NUREG/CR-6115, Forwards Draft NUREG/CR-6115, PWR & BWR Pressure Vessel Fluence Calculation Benchmark Problems & Solutions, Being Made Available to Facilitate Review of Document by Interested Members of Public
| ML20138C704 | |
| Person / Time | |
|---|---|
| Issue date: | 09/07/1999 |
| From: | William Jones NRC OFFICE OF NUCLEAR REGULATORY RESEARCH (RES) |
| To: | NRC |
| References | |
| RTR-NUREG-CR-6115 NUDOCS 9909080008 | |
| Download: ML20138C704 (280) | |
Text
{{#Wiki_filter:, 9 NOTE TO NUREG/CR-6115 FILE Septomber 7,1999 h FROM: William R. Jones, RES RE: DRAFT NUREG/CR k The attached DRAFT NUREG/CR 6115,"PWR and BWR Pressure Vessel Fluence Calculation Benchmark Problems and Solutions"is being made available to facilitato review of the i document bv interested members of the public at this time. Some additional NRC review is also being performed at this time. Thus, the document is being released as a DRAFT. l The DRAFT NUREG/CR 6115 provides detailed specification and corresponding numerical solutions for a set of PWR and BWR pressure vessel fluence benchmark problems which can be used in conjunction with DRAFT Regulatory Guide-1053, " Calculational and Dosimetry Methods for Determining Pressure Vessel Neutron Fluence." Several benchmark problems i have been specified for PWRs (standard core loading, low-leakage core loading and part length ) shield assembly core design). The benchmark problems allow detailed assessment for the ) numerical procedures, code implementation, and the various modeling approximations against j state-of-the-art solutions for representative fuel cycle design schemes. l l Detailed neutron flux solutions are provided at selected pressure vessellocations. A Pin-wise core neutron source is provided which includes fuel exposure dependence. A typical set of fast neutron dosimeter responses are calculated. 9909080008 990907 CF SUBJ hO RES-1B-1 CF b
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- NOTE TO: DOCUMENT CONTROL DESK FROM:- William R. Jones, RES,4 -7558 //
Please makp the attached /enclosedidocumen (0:di P.0;; Guide 105HStrikeouttruthna &>p
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- Dra't NUREG/CP. 6115) available in the PDR.
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I a NUREG/CR-6115 l BNL-NUREG-52395 1
- PWR AND BWR PRESSURE VESSEL FLUENCE CALCULATION BENCHMARK PROBLEMS AND
- SOLUTIONS '
Prepared by J. F. Carew, K. Hu, A. Aronson, A. Prince, and G. Zamonsky Brookhaven National Laboratory Prepared for U.S. Nuclear Regulatory Comm.ssion , 4 9 4
NUREG/CR-6115 . BNL-NUREG-52395 4 PWR AND BWR PRESSURE tESSEL FLUENCE ' CALCULATION BENCHMARK PROBLEMS AND SOLUTIONS Manuscript Completed: May 20,1997 Date Published:
- Prepared by -
J. F. Carew, K. Hu, A. Aronse , A. Prince, and G. Zamonsky Brookhaven National Laboratory Upton, NY 11973-5000 Prepared for Division of Engineering Office of Nuclear Regulatory Research U. S. Nuclear Regulatory Commission Washington, DC 20555 4 NRC FIN A-3954-1
c H f . ? 1-ABSTRACT
. In order to provide the high confidence required in the determination of pressure vessel embrittlement and the
, evaluadon of the RTm screening criteria, Regylatory Guide-1053 recommends detailed benchmarking of pressure
- vessel fluence calculations, in response to this recommendation, this report provides the detailed specification and corresponding munerical solutions for a set of PWR and BWR pressure vessel fluence benchmark problems.
PWR benchmark problems have been specified for (1) a standard core loading pattern, (2) a low leakage core loading pattern and (3) a partial length shield assembly core des gn. Since BWR fuel loading pat' erns are presently not being designed for vessel fluence reduction, only a single BWR problem is gecified. '!hese i benchmark problems a: low a detailed assessment of the numerical procedures, code implementation, and the various modeling approximations against state of the-art solutions for representative operating configurations.
- 'Ihe problems have been solved using the DORT discrete ordinates transport code, the MESH source processing l code, and the BUOLE 93 ENDF/B VI nuclear data. Detailed neutron flua solutions are provided at selected i
pressure vessel azimuthal, radial, and axial locations A pin-wise core neutron source is provided which includes
- the fuel burnup dependence of both the magnitude and energy dependence cf the neutron source Dosimeteri responses are calculated for a typical .iet of LWR fast neutron dosimeter materials. In addition, MCNP Monte
- Carlo calculations have been performed for both *.he stanriard core and partial length shield assembly core loedtags. Comparisons of the MCNP and DORT vessel fluence calculations are presented.
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a CONTENTS Page Abstrac t . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ............................ . . . . iii List of Fi gures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vii List of Tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . viii
- Ac knowledgm ents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xi 1
I ntroduc tion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 1.1 Background .................................................... 11 1.2 Regulatory Guide- 1053 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 1.3 Pressure Vessel Fluence Benchmark Problems . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1.3.1 DORT Discrete Ordinates Calculations . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1.3.2 MCNP Monte Carlo Calculations ............................... 12 1.4 Application of the Benchmark Problems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 2 Benchmark Problem Specification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 2.1 PWR Probicm Specification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2.1.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 2.1.2 Specification of the Standard Core Loading Problem . . . . . . . , . . . . ...... 2-1 2.1.3 Specification of the Low-Leakage Core leadmg Problem . . . . . . . . . . . . . . . 2-2 2.1.4 Specification of the Partial Length Shield Assembly Core Loading Problem . . . . . 2-3 2.2 BWR Problem Specification . . . . ....................................,2-2.2.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2.2.2 Specification of the BWR Problem . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . 2-3 DORT Calculational Methodology . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 3.1 Introduction ................................................... 3-1 3.2 Neutron Cross Sections and Fission Spectra . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31 3.3 Core Neutron Source . . . . . . . . . . . . . . . . . . . .......................... 3-1 3.4 Neutron Transport Calculations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 3.5 Flux Synthesis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 2 3.6 Dosimetry Cross Sections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-2 4 DORT Benchmark Problem C4culation Resuhs , . . . . . . . . . . . . . . . . . . '. . . . . . . . . . ....... .41 4.1 PWR Benchmark Problem Calculation Results .............................. 4 4.1.1 Calculated Flux, Reaction Rates and Spectra . . . . . . . . . . . . . . . . . . . . . . . . . 4-1 4.1.2 Standard Core Loading Benchmark Problem . . . . . . . . . . . . . . . . . . . . . . . .... . 41 4.1.3 Low Leakage Core leadmg Benchmark Problem . ..... . . .. . .... . .... 4-2 4.1.4 Partial Length Shic!d Assembly Core Loadmg Benchmark Problem . . . . . . . . . . . . 4-2 4.2 BWR Benchmark Problem Calculation Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-4.2.1 Calculated Flux, Reaction Rates and Spectra . . . . . . . . . . . . . . . . . . . . . . . . . , , 4-4.2.2 BWR Benchmark Problem Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
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$. PWR and BWR MCNP Benchmark Problem Calculadons . . . . . . . . . . . .. ...................... 51 5.1 Introduc6cn . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 1 5.2 Calculadon Methodology . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...................... . . 51 5.3 >- PWR MCNP Calculadons and Comparison with DORT . . . . . ........... ......... 52 5.4 BWR MCNP Calcula6ans and Comparison with DORT . . . . . .................... 52 6 Refenmoes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 1
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e i FIGURES Page t 2.1.2.1 Standard Core leading . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 56 2.1.2.2 _ Standard Core leading Axial Geometry at 0 = 0* . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .> 2 57 2.1.2.3 ~ IAcetion of Surveillance Capsules . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 58 2.1.2.4 _ Surveillance Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , , 2 5 9 2.1.3.1 IAw IAnkage Core IAnding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 240 _ 2.1.3.2 1Aw lankage Core tmeding Axial Geometry at 0 = 0' . . . ,'. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 241
- 2.1.3.3 : I madan of Surveillance Capsules . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 242 2.1.3.4 Survemance Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 43 2.1.4.0 Panial iength Shield Assembly Core IAnding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 244 2.1.4.2 Partial Lansth Shield Assembly Core Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 245 2.1.4.3 Partial 14nsth Shield Assembly Core Leading Axial r1=a==evy at 0 = 0' . . . . . . . . . . . . . . . . . . . . 246 2.2.2.1 i BWR Planar Oseesty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 56 2.2.2.2 BWR Axial Geometry at 0 = 0' . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 57 2.2.23 Survallance Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 59 4.1.2.1 Standard Core leading Pressure Vanaal Flux Spectrum at the O.T I == dan . . . . . . . , . . . . . . . . . 441 4.1.2.2 Standard Core leading Pressure Vessel Flux Spectrum at the T/4 L-daa ..................442
- 4.1.2.3 - Standard Core Loading Pressure Vessel Flux Spectrum at the T/2 Location . . . . . . . . . . . . . . . . . . 443 4.1.2.4 Samndard Core Loading Pressure Vessel Flux Spectrum at the 3T/4 Location . . . . . . , . . . . . . . . . . 4 44 s ' 4.1.2.5 - Standard Core Loading Pressure Vessel Flux Spectrum at the I.T Location . . . . . . . . . . . . . . . . . . 445
= 4.1.2.6 Standard Core Landing Thermal Shield Capsule Flux Spectrum . . . . . . . . . . . . . . . . . . . . . . . . . . . 446 4.1.2.7 Standard Core Loading Pressure Vessel Capsule Flux Spectrum . . . . . . . . . . , . . . . . . . . . . . . . . . . , 447 4.1.2.8 Standard Core Imading Cavity Capsule Flux Spectrum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 448 4.1J.1 Low-Leakage Core Leading Pressure Vessel Flux Spectrum at the O T Location . . . . . . . . . . . . . . 449 4.1J.2 Low-Lankage Core Loading Pressure Vessel Flux Spectrum at the T/4 Location . . . . . . . . . . . . . . . 4-70 '
4.1.33 Low-Leakage Core Landmg Pressure Vanael Phix Spectrum at the T/2 Location . . . . . . . . . . . . . . . 4-71 4.1.3.4 Low LAnkage Core loading Pressure Vessel Flux Spectrum at the 3T/4 Location , , , . . . . . . . . . . . 4-72 4.1.3.5 L9w-Leakage Core Loading Pressure Vessel Flux Spectrum at the 1 T Location . . . . . . . . . . . . . . . 4 73
' 4.1J.6 Low Leakage Core Loading Thermal Shield Capsule Flux Spectrum . . . . . . . , , . . . . . . . . . . . . . . 4 74
; 4.1J.7 Low-Leakage Core landing Pressure Vessel Capsule Flux Spectrum . . , . . . . . . . . . . . . , . . . . . . . 4-75 4.1J.8 _ Low-Leakage Core Loading Cavity Capsule Flux Spectrum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-76 4.1,4.1 Flux >l.0 MeV at the Pressure Vessel Wold Surface . _. . . . . . . . . . . . . t . . . . . . . . . . . . . . . , , , . . , . 4-77 4.1.4.2 Flux >0.1 MeV at the Pressure Vessel Weld Surface . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . 4-78 4.1.43 dup ar===nes l Per Atom at the Pressure Vessel Weld Surface . . . . . . . . . . . . . . . . . . . . . . . . . . . , . 4 79 4.1,4.4 Pressure Vessel Weld Flux Spectrun at 0 = 0' . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-80
. 4.2.2.1 Pressure Vessel Flux Spectrum at the O-T IAcation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 441
- 4.2.2.2 . Pressee Vessel Flux Spectrma at the T/4 I reanian ....................................442 4.2.23, Pressus Vessel Flux % at the T/21 ee=da= ....................................443 4.2.2.4 Pressee Vessel Flux Spectrun at the 3T/4 Location ...................................444
. 4.2.2.5 Passee Vessel Flux 0,,, at the 1-T Location . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 445 4.2.2.6 Pressure v emel Capsule Flux Spectrum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 446 4.2.2.7 Cswity Flux Spectrum . . . . .~ . . . . . . . . c. . '.7. . '. . . .'. . . W.h $. .n. . . . i. . .i . ch.?. . . . .'448 y F c '
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r != FIGURES (Cont'd.) Page 5.3.1 MCNP Region Wise imponances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 7 5.3.2 MCNP Radial Geometry Standard Core Loading .. .. .....................,.............,58 5.0 MCNP Axial Geomeuy Standard Core Loading . . . , . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . 5 9 5.3.4 MCNP Radial Geomeuy PLSA Core Loading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 10 5.3.5 MCNP Axial Geometry PLSA Core Loading .........................................511 5.3.6 - MCNP Standard Core Loading Flux (E>l.0 MeV) at Pressure Vessel Inner Wall . . . . . . . . . . . . . . 5 12 5.3.7 MCNP Standard Core Loading Flux (E>l.0 MeV) at Pressure Vessel T/41Acation . . . . . . . . . . . 5 13 5.3.8 MCNP Standard Core Loading Flux (E>l.0 MeV) at Pressure Vessel Lower Weld . . . . . . . .... 5 14 5.3.9 MCNP Partiallength Shield Assembly Core Loading Flux (E>l.0 MeV) at Pressure Vessel Lower Wold . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5- 15 5.4.1 MCNP Radial Geometry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-8 5.4.2 - MCNP Axial Geomeuy Standard Core Loading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-9 5.4.3 ' Radial Region . Wise Importances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10 5.4.4 Axial Region - Wise Importance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 11 5.4.5 MCNP Flux (E> l .0 MeV) at Downcomer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12 5.4.6 MCNP Flux (E>l.0 MeV) at Pressure Vessel Wall . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 13 5.4.7 MCNP Flux (E>1.0 MeV) at Downcomer Homogenized Water Gap . . . . . . . . . . . . . . . . . . . . . . . 5 14 5.4.8 MCNP Flux (E>1.0 MeV) at Pressure Vessel Wall - Homogen! zed Water Gap . . . . . . . . . . . . . . . . 5 15 4
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- 2.1.1.1 L Fracta of Fisons by laatope as a Functica of Exposure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 4 2.1.2.1 ' Standard Core Loading Basic Desip Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 5 2.1.2.2 Standard Core Loadas Core and Fuel Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6
- 2.1.2.3 Standard Core lendmg Desip W '= Material Compositions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 7 2.1.23.1 _ lsolopic Frechens in Cr, Fe and Ni . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 9 12.1.2.4 Standard Cm leadmg Axial Zone Asapawats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 10 12.1.2.5 : Saandand Core Loadmg Fuel Assembly Geometry, Power. and Burnup Distributions . . . . . . . . . . . . . . . . 2 11 2.1.2.6 Standard Core Londmg Pin Ooometry, Power, and Burnup Distributions . . . . . . . . . . . . . . . . . . . . . . . . . 2 12 l 2.1.2.7 _ Samaderd Core Loadag Axial Power Distributions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 17 2.1.2.8 Standard Core leading Edit L~ '== . . . . . . . . . . . . . . . . . . . - . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 19 i
2.1.3.1 low-1Aakage Core lendag Basic Desip Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 20
; 2.1.3.2 low-laskege Core IAedag Core _and Fuel Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 21 2.1.33 . Iow-IAskage Core leedag Desip Specinceban Material Compositions . . . . . . . . . . . . . . . . . . . . . . . . . 2-22
- 2.13.4 L law-1Ankap Core lendmg Axial Zone Assipments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 24 2.1J.5 law.1Ankage Core leedme Fuel Assembly Geometry, Power, and Bumup Distributms . . . . . . . . . . . . 2 25 2.1J.6 L low-1Atkage Core Londmg Pin Geomony, Power, and Burnup Distributions . . . . . . . . . . . . . . . . . . . . . 2 26 2.13.7 Low-Le kage Core leedmg Axial Power Distribuuons . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 31 2.1J.: low tAthap Cm lAedag Edit Imcations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 33 2.1.4.1 Partial length Shield Assembly Core 14edag Basic' Desip Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 34
- 2.1.4.2 - Partiallength Shield Assembly Core toedag Core and Fuel Assemblies . . . . . . . . . . . , . . . . . . . . . . . . . 2 35
