12 13 14 1 1.3131 1.1889 1.4089 1.3217 1.4145 1.4268 1.4157 1.4157 * .4268 1.4145 1.3217 1.4089 1.1889 1.3131 2 1.;105 1.4365 1.3342 1.4449 1.3797 1.4291 1.4234 1.4'3d 1.4291 1.3797 1.4449 1.3342 1.4365 1.2105 3 1.4539 1.3523 ---- ---- 1 4956 1.4905 1,4571 1. # a il 1.4905 1.4956 ----

1.3523 1.4539 4 1,3900 1.4821 ---- --~~ 1.4129 1.5148 1.4942 la*44 1.5148 1.4129 ---- ---- 1.4821 1.3800 5 1 4936 1.4313 1.5309 4.4292 1.5751 1.5466 1.5386 1.5386 1.5466 1.5751 1.4292 1.5309 1.4313 1.4936 6 1.5233 1.4995 1.5433 1.5501 1.5646 1.5996 1,4473 1,4473 1.5996 1.5646 1.5501 1.5433 1.4995 1.5233 7 1.5278 1.5108 1.5267 1.5474 1.5754 1.4650 ----

1.4650 1.5754 1.5474 1.5267 1.5108 1.b278 8 1.5438 1.5265 1.5423 1.5632 1.5919 1.4828 ----

1.4828 1.5919 1.5652 1.5423 1.5265 1.5438 9 1.5754 1.5514 1.5966 1.6039 1.6189 1.6557 1.5004 1.5004 1.6557 1.6189 1.6039 1.5966 1.5514 1.5754 10 1.5830 1.5193 1.6238 1.5170 1.6695 1.6391 1.6310 1.6310 1.6391 1.6695 1.5170 1.6238 1.5193 1.5830 11 1.5007 1.6119 --*-

1.5363 1.6447 1.6220 1.6220 1.6447 1.5363 ----

-+-- 1.6119 1.5007 12 1.6199 1.5093 ----

1.6652 1.4579 1.6204 1.6204 1.6579 1.6652 ----

1.5093 1.6199 13 1.3846 1.6430 1.5266 1.6508 1.5760 1.6295 1.6223 1.6221 1,6295 1.5760 1.650s 1.5266 1.6430 1.3846 14 1.5400 1.1962 1.6522 1.5497 1.6556 1.6685 1.6548 1.6548 1.6645 1.6556 1.5497 1.6512 1.3962 1.5400 j FUEL TYPE . TYFE1 ANUSTEL 2D PIN POWER $ FOR ASSEMBL't 13. SERIAL NUMBER OMS 013 (INCLUDES CRID 01P FACTOP OF 1.0075) I 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1 1.3048 1.1758 1.3985 1.3064 1.4075 1.4224 1.4119 1.4119 1.4224 1.40'15 1.3084, 1.3985 1.1758 1.3048

)

2 1.1993 1.4264 1.3214 1.4375 1.3689 1,4251 1.4210 1.4210 1.4251 1.2689 1.4375 1.3214 1.4264 1.1993 1 3 1.4475 1.3410 ----

1.4919 1.4888 1.4572 1.4572 1.4888 1.4919 ----

-~~- 1.3410 1.4475 4 1.3718 1.4780 ---- ---- 1.4063 1,5152 1.4961 1.4961 1.5152 1.4063 ----

1.4780 1.3718 5 1.4942 1.4256 .1.5311 1,4245 1.5763 1 5499 1.5419 1.5419 1.5499 1.5763 1.4245 1.5311 1.4256 1.4942 6 1.5292. 1.5034 1.5482 1.55S2 1.5706 1.6045 1.4460 1.4460 1.6045 1.5706 1.5552 1.5482 1.5034 1.5292 7 1.5377 1.5199 1.5369 1.5577 1.5850 1.4666 ---- + -- 1.4666 1.5850 1.5577 1.5369 1.5199 1.5377 8 1.5579 1.5395 1.5567 1,5777 1.6059 1.4879 ----

1.4879 1.6059 1.5777 1.5567 1.5395 1.5579 9 1.5936 1.5671 1.6140 1.6216 1.6376 1.6736 1.5101 1.5101 1.6736 1.6376 1.6216 1.6140 1.5673 1.5936 10 1.6027 1.5312 1.6442 1.5304 1.6921 1.6638 1.6558 1.6554 1.6638- 1.6921 1.5304 1.6442 1.5312 1.6027 11 1.5161 1.6350 -- ---- 1.5557 1.6747 1.6534 1,6536 1.6747 1,5557 ~~ - - - 1.6350 1.5161 12 1.6475 1.5294 ---

1.6994 1.6948 1.65R8 1.6588 .1.6948 1,6994 ----

1.5294 1.6475 l 13 1.4076 1.6762 1.5537 1.6887 1.6077 1.6718 1.6665 1.6665 1.6718 1.6077 1.6887 1.5537 1.6762 1.4076 l 14 1.5796 1.4257 1.6950 3.5857 1.7040 1.7213 1.7080 1.7080 1.7213 1.7040 1.5857 1.69,50 1.4257 1.5796 MAXIM'lM 2D CNE P!N POWER e 1,7213 AT ROW 14 COLT %f 6 MAXIMUM 2D ONE PIN POWER W/UNC = 1.9502 (1.*/213 X 1.1000 # 1.0300)

MAX 1 MUM CHANNEL POWEP e 1.6919 AT ROW 13 C01.UMN 6 MAXIML9f 3D ONE PIN POWER =

2.3432 AT POW 14 COLUMN 6'(INCLUDES GRID E!P FACTOR CF 1.0075)

MAXIMUM 3D ONE PIN POWER W/UNC = 2.6548 (2.3432 X 1.2000 X 1,0300) 1 MAXIMUM LHCR = 14.0549 FW/FT (2.3432 X 4.0000) '

MAX 1 MUM LMCR W/UNCERTAllTTY = 16.7347 FW/PT (2.6540 X 6.0000 X 1,0300 X 1.02001 PL TO 15. 00 FW/ PT W /O L77' s. 109.4297 8 15.00 X 100.00 /(14.0589 x .97501)

PL 7015.00 FW'FT W/UN"KPTAINTY = 68.9323 ( 15.00 X 100.00 /(16.7147 x .9750: - 3.00001 AS$lO4BLY ARIAL EMAPE INDEX e 1956 ASSDtBLY AXI AL CHAPE INDEX W/t1NCe .1556 N'JPMALIEED ASSEMBLY X1AL POWER THAPEt NOLE 1 2 3 4 5 6 7 8 AXIAL POWEP .6943 1,0619 1.2424 1.3448 . 3613 1.3606 1.2867 1.2129 N%E 9 10 11 12 13 14 15 16

. AX1AL FJWER 1.0975 1.0171 .9235 .8644 .7873 7203 .6021 .4223 I

l ASAS Manual Revision 0 78 April 19,1994

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Figure 13 Sample User Output File Page 26 of 37 l 1 PROCRAM ASAE VERSION 1. REV DATE 4 /12 /94. TODAY'S DATE IS 04/12/94. THE TIME IS C8:19:49 PAGE 26 A CODE TO CREATE NOT CHANNEL DATA FILF5 FROM A $1MULATE-3 PIN FILE FIN FILE NAME a / R PG3 /SpiGPPD/ s 30tes t . p RUN TITLE i Fort Calhoun Cycle 15 BDC 10.5 Hours - asatest CASE ID B-10.5-J PDIL CASE J - 20% POWER. BANK 3 AT 574 X F0 = 10.500 GWD/MT, EBAP = 16.119 GWDIMT. POWER

  • 20.00t. FLOW = 100.004 NOTWT e 24164. ETEPS INSERTED, FQ e 2.628 F-DELTA-H = 1.890. %NCORE ASI = .2058, PERIPHERAL ASI = .1549 l TOTAL RELATIVE EXCOEA SIGNAL * .4347 FUEL TYPE : TYPE 1 - -l <

PIN POWERS FOR LIMITIPG LHCR PLANE 6 FOR ASSEMBLY 16 KERIAL NUMBER OMS 019 12 13 14  !

1 2 3 4 5 6 7 8 9 1D 11 1 1.4886 1.4131 1.8028 1.9035 1.9142 1.9409 1.9620 1.9914 2.0349. 2.0774 2.1422 2.1102 1.7295 1,9236 2 1.4079 1.7811 1.6815 1.8938 1.8681 1.9689 1.9879 2.0143 2.0532 2.0081 2.C998 1.9299 2.1257 1.7711

1.9544 2.1888 1 1.7915 1.6773 ---- ---- 2.0264 2.0726 2.0444 2.0674 2.1488 2.1559 ----

4 1.8880 1.8858 ---- ---- 2.1048 2.1387 2.1045 2.1245 2.2055 2.2183 ---- ---- 2.1470 2.2440 5 1.8962 1.8582 2.0213 2.1031 2.2254 2.1575 2.2051 .2.2226 2.2142 2.3258 2.2399 2,1979 2.0740 2.1976 6 1.9216 1.9578 2.0671 2.1370 2.1577 2.0908 2.2233 2.2392 2.1395 2.2401 2.2533 2.2169 2.1454 2.1747 7 1.9436 1.9776 2.0401 2,1045 2.2075 2,2257 ---- ---- 2.2730 2.2828 2.2040 2.1653 2.1332 2.1459  !

8 1.9754 2.0070 2,0667 2.1283 2.2291 2.2451 ---- ---- 2.2869 2.2941 2.2126 2.1718 2.1379 2.1488 9 2,0206 2.0492 2.1529 2.2155 2.2274 2.1514 2.2795 2,2893 2.1798 2.2745 2.2814 2.2386 2.1611 2.1954 10 2.0654 2.0081 2.1655 2 2355 2.3481 2.2614 2.2980 2.3047 2.2828 2.3855 2.2866 ----

2.2341 2.2000 2.2166

2.1846 2.2721 11 2 1329 2.1039 ---- ---- 2.2701 2.2845 2.2286 3.2333 2.3004 2.2974 12 2.1029 1,9355 ---- ---- 2.2341 2.2555 2.1989 2.2020 2.2666 2.2540 ---- ---- 1.9990 2.2259 il 1.7119 2.1272 1.9671 2.1726 2.1065 2.1834 2.1710 2.1727 2.1900 2.1195 2.1945 .1.9997 2.1862 1.8112 t

14 1.9035 1.7531 2.1768 2.2438 2.2078 2.1936 2.1745 2.1743 2.'955 2.2145 2.2583 2.2032 1.7922 1.9840 l

FZ FACTOPS FOR ASSEMBLY 16, SERIAL NUMBER OMSOl9 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3403 1.3354 1.3415 1.3439 1.3448 1.3462 1.3465 1.3468 1.3472 1.3466 1.3464 3.3450 1.3400 1.3468 2 1.3354 1.3397 1.3382 1.3442 1.3407 1.3463 1.3476 1.3479 1.3473 1.3423 1.3466 1.341b 1.3442 1.3420 .

i l 3 1.3418 1,'3385 ---- - -- 1.3471 1.3479 1.3485 1.3487 1.3488 1.34s6 ---- ---- 1.3425 1 3482 i 4 1.3445 1.3448 ---- ---- 1.3489 1.3488 1.3498 1.3501 1.3496 1.3502 ----

--- . 1.3485 1.350!

5 1.3458 1.3416 1 3478 1.3493 1,3491 1.3490 1.3500 1.3502 1.3498 1.3502 1.3509 1.3501' 1.3449 1.3514 6 1.3475 1.3476 1.3489 1.3495 1.3494 1.3452 1,3508 1.3511 1.3459 1.3505 1.3510 1.3511 1.3508 1.3529 7 1.3481 1.3492 1.3498 3.3509 1.3507 1.3512 --~~ ---- 1.3519 1.3518 1.3524 1.1519. 1.3524 1.3535 8 1.3487 1.3498 1.3504 1.3515 1.3512 1.3518 ---- ---- 1.3525 1.3524 1.3531 1.3527 1.3531 1.3543 9 1.3494 1.3495 1.3507 1.3512 1.3511 1.3469 1.3526 1.3529 1.3476 1.3524 1.3530 .1.3531 1.3529 1.3552 10 1.3489 1.3447 1.3508 1.3522 1.3519 1.3519 1.3529 1.3532 1.3528 1.3533 1.3541 1.3534 1.3483 1.3551 Il 1.3469 1.3491 ----

1.3529 1.3528 1.3539 1.3543 1.3538 1.3545 ---- ---- 1.3533 1,3556 -

12 1.3476 1.3442 ---

--+- 1.3524 1.3532 1.3538 1.3542 1.3543 3.3542 ---- ---- 1.3488 1.3550 13 1.3425 1.3469 1.3453 1.3512 1.3475 1.3531 1.3544 1.1549 1.3544 1.3494 1,3540 1.3491 1.3523 1.3506 14 1.3492 1.3445 1.3508 1.3530 1.3538 1.3552 1.3554 1.3558 1.3565 1.3561 1.3563 1.3552 1.3506 1.3583 ASSEMBLY AXIAL PEAK 1NG FACTOR = 1.3496 IFROM 16 PLANE DATA)

(

b L

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ASAS Manual Revision o 79 April 19,1994

---e e r w-. .- . . , , . .

-. - . - - ~ . . -

I Figure 13 Sample User Output File Page 27 of 37 1 PROGPAM ASAS VERSION 1. REV DATE 4/12 /94. TODAY'E DATE IS 04/12/94 THE TIME IS J8419:49 PAGE 27 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A $1MULATR-3 P1N FILE PIN FILE RAME 4 /RPG3/Sp/OPPD/s30 test.p P.UN TITLE 2 Fort Calhoun Cycle 15 maC 10.5 Mours - asatest CAss ID  : B-10.5-J PDIL CASE J - 206 MMER. b4NK 3 AT 574 KPo 10,500 OWD/NT. EBA8

  • 16.119 CWD/KT, POWER = 20.004 FIDW = 100.004 .

NO1WP a 24164. STEPS INSEPTED. PQ

  • 2.628 F-DELTA-H e 1.890. JNCORE ASI = ,2058 PERIPHERAL AS1 = .1549 a TOTAL DELATIVE EXCORE SIGNAL = .4347 FUEL TVPE TYPE 1 2D P!N POWERS FOR ASSEMBLY 16. SERI AL smMaER OMS 019 1 2 3 4 5 6 7 6 9 10 11 12 13 14 1 1.1106 1.0582 1.3438 1.4164 1.4234 1.4417 1.4571 1.4786 1.5104 1.5427 1.5910 1.5689 1.2907 1.4283 2 1.0543 1.3295 1.2565 1.4089 1.3934 1.4624 1.4751 1.4944 1.5240 1.4961 1.5594 1.4387 1.5814 1.3197 3 1.3351 1.~531 ----

1.5043 1.5377 1.5161 1.5129 1.5931 1.5986 ---- ---- 1.4558 1.6235 4 1.4042 1,4023 ---+ +--- 1.5604 1.5856 1.5591 1.5736 1.6942 1.6429 ---- ---* 1.5922 1.6617 5 1.4090 1,3850 1.4997 1.5587 1.6495 1.5993 1.6335 1.6462 1.6405 1.7225 1.6581 1 6280 1.5422 1.6261 6 1.4261 1.4528 1 5324 1.5815 1.5990 1.5543 1.6439 1.6573 1.5897 1.6587 1.6678 1.6409 1.5883 1.6074 1.4418 1.4657 1,5114 1.5579 1.6343 1.6472 7 ----

1.6813 1.6888 1.6296 1.6016 1.5773 1.5854 8 1.4646 1.4868 1.5304 1.5749 1.6497 1.4609 ----

1.6908 1.6963 1.6352 1.6054 1.5799 1.5867 9 1,4974 1.5185 1.5938 1.6396 1.6485 1.5973 1.6852 1.6921 1.6175 1.6819 1.6862 1.6544 1.5974 1.6126

'10 1.5312 1.4933 1.6031 1.6513 1.7368 1.6738 1.6986 1,7032 1.6875 1.7627 1.6887 1.4507 1.5575 1.6158 11 1.5812 1.tS94 ---- ---+ 1.6779 1.6887 1.6460 1.6490 1.6992 1,6961 ---- ---- 1.6142 1.6761 i 12 1.5605 1,4399 ---- ---- 1.6519 1.6668 1,6243 1.6261 1.6736 1.6644 --- ---- 1.4820 1.6428 13 1.2826 1.5793 1.4623 1.6079 1.5633 1.6136 1.6029 1.6036 1.6170 1.5707 1.6207 1.4823 1.6166 1.1411 14 1.4108 1.3039 1.6115 1.6584 1.6308 1.6187 1.6044 1.6036 1.6185 1.6330 1.4651 1.6257 1.3270 1.4606 FUEL TYPE e TYFE1 A MUSTED 2D PIN POWEkB FOR ASSEMBLY 16. SERIAL NUMBER oms 019 (INCLUDES CRID D1P FAC1tR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.1111 1.0547 1.3456 1_4208 1.4287 1.4487 1.4644 1.4864 1.51d9 1.5505 1.5989 1.5750 1.2907 1.4358 2 1.0509 1.3294 1.2550 1.4135 1.3943 1.4696 1.4837 1.5035 1.5325 1.4989 1.5673 1.4405 1.5866 1.3219 3 1.3372 1.2519 ---- ---- 1.5125 1.5470 1.5259 1.5431 1.6039 1.6091 ---- ---- 1.4588 1.6337 4 1.4092 1.4076 +--- ---- 1.5710 1.5964 1.5708 1.5857 1.6462 1.6557 ----

1.6025 1.6749 5 1.4153 1.3870 1.5087 1.5698 1.6611 1.6104 1.6459 1.6590 1.6527 1,7360 1.6718 1.6405 1.5480 1.6403 6 1.4343 1.4613 1.5428 1.5951 1.4105 1.5606 1.6595 1.6713 1.5969 1.6720 1.6819 1.6547 1.6013 1.6232 7 1.4507 1.4761 1.5227 1.5708 1.6477 1.6612 ---- ---- 1.6966 1,7039 1.6451 1.6162 1.5922 1.6017 8 1,4744 1.4980 1.5426 1.5887 1,6618 1.6758 ---- ---- 1.7069 1.7123 1.6515 1.6210 1.5957 1.6039 9 1.5082 1.5295 1.6069 1.6537 1.6625 1.6058 1.7014 1.7087 1.6270 1.6977 1.7028 1.6709 1.6130 1.6312 to 1.5416 1.4988 1.6164 1.6685 1.7526 1.6879 1.7152 1.1202 1.7039 1.7805 - 1.7067 1.6675 1.5674 1.6545 11 1.5920 1.5701 ---- - - - 1.6944 1.7051 1,6634 1.6669 1.7170 .1 7148 -----

1.6306 1.6959 12 1.5696 1.4447 ----

1.4675 1.6835 1.6412 1.6436 1.6918 1.6823 ---- --- 1.4920 '2.6614 13 1.2852 1.5878 1.4684 1.6216 1.5723 1.6296 1.6204 1.6217 1.6346 1.5820 1.6379 1.4926 1.6317 1.3519 14 1.4208 1.3085 1,f248 1.6748 1.6479 1.6313 1.6231 1.6229 1.6387 1.6529 1,6856 1.6444 1,3377' 2.4808 MAXIMUM 20 ONE P1H POWER e 1.7805 AT ROW 10 COLUMN 10 MAAIM'JM 2D ONE PIN POWER W/UNC a 2.0173 (1.7905 K 1.1000 X 1.03003 MAJtIMUM CHANNEL PWEP e 1.7291 AT POW 10 COLtHN 9 MARIMUM 3D ONE PIN (CWEP a 2.4014 AT ROW 10 COLUMN 10 IINCLUDES GRID DIP PACTOR OF 1.0075)

MAXIMUM 3D ONE PIN POWER W/UNC e 2.7230 12,4034 X 1.1000 X 1.0300)

MAXIMUM LHGR

  • 14.4203 FW/FT 42.4034 X 6.0000)

MAXIMUM 1.MGR W/UNCERTAltrY e 17.1649 FW/FT (2,7230 X 6.0000 X 1.0300 X 1.02006 PL TO 15.00 KW/FT W/O UNC s 106.6871 ( 15.00 X 100.00 /t14.4203 X .97506)

PL TO 15,00 FW/FT W/UNCEPTA1HTY a 86.6282 1 15.00 X 100.00 /t17.1649 X .9750) - 3.0000)

ASSEMBLY AXIAL SHAPE INDEX e .1744 AS$ltMBLY A11 AL EHAPE INDEX W/UNC= .1344 NDPJ4 ALII.ED ASSEMBLY AXI AL POWER SHAPE:

NQOE 1 2 3 4 5 6 7 8 ARIAL POWEh .6266 1.0180 1.2147 1.1243 1.1447 1.3498 1.2862 1.2200 NODE 9 10 11 12 13 14 15 16 AKIAL POWER 1.1274 1.0550 .9611 8998 .8162 .7407 6046 .3997

.i ASAS Manual Rev sion 0 i 80 April 19,1994

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I?ig32re 13 Sample User Output File  ;

Page 28 of 37 1 1 PROGRAM AEAS VERSION 1. REV DATE 4 /12/94. TODAY'S DATE IS 04/12/94. THE TIME IS 08:19:49 PAGE 28 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME 1 / R PG3 / Sp /0 PPD / s 30 test .p PUN TITLE Fort Calhoun cycle 15 BOC 10.5 Hours - asatest CASE ID i B-10.5-J PDIL CASE J - 20% POWER. BANK 3 AT 574 XPO = 10.500 GWD/Kr, EBAR e 16.119 GWD/MT, POWER = 20.004. Flow = 100.004 NUTWT = 24164. ETEPS INSERTED, FQ = 2.628. F-DELTA-H = 1.890, INCORE ASI = 2058. PER1PHERAL ASI e .1549 TOTAL PELATIVE EXCORE SIGNAL = .4347 FUEL TYPE : TYPE 1 PIN POWERS FOR LIMITING I M A PLANE 6 FOR ASSEMBLY 11,$ERIAL NUMBER OMS 009 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1- 1.7052 1.5435 1.8360 1.7169 1.8444 1.8625 1.6480 1,8507. 1.8694 1.8544 1.7287 1.8524 1.5611 1.7331 2 1.5720 1.8823 1.7465 1.8980 1.8058 1.8775 1.8720 1,8737 3.8813 1.8108 1.9058 1.7563 1.8989 1.5954 3 1.9051 1,7793 ---- - - - 1.9760 1.9693 1.9273 1.9282 1.9711 1.9784 -- - ---- 1.7897 1.9291 4 1.8142 1.9686 ---- -.-- 1.8685 2.0093 1.9431 1.9834 2.0093 1.8680 ---- ---- 1.9755 1.8315 5 1.9829 1.9048 2.0454 1.8998 2.0963 2.0577 2.0460 2.0458 2.0567 2.0945 1.8973 2.0441 1.9069 1.9964 -