' 2.1.43 Partial Length Shield Assembly Cm leedmg Desip Speci5cata Material Compositions . . . . . . . . . 2 36 2.1,4.4 ' Partial Length Shield Assembly Core Loadmg Axial Zone Assignments . . . . . . . . . . . . . . . . . . . . . . . . . . 2 38 2.1.4.5 : Upper Partial Length Anaamhly Core Loadag Fuel Assembly Geometry, Power, and Burnup Distribuuons . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 39 2.1.4.6 L Lower Partiallength Assembly Core Loadag Fuel Assembly Geometry, Power, and Burnup Distributions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-40 2.1.4.7 ' Upper Partial Length Assembly Core loedmg Pin Geometry, Power,
- and Burnup Distribuuons . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 41 2.1.4.8 : Lower Partial Length Assembly Cm Loadmg Pin Geometry, Power, and Burnup Distribuuans . . . ' . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-46
- 2.1.4.9 Upper Partial Length Assembly Cm 14admg Axial Power Distributions . . . . . . . . . . . . . . . . . . . . . . . . . 2 51
, 2.1.4.10 lower Partiallangth Assembly Core leedag Axial Power Distribuuons . . . . . . . . . . . . . . . . . . . . . . . 2-53
- 2.1.4.11 Partial Lansth Stueld Assembly Core imedag Edit L~ah . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 55
_2.2.1.1 Frecuan of Fismons by Isotope as a Functa of Exposure . . . . . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . 2 4 2.2.2.1 1 Basic Desip Deta . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 5
- 2.2.2.2 Core and Fuel Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6 2.2.2.3_ . Desip Spama Material Compositions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 7
- 2.2.23.1 Isotopec Frecuans in Cr, Fe and Ni . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 9 2.2.2.4 Fuel Assembly Geometry, Power, and Burnup Distribuhans . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . 2 11 -
2.2.2.5 L Pin Geometry. Power, and Burnup Distributions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 12 2.2.2.6 Axial Power Distninsuons . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 17 2.2.2.7 ? Bdit iesehens % . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ._ . . . . . . . . . ._ . . . . 2 19 . Y'Q
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-Page 3.2.1 Fission Spectna by Isotope . . ._ . . . . . . . . ._ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 3 3.4.1 Sensitivity of the DORT Calculated Flux to Numerical input Parameten . . . . . . . . . . . . . . . . . . . . . . . . . . 3 4 3.4.2 ; Sensitivity of the DORT_ Calculated Flux to S Quadrature . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . 3 6
. 4.1.1.1 Mesh Used in DORT Calculation (Inner Model) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 3 14.1.1.2 Mesh Used in DORT Calculation (Outer Model) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 6 4.1.13 47 Oroup Energy Structure of Cross-Section Library . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 9 4.1.1.4 Nuclear Parameters for Neutron Flux Morutors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 10 4.1.1.5 Da-nater Activation Cross Sections (BUOLE 93) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 11 4.1.2.1 Standard Core leading Flux (E>l.0 MEV) at Passure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 14 4.1.2.2 Standard Cm i andmg Flux (E>0.1 MEV) at Pressure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 16 4.1.2.3 Standard Core 14edag DPA Rate at Pressure Vessel . . . . . . . < . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 18
, , 4.1.2.4 : 3tandard Core Leedag Flux (B>l.0 MBV) et Pressure Vessel lower Weld . . . . . . . . . . . . . . . . . . . . . . . 4 20 4.1.2.5 Standard Core Londmg Flux (E>0.1 MEV) at Pressure Vessellawa Wold . . . . . . . . . . . . . . . .. . . . . . . 4 22 '
4.1.2.6. Standard Core imeding DPA Rates at Pressure Vessel Lower Weld . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 24 14.1.2.7 : Standard Core Imeding Downcomer Fluxes and DPA Rates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 26 4.1.2.8 Standard Core loadmg Cavity Fluxes and DPA Rates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 28
- 4.1.2.9 Standard Core leedmg Flux Spectnan at Pressure Vessel >
(Pressure Vessel Capsule In) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 30 4.1.2.10 Standard Core Londmg Flux Spectrum at Capsule 1 ac=ema . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 31 . 4.1.2.11 Standard Core Londms-Esect of Selected Cross Sections on the
. Calculated Reaction Rates at the 'Ihermal Stueld Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . .........432 4.1.2.12 Standard Core Londmg.Effect of Selected Cross %esiana on the Calculated Reaction Rates at the Pressure Vessel Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-33 4.1.2.13 Standard Core Loadmg Esect of Selected Cross Sections on the Calenla*=d Re .ction Rates at the Cavity Capsule . , . . . . . . . . . . . . . . . . . . . . . .................... 4 34 4.1.3.1 low-leakage Cm Londmg Flux (E>1.0 MEV) at Piessure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 35 4.13.2 low-leakage Core leedmg Flux (E>0.1 MEV) at Pressure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 37 4.133 low Leekage Core Londmg DPA Rates at Pressure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 39 4.1J.4 Irv Leakage Core Londmg Flux (E>l.0 MEV) at Pressure Vesselinwer Weld . . . . . . . . . . . . . . . . . . . 4 41 14.13.5 Low-Leekage Core Londmg Flux (E>0.1 MEV) at Pressure Vessellower Weld . . . . . . . . . . . . . . . . . . . 4-43
- 4.13.6 Imw-Leakage Core lmeding DPA Rates at Pressure Vessel lower Wold . . . . . . . . . . . . . . . . . . . . . . . . . 4-45
; 4.1.3.7 Low-Leekage Core 1medag Downocener Fluxes and DPA Rates . . . . . . . ... . . . . . . . . . . . . . . . . . . . . . . . 4 47 4.1J.8 Low-Leekage Core Londmg Cavity Fluxes and DPA Rates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-49
- 4.13.9 : low-Leekage Core imedag Flux Spectrum at Pressure Vessel (Pressure Vessel Capsule in) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 51 4.1J.10 Low-Imakage Core Loadag Flux Spectrum at Capsule i ac=sen . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-52
- 4.1J.11 low-leakage Core Loadag-Effect of Selected Cross Sections on the Calculated Rsectaca Rates at the Thermal Stueld Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 53 -
? 4.1.3.12 Inw-IAskage Core Indms-E5ect of Selected Cross %cemns on the Calculated Reactaca Redes at the Pressure Vessel Capsule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 54 4.1.3.13 Lc ' - Core Imedag-E5ect of Selected Cross Secticas on the -
m Calculated Reececa Rases at the cavity Capsule . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .a . 4 55
' 4.1.4.1 L PartialIAnglh Shield Assembly Core loadag Fhmes and DPA Raise-
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TABLES (Cont'd.) - Page 4.1.4.2 Partial Length Shield Assembly Core Loading Flux Spectrum. Pressure Vessel Inner Wall at Lower Weld (z = 67.1048 cm) . . . . . . . . . . . . . . . ...................458 4.1.4.3 Partial Length Shield Assembly Core Loading-Reduction Factors for Fluxes and DPA Rates-Pressure Vessel Inner Wall at Lower Weld (z = 67.1048 cm) . . . . . . . . . . . . . . . . . 4 59 4.2.1.1 Mesh Used in DORT Calculation . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . 43 4.2.1.2 47 Oroup Energy Structure of Cross-Section Library . . . , . . . . . . . . . . . . . . 49 4.2.1.3 Nuclear Parameters for Neutron Flux Monitors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 10 4.2.1.4 Dosimeter Activation Cross Sections (BUOLE 93) . . . . . . . . . . . . . . . . . . . . . . . . . .... . . . 4 11 4.2.2.1 Flux (E>l.0 MEV) at Pressure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . ... ... ..... .. . . 4 14 4.2.2.2 Flux (E>0. l MEV) at Pressure Vessel . , . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . 4 16 4.2.2.3 DPA Rate at Pressure Vessel . . . . . . . . . . . . . . . . . . . . . . . ......................,418 4.2.2.4 Flux (E>l.0 MEV) at Pressure Vessel (Axial Midplane) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 20 4.2.2.5 Flux (E>0.1 MEV) st Preasure Vessel (Axial Midplane) {. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-22 , 4.2.2.6 DPA Rates at Pressure Vessel (Axial Midplane) . . . . . . . . . . . . . .........................424 4.2.2.7 Downcomer Fluxes and DPA Rates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , 4-26 4.2.2.8 Downcomer Fluxes and DPA Rates (Axial Midplane) , . . ..... .....................428 4.2.2.9 Cavity Fluxes and DPA Rates . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-4.2.2.10 Flux Spectrum at Pressure Vessel . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . ....... . . 4 30 4.2.2.11 Flux Spectan at the Downcomer, Capsule and Cavity Locations . . . . . . . . . . . .. .. . 4-31 4.2.2.12 Calculated Reaction Rates at the Capsule .. .......... ... . . . .. .. .. ..... . 4-32 53.1 MNCP Standard Core leading Flux (E>l.0 MeV) at Presse Vessel Inner Wall Peak Axial Location . . . . . . . . . . . . . . . . . . . . . . . .. . .. . .. . . .. . . . 53 5.3.2 MNCP Standard Core Loading Flux (E>l.0 MeV) at Pressure Vessel 1/4 T Peak Axial Location . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... .... ........ 5-4 5.3.3 MNCP Standard Core Loadmg Flux (E>1.0 MeV) at Pressure Vessel Inrier Wall Lower Weld Location . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... .... . . . . . . . 55 5.3.4 MCNP Flux (E>l.0 MeV) Partial Length Shield Assembly Core Loadmg at Pressure VesselInner-WallLowerWeldLocation . .. .. .... ... . . .. .. . . 5-5.4.1 MNCP Flux (E>l.0 MeV) at Downcomer - Explicit Water Osp - Peak Axial location . . . . 5-5.4.2 MNCP Flux (E>l.0 MeV) at Pressure Vessel Wall- Explicit Water Gap Peak Axiallocation . . . S-5.4.3 MCNP Flux (E>l.0 MeV) at Downcomer - Homogenized Water Gap . . . . . . . . ... . . 5-5.4.4 MCNP Flux (E> l .0 MeV) at Pressure Vessel Wall - Homogemzed Water Gap ... ........... ... . 5-gkp 4 ' 4-8 i - r Td n l
l l l ACKNOWLEDGMENTS The work documented in this report was performed under the auspices of the United States Nuclear Regulatory Commission (USNRC). It was funded by the Materials Engineering Branch, of the Division of Engineering, in the Office of Nuclear Regulatory Research, under FIN Number A 3954. The program was monitored at the USNRC by Carolyn Faubanks and Al Taboada, whose support of this work is gready appreciated. The authors are also grateful to Mike Mayfield and Chuck Serpan, Jr. of the Office of Nuclear Regulatory Research for many valuable discussions and contributions to this work. Special thanks are also due to Mrs. N. Siemon and Mrs. N. Santiago who accomplished the difficult task of editing and bringing this final report to compliance with NRC h-tation requirements. 9 p to j % .k u e > .
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I INTRODUCTION vessel RTwr, certain PWR plants are approaching the l.1 Backgrouud RTmscreerdag criteria with the potential,in some cases, for reaching this limit prior to end-of. license. The De U.S. Nuclear Regulatory Commission (NRC) has promulgated -regulations that ensure t%e structural approach to this limit, together with the difficulty in making an accurate determination of the vessei neutron integrity of the reactor pressure vessel for light water fluence using calculanons and/or measurements, requires power reactoss : Specific fracture toughness require, that the most accurate methods and procedures be used ments for normal operation and for anticipated to determine the pressure vessel fluence, operational occurrences for power reactors are set forth in Appendix 0, " Fracture Toughness r@. .;..ts," of De difBculty in calculating the vessel fluence is due te < 10 CPR Past 50," Domestic Liceesing of Producdon and (1) the strong attenuation of the flux between the core Utilization Facilities"f Additionally, in response to and the wssel and (2) the complexity of the neutron concerns overpotential pressurized thermal shock (PTS) anrce calculadon. The neutmn nunce is atunuated by events in pressurized water reactors (PWRs), the NRC semal decades (typically ~4 in the case of both PWRs issued 10 CFR - 50.61, " Fracture Toughness Requirements for Protection Against Pressurized and BWRs) between the core and the vessel which
' results in a very strong sensitivity of the calculated Thermal Shock Events."
fluence to the representation of the core and internals la order to satisfy the requirements of both Appendix 0 geometry and material compositions, nuclear cross sections and nurnerical procedures for performing the
- and 10 CFR 50.61, methods for determining the fast transport calculation. The rapid spatial nriation of the neutron fluence (E > I MeV) are necessary to estimate .
amtmn source near the core bandary requires that the the fracture toughness of the pressure vessel materials. detailed fuel pin-wise source nriation be explicitly Appendix H, " Reactor Vessel Material Surveillance represented. in addition,in onier to account for the fuel Program requirements," of 10 CFR Part 50 requires the burnup dependence of this source data, the source must installation of surveillance capsules, including material be calculated for each plant operating cycle, The source test specimens and flux dosimeters, to provide data on determination is further complicated by the coordinate material damage correlations as a function of fluence. transformation required to convert the data from the rectangular (x,y) core geometry to the cylindrical (r,0) The fracture toughness of pressure vessel matenals is geomeuy typically used for the core-to vessel neutron
, related to the - matenal's - " reference ail ductility temperature," or simply reference ;.c. .;,,.., which is transport ~"8=*M denoted as RTer. The RTer is defined by a correlation in pracance,the presmire wesel fluence esumates reqmrod on'the fast neutron fluence (E > 1 MeV), matenal for the Appendix 0 and RTm analyses have been
- chamistry (concentrations ofCu and Ni), initial reference detennined usbg unous modeling approximations, . temperature, and margin to account for uncertainties in computer codes and nuclear cross section sets. Over the ,
- the correlation and input values. Section 10 CFR 50.61 past decade, substantial 4wts have been made requussevaluationofthereferencet . wbasedon in both the calculation and measurement of the pressure the best osnmase of the fast neutron fluence at the end of vessel fluence. Dess improvamanta haw mammM from the hcense period, and the wA reference bothNRCandindustryprograms nessimprovenansa temperatureistenned RTm-7 include the ! ,in and improvement of 75 r codes and t'alat**ia==1 models, revision ofbasic cross.
#Ctiondata,imprmdnuesuruuntuchnicius,andthe 1.2 Regulatory Guide-1053 symannele quaWeiaa of the fluence methods by comparison to NRC-sponsored hanchmark experiments.
- As the pressus vessels cf operatmg plants continue to accumulate neutron fluence reducing the margin to the He' NRC has issued Regulatory Guide.1053,
- 9 w, 4g ~g <
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, e li introduction
" Calculational End Dosimetry Methods for Det:rmining - calculation of typical in-vessel and/or ex vessel Pressure Vessel Neutron Fluence," to provide guidance dosimeter reaction rates.
on the methods and assumptions acceptable to the NRC - _ star for determining ; vessel Guence. This Ovide > provides a detailed description of the methods for constructing the neutron trar. sport model, dotarmination of the core neutron sou.ce,- and recommendations for the- 1.3,1 DORT Discrete Ordinates asometric and nuclear input data. Because of the. Calculations importance and durie4 of these calculations, the Ouide
==== &m &c Calcula ional mo&odology used for
.!he three benchmark problems were calculated using the the detonninetion of vessel fluence be validated against power mactor and meet sianulata mensaments and ORNL DORT Discrete Ordinates Transport code ental =*ia=al beclunarks, (Reference 1) and the BUGLE 93 (Reference-2) cross section library. The BUOLE 93 cross section library includes the most recent version ofthe ENDF/B-VI fron,
. In seppet of es duelopawat of tlw Regulamry Guide, hydrogen and oxygen cross sections, which are expected
( the Materials Engineering Branc.h of the NRC Division 2 have a signincas efect on dw meal noences in of Enginsenag has requested that BNL develo : a typical pufwming &c calculmions, a siih=*manial efon was se of PWR and BWR power-mactw cabladonal ma6 to insure an accurate representation of the spatial _ h"""h"k problems together with solutima detemined
;.ad energy dependence of the neutron source, in order with the methods desenbod in the Regulabry Gu'?"
to determies the annealing or Rattening of the axial Gux Mis sport documents the PWR and BWR power-rescacr stupe h es com and se vasel, calculmions wac benchmark problems and the menaciasad vessel Buence pufwned in DORT(r,0), (r,4 and (r) gwme tria. The calculmions and results. methodology used in the benchmark cshulations was basically that described in Regulatory Guide 1053.