6 2.0354 2.0114 2.0697 2.0739 2.0888 2.1301 1.9195 1.9184 2.1285 2.0861 2.0701 2.0659 2.0102 2.0434 7 2.0515 2.0340 2.0527 2.0139 2.1042 1.9447 ---- ---- 1.9431 2.1017 2.0698 2.0474 2.0293 2.0530 8 2.0788 2.0585 2.0760 2.0964 2.1272 1.9694 - - - - ---- 1.9677 2.1243 2.0917 2.0694 2.0515 2.0761 ,

9 2.1216 2.0916 2.1478 2.1496 2.1633 2.2070 1.9947 1.9943 2.2054 2.1597 2.1437 2.1390' 2.0832 2.1178 L 10 2.1277 2.0386 2.1808 2.0227 2.2260 2.1842 2.1756 2.1759 2.1828 2.2225 2.0167 2.1727 2.0301 2.1241 11 2.0065 2.1664 ---- ---- 2.0389 2.1881 2.1618 2.1620 2.1869 2.0358 ---- ---- 2.1594 2.0043-

  • 12 2.1709 2.0198 ---- ---- 2.2161 2.2043 2.1578 2.1575 2.2035 2.2143 ---- ---- 2.0151 2.1707 13 1.8546 2.2100 2.0428 2.2089 2.0959 2.1711 2.1602 2.1591 2.1698 2.0942 2.2072 2.0401 2.2075 1.8550 '

14 2.0965 1.8971 2.2463 2.0935 2.2379 2.2493 2.2159 2.2132 2.2451 2.2342 2.0900 2.2428 1.8931 2.0932 i

F2 FACTORS FOR ASSEMBLY 11 SERIAL NUMBER OMS 009 1 2 3 4 5 6 7 8 9 10 11 12 13 14

-1 1.3374 1.3318 1 3358 1.3319 1.3376 1.3396 1.3399 1.3399 1.3393 1.3370 1.3307 1.3343 1.3298 1.3358 2 1.3321 '1.3355 1.3322 1.3370 1.3332 1.3389 3.3401 1.3401 1.3386 1.3324 1,3361 1.3307 1.3342 1.3311 3 1.3366 1.3328 ---- ---- 1.3387 1.3399 1.3412 1.3412 1.3397 1.3382 ---- ---- 1.3317 1.3367 4 1.3335 1.3384 ---- ---- 1.3348 1.3403 1.3414 1,3414 1.3402 1.3343 ---- ---- 1.3381 1.3339 5 1,3398 1.3353 1.3402 1.3356 1.3399 1.3412 1.3411 1.3411 1.3412 1.3399 1.3353 1.3402 1.3354 1.3412 6 1.3424 1.3417 1.3421 1.3419 1.3420 1.3408 1.3359 1.3358 1.3410 1.3423 1.3423 1.3428 1.3427 1.3447 7 1.3433 1.3435 1.3442 1.3437 1.3426 1.3367 ---- --- 1.3369 1.3433 1.3447 1.3455 1.3453 1.3463 8 1.3439 1.3441 1.3448 1.3443 1.3434 1.3377 - - -

1.3381 1.3445 1.3458 1.3468 1.3467 1.3478 9 1.3441 1.3434 1.3440 1.3440 1.3443 1.3433 1.3388 1.3390 1.3441 1.3457 1.3459 1.3467 1,3469 1.3491 10 1.3427 1.3384 1.3434 1.3391 1.3436 1.3453 1.3456 1.3460 1,3464 1.3455 1.3414 1.3468 1.3425 1.3487 11 1.3375 1.3426 ---- ---- 1.3400 1.3459 1.3474 1.3480 1.3474 1.3422 ---- ---- 1.3480 1.3444 12 1.3418 1.3384 ----

1.3453 1.3470 1.3490 1.3497 1.3488 1.3482 ---- ---- 1.3446 1.3502 13 1.3384 1.3425 1.3396 1.3448 1.3415 1,3477 1.3496 1.3503 1.3498 1.3448 1.3496 1.3454 1.3501'.1.3478 14 1.3452 1.3401 1.3451 1.3418 1.3481 1.3507 1.3517 1.3523 1.3528 1.3517 1.3468 1.3518 1.3487 1.3557 ASSEMBLY AX1AL PEAKIN'1 FACTOR = 1.3422 (FRCH 16 PLANE DATA)

ASAS Manual Revision 0 81 April 19,1994

Figure 13 Sample User Output File Page 29 of 37 1 PROGRAM AKAS VEPS10N 1. PE'/ DATE 4/12/94. TODAY'S DATE IS 04/12/94. THE TIME IS 08519149 PAGE 29 A CODE 70 CPEATE HOT CHANNEL DATA FILES FRGM A 51MULATE-3 PIN FILE l PIN FII.E NAME : /RPG3/Sp/OPPDin30 test.p RUN TITLE  : Fort Calhoun Cycle 15 MOC 10 5 Hours - asetest CALE ID 4 b 10.5-J PDIL CAE8 J - 20% POWER. BANt! 3 AT $74 XPO e 10 $00 GWD/MT. EBAR e 16.119 GWD/KT, POWEN e 20.006. FwW = 100.009 NOTbff a 24164. 3TEPS INSEPTED, FQ s 2.628, F-DELTA-M a 1,890 INCOP.E ASI * ,2D58, PER1PHERAL ASI e ,1549 TO7AL REIATIVE EXCOPE SICNAL = .4147 1 FUEL TVPB s TYPE 1 2D PIN POWER $ F0R AJSEMBLY 11. SERIAL NUMBER OMS 009 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1,2751 1.1590 1.3745 1.2890 1,3789 1.1904 1.3792 1.3812 1.3958 1.3870 1.2991 1.3883 1.1739 1.2974 2 1.1801 1.4096 1.3110 1.4196 1.3S44 1.4022 1.3969 1.3982 1.4054 1.3590 1.4264 1.3198 1.4212 1.198%

3 1.4253 1.3350 ---- ---- 1.4760 1.4697 1,4369 1.4376 1.4713 1.4784 ---- --- 1.3439 1.4433 4 1.3605 1.4709 ----

--- 1.3998 1.4991 1.4784 1.4786 1.4993 1.4000 ---- ---- 1.4764 1.3730 5 1.4799 1.4265 1.5262 1.4224 1.$445 1.$342 1.5257 1.5254 1 5314 1.5632 1.4209 1.5252 1.4280 1.4885 6 1.4162 1.4992 1.5420 1.5455 1.5565 1.5887 1.4369 1.4342 1.5873 1.5541 1.5422 1.5386 1.4971 1.5196 7 1.5272 1,$139 1.5211 1.5435 1.5672 1.4549 - - - - --- 1.4534 1.5646 1.5393 1.5217 1.5084 1.5250 8 1 $468 1.$116 1.5437 1.S$95 1.ts14 1.4722 --*- ---- 1.4704 1.5801 1.5542 1.5365 1.5213 1.5404 9 1.5784 1.5569 1.5980 1.$995 1.6092 1.6429 1.4899 1.4894 1.6407 1.6049 1.5927 1.5889 1.5466 1.5699 s to 1.5846 1.5232 1.6233 1.5105 1.6567 1.6236 1.6168 1.6166 1.4212 1.6518 1.$034 1.4132 1.S122 1.5750 11 1.5002 1.6136 ---- --- 1.$216 1.62S7 1.6044 1.6038 1.6231 1.5168 - ~ ~ ---- 1.6019 1.4907 ,

12 1.6179 1.$091 ----

-- - 1.6473 1.6364 1.5995 1 5985 1.6336 1.6424 .--- -~~~ 1.4986 1.6078 13 1.3857 1.6462 1.5250 1.6426 1.5624 1.6109 1.6006 1.5990 1.6075 1.5573 1.6.55 1.516) 1.6351 1.1763 14 1.5585 1.4152 1.6700 1.5602 1.6601 1.6653 1.6394 1.6366 1.6596 1.6528 1.S$19 1.6591 1.4037 1.S439 FUEL TYFE i TYPEl ANUSTED 2D FIN POWERS FOR ASSEMBLY 11. SE71A1. NLMBER OMS 009 (INCLUDES CRID DIP FAC70R OF 1.007S) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.2800 1.15R6 1.3741 1.2887 1.3844 1.3980 1.3871 1.3891 1.4012 1.3919 1,2976 1.390$ 1.171N 1.3009 2 1.1800 1.4129 1.3110 1.4247 1.1654 1.4093 1.4052 1.4064 1.4121 1.1592 1.430$ 1.3183 1.4253 1.1915 3 1.4300 1.3355 ~~ - - - - 1,4832 1.4782 1.4466 3.4473 1.4795 1.4850 --~ +- 1.1434 1.4480 4 1.3417 1.4777 ---- ---- 1.4025 1.508J 1.4886 1.4688 1.5082 1.4022 ---- ---- 1.4828 1.3747

$ 1.4884 1.4294 1.53S3 1.4260 1.$735 1.$44S 1.5358 1.3356 1.$418 1.S722 1.4242 1.5341 1.4313 1.4985 6 1.5278 1.5098 1,5535 1.5567 1.5679 1.S989 1.44C8 1.4400 1.5977 1.5659 1.5539 1.$507 1.$089 1.5338 7 1.5398 1.5267 1.5408 1.S567 1.5795 1.4597 -- + - -

1.4385 1.5776 1.5536 1.5168 1.5232 1.$410 8 1.5603 1.5452 1.S583 1.5736 1.5967 1.4783 ---- - ~* 1.4769 1.$945 1.5700 1.5513 1.5399 1.5583 9 1.5925 1.5700 1.6121 1.613$ 1,6238 1.6566 1.4973 1,4969 1,6S$4 1.6211 1.6090 1.6061 1.5637 1.5897 10 1.S971 1.5102 1.6369 1.$183 1.6708 1.639$ 1.6330 1,6332 1.6184 1.6682 1.5138 1,6308 1.5238 1.5944 y 11 1.5061 1.6261 --- ---- 1.$304 1.6424 1.6327 1.6228 1.6415 1.9281 - -- ---- 1.6208 1.5042 ,i 12 1.6295 1.S161 ---- ---- 1.6635 1.4546 1.6197 1.6194 1.4540 1.6621 - - - -- 1.$126 1.4294 13 1.3921 1.6589 1.5333 1.6580 1.$712~ 1.6296 1.6215 1.6237 1.6287 1,$719 1.6568 1.S114 1.6570 1.3923 14 1 $137 1.4240 1.6H&1 1.5714 1 6798 1.6883 1.6633 1.6612 1.6852 1.6770 1.5688 1.6835 1,4210 1.$712 {

MAXIMUM 20 DNE PIN PnWirP = 1.6693 AT RN 14 COLU)cJ 6 {

MAXIMUM 2D ONE FIN POWEP W/UNC = 1.9129 (1.6883 X 1 1000 X 1.0300)

MAXIM'FM CHANNEL POWEN = 1,6507 AT ROW 13 COLJMN 6 MAXIMUM 3D ONE PIN POWER = 2.2662 AT POW 14 COLUMN 6 (INCLUDES GPID DIP FACTOR OF 1.00755 i MAXIMUM 3D ONE PIN POWER W/UNc = 2.5676 12,2662 X 1.1000 X 1.03001 MAXIMUM LHOR e 13.$970 FW/PT (2.2662 X 6.00001 MAXIM'.fM LMGR W/UNCERTAltf1'Y e 16.1849 kW/FT (2.5676 X 6,0000 X 1.0300 X 1.02006 6 PL TO 15.00 EW/PT W/O UNC = 113.1475 ( 15.00 1 200.00./(13.5970 K ,9750)I PL 70 1$.00 FW/FT W/UNC ERTAINTY

  • 92.0 % 6 ( 15,00 X 100.00 /136.1849 x .97501 - 3.0000)

ASSEMBLY AX1AL SHAPE INLEX * ,1730 AMEMBLY A11 AL Sl*. APE INDEX W/UNCe .1330

{

NORMALIM.D ASSEMBLY AXI AL POWER SHAPE)

NOCE 1 . 2 3 4 5 6 7 #

AX1AL POWER 6558 1.0203 1.2091 1.3167 1.3371 1,3422 1.2797 1.2230 NODE 9 10 11 12 13 14 15 16

  • AXIAL POWrn 1.1226 1.0507 .9581 .9974 .8151 .7411 ,6104 .4206 L

t e

t a

- ASAS Manual hvision 0 82 April 19,1994 w -.--------__.-,e . * - , . .

~n - ne . ,n,., ~ .-- y

i Figure 13 Sample User Output File  ;

Page 30 of 37 l 1 PROGRAM ASAS VERSION 1, REV DATE 4/12/94. TODAY'S DATE IS 04/12/94 TNE TIME IS 08:19:49 PAGE 30 A CODE TO CREATE HOT CHANNEL DATA FILES FROM A SIFJLATE-3 PIN FILS PIN FILE NAME : / RPG3 / SplOPPD/ s 30t est . p PUN TITLE  : Fort Calhoun Cycle 15 BOC 10.5 Hours - asatest CASE ID 4 8-10.5-J PD1b CASE J - 20% POWER, BANK 3 AT 574 KPO e 10.500 GWD/prr, EaAR = 16.119 GWD/MT. POWER = 20.00%. FLOW = 100.004 NO1VT = 24164 STEPS INSKFTEu. FQ

  • 2.628 F-DELTA-H = 1.890, INCORS ASI = .2052, PERIPHERAL ASI = .1549 T(ffAL RELATIVE EXCORI SIGNAL * .4347 FUEL TYPE : TYPE 1 FIN POWERS FCR LIMITING LHGR PLANE 5 FOR ASSEMBLY 18. SERIAL IfJMBER OMS 027 1 2 3 4 5 6 7 8 9 10 11 12 13 . 14 1 1.9280 1.7309 7.98:7 1.9387 2.0812 2.1058 2.0958 3.1031 2.1246 2,1089 1,9722 2.1242 1.7685 1.9607 2 1.7613 2.1182 1.9175 2.0735 2.0134 2.1049 2.1018 2.1083 2.1226 2.0404 2.1106 1.9586 2.1645 1.7874 3 2.1371 1.9345 ---- ---- 2.1289 2.1749 2.1384 2.1448 2.1940 2.1596 ---- ---- 1.9817 2.1721 4 1.9997 2.1020 ----

1.9881 2.1894 2.1712 2.1776 3.2100 2.0196 ---- - -- 2.1590 2.0385 5 2.1511 2.0462 2.1445 1.9933 2.2446 2.2132 2.2089 2.2154 2.2349 2.2820 2.0394 2.2047 2.1069 2,1997 6 2.1744 2.1409 2.1940 2.1984 2.2165 2.25?2 1.9989 2.0049 2.2812 2.2536 2.2500 2.2576 2.2084 2.2321 7 2.1505 2.1355 2.1590 2.1831 2.2155 2.0019 ---- - -- 2.0191 2.2494 2 2316 2.2206 2.2061 2.2213 8 2.1502 2.2367 2.1614 2.1865 2.2197 2.0068 ---- ---- 2.0246 2.2542 2.2356 2.2237 2.2082 2.2222 9 2.1759 2.1469 2.2031 2.2097 2.2295 2.2737 2.0129 2.0197 2.2970 2.2683 2.2634 2.2693 2.2175 2.2375 10 2.1557 2.0570 2.1601 2,0114 2.2670 2.2371 2.2338 2.2412 2.2605 2.3070 2.0609 2.2247 2.1229 2.2102 11 2.0079 2.1179 ---- ---- 2,0170 2.2231 2.2060 2.2130 2.2457 2.0518 ---- ---- 2.1817 2.0538 1 12 2.1508 1.9546 ---- -- - 2.1683 2.2186 2.1832 2.1897 2.2398 2.2032 ---- ---- 2.0091 2.1938 13 1.780D 2.1461 1,9496 2.1147 2.0593 2.1565 2.1551 2.1612 2.1757 2.0900 2.1573 1.9972 2.1999 1.8118 14 1.961? 1.7606 2.1217 1.9827 2.1344 2.1639 2.1538 2.1596 2.1816 2.1630 2.0188 2.1679 1.8010 1.9959 F2 FACTORS FOR ASSEMBLY 18, SERIAL NUMBER OM5027 1 2 3 4 5 6 7 8 9 10 il 12 13 14 .

I 1.3606 1.3562 1.1631 1.3609 1.3707 1.3752 1.3785 1.3810 1.3825 1.3826 1.3772 1.3840 1.3805 1.3899 2 1.3568 1.3621 1.3609 1.3697 1.3677 1.3779 1.3820 1.3846 1.3855 1,3802 1.3871 1.3831 1.3891 1.3876-3 1.3447 1.3618 --+- ---- 1.3778 1.3821 1.3863 1.3890 1.3903 1.3915 ---- ---- 1,3910 1.1991 4 1.3634 1.3715 - -- ---- 1.3760 1.3858 1.3905 1.3934 1.3947 1.3908 ---+ - -- 1.4036 1.4009 5 1.3741 1.3706 1.3799 1.3771 1.3856 1.3902 1.3934 1.3966 1.3999 .1.4019 '1.3996 1.4089 1.4056 1.4154 4 1.3797 1.3818 1.3852 1.3879 1.3912 1.3933 1.3904 1.3939 1.4040 1.4091 1.4127 1.4169 1.4203 1.4248 7 1.3840 1.3870 1,3904 1.1937 1.3956 1.3914 ---- ---- 1.4033 1.4152 1.4209 1.4251 1.4289 1.4331 8 1.3873 1.3906 1.3942 1.3977 1.3999 1.3961 ---- ---- 1.4091 1.4214 1.4276- 1.4322 1.4364 1.4408 9 1.1897 1.3926 1.3968 1.4003 1.4046 1.4076 1.4058 1.4104 1.4218 1.4281 1.4330 1.4384 1.4429 1.4483 10 a 3908 1.3884 1.3992 1.3977 1.4079 1.4141 1.4191 1.4241 1.4295 1.4336 1.4333 1.4448 1.4434 1.4552 11 1.3865 1.3966 ---- ---- 1.4070 1.4192 1.4263 1.4318 1.4359 1.4348 ----

1.4572 1.4574 12 1.3945 1.J938 ---- ---- 1.4178 1.4249 1.4321 1.4380 1.4430 1.4480 ---- ---- 1.4602 1.4733 13 1.3926 1.4014 1.4030 1,4150 1.4161 1.4300 1.4376 1.4440 1.4495 1.4485 1.4609 1.4622 1.4747 1.4799 14 1.4043 1.4018 1.4128 1.4140 1.4279 1.4365 1.4438 1.4505 1.4571 1.4627 1.4634 1.4777 1,4824 1.5026 ASSEMBLY AX1AL FEAK!NG FACTOR e 1.4075 (FROM 16 Pl.ANE DATA) l-ASAS Manual Revision o 83 April 19,1994

Figure 13 Sample User Output File  :

Page 31 of 37 1 PRCGtAM ASAS VERSION 1, REY DATE 4/12/94. TODAY'S DATE IS 04/12/94, THE TIME IS 08:19149 PAGE 31 A CODE TO C7J. ATE MOT CHANNEL DATA FILES FROM A $1rJ1 ATE-3 FIN FILS PIM FILE NAME a /RPG3/Sp/GPPD/m30 test.p PUN TITLE i Fort Calhoun Cycle 15 Bac 10.5 Hours - esatest CASE ID i B 10.5-J PDIL Casa J + 20% POWER, BANK 3 AT 574 XPO

  • 10.500 GWD/MT, EBAR = 16.119 GWD/MT. POWER = 20,00%. F14W = 100.006 NOTWr a 24164. STEPS INSERTED, FQ = 2.628. F-DELTA-H = 1.890, INCORE ASI = .3058. PERIPHERAL ASI = .1549 TOTAL PELATIVE EXCORE SIGNAL = .4347 FUEL TYPE TYPE 1 2D PIN FCWERS FOR ASSEMBLY 18. SERIAL NUMBER OMS 027 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.4173 1.2770 1.5271 1.4245 1.5184 1.5311 1.5204 1.5229 1.5367 1.5253 1,432D 1.5349 1.2810 1.4107 2 1.2988 1.5551 1.4089 1.5139 1.4722 1.5276 1.5208 1.5226 1.5320 1.4784 1.5215 1.4161 1.55a2 1.2881 3 1.5660 1,4206 ----

1.5451 1.5736 1.5425 1.5441 1.5781 1.5520 ---- ---- 1.4246 1.5525 4 1.4667 1.5326 ---- ---- 1.4449 1.5800 1.5615 1,5628 1.5846 1.4521 ---- ---- 1.5381 1.4551 5 1 5654 1.4930 1.5541 1 4475 1.6199 1.5920 1.5852 1.5863 1.5964 1.6278 1.4571 1.5649 1.4990 1.5541 6 1.5760 1.5494 1.5839 1.5840 1.5932 1.6215 1.4377 1.4383 1 6248 1.5993 1.5926 1.5933 1.5549 1.5666 7 1.5538 1.5396 1.5527 1.5665 1.5875 1.4387 ----

1.4388 1.5895 1.5706 1 5582 1.5439 1.5500 8 1.5499 1.5)66 1.5502 1,5643 1.5856 1.4374 ---- - - - 1,4368 1.5859 1.5660 1.5536 1.5373 1.5423 ,

9 1.5657 1.5437 1 5773 1.5780 1.5813 1.6153 1.4319 1.4320 1.6156 1.5883 .1.5795 1.5776 1.5369 1.5449 10 1.5500 1.4816 1.5439 1.4391 1.6102 1.5819 1.5741 1.5737 1.5812 1.6093 1.4179 1.5398 1.4708 1.5188 11 1 4482 1.5165 --

1.4335 1.5665 1.5467 1.5457 1.5640 1.4300 ----

1.4972 1.4092 12 1.5423 1.4023 -- - - - 1.5294 1.5569 1.5245 1.5227 1.5522 1.5215 ---- ---- 1.3759 1.4890 11 1.2781 1.5314 1.3897 1.4945 1.4541 1.5081 1.4991 1.4966 1.5012 1.4428 1.4767 1.3659 1.4917 1,2242 i 14 1.3969 1.2560 1.5018 1.4021 1.4948 1.5064 1.4918 1.4888 1.4972 1.4787 1.3795 1.4670 1.2150 1.3283 FUEL TYPE . TYFE1 ,

AIA7USTED 2D PIN POWERS FOR ASSEMBLY 18. SERIAL NUMBER OMS 027 (INCLUDES CRID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3804 1.2398 1.4901 1.3877 1.4898 1.5074 1.5002 1.50%$ 1.5208 1.5096 1.4118 1.5206 1.2659 1.4035 2 1.2614 1.5163 1.3726 1.4843 1.4412 1.5061 1.5045 1,5091 1.5194 1.4606 1.5108 1.4020 1.5494 1.2795 3 1.5298 1.3848 ---- ---- 1.5239 1.5568 1.5307 1.5353 1.5705 1.5459 ----

1.4185 1.5548 4 1.4314 1.5046 ----

1.4232 1.5673 1.5542 1.5588 1.5819 1.4457 ----

1.5454 1.4592 5 1.5398 1.4647 1.5351 1.4268 1.6067 1.5843 1.5812 1.5858 1.5998 1.6335 1.4598 1.57F2 1.5082 1.5746  ;