' 1.3 Pressure Vessel Fluence Tiw neutron aux (nuence pa unit time) solution is Benchmark Problems pramel in tams of the Dux above 1-MeV (>1 McV),
above 0.1 MeV (>0.1 MeV), and the displacements-per-
'the PWR vessel Buence benchmark problems are for a 80m por secona (dps/s).1hese edits art provided at the typical 204 fuel assembly PWR core including the core axial locations of the peak Gux and the lower baSle and beni, &amat shield, and a venet having an circumferential seld,- and at selected _ radial and ILaer radms of-219.1 cm. The renal power is 2527.73 anmunhal locations. In the case of the PWR PLSA core MW, with an average coolant temperature of 293.3'C. loading pauern, se Sax h at &e mael inner The core power and fbel burnup distnbutions are for a - waH at es loww cucumfundal weld (mW 2 &c typral equilibrima cycle. Benchmark probleau are - mandard ome loading)is also calculmed. De nulugmup danned for three typec of fbol loadings: 1) a Standard neutron energy spectrun is calculated at semal miial out-in Core Loadin6, (SCL), 2) a law-Leakage Core '
Imading (LLCL) and 3) a core including Partial Length Sinald A===huan (PLSAs); 1.3.2. MCNP Monte Carlo Calculations 1he BWR vessel Suonce bendmark problem is for a MCNP Monte Carlo (Reference-3) calculations of the typical .800 thel bundle core nacindiap the shroud, jet ' PWRStandardCore andParnallAngthShield Amma=hly pumpc and rieses and a veneet having an inner radas of o Core Loadungs and the BWR benclunark problem wue
'- ^
' 321.8cm. The raced power is 3833 MW,with a core
~
also performed in order.to pro 9e an ' ' , inlet temperemme of 278.9'Ci As in the case cf the PWR - h""#8""*'k solution and to allow waparison with the hancinnarks, - the L core power - and fuel burnup DORTdiscreteordinatesmethodology Decalmlations detrhesions are $st a typical equilibrium cycle.1 were perfbnned in thme<iuneasions using an ENDF/B. . VI;multigroup nuclear cross section . library, .A_ Jihe hanch==k problem calculation : requira de - =*==nriai saart wai made in the modeling io provide an w ce . s ' em # .. < . ejm b Yh hk b5$$kh f? Okl ~ Q , +t $'S * $M Lyd-+ M t;:yfO QQ$ p _ y gy y mmly
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- 1. Introduction exact spatial representation of the benchmark problem wssel fluence calculational uncertainty slaih3 to the geometry. -1he methodology used in the benchmark benchmark solutions.
mimidlana was essentially that described in Regulatory Guide 1053. The neutron flux ateve 1 MeV was The reference solutions provided in this report are based calculated at the inner wall of the vessel as a function of on present methods and available data. It is intended that azimuth and compared to the cos.Wng DORT as the calculational methods and nuclear data are prabetions improved, the benchmark solutions will be updated as a.m -y. 1.4 Application of the Benchmark N benchmark problem specifications are given in Chapter 2 for the PWR standard core, low leakage cure, Problems and the pa,tial lengih shield assembly core loadings and for the BWR hanchniark problem. The DORT - M benchmark problems provide a well docmamated miml=eiaa and modeling saethodologyused to determine M ' and format which _will allow detailed the solutions is presented in Chapter 3, and the detailed intercomparisons of pressure - vessel fluence benchmark solutions are given in Chapter-4. The MCNP computational methodologies. The benchmark problems Monte Carlo calculations together with comparisons with include all the features which have a significant e5sct on the DORT results are presented in Chapter 5. the cakadation of pressure vessel fluence and include adReimas spaco energy detail to allow (1) comparison of the multigroup fluences through the vessel and cavity - and (2) evaluation of the extrapolation of the dosimetry measurements from the surveillance capsules to the vessel The fluence solutions provided are based on state-of-the-art transport ==thadalogy.' These solutions have the advantage that they do not include the as built and experimental vr. lability that typically limits ti,e
. benchmarking process when comparisons are made
- directly with fluence dosimeter measurements.
The calculauon-to<:alculation benchmark compansons allow an mammamawns of the numencal procedures, code , 1 implementation, and.: the -various modeling apprammariana against detailed validated solutions for seposentative operating configurations. The difforences ruulting ham the uncenainty in the numerical pro-calderas and the madaling of the source and geometry should be anall and with present ir6 can be ; aduced to s(5-10)%.1he e6ects ofusing pre ENDF/Bi
--VI andtigroup ceces secuan sets can be larger, up to a
~20% (30%) underprabstion of the >1-MeV and >0.1-MeVilmenoss at the vessel inner (outer) wall. , - -
., n .
The obegived mimla8Whl=**aa. diffemeces provide the quantitative eSect of the procedures and __ apps-im eia- used in the proposed mathadalogy and abasisformodelWandirnprovmame lhese differences anay also be used to estimate the pressure n,
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I 2 BENCHMARK PROBLEM SPECIFICATION 2.1 PWR Problem Specification Po"er dimibutim is based on a detailed 1515 fuel assembly pin wise power distributinn for a typical core loading. The fuel nuclide fission fraction is provided in 2.1.1 Introduction Table 2.1.1.1 to allow the determination of the exposure t dependence of the neutron source strength (neutrons / l ne PWR pressure vessel fluence benchmark problems MeV) and the source spectrum. are for a 204 fm! assembly PWR core having an exial height of 1i ft -nd including a core barrel, thermal The required edits ir.clude the flux above I-MeV and shield, vesse! and an outer concrete bmlogical shield. 0.10 MeV, the displacements-per-atom /sec., and the j The pressure vessel has an inner radius of 86.25 in and is group-wise flux at speciSed lxations. ' 8.$ in thick including a 0.25 in stainless steelliner on the inner su-face. Separate benchmark problems are in order to evaluate the method of predicting vessel provided for a standard core loading, a low-leakage core fluence as the product of the surveillance capsule ler.d loading and a partial length shield assembly core. He factor and a dosimetry measurement, dosimetry reaction SCL is for a typical equilibiium cycle core and the LLCL rates are calculated for a surveillance capsule, at the is based on recent core designs in which high burnup fuel following locations: (1) on the outer wall of the thermal assemblies are loaded on the core periphery to reduce the shield, (2) on the inner wall of the vessel, and (3) in the core leaksge, and which ultimately reduce the vessel cavity, ne inner capsule is located at an azimuth of 20' inner wall fluence. The PLSA core benchmark problem on the outer surface of the thermal shield at a radius of is representative of core designs that have been used to 202.25 cm. De vessel capsule is located at an azimuth redu the vessel fluence at the off beltline axial beations of 20' near the inner surface of the pressure vessel at a of circumferential welds. In the PLSA core design partial radius of 215.43 cm. He cavity capsule geometry and length shield assemblies, in which the fael rods in the materials are not represented in the benchmark problem, lower n&ns of the fuel assembly have been replaced however, the capsule edit is taken at the azimuth of 9.5' with stekss steel rods for shielding, are located on tlie near the concrete shield at a radius of 320.06 cm.t In periphery of tne core. The LLCL and PLSA problem performing the calculations, both the vessel and thermal geometry and materials are identical to the standard core shield capsules are never in the problem simultaneously. benchmark problem specifications, except for the fuel ne vessel capsule is always inclued in the model assembly core loadings. except when the thermal shield capsule resp.sc or downcomer flux and spectrum are being calcu'ated. He problem specification conststs of the defmition of the - problem geometry, material compositions by region, core ne detailed speciScations of the benchmark problems neutron source, and specification of the solution edits. for the standard core, low-leakage core and i'LSA core The problem geometry is specified for a honzontal plane are provided in the tables and figures of the following and is assumed to be uniform over the height of the core Sections 2.2,2.3 and 2.4, respectively. or, as in the case of the PLSA core, over the specified (upper or lower) section of the core. He regions above and below the core are assumed to be unifen 2,1.2 Specification of 8he Standard Core l imgsaus compositims out to the core baffle. All L4ading Prol%n l regions in the 1mrizontal geometry, except for the core (arid including the dosistry capsules) are assumed to be uniform in the axial dunension and to extend over the fbil l beight of the core. The material compositions are 'The cavity capsule was not included in the problem specified for each gemetrical region. in order to avoid unnecessarily ccanplicatmg the azimuthal mesh and to minimize rimning timesc la ne source description includes the core power and practice, however, the cavity capsule rhauld be mposure distributions in rectanguler pu-uy. He modeled explicitly.
.8, .,, .
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- 2. Denchmuk Problem Specifcation -
l- The basic design data for the standard core loading is geometry, material laydown and orientation are given in presented in Table 2.1.2.1 including the radii of the Figure 2.1.2.4. various material regions. The pressure and terr.perature of the coolant regions is included to allow the The specific edit quantities and corresponding locations determination of the coolant density. The material map for the standard core loading are ghtn in Table 2.1.2.8. is given in Figure 2.1.2.1 along with the component The axial location of the peak flux edits varies since the locations and dimensions. The x and y orientations are axial peak location depends on the radial location. also given in order to orient the cource data given in Tables 2.1.2.5 and 2.1.2.6. The core and fuel assemblics 2.1.3 Specification of the Low-Leakage are described in Table 2.1.2.2 including the reflector Core Loading Problem mate %1s and temperatures for the upper andlower teilector regions to be used in the axial calculations. The The basic design data for the low-leakage core loadmg is s#tcation material compositions are provided in Table I prespnted in Table 2.1.3.1 including the radil of the 2.1.2.3 for each mhture used in the radial and axial geometry of the benchmark problem. ne fragtfon of the vanous material regions. The pressure and temperature i of the coolant regions is included to allow the individual isotopes (taken from Reference 4) is given in Table 2.1.2.3.1. determination of the coolant density. The material map is g ven in Figure 2.1.3.1 along with the component locations and dimensions. The x and y orientations are The axial map of the SCL benchmark problem b ghtn da pven in order to orient the source data ghtn in in Figure 2.1.2.2. This map represents . vertical plane throue,h the core at the core flats at 0 = 0' The material Tables 2.1.3.5 and 2.1.3.6. The core and fuel assemblics are described in Table 2.1.3.2 including the reflector regions outside the core (Regions 4 th ough 16) are considered to be axially uniform. The axial regions of materials and temperatves for the upper and lower Figure 2.1.2.2 are assigned in Table 2.1.2.4. reflector regiomo M und in ik ahcubdom. TM specification material compositions are provided in
,ihe SCL fuel assembly source data is provided in Table 2.1.3.3 for each mixture used in the radial and axial geometry of the benchmark problem.
Table 2.1.2.5 incluong the location, relative assembly power, and the beginning and end of-cycle (BOC and EOC) fuel burnup for each fuel assembly m the octant %c axial map of the LLCL benchmark problem is given representation. The locanons of the peripheral fuel in Figure 2.1.3.2. This map represents a venical plane througl the core at the core flats at 0 = 0* The material assemblics are included with the assembly pin power regions outside the core (Regions 4 through 16) are data of Table 2.1.2.6. The fuel pin wise geometry, considered to be axially uniform. The axial regions of power and burnup data for a selectM peripheml assembly are given in Table 2.1.2.6. The orientation of F gure 2.1.3.2 are assigned in Table 2.1.3.4. this data is defined by the pin-cell boundaries and the ducctions given in Figure 2.1.2.1. The pin-wise data for The LLCL fuel assembly source data is provided in all the peripheral ass-mblies is available as a computer Table 2.1.3.5 including the location, relative assembly file on several physical media (e.g., 3.5" or 5.25' floppy poutr, and the beginning and end-of cycle fuel burnup disk,8 mm data tape, DC 6150 data cartridge, etc.) to be for each fuel assembly in the octant representation. The selected by the user. The axial power distrilmtions to be locations of the peripl.eral fuel assembly are included with the assembly pin power data of Table 2.1.3.6. The used in determining the axtal source are provided in fuel pin-wise geometry, power and burnup data fm a Table 2.1.2.7 for each of t'.4 four radial zones defined at selecux! peripheral assembly are given in Table 2.1.3.6. the bononn oGable 2.L23. The orientation of this data is defined by the pin cel! TE ~ spec:fic locations of the m. vessel snrveillance boundaries and the directions given in Figure 2.1.3.1.
, r.apsules and thelocation where the esvity capsule edit is Tk pin-wise data fu dl b periphere unmMies b to be taken are presented in Firv e 2.1.2.3. Unlike the available as a coniputer file on several physical media in-vessel survedlance locations, no physical capsule is (e.g., 3.5" or 5.25* floppy diA, 8 mm data tape, DC 6150 data cartridge, etc.) to be selected by the user. The present at the cavity location. The in-vts el capsule axh1 power distribudom tm und in determidng h W@@s%WMP$b %MMMW 30 W MMWH 15- #4 L '
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- 2. Benchmark Problem Specification axial source are provided in Table 2.1.3.7 for each of the regions, respectively, including the location, relative
- four radial zones defined at the bottom of Table 2.1.3.7. assemblypower,andthebeginningandend of cyclefuel o burnup for each fuel assembly in the octant
- ne'speciAc locations of the in-vessel surveillance representation. The locations of the peripheral fuel capsules and the location w here the cavity capsule edit is assemblies are included _ with the assembly pin power to be taken are presented in Figure 2.1.3.3. _Unlike the data of Tables 2.1.4.7 and 2.1.4.8. He fuel pin wise in vessel surveillance locations, no physical capsule is geometry, power and burnup data for 'a selected present at the cavity location. De in vessel capsule peripheral assembly for the upper and lower cores are geometry, material laydown and orientation are given in given in Tables 2.1.4.7 and 2.1.4.8, respectively. The Figure 2.1.3.4. orientation of this data is denned by the pin cell boundaries and the directions given in Figure 2.1.4.1.
De speci8c edit quanthies and corresponding locations ne pin-wise data for all the peripheral assemblies is for the low leakage core loading are given in Table available as a comp"ter Sie on several physical media 2.1.3.g. De axiallocation of the peak Aux edits varies- (e s., 3.5" or 5.25" Goppy disk, 3-aun data tape, DC since the axial peak location depends on the radial 6150 data cartridge, etc.) to be selected by the user. The location. axial power distributions to be used in deterndning the axial source are provided in Tables 2.1.4.9 and 2.1.4.10 for the upper and lower cores, respectively, for 6ach of 2,1.4 Specification of the Partial Length the four radial zones deAned at the bottom of Tables. '
- Shield Assenibly Cere Loading Problem W 8PunSc edit quandda and conssponding lxadons for the partial length shield assembly core loading are The basic design data for the partial length shield assembly core loading is presented in Table 2.1.4.1 including the radii of the various material regions. De ,
pronum and temperame of the coolant regions is 2.2 BWR Problem Specification included to allow the determination of the coolant density. De material map is given in Figure 2.1.4.1 along with the component locations and dimensions. 2.2.1 Introduction h x and y orientations are also given in order to orient the source data given in Tables 2.1.4.5 through 2.1.4.8. De BWR pressure vessel Duence benchmark problem is De core and fuel assemblies are described in - for a 800 fuel bundle core having an axial height of l Table-2.1.4.2 including the reGector materials and 381.0 cm and including the shroud, jet pumps and riser, j _ temperstmasfortheupperandlowerreDectorregionsto vessel and an outer concrete biological shield. The be used bi the axial calculations. De specnAcation pressure vessel has an inner radius of ~ 321.786 cm and material compositions are provided in Table 2.1.4.3 for is 16.129 cm thick with a 0.476 cm stainless steelliner each mixture used in the radial and axial geometry of the on the inner surface The core power and fuel bundle h-h=* publem. burnup distributions are for a typical equilibrium core. De PLSA con 8 3uration is pnnented in Figure 2.1.4.2, %e problent specificatica consists of the de6aition of and the axial map of the PLSA problem is given in the problem geometry, material compositions by region, - Figme 2.1.4.3.: This map represents a vertical plans = ; core neutron source, and 7 N= of the solution thmugh the cue at the con Bus at 8_= 0', De mahrial . edits. De *==k= are spectSed for each of the agions outside the core (Regions 6 through 18) are geometrical regions used to de6ae the problema De considsed to be axially uniform. The axial regions of ' inner and partphant oore see each divided into seven Figure 2.1.4.3 an assigned in Table 2,1.4.4. ? axial material regions. The regions slme andbelow the 4 The PLSA thel assembly source data is provided in core . am assened to be unisorm - E m compositions out to the edge of the core.1 All regions in Tables 2.1.4.5 :.nd 2.1.4.6 for the upper and lower core the horizontal geometry, except for thelcore'(and
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- 2. Benchmark Problem Specification including the dosimetry capsules) are assumed to be The axial map of the benchmark problem is gimn m uniform in the axial dimension and to extend mtr the Figure 2.2.2.2. This map represents a vertical plane full height of the core. The material compositions are through the core at the core 'lats at 0 = 0'. De material specified for each geometrical region. regions outside the core are considered to be axially unifonn. 3e axial extent of thejet pumps and risers is The source deacription includes the core power and taken to be the same as the height of the core. The axial exposure distributions in rectangular geometry. The regions of Figure 2.2.2.2 are assigned the compositions power distribution is based on a detailed 8 = 8 fuel bundle in Table 2.2.2.3.
pin wise power distribution for a typical core Ir.ading. The fuel nuclide fission fraction is prmided in Table The fuel assembi source data is prmided in 2.2.1.1 to allow the determination of the exposure Table 2.2.2.4 including the location, relative assembly demadana of the neutron source strength (neutrons / power, and the fuel burnup for each fuel assembly in the MeV)and the source spectrum. octant representation. The locations of the peripheral fuel assemblies are included with the asserrbly pin The required edits include the flux above 1 McV and power data el Table 2.2.2.5. The fuel pin wise 0.10 MeV, the displacements-per stom/sec., and the geometry, power and burnup data for the peripheral group-wise flux at specified locations. ademblies are given in Table 2.2.2.5. De orientation of this data is defined by the pin <cil boundaries and the In order to evaluate the method of predicting vessel directions given in Figure 2.2.2.1. The pin power Duence as the product of the surveillance capsule lead dir.;.'b..d= f:r assemblies on the edge of the core are factor and a dosimetry measurement, dosimetry reaction represented with an 8x8 array, assemblies one-row from rates are calculated for a surveillance capsule on the the edge are represented with a 4x 4 array, and assemblies innerwallof thevessel, nesesselcapsuleislocated at two rows from the edge are represented with a 2x2 array. an azimuth of 3* at the inner surface of the pressure The pin wise data for all the peripheral assemblies is vessel at a radius of 319.195 cm. available as a computer file on several physical media (e.g., 3.5" or 5.25" floppy disk, 8 mm data tape, DC The detailed specifications of the benchmark probicm is 6150 data cartridge, etc.) to be selected by the user. The prmided in the tables and figures of the fellowing axial power distributions to be used in determining the Section. axial source are prmided in Table 2.2.2.6 for each of the . three radial zones defined at the bottom of Table 2.2.2.6. The pressure vessel capsule geometry, materiallaydown 2.2.2 Specification of the BWR Benchmark and orientation are given in Figure 2.2.2.3. Problem ne specific edit quantities and corresponding locations The basic design data for the BWR benchmark problem for the standard core loading are given in Table 2.2.2.7. is presented in Table 2.2.2.1 including the radii of the ne axial location of the peak flux edits varies since the various material regions. The material map is given in axial peak location depends on the radial location. Figure 2.2.2.1 along with the component locations and dimensions. The x and y orientations are also given in order to orient the source data given in Tables 2.2.2.5 and 2.2.2.6. The core and fuel assemblies are described in Table 2.2.2.2 inMag the reflector materials for the Upper and lower reflector regions to be used in the axial ypn.nnmandana 'lkspeci6cationmaterialcomposttions'are' ' provided in Table 2.2.2.3 for each mixture used in the radial and axial geometry of the t= hi problem. The fraction of the individual isotopes (taken from Referetwe 4) is given in Table 2.2.2.3.1.