6 1.5565 1.5325 1.5705 1.5736 1.5866 1.6172 1.4309 1.4351 1.4329 1.6132 1.6106 1.6161 1.5808 1.5978 7 1.5394 1.52R6 1.5455 1.5627 1.5P59 1.4330 ----

1.4453 1.6102 1.5975 1.5896 1.5792 1.5901 N 1.5391 1.5295 1.5472 1.5652 1.5889 1.4365 ---- ---- 1.4492 1.6136 1.6003 1.5918 1.5807 1.5907 9 1.5576 1.5.368 1.5710 1.5818 1.5959 1.6276 1.4409 1.4458 1.6442 1.6237 1.6202 1.6244 1.5871 1.6016 10 1.5431 1.4725 1.5462 1.4398 1.6228 1.6013 1.5990 1.6043 1.6181 1.6514 1.4752 1.5925 1.5196 1.5821 11 1.4373 1.5160 --- ---- 1.4438 1.5914 1.5791 1.5841 1.6075 1,4687 e--- ---- 1.5617 1.4701 12 1.5396 1.3991 ---- ---- 1.5521 1.5881 1.5628 1.5674 1.6013 1.5771 ---- ---- 1.4382 1 5704 13 1.2741 1.5363 1.3956 1.5117 1.4741 1.5437 1.5427 1.5470 1.5574 1.4961 1.5443 1.4297 1.5747 1.2969 14 1.4043 1.2603 1.5188 1.4192 1.5279 1.5490 1.5417 1.5459 1.5616 1.5483 1.4451 1.5524 1.2892 1.4287 MAKfMUM 2D ONE PIN POWER = 1.6514 AT row 10 COLUMN 10 MAXIM'tM 2D ONE PIN POWER W/UNC e 1.8711 (1.6514 X 1.1000 X 3.0300)

MAXIMUM CHANNEL PCWER e 1.6344 AT $ TOW 9 COLUMN 9 MAXIMUM 3D ONE FIN POWER = 2.3244 AT POW 10 COLUMN 10 (INCLUDE $ GRID D1P FACTOR OF 1.0075)

MAXIMUM 3D ONE PIN l'OWF.R W/UNC = 2.6335 (2,3244 X 1.1000 X 1.03001 4 MAXIMUM LMGP a 13.9461 FW/FT (2.3244 X 6.00001 MAXIMUM LNGR W/UNCFRTAINTY a 16.6005 FWtrT (2.6335 x 4.0000 X 1.0300 X 1.02001 PL TO 15.00 FW/FT W/O UNC = 110,3148 ( 15.00 X 100.00 /(13.9461 X .9750):

l'L TO 15.00 FWIFT W/UNCEPTAINTY a 89.6758 1 15.00 X 100.00 /(16.6005 x .97501 - 3.0000)

ASSEM9LY AX1AL SKAPE INDEX e .2286 ASSEMBLY AXIAL SHAPE INDEX W/UN~s .1886 NORMAL 11ED ASSEMRI.Y AX1AL POWER $ RAPE:

M3DE 1 2 3 4 $ 6 7 8 AXIAL F-OWER .7181 1.09a8 1.2884 1.3935 1.4075 1.4007 1.3108 1.2109 HODE 9 10 11 12 13 14 15 16 AX1AL POWEP 1.0719 .9802 .8845 .8258 .7513 .6869 .5712 .3996 i

ASAS Manual Revision 0 84 April 19,1994 - l r

Figure 13 Sample User Output File Page 32 of 37 1 PROGRAM ASAS VERSION 1. REV LATE 4/12/94. TODAY'S DATE IS 04/12/94. THE TIME IS 08:19:49 PACE 32 A CODE TO CREATE NOT CHANNEL LATA FILES FROM A SIMULATE-3 FIN FILE PIN FILE NAME o iRPG3/Dp/OPPD/s30 test.p RUN TITLE i Fort Calhoun Cycle 15 BOC 10.5 Mours - esatest CASE ID B-10.5-J PDIL CASE J - 20t POWER. BANK 3 AT 574 XPo = 10.500 GWD/MT. EBAR = 16.119 GWD/prT. POWER s 20.004. Flow = 100.004 NOTW't

  • 24164. STEPS INSERTED, FQ = 2.628. F-DELTA H e 1.890 INCORB A31 e .2058, PERIPHEPAL AS1 m .1549 TCFTAL PELATIVE EXCORE SIGNAL = .4347 FUEL TYPE : TYPE 2 PIN POWEPS FOR LIMITING 1RGR PLANE 6 FOR ASSEMBLY 10,5ERIAL NUMBER OMR013 1 2 3 4 5 6 7 8 9 to 11 12 13 14 1 .9444 1.0061 1.1620 1.2274 1.2709 1.3071 1.3497 1.3982 1.4676 1.5484 1.6263 1.6752 1.5703 1.6201 2 9316 1.1069 1,1584 1.2360 1.3058 1.3172 1.3451 1.3904 1.4746 1.5879 1.6433 1.6784 1,7549 1.6190 3 1.0229 1.0997 ---- - -- 1.3211 1.3574 1.3745 1.4199 1.5217 1.6144 ---- ---- 1.7473 1.7984 4 1.0443 1.1312 ---- ---- 1.3521 1.3953 1.4183 1.4645 1.5632 1.6504 - -- - - - - 1.7913 1.8291 5 1.0585 1.1648 1.2373 1.3138 1.4073 1.4351 1.4900 1.5453 1.6030 1.7077 1.7336 1.7758 1.8198 1.8330 6 1,0762 2.1549 1.2455 1.3262 1.4028 1.5033 1.5482 1.6130 1.6752 1.6869 1.7287 1.7634 1.7827 1 8367 7 1.1093 1.1674 1.2429 1.3251 1.4298 1.5190 ---- ---- 1.6964 1.7111 1.7081 1.7358 1.7778 1.8601 ,

8 1.1473 1.2043 1.2794 1.3618 1.4692 1.5628 ---- ---- 1.7474 1.7547 1,7473 1.7714 1.8097 1.8949 9 1.1932 1.2737 1.3685 1.4495 1.5232 1.6229 1.6659 1.7367 1.7898 1.8021 1,8415 1.8706 1.8818 1.9368 10 1.2624 1.3764 1.4533 1.5297 1.6206 1.6321 1.6785 1.7364 1.7938 1.9056 1.9271 1.9611 1.9886 2,0023 11 1.3414 1.4344 ----

1.6482 1.6736 1.6767 1.7262 1.8291 1.9224 ~~-- ---- 2.0386 2.0673 12 1.4101 1.48R7 ---- ---- 1.6993 1.1146 1.7092 1.7531 1.8601 1.9576 ---- ---- 2.0496 2.1006 13 1.3660 1.5923 1.6326 1.7071 1.7654 1.7500 1.7625 1.8027 1,8824 1.9957 2.0494 2.0592 2.1346 1.9380 14 1.4645 1.5245 1,7270 1.7842 1.8096 1.8303 1.8682 1.9140 1.9650 2.0372 2.1059 2.1376 1.9626 2.0263 FZ FAC'PDPS FOR ASSEMBLY 10 SERIAL N'JMPER CMP 01) .

1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3102 1.3130 1.3121 1.3140 1,3166 1.3189 1.3203 1.3219 1.3229 1.3236 1.3245 1.3256 1.3301 1.3284 2 3,3111 1.3104 1.3103 1.3121 1.3167 1.3204 1.3218 1.3228 1.3241 1.3247 1.3241 1.3264 1.3276 L1.3311. ,

3 1.3084 1.3086 ---- ---- 1.3145 1.3196 1.3237 1.3229 1.1234 1.3230 ---- ---- 1.3280 1.3284 4 1.3089 1.3090 ---- ---- 1.3145 1.3198 1.3226 1.3228 1.3236 1.3230 . ---- ---- 1.3278 1.3292 5 1.3106 1.3125 1.3119 1.3133 1.3170 1.3209 1.3216 1.3228 1.3243 1.3248'1.3252 1.3271 1.3305 1.3305 6 1.3124 1.3156 1.3163 1.3179 1.3201 1.3203 1.3166 1.3211 1.3249 1.3266 1.3280 1.3298 1.3320 1.3319 7 1.3136 1,3166 1.3190 1.3201 1.3202 1.3180 ---- ---- 1.3231 1.3270 1.3292 1.3313 1.3328 1.3327 8 1.3156 1.3181 1.3203 1.3212 1.3219 1.3206 ---- -- - 1.3256 1.3288 1.3306 1.3322 1.3336 1.3340 9 1.3164 1.3193 1.3200 1.3215 1.3236 1.3243 1.3231 1.3254 1.3289 1.3297 1.3310 1.3325 1.3347 1.3344 10 1.3175 1.3197 1.3191 1.3204 1.3235 1.3265 1.3272 1.3284 1.3295 1.3298 -1.3312 1.3324 1.3358 1.3354 il 1.318a ,1.3193 --, - +- 1.3235 1.3275 1.3297 1.3302 1.3306 1.3310 +--- ---- 1.3347 1.3353 12 1.3206 1,3213' ---- ---- 1.3253 1.3290 1.3318 1.3318 1.3321 1.3322 -*-- ---- 1.3368 1.3365 13 1.3252 1.3237 1.3242 1.3253 1.3288 1.3313 1.3326 3.3333 1.3343 1.3355 1.3345 1.3367 1.3.169 1.3401 14 1.3246 1.3276 1.3259 1.3273 1.3291 1.3308 1.3323 1.3339 1.3342 1.3351 1.3350 1.3364 1.340D 1.3386 ASSEMBLY AXI AL PEAFING FACTOR e 1.1260 {FROM 16 PLANE CATAl Y

ASAS Manual Revision o 85 April 19,1994 -

(

Figure 13 Sample User Output File Page 33 of 37 1 PROGFAt; ASAS VERSION if REV LAT6 4/12/94. TODAY'S DATE 18 04/12/94. THE TIME IS 08:19:49 PACE 33 A COLE '19 CREATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN F11.E MAME i / RPG3 /Sp/OPPD/e 30t est . p RUN TITLE  : Fort Calhoun Cycle 15 BOC 10.5 Hours - esatest CASE ID s B-10.5 J PDIL CASE J - 20% PCWEA. DANK 3 AT 574 XPO e 10.500 GWD/MT, EBAR

  • 16.119 GWD/pfr. POWER = 20.004, FIDa a 100.009 NCP!WT = 24164. STEPS INSERTED. FQ s 2.628, F-DELTA-H e 1.890, INCORE AS! a .2058 PERIPHERAL ASI = .1549 1VTAL PELATIVE EXCORE SIGNAL e ,4347 FUEL TYPE : TYP22 2D P1h POWEPS FOR ASSEMBLY 10. SERIAL NUMBEP OMR013 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 .7208 .7662 .8856 .9341 .9653 .9910 1.0222 1.0577 1.1093 1.1699 1.2279 1.2631 1.1806 1.2196 2 .7106. .8447 .8841 ,9419 .9917 .9976 1,0176 1.C511 1.2137 1.1986 1.2410 1.2653 1.3218 1.2163 3 7818 .8404 ----

-- - 1.0051 1.0286 1.0391 1.0733 1.1498 1.2202 ---- ---- 1.3157 1.1539 4 .7980 .8642 ----

1.0286 1.0572 1.0724 1.1087 1.1811 1.2415 ---- ---- 1.3491 1.J761 5 .8076 .4815 .9431 1.0003 1.0685 1.0865 1.1274 1.1682 1.2104 1.2891 1.3082 1.3380 1.3677 1.3177 6 .8201 .8779 .9462 1.0063 1.0627 1.1386 1,1741 1.2210 1.2644 1.2716 1.3017 1.1260 1.3383 1.3790 7 .8444 .8867 9423 1.0038 1.0830 1.1525 ----

- - - - 1.2821 1.2894 1.2850 1.3018 1.3339 1.3957 8 .8720 .9137 .9691 1<0307 1.1115 1.1834 ---

1.3182 1.3206 1.3131 1.3296 1.3570. 1.4204 9 .9064 .9655 1.0368 1.0969 1.1508 1.2255 1.2591 1.3103 1.3468 1.3552 1.3836 3.4038 1.4098 1.4514 10 .9581 1.0430 1.1017 1.1585 1.2245 1.2304 1.2647 1.3072 1.3492 1.4329 1.4477 1.4718 1.4887 1.4994 11 1 0171 1.0872 +---

1.2454 1.2607 1.2610 1.2977 1.3744 1.4443 ----

1.5274 1.5482 12 1.0678 1.1267 ---- - -- 1,2823 1.2901 1.2834 1.3164 1.3963 1.4695 ---- ---- 1.5332 1.5717 13 1.0307 1.2029 1.2129 1.2882 1.3286 1.3146 1.3226 1.3521 1.4107 1.4944 1.5358 1.5405 1.5967 1.4462 14 1.1056 1.1483 1.3025 1.3442 1.3615 1.1753 1.4022 1.4348 1.4728 1.5258 1.5774 1.5996 1,4646 1.5137 FUEL TYPE r TY F'E 2 A!MUSTED 2D PIN POWERS FOR ASSEMBLY 10 SERIAL NUMBER OMR013 (INCLUDES CRID DIP FAC19R OF 3.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 7175 .7644 .8829 9326 .9656 .9911 1.0255 1.0623 1.1150 1.1765 1.2356 1.2728 1,1931 1.2 M J 2 .7079 .8410 .8801 .9391 .9922 1.0008 1.0220 1.0564 1.1204 1,2065 1.2486 1.2752 1.3333 1.2301 3 .7772 .9356 ----

-*-- 1.0038 1 0313 1.0441 1.0789 1.1562 1.2266 - -- ---- 1.3276 1.3664 4 .7936 .8595 ----

+-+- 1.0273 1.0601 1.0776 1.1142 1.1877 1.2539 ----

1.3610 1.3897 c 5 .8042 .8850 .9400 .9982 1.0692 1.0904 1.1321 1.1741 1.2179 1.2975 1.3172 1.3492 1.3827 1.3927

  • 6 8177 .4775 .9463 1.0076 1.0658 1.1422 1.1763 1.2256 1.2728 1.2817 1.3134 1.3?98 1.3544 1.3955 ,

7 .8428 .8870 .9444 1.0068 1.0864 1.1541 ---- ---- 1.2889 1.3001 1,2978 1.3188 1.3508 1.4131 8 .8717 .9150 .9721 1.0346 1.1163. 1.1874 --

1.3276 1.3332 1.3276 1.3459 1.3750 1.4397 9 .9066 .9678 1.0398 1.1013 1.1573 1.2331 1.2657 1.3195 1.3599 1.3692 1.3991 1.4213 1.4297 1.4715 10 .9591 1.0458 1.1042 1.1623 1.2313 1.2401 1.2753 1.3193 1.3629 1.4478 1,4642 1.4900 1.5109 1.5213 i 11 1.0192 1.C898 ----

1.2523 1.2714 1.2739 1.3116 1.3897 1.4606 ----

1-5489 1.5707 12 1.07)4 .1.1311 ---

1.2911 1.3027 1.2987 1.3320 1.4133 1.4874 ---

1.5572 1.5960 13 1.0* 18 1 2098 1.2404 1.2972 1.3413 1.3297 1.3391 1.3696 1.4302 1.5163 1.5571 1.5645 1.6218 1.4725 14 1.1127 1 1583 1.3121 1.3556 1.3749 1.3907 1.4195 1.4542 1.4930 1.5478 1.6001 1.6242 1.4911 1.5396 MAXIMUt 2D ONE PIN POWER = 1.6242 AT ROW 14 COLUMN 12 MAXIMt'.4 2D ONE FIN POWER W/UNC = 1.8402 11.6242 X 1.2000 X 1.0300)

MAXIDTJH CHANNEL POWER e 1.5865 AT ROW 13 COLUMN 11 MAXIIUM 3D ONE PIN POWER = 2.1537 AT ROW 14 COLUMN 12 11NCLUDES CR1D DIP FACTQR OF 1.0075)

MAXID.UM 3D ONE FIN POWER W,UNC a 2.4401 (2.1537 X 1.1000 X 1.0300s MAXIMUM LH7R

  • 12.9221 FW/FT (2.1537 x 6.0000)

MAXIMUM LHGR W/UNCEPTA!!rrY a 15.3815 FW/FT 12.4401 X 6.0000 x 1.0300 X 1.0200)

PL TO 16.00 FW/FT W/O UNC = 126.9941 t 16.00 X 100.00 /t12.9221 X .97501)

PL TO 16.00 EWr PT W/UNCEPTAINTY

  • 103.6882 ( 16.00 X 100.00 /(15.3815 X .97501 - 3.0000) >

ASSEMBLY AX1AL SHAPE INDEX * .1607 '

ASSEMBLY AX1AL SHATE INDEX W/UNC= .1207 NOPMALIZED ASSEMDLY AX1 AL KMER SHAPE:

~

I NOL1 1 3 4 5 6 7 8 l

AXI AL PCMFR .6389 1.0164 1.1960 1.2977 1.3193 1.3260 1_2709 1.2205 NODE 9 10 11 12 13 14 15 16 AXI AL MMEP 1.1288 1.0611 .9725 .9126 8325 .7600 .6288 .4178 l

ASAS Manual Revision 0 86 April 19.1994 I 1

Figure 13 Sample User Output File Page 34 of 37 1 PROGRAM ASAS VERSION 1. PEV DATE 4/12/94. TODAY'S DATE IS 04/12/94. THE TIME IS 08:19:49 PAGE 34 A CODE TO CPEATE HOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE PIN FILE NAME : /RPG3/Sp/OPPD/m30 test.p RUN TITLE i Fort Calhoun Cycle 15 BOC 10.5 Hours - asatest CASE ID Bs10.5-J PDIL CASE J - 20% POWER, BANK 3 AT 574 XPO = 10.500 CWD/M. EBAR = 16.119 GWD/MT, POWER = 20.000 FIiM a 100.004 Nr/TW

  • 24164. STEPS INSERTED, FQ = 2.628. F-DELTA-N a 1.890, INCOP.E ASI * .2058, PERIPHERAL ASI = .1549 TOTAL RELATIVE EXCCRE SIGHAL * .4347 i FUEL TYPE e TYPE 2 P!N POWERfl FOR LIMITING LNGR P1ANE 4 FOR ASSD!BLY 39. SERIAL NUMBER OM5026  ;

1 2 3 4 5 6 7 8 9 10 il 12 . 13 14 .

1 1.1476 .9643 1.0808 1.0040 1.1250 1.1944 1.2117 1.2117 1.1944 1.1250 1.0040 1.0808 .9643 1.1476 2 .965) 1.0000 .7445 .7813 .9199 1.0795 1.1305 1.1305 1.0795 9199 7813 7445 1.0000 .9653 3 1.0830 7452 ---- ---- 7638 1.0097 1.0727 1.0727 1.0097 .7638 ---- ---- 7452 1.0830 4 1,0068 .7827 ---- .--- .6909 .9584 1 0151 1.0151 .9584 6909 ---a ---- 7827' 1.0068 5 1.1287 .9221 .7649 .6913 .8792 .9233 .9309 .9309 .9233 ..8792 .6913 7649 .9221 1.1287 6 1.1985 1.0824 1.0116 .9595 .9238 .8571 .6515 .6515 .8571 .9238 .9595 1.0116 1.0824 1.1985 7 1.2158 1.1337 1.0749 1.0165 .9317 .6517 ---- ----

.6517 9317 1.0165 1.0749 1.1337 1.2158 8 1.2158 1.1337 1.0749 1.0165. ,9317 .6517 - ---- .6517 ..9317 1.0165 1.0749 1.1337 1.2158 9 1.1985 1.0824 1.0116 .9595 .9238 .8571 .--

6515 .6515 .8571 .9238 .9595 1.011A 1.0824 1.1985 e 10 1<1287 .9221 7649 .691) .8792 .9233 .9109 .9309 .9233 8792 .6913 .7649 .9221 1.1287 11 1.0068 .7827 ---- ----

.6909 .9584 1.0151 1.0151 .9584 ..6909 ---- ----

7827 1.0068 12 1.0830 7452 ---- ----

.7638 1.0097 1.0727 1.0727 1.0097 .7638 ---- ---- 7452 1.0830 13 .9653 1.0000 744% ,7833 .9199 1.0795 1.1305 1,1305 1.0795 .9199 7813 .7445 1.0000 .9653 14 1.1476 .9643 1.0808 1.004D 1.1250 1.1944 1,2117 1.2117 1.1944 1.1250 1.0040 1.0808 .9643 1.1476 FZ FACTORS FOR ASSEMBLY 39 SERIAL NUMBER OMS 026 1 2 3 4 5 6 7 8 9 to 11 12 13 14 1 3.5226 1.5100 1.5149 1.5094 1.5205 1.5250 1.5265 1.5265 2.5250 1.5205 1.5094 1.5149 1.5100 1.5226 2 1.5100 1.5089 1,4971 1.5039 1.5054 1.5185 1.5215 1.5215 1.5185 1.5054 1.5039 1.4911 1.5088 1.5100 3- 1.5149 1.4971 ---- ---- 1.5044 1.5145 1.5180 1.5180 1.5145 1.5044 ---- ---- 1.4971 1.$149 4 1.5095 1.5040 ---- - -- 1.4955 1.5115 1.5150 1.5150 1.5115 1.4955 ---- ---- 1.5040 1.5095 5 1.5206 1.5054 1.5044 1.4956 1.5065 1.5095 1.5101 1.5101 1.5095 1.5065 1.4956 1.5044 1.5054 1.5206 6 1.5251 1.5186 1.5145 1.5116 1.5095 1.5050 1.4921 1.4921 1.5050 1.5095 1.5116 1.5145 1.5186 1.5251 7 1.5266 1.5215 1.5181.1.5150 1.5101 1.4921 ---- ---- 1.4921 1.5101 1.5150 1.5181 1.5215 1.5266 8 1.5266 1.5215 1.5181 1.5150 1.5101 1.4921 ---- ---- 1.4921 1.5101 1.5150 1.5181 1.5215 1.5266 9 1.5251 1.5186 1.5145 1.5116 1.5095 1.5050 1.4921 1.4921 1.5050 1.5095 1.5116 1.5145 1.5186 1.5251 10 1.52c6 1.5054 1.5044 1.4956 1.5065 1.5095 1.5101 1.5101 1.5095 1.5065 1.4956 1.5044 1.5054 1.5206 11 1.5095 1.5040 ---

1.4955 1.5115 1.5150 1.5150 1.5115 1.4955 ---- ---- 1.5040 1.5095 12 1.5149 1.4971 ---- - -+ 1.5044 1.5145 1.51B0 1.5180 1.5145 1.5044 ---- ---- 1.4971 1.5149 ,

13 1.5100 1.5088 1.4971 1.5039 1,5054 1.5185 1.5215 1.5215 1.5185 1.5054 1.5039 1.4971 1.5089 1.5100 14 1.5226 1.5100 1.5149 1.5094 1.52C5 1.5250 1.5265 1.5265 1.5250 1.5205 1.5094 1.5149 1 5100 1.5226 .

ASSEMBLY AX1AL PEAEING FACTOR = 1.5115 (FROM 16 PLANE CATA)

P 4

e i

- r ASAS Manual Revision 0 87 April 19,1994

-r- --~r 4 t

)

l i

<a Figure 13 Sample User Output File Page 35 of 37 1 PPDGRAM ASAS VER$16N 1. REV DATE 4/12/94. TODAY'S DATE IS 04/12/94. THE TIME !$ 08:19:49 PAGE 35

& CODE TO CREATE HOT CHANNEL DATA FILES FROM A SINULATE-3 P!N FILE FIN FILE NAME a / 8 PG3 / Sp /OPPD/ s 30t es t . p RUN TITLE Fort Calhoun Cycle 13 BOC 10.5 Hours - asatest CASE 2D B-10.5-J PD1L CASE J - 20% POWER, BANK 3 AT 574 XPO = 10.500 ' GWD/ wr. EBAR = 16,119 GWD/MT. POWER = 20.006, FLOW

  • 100.004 MOWT= 24164. ETEPS INSFRTED. FQ = 2.628. F-r'ELT A-H w 1.890 INCORE AST = .2058 PERIPMERAL A51 e .1549 TUTAL RELATIVE EXCORE SIGNAL a ,4347 FUEL TYPE t TTPE2 2D PIN POWERS FOR A$$EMBLY 39 SERI AL NUMBER CHS026 3 2 3 4 5 6 7 8 9 10 11 12 13 14 1 7517 .6386 .7135 ,6652 .7399 .7832 .7937 .7937 .783i 7399 .6652 7135 .6386 7537 2 .6393 .6628 ,497) .5195 .6111 .7109 7431 7431 .7109 .6111 .5195 .4973 ,6628 .6393 3 7149 .4978 -- - ---- .5077 .6667 7067 7067 .6667 .5077 - - - ---- .4978 7149 4 .6670 .5204 ---- - -- .4620 .6341 .6700 .6700 .6341 .4620 ---- ---* .5204 .4670 5 7423 .6125 3 084 .4623 .5836 .6117 6165 .6165 .6117 .5816 .4623' .5084 .6125 7423 6 7859 .7128 .6679 .6348 .6120 .5695 .4366 .4366 .5695 .6120 6348 .6679 .7128 - 7859 7 1964 7451 7001 .6709 .6170 .4348 ~+' ----

.4368 .6170 .6709 .7081 7451 7964 8 7964 .7451 .1081 .4709 .4170 .4368 ---- ---- .4368 .6170 .6709. 7081 .7451 7964 9 .7859 7128 .6679 .6348 .6120 .5695 .4366 .4366 .5695 .6120 .6348 6679 .7128 ,7859 10 7423 .6125 .5084 .4623 .5836 .6117 .6165 6165 .6117 .5816 .4623 .5084 .6125 7423 13 .6670 .5204 ---- ---- .4620 .6141 .6700 .6700 .6341 .4620 *--- ---- .5204 .6670 12 .7149 .4978 - - - - ---- .5077 .6667 7067 7067 .6667 ,5077 ---- ---- .4978 . .7149 13 .6393 .6628 .4973 .5195 .6111 .7109 7431 7431 7109 .6111 .5195 .4973 .6628 .6393 14 s7537 .6386 7135 .6652 .7399 .7832 7937 .7917 .7812 .7399 .6652 .7135 .6386 7537 P'JEL TYPE 2 TYPE 2 AIATUSTED 2D FIN POWEPS FDP ASSEMBLY 39 SERIAL NUMBER CM5026 (INCLUDRS GPID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 _14 1 .7644 .6423 .7199 .66A8 7494 .7956 .8071 .8071 1956 7494 .6688 .7199 .6423 .7644 2 .6430 .6661 .4959- .5204 .612A 7190 7531 ,7531 .7190 6128 .5204 .4959 .6661 .6430 3 .7214 .4964 ---+ ---- .5081 .6726 7145 7145 .6726- .5087 -~~ ---- .4964 .7214 4 .6706 .5211 ---- ----

.4602 .6384 6761 .6761 .6384 .4602 --- --*+ .5213 .6706 5 ,7518 .6142 .5095 .4605 .5856 .6150 .6201 .6201 .6150 .5856 .4605 .5095 .6142 7518 6 7983 7210 .6738 .6391 .6153 .5709 .4340 4340 .5709 .6153 .6391 .6738 7210 7983 7 .8098 .7551 7140 .6771 .6206 .4341 - + - ---- .4341 .6206 .6771 .7160 .7551 .8098 8 .809R 7551 7160 6771 6206 .4341 --- ---- .4341 .6206 .6771 7160 7551 8098 9 .7983 7210 .67.38 .6391 .615) A709 .4340 .4340 .5709 .4153 .6391 .6738 .7210 7983 to .7518 .6142 .5095 .4605 ,5856 .4150 .6201 .6201 .6150 .5856 .4605 .5095 .6142 7518 11 .6706 .5213 - - -+-- .4602 6384 .6761 .6761 .6384 .4602 --- ---- .5213 .6706 12 .7214 .4964 ---- ---- .5087 6726 .7145 7145 .6726 .5087 ---- ---- .4964 ,7214 33 .6430 6661 .4959 .5204 .6128 '.7190 .7531 7531 7190 .6128 .5204 .4959 .6661 .6430 14 7644 '.6423 ,7199 ;6688 7494 ,7956 ,8071 .8071 .7956 .1494 .6688 .7199 .6423 7644 MAXIMUM 2D ONE PIN POWER = .8098 AT POW 7 COIJJMN 1 MAXIMUM 2D ONE PIN POWER W/UNC

  • 9176 i .8098 X 3.1000 X 1.03001 MAXIMW CHANNEL POWER = 7825 AT POW 7 COLUMN 1.

MAXiNUM 3D ONE FIN POWEP

  • 1,2 249 AT RDW 7 COLUMN 1 IINCLUDES GRID DIP FACTOR OF 1.00751 MAXIMUM 3D ONE PIN POWER W'UNC w 1.3878 t1.2249 x 1.3000 X 1,0300)

MAX] MUM LNGR = 7,3496 FW/FT 11.2249 X 6 00003 i MAXIWJM LMCR W/ UNCERTAINTY = 8.7484 KW/FT (1<3878 X 6.0000 X 1.0300 X 1.0200)

PL TO 16.00 KW/PT WlO UNC . a 223.2824 i 16.00 X 100,00 It 7,3496 X .9750))

PL TO 16.00 EW/PT W/ UNCERTAINTY

  • 184.5803 ( 16.00 X 100.00 /( 8.7484 X ,9750) - 3.0000)

ASSEMBLY AXJAL SKAPE IMLEX = .3308 ASSEMBLY AX1 AL SMAPE INDER W/UNC= 2908 NONMAL12ED ASSFMBLY AX1AL POWER SHAPE:

NODE 1 2 3 4 5 6 7 8 AX1AL PCWER 9392 1.2599 1.4258 1.5125 1.5105 1.4774 1.3424 1.1786 NODE 9 10 11 12 13 14 15 16 AX1AL FOWER .9840 .8554 .7519 .6955 .4364 5887 .4936 .3482 1

i i

ASAS mnual Revision 0 88 April 19,1994 1

i

_ _ _ __ _ _ m _

Figure 13 Sample User Output File Page 36 of 37 1 PPOGPAM ASAS VERSION 1. REV DATE 4/12/94 TODAY'S DATE IS 04/12/94 THE TIME IS 08:19:49 PAGE 36 A CODE 10 CREATE HDT CHANNEL DA1A FILES FROM A SIMULATE-3 P!H FILE PIN F11.E NAME : / FPC3 / Sp/OP PD/ e 30t est .p RUN TITLE  : Fort Calhouri Cycle 15 Boc 10.$ Hours - asatest CASE ID 8-10.5-J PDIL CASS J - 20% POWER. BANK 3 AT 574 XPO = 10.500 Owo/MT. EsAR

  • 16.119 GWD/MT, POWER e 20. 00 4. FwW ' = 100.00%

WJrW1' o 24164. STEPC INSERTED. FQ e 2.628. F-DELTA-H = 1.890, INCORE ASI e .2058, PERIPHERAL ASI e ,1549 TOTAL RELAT1VE EXCOFE SIGNAL e .4347 FVEL TYPE i TYPE 2 PIN POWERS FOR LIMITING LHGR PLANE 6 FOR ASSE21BLY 35. SERIAL NUMBER OMS 020 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1,9810 1.8253 2.2642 2.3299 2.2894 2.2743 2.2587 2.2646 2.2919 2.3188 2.3733 2.3227 1,8896 2.0737 2 1.8142 2.2363 2.0638 2.2750 2.2030 2.2841 2.2747 2.2802 2.3021 2.2337 2.3206 2.1203 2.3172 1.8992 3 2.2440 2.0567 ---- ---- 2.3631 2.3862 2.3288 2.3343 2.4060 2.3982 ---- ---- 2.1363 2,3520 4 2.3058 2,2644 ---- ---- 2.4298 2.4445 2.3857 2.3918 2.4666 2.4687 ---- ---- 2.3558 2.4212 5 2.2637 2.1897 2.3549 2.4254 2.5437 2.4469 2.4852 2.4919 2.4706 2.5869 2.4855 2.4327 2.2825 2.3808 6 2 2471 2.2671 2.373) 2.4349

. 2.4413 2.3514 2.4876 2.4954 2.3769 2.4846 2.4971 2.4537 2.3645 2.3653 7 2.2295 2.2535. 2.3105 2.3694 2.4716 2.4793 ---- ---- 2.5061 2.5164 2.4309 2,3893 2.3505 2.3469 8 2.2295 2.2535 2.3105 2.3694 2.4716 2.4793 ---- - - - 2.5061 2.5164 2.4309 2.1893 2.3505'2.3469 .

9 2.2471 2.2671 2.3733 2.4349 2.4413 2.3514 2.4816 2.4954 2.3769 2.4846 2.4971 2.4537 2.3645 2.3653 10 2.2637 2.1891 2.3549 2.4254 2.5437 2.4469 2.4852 2.4919 2.4706 2.5869 2.4855 2.4327 2.2825 2.3808 11 2,3058 2.2644 ---- ---- 2.4298 2.4445 2.3857 2.3918 2.4666 2.4687 ---- --- 2.3554 2.4212 12 2.2440 2.0567 ----

2.3631 2.3862 2.3289 2.3343 2.4060 2.3982 ---- ---- 2.1363 2.3520 13 1.8142 2.2363 2.0628 2.2750 2.2030 2.2841 2.2747 2 2802 2.3021 2.2337 2.3206 2.1203 2.3172 1.8992 14 1.9810 1.8253 2.2642 2.3299 2.2894 2.2743 2.2587 2.2646 2.2919 2.3188 2.3733 2.3227 1.8896 '2.0737 F2 FACTOF3 FOR ASSEMBLY 35, SERIAL NUMBER OMS 020 .

I 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.3454 1.3409 1.3480 1.3514 1.3535 1.3564 1.3585 1.3610 1,3638 1.3655 1.3681 1.3696 1.3672 1.3772 2 1.3396 1.3443 1.3433 1.3506 1,3481 1.3556 1.3589 1.3612 1.3618 1.3599 1.3673 1.36es 1.3710 1.3715 1.3456 1.3422 1.3545 1.3570 1.3595 1.3619 1.3642 1.3666

  • 3 +--- ---. ---- +--- 1.3693 1.3787 4 1.3478 1.3483 ---- ---- 1.3561 1.3578 1.3608 1.3632 1.3650 1.3683 ---- ---- 1.3760 1.3820 5 1.3485 1.3444 1.3518 1.3546 1.3561 1.3578 1.36C8 1.3632 1.3652 1.3685 1.3721 1.3745 1.3722 1.3832 6 1.3497 1.3501 1.3525 1.3545 1.3560 1.3534 1.3614 1.3638 1.3608 1.3685 1.3722 1.3755 1.3787 1.3850 1 3.3447 1.3512 1.3529 '1.3554 1.3568 1.3592 +--- *--- 1.3668 1.3695 1.3732 1.3759 1.3801 1.3854 8 1.3497 1.3512 1.1529 1.3554 1.3568 1.3592 ---- --+- 1.3668 1,3695 1.3732 1.3759 1.3801 1.3854 9 1.3497 1.3501 1.3525 1.3545 1.3560 1.3534 1.36'14 1.3638 1.3608 1.3685 1.3722 1.3755 1.3787 1.3850 10 1.3445 1.3444 1.3518 1.3546 1.3561 1.3578 1.3608 1.3632 1.3652 1.3685 1.3721 1.3745 1.3722 1.3832 11 1.3478 1.3483 ----

1.3561 1.3578 1.3608 1.3632 1.3650 1.3683 ---- -- - 1.3760 1,3820' 12 1.3456 1.3422 ---- ---- 1.3545 1.3570 1.3595 1.3619 1.3642 1.3666 +--- ---- 1.3693 1.3787 13 1.3396 1.3443 1.1433 1.3506 1.3481 1,3556 1.1589 1.3612 1.3628 1.3599 1.3673 1.3648 1.3710 1.3715 -

t le 1.3454 1,3409 1.3480 1.3514 1.1535 1.3564 1.3545 1.3610 1.3638 1.3655 1.36s1 1.3696 1.3672 1.3772 -

ASSEMBLY AXIAL PEAFING FACTOR = 1.3613 IFROM 16 PLANE DATAI

(

t r

ASAS Manual Revision 0 89 April 19,1994

Figure 13 Sample User Output File Page 37 of 37 -

t 1 PROGRAM ASAS VERSION 1. REV DATE 4/12/94. TODAY's DATE'!S 04/12/94. THE TIME !$ 08:19:49 PACS 37 A CODE TO CRJ. ATE MOT CHANNEL DATA FILES FROM A SIMULATE-3 PIN FILE FIN FILE NAMS t / PPG 3/Sp/OPPD/m30 test.p PUN TITLE i Fort. Calhoun Cycle 15 BOC 10.$ Hours - esatest

  • CASE ID D-10.5-J PDIL CASE J - 20t POWER, BANX 3 AT 574 XPO = 10.500 GWD/MT. EEAR
  • 16.119 CWD/MT, POWER = 20.004. Flow e 100.006 W TWT e 24164. STEPS INSERTED, FQ e 2.638, F-DELTA-M
  • 1.890, .INCOPE AS1 .2058, FERIPHERAL AS1 * .1549 TOTAL PELATIVE EXCORE SIGNAL a ,4347 FUEL TYPE : TYPE 2 2D PIN POWERS FOR ASSEMBLY 35 SERIAL NUMBER OMS 020 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.4724 1.3613 1.6796 1.7241 1.6915 1.6767 1.6626 1.6639 1.6806 1.6982 1.7347 1.6960 1.3822 1.5058 2 1 1542 1.6636 1.5356 1.6845 1.6341 1.6849 1.6739 1.6751 1.6893 1.6425 1.6972 1.5535 1.6901 1 3847 3 1.6676 1.5323 ---- ---- 1.7447 1.7585 1.7129 1.7140 1.7637 1.7549 ---* -+-- 1.5602 1.7063 4 1.7108 1.6795 ---- - - - - 1.7917 1.8004 1.7532 1.7546 1.8070 1.8042 ---- ---- 1.7121 1.7530 5 1.6188 1.6288 1.7420 1.7905 1.8758 1.8021 1.8263 1.8281 1.8098 1.8904 1.8115 1.7699 1.6633 1.7224 6 1.6649 1.6792 1.7547 1.7976 1.8003 1.7375 1.8272 1.8297 1.7467 1.8155 1.8198 1.7840 1.7154 1.7093 7 1.6519 1.6677 1.7077 1.7481 1.8216 1.0241 ----

--- 1.8336 1.8375 1.7702 1.7365 1.7037 1.6959 8 1.6519 1.6677 1.7077 1.7481 1.8216 1.0241 ---- ---- 1.8336 1.8375 1.7702 1.7365 1.7037 1.6959 9 1.6649 1.6792 1.7547 1.7976 1.8003 1.7375 1.8272 1.8297 1.1461 1.8155 1.819a 1.7840 1.7154 1.7093 30 1.6788 1.6288 1.7420 1.7905 1.8758 1.8021 1.8263 1.8281 1.8098 1.8904 1,8115 1.7699 -1,6633 1.7224 11 1.7108 1.6794 -~~~ ---- 1.791? 1.8004 1 J532 1.7546 1.8070 1.8042 ---- +-- 1.7121 1.7530 12 1.6676 1.5323 ---- - - - 1.7447 1,7585 1.7129 1.7140 1.7637 1.7549 ---- ---- 1.5602 1.7063 13 1.3542 1.6636 1.5356 1.6845 1.6341 1.6849 1.6739 1.6751 1.6893 1.6425 1.6972 1.5535 1.6901 1.3842 14 1.4724 1.3613 1.4796 1.7241 1.6915 1.6767 1.6626 1.6639 1.6806 1.6982 1.7347 1.6960 1.3822 1,5058 FUEL TYPE . TYPE 2 ADJUSTED 2D PIN POWEPS FOR ASSEMBLY 35. SERIAL NUMBEP OM3020 11NCLUDES CRID DIP FACTOR OF 1.0075) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 1.4662 1.3509 1.6757 1.7244 1.6944 1.6833 1.6717 1,6760 1.4951 1.7162 1.7565 1.7191 1.3986 1.5340 2 1.3427 1.6552 1.5267 1.6838 1.6305 1.6905 1.6835 1.6876 1.1039 1.6532 1.7175 1.5693 1.7150 1.4056 3 1.6608 1.5222 ---- ---- 1.7490 1.7660 1.7236 1.7277 1.7807 1.7749 ---- -*-- 1.5811 1.7412 4 1.7066 1.6759 ---* ---- 1.7983 1.8092 1.7657 1.7702 1.8256 1.8271 ---- ---- 1.7437 1.7931  !.

5 1.6754 1.6206 1.7429 1.7951 1.8427 1.8110 1.8394 1.8443 1.8286 1.9146 1.8396 1.8005 1.6893 1.7633 6 1.6631 1.6779 1.7565 1.8021 1.8068 1.7403 1.8411 1.8469 1.7592 1.8389 1.8482 1.8161 1.7504 1.7521 7 1.6501 1.6679 1.1100 1.7536 1.8213 1.8350 +--- ---- 1.8548 1.8624 1.7991 1.7684 1.7403 1.7389 8 1.6501 1.6679 1,7100 1.7536 1.8293 1.8350 ---* ---- 1.8548 1.8624 1.7991 1.7654 1.7403 1.7389 9 1.6631 1.6779 1.7565 1.8021 1.8068 1.7403 1.8411 1.8469 1.7592 1.8389 1.8482 1.8161 1.1504 1.7521 10 1.6754 1.6206 1.7429 1.7951 1.8827 1.8110 1.8394 1.8443 1.8266 1.9146 1.8396 1.8005 1.6893 1.7633 11 1.7066 1.6759 ---- ---

1.7983 1.8092 1.7657 1.7702 1.8256 1.8271 - -- ---- 1,7437 1.7931 12 1.6608 1 5222 ---- ---- 1.7490 1.7660 1.7216 1.7277 1.7807 1.7749 ----

1.5811 1.7412 13 1,3427 1.6552 1.5267 1.6838 1.6305 1.6905 1.6835 1,6876 1.7039 1.6532 1.7175 1.5693 1.7350 1.4056 14 1.4662 1,3509 1.6757 1.7244 1.6944 1.4833 1.6717 1.6760 1.6963 1.7162 1.7565 1.7191 1.3986 1.5348 MAXIMUM 2D ONE PIN POWER e 1.9146 AT ROW 5 COLtPCI 10 MAXIMUM 2D ONE PIN POWER W/UN' e 2,1692 (1.9146 X 1.1000 3 1.0300)

MAXIMUM CHANNEL POWER

  • 1.8603 AT ROW 5 COLtmN 10 MAXIM'JM 3D ONE PIN POWER = 2.6063 AT kW 5 COLUMN 10 (INCLUDES GRID DIP FACTOP OF 1.0075)

MAXIMUM 3D ONE PIN POWF.R W/Urc = 2.9529 12.6063 X 1.1000 X 1.0300)

MAXIMUM LMGP = 15.6376 FW/FT 12.6063 X 6.0000)

MAXIMUM LHG9 W/UNCFPTAIVry = 18.6140 EW/FT (2.9529 X 6.0000 X 1.0300 X 1.0200)

Pb TO 16.00 KW/FT W/O UNC

  • 104.9407 ( 16.00 X 100.00 /(15.6376 K .97501)

PL To 16.00 FW/FT W/tmCEPTAINTY

  • F5.1610 t 16.00 X 100.00 /418.6140 X .97501 - 3.0000)

ASSEMBLY AXI AL SHAPE INDEX = .1971 ASSEMB1.Y AX1AL SHAPE INDEX W/UPCs .1471 NOPMALIZED ASSEMBLY AXIAL POWER SHAPE:

NGDE 1 2 3 4 5 6 7 8 i AFIAL PWER .6498 1.0409 1.2320 1.3392 1.3586 1.3613 1,2912 1.2233 NODE 9 10 11 12 13 14 15 16 AXIAL POWER 1.1123 1.0349 r 9410 .8808 8002 .7295 .6019 .4031 1

a ASAS Manual Revision 0 90. April 19,1994

Figure 14 Sample CTS Output File

  • CASE *
  • CASE 1D
  • A$1-A85 *
  • AEl- PER *
  • ASI-CORE * ' PFDL. * *L.HGA N/1MC' 'F214C-FISS* *ASSEMB:.Y 8 *EXOOps RES*

J

  • B- 1 D. 5 - A11 * +1. 5 5115 RE-02 2. 26 30 2 6 E-03 7. 7 64136 E -03 4. 2 00959 E. 0 2 3.636200s.00 8 1 4. 4 2 54 62 E- 01 1
  • p- 10. 5- A 12
  • 1.512322E-02 2.263026E-03 7.7641365-03 1. 09 34 69 E. 02 1.3 6 93 8 %E* 01 8 18 4. 4 25 4 62 E-01 1
  • B - 10. 5 - A13
  • 2.72&D81E-02 2.2 6 30 26E-0 3 7.16413 4E-0 3 1.0443235 02 1.432029E*01 8 16 4. 4 254 62 E-01 1
  • B-10. 5- A14
  • 5.5215205-03 2.2630265-03 7.764136E-03 1.1341655 02 1.321514E 01 8 25 4.4J5462E-01 1 *s 10.5 A21* 2.057 73 4E-02 2.263C26E-03 7.744136E-03 1.211895t*02 1.32138 8E+ 01 8 10 4.425462E 01 1 *D 10.5.A22' 4.615373E-03 2.263026E-03 7.764136E-03 1.314050s.02 1. 2 20956 E
  • 01 8 39 4.425462E 01 1 *a 10.5-A23* 2.3855325-02 2. 26 3G 26 E- 0 3 7.764136E-03 1,117916E 02 1. 4 2 956 9E+01 8 35 4.4254621-01 1 *s-10.5-A24' 7. 412 684 E- 0 3 2.263026E 03 7.7641165-0) 1. 251704 E* 02 1. 2 74 381E+0! # 19 4. 4 254 62 E- 01 2 ' 8 -10. 5 -J11
  • 1.5 0812 ) E-01 1. 5 4 8 5 50E-01 2.058113E-01 3. 52 274 a E*02 4.330351E+00 5 1 4. 341418 E-01 2
  • s- 10. 5-J12
  • 1.956038E-01 1 54 8 550E-01 2.058113E-01 8. 8 932 26 E+ 01 1. 673 47 3 E + 01 5 13 4.3474185-01 1
  • D 10. 5-J 13
  • 1.741356E-01 1. 54 8550E-01 2.058113E C1 8. 66 2 815 E+ 01 ' 1.716494E+01 5 16 4.347418E 01 i 2
  • s- 10.5 -J14
  • 1.1370362-01 1. 54 8560E-01 2. 059113 E -01 9. 20 5 556 E. 01 3 . 618 4 875 +01 5 11 4.341418E-01 2
  • B- 10. 5 J 15
  • 2.2 85 85 6 E-01 1. 54 8550E- 01 2.058113E-01 8. 9675 83 E. 01 1.66004f E+01 5 18 4.347418E-01 2
  • D- 10.5-J 21
  • 1.6072425-01 1. 54 6 550 E-01 2.058111E-01 1.03 6 88 2 E.02 1.538151E+01 5 10 4. 3 4 7418E-01 2
  • N 10. 5-J 2 2
  • 3. 309019E - 01 1. 94 8550E-01 2.058113E-01 1. 8 4 5 BD] E
  • 03 8.748392E+00 5 39 4.3474158-01 2 '* 3 10,5-J 2 3
  • 1 870529 E-01 1. 54 8 550E- 01 2 . 05 8113 K - 01 8. 516104 E. 01 1. 8 613 9 5t
  • 01 5 21 4.347418E-01 4

F 1

I i

8 ASAS Manual Revision 0 91 April 19.1994

-m - , -.-- - ~ .