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Table 2.1.1.1 . Fraction Of Fissicna by Isotope as Function of Exposure , E sure ( ) 0 235 U 238 Pu 239 Pu 240 Pu 241 Pu 242 1.500E+02 5.000E+02 9.28100E 016.17165E 02 1.01828E 02 1.65450E 07 4.25775E 07 0.00000E+00
- 1.000E+04 9.05149E 01 6.21387E 02 3.26955E 02 1.77633E 06 1.49927E 051.80072E 10 2.000E+04 5.57019E 01 7.07435E 02 3.39497E 01 3.10546E 04 3.24187E 02 1.08465E 05 4.000E+04 3.56399E 01 7.81926E 02 4.64707E 01 7.40748E-04 9.98821E.02 7.83614E 05 1.23133E 01 9.01196E 02 5.82823E 01 1.43769E 14 2.035445 01 3.00635E 05 6
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i Table 2.1.2.1 Standard Core Loading Basic Design Data 4................
.. Reactor Material
..........................................l.........
.' Thermal Power . 2527.73 3et(TE) .
-- . I
. Core Inlet Temp. . . 536'F . - .
. Core Operating Pressure . 2010 psia .
. Baffle Thickness' . 1.5075 cm .- 88 304 .
e
. By Pass . -- . E20 (560 F .
. . - . 2010 psia).
j . Inner Radius of Core Barrel. . 190.105 cm . - , f
. Barrel Thickness . 3.01 cm . 58 304 .
l . Inner-Inlet Thickness . J.54 cm . E20 (536*F . [_
.- . . 2010 psia).
j . Inner Radius of Thermal-Shield. 196.535 cm . - . I i i . _. Thermal Shield Thickness . 3.01 cm . 88 304 . l j
.: Outer Inlet Thickness . 10.095 cm- . E2 0 (536*F .
j_ . . . 2010 psia) , j _,..................................................................,
. Inner Radi us of Li ner Clad -. 210.440 cm . -- . i
.-Vessel Liner Clad Thickness . 0.635 cm . 88-304 .
T
. Vessel Thickness . 21.59 cm . SA 3023. .
l ....................................... ...........................,
. FY Insulation Air Thickness . 1.035 cm . Air .
g ,................................................................... l l e
.. FT. Insulation Thickness . 10.16 cm . PV Insulation .
L I
, -, Cavity Thickness . .. 02.52 cm . Air .
j - p%Qmpup r Zaner' medius tof f * ' ~" d VM"335;200 osE # OF ^ WN ' W .; '
. Biological Shield
[ . l~ ..-Bio Shield Liner Thickness . 0.635 cm . SA 3023 . 4 ...................................................................., t
.-Bio Shield Thickness .- 213.36:em . ~ - . Concrete 1 ..
- ......e.........................................................e..
- k. + 3 b*#
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l Table 2.1.2.2 Standard Core Loading Core and Fuel Assemblies Total-Number of Fuel Assemblies 204 .
- .- Number of Roda per assembly (15x15) 214 fuel rods .
. 3 guide tubes .
1 instrument tube . Assembly Pitch 21.495 cm . Pin Pitch 1.4*,233 cm
. Fuel Material Sintered UO2 Pellets .
. Cladding Material Zr.4 [
. Fuel Active Length 335.20 cm .
Standard Core Loading Sesic Design Dat,
"";per and Lower Reflectors
. Lower Reflector Thickness 13.97 cm 88 304 + Water (536*F) .
. Upper Reflector Thickness
-32.865 cm S8-304 + Water (554'F)
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- Table 2.1.2.3 Standard Core Loading Design Specification Material Compositions
. Mixture Component Atom Densities .
(atos/b*ca) .
. E 2.82500E 02 .
. B 2.69200E 05 .
. O 1.41200E 02 .
. C 2.58100E 05 .
O (fuel) 1.28500E 02 .
. Al 3.56000E=04 .
. Core Cr 1.608005 05 .
. Fe 2.20500E 05 .
. Mi 3.87700E 05 .
. Er 5.44800E 03 .
. U 235 1.12000E 04 .
. U-238 6.03000E 03 .
Pu 239 2.20000E 05 .
. Pu 240 7.12000E 06 .
.................................................................. t
. Cr 1.05300E-02 .
. Baffle Mn 1.75200E*03 .
. (SS-304) Fe 5.00700E 02 .
. Mi 8.57400E 03 .
. Bypass + E 4.92900E 02 .
. (560 F) 0 2.464005 02 .
. S 4.90000E 06 .
. Cr 1.85300E*02 .
. Core Barrel Mn 1.75200E 03 .
. (88 304) -Fe 5.80700E-02 .
. N1 8.57400E 03 .
. Inlet Water Gap I '5.09600E 02 .
. (53C F) 0 2.54800E 02 .
. B 5.10000E 06 .
. Cr 1.853005 02 .
. Thermal Shield Mn 1.75200E 03 .
. (SS 304) Fe 5.80700E 02- .
. Ni 8.57400E 03 .
. Cr 1.85300E=02 .
. EFV Liner Mn 1.75200E 03 .
fi .' -(SS 304) Fe 5.807004-02' .
. Ni 8.57400E 03 .
. ..............................~....................................
. Cavity. N 3.20000E-05 .
. (Air) O 8.00000E 06 .
~ - '
+This composition is also to be used in the water region between the fuel assembly-and the core ballle (see Fqure 2.2.1).'
~
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1 Table 2.1.2.3 Standard Core Loading Design Specification Material Composizions (cont'd)
. Mixture Component Atom Densities .
. (a tom /b
- cm) .
. C 9.84000E-04 .
. RPV Wall Si 7.58900E 04 .
. (FA.302B) Mn 1.39100E 03 .
. Fe 8.18300E 02 .
. Mo 3.24800L.04 .
. Cr 3.43000E.04 .
. Mn 3.24000E.33 .
. RPV Fe 1.07400C 03 .
. Insulation Ni 1.59000E 04 .
. # A1 1.30000E.04 .
. N 3.77000E 06 .
. O 9.96000E 06 .
. C 9.84000E 04 .
. Bio Shield Liner Si 7.589002 04 .
. (SA 302B) Mn 1.3910CE CJ .
. Fe 8.1830CE 02 .
. No 3.14000.1-04
. H 7.77000E 03 .
. C 1.15000E.04
. 0 4.38000E-02 .
. Na 1.tS000E-03 .
. Bio-Shield Mg 1.49000E.04 .
. (Concrete) Al 2.33000E-03 .
. Si 1.58000c-02 .
. K 6.93000E.04 .
. Ca 2.29000E 03 .
. Fa 3.13000E-04 .
. Cr 4.63250E-03 .
. Mn 4.38000E-04 .
. Lower Reflector Fe 1.45175E-02 .
. (Water Steel) Ni 2.14350E 03 .
. (536 F) H 3.92200E-02 .
. O 1.91100E-02 .
. B 3.82500E 06 .
Cr 4.63250E-03 .
. Mn 4.39000E.04 .
. Upper Reflector Fe 1.45175E.02 .
. (Water Steel) Ni 2.14350E-03 .
. (584 F) H 3.55383E.02 .
. O 1.77656E.02 .
. B 3.53293E-06 .
u '. . 44
. \. .
4
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l I 4 Table 2.1.2.3.1
. Isotopic Fractions in Cr, Fe and Ni*
i . ............................................................
. ISOTOPE . MT % . ISOTOPE . WF %^ . ISOTOPE . WT % .
. . . . -Cr 50 . 4.345 . Fe 54 . / 5.9 .--Ni 58 . 60.27 .
. Cr 52 . 03.79 *. Fe 56 . 91.72 . Ni 60 . 26.10 .
. Cr 53 . 9.5 . Fe.57 . 2.1 . Ni 61 . - 1.13 .
. Cr 54. . 2.365 . Fe 58 . 0.20 . Ni+62 . 3.59 .
. . _ ..... . ..... . ..... . Ni 64 . 0.91 .
*Taken from Reference 4 -
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Tab'4 2.1.2.4 Standard Core Loading Axial tone Assignments
. Eone Description .
4.......................................
. . Lower Reflector .
. 2 Active Core Puel Assemblies .
J Uppt.r Reflector .
. 4 Core Battle . .
. 5 By Pase .
.s
. 6 Core Barrel .
7 Inner Inlet Water Gap . -
. 8 Thermal shield .
. 9 Outer Inlet Water Gap .-
10 R6 actor Praasure Vessel Liner .
. 11 Reactor Pressure vessel .
. 12 Air Gap ,
. 13 Pressure Vessel Insulation l
, 14 Cavity .
. 15 Biological shield Liner .
. 16 Biological shield .
........................ 5....................e..............
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Table 2.1.2.6 Standard Core Loading Pin Geometry. Power. and Burnup Distributions Assembly 6 Fin Power Set 13 Belative ROC EOC Pin Burnup Eurnup E.Left E Eight Y. Rot Y.Yop Power (MND ) (NWD ) 1.07425E+02 1.000578+02 0.00000E+00 1.43223E+00 1.09342E+00 6.621E+03 1.092E+04 1.074285+02 1.000573+02 1.41223E+00 2.064465+00~1.032565+00 6.621E+03 1.092E+04 1.074285+03 1.000575+02 2.064463+C0 4.29649E+00 1.00315E+00 6.621E+03 1.092E+04 1.07425E+02 1.00057E402 4.296695+00 5.72092E+00 1.006193+00 6.621E+03 1.092E+04 1.07425E+02 1'.000575+02 5.72092E+00.7.16115E+00 0.00000B+00 6.621E+03 1.092E+04 1.07425E+02 1.000575+02 7.16115E+00 0.59330E+00 9.900753 01 6.6215+03 1.092E+04 1.07425E+02 1.000575+02 0.59330E+00 1.002563+01 9.757603 01 6.621E+03 1.092E+04 1.07425E+02 1.000573+02 1.002563+01 1.14570E+01 9.696743 01 6.621E+03 1.092E+04 1.07435E+02 1.000575+02 1.14570B+01-1.20901E+01 9.777893 01 6.621E+03 1.092E+04 1.07425E+02 1.000575+02 1.20901E+01 1.43223r+01 1.00213E+00 6.621E+03 1.092E+04 1.07425E+02 1.000575+02 1.43223E+01 1.57545B+01 0.00000E+00 6.621E+03 1.092E+04
- 1.07425E+02 1.000575+02 1.57545E+01 1.71060E+01 1.005175+00 6.621E+03 1.092E+04 1.07425E+02 1.00057E+02 1.71060E+01 1.06190E+01 9.909755 01 6.621E+03 1.092E+04 1.07425E+02 1.000575+02 1.06190E+01 2.00512E+01 9.96046E.01 6.621E+03 1.092E+04
. 1.074253402 1.000573+02 2.00512E+01 2.14035E+01 1.01633E+00 6.621E+03 1.092E+04 1.000575+02 1.102093+02 0.00000E+00 1.43223E+00 1.09030E+00 6.621E+03 1.092E+04 1.000573+02 1.102095+02 1.43223E+00 2.064465+00 1.03350E+00 6.621E+03 1.092E+04 1.000573+02 1.102093+02 2.06446E+00 4.296695+00 1.00112B+00 6.621E+03 1.092E+04 1.000573+02 1.102093+02 4'.296695+00 5.72092E+00 1.02050E+00 6.621E+03 1.092E+04 1.000575+02 1.102093+02 5.72092E+00 7.16115E+00 1.032565+00 6.621E+03 1.092E+04 1.000573+02 1.102093+02 7.16115E+00 0.59330E+00 1.025465+00 6.621E+03 1.092E+04 1.000575+03 1.10209E+02 0.59330E+00 1.00256E+01 1.00923E+00 6.621E+03 1.092E+04 1.000575+02 1.102093+02 1.00256E+01 1.14570E+01 1.002135400 6.621E+03 1.092E+04 1.000575+02 1.102095+02 1.14570E+01 1.20901E+01 1.011265+00 6.621E+03 1.092E+04 1.000575+02 1.102093+02 1.20901E+01 1.43223E+01 1.02952E+00 6.621E+03 1.092E+04 1.000375+02 1.10209E+02 1.43223E+01 1.57545EIO1 1.03560E+00.6.621E+03 1.092E+04 1.000575+02 1.102095+03 1.5754b5+01 1.71060E+01 1.02640E+00 6.621E+03 1.092E+04 1.000575+02 1.102093+02 1.71060E+01 1.06190E+01 9.040095 01 4.623B+03 1.092E+04 1.000573+02 1.102095+02 1.06190B+01 2.00512E+01 9.919993 01 6 321E+03 1.092E+04 1.000575+02 1.102093+02 2.00512E+01 2.14035E+01 1.00112E+04 6.621E+03 1.092E+04 1.102095+02 1.11722E+02 0.00000E+00 1.43223E+00 1.09240E+00 6.621E+03 3.092E+04 1.103095+02 1.11722E+02 1.43223E+00 2.06444E+00-1.032563+00 6.621E+03 1.092E+04 1.102093+02 1.11722E+02 2.064465+00 4.296695+00 1.006195+00 6.621B+03 1.092E+04 1.10209E+02 1.11722E+02 4.296693+00 5.72092E+00 1.011263+00 6.621E+03'1.092E+04 1.102095+03 1.11722E+02-5.73062B+00 7.16115B+00 1.011365+00 6.621E+03 1.092E+04 1.102093+02 1.11722E+02 7.16115B+00 0.59330E+00,6.095963 01 6.621E+03:1.092E+04
- 1kl02098+03 1.11722E+02 0.59330E+00 1.002563+01 9.990093 01 6.621E+03 1.092E+04 1'.102093+02 1.11722E+02 1.002565+01 1.14570E+01-2.909753 01 4.6215+03 1.092E+04 1.102093+03 1.11722E+02 1.14570E+01 1.20901E+01'1.00112E+00 6.621E+03 1.092E+04 1.102095+02 1.11722E+02 1.20901B+0111.43223E+01 6.16697E.01 6.621E+03'1.092E+04 1.102093+03 1.11722E+02 1.43223E+01 1.57545E+01'1.013293+00 6.621E+03 1.092E+04
- 1;103095+02'l.117222+02 1.57545E+01'1'71060E+01:1.0073
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- f Table 2.1.2.6 Standard Core Loading Pin Geometry, Power, and Burnup Distributions (cont'd)
Assembly 6 Fin Power set 13 Bele *,1ve - 30C 50C Fin Burnup Eurnup E.Left~ I.Right Y.Eet Y. Top # Power (MWD ) (MWD ) 1.11722E+02 1.13154B+02 0.00000E+00 1.43223B+00 1.10762E+00 6.621E+03 1.092E+04
-1.117225+02 1.13154E+02 1.43223E+00 2.464465+00 1.077195+00 6.621E+03 1.092E+04 1.11722E+03- 1.13154E+02 2.064465+00 4.296495+00 1.02640E+00 6.631E+03 1.092E+04 1.11722E+02 1.13154E+02 4.296695+00 5.73092E+00 1.00113E+00 6.621E+03 1.09 2E+04 1.11722E+02 1.13154E+02 5.72092E+00 7.16115E+00 9.930035 01 6.6312+03 1.092E+04 1.11723E+02 1.13154E+02 7.16115B+00 0.59330E+00-9.909755 01 6.621E+03 1.092E+04 1.11722E+02 1.13154E+02 0.59330E+00 1.002565+01 9.030745 01 6.621E+33 1.092E+04 1.11722E+02 1.13154E+02 1.002565+01 1.14510B+01 9.70003E.01 6.621E+03 1.092E+04 1.11722E+02 1.13154B+02 1.14570E+01 1.209 01E+01 9.059 035 01 6. 6315+03 1.092E+04 1.11722E+02 1.13154B+02 1.209015+01 1.43223B+01 9.940175 01 6.621E+03 1.092E+04 1.11722E+02 1.13154E+02 1.43223E+01 1.57545E+01 9.950325 01 6.621E+03 1.092E+04 1.11722E+02 1.13154E+02 1.57545B+01 1.71060E+01 9.970608 01 6.621E+03 1.09 2E+04 1.11722E+02 1.13154E+02 1.71060E+01 1.06190E+01 1.00022E+00 6.621E+03 1.092E+04 1.11722E+02 1.13154E+02 1.061903+01 2.00512E+01 1.03053E+00 6.621E+03 1.092E+04 1.11722E+02 1.13154E+02 2.00512L+01 2.14035E+01 1.01532E+00 6.621E+03 1.092E+04 1.13154E+02 1.145065+02 0.00000E+00 1.43223B+00 0.00000B+00 6.621E+03 1.092E+04 1.13154E+02 1.145063+02 1.43223E+00 2.064465+00 1.00733E+00 6.621E+03 1.092E+04 1.13154E+02 1.145063+02 2.064465+00 4.296695+00 1.03256E+00 6.621E+03 1.092E+04 1.13154E+02 1.145063+02 4.296695+00 5.72092E+00 9.990095 01 6.621E+03 1.092E+04 1.13154E+02 1.145065+02 5.73092E+00 7.16115E+00 9.790175 01 6.621E+03 1.092E+04 1.13154E+02 1.145063+02 7.16115E+00 0.5933 0E+00 9.727175 01 6.621E+03 1.092E+04 1.13154E+02 1.145065+02 0.59330E+00 1.002565+01 9.69 6745 01 6.621E+03 1.09 2E+04 1.13154E+02 1.145065+02 1.002565+01 1.14570B+01 9.696745 01 6.621E+03 1.092E+04 1.13154E+02.1.145065+02 1.14570E+01 1.209015+01 9.7170?t 01 6.621E+03 1.092E+04 1.13154B+02 1.145065+02 1.20901E+01 1.43223E+01 9.767743 01 6.621E+03 1.092E+04 1.13154B+02 1.14506E+02 1.43223E+01 1.575453501 9.020603 01 6.621E+03 1.092E+04 1.13154E+02 1.145065+02 1.5754 5E+01 1.71060E+01 9.9 60465 01 6.621E+03 1.09 2E+04 1.13154B+02 1.145065+02 1.71060B+01 1.0619 0E+01 1.01532E+00 6.621E+03 1.092E+04 1.13154E+02 1.145065+02 1.06190E+01-2.00512E+01 1.041695+00 6.621E+03 1.092E+04 1.13154E+02 1.145065+02.2.00512E+01 2.14035E+01 0.00000E+00 6.6215+03 1.092E+04
-1.145045+02 1.16010E+02 0.00000E+00 1.43123E+00 1.10450E+00 6.621E+03 1.092E+04 1'.145065+03 1.16010E+02 1.43233E+00 2.064465+00 1.00023E+00 6.621E+03 1.092E+04 1.145065+02 1.16010E+02 2.064463+00 4.296695+00 6.19739E.01 4.621E+03 1.092P+04 1.145065+02 1.16010E+02 4.296695+00 5.72092E+00 9.97060E+01 6.621E+03 1.092E+04 1.145065+02 1.16010E+03 5.72062E+00 7.16115E+00 9.737315 01 6.6215+03 1.692E+04 1.145065+02 1.16010E+02 7.16115E+00 0.59330B+00 9.656175 01 6.6215+03 1.092E+04
^ 1;145065+02.1.16010E+02 0.59330B+00 '1.002565+01- 9.654175 01 6 ;621E+03' 1'.09 2E+04 -
1.145065+02 1.16010E+02 1.002565+01 1.14570E+01 9.606405 01 6.421E+03 1.092E+04 1.145065+02 1.16010E+02=1.14570E+01 1.20901E+01 9.606605 01 6.421E+03 1.092E+04 1.145065+02' 1.16010E+02 1.209 01E+01 1.43223E+01. 9.69 6745 01 6.621E+03 1.09 2E+04
'1.145065+02 1.160185+03 1.43223E+01 1.57545E+01 9.747743 0L 4.6215+03'1.092E+04 1.14504E+02 1.160195+02 1.575453401 1.71060E+01 9.950325 01 6.6215+03cle092E+04 1.145065+02 1.16010E+02.1.71060E+01 1.04190E+01.6.250255 01 6.6215+03 1.092E+04 1.145065+02 1.14010E+02 1.04190E+01 2.00512E+01 1.03662E+00 6.621E+0341.092B+04 Q li145065+02 1.16010E+02 2.06512E+01-2.14035E+01 1.012275+00 6.621E+03 1.092E+04
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4%@MghQnMbMW *mee *ms ,&- yW &9WOd@WM
r l TaWe 2.1.2.6 Standard Core !.oading Pin Geosotry, Power and Burnup Distributions (cont'd) Assembly 6 Fin Power Set 13 Belative ROC EOC Pin Burnup Eurnup I+Left E.Eitht Y. Bot Y+Yop Power (NWD ) (MWD ) 1.160195+02 1.174515+02 0.00000E+00 1.43223E+00 1.002265+00 6.621E+03 1.092E+04 1.16010E+02 1.17451E+02 1.43223B+00 2.064465+00 1.06094E+00 6.621E+03 1.092E+04 1.16010E+02 1.17451E+02 2.064465+00 4.296695+00 1.01930E+00 6.621E+03 1.092E+04 1.16010E+02 1.174515+02 4.29669E+00 5.72092E+00 9.079325 01 6.621E+03 1.092E+04 1.16010E+02 1.174515+02 5.72092E+00 7.16115E+00 9.60660E*01 6.621E+03 1.092E+04 1.16010E+02~1.17451E+02 7.16115E+00 0.89330E+00 9.646035 01 6.6215+03 1.092E+04 1.16010B+02 1.174515+02 0.59330E+00 1.002565+01 9.72717E*01 6.621E+03 1.092E+04 1.16010B+03 1.17451B+02 1.002565+01 1.14570E+01 9.020603 01-6.621E+03 1.092E+04 1.16010B+02 1.17451E+02 1.14570E+01 1.24901E+01 9.757505 01'6.621E+03 1.092E+04 1.16010E+02 1.174515+02~1.209015+01 1.43221E+01 9.606603 01 6.621E+03 1.092E+04
-1.160195+02 1.17451E+02 1.43223E+01 1.57545E+01 9.72717E 01 6.6215+03 1.092E+04 1.16010E+02 1.17451E+02 1.57545E+01 1.71060E+01 9.069175 01 6.621E+03 1.092E+04 1.16010E+02 1.17451E+02 1.71060E+01 1.06190E+01 1.004163+00 6.621E+03 1.092E+04 1.16010B+02 1.174515+02 1.06190E+01 3.00512E+01 1.010363+00 6.621E+03 1.092E+04 1.16010E+02 1.17451E+02 2.00512E+01 2.14035E+01 9.00946E+01 6.621E+03 1.092E+04 1.17451E+02 1.10003E+02 0.00000E+00 1.43223B+00 1.07415E+00 f.621E+03 1.092E+04 1.17451E+02 1.10003E+02 1.43223E+00 2.064465+00 1.05002E+00 6.621E+03 1.092E+04 1.17451E+02 1.10003E+02 2.044465+00 4.296695+00 1.00022E*00 6.621F+03 1.092E+04 1.17451E+02 1.10003E+02 4.296695+00 5.72092E+00 9.00J12E+01 6.621E+03 1.092E404 1.174515+02 1.10003E+02 5.*/2092E+00 7.16115E+00 9.656375 01 6.621E+03 1.092E+04 1.17451E+03 1.10003E+02 7.16115E+00 0.59330E+00 9.635035 01 6.621E+03 1.092E+04 1.17451E+02 1.10003E+02 0.59330E+00 1.002565+01 9.79017E*01 4.621E+03 1.092E+04 1.17451E+02 1.10003B+02 1.00256E+01 1.14570E+01 0.00000E+00 6.621E+03 1.092E+04 1.174515+02 1.10003E+02 1.14570E+01 1.20901E+01 9.02060E 01 4.621E+03 1.092E+04 1.174515+02 1.10003E+02 1.209015+01 1.43223E+01 9.60660E*01 6.621E+03 1.092E+04 1.17451E+02 1.10003E+02 1.43223E+01 1.57545E+~01 9.696743 01 6.621E+03 1.092J+04
.1.17451E+02 1.10003E+02 1.57545E+01 1.71060E+01 9.790175 01 6.621E+03 1.092E+04 1.17451E+02 1.10003E+02 1.71060B+01 1.06190E+01 9.94017E+01 6.621E+02 1.092E+04 1.17451E+02 1.10003E+02 1.06190E+01 2.00512E+01 1.00022E+00 6.6215+03 1.092E+04 1.17451E+02 1.10003E+02 2.00512E+01 2.14035E+01 9.000325 01 6.621E+00 1.092E+04 1.10003E+02 1.20315E+02 0.00000E+00 1.43223E+00 1.07922F.+00 6.621E+03 1.092E+04 1.10003B+02 1.20315E+02 1.43223E+00 2.064465+00 1.05792E+00 6.621E+03 1.092E+04 3
1.10003E+02 1.20315E+02 2.064465+00 4.296695+00 1.01532E+00 6.621E+03 1.09 2E+04 1.10003B+02 1.20315E+02 4.29669E+00-5.720922+00 9.040095 01 6.621E+03 1.092E+04 1.10003B+02 1.20315E+02 5.720$2E+00 7.16115E+00 9.64603R*01 6.621E+03 1.092E+04' 1.10003E+03:1.20315E+03 7.16115E+00 0.59330E+00 9.605455*01'6.621E+03 1.092E+04 1.10003E+02L1.20315E+02 0.59330B+00 1.002565+01 9.698745 01-6.621E+03'A.093E+04
- 1.10003E+02 1.20315E+02 1.002565+01'1.145795+01 9.79017E*01 6.821E+03 1.092E+04 1.10003E+02 1.20315E+02 1.14570E+01 1.20901E+01 9.727175 01 6.621E+03 1.092E+04 1.10003E+02 1.20315E+02 1.20901E+01 1.43223E+01 9.656173 01 4.621E+03 1.092E+04 1.10003E+03 1.20315E+02 1.43223E+01 1.57545E+01 9.698745 01 6.621E+03 1.092E+04 e 1.10003E+02 1.20315E+02 1.57545B+01_1.71060E+01 9.040093 01 6.621E+03 1.092E+04 1,10003E+02'1.20315E+02 I
1.71060E+01 1.06190E+01'1.00315E+00 6.621E+03 1.092E+04 1.10003B+02 1.20315E+02 1.06190E+01 2.00512E+01'1.01735E+00'6.6215+03*1\092E+04
, 1.100035 02 4.203155 02 . 005,25 01 2.140353 01 9.079325 01 . 4215 03 1.0925 04
_ + . n. s: ,m. ,. < a- ,
,.3 g y ; chl q ,. t h k
$ g }q ,1 } t l- t ! -
-d fin ke' MbMWMm . 3 A g g % ,, W p w 4. -
- W -
- - - . . ~ - _ . . -.. - . - --. _- - - - - .- - - - - - -
Table 2.1.2.6 Etandard Core Loading Pin Geometry, Power. and turnup Distributions (cont'd) Assambly 6 Fin Power Set 13 Belative BDC EDC Pin Burnup turnup 2*Left X*Right Y'90t Y Top Power (mwd ) (MWD ) 1.20315E+02 1.21747E+02 0.00000E+00 1.43223E*00 1.0974 8E+00 6.621E+03 1.092E+04 1.20315E+02 1.21747E+02 1.43223E+00 2.86446E+00 1.07415E+00 6.621E+03 1.092E+0 4 1.20315E+02 1.217475+02 2.06446E+00 4.29669E+00 6.15602E*01 6.621E+03 1.892E+04 1.20315E+02 1.21747E+02 4.29669E+00 5.72092E+00 9.90975E 01 6.621E+03 1.0923404 1.20315E+02 1.217475+02 5.72092E+00 7.16115E+00 9.67646E*01 6.621E+03 1.092E+^4 1.20315E+02 1.217475+02 7.16115E+00 8.59330E+00 9.59531E 01 6.621E+03 1.092E+04 1.20315E+ 02 1.21747E+02 8.5933 0E+00 1.00256E+01 9. 59 533 E* 01 6. 621E+ 03 1.092E+ 04
- 1. 20315E+ 02 1.21747E+ 02 1. 00256E+01 1.14570 E+01 9. 62574E+ 01 6. 621E+ 03 1. 89 2 E4 04 1.20315E+02 1.217475+ 02 1.14570E+01 1.209 01E+ 01 9. 63500E + 01 6. 621E+03 1. Oh J+ 04
- 1. 20315E+02 1. 21747E+02 1. 209 01E+01 1. 43223 E+ 01 9. 64 603 E* 01 6. 421E+03 1. 39 2E + 04
- 1. 20315E+02 1. 21747E+02 1.43 223 E+01 1.57545E+ 01 9.72717E
- 01 6. 621E+ 03 1. 89 0E+ 04 1.20315E+02 1.21747E+02 1.57545E+01 1.718 60E+01 9.93 003E 01 6. 621E+03 1. 092E+04 1.20315E+02 1.21747E+02 1.71060E+01 1.06190E+01 6.21768E.01 6.621E+03 1.092E+04 1.20315E+02 1.21747E+02 1.0619 0E+01 2.00512E+01 1.03662E+00 6.621E+03 1.092E+04 1.20315E+02 1.21747E+02 2.00512E+01 2.14035E+01 1.01227E*00 6.621E+03 1.092E+04 1.21747E+02 1.23180E+02 0.00000E+00 1.43223E+00 0.00000E+00 6.621E+03 1.092E+04 1.21747E+02 1.23180E+02 1.43223E+00 2.06446k+00 1.00125E+00 6.C21E*03 1.09 2E+04 1.21747E+02 1.23190E+02 2.06446E+00 4.29669E+00 1.02546E+00 6.621E+03 1.092E+04 1.21747E+02 1.23100E+02 4.29669E+00 5.72092E+00 9.919095+01 6.621E+03 1.092E+04 1.217475+02 1.23140E+02 5.72092E+00 9.16115E+00 9.727175 01 6.621E+03 1.092E+04 1.21747E+02 1.23100E+02 7.16115E600 0.59330E+00 9.658175 01 6.621E+03 1.092E+04 1.21747E+02 1.23180E+02 8.59330E+00 1.00256E+01 9.63500E*01 6.621E+03 1.092E+04 1.21747E+02 1.23180E+02 1.002565+01 1.14578E+01 9.63580E 01 6.621E+03 1.892E+04 1.217475+02 1.23180E+02 1.14570E+01 1.20901E+01 9.66631E*01 6.621E+03 1.892E+04 1.21747E+02 1. 2318 0E+02 1. 2 0 9 01E+01 1.43 223 E+01 9.717 03 E + 01 6. 6 21E+03 1. 09 2E+ 04 1.21747E+02 1.23100E+02 1.43223E+01 1.575453401 9.7000,3E 01 6.621E+03 1.892E+04 1.217475+02 1.23100E+02 1.57545E+01 1,71868E+01 9.94017E*01 6.621E+03 1.092E+04 1.217475+02 1.23100E+02 1.71060E+01 1.06190E+01 1.01532E+00 6.621E+03 1.092E+04 1.21747E+02 1.23100E+02 1.0619 0E+01 2.00512E+01 1.0406 BE+00 6.621E+03 1.09 2E+ 04 1.21747E+02 1.23180E+02 2.00512E+01 2.14035E+01 0.00000E+00 6.621E+03 1.092E+04 1.23100E+02 1.24612E+02 0.00000E+00 1.43223E+00 1.10255E+00 6.621E+03 1.092E+04 1.23160E+02 1.24612E+02 1.43223E+00 2.06446E+00 1.07415E+00 6.621E+03 1.092E+04 1.23100E+02 1.24612E+02 2.06446E+00 4.29669E+00 1.02343E+00 6.6211+03 1.092E+04 1.23100E+02 1.24612E+02 4.29669E+00 5.72892E+00 9.97060E*01 6.621E+03 1.0*2E+04
.1.23180E+02 1.24612E+02 5.720$2E+00 7.16115E+00 9.89960E.01 6.521E+03 1.092E+04 1.23190E+02 1.24612E+02 7.16115E+00 .9.59330E+00 9.079325 01 6.621E+03 1.092E+04