Figure 15 Sample ATS Output File Page 1 of 16 40

  • Axial Nodes
  • 2
  • Fields on File
  • 1
  • case Number *
  • B-10.5-A11*
  • case ID*

100.000

  • Percent rull Power
  • 77641E-02
  • core Average ASI*

1.77000 *padial Peaking Factor IFR)*

1.18769

  • Axial Peaking Factor
  • 1.14813 ' Assembly Peaking Factor
  • 1 ' Assembly Number *
  • Reason For Selection *
  • K* *RPOW-HPTH * ' ASS-AX1AL
  • 1 .45136 62061 2 .58215 ,68913 3 71219 .75737 4 .82428 .81884 5 .90120 .86707 6 .94830 .90412 7 98984 ,93942 8 1,03160 .97511 9 1.06685 1.00650 10 1.08886 1.02890 11 1.20080 1.04439 12 1.11660 1.06220 13 1.13928 1.0843D 14 1.15891 1.10388 15 1.16554 1.11409

'16 1.16260 1.11730 17 1.16554 1.12410 I 18 1.17771 1.1J681 19 1.18769 1414747 20 1.18407 1,14813 21 1.17046 1.14133 22 1.16334 1.13865 l

23 1.16635 1.14262

( 24 1.16773 1.14489

[ 25 1.15578 1,13719 i 26 1.13399 1.12201 l 27 1.11837 1.11086 28 1.11244 1.10628

  • 29 1.10484 1.20002 30 1.08411 1.08378 31 1.05313 1.05966 32 1.02495 1.03745 33 1.00248 1.01923 34 .97530 .99722 .

35 .93300 .96356 l 36 .87466 .91961 37 79864 .86542 38 70472 80485 39 .60189 74055 40 .49861 .67607 i

'ASEDtBLY 2D PIN POWERS *

.0500 .0521 .0556 .0589 .0620 .0655 .0708 .0726 ,0717 .0728 .0745 .0760 .0775 .0809

.0568 .0624 .0686 .0729 .D747 .0760 .0781 .0800 .C825 .0863 .0903 .0919 .0914 .0928

.0667 .0'52 .0000 .0000 .0898 .0891 .0897 .0918 .0962 .3029 .0000 .0000 .3083 .1072

.0786 .0879 .0000 .0000 .1043 .3034 .1038 .1062 .3112 .3188 .0000 .0000 .2243 .1224

.0926 ,0999 .1049 .1149 .1172 .1190 .1207 .1235 .1279 .1330 .1385 .2402 ,1381 .1381

.1107 ,1136 .1198 .2258 .1312 .1374 .1435 .1469 .1481 .1492 1512 .1527 .1530 .1550

.1373 .1314 .1342 .1396 .1466 .1576 .0000 .0000 .2720 .1687 .1691 .2701 .1709 .1734

.1584 .1515 .1542 .3597 .2671 .2798 .0000 .0000 .1950 .1900 .1902 .1914 .1928 .1970

.1728 .1747 .1822 .1894 .1956 .2026 .3083 .2123 .2146 .2157 .3184 .2201 .2203 .2236

.1981 .2064 .2206 .2285 .2286 .2281 .2268 .2300 .2392 .2488 .2594 .2617 .2563 .2558

.2317 .2457 .0000 .0000 .2672 .2586 .2548 .2583 .2707 .2897 .0000 .0000 .2998 .2935

.2712 .2840 .0000 .0000 .3020 .2922 .2895 .2942 .3067 .3279 .0000 .0000 .3410 .3351

.3157 3189 .3110 .3356 .3311 .3286 .3326 .3397 .3477 .3619 ,3781 .3833 .3782 .3818 l- .3716 .3628 .3641 .3662 .3687 .3761 .3950 .4072 .4046 .4102 .4185 .4250 .4302 .4441 l

i f

I I

i-r ASAS Manual Revision 0 92 April 19,1994

.mm Figure 15 Sample ATS Output File Page 2 of 16 40 *Axin! Nodes

  • 2 ' Fields on File
  • 1 *Oase Number *
  • a-20.5-A12*
  • Case ID*

100.000

  • Percent Full Power *

.77641E-02

  • Core Average AS1*

1.77000 *Padial Peaking Factor (FR)*

1.18769

  • Axial Peaking Factor
  • 1.19574 ' Assembly Peaking Factor
  • 18
  • Assembly Numter*

FQ-F1ANE 1 * ' Reason For Selection *

  • K'
  • R.PCM-HPTH *

' ASS- AX1AL

  • 1 45136 45359 2 .58215 .58283 3 71219 .71137 4 .82428 .62325 5 .90120 .90250 6 .94830 .953R6 7 .99984 .99903 -

8 1.03160 1.04J15 9 1.06685 1.07946 10 1,0B886 1,10120 13 1.10080 1.11397 12 1.11660 1.1272P 13 1.13929 1.15053 14 1.15891 1.17051 15 1.16554 1.17604 16 1.16260 1.17100 17 3.16554 1.17285 18 1.17771 1.18541 19 1.18769 1.19574 20 1.18407 1.19093 21 1.17D46 1.17507 22 1.16334 1.16667 23 1.16635 1.16987 24 1.16773 1.17144 25 1.15578 1.15425 26 1,13399 . 13414 27 1.11837 1.11680 28 1.11244 1.11009 29 1.10404 1.10165 30 1.06411 1.07896 31 1.05313 1.04516 32 1.02495 1.01468

3) 1.0024R .99071 34 91530 96134 35 .93300' .91476 36 .87466 .R5117 17 79864 77396 28 70412 .68403 39 .60199 .5877) 40 .49841 .49111

' ASSD4RL,Y 2D PIN POWTP.$

  • 1.3413 1.2075 1.4451 1.3441 1.4385 1.4537 1.4455 1.4491 1.4630 1.4517 1.3634 1.4630 1,2211 1.3466 1.2316 1.4736 1.3290 1.4298 1.3965 1.4548 1.4511 1.4542 1.4G34 1.4095 1.4467 1.3467 1.4905 1.2340

.0000 1.3629 1.4961 1.4906 1.3441 .0000 .0000 1.4664 1.5035 1.4774 1.4604 1.5129 1.4814 .0000 1.4001 1.4562 .0000 .0000 1.1744 1.5139 1.5016 1.5047 1.5243 1.3904 .0000 .0000 1.4809 1.4101 1.4999 1.4290 1.4840 1.3811 1.5564 1.5338 1.5280 1.5310 1.5451 1.5761 1.4051 1.5143 1.4576 1.5162 1.5169 1.4927 1.5269 1.5271 1.5397 1.5675 1.3851 1.3879 1.5790 1.5595 1.5546 1.5603 1,5263 1.5405 1.5017 1.4901 1.5047 1.5202 1.5397 3.3905 .0000 .0000 1.3993 1.5577 1.5463 1.5374 1.5269 1.5354 1,5028 1.4923 1.5071 1.5239 1.5441 1.3954 .0000 .0000 1.4049 1.5630 1.5512 1.5421 1.5307 1.5385 1.5J33 1.5021 1.53BR 1.5407 1.5550 1.5844 1.4013 1.4050 1.5978 1.5777 1.5721 1.5770 1.5413 1.5534 1.5121 1.4457 1.5044 1.4032 1.5814 1.5622 1.5576 1.5617 1.5763 1.6078 1.4331 1.5427 1.4836 1.5396

,0000 1.5184 1.4427 1.4184 1,4R06 . 0 0'JO .0000 1.4099 1.5541 1.5434 1.5474 1.5492 1.4308 .0C00 1.5175 1.3745 .000D .0000 1.5141 1.5557 1.5309 1.5348 1.5695- 1.5367 .0000 .0000 1.4086 1.5420 1.2624 1.5156 1.3725 1.4920 1.4528 1.5168 1.5151 1.5189 1.5298 1.4739 1.5109 1.4046 1.5516 1.2829 1.3872 1.2500 1.5004 1.4056 1.5051 1.5250 1.5174 1.5212 1.5375 1.5256 1.4320 1.5341 1.2798 1.4129 ASAS Manual Revision 0 93 April 19,1994

-I Figure 15 Sample ATS Output File Page 3 of 16 40

  • Axial Modes
  • 2 *Fleidd on F1)e*

1

  • Case Number *
  • B-10.5-A13* ' Case 3D* .
  • 100.000 ' Percent rull Power *

.776418-02 " core Average As!' s 1.77000 'Pedial Peaking Factor (FR)"

1.19769 *Axlal Peaking Factor

  • 1.21041
  • Assembly Peaking Factor?

16 ' Assembly Numter*

  • FQ. PLANE 2 *
  • Peason For $ elect.1on*

'K* ' R FCM- M PTM ' 'AS$ AXIAL

  • 1 45136 .41221 2 .58215 .55581 3 .71219 .69865 4 .82428 82315 5 .90120 .91176 6 .94830 96947 1 .98984 1.01934 4 1.03160 1.06664

.9 1.06685 1.10519 10 1.08886 1.12763 .'

11 1.10000 1.13791

.12 1.116E0 1.15263 13 1.13928 1.17523 14 1.15B91 1,19422 15 1.16554 1.19805 16 1.16260 1.19079 8 17 1.16554 1.19066 la 1.17771 1.20167 19 1.18769 1,21041 20 1.18407 1.20154 21 1.17046 1.19529 22 1.16334 1.174a5 23 1.16635 1.17648 24 1.16773 1.17647 25 1.15578 1.14122 26 1.13399 1.13470 27 1.11837 1.11529 28 1.11244 1,10696 29 1.10484 1.09693 30 1.08811 1.0'225 31 1.05313 1.03613 32 1.02495 1.00325 33 1.00248 .97478 34 .,97530 94476 35 .93300 .89520 36 .47466 .82795 .

37 79864 .74511 38 .70472 .64727 39 .60189 ,54182 40 .49861 .43606

  • A$$EMBLY 2D PIN POWF.R$'

1,1306 1.1043 1.3M16 1,4370 1.4302 1.4360 1.4168 1.4462 1.4702 1,4917 1.5289 1.5027 1.2329 1.3621 1.10C2 1.3692 1.2711 1.4107 1.3869 1.4480 1.4508 1.4588 1.4779 1,4392 1.4880 1.3697 1.5102 1.2572 1.3721 1,2673 .0000 .0000 1.4818 1.5113 1.4842 1.4907 1.5170 1.5279 .0000 .0000 1:3802 1.5453 1.4234 1.4031 .0000 .0000 1.5257 1.5502 1,5177 1.5227 1.5718 1.5644 0000 .0000 1.5081 1.5795 1.4137 1.376H 1.4759 1.5232 1.6094 1.5548 1.5796 1.5835 155724 1.6427 1.5708 1.5412 1.4639 1.5469 1.4174 3.4356 1.5035 1,5462 1.5535 1,5008 1.5744 1.5780 1.5167 1.5809 1.5868 1.558a 1.5107 1.5294

-1.4176 1.4377 1.4761 1.5136 1.5782 1.5744 .0000 .0000 1.5908 1.6050 1.5498 1.5235 1.4999 1.5054 1.4275 1.4465 1.4837 1.5199 1.sn36 1.5790 .0000 .0000 1.5948 1.6081 1.5520 1.5249 1.5007 1.5056 1.4512 1,4664 1.5315 1.5713 1.5752 1.5201- 1.5915 1.5944 1.5299 1.5916 1.5952 1.5648 1.5149 1.5316 1.4729 1,4291 1.5246 1.5669 1.6494 1.5A84 1.6095 1.6109 1.5948 1.6617 1.5851 1.5518 1.4713 1.5515 .

1.5099 1.4794 .0000 .0000 1.5A08 1.5965 1.5586 1.5593 1.6031 1.5897 .0000 .0000 1.5189 1.5870 1 4835 1.3594 .0000 ,0000 1.5528 1.5730 1.5359 1.5362 1.5761 1.5596 .0000 .0000 1.3935 1.5563.

1.2142 1.4943 1.3735 1.5090 1.4709 1.5219 1.5125 1.5123 1.5237 1.4760 1.5190. 1.3908 1.5294 1.270' 1.3318 1,228A 1.5171 1.5591 1,5347 1.5244 1.5086 1.5077 1.5245 1.5377 1.5673 1.5335 1.2546 1.3852 i

l ASAS &nual bision 0 94 . April 19,1994

'l l

. _ = = _-__ _ . _ _ . __

e 1.

i j

I Figure 15 Sample ATS Output File i: ~j l Page 4 of 16 h I I *Axlal podes*

40 2 *Fielda on File

  • 1
  • Case Number *

, 's-10.5-A14*

  • Case ID*

1 100.000

  • Percent Full Power *

,77641E-03

  • Core Average A31*

l 1.77000 *Padial Peaking Factor (FPl*

l 1.18769

  • Axial Feaking Factor
  • y 1.18670
  • Assembly Peaking Factor
  • 25
  • As sembly Number
  • j
  • FQ-FLANE 16 * * 'Pesson For Selection *
  • K* *RPOW+HPTH
  • ASS-AXIA1
  • 1 .45136 .47040 2 .58215 .59118 3 71219 .71133 4 .82428 .81635 5 90120 .89172 f 6 .94830 .94168
1. 7 .98984 98573 8 - 1.03160 1.02846 I' 9 1.06685 1.06360 10 1.0A886 1.08489 11 1.10080 1.09581 12 1.11660 1.11142 13 1.1.1928 1.13502 1 14 1.15891 1.15559  ;

15 1.16554 1.16212 5 16 1.16260 1.15841 17 1.16554 1.16153

! 18 1.17771 1.17520 1 19 1.18769 1.18610 1 20 1.18407 1.18331 '

1.17046 1.16908 21 22 1.16334 1.16219 23 1.16635 1.16671 24 1,16773 1.16962 25 3.15578 1.15797 26 1.13399 1.13557 i

. 27 1.11837 1.12002 3 i

28 1.11244 1.11522 r

!' 29 1.10484 1.10857 l

30 1.08411 1.08757 ,

31 1.05313 1.05536 i 32 1.02495 1.02657  ;

33 1.00246 1.00436 34 .97530 .97646 '

35 .93300 .93050  !

36 .87466 86717 5 37 79864 .79190 +

34 70472 70612 39 .60189 .61500 i 40 .49861 .52363 i

  • AESEMBI.Y 2 D FIN PMR3' 1.4188 1.2899 1.5461 1.4389 1.5296 1.5115 1.3608 1.3608 1.5115 1.5296 1.4389 1.5461 1.2899 1.4188 1.2647 1.5506 1.4007 1.4999 1.4411 1.4991 1.4762 1.4762 1.4991 1.4411 1.4999 1.4007 1.5506 1.2847

! 1.5314 1 3930 .0000 .0000 1.3746 1.5205 1.5066 1.5066 1.5205 1.3746 .0000 .0000 1.3930 1.5314 1.4159 1.4821 .0000 .0000 1.3835 1.5306 1.5176 1.5176 1.5306 1.3835 .0000 .0000 1.4821 1.4159 1.4943 1.4141 1.3565 1 3741 1.5429 1.5410 1.5309 1.5309 1.5410 1.5629 1.3741 1.3565 1.4141 1.4943 5 1.4649 1.4602 1.4698 1.5094 1.5302 1.5581 1.3753 1.3753 1.5581 1.5302 1.5094 1.4898 1.4602 1.4649 1.3072 1.4267 1.4656 1.4862 1.5097 1.3659 .0000 .0000 1.3659 1,5097 1.4862. 1.4656 1.4267 1.3072 1.2914 1.4181 1.4573 1.4782 1.5016 1.3511 .0000 .0000 1.3571 1.5016 1.4782 1.4573 1.4181 1.2974 1.4321 1.4287 1.4587 1.4787 1.4994 1.5266 1.3462 1.3462 1.5266 1.4994 1.4787 1.4587 1.4287 1.4321 1.4367 1.3604 1.3059 1.3239 1.5079 1.4873 1.4775 1.4775 1.4873 1.5079 1.3239 1.3059 1.3604 1.4367 1.3381 1.4039 .0000 -0000 1.3134

. 1.4551 1.4410 1.443D 1.4551 1.3134 .0000 .0000 1.4039 1.3383 1.4266 1.2967 .0000 .0000 1.2857 1.4247 1.4121 1.4121 1.4247 1.2857 .0000 .0000 1.2987 1.4266 1.1816 1.4273 1.2901 1.3941 1.3306 1.3864 1.3658 1,3658 1.3864 1.3306 1,3841 1.2901 1.4273 1.1816 1.3000 1.1764 1.4109 1.3137 1.3993 1.3843 1.2455 1.2455 1.3843 1.3993 1.3137 1.4109 1.1764 1,3000 i

I t

ASAS Manual Revision 0 95 April 19,1994

- . - . . - - , . - - . . . . ~ . . . _ _ _ . . . . _ _ __ .. _ - , !

i Figure 15 Sample ATS Output File l Page 5 of 16  ;

1 40 *Arial Nodes

  • 2 'Fleids on File" 1 ' Case Number'
  • a-10.5-A21' ' case It" 200.000 " Percent Full Power'

.71641E-02

  • Core Average ASI' 2.17000 ' Radial Peaking Factor (FRl' 1.18749 ' Axial Peakin0 Factor
  • 1.20018 ' Assembly-teaking Factor
  • 10 ' Assembly Number'
  • USER SELECT *

'Peemon For Selection *

'K' 'RPCW HPTH *

  • ASS-AXIA1,*

1 445136 41996 2 .58215 .t6307 3 71219 ,70538 4 .82428 .82828 5 .90120 91315 6 .94830 .96557 7 .98984 1.01101 8 1.0.1160 1.05555 9 1.06685 1.09214 10 1.08846 1.11453 11 1.10080 1.12557 12 1.11660 1.14039 13 1.13928 1.16230 14 1.15891 1.18086 15 1.16554 1.18566 16 1.16260 1.18032 17 1.16554 1.18117 18 1.17771 1.19177 19 1,18769 1.20018 20 1,18407 1.19448 21 1.17046 1.17845 22 1.16334 1,16924 23 1.16635 1.17066 24 1.16773 1.17051 25 1.15514- 1.15665  !

26 1.13399 1.13268 ,

27 1.11837 1.11513 28 1.11244 1.10759 29 1.10484 1.C9940 30 1.08411 1.07593

  • 31 1.05313 1.04292 ,

32 1.02495 1.01259 33 1.00248 98718 34 .97530 .95789 35 .93300 .91233 36 .87466 .85006 I 31 .79864 .76923 38 70472 .66956 39 .601R9 .56027 40 .49861 .45060

  • ASSEM11LY 2D PIN PCMEPS"

.8499 8681 ,9735 1.0044 1.0222 1.0351 1.0538 1.0737 1.1133 1.1621 1.2084 1.2355 1.1495 1.1798

.8483 ,9603 .9703 1.0106 1.0474 1.0409 1.0480 1.0658 1.1172 1.1872 1.2155 1.2302 1.2820 1.1760

.9370 .9553 00C0 .0000 1.0589 1.0723 1.0705 1.0888 1.1506 1.2028 .0000 .0000 1.2702 1.3055

.9576 .9846 .0000 .0000 1.0849 1.1019 1.1039 1.1219 1.1805 1.2286 .0000 .0000 1.3022 1.3258

.9683 1.0137 1.0403 1.0770 1.1307 1,1331 1.1546 1.1795 1.2088 1.2737 1.2773 1.2974 1.3235 1.3284

.9772 1.0037 1.0491 1.0892 1.1283 1.1855 1.1995 1,2254 1.2590 1.2570 1.2766 1.2921 1.2983 1.3301

.9929 1.0092 1.0459 1.0894 1.1513 1.1971 .0000 .0000 1.2710 1.2727 1.2600 1.2719 1.2920 1.3446 1.0198 1.0327 1.0686 1.1106 1.1735 1.2220 .0000 .0000 1.2998 1.2978 1.2814 1.2910 1.3103 1.3632 1.0642 1.0870 1.1318 1.1702 1.2055 1.2607 1.2734 1.3028 1.3313 1.3297 1.3465 1.3591 1.3606 1.3920 1.1198 1.1630 1.1875 1.2211 1.2725 1.2624 1.2812 1.3041 1.3329 1.4012 1.4009 1.4158 1.4318 1.4376 1.1766 1.1990 .0000 .0000 1.2826 1.2876 1.2752 1.2927 1.3548 1.405B .0000 .0000' 1.4627 1.4430 1.2198 1.2295 0000 .0000 1.3137 1.3127 1.2955 1.3101 1.3752 1,4286 ,0000 .0000 1.4689 1.5072

.1.1596 1.3025 1.2979 1.3331 1.3595 1.3341 1.3286 1.3424 1.3898 1.4582 1.4840 1.4822 1.5365 1.3904 1.2148 1.2288 1.3647 1.3671 1.3897 1.3e01 1.4034 1.4186 1.4455 1.4885 1.5295 1.5454 1.4131 1.4554 e

f

' ASAS Manual Revision o 96 April 19,1994 8

~w e + w w 5 "r^

c  !