.1.23100E+02 1.24612E+02 8.59330E+00 1.00256E+01'9.81046E 01 6.621E+03 1.092E+04 1.23100E+02 1.24612E+02 1.00256E+01 1.14578E+01 9.767743 01 6.621E+03 1.092E+04 1.23100E+02 1.24612E+02 1.14570E+01 1.20901E+01 9.84009E 01 6.621E+03 1.092E+04 1.23100E+02-1.24612E+02 1.20901E+01 1.43223E+01 9.95032E 01 6.621E+03 1.092E+04 1.23180E+02 L1'.24612E+02:1".43223E+01* 1.57545E+01 9.9 0075E 01 6.621E*03 1.092E+04 1.23180E+02 1.24612E+02 1.57545E+01 1.71868E+01 1.001128400"6.621E+03 l'.092E+04 1.23180E+02 1.24612E+02 1.71868E+01 1.06190E+01 1.01430E+00.6.621E+03;1.092E+04 1.23100E+02 1.24612E+02 1.86190E+01 2.00512E+01 1.03966E+00 6.621E+03 1.092E+04
. 1. 23100E+02 1., ;24,612E+02 ' 2. 00 512 E+ 01 2.14 1'. 89 2E + 04 m, ,
,e 83 5 E+ 01 1. 02241E+00 - 6. 6 21E+ 03, opw i r ;ft l , O$ N h! - ,
s j
.!pe
- 4 Qd%M 3 e .[7 - ; ja 4- { [% M g6.qha 4 4,.> 4 y Q
Table 2.1.2.6 Standard Core Loading Pin Geometry, Power. and Burnup Distributions (cont'd) Assembly 6 Pin Power Ret 13 Relative ROC Eoc Pin Burnup Burnup 1.Left X.Right Y. Bot Y. Top Power (MWD ) -0063 ) 1.24612B+02 1.26044E+02 0.00000E+00 1.43223E+00 1.09740E+00 6.6215 03 1.092E+04 1.24612E+02 1.26044B+02 1.43223E+00 2.064465+00 1.03763E+00 6.621E+03 1.09 25*04
- 1.24612E+02 1.36044E+02 2.06444E+00 4.296695+00- 1.013295+00 6.621E+03 1.092E+04 1.24512E+02 1.36044D+02 4.296698+00 5.72092E+00 1.020395+00 6.621E+03 1.092E+04 1.24612E+02 1.26044E+02 5.72092E+00 7.16115E+00 1.02242B+00 6.621R+03 1.092E+04
' 1.24612E+02 1.26044E+02 7.16115E+00 0.59330E+00 6.156025 01 6.6215+03 1.092E+04 1.24612B+02 1.36044E+02 0.59330E+00 1.002565+01 1.01025E+00 6.631E+03 1.092E+04 1.24612B+02 1.26044E+02 1.002565+01 1.14570E+01 -1.00315E+00 6. 621E+03 1.09 2E+ 04 1.24612E+02 1.26044E+02 1.14470E+01 1.209015+01 1.01532E+00 6.621E+03 1.092E+04 1.24612E+02 1.26044E+02 1.209 01E+01 1.432233,01 6 :237975 01 6.621E+03 1.09 2E+04 1.24612E+03 1.26044B+02 1.43223E+01 1.57545E+01 1.03155E+00 6.621E+03 1.092E+04 1.24612E+02.1.26044E+02 1.57545E+01 1.71060E+01 1.02640E+00 6.621E+03 1.092E+04 1.24612E+02 1.26044E+02 1.71060E+01 1.06190E+01 1.006195+00 4.621E+03 1.092E+04 1.24612E+03 1.26044E+02 1.86190B+01 2.00512E+01 1.006195+00 6.621E+03 1.092E+04 1.24612E+02 1.26044E+02 2.00512E+01 2.14035E+01 1 01930E+00 6.621E+03 1.092E+04 1.26044E+02 1.274765+02 0.00000E+00 1.43223E+00 ?.117765+00 6.621E+03 1.092E+04 1.26044E+02 1.274765&02 1.43223E+00 2.06446E+00 1.46400E+00 6.621E+03 1.092E+04 1.26044E+02 1.274765+02 2.064465+00-4.296695+00 1.03256t+00 6.621E+03 1.092E.04 1.26044E+02 1.274765+02 4.296695+00 5.72092B+00 1.06900E+00 6.621E+03 1.092E+04 1.26044B+02 1.274763+02 5.72092E+00 7.16115E+00 1.075165+00 6.421E+03 1.092E+04 1.26044E+03 1.274765+02 7.16115E+00 0.59330B+00 1.068065+00 6.621E+03 1.092E+04
- 1.26044B+02 -1.2747Cd+02 0.5933 0B+00 - 1.002565+01 1.049 00B+00 6.621E+03 1.09 2E+04 1.26044E+02 1.274763+02 1.002563+01 1.14570E+01 1.04372B+00 6.621E+03 1.092E+04 1.26044E+02 1627476t+02 1.14570E+01 1.20901E+01 1.05400E+00 6.6215+03 1.092E+04 1.26044E+02 1.274765+02 1.28901E+01 1.43223E+01 1.07020E+00 6.621E+03 1.092E+04 1.26044E+02 1.274765+02 1.43223E+01 1.57545E+01 1.00733E+00 6.621E+03 1.092E+04 1.26044E+02 1.274763+02 1.57545E+01 1.710685+01 1.07010E+00 6.6215+03 1.09 2E+04 1.26044E+02 1.274765+02 1.710683+01 1.06190B+01 1.03053E+00 6.621E+03 1.09 2E+04
-1.26044E+02 1.274765+03:1.06190E+01 2.00512E+01 1.039665+00 6.621E+03 1.092E+04 1.26044E+02 1.274765+02 2.00512E+01 2.14835B+01 1.050025400 6.621E+03 1.092E+04 1.274765+02=1.20900E+02 0.00000E+00 1.43223E+00 1.160485+00 6.6215+03 1.092E+04 1.27476E+02-1.20900E+02 1.43223E+00 2.064465+00 1.112695+0014.621E+03 1.092E*04 1.274765+02 1.20900E+02 2.064463+00 4.29649E+00 1.00733E+00 6.421E+03 1.092E+04 1.274765+02 1.20900E+02 4.296695+00 5.72092E+00 1.09139E+00 6.621E+03 1.092E+04 1.27474B+02 1.20900E+02 5.72092E+00 7.16115E+00 0.00000E+00 6.621E+03 1.092E+04 1.27474E+02 1'20900E+03-7.16115E+00 8.59330E+00 1.004293+00 6.E21E+03 1.092E+04 1.27474E+02it.20900E+02 0.59330E+00.1.002563+01 1.06400E+00 6.621E+03;1.092E+04 ~
1.27474B+02 1.20900E+02 1.002565+01 1.14570B+01 1.050935*00 6.621E+03 1.0$2E+04 1.274765+02 1.209 00E+02 1.14570E+01 1.20901E+01' 1.06900E+00 6.621E+03 1.09 2E+04 1.274765+02 V.20900E+02 1.20901E+01-1.43223E+01 1.09545E+00 6.621E+03'1.092E+04 1.274785+02 1.20900E+02 1.43223E+01 1.57545E+01 0.00000E+00 6.621E+03 1.092E+04-
.1.274768+02'1.20900E+02 1.57545E+01;1.71060E+01'1.10450E+00 6.621E+03 1.092E+04 "1.274765+02:li20900E+02/1.7106tt+0141'.06190E+01:1.09240E+00 6;621E+03 1.092E+04
.- 1.274765+02 1.20900E+02 1.06190E+01 2.00512B+01-1.09951E+00 6.621E*03 1.892E+04 j 1.274765+02 1.20900E+02 2.00512E+01'2;14035E+01 1.11070E+00 6.621E+03"1~.092E+04 iwdWiggdgWngfM w&% y ~ % M Q &l Q % % W m g + ^' ,, MQg;ybv
*p qv
,p , q *.f m t e ai to
% H; s * %. w
.f
. [*#*
- w: ,, .q . . e M9Q pg q:
a e (l' - YA'
- n' S=
- L*- -
b 2{ 0' ~ t v :-E-N f k & -$ k- Nf T- ?N A YN U
s Table 2.1.2.7 Standard Core Loading Axial Power Distributions Eone Radial zone Axial huhn 1 2 3 4 0.0000E+00 0.0000E+00 0.0000E+09 0.0000E+00 0.0000E+00 1' 1.3970E+01 4 1.9360E 02 2.07475 02 1.95013 02 1.7615E 02 2 2.7301E+01 ' 2.02415 02 2.93005 02 2.04115 02 2.70025 02 3 4.0792E+01 3.5325E 02 3.6001E 02 3.54455 02 3.4601E 02 4 5.4204E+01 4.04475 02 4.07455 02 4.05225 02 4.0195E 02 4.3715E 02 4.36025 02 4.3754E 02 4.3044E 02 6 0.10265+01 4.5463E 02 4.5160E 02 4.5466E 02 4.5040E*02 7 9.44375+01 4.61115 02 4.56205 02 4.6007E*'02 4.6649E 02 0 1.0705E+02 4.60073 02 4.54995 02 4.6053E 02 4.6700E 02 9 1.21265402 4.5767E 02 4.5147E 02 4.5726E 02 4.6412E 02 10 1.34675+02 4.5307E 02 4.4770E 02 4.5332E 02 4.6035E 02 11 1.4000E+02 4.5075E 02 4.4495E 02 4.50115 02 4.5710E 02 12 1.61495+02 4.4035E 02 4.43195 02 4.47735 02 4.$4763 C2 13 1.7490E+02 4.47155 02 4.42105 02 4.46323 02 4.53613 02 14 1.0032E+02 4.46035 02 4.41923 02 4.4576E 02 4.5362E 02 15 2.0173E+02 4.46635 02 4.4109E 02 4.45423 02 4.52005 02 16 2.15'J4E+02 i 4.47075 02 .4;4250E 02 4.45655 02 4.5260E 02 17 2.2055E+02 4.4771E 02 4.43705 02 4.4630E 02 4.52465 02-le 2.41965+02 l 4.4759E 02 4.44465 02 4.46263 02 4.51465 02 19 2.55375+02 l (#4459E-02 4.42645-02 4.4340E-02 4.47205 02 '
.20 2.6070E+02-
~
4.3543E 02 4.35155 02 4.34595 02 4.3642E 02 21 ~2.02195+02 ,,, n . , .: ..;: 4p ,s,, ,- , l 4.1611E 02 _'4.1000E 02, ,4.1503E-02 4.1492E 02
-22 2.9561E+02 *
, m t + s- , %g p l, , i s_ N) ys- &L + , i bl hk ' **
Tabie2.1.2.7 Standard Core Loading Axial Power Distributions (cont'd) Eone Radial Zone Axisi Boundary 1 2 3 4 22 2.9561E402 3.83015 02 3.0710E 02 3.8329E 02 3.7878E*02 23 3.0902E+02 3.33085 02 3.39625 02 3.3340E 02 3.25295 02 24 3.2243E+02 . 2.65325 02 2.7405E.02 2.6793E*02 2.53725 02 25 3.3584E+02 1.8132E+02 1.91635 02 1.04175 02 1.6600E 02 1 26 3.49255402 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 27 3.8211E+02
- Eone Radial Radial zone Boundary 1 107.175 2 128.610 .
3 150.040 4 184.461 es ,
'p- -~', -
p y ': , p
- p L ' .l
- q. g* q gg. g g ig.3 , , ;; ,y~ , , ,
% m; j- ij . o; . _
.,. . ; g g ,. ,, .,
We A 19 , , r; .
..jja.,(1-g ,, ;., .
Table 2.1.2.8 Standard Core Loading Edit Locations alcal t(cal tidegrees).
. Thorsal Shield Copowies .
. Flum Spectrum and .
Peak Reecion Rates 203.25 121.79 20
. Pressure vessel capsules .
. Flua spectrum 215.43 121.79 20 .
. Peak Reaction Rates 215.43 '18.49 20
. Cavity Copsules .
. Plus Spectrum and .
, . Peak Reaction Rates 320.06 177.27 9.5 .
. Flumes sad DFA Estes 220.06= 177.27 0 49
. Pressure Vessel 0*Ts + .
. (A) Asial Peak Location .
e (a) 5 > 1.0 Msv 219.393 128.400 0 45 .
. (b) 5
- 0 1 MtY 219.393 125.400 0*45 .
. (c) DPA Rates 219.393 125.400 0 48 .
. (d) Flua spectrum 219.393 125.480 18.5 .
. (D) Lower Weld Locetion - 219.393 67.1040 0 45
. Pressure vessel 1/4 To .
. (A) Asial Peak Location .
. (a) ED 1.0 MEV 224.473 125.400 0 48 .
. (b) E o 0.1 Mtv 224.473 125.400 0 45 .
. (e) DPA hates 224.473 129.105 0 45
. (d) Plus spectrum 224.473
( 175.400 18.5 .
. (t) Lower Wold Locatloa 224.473 67.1040 0 45
. Pressure vessel 1/2 Ts .
. (A) Aniel Peak Locattua
. (a) s = 1.0 Mtv 239.070 125.400 0 45.
. (b) 5
- 0.1 Mtv 229.070 132.005 0 45 .
. (c) DPA Rates 229.070 132.005 0 45' .
. (d) Flua Spectrum 229.9.70 125.400 15.$ .
. (s) Lower weld Location 229.870 67.1040 0*45
. Presente Vessel 3/4 Ts .
. (A) Asial Peak Locatica .
. (a) E > 1.0 Mrv 238.260 129.188 0 45 (b) E > 0.1 Mtv 238.258 143.901 0 45 .
. (c) DFA Bates 235.260 136.583 0 45 .
. (d) Flus Spectrum 235.288 128.400 13.8 .
. (3) Lower Wold Location 235.260 67.1040 0 48 .
. Pressure Vessel outer Te .
. (A) Aalal Peak Location .
. (a) R = 1.0 MEV 240.342 140.202-. 0 45
. (b) R > 0.1 Msv 340.342 162.472 0 48 .
. (c) DFA notes 240.342 150.775 0 48
. (d) Flus Spectrum (B) Lower Weld Looetion 240.342 240.342 125.400 15.8 . . .
57.1040 0 45 . 210.50 121.79 0 48
..'Downcener K e
+ne immar wall (0 T) and vettel outer. wall (T) edits were taken at the conter of the mesh blocks hamediately inside the vessel. De vessel laternal edits were takes -
y;ppqgyy
- J t. :
' at mesh blocks centered about the required edit location. ~
n a r:wggy n ; . p , wy 9; ,
,e d a- . .
43 4
?.k . Epi 5 6i Ci .. < 0 f 9 % #
- jyh m , _
t n N @ f% WL
Table 2.1.3.1 , Low Leakage Core Loading Basic Design Data .
. Reactor . . Material .
. Thermal Power . 2527.73 MW(TN) . .. .
. Core Inlet Temp. . 536'F .
. Core Operating Pressure . 2010 psia .
. Saffle Thickness . 1.5075 cm . 85 304 .
e
. Dy Pass . .. .N02 (560 F .
. . . 2010 psia).
. Inner Radius of Core Barrel . 190.185 cm .
. Ba.rrel Thickness . 3.81 cm . SS.304 .
e
. Inner Inlet Thickness . 2.54 cm . Hg,0 ($36 F .
. . . 2010 psia).
. Luner Radius of Thermal Shield. 196.535 cm .
. Themel Shield Thickness . 3.51 cm . 88 304 .
. Outer Inlet Thickness . 10.095 cm . H2O (536'F .
. . . 2010 psia).
. Inner Radius of Liner Clad . 218.440 cm . .. .
. Vessel Liner Clad Thickness . 0.635 cm . S8 304 .
. Vessel Thickness . 21.59 cm . SA.3025 .
. tv Air Insulation Thickness . 1.835 cm . Air .
. PV Insulation Thickness . 10.16 cm . PV Insulation .
.......................q............................................
-. Cavity Thickness . 92.42 cm . Airi .
. Inner Radius of . 335.280 cm .
. Biological Shield . . .
s. Bio. Shield Lin.er Thickness s ., . 0.635 cm . SA.302m ,
< s .a.... . . .. . . ......... ..................................................,
. Bio. Shield Thickness . 213.36 cm' 1 Concreta .
?
., i g
- w( f -% Aj n ,.,f~,
_ h$ .V 4 Y ^'Y ' * '?
=n: ,
,i,~ ?ppip a tq-yjb r y ig -/ jj
- g%g 40 . 14 ' , n , , , ,
g . gg.4.; p 3n u4 -
. . , , _ . . . - . ,. 4 ., . _ _ . _ _ _ ,_ ~ .
, _ . ~ _ _ . .
f Table 2.1.3.2 Low Leakage Core Loading Core and Fuel Assemblies
. ......................................... 4.......................
. Total Number of Fuel Assemblies 204 .
. Number of Rodt per assembly (15a15) 214 fuel rode .
. O guide tubes .
. 1 instrument tube .
. Assembly Pitch 21.405 cm .
. Fin Pitch 1.43233 cm .
Fuel Material Sintered U02 Pellets .
. Cladding Material Er.4 .
. Fuel Active Length 335.20 cm .
Low Leakage Core Loading Basic Design Data a Upper and Lower Reflectors
. Lower Reflector Thickness 13.97 cm 88*304 + Water (536*F) .
. Upper Reflector Thickness 32.845 cm 88 304 + Water (504*F) .
4 I 8 i i / 1
-I 4 ', f .u 6, . ' , , . - g, __ p $_
? I. - _ -' .- L- N
'Q'
, 5
,_4 .
1 g/04 (4N 5 ~ a * * , /s4 n >. - ;
$$h didb.4fVM- ,
e j{, n e ct 7,4 p . gga a~ 4< l, , - q. -g
Table 2.1.3.3 Low Leakage Core Loading Design Specificatien Material Compositions
. Kinture Component Atos Densities .
(a tos/b
- cm) .
. N 2.425005 02 .
. 5 2.692005 05 .
. O 1.41200E*02 .
. C 2.58100E*05 .
. O (fuel) 1.28500E*02 .
. Al 3.56000E*04 .
. Core Cr 1.60800E+05 .
. Fe 2.20500E*05 .
. Mi 3.87700E*05 .
. Er 5.44800E*03 .
. 0 235 1.12000E*04 .
. U+238 6.03000E*03 .
. Pu 239 2.20000E*05 .
. Pu 240 7.12000E*06 .
. Cr 1.85300E*02 .
. Battle Mn 1.752005 03 .
. (58 304) Fe 5.807003 02 .
. Ni 8.57400E*03 .
. Dypass+ N 4.92900E*02 .
. (5 6 0* F) 0 2.46400E+02 .
. 5 4.50000E*06 .
. . Cr 1.05300E*02 .
. Core marrel Mn 1.752005 03 .
. (55 304) Fe 5.80700E*02 .
. Ni 8.574002 03 .
Inlet Watgr Gap N 5.09600E*02 .
. (536 F) 0 2.54800E*02 .
. 5 5.10000E*06 .
. Cr 1.85300E*02 .
. Thermal Shield Me 1.75200E*03 .
. (35 304) Fe 5.80700E*02 .
. Ni 8.57400E*03 .
. Cr 1.85300E*02 .
. EFV Liner Ma 1.752005 03 .
. (88*304) Fe 5.80700E*02 .
. Ni 8.5?400E*03 .
. Cavity N 3.20000E*05 .
< . (Air) O 8.000005 06 .
nhis composition is also to be used la the water region betweta the fuel 4 - assembly . . and the core baffle (see . Figurs cr 2.3.1).gm
, 3g z , gg j m , t
<i$tv. te gm M 3 +
,4 sieQws e g vs - - -
g gggy - s . -41 >. z # 3
Table 2.1.3.3 Low Leakage Care Leading Design specification Meterial Ccapositions
. Mixture component Aton Densities .
(atos/b*es) .
. C 9.84000E 04 .
. RFV Well Si 7.50500E.04 .
. (8A*3023) Mn 1.39100E 03 .
. Fe 0.18300E.02 .
. , No 3.14800E 04 .
. Cr 3.430003 04 .
. Mn 3.24000E+05 .
. EFY Fe 1.074005 03 .
. Insulation Ni 1.59000E 04 .
. A1 1.300005 04 .
- . N 3.77000E*05 .
. O 9.96000E*06 .
. C 9.840005 04 .
. Bio
- Shield Liner Si 7.38900E*04 .
. (SA 3025) Mn 1.39100E 03 .
. Fe 0.18300E 02 .
. No 3.14000E*04 .
. H 7.770003 03 .
. C 1.15000Ea04 .
- . O 4.30000E 02 .
. No 1.05000E*03 .
. Bio. Shield Mg 1.48000E 04 .
. (concrete) Al 2.39000E 03 .
. Si 1.58000E*02 .
. E 6.93000E 04 .
. Ca 1.29000E*03 .
. Fe 3.130005 04 .
. Cr 4.63250E 03 .
. Mn 4.380005 04 .
. Lower Reflector Fe 1.45175E 02 .
. (Water Steel) Ni 2.14350E*03 .
. (536*F) R 3.82200E*02 .
. O 1.91100E 02 .
. B 3.82500E 06 .
Cr 4.63250E 03 .
. Mn 4.380005 04 .
. Upper Reflector Fe 1.45175E*02 .
- . (Water. Steel) Ni ,2.14350E*03
. (5 04 *F) H 3.55303E 02 .
. O 1.77656E 02 .
. B 3.53293E*06 .
4 F 1[ _.. k Y ._
- l & ~: k ?
{l). f q' g # , T S h- .' . h' h %.h ,h } f *
- 4 A[ .hj ]- g 9 f -
"~
_ $;- 1 . ,4 s 6 i Y k hi . Y '_. ,- h % l g. + f y _ .' 6
1 Table 2.1.3A Low Leakage Core Loading Axial zone Assignments
. Zone Discription .
. 1 Lower Reflector .
. 2 Active Core Fuel Assemblies .
. 3 Upper Reflector .
. 4 Core Baffle .
. 5 By. Pass .
. 6 Core Barrel . ,
. 7 Inner Inlet Water cap .
. 8 Thermal Shield .
. 9 Outer Inlet water Oop .
. 10 Reactor Pressure Vessel Linar .
. 11 Reactor Pressure Vessel .
. 12 Air cap .
. 13 Pressure Vessel Insulation .
. 14 Cavity .
. 15 Biological Shield Liner .
. 16 Biological Shield .
4 T 'c *; k AJ ,% ( (
, i ' t - r ' i jj +
s d ~ 3 3 - 2 ,5 b h
'J 4 i y ' k M '-M , r f b ,. .4 f
a
sg w 9. u. < 3
?: N,
#m .. ~ _ . -
ge' '
.' . Table 2.1.3.5 s w . .
S - % h'
, p :
L y i
~
; 4 Ier id"Ja Core T M My f1 y F- '
Fuel Assembly Geometry, Power, and Burng Distre hHcuss . j o Relative BOC Buraq EOC Burney Axial Pin Assembly Dem ) Opc ) Peaking Power
. naammhly' muuher - X-Inft ~ X-Eight T-Bot T-Top Power Factor Set 1 .0.00000E+00 "2.14850E+01 0.00000E+00 2.14850E+01 1.08800E+00 1.63043E+04 2.44443E+04 1.0000 0 1.0000 0 2 2.14850E+01 ~ 4.29700E+01 0.00000E+00 2.14850E+01 1.19500E+00 1.63043E+04 2.44443E+04 1.0000 0 3 4.29700E+01 '6.44550E+01 0.00000E+00 2.14850E+01 1.23700E+00 1.63043E+04 2.44443E+04 1.0000 0 4 6.44550E+01S.59400E+01 0.00000E+00 2.14850E+01 1.13200E+00 1.63043E+04 2.44443E+04 1.0000 0 5 S.59400E+01' 1.0742SE+02 0.00000E+00' 2.14850E+01 1.25100E+00 1.63043E+04 2.44443E+04 1.0000 13 6 1.07425E+02 0.00000E+00 0.00000E+00 0.00000E+00 1.28000E+00 1.50810E+04 2.71080E+04 1.0000 14
~1 1.28910E+02 0.00000E+00 0.00000E+00 0.00000E+00 1.22700E+00 0.00000E+00 1.14300E+04 1.0000 15 S 1.50399E+02 0.00000E+00 0.00000E+00 0.00000E+00 3.51000E-01 3.44510E+04 3.78570E+04 1.0000 0 9 2.14850E+01' 4.29700E+01 2.14850E+01 4.29700E+01 1.20900E+00 1.63043E+04 2.44443E+04 1.0000 0 10 4.29700E+01"'G.44550E+01 2.14850E+01 4.29700E+01 1.04000E+00 1.63043E+04 2.44443E+04 11, 6.44550E+01 S.59400E+01 2.14850E+01 4.29700E+01 1.29100E+00 1.63043E+04 2.44443E+04 1.0000 0
' 1.0000 0 12 8.59400E+01- 1.0742SE+02 2.14850E+01 4.29700E+01 1.06600E+00 1.63043E+04 2.44443E+04 '1.0000 10 13 1.07425E+02 0.00000E+00 2.14850E+01 0.00000E+00 1.31300E+00 0.00000E+00 1.22710E+04 1.0000 11 i 14 1.28910E+02 0.00000E+00 2.14850E+01 0.00000E+00 1.22200E+00 7.56600E+03 1.90260E+04 1.0000 12
_ 15 1.50399E+02 0.00000E+00 2.14850E+01 0.00000E+00 4.47000E-01 2.67040E+04 3.20300E+04 1.0000 0
. 116 4.29700E+01 6.44550E+01 4.2970CE+01 6.44550E+01 1.04900E+00 1.6304 3E+04 2.44443E+04 1.0000 0 17 6.44550E+01 S.59400E+01 4.29700E+01 6.44550E+01 1.10200E+00 1.63043E+04 2.44443E+04
~
1.0000 0
. 18 S.59400E+01 1.07425E+02 4.29700E+01 6.44550E+01 1.29200E+00 1.63043E+04 2.44443E+04 1.0000 7 19 1.07425E+02 0.00000E+00 4.29700E+01- 0.00000~+00 ,1.38500E+00 9.28750E+03 2.22845E+04 1.0000 8 2: 20 1.28910E+02. 0.00000E+00 4.29700E+01 0.00000E+00 1.06300E+00 0.00000E+00 9.90600E+03 1.0000 9
' I -
21 1.50399E+02 0.00000E+00 4.29700E+01 0.00000E+00 3.55000E-01 2.58990E+44 2.93340E+04 1.0000 0
'22 6.44550E+01' S.59400E+01 6.44550E+01 S.59400E+01 1.24000E+00 1.63043E+04 2.44443E+04 1.0000 4
/ '23 8.59400E+01~' O.00000E+00 6.44550E+01 0.00000E+00 1.27100E+00 1.10260E+04 2.29480E+04 1.0000 5
!. ,, 24 1.07425E+02 0.00000E+00 6.44E50E+01 0.00000E+00 1.13200E+00 0.00000E+00 1.05460E+04 1.0000 6
;A 25 1.28910E+02 0.00000E+00 6.44550E+01 0.00000E+00 5.25000E-01 2.64120E+04 3.13230E+04 -1.0000 1
% 26 8.59400E+01' 'O.00000E*00 8.59400E+01 0.00000E+00 7.72000E-01 2.68580E+04 3.40760E+04 1.0000 2, "M 27 -1.07425E+02_ 0.00000E+00 S.59400E+01 0.00000E+00 4 ."J 6000 E- 01 2.60160E+04 3.06280E+04 1.0000 3
- A 28 1.28910E+02 0.00000E+00 S.59400E+01 0.00000E+00 1.69000E-01 3.52640E+04 3.68980E+04 e y pace: Assemblies' including pin powe'r sets do not have right or top boundaries specified taere. these data are included with the pin
- r ,
pmometry data. L. T 1
.jQ , m
, m
.s .
r ** m. N
.. t Y'
- e '*
v M
Table 2.1.3.6 t
-Low Leakage Core Loading Pia Geometry, Power, and Burnup Distributions Assembly 6 Pin Power set 13 Relative 500 EOC Fin Burnup Durnup E+Left E Eight T+ Bet Y Top Power (MWD ) (NWD )
1.G /425B+02 1.000573+02 0.00000E+00 1.43223E+00 1.02603E+00 1.500E+04 2.711E+04 1.07425E+02 1.000573+02 1.43223E+00 2.064465+00 1.00624E+00'1.500E+04 2.711E+04 1.07425E+02 1.080573+03 2.064465+00 4.296695+00 9.737025 01 1.500E+04 2.7115+04 1.074285+02 1.000673+03 4.296698+00 5.72092E+00 9.63490E+01 1.500E+04 2.711E+04 1s07425E+02 1.000573+02 5.72092E+00_7s16115E+00 0.00000E+00 1.500B+04 3.7115+04 1.07425E+02 1.000573+02 7.16115E+00 0.593385+00 9.413235+01 1.500E+04 2.711E+04 , 1.074285+02 1.000575+02 0.59330E+00 1.002565+01 9.339065 01 1.500E+04 2.711E+04 1.07425E+02 1.000575+02 1.002565+01 1.14570E+01 9.103645*01 1.500E+04 2.711E+04 1.07425E+02-1.000575+03 1.14570E+01 1.20901E+01 9;183645 01 1.500E+04 2.7411E+04 1.07425E+02 1.000575+02 1.209015+01 1.43223E+01 9.294405 01 1.500E+04 2.711E+04 1.07435B+02 1.000573+02 1.43223E+01 1.57545E+01 0.00000E+00 1.508E+04 2.711E+04
, 1.07425E+02 1.000573+02 1.57545E+01 1.71060E+01 9.310313 01 1.500E+04 2.711E+04 1.07425E+02 1.000573+02 1.71060E+01.1.06190E+01 9.19947E*01 1.500E+04 2.711E+04 1.07425E+02 1.000575+02 1.06190E+01 2.00512E+01 9.144065 01 1.500E+04 2.7115+04 1.07425E+02 1.000575+02 2.00512E+01 2.14035E+01 0.764043 01 1.500E+04 2.711E+04 1.00057E+02 1.102095+02 0.00000E+00 1.43223E+00 1.007793+00 1.500E+04 2.711E+04 1.000573+02 1=.102095+02 1.43223E+00 2'064465+00 1.02603E+00 1.500E+04 2.711E+04 1.000573+02 1.102093+02 2.064465+00 4.296695+00 9.91200E 01 1.500E+04 2.711E+04 1.000573+02 1.102093+02 4.296695+00 5.72092EiOO 1.02524E+00 1.500E+04 2.711E+04 1.000575+02 1.102095+02 5.72092E+00 7.16115E+00 1.00062R+00 1.500E+04 2.711E+04 1.008575+02 1.102893+02 7.14115E+00 0.59330E+00 9.943675 01 1.500E+04 2.7113+04 1.000575+02 1.102095+02 0.59330E+00 1.00256E+01 9.000335 01 1.500E+04 2.711E+04 1.000575+02 1.102095+02_1.002565+01 1.14570E+01_9.072415 01 1.500E+04 2.711E+04 1.000575+02 1.102095+03 1.14570E+01 1.20901E+01
- 9.824915 01 1.500E+04 2.711E+04 1.009575+02 1.102093+02 1.20901E+01 1.43223E'+01 9.04075E*01 1.500E+04 2.711E+04 1.000573+02 1.102095+02 1.43223E+01 1.57545E+01 9.904005 01 1.500E+04 2.711E+04 1.000575+02 1.102893+02 1.57545E+01 1.71060E+01 9.943675 01 1.500E+04 2.711E+04
.1.000575+02 1.102095+02 1.71060E+01 1.06190E+01 9.413235 01 1.500E+04 2.7115+04
- 1.000573+02 1.102095+02 1.96190E+01 2.00512E+01 9.365735 01 1.500E+04 2.711E+04 1.000575+02 1.102095+02 2.00512E+01 2.14035E+01 9.262015 01 1.5065+04 2.711E+04 1.102895+02 1.11722E+02 0.00000E+00 1.43223E+00 1.099665+00 1.500E+04 2.711E+04 11.102093+03.1.11722E+02.1.43223E+00 2.064465+00 1.03553E+00 1.500E+04 2.711E+04 1.102095+02 1.11722E+02 2.064465+00 4.296695+00 6.601095 0111.5095+04'2s711E+04 1.103093+02 1.11722E+02 4.29669E+00 5.72092E+00 1.01091E+00 1.500E+04 2.711E+04
-1.102893+03-1.11722E+02 5.72092E+00 7.16115E+00 9.91783E+01 1.500E+04 2.711E+04
,,7 1.102098+02(1.11722E+02,7.16115E+00 0.593385+00 9.016998 01 1.5085+04 2.711E*04 1'.102098+02 1.11722E+02 0.593385+00 1.002565+01 9.056505 01' 1.500E+0412' 711E+04 -
tiki 4 11 1'.192093+02)1.11722E+02 1.002565+01!1.14570E+01g6.270135 01tl.500E+04,2.7115+04 ~ 1.102895+02'1.11722E+03 1.14570E+01 1.20901E+01~ 9.016995 01 /1'.500E+04' 2;111E+04 ' 1.102093+02 1.11722E+02 1.28901E+01 -1.43223E+01- 9.729915 01 1.500E+04 2.711E+04 1'.102093+02 1.11722E+02 1.43223E+01 1.57545E+01 9.769495 01 1.500E+04 - 2.711E+04 1.102895+02 1.11722E+02 1.57545E+01 1.71060E+01 9.91200E 01 1.500E+04 2.711E+04 1.102893+0221;11722E+02 1.71860E+01 1.06190E+01 6.40400E*01.1.500E+04 2.711E+04 4 jpgSi 1~.102993+02)1'.11722E+02 1.06190E+01_2 00512E+01 9.49240E*01.1.500E+04 2.711E+04 1 i e' MNmm.192493+02 % ? 1'.11722E+0212.00512E+01 gm. , ,g . mm - 2 414835E+01* 9 ;3094tE OI!1iS0 4*%yggny . w n x,, ,