!.. i i

i l l.

Figure 15

Sample ATS Output File

!- Page 6 of 16 i.

) 40

  • Axial modes
  • 2 *Fleids on File
  • 1
  • Case Number *
  • B 10. 5- A2 2' ' Case 10*

100.000

  • Percent rull Power *

.77641E-02

  • Core Average ASI" 1.77000
  • Radial Peaking Facter (FR)*

1.18769

  • Axial Peaking Factor"

. 1.18005

  • Assembly Peaking Factor" l 39
  • Assembly Num.ber*

USER SELECT * ' Reason for Sel ectio n*

! *F* 'PPOW.HPTH *

  • ASS-AX1A1,
  • l 1 .45136 .44891
2 .58215 .57648 i 3 71219 .70133

' 4 82478 .81305

! $ .90120 .8H922 l- 6 .94830 .93674 7 .989R4 .97802

9 1.03160 1.01839

! 9 1.06685 1.05173

. 10 1.08886 1.07188 11 1.10080 1.04230 4 12 1.11f60 1.09780 13 1.13928 1.12162 14 1.15891 1.14276 '

15 1.16554 1.15021 l l 16 1.16260 1.14771 1 l 17 1.16554 1.15214 1 l 18 1.17771 1.16715 l l 19 1.18769 1.18005 t 20 1.18407 1.17813 4- 21 1.17046 1.16542

! 22 1.16334 1.16011 l

} 23 1.16615 1.16625 1 e 24 1.16773 1.17058 -

! 25 1.15578 1.16001 I I

26 1.13399 1.13855 i

27 1.11837 1.12458 l.

i 28 1.11244 1.12210 #!

i 29 1.10484 1.11812

  • l 30 1.05411 1.09946 31 1.05313 1.06944 ,

32 1,0249$ 1.04323 33 1.00248 1.02409 5 34 .975J0 99928 35 .93300 .95593  ;

36 .87466 .99408 >

37 79864 .81613 34 70472 72283 1 39 .60189 .62176 ,

40 .49861 .52040

  • ASSEMBLY 2D PIN POWEP$* j 1.2621 1.1349 1.3710 1.2833 1.3754 1.3919 1.3822 1.3827 1.3919 1,3754 1.2833 1.3710 1.1389 1.2621 1.1395 1.3793 1.2509 1.3528 1.3232 1.3806 1.3750 1.3750 1.3806 1.3232 1.3528 1.2509 1.3793 1.1395 1.3724 1.251$ .0000 .0000 1.3819 1 4165 1.3892 1,3892 1.4165 1.3819 .0000 .0000 1,2515 1.3724 i 1.2851 1.3540 .0000 .0000 1.2867 1.4175 1.4027 1.4021 1.4175 1.2867 .0000 .0000 1.3540 1.2851 i 1.3776 1.3247 1.1829 1.2872 1.4513 1.4283 1.4195 1.4195 1.4293 1.4513 1.2872 143829 1.3247 1.3776 .

1.3942 1.3825 1.4179 1.4184 1.4287 1.4517 1.2788 1.2788 1.4517 1.4287 .1.4184 1.4179 1.3825 1.3942  ;

1.3843 1.3768 1.3906 1.4031 1.4201 1.2790 .0000 .0000 1.2790 '2.4201 1.4037 1.3906 1.3788 1.3843  ;

1.3841 1.3768 1.3906 1.4037 1.4201 1.2790 -0000

. .0000 1.2790' 1.4201 1.4037 1.3906 1.3768 1.3843 5 1.3942 1.3825 1.4179 1.4184 1,4287 1.4517 1.2788 1.2788 1.4517 1.4287 1.4184 1.4179 1.3825 1.3942 F 1.3776 1.3247 1.3829 1.2812 1.4513 1.4283 1.4195 1.4195 1.4283 1.4513 1.2872 1.3829 1.3247 1.3776 1.2851 1.3540 .0000 .0000 1.2867 1.4175 1.4027 1.4027 1.4175 1.2867 .000C .0000 1.3540 1.2851 1.3724 1.2515 .0000 .0000 1,3819 1.4165 1,3892 1.3892 1.4165 1.3819 .0000 .0000 1.2515 1.3724 1.1395 1.3793 1.2509 1.3528 1.3232 1.3806 1.3750 1.3750 1.3606 1.3232 1.3528 1.2509 1.3793 1.1395 1.2621 1.1389 1.3710 1.2833 1.3754 1.3919 1.3822 1.3822 1.3919 1.3754 1.2833 1.3710 1.1389 1.2621

' k b

i D

ASAS Manual Revision 0 97 April 19,1994 i C

9 w s..< a r-e *e.ee + w-em n e ..-+ w ww e- _-.m_ _. _ . , - . _

- . ... - - . . . , . - - -. . =- .. ..

l Figure 15 Sample ATS Output File Page 7 of 16 40 " Axial Nodes

  • 2 *rields on rile
  • 1 " Case Namber*
  • B-10.5-A23*
  • Case ID*

100.000 *rercent rull Power

  • 776418-02 *Cora Average As1*

1,77000

  • Radial Peeking Factor (FBl* 8 r

1.18769

  • Axial Feaking Factor
  • 1.20500
  • Assembly Peaking rector
  • 35
  • Assembly Number
  • FQ PLANE 1 *
  • Reason For Celection*

"F" *PPOW.HPTH * *A55-AX1A1. *

  • 1 45136 .42543 2 .58215 .56669 3 71219 .70716 '

4 .82428 .82879 5 .90120 .91352 6 .94830 .96675 7 .98994 1.01319 8 1,03160 1.0587J 9 1.06685 1.09614

  • 10 1.08886 1 11823
E 11 1.100A0 1.12870 12 1,11660 1.14359 13 1.13s28 1.16643 14 1.15b91 . 18580 lb 1.165'.4 1.19 us 16 1.16260 1..G 78 17 1.16554 1.18434 18 1.17771 1.19581 19 1.18769 1.20500 20 1,18407 1.19874 21 1.17046 1.18119 22 1.16334 1.17131 23 1.16635 1.17331 24 1.16773 1.17367 25 1.15578 1.15895 26 1.13399 1.33307 27 1.11837 1.11417 28 1.11244 1.10619 29 1.10484 1.09651 30 1.C8411 1.0724J 31 1.05313 1.03709 32 1.02495 1.00514 33 1.00246 .97976 34 ,97530 .94937 35- .93300 .90240 3 36 .87466 .83843 17 79464 .75812 38 .70472 66107 39 .60189 .55739 43 .49861 .45260 '

"ASSEMBI,Y 2D PIN POWEPP 2.2642 1.1704 1.4484 1.4909 1.4702 1.4648 1.4569 1.4634 1.4873 1.5091- 1.5419 1.5232 1.2491 1.3710 1.1603 1.4295 1.3153 1.4481 1.4143 1.4688 1.4665 1.4728 1.4912 1.4529 1,5048 1.3851 1.5261 1.2576 1.4275 1.3075 .00D0 .0000 1.5031 1.5281 1.4987 1.5049 1.5517 1.5446 .0000 .5000 1.3982 1.5480 1.4628 1.4328 .0000 .0000 1.5409 1.5634 1.5308 1.5371 1.5P85 1.5847 0000 .0000 1 5337 1.5881 1.4367 1.3912 1.4890 1.5336 1.6186 1.5636 1.5905 1.5972 1.5894 1.6660 1.5991 1.5737 1.4939- 1.5618 1.4256 1.4405 1.5065 1.5483 1.5557 1.5043 1.5810 1.5881 135109 1.6023 1.6157 1.5933 1.5450 1.5510 i 1 4124 1.4116 1.4699 1.5077 1.5734 1.5717 .0000 .0000 1.5990 1.6209 1.5736 1.5547 1.5352 1.5361 .

1.4124 1.4316 1.4699 1.5077 1.5734 1.5717 .0000 .0000 1.5990 1.6209 1.b736 1,5547 1.5352 1.5361 1.4258 1.4405 1.5065 1.5483 1.5557 1.5043 1.5810 1.5881 1.5309 1.6023 1.4157 1.5933 1.5450 1.5510 1.4367 1.3932 1.4890 1.5336 1.6186 1.5636 1.5905 1.5972 1,5894 1.6660 1.5991 1.5137 1.4939 1.5618 ,

1.4628 1.4128 ,0000 .0000 1.5409 1.5634 1.5308 1.5371 1.5885 1.5847 .0000 0000 1.5337 1.5881 >

1.4275 1.3075 .0000 .0000 1.5031 1.5281 1.4987 1.5049 1.5517 1.5446 .0000 0000 1.3982 1.5480 1.1603 1.4295 1,3153 1.4481 1.4143 1.4685 1.4665 1.4728 1.4912 1.4529 1,5048 1.3851 1.5261 1.2576_

1.2642 1.1704 1.44a4 1.4909 1.4702 1.4646 1.4569 1.4634 1.4873 - 1.5091 1.5479 1.5232 1.2491 1.3710 ,

a b

r l

ASAS Manual Revision 0 98 April 19,1994 1

I

Figurc 15 Sample ATS Output File Page 8 of 16 40 *A.wial Nodes

  • 2
  • Fields on File
  • 1
  • Case Number *
  • 3-10.5-A24*
  • Case ID*

100.000

  • Percent rull Power *

.77641E-02

  • Core Average AS1*

1.77003

  • Radial Peaking ractor trP1' 1.16769
  • Axial Peaking Factor
  • 1.18044
  • Assembly Peaking Factor
  • 19
  • Assembly Number
  • FQ-FLAffE 16 *
  • Reason For Selection *
  • F* 'RPOW-HPTH *
  • ASS-AX1AL *
  • 1 .45136 ,47071 2 .56215 .59980 3 71219 72809 4 .82428 .83753 5 .90120 .91003 6 .94830 .95150 ,

7 .98984 98866 8 1.03160 1.02789  !

9 1.06685 1.06183 10 1.08886 1.08308 11 1.10080 1.09470 12 1.11660 1.11005 i

?

13 1.13928 1,13208 14 1.15891 1.15125 15 1.1E554 1.15805 16 1.16260 1.15572 17 1.16554 1.15848 18 1.17771 1.17072 39 1.18769 1.18044 20 1.18407 1.17714 21 1.17046 1.16453 22 1.16334 1.15784 23 1.16635 1.16060 4 24 1.16773 1.16176 25 1.15578 1.15032 26 1.13399 1.12957 7 27 1,11837 1.11446 28 '1.11244 1.1b829 29 1.10484 1.10046 30 1.08411 1.08029 31 1.05313 1.05043 32 1.02495 1.02312 33 1.00248 1.00113 34 .97530 .97500 35 .93300 93540 36 .87466 .88095 37 79864 ,80846 38 .70472 71725 3 39 .60189 .61650 >

40 .49861 .51540  !

l

  • ASSF.MBl.Y 2D FIN POWERS * -

1,3175 1.2952 1.3918 1.3798 1.3674 1.3484 1,3487 1.3487 1.3484 1.0674 1.3798. 1.3918 1.2952 1.3175 1.3245 1.4285 1.3885 1.3934 1.4002 1.3555 1.3311 1.3311 1.3555 1.4002 1.3934 1.3685 1.4285 1.3245 1.4433 1.4082 .0000 .0000 1.3996 1.3784 1.3411 1.3411 1.3764 1.3496 .0000 0000 1.4082 1.4433 ,

1.4451 1.4273 ,0000 .0000 1,4035 1.3954 1.3592 1.3592 1.3954 1,4035 .0000 .0000 1.4273 1.4451 1.4431 1.4452 1.4246 1.4142 1.4466 1.4073 1.3998 1.3998 1.4D73 1.4466 1.4142 1.4246 1.4452 1.4431 1.4311 1.4071 1.4109 1.4141 1.4153 1.4495 1.4108 1.4108 1.4495 1.4153 1.4141 1.4109 1.4071 1.4311 1.4364 1.38E5 1.3773 1.3818 1.4122 1.4152 .0000 .0000 1.4152 1.4122 1.3818 1.3773 1.3865 1.4364 1.4404 1.3863 1.3754 1.3794 1.4128 1,4192 ,0000 .0000 1.4192 1.4128 1.3794 1.3754 1.3863 1.4404 1.4461 1.4187 1.4213 1.4247 1.4265 1.4646 1.4321 1.4321 1.4646 1.4265 1.4247 1.4213 1.4187 1.4461 1.4734 1.4730 1.4507 1.4399 1.4724 1.4335 1.4319 1.4319 1.4335 1,4724 1.4399 1.4507 1.4730 1.4734 1.4925 1.4724 ,0000 .0000 1.4431 1.4341 1.3990 1.3990 1.4341 1.4431 .0000 .0000 1.4724 1.4925 1.5108 1.4716 .0000 .0000 1.4535 1.4288 1.3901 1.3901 1.4288 1.4535 .0000 .0000 1.4716 1.5108 1.4039 1.5148 1.4690 1.4695 1.4711 1.4186 1.3874 1.3874 1.4186 1.4711 1.4695 1.4690 1.5148 '1,4039 3.4240 1.3983 1.5015 1 4815 1.4605 1.4288 1.4117 1.4117 1.4288 1.4605 1.4815 1.5015 1.3963 1.4240 E

i ASAS Manual Revision 0 99 April 19,1994 i

4 Figure 15 Sample ATS Output File q ^

Page 9 of 16 40

  • Axial Nredes*

2 *Fle1ds on File

  • 2
  • Case Numt.er*
  • B-10.5+J11*
  • Case 3D*
  • 20.000
  • Percent Full Power *

.20581E*00

  • Core Average As1*

2.33200 *padial Pesking Factor (FPl*

1.37822 'Axtel Peaking Factor *  ;

1.27083 ' Assembly Peaking ractor*

1

  • Assembly Number *
  • USER SELECT *
  • Peeson for Selection'
  • R* *RPOW.HPTH ' AS$- AX1AL
  • 1 .58414 78065 2 75266 .86673 3 .92019 .95242 4 1,06408 1.02881 5 1.16166 1.08696 6 1.21965 1.12944 7 1.26866 1.16796 8 1.31597 1.20521 9 1.35251 1.23500 10- 1.36919 1.25115 11 1,36988 1.25618 12 1.37165 1.26125 13 1.37022 1.26879 14 1.37750 1.27083 15 1.35736 1.25933 16 1.32139 1.23717 17 1.28599 1.21?ll 18 1.25487 1.20200 19 1.21943 1.18400 20 1.17105 1.15526 21 1.11419 1.11864 "

22 1.06808 1.08696 23 1.03704 1.06313 24 1,00947 1.03963 25 .97368 1.00897 26 .93262 .97355 27 90009 .94403 28 .87901 .92286 29 85977 90284 30 ,83256 .87661 31 79954 84646 32 ,77047 .81979 33 .74879 .79853 34 72497 ,.77622 35 .69127 .74628 36 64654 70874 37 .58814 .66482 3B .51554 61486 39 .43578 .56188 40 .35570 .50875

  • ASSEMBLY 2D PIN P'.MER$ *

.0502 .0530 0568 .0604 .0617 .0675 .0730 .c750 0742 .0754 .0773 .0789 .0806 .0842

.0576 .0639 0705 _0751 .0772 .0788 .0810 .c832 .0659 .0899 .0941 .0959 .0957 .0972

.0679 .0771 .0000 .0000 .0930 .0926 .0934 .0958 .3005 .1075 0000 .0000 .1136 .1127 '

.0801 .0904 .0000 .0000 .1081 .3076 .1083 .1110 .1165 .1243 .0000 .0000 .1306 .1291

.0945 .1028 .1125 .3190 .2218 .1240 .2261 .1293 .1341 .1397 1454 .3474 .3456 .3459 I

,1132 ,1171 .1240 ,1306 .1366 .3433 .1499 .1540 .1556 .1569 .1593 .1611 .1617 ,1640 '

l

.1402 .1354 .1390 .1451 .2528 .3646 .0000 .0000 .1809 .1779 .1786 .1799 .3810 .1838

.2620 .1565 .3602 .1666 .1749 .1867 .0000 0000 .2061 .2012 .2017 .2033 .3051 .2098

.1769 .1807 .1898 .2980 .2051 .2131 .2196 .2244 .2273 .2290 .2321 .2343 234R .2386

.3033 .2140 .2300 .2392 .2401 .2402 .2395 .2436 .2539 .2646 .2763 .2792 .2738 .2736

.2385 .2552 .0000 .0000 .2809 .2727 .2695 .2740 .2B77 .3085 0000 .0000 .3210 .3147

.2797 .2955 .0000 .0000 .3181 .3087 .3066 .3125 .3265 .3498 .0000 .0000 .3657 .3599

.3264 .31J2 .3469 .3530 .3493 .3476 .3527 .3613 .3706 .3866 .4049 .4111 .4063 .4107

.3854 .37R9 ,3823 .3861 ,3899 .3988 .4197 ,4339 .4319 .4389 .4488 .4566 .4629 .4788 1

1 ASAS Manual Revision 0 100 April 19,1994  ;

- -- . . - - - - . . . . .. . _ ~ ,-

Figure 15 Sample ATS Output File ,

Page 10 of 16 .

1 40 'Arial Nodes' 2 " Fields on File

  • 2 ' Case Number *
  • b-10.5-J12* ' Case ID*

20.000 ' Percent Full Power"

.20581E+00

  • Core Average AS!' j 2.33200 ' Radial Peakin0 Factor (FR)*

1.37822

  • Axial Feeking Factor" 1.36853 ' Assembly Peaking Factor' ,

13

  • Assembly Number
  • FQ-PI.ANE 1 *

"Peason For Selection *

  • F' " k POW - Hl'TH *
  • ASS- AX1AL
  • 1 .58414 .57013 i 2 75266 73565 3 .92019 .90025 .i e 1.0440s 1.04267 5 1.16168 1.14166 6 1.21965 1.20332 7 1.26866 1.25576 8 1,31597 1.30559 -,

9 1.3%251 1.34343 10 1.3e919 1.35991 11 1.36988 1.359.'8 12 1.37165 1.36094 13 1.37822 1.36840 14 1.37750 1.36853 15 1.35736 1.34763 t 16 1.32139 1.31029 17 1.28598 1.27722 18 1.25467 1.25311 19 1.21943 1.22565 20 1.37105 1.18266 21 1.13419 1.12877 22 1.06608 1.08464 23 1 03704 1.05496 24 1,00947 1.02765 1 25 ,97368 .99067 26 .93262 .94738 27 .90009 .91337 28 .87901 .89213 29 ,85977 .87270 30 .83256 .84418 31 79754 .00900 32 .77087 77875 33 74R79 75592  !

34 12497 73127  !

15 .69127 .69538 I 36 .64654 .64795 37 .54914 .596R4 3R ,51554 .51812 39 .41578 44155 40 .35570 36473

' ASSr.MALY 2D PIN POWERS * '

1.304R 1.1758 1.39H5 1.3084 1.4075 1.4224 1.4119 1.4119 1.4224 1.4075 1.3084 1 3985 1.1758 1.3048 2.1993 1.4264 1 3214 1.4375 1.3689 1.4251 1.4210 1.4210 1.4251 1.3689 1.4375 1.3214 1.4264 1.1993 1.4415 1.3410 .0000 .0000 1.4919 1.4888 1,4572 1.4572 1.4888 1.4919 .0000 .0000 1.3410 1.4475 ,

1.3718 1.4780 .0000 0000 1,4063 1.5152 1.4961 1.4961 1.5152 1.4063 .0000 - .0000 1.4780 1.3118 i' 1.4942 1.4256 1.5311 1.4245 1 5763 1.5499 1.5419 1.5419 1.5499 1.5763 1.4245 1.5311 1.4256 1.4942 1.5292 1.5034 1.5482 1.5552 1.5706 1.6045 1.4460 1.4460 1.6045 1.5706 1.5552 1.5482 1.5034 1.5292 1.5377 1.5199 1.5369 1.5577 1.5850 1.4666 .0000 ,0000 1.4666 1.5850 1.5577 1.5369 1.5199 1.5377 1.5579 1.539% 1.5567 1.5777 1.6059 1.4879 .0000 .0000 1.4879 1.6059 1.5777 1.5567 1.5395 1.5579 1.5936 1.5673 1.6140 1.6216 1.6376 1.6736 1.5101 1.5101 1.6736 1.6376 1.6216 1.6140 1.5673 1.5936 1.6027 1.5312 1.6442 1.5304 1.6921 1.6638 1.6558 1.6558 1.6638 1.6921 'l 5304 1.6442 1.5312 1.6027 1.bl61 1.6350 .0900 .0000 1.5557 1.6747 1.6536 1.6516 1.6747 3.5557 .0000 .0000 1.6350 1.5161 i 1.6475 1.5294 .0000 .0000 1.6994 1.6948 1.6588 1.6588 1.6948 1.6994 .0000 .0000 1.5294 1.6475 1.4076 1.6762 1.5537 1.6887 1.6077 1.6718 1.6665 1.6665 1.6718 1.6077 1.6887 1,5531 1.6762 1.4076  !

1.5796 1.4257 1.6950 1.5857 1.7040 1.7213 1.7060 1.7080 1.7213 1.1040 1.5857 1.6950 1.4251 1,5796

?

,i t

ASAS Manual Revision o 101 April 19,1994

- . . . - - .. . ~

I I

i 1

Figure 15 Sample ATS Output File Page 11 of 16 40

  • Axial Nodes
  • 2
  • Fields on File" 2
  • Case Number *
  • B-10.5-J13*
  • case ID*

20.000

  • Percent Full Power * '

.20581t+00

  • Core Average ASI*

2.33209 'Padial Peakirg Factor (FPl*

1.3782

  • Axial Peaking Factor
  • 1,35690
  • Assembly Peaking Factor" 16 " Assembly Numter*

FQ-PLANr. 3 *

  • Reason For Selection *
  • K* 'RPOW-HFTH * " ASS-AZIAL
  • 1 .58414 .49767 2 .752f6 .67229 3 .92019 .84597 4 1.06408 .99702 5 1.16168 1.10375 6 1.21965 1.17209 1 1.26866 1,22954 8 1.31597 1.28260 9 1.35251 1.32257 10 1.36919 1.34071 11 1.36988 1.34155 12 1.37165 1.34462 13 1.37822 1.35423 14 1.37750 1,35690 15 1.35736 1.33911 16 1.32139 1.30563 17 1.28598 1.27787 la 1,254a7 1.26060 19 1.21943 1.24034 20 1.17105 1.20364 21 1.11419 1.15514 22 1.06808 1.11572 2J 1.03704 1.09009 24 1.C0947 1.06554 25 97368 1.02943 26 .93262 .98548 27 .90009 .95077 28 .87901 .92906 29 .85977 .90378 30 .83256 87826 31 79954 .84016 .

32 .77087 ,80686 33 74879 78107 34 .72497 75261 35 .69127 .71141 36 .64654 .65701 37 .58814 .58937 38 .51554 .50880 39 .43578 .42161 40 .35570 .33412

' ASSEMBLY 2D FIN POWF.FS*

1.1111 1.0547 1.3456 1.4208 1.4287 1.4487 1.4644 1.4864 1.5189 1.5505 1.5989 1.5750 1.2909 1.4358 1.0509 1.3294 1.2550 1.4135 1.3943 1.4496 1.4837 1.5035 1.5325 1.4989 1.5673 1.4405 1.5866 1.3219 1.3372 1.2519 .0000 .0000 1.5125 1.5410 1.5259 1.5431 1,6039 1.6091 .0000 .0000 1.4588 1.6337 1.4092 1.4076 .0000 .0000 1.5710 1.5964 1.5708 1.5857 1.6462 1.6557 .0000 .0000 1.6025 1.6749 1.4153 1.3870 1.5087 1.5698 1,6611 1.6104 1.6459 1.6590 1.6527 1.7360 1.6718 1.6405 1.5480 1.6403 1.4341 1.4613 1.t428 1.5951 1.6105 1.5606 1.0595 1.6713 1.5969 1.6720 1.6819 1.6547 1.6013 1.6232 1.4507 1.4761 1.5227 1.5708 1.6477 1.6612 .0000 .0000 1.6966 1.7039 1.6451 1.6162 1.5922 1.60.17 1.4144 1.4980 1.5426 1.5887 1.6638 1.6758 .0000 .0000 1.7069 1.7123 1.6515 1.6210 1.5957 1.6039 1.5082 1.5295 1.6069 1.6537 1.6625 1.6058 1.7014 1.7087 1.6270 1.6977 1.7028 1.6709 1.6130 1.6312 1.5416 1.4988 1.6164 1.6685 1.7526 1.6879 1.7152 1.720.2 1.7039 1.7805 1.7067 1.6675 1.5674 1.6545 1.5920 1,5703 .0000 ,0000 1.6944 1.7051 1.6634 1.6669 1.7170 1.7148 .0000- .0000 1.6306 1.6959 1.5696 1.4447 ,0000 .0000 1.6675 1.6835 1.6412 1.6436 1.6918 1.6823 .0000 .0000 1.4920 1.6614 1.2952 1.5878 1.4644 1.6216 1.5723 1.6296 1,6204 1.6217 1.6346 1.5820 1.6379 1.4926 1.6317 1.3519 1.4208 1.3065 1.6248 1.6749 1.6479 1.6373 1.6231 1.6229 1.6387 1.6529 1.6856 .1.6444 1.3377 1.4808

)

1

\

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i l

1 l

ASAS Manual Revision 0 - 102 April 19,1994  ;

I

Figure 15 Sample ATS Output File Page 12 of 16

  • 40
  • Axial Nodes
  • 2 *Flelds on File
  • 2
  • Case Number *
  • B-10.5-J14' ' Case ID*

20.000

  • Percent Full Power *

.20581E*00

  • Core Average ASI*

2.33200

  • Radial Peaking Factor (FR)*

1.37822 ' Axial Peaking Factor

  • 1.34918
  • Assembly Peaking Factor
  • 11 ' Assembly Numtgr*
  • i FQ-PLAN 8 16* *
  • Reason For Selection *
  • K* "RPOW-HPTH
  • ASS-AKIAI.
  • 1 .58414 .53356 2 .75266 69656 3 .92019 .85871 4 1.06408 1.00022 5 1.16168 1.10132 6 1.21965 1.16741 7 1.26866 1.223*6 8 1.31591 1.27564 9 1.35J51 1.31499 10 1.36919 1.33291 11 1.36948 1,33386 12 1.37165 1.33701 13 1.37822 1.34651 14 1.37750 1.34918 15 1.35736 1.33176 16 1.32139 1.29893 17 1.28594 1.27151 18 1.25487 1.25434 19 1.21943 1.23413 20 1.17105 1.19786 21 1.11419 1.15004 22 1.06808 1.11108 23 1.03704 1.08556 1 24 1.00947 1.06114 25 .97368 1.02546 26 .93262 .98217 27 .90G09 94793 24 87901 92635 29 .B5977 .90618 30 .83256 .87608 31 .79954 .83801 32 .77081 40593 '

33 ,74879 ,78062 34 72497 75278 35 .69127 71261 e 36 .64654 .65979 37 58814 .5957E 38 .51554 .52094 39 .43578 .44068 40 .35570 .36017

  • AS$FMULY 2D FIN POWER $*

1.2800 1.1586 1.3781 1.2887 1.3444 1.3980 1.3871 1.3891 1.4032 1.3919 1.2976 1.3905 1.1718 1.3009 1.1800 1.4129 1.3110 1.4247 1.3554 1.4093 1.4052 1.4064 1.4121 1.3592 1.4305 1.3183 1.4253 1.1975 1.4300 1.33t5 ,0000 .0000 1.4832 1.4782- 1.4466 1.4473 1.4795 1.4850 .0000- .0000 1.3434 1.4480 1.3617 1.,4777 .0000 .0000 1.4025 1.5082 1.4R86 1.4888 1.5062 1.4022 .0000 .0000 1.4828 1.3747 1.4884 1.4218 1.5353 1.4260 1.5735 1.5445 1.5354 1.5356 1.5438 1.5722 1.4242 1.5343 1.4313 1.4985 1.5278 1.5098 1.5535 1.5567 1.5679 1.5999 1.4408 1.4400 1.5977 1.5659 1.5539 1.5507 1.5049 1.5338 1.5398 1.5267 1.5408 1.5567 1,5795 1.4597 .0000 .0000 1.4585 1.5776 1.5536 1.5368 1,5232 1.5410 1,5603 1.5452 1.5583 1.5736 1.5967 1.4783 .0000 .0000 1.4769 1.5945 1.5700 1.5533 1.5399 1.5583 1.5925 1.5700 1.6121 1.6135 1.6238 1.6566 1.4973 1.4969 1.6554 1.6211 1.6090 1.6061 1.5637 1.5897 1.5971 1.5302 1.4369 1.5183 1.6708 1.6395 1.6330 1.6332 1.6384 1.6682 1.5138 1.6308 1.5238 1.5944 1.5061 1.6261 .0000 .0000 1.5304 1.6424 1,6227 1.6228 1.6415 1.5281 .0000 .0000 1.6208 1.5042 1.6295 1.5161 .0000 .0000 1.6635 1.6546 1.6197 1.6194 1.6540 1.6621 .0000 .0000 1.5126 1.6294 1.3921 1.6589 1.5333 1.6580 1.5732 1.6296 1.6215 1.6207 1.6287 1.5719 1.65E4 1.5314 1.6570 1.3923 1.5737 1.4;40 1.6861 1.5714 1.6798 1.6883 1.663) 1.6612 1.6852 1.6770 1.5688 1.6835 1.4210 1,5712 s

l I

1

)

ASAS Manual Revision 0 103 April 19,1994 4

$,a j

-~ _

. - ~. . . - _-

Figure 15 Sample ATS Output File Page 13 of 16 40

  • Axial Nodes
  • 2
  • Fields on File
  • 2
  • Case Number *
  • s-10.5-J15"
  • Case ID*

20.000

  • Percent rull Power *

.20581E*00 " Core Averego AE1*

2.33200 *Redial Peaking Factor (FRl' 1.37822 *Aaial Peaking Factor

  • 1.41253
  • Assembly Peaking Factor
  • Reason For Selection *

'E' 'PP(M-HPTH * " ASS-AX1AL

  • 1 .58414 .58975 2 .75266 76083
  • 3 .92019 .93096 4 1.06408 1.07857 5 1.16168 1.18209 6 1.21965 1.24749 7 1.26846 1.30259 8 1.31597 1.35394 9 1.35251 1.39229 10 1.36919 1.4083A 11 1. 36 9E 8 1.40668 12 1.37165 1.40665 13 1,37822 1.41253 14 1.37750 1.4099H 15 1.35736 1.38463 16 1.12139 1.34101 17 1.28598 1.29957 18 1.254A1 1.26499 19 1,21943 1.22627 20 1 17105 1.17251 21 1.11419 1.10870 22 1.04808 1.05677 23 1.03704 1.02172 24 1.00947 .99101 25 97364 .95220 '

26 .93262 .90641 27 .90009 .R7427 24 87901 .85296 29 .85977 .R3381

.10 .83256 .60611 31 79954 .77217 32 77087 .74302 33 74979 72109 34 .72497 .69711 35 .69127 .46199 36 .64654 .61542 37 .58814 .55821 38 .51$54 .49067 39 .43578 .41747 40 .35570 .344R5

" AS$DiBLY 2D FIN POWI PS*

1.3R04 1.2398 1.4901 1.3R77 1.4896 1 5074 1.5002 1.5055 1.5208 1.5096 1.4118' 1.5206 1.2659 1,4035 1.2614 1.5163 1.3726 1.4843 1.4412 1.5367 145045 1.5091 1.5194 1.4606 1.5108 1.4020 1.5494 1.2795 1.5296 1.3848 .0000 .0000 1.5239 1.5568 1.5307 1.5353 1.5705 1.5459 ,0000 .0000 1.4185 1.5518 1.4314 1.5046 .0000 .0000 1.4232 1.5673 1.5542 1.5588 1.5819 1.4457 .0000 .0000 1.5454 1.4592 1.5398 1.4647 1.5351 1.4266 1.6067 1.5843 1.5812 1.5858 1.5998 1.6335 1.4598 1.5182 1,5082 1.5746 1.5565 1.5325 1.5705 1.5716 1,5866 1.6172 1.4309 1.4351 1.6329 1.6132 1.6106 1.6161 1.5808 1.5978 1.5394 1.5286 1.5455 1.5627 1,5859 1.4330 .0000 ,0000 1.4453 4.6102 1.5975 1.5896 1.5792 1.5901 1.5391 1.5295 1.5472 1 5652 1.5889 1.4365 .0000 .0000 1.4492 1.6136 1.6003 1.5918 1.3807 1.5907 1.5576 1.5368 1.5??0 1.5818 1.5959 1.6276 1.4409 1.4458 1.6442 1,6237 1.6202 1.6244 1.5873 1.6014 1.5431 1.4725 1.5462 1. 4."+ 8 1.6228 1.6013 1.5990 1.6043 1.6181 1.6514 1.4752 1.5925 1.5196 1.5821 1 1.4373 1.5160 .0000 .0000 1.4438 1.5914 1.5791 1.5841 1.6075 1.4687 .0000 .0000 1.5617 1,4701 1.5396 1.3991 .0000 .0000 1.5521 1.5881 1.5678 1.5674 1.6033 1.5771 .0000 .0000 1,4362 1.5704 1.2741 1.536) 1.1956 1.5137 1.4741 1.5437 1.5421 1.5470 1.5574 1.4961 1.5443 1,4297 1.5747 1.2969 1.4043 1.2603 1.5188 1.4192 1.5279 1.5490 1.5417 1.5459 1.5616 1.5483 1.4451 1.5518 1.2892 1.4287 i l

1 l

l 1

l 1

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ASAS Manual Revision o 104 Apnl 19,1994 j l

j L

Figure 15 Sample ATS Output File Page 14 of 16 40 'Axlal Nodes' 2 'rields on File

  • 2 ' Case Number'
  • p-10.$-J21*
  • Case 3D*

20.000

  • Percent Full Power *

.20581E*00 " Core Avera2e ASI' 2.33200

  • Radial peaking Factor trRI' 1.37822 " Axial Peaking Fact or' 2.33216 ' Assembly Pesking Factor" 10
  • Assembly Number *
  • Reason For Selection *

'R' 'RPOW-MrTH * ' ASS-AX1AL

  • 1 58414 .51095 2 75366 68154 J .92019 .85116 4 1.06408 .99726 5 1.16168 1.09732 6 1.21965 '1.15789 7 1.26866 1.20905 8 1.31597 1.25794 9 1.35251 1.29575 10 1.36919 1.31365 11 1.36988 1.31*68 12 1.37165 1.31949 13 1.37822 1.32897 14 1,37750 1.33216 15 1.35736 1. 31'f 05 s 16 1.32139 1.28790 17 1.28t98 1.26369 18 1.25487 1.J4861 19 1.21943 1.23065 20 1.17105 1.19780 21 1.11419 1.15415 22 1.06808 1.11828 21 1.03704 1.09415 24 1.00947 1.07104 25 .97368 1.03704 26 .93262 99514 e

(

27 .90009 96272 2a 87901 94172 29 .85977 .92120 30 83256 .89180 31 .79954 .85556 32 .77087 .82365 33 .74879 79856 34 .72497 77117 35 .69127 73234 36 .64654 .68096 37 .58814 .61417 38 .51554 .51145 39 .43578 .44062.

40 .35570 .34945

  • ASSrMBLY 2D FIN FOWEPs*

7175 .7644 8829 .9326 .9656 .9931 1.0256 1.0623 1.1150 1.1765 1.2356 1.2728 1.1931 1.2310 1079 8410 .8801 .9391 .9922 1.0008 1.0220 1.0564 1.1204 1.2065 1.24A6 1.2752 1.3333 1.2301

.7772 .8356 .00C0 .0000 1.0038 1.0313 1.0443 1.0789 1.1562 1.2266 .0000 30000 1.3276 1.3664 7916 .8595 .0000 .0000 1.0273 1.0601 1.0776 1.1142 1.1877 1.2539 .0000 .0000 1.3610 1.3897

.8042 .8450 9400 .9982 1.0692 1.0904 1.1321 1.1741 1.2179 1.2975 1.3172 1,3492 1 3827 1.3927

.8177 ,8775 .9463 1.0D76 1,0658 1.1422 1.1763 1.2256 1.2728 1.2817 1.3134 1.3394 1.3544 1.3955

.842a .887c .9444 1.0068 1.0864 1.1541 .0000 .0000 1.2889 1.3001 1.2978 1.3188 1.3508 1.4133

.8711 9150 .9721 1,0346 1.1163 1.1874 .0000 0000 1,3276 1.3332 1.3276 1.3459 1.3750 1.4397

,9066 .9678 1.0398 1.1013 1.1573 1.2331 1.2657- 1.3195 1.3599 1.3692 1.3991 1.4213 1.4297 1.4715

.9591 1,0458 1.1042 1.1623 1.2313 1.2401 1.2753 1.3193 1.3629 1.447a 1.4642 1.4900 1.5109 1.5213 1.0192 1.0898 .0000 .0000 1.2523 1,2716 1.2739 1.3116 1.3897 1.4606 .0000 .0000 . 5489 1.5707 1.0714 1.1311 .0000 .0000 1.2911 1.3027 1.2987 1.3320 1,4133 1.4874 .,0000 .0000 1.5572 1.5960 1.0378 1.2098 1.2404 1.2972 1.3413 1.3297 1.3391 1.3696 1.4302 1.5163 1.5571 1.5645 - 1.6218 1.4725 1.1127 1.1583 1.3121 1.1556 1.3149 1.3907 1.4195 1.4542 1.4930 1.5478 1.6001 1.6242 1.4911 1.5396 ASAS Manual Revision 0 105 April 19,1994 i

.,- .., ~ .:-- ,. -

y

k i

l Figure 15 Sample ATS Output File Page 15 of 16 40 . " Axial Modes

  • 2
  • Fields on File
  • 2
  • Case Number *
  • B-10.5-J22* = case 1D*

20.000

  • Percent Full Power *

.20581E+00

  • Core Average ASI*

2.33200

  • padial Peeking Factor (FP.)
  • 1.37822
  • Axial Peaking Factor
  • 1.52250
  • Assembly Peaking Factor
  • 39 ' Assembly Number *
  • USER SELECT * *Peason For Selection *
  • F* *RPOW-HPTH *
  • ASS-AX1AL
  • 1 .58414 .83171 2 75266 .97502 3 .92019 1.11759 4 1.06408 1.24213 5 1.16168 1.33141 6 1.21965 1.38989 7 1.26866 1.43850 8 1.31597 1.48310 9 1.35251 1.51275  :

10 1.36919 1.52250  !

11 1.36989 1.51527 12 1.37165 1.50819 13 1.37822 1.50489 14 1.37750 1.49066 15 1.35736 1.45078 16 1.32139 1.3k949 17 1.28598 1.32625 le 1.25487 1.20561 19 1.21943 1.19988 20 1.17105 1.12143 21 1.11419 1.03539

' 22 1.06808 .96357 23 1.03704 .91097 24 1.30947 .86711 25 .97368 .82147 26 .93262 .77617 27 90009 ,74157 28 .87901 71984 29 85977 4,70197 30 .83256 .67879 31 79954 .65202 32 .77087 .63001 33 74879 .61448 34 72497 .59701 35 .69127 .55sie 36 .64654 53074 37 .58814 ..48279 38 .51554 .42558 ,

39 .43578 .36368 40 .35570 .30159

  • ASSDtBLY 2D PIN POWERS * .

1644 .6423 7199 .6688 .7494 7956 .8071 .8071 7956 47494 .6688 .7199 .6423 7644

.6430 .6661 .4959 .5204 ,6128 .1190 7531 7531 .7190 .6128 45204 .4959 .6661 .6430 7214 .4964 .0000 .0000 .5047 6726 7145 .7145 .6726 .5087 .0000 .0000 .4964 .7214

,6706 .5213 ,0000 .0000 .4602 ..6384 .6761 .6761 ,6384 .4602 ,0000 .0000 .5213 .6706 7518 .6142 .5095 .4605 .5856 6150 .6201 .6201 .6150 .5856 .4605 .5095 .6142 7518 7983 .7210 6738 .6391 ,6153 .5709 .4340 .4340 .5709 6153 .6391 .673b 7210 .7983

.809a 7551 7160 .6771 .6206 .4341 ,0000 .0000 .4341 .6206 .6771 ,7160 7551 .8098

.8098 7551 '.7160 .6771 .6206 .4341 .0000 .0000 .4341 .6206 .6771 7160 .7551 .8098 7983 .7210 .6738 .6391 .6153 5709 .4340 .4340 .5709 .6153 ,6391 .6738 7210 .7983

.7518 .6142 .5095 .4605 .5856 ..6150 6201 ,6201 .6150 .5856 4605 .5095 .6142 .7518

.67D6 .5213 .0000 .0000 .4602 .6384 .6761 ,6761 .6384 .4602 .0000 .0000 .5213 .6706 7214 .4964 '.0000 .0000 .5087 6726 .7145 7145 .6726 .5087 . .0000 000' .4964 .7214 '

.6430 .6661 .4959 .5204 .6129 ,7190 7531 7531 .7190 6128 ,5204 49's .6661 .6430 i 7644 .6423 .7199 .6688 7494 .7956 .5071 .8071 7956 7494 .6688

. .71 4 .642) 7644 1

l i

l ASAS Manual Revision o .106 ' April 19,1994

---w-" s- c y

Figure 15 Sample ATS Output File Page 16 of 16 -

40

  • Axial Nodes
  • 2 *Flelds on Flie*

3

  • Cave s ' umber *  ;

J

  • a-10.5-J23*
  • case 13*

20.000 'Perriat Full Power *

.20581E+00  ;..e Average AS1*

2.33200 *h dial Peaking Factor f rR )

  • 1.37822 'A:tal Peaking Factor
  • 1.36887 *As.embly Peaking Factor
  • 35
  • Assembly Number
  • FQ-PLANE 1 * 'Reas,n For Selection *
  • E' 'APCW-dPTH * 'ASSWsXIAL
  • 1 .58414 .51 '72 2 75266 ,693R7 3 .92019 .66903 4 1.06408 1.02054 5 1.16168 1.12574 6 1.21965 1.19106 7 1.26866 1.24617 a 1.31597 1.29809 9 1.35251 1.33756 10 1.36919 1.35531 11 1,36988 1.35581 l 12 1.37165 1 35839 13 1,37822 1.36732 14 1.37750 1.36887 15 1.35736 1.34932 16 1.32139 1.31335 17 1.28598 1.28219 l 18 1.25487 1.26053 19 1.21943 1.23560 20 1.17105 1.19459 21 1.11419 1.14224 22 1.06808 1.09964 23 1,03704 1.07155

.' 4 1.00947 1.04541 25 .97368 1.00873 26 .93262 .96504 i 27 .90009 .93C69 28 .87901 ,90926 29 .85977 .88944 30 .83256 .85986 31 .79954 82311 32 77067 .79126 33 .74879 76692 34 .72497 74051 35 .69127 .70241 36 .64654 .65179 37 .58814 .58760 38 .51554 .50957 39 .43576 .42461 4D .35570 .33914

  • ASf!MBLY 2D PIN POWEFS*

1.4662 1.3509 1.6757 1.7244 1.6944 1.6833 1.6717 1.6760 1.6963 1.1162 1.7565 1.7191 1.3986 1.5348 1.3427 1.6552 1.5267 1.6834 1.6305 1.6905 1.6835 1.6876 1.1039 1.6532 1.1175 1.5693 1.7150 1.4056 1.6609 1.5222 .0000 .0000 1.7490 1.7660 1.7236 1.7277 1.7807 1.7749 .0000 .0000 1.5811 1.7412 1.7066 1.6759 ,0000 .0000 1.7983 1.8092 1.7657 1.7702 1.8256 1.8271 .0000 .0000 1.7437 1.7931 1.6754 1.6206 3.7429 1.7951 1.8827 1.8110 1.6394 1.8443 1.8286 1.9146 1.9396 1.8005 1.6893 1.7633 1.6631 1.6779 1.7565 1.8021 1.8068 1.7403 1 8411 1.8469 1.7592 1.8389 1.8482 1.8161 1.7504 1.7521 1.6501 1.6679 1.7100 1.7536 1.8293 1.8350 .0000 .0000 1.8548 1.6624 1.7991 1.7684 1.7403 1.7389 1.6501 1.6679 1,7100 1.7536 1.8293 1,8350 .0000 .0000 1,8548 1.8624 1.7991 1.7684 1.7403 1.7389 1.6631 1.6779 1.7565 1.8021 1.8068 1.7401 1.8411 1.8469 1,7592 1.8389 1.8482 1.8161 1.7504 1.7521 1.6754 1.6206 1.7429 1.7951 1.8827 1.8110 1.8394 1.6443 1.8286 1.9146 1,8396 1.8005 1.6893 1.7633 1.7066 1.6759 ,0000 .0000 1.7983 1.8092 1.7657 1.7702 1.8256 1.8271 .0000 .0000 1.7437 1.1931 1.6608 1.5222 ,0000 .0000 1.7490 1.7660 1.7236 1.7277 1.7807 1.7749 ,0000 ,0000 1.5811' 1.7412 1.3427 1.6552 1.5267 1.6838 1.6305 1.6905 1.6835 1.6376 1.7039 1.6532 1.7175 1.5693 1.7150 1.4056 1.4662 1.3509 1.6757 1.7244 1.6944 1.6833 1,6717 1.6760 1.6963 1.7162 1.7565 1.7191 1.3986 1.5348 i

I l

ASAS Manual Revision 0 107 April 19,1994

Y.n

$ FIGURE E AXIAL POWER SHAPES FOR CORE AVERAGE i E CASEID = B-10.5-A PDil CASE A - 100% POWER, ARO E

40 PLANE AVERAGE = 1.00000 l:

o 1.6 1.4 1.2 m f O $

1.0 j ( h%

Yh

- g 3m y a w s  % -i]me

n. >

7 N (

E-d!

e ea w 0.8 [" ] g]3M P

5 7 l 5 5

a g

1 e 0.6 / \ o i g_ g 0.4 }

0.2 Y

E

_G 0.0 g 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 FRACTION OF CORE HEIGHT

h

$ FIGURE AXIAL POWER SHAPES FOR FUEL TYPE TYPE 2 S CASEID = B-10.5-J PDlL CASE J - 20% POWER, BANK 3 AT 574

? ASSEMBLY NUMBER 30 i: 40 PLANE AVERAGE = 1.00000 s

o 1.6 1.4 1.2 P .~ Cn

+

E s* s 'o 3

2 I  %+ N #73m

>9 %2 O

1 --

l Q h.  ?) to cn g 2oO W 0.8 -

2 /  % = "o OWM Et

$ h s o m w

  • 0.6 5

m

~\

S L

0.4 0.2 l

1

_G 0.0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 g

FRACTION OF CORE HEIGHT I

- .- = - . - - -._

\

Figure 17 POSTER. TOP File Added to Top of ASAS Plot Filo Prior to Plotting Page 1 of 5 4tPs-Adobe.2.0 EPSF 4%Creatorer JPG SW MEC JWK (YAEC)

%%Creatiork Dat e 11/17/91

%QTitlet POSTER 7. EPS

%%8oundington 0 0 792 612

%QPages 0 MDocumentFontsa Helvet ica Symbol

%%Endcomments

/STAPT (statundiet /lettertray known (statusdict begin lettertray end) if

/shwpge (showpage) det

% Added for OrPD

/printerswitch 1 def

/colorswitch 0 def

/slideswitch 0 der

% Added for oPro

/ print er switchar ray ( 1 0 0 1 1 1 1 0 1 ] def

/colorswitcharray [ 0 1 1 1 0 0 0 1 0 ) def

/alldeswitcharray ( 0 0 0 D 0 0 0 0 0 1 def

/versionarray ((47.0) 12.1 ) ( $ 4 . 0 ) ( 2 011.108 b ( 50. 5 ) ( 52. 2 ) t 2011.110 ) (1007.1 ) ( 2010.118 ) ) def 4 lNEC890lIGSD)(GSWI)(TEKTPQNX) (IA5ERJT 4 i IXVIEW) (LASERJT1) 0 1 versionarray length 1 sub (/whichewitch exch det versionarray whichswitch get t version eq (colorswitcharray whichewitch get /colorswitch exch det printer switchar ray whichewit ch get /printerswitch excn det slideswitcharray whichswitch get /slideswitch auch def lif ) for save Posterdict? begin 1 setlinewidth 0 setlinecap 0 setlinejoin

() O setdash 0 setgray 10 setmiter11mit /wp D def /LGL 0 det) def ,

/ FINISH (end restore shwpge) def

/Posterdict? 500 dact def Posterdict7 begin stack

% ~ arrays and stringe

/istrg 12 string def

/sbtyp 16 def /sbary obtyp array def

/1 gary sbtyp array def /1 stag 80 string def /legx O def ,

/t xtseg 100 array def /subseg 3 00 array def

/ sites  ! IMD) (MEl (59) (SP) ( R 2.) (LWil def %v3.0 .

/aaenum 'l 00 42 95 94 126 64 1 def tv3.0

/ a sect.ar (*) (*) (.) (*) l-) len 1 def tv1.0 ffontt (HFNOH) (HFN3Hb (SFNOH)] def

/intnum 00 58 61 ) def

%-~ common macros

/s /shcw load def

/ inch (72 mul) def

/init (emch inch exch inch) def

/actn ( { st agwp) (pop) (s)) def

/fotse (thgt mul) def

/cystag (/istrg 12 string def intrg cys) bind def

'/strgwp (stringwidth pop) bind det

/r ( findf ont. exch dup /that exch def scalefont settont) def

/FNOH (findfont euch scalefcnt setfont) def

/HF (/Helvetica F) def

/SP (/ Symbol F) def

/ HFf0H (/Helvetica FNOH) def

/SFNOH (/ Symbol FNOHl de!

/F7FTMULT (/fontmult exch def) def

/FtrtMULT2 (/f ontmult2 exch def ) def

/FKrMULT1 (/fontault3 exch det) def

/0ELX57 (/deixstrt exch det) de!

/DELYST (/delystrt exch det) def

/XBOXM (/aben exch del) def

/YBOXM (/ybox each det) def

/ TRIM (Itril each def) def L

/YBoxMAR (/ year euch def) def

/XAXE34DS( / xnoenda exch def) de f

/YAKENDS(/ynoends each det) def '

/MD (0mave 1.0 intse fontt ifnt get evx exec actn ipsa get exec gresterol def

/grynam 1 def /gryman 0 det

% ~ page formats

/P14TSFTUP 4 set inital plot values (tilina O def /yaf 0.0 def /irot I de f /y f a de f lymar . 05 de f

/deixatst 0 def /delystrt 0 def /fontault I def /sigeall 0 def 7

/fontmult2 1 def /fontmult! I def /x.ogdat 0 def /ylogdat 0 def r

/naxdia O def /xnoends o def /ynoends o def

/datal 11 def / data 2 [] def /datal () def /datastar () def

/ data 4 () def / data 5 () def / data 6 [] def /graydat () def /colordat () def

/boxin () def /fueltype () def / enrichment () def /triin 11 def

' /ilmax -1 def /12 max -1 def /ilmax -1 def /dateaxis 0 def

/14 max -1 def /15 max -1 def /16 max -1 def '

/mycycle O def /xbox 0.5 def /ybox 0,1 def /bindwid 0 def 14L 0 eq ( /mit 7.50 inch der /x1 10.25 inch def /xo 0 25 inch def l

/ylf 5.00 inch def /y1 7.50 inch def tyo 0.50 inch det)

(/xit 10,50 inch def /x1 11.25 inch det exo 0.25 inch def tylt 6.00 inch def /y1 8.00 inch def /yo 0.50 2nch del) ifelse wp 1 It (yo x1 xo a11 t ranslate 270 rotate)

(grinterswit ch 0 eq (xo .25 sub yo translate .9 ,9 scale }

ASAS Manual Revision 0 110 April 19,1994 l

F

,. - - --. , . . , - . , , ~-

l Figure 17 l

POSTER. TOP File Added to Top of ASAS Plot File Prior to Plotting Page 2 of 5 (so yo translate) ifelse ) ifelse

/xof 0 def /yof 0 det 14 HF

) band det

%--- frame formats

/P1hTFRAME (gsave 4 2 roll Irot i eq (I add exch 1.5 add exch) ( .'15 add exch .5 aM exch) ifelse init translate 10 HF

/yf exch def /mi exch def Iyaf 0 def

/ylt ylf yf avi def /xif x1f xf mol def

/iline o def /iplcre 1 det ) def

/RESrf Pli/T (prestore /ylf ylt yf div def /alf x1f xf div def} def

/sigdig 3 def

/sigmult (10 sigdig exp) def

/SIODIGIT (/sigdag exch def

/siocall 1 det) def

/CLIPON tv3.0 (9save newpath 0 0 moveto 0 yli lineto x1f ylf 1sneto x1f 0 lineto closerath clip) def

/CL3POFF tv3.0 (grestore) def

/ FPAMETITLE (12 fontmult mol HF x1f ,5 mul de1xstrt Anch adj /xtremerit exch def inch ylf aM delyst rt inch aM /yf rametit exch def xframetit yftametit CI'PNT 12 NF ) def

/CTRNT

(/1pns -0.5 def moveto FRINT2) def

/ FOPMAT

( lifnt 2 def /iste 7 def d.p 0 get  % cheek ist char I

j (dup intous ifnt get eq lexit) af

/ifnt ifnt 1 sub det Alot 0 eq fexit) If

) loop pep i f r+t 0 gt

{r 1 get Scheck 2nd char soup seenum late get eq (exit) if

/isze (sze 1 sub def isse 0 eq (exit) if

) loop pop isse 0 gt (1ste 3 pt (subseg di 1 put) (subseg di 0 put) ifelse stechar isse get search (pop pop) it) if sizes isse get evx exec

) (subseg di 0 put MD) itelse ipss O eq ftxtseg di 3 -1 roll put) if I def

/DLIMTR

( (t//) search (dup lengt h 0 at (3 da ail I soll pep /di da 1 aM def t (pop pct) ifelse)

(di 0 gt ( di 1 add i s oll ) if /dl di 1 aM c'/f exit) ifelse ) loop } def

/CSHOW

(/ ipos -0.5 det PRINT 2) bind def

/CYtHOW (osave dup stagwp / temp exch det t emp yaf gt ( / ya f t emp del l if ty 0 at itemp 0 exch rmoveto) if ty -1 eq (temp yax2maglen sub 0 exch rmoveto) if

%RIGHT JUSTIFT YAXIS2 LABELS 10/91 2'10 rotate 0 that 0.5 mot neg 2 3 div mul tmoveto a gu estore) bind def

/PPINT2

(/oldfhqt2 ihqt det fontsult) fntec HF dup length 0 gt (

dup dap /ipsa O def /tc.t 0 det

(/d1 0 def DLIMTR /deeg di def (ipsa 1 eq ( di 0 gt (subseg di get I eq (subseg di 1 sub get 1 eq ftxteeg di get txtseg di 1 sub get vt (txteeg di 1 sub txtseg di get put tatseg di 0 put)

(turseg da O put) ifelse 1 .i f ) if ) if / tot tot tatseg di get add def ) If npas 2 eq (

l~ di daeg ne (txtseg di 1 add get 0 Imoveto)

(tot ipos mul 0 reoveto) ifelse f

ilf FOPMAT /di di 2 sub def di 1 It (ewit) if 11oop spas 2 It (/Jpea ipso 1 add def) (exit) ifelse ) locp

) ( pc p ) ifelse oldfhgt2 HF

) def 4-- avis pr ocessing

/XAXIS  % label.minrzt, stp, maxrr t ,grd.tek on st ack

(/a1 not def /a2 yof def /b1 alt def /b2 ylf det ity 0 def

/noends xnoends def /mlogdat 0 def ASAS Manual Revision 0 111 April 19,1994

l 1

1 1

1 Figure 17

- POSTER. TOP File Added to Top of ASAS Plot File Prior to Plotting Page 3 of 5 este /stek tch def /retp stp def

/xscale L1 mausse minass sub dsv def /xmin minnes def

/munite (smin sub uscale mull def i

/rzunite (mscale mul) def

)def {)

/VMIS 4 label,minsa s, stp,maxr as,grd. t ek on st ac k 1

(/a1 yof def /a2 alf def /b1 y11 det /b2 ref def / t y 1 de f / ylogdet 0 def -]

/hoends ynoervSe det goevo e2 yof translate 90 rotate anta greetore

/yscale L1 manass miness sub dav def /ymin minsas def

/yunits (31nin aub yacale m418 der Iryunit s (yscale av1) dat )def taxis timbel,minssa,s*p siansas.grd.tek on atack

(/tch each def /grd exer def /mansas auch def

/stp eac h def /minses such def /manis 0 def /ya42manien 0 def

/ sci b1 mausas minnat sub div def tanvnt (minas sub act mull def

/minasam 0 def /ettei stp eigmult mul mansas aigmult mul minssa sigmult mul sub div b1 mol def taarassa b1 def

/ scia b1 max:: a minsase sub div def taxunts (minasam sub sc1m muni der

/mintemp minssa det imantemp mansar.oef moends O ne (noende 1 eq (imintemp mansas stp add def) if noends 2 eq (/maxtemp maxs s stp sJb def) if noonds ) eq (/mintemp minssa sip add def

/mmetemp mawass stp sub def t if 1 if newpath al a2 enveto b1 e2 lineto at t.2 movet o bl b2 11 net o stroke 10 HF /eldfbyt thgt det font mult 2 int sc NF dop stigwp .01 gt (ty -1 eq (

mant emp stp mast emp $ stp mul s&l kFIND MARIMUM MIS LAfdL LAN37M FON YAXf52 (datea.r t s 1 eq (dat ef or m DATFCDPN /aigcoll -1 det )

(eigeall 1 eq (NLM2CHA)l (10000 mul round 10000 div sep .9 gt (ed) If cvatrgi trelse

) ifelse strgwp dup yax2maxlen gt (tye=2marlen each def) (pop) ifelse

) for i if pant emp atp mant emp .$ stp mul adi its1NT AXI$ IARELS (dat een is 1 sq (cvi) it dap axunt b1 1 add le (dup axunt a2 ty 0 eq (11 2 1 div f nt sc add)

(11) ifelse ty 0 le (sub) (a4:11 if else ty 0 eq (dup .12 gt (pop -12) if) If moveto 4----- NUM2CKAR for angnificant digit s on aten stied to the f ollowirig line.

%-- - use $1GDIGIT to activate (JWX 3/91) datenzig i eq (dat ef orm DATECOFN /slycall al det ) (sigeall 1 eq (nth 2 CHM)

(10000 mul round 10000 div stp .9 gt (evil if evotrgi Atelse ) ifelse af and maximum arts label lenoth dup strgwp dup masis gt (/ maxis exch det) (pnp) ifelse ty abe 1 It icSnow) (CY$NOW) ifelse) (pop) ifelse i for oldthgt HF bl 5 mul . SPRINT AXIS TITLE m2 t y 0 eq (11 2 1 div f ontmult 2 mul int se a41 9 a4J dup /naxdts exch def 2 3 div fontmult mul fntsc add)

(11 masts a&1 7 wLi dup mandas it (pop marts) if ty -1 eq (fon*mult entse a11) If) italee t y 0 l a ( s ub') (add) ifelse /oldfhgt thgt det fontmult intec HF ty 0 lt (goave translate 140 re> tat e el that neg CFwf grest or e)

(CFPWT) ifelse cidthgt HF) (pop) ifelse tek 0 ne taajor ticks, main axis (newpath minaarm stpm maxssam . 5 stom mu) sit (dup exonts bl 1 add le (dup exunt o a2 movet o arunto a2 6 ty 0 le (sub) (add) ifelse Ilheto)

(Imp) Afelse) for stroke teinor ticks, main axis tch abe 1 gt (psave current 1&newidt h 2 div setlinewidt h newpath mins sam st pn tch abs div maststm (dup asunta 61 1 add le (dup asunta a2 movet.o asunt s a2 3 ty 0 le (sub! ( a41) if else lineto)

(pop) ifelse) for stroke grestore) if tsajot ticks, aux au s tck 0 it (

newpath minusta stpm marassm ,$ atta mul add j

(dup awunta b1 1 e41 le (dup awunta L2 seveto ASAS Manual Itevision 0 112 Apnl 19,1994

Figure 17 POSTER. TOP l File Added to Top of ASAS Plot File l Prior to Plotting ,

Page 4 of 5 arunts b2 6 ty 0 le (add) (sub) Afelee linetol (pop) ifelse) for stroke tainor ticks, aus axis tch aba 1 et (gsave current 1&newidth 2 div setlinewidth newpath siintram stge tek aba div maxaram (dup asunts bl 1 add le (dup exunts b2 moveto asunts b2 3 ty 0 le ( a41) (sub) ifelse lineto)

(pop) ifelse) far stroke grestore) if) if) if

% major grido grd o ne (currentlinewidth 2 dav set 11newidth grd 0 Jt (131 0 setdash) if negar h mintate st re add st pa mazzarm .5 atpm mul sub (dup asunts bl 1 edi le .

(dup anunta a2 moveto axunts b2 lineto)

(pop) ifelse) for stroke currentilnewidth 2 mul setlinewidth) if '

Il 0 setdesh 4 minor grida grd obs 1 gt (osave currentlinewidth 16 div settinewidth grd 0 it ((3) 0 setdash) if newpeth stre grd abs div /gine each det minatzm ginc eS1 gir.c manserm ginc sub ginc .5 mut edi (dup exunts b1 1 add le (cap axunta a2 sioveto axuntm b2 lineto)

(pop) ifelse) for at soke grestore) if fl 0 setdash

) barg1 def

/NLM2 CHAR

(/num2ord2 sigdig 1 add string def /num2 sin 1 strLng def num2oed2 0 t.) putinterval .

1 1 sig-ito (num2ord2 eac h (0) putintervell for sigmult mul round dup 0 It iin e2 sin 1-1 def) (/num2 san () def) ifelse ,

ahs Int.m2muinum exrts de f -

num2muinum sigmult div t runcate evstrg /num2absc exch det nus2mulnum sigmult div dap t runcat e sub sigsult mul round sigmult div sigmult mul evi cvstag /num2or d exch det eigdig 0 ne i nus,2ord2 num2crd2 length num2crd length sub nue2crd 0 num?ord Jength getinterval putinterval p pfinterswatch 0 eq (num2 sin num2absc num2ord2 3 CONCATENATE)

(num2 sin num2absc 0 num2absc len2th 2 sub getinterval num2ord2 .3 CONCATENATE) ifelse 3

( i printerswite:h 0 eq (num2 sin num2abac 2 CONCATE.NATE) '

(num2stn num2absr 0 nusn2absc length 2 sub getinterval 2 CONCATENATE) ifelse

) ifelse

) def

/ CONCATENATE (

/concat num exc.h def

/concatstag 0 string def

/concattotien 0 def

/concatind en 0 det dup length /concettotien exch def concatnum -1 2 ( 1 roll dup length ,

/concattotien exch concettotien a&1 def} for

/enncat stry concettotien string det 1 1 concatnum (pop dup concatstag concatinclen 3 al roll putinterval length /concatinclen each cencatinclen add del) for concatstry

) def e

  • curve processing I

! K WT

(/numela exch def /dat al numela arr ay det dat al astere slo pat i eq (D 1 numelm I sub (/cv oc h der datal cv detal cv get log put) for) if pop) def

/YWT

(/numelm each def /dat a2 numel.m array det data 2 ast ore ylogdat 1 eq

{0 1 numela 1 sub 1/cv e=ch det data 2 ev data 2 cv get 100 put) for) if pop) def

/unt (symerale 0 gt (sysscale .0'It inch mull (.075 inch) ifelse mull tdnd def

/CURVEtoPOINT (ger 11 savesym /syyscale exch def /1typ 2 def curvedraw) det

/savenym (dop o eq (11Ane 0 at (111ne obtyp 2 sob lt (sop sbary illne 1 sub get 1 adi dup sbtyp 2 sub ge trop 0) if) afi if ) if dop o it (gep 01 if tv3,0 dup sbary 21sne 3 -1 roll put 12 eq (dashast dashet dashpat put) if

) de!

ASAS Enual Revision 0 113 April 19,1994

Figure 17 POSTER. TOP File Added to Top of ASAS Plot File Prior to Plotting Page r> of 5

/curvedrew (1 gary illne 1 -1 roll put Ityp 3 lt niine (gsave 1typ 2 le {ldashpat 3) O aetdashi if newpath detal 0 get wunito data 2 0 get yunits moveto 1 1 datet length 1 sub (dup datal euch get xunit e euch data 2 euch get yunits 1&neto) for

% curvefill 8/90 Ityp -1 eq (goave .8 setoray closepath fall grestore /1typ 2 def )

(stroke) Afalse % fill a closed path 'l

% curvefill e r90 strnke grestore) if Ityp abe 2 ne  % symbols (gsave () O setdesh evrrent linewidth 4 div set 11newidth 01 detal length 1 sub (newpath dup datal each get munito exch data 2 exch get yunits moveto symbols abary lline get get evx exec

) for grestore) if .

/iline 11sne 1 add det i t ine st,t yp gt (/131ne O det) if

) bind def

/eymbols I tv3.0 (citet (boxl (triangle) (diaal (iravt ril latar)

(circfill) Itexfilli Itrifilin (dnamfill) floverifill)

(!nel (dine) totarfill) 1 def

/ circ (currentpoint newpath .5 unt 0 360 arc stroke) bind def

/cirefill (cur rent goint .5 unt 0 .360 are fill) t.And def

/ box

( 0.S unt 0.5 unt rooveto -1.0 unt 0.0 t 31 net o 0.0 -1.0 unt r11neto 1.0 unt 0.0 rlineto closepath stroke) bind det vboxfill

( 0. 5 ut.t 0.5 unt rmoveto -1.0 unt 0.0 alincto 0.0 -1.0 unt rlineto 1.0 unt 0.0 rlineto closepet.h fil t) bind def

/ triangle

( 0.0 0.5 unt rooveto 5 unt -1 unt rlineto

-1.0 unt 0,0 rianeto closepath stroke) bind def

/trifill l

( 0.0 0.5 unt ruoveto .5 unt -1 unt rlineto

-1. 0 unt 0,0 r11neto closepath fill) bind def

/ dias

( 0.4 unt 0.0 rmoveto -0,4 unt 0.5 unt r11neto

-0.4 unt 0.5 unt rlinato 0.4 urt -0.5 unt 111neto closepath stroke) bind def

/diamfill

( 0.4 unt 0.0 rmwet > -0.4 unt 0.5 unt rlineto 0.4 unt -0.5 unt rlineto 0.4 unt -0.5 unt riiheto closerath fill) bind def

/invtri

( 0.0 -0.5 unt smoveto <$ unt 1,0 unt rlincto

-1.0 unt 0.0 rlineto closepath stroke) bind def

/1nytrifill

( 0.0 +0.5 uot smoveto .5 unt 1.0 unt slinato

-1.0 unt 0.0 rtineto closepath filli t And def

/starmidlen (72 sin .5 s.ul 1, unt mul) det tv1.0

/etarside . tv3.0 (i unt 0 811neto currentpoint translate -144 rotate) def

/et ar tv3.0 (gsave 18 cos stermidlen mal neg 18 min stermidlen mul rmoveto cus s entpoint transiste 4 (starside) rereat closepath stroke grestore) bind def letarfill tv1.0 (goave 18 ces stareidlen sul nog 18 ein starmidlen mul twoveto cur r ent point translate 4 (starside) repeat closepath gsave O setgrey fill prestore stroke grentore) band def

/ine

(-1.2 unt 0.0 rooveto 2.4 unt 0.0 111neto strokal bind def

/ dine (gsave (daehart dashet get 11 0 setdash

-1.2 unt 0.0 rooveto 2.4 unt 0.0 r11neto strcke grestore /dashet dashtt I add def) bind det end 4 % End Pr olog 4tPaget one 1 ASAS Manual Revision 0 114 April 19,1994 1

l

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REFEltENCES I

1. SIMULATE-3 Advanced Three-Dimensional Two-Group Reactor Analysis Code, SOA-92/01, Studsvik of America, Inc.,1992.
2. W. II. Press, B. P. Planney, S. A. Teukolsky, and W. T. Vettering, Numerical Recipes - The Art of Scientific Computing (Fortran Version). Cambridge University Press,1989.

l ASAS Manual Revision 0 115 April 19,1994

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