, m4 ,;pgggggg p 4 g ,g g g g_
wM go . p- . 9%wQg : me - 4mymgg ggypp
l l Table 2.1.3.6 Low Leakage Core Loauang Pin Geometry, Power, and Burnup Distributions (cont'd) Assembly 6 Fin Power Spt 13 Relative ROC EOC Pin turnup Eurnup I*Left X Right Y* Dot Y' Top Power (MWD ) (MWD ) 1.16018E+02 1.17451E+02 0.00000E+00 1.43223E+00 1.09729E+00 1.508E+04 2.711E+04 1.16018E+02 1.17451E+02 1.43223E+00 2.86446E+00 1.08304E+00 1.500E+04 2.711E+04 1.16018E+02 1.17451E+02 2.8644GE+00 4.29669E+00 1.03158E+00 1.508E+04 2.711E+04 1.16018E+02 1.17451E+J2 4.29669E+00 5.72892E+00 9.95158E*01 1.500E+04 2.711E+04 1.16018E+02 1.17451E+02 5.72892E+00 7.16115E+00 9.72991E+01 3.508E+04 2.711E+04 1.160185+02 1.17451E+02 7.16115E+00 0.593385+00 9.690325 01 1.F00E+04 2. /11E+04 1.160185+02 1.17451E+02 8.55330E+00 1.002565+01 9.79324E*01 1.500E+04 2.711E+04 1.16018E+02 1.17451E+02 1.00256E+01 1.145785+01 9.87241E*01 1.5085+04 2.711E+04 1.160185+02 1.17451E+02 1.1457 8E+01 1.289 01E+01 9.769 49 E
- 01 1.500E+04 2.711E+04 - ,
1.16018E+02 1.17451E+02 1.28901E+01 1.43223E+01 9.64282E 01 1.508E+04 2.711E+04 1.16018E+02 1.17451E+02 1.43223E+01 1.57545E+01 9.63490E*01 1.500E+04 ?.711E+04 1.160182+02 1.17452E+02 1.57545E+01 1.71868E+01 9.76949E 01 1.508E+04 2.711E+04 1.16018E+02 1.17451E+02 1.71868E+01 1.86190E+01 9.94367E*01 1.508E+04 2.711E+04 1.16016:+02 1.17451E+02 1.86190E+01 2.00512E+01 1.00545E400 1.508E+04 2.711E+04 1.16018E+02 1.17451E+02 2.00512E+01 2.14835E+01 9.54782E*01 1.500E+04 2.711E+04 1.17451E+02 1.19803E+02 0.00000E+00 1.43223E+00 1.09570E+00 1.508E+04 2.711E+04 1.17451E+02 1.19883E+02 1.43223E+00 2.06446R+00 1.08620E+00 1.506E+04 2.711E+04 , 1.17451E+02 1.19803E+02 2.864+6E+00 4.29669E+00 6.56314E 01 1.508E+04 2.711E+04 \ 1.17451E+02 1.18883E+02 4.19669E+00 5.72892E+00 1.00149E+00 1.b083+04 2.711E+04 1.17451E+02 1.18883E+02 5.72892E+00 7.16115E+00 9.76158E* 01 1.508t+04 2.711E+04 1.17451E+02 1.19883E+02 7.16115E+00 0.59338E+00 9.72991E*01 1.508M+04 2.711Et04 1.17451E+12 1.18883E+02 0.593385+00 1.00256E+01 9.89 616E 01 1.508E+04 2.711E+04 1.17451E+02 1.7.8883E+02 1.00256E+01 1.14578E+01 0.00000E+00 1.508E+04 2.711E+04 1.17451E+02 1.18883E+02 1.14578E+01 1.28901E+01 9.98033E*01 1.508E+04 2.711E+04 1.17451E+02 1.18883E+02 1.289 01E+01 1.43223E501 9.69 032E 01 1.500E+04 2.711E+04 1.17451E+02 1.18883E+02 1.43223E+01 3.57545E+01 9.67449E* 01 1.500E+04 2.711E+04 3.17451E+02 1.18883E+02 1.57545E+01 1.71868E+01 9.84075E 01 1.500E+04 2.731E+04 1.17451E+02 1.18883E+02 1.7186BE+01 1.86190E+01 6.26521E*01 1.508E+04 2.711E+04 1.17451E+02 1.18883E+02 1.86190E+01 2.00512E+01 1.01099E+00 1.500E+04 2.711E+04 1.17451E+02 1.18883E+02 2.00512E+01 2.14835E+01 9.55574E*01 1.508E+04 2.711E+04 1.18883E+02 1.20315E+02 0.00000E+00 1.43223E+00 1.09966E+00 *.408E+04 2.711E+04 1.18883E+02 1.20315E+02 1.43223E+00 2.86446E+00 1.08541E+00 1.508E+04 2.711E+04 1.19883E+02 1.20315E+02 2.86446E+00 4.29 669E+00 1.034'r4r+00 1.500E+04 2.711E+04 1.18883E+02 1.20315E+02 4.29669E+00 5.72892E+00 9.97533E 01 1.508E+04 2.711E+04 1.18883E+02 1.20315E+02 5.72892E+00 7.16115E+00 9.7536(E*01 1.508E404 2.111E.04 1".18883E+02 1.20315E+02 7.16115E+00 8.59338E+00 9.72199E+01 1.5065+04 2.711E+04 1=.19803E+02 1.20115E+02-8.59330E+00 1.00256E+01 9.82491E-01 1.500E+04 2.711E+04 1.18883E+02(1.20315E+02 1.00256E+01.1.14578E+01 9.90408E*01.1.508E+04 2.711E+04
' 1.19 8 0 3 E+02' 1. 20315E+02 1".14 57 8E+01 1.199 01E+01' 9. 809 08E+ 01 '1. 5085+04' 2.711E+ 04 1.18883E+02 1.20315E+02 1.28901E+01 1.43223E+01 9.68241E 01 1.508E+04 2.711E+04 1.18883E+02 1.20315E+02 1.43223E+01 1.57545E+01.9.68241E.01 1.500E+04 2.711E+04 1.18883E+02 1.20315E+02-l'.57545E+01 1.71868E+01 9.80908E 01 1.500E+04 2.711E+04 1.19883E+02 1.20315Et02 1.71868E+01 1.86190E*01 9.99908E+01 1.500r,04-2.711E+04 1.18883E+02 1.20315E+02 1.86190E+01 2.00512E+01 1.01099E+00 1.508t+04 2.7112+04
~ "
~
" 'P11188L1t+02? 1.20315E+02 ' 2.00512E+01 2.1483 5E+01 9.60324E* 01 1.508E+04 2.711E+04
, ;ri m + ilta m .
j , I
'- !NAti- s .,f , 4 4* Ag, W,
+$$> ] l _ l' k$Nh.b; a , <
wh s ; 4 m pe.WgWqgb@ ,. - o
1 l Table 2.1.3.6 Low Leakage Core Loading Pin Geometry, Power, and Burnup Distributions (cont'd)
- Assembly 6 Pin Power set 13 Belative DOC EOC I
Pin surnup turnup I.Left E. Bight Y. Bot Y. Top Power (Nwn ) (Nwn ) 1.11733E+03 1.13154B+03 0.00000E+00 1.43223E+00 1.11075E+00 1.500E+04 2.711E+04 t 1.11723E+03 1.13154E+02 1.43223E+00 2.064465+00 1.09 0075+00 1.500E+04 2.711E+04 1.11723E+02 1.13154E+02 2.06446E+00 4.39669E+00 1.04345B+00 1.500E+04 2.711E+04 1.11733E+03 1.13154E+02 4.396693+00 5.72092E+00 1.003073+00 1.500E+04 2.711E+04 ' 1.117383+03 1.13154E+03 5.73093E+00 7.16115E+00 9.001185 01-1.500E+04 3.711E+04 1 1.117385+03 1.13154E+03 7.16115B+00 0.09330B+00 9'.706163.C1 1.500E+04 2.711E+04 1.11733E+03 1.13154E+03 0.59330Be00 1.00256E+01 9.729915 01 1.500E+04 2.711E+04 1.11723E+03 1.13154E+03 1.002563+01 1.14570E+01 9.76150E*01 1.560E+04 2.711E*04 1.11723E+03 1.13154B+03 1.14570B+01 1.30901E+01 9.690245 01 1.500E+04 2.711E+04 1.11723E+03 1.13154E+03 1.20901E+01 1.43223F+01 ,9.63490E.01 1.500E+04 2.711E+04 1.11723E+03 1.13154B+02 1.43223E+01 1.57545E+01 9.6f6573 01 1.500E+04 2.7111+04 3.11722E+02 1.13154E+02 1.57545k+01 1.71060k+01 9.793245 01 1.500E+04 2.711E+04 1.117225,03 1.13154B+02 1.71060E+01 1.06190E+01 9.967425 01 1.500E+04 2.711E+04 i 1.11722E+03 1.13154E+02 1.06190E+01 2.00512E+01 1.00703E+00 1.500E+04 2.711E+04 1.11722E+02 1.13154B+03 2.00512E+01 2.14035E+01 9.547025 01 1.500E+04 2.711E+04 1 13154E+03 1.145065+02 0.00000E+00 1.43223E+00 0.00000E+00 1.500E+04 2.711E+04 1.13154E+02 1.145065+02 1.43223E+00 2.06446E+00 1.09491E+00 1.5003404 2.711E+04 1.13154E+02 1.145065+03 - 2.064465+00 4.296695+00 1.02920E+00 1.500E+04 2.711E+04 1.13154E+03 1.145065+03 4.296693+00 5.72092E+00 9.919913 01 1.500E+04 2.711E+04 1.13154B+03 1.145065+02 5.72092E+00 7.16115B+00 9.721992 01 1.500E+04 2.711E+04 1.13154E+02 1.145065+02 7.16115E+00 0.59330E+00 9.642023 01 1.500E+04 2.711E+04 1.13154E+03 1.34304E+02 0.59330E+00 1.002565+01 9.62699E.01 1.500E+04 2.711E+04 1.13154E+02 1.145065+02 1.00254E+01 1.14570E+01 9.42699E 01 1.500E+04 2.711E+04
=1.13154E+02 1.145965+02 1.145795+01 1.20901E+01 9.603243 01 1.500E+04 2.711E+04 1.13154E+02 1.145363+02 1.20901B+01 1.43223N&01 9.579495 01 1.500E+04 2.711E+06 1.13154E+03 1.1450$E+02 1.43223E+01 1.57545E+01 9.f 0324K.01' 1.500E+04 2.711E+04 1.13154E+02 1.145065+02 1.57545E+01 1.71060E+01 9.6902'43 01 1.500E+04 2.711E+04 1.13154E+02 1.145065+02 1.71060E+01 1.06190E+01 9.056505 01 1.500E+04 2.711E+04 1.13154E+02 1.145065+02 1.0(190E+01 3.00512E+01 1.00703R+00 1~500E+04 2.711E+04 .
1.13154E+02 1.145065+02 2.00512E+01 2.14035E+01 0.00000E+00 1.500E+04 2.711E+04 1.14504E+03 1.11010E+02 0.00000E+00 1.43223E+00 1.10750E+00 1.500E+04 2.711E+04 , 1.11506E+02 1'.16010B+02 1.432235,00 2.06444B+00 1.00620E+00 1.500E+04 2.711E+04 1.145065+02 1.16010E+02 2.064463+00 4.296693+00 1.0344CM+00-1.500E+04 2.711E+04 ; 1.145065+02 1.16010B+02 4.296695+00 5.72092E+00 9.000253 91 1.500E+04 2.711E+04 1,14506E+02 1.16010E+02 5.72092E+00 7.16115E+00 9.706165 01 1.500E+04 2.711E+04 1.145065+01 1.16010E+02 7.16115E+00 0 59330E+00 9.642025.C1 1.f90E+04.3.711E+04 3 i 1'.145063402 1.16010E+03 0.59330E+00:1;00356E+01 9~65074EkO1'1.500E+04'?.711E+04 . l
' : 14145063,03 ; 1.16010E+98 t t . 003565+ 01 + 1.14570E+0119 . 66657E
- 01i 11500E +0413 !?11E+ 04 -
, ? j' 1".145663+03 1.14010E+03 1.14570F+01 1.199015+01 9.626993 01=1.50sB+04'2.711E+04- <
>1.145365+02!1.16010E+02 1.209015+01 1.43223E+01 9.50740E.01 1.500E+04 2.711Ee04 11.14506E+32 1.16010E+02 1.43223E+01 1.57545E+01 9.603245 0111.500E+04 2.711E+04 3 .
1.14506E+02 1.160185+02.1.57545B+01 1.71060E+01 9.690325 01;1.500E+04 12.711E+04 1.145065+02 '1.160103403 '1.71060E+01'1.0619 0E+01 9.040665 01 1.500E+0412.711E+04 - i
' 1.145065+02-1.16010B+02 1.061f0E+01,2.00512E+0111'.004665+00;1'.5005404:3.711E+04'
^
M 12145065+03 L.160103403 3.00513B+01ta;14035540119.619075 0131'.500E+04.3.7115404 gmnMW/ W o;a^ w < W W W W k W Y^ W W W * * " IF- x t .. W b5 ' f , mus@4M m e m W W W w & V W W W 6 W N " W M * *
- N ",.
- _ _ _ _ _ __ _ .__._.___._m___._____ _ _ _ ._ _
o Table 2,1,3.6 Low Leakage Corn Loading Pin CapWAry, Power, and turnup Distributions (cont'd) Assembly 6 Pin Power Set 13 Relativi BOC IOC Ptn Burnup Burnup 2+Left X Right Y. Bot Y Yop i Power (MWD ) (MWD ) 1.20315Ee02 1.217473+02 0.00000E+00 1.43223E+00 1.11312E+00 1.50SE+04 2.711E+04 1.20315E+02 1.21747E+02 1.43223E+00 2.86446E+00 1.09254E+00 1.500E+04 2.711E+04 1.20315E+02 1.217473+02 2.86446E+00 4.296695+00 1.03078E+00 1.500E+04 2.711E+04 1.20315E+02 1.217475+02 4.296698+00 5.72892E+00 9.95158E*01 1.500E+04 2.711E+04 ' 1.20T.4E+0J.1.217475+02 5.72092E+00 7.16115E+00 9.76949E*01 1.800E+04 2.711E+04 1.20315E+02 1.217475+02 7.16115E+00 8.59330E+00 9.706165+01 1.500E+04 2.711E+04 1.20315E+02 1.217475+02 f.593385+30 1.00256E+01 9.721995 01 1.500F+04 2.711E+04 1.20315E+02 1.217475+02 1.00256E+01 1.145785+01 9.74574E 01 1.500E+04 2.711E+04 1.20315E+02 1.217475+02 1.145785+01 1.20901E+01 9.71407E*01 1.500E+04 2.711E+04 1.00315E+02 1.217475+02 1.20901E+01 1.43223E+01 9.57449E*01 1.500E+04 2.711E+04 1.20315E+02 1.217475+02 1.43223E+01 1.57545E+01 9.69824E.01 1.500E+04 2.711E+04
, 1.20315E+02 1.217473+02 1.57545E+01 1.71860E+01 9.79324E+01 1.500E+04 2.711E+04 1.20315E+02 1.217475+0? 1.71868E+01 1.861905+01 9.95950E+01 1.500E+04 2.711E+04 1.20315E+02 1.21747E.02 1.56190E+01 2.00512E+01 1.01733E+00 1.500E+04 2.711E*04 1.20315E+02 1.21747E+02 1.00512E+01 2.14835E+01 9.74574E 01 1.508E+04 2.711E+04 1.21747E+02 1.23180E+02 0.000C0E+00 1.43223E+00 0.00000E+00 1.508E+04 2.711E+04 1.21747E+02 1.23180E+02 1.43223E+00 2.86446E+00 1.10679E+00 1.C00E+04 2.711E+04 1.21747E+02 1.23180E+02 2.06446E+00 4.29669E+00 1.04108E+00 1.508E+04 2.711E+04 1.21747E+02 1.23180E+02 4.29669E+00 5.72892E+00 1.003875+00 1.50$E+04 2.711E+04 1.21747E+02 1.23180E+02 5.72092E+00 7.16115E+00 9.04066E 01 1.509E+04 2.711E+04 1.21747E+02 1.23100E+0) 7.16115E+00 8.59330E+00 9.77741E+01 1.500E+04 2.711E+04 1.21747E+02 1.23100E+02 8.59338E+00 1.00256E+01 9.76949E*01 1.508E+04 2.711E+04 1.217&7E+02 1.23180E+02 1.00256E+01 1.14578F+01 9.777415 01 1.508E+04 2.711E404 1.21747E+02 1.23180E+02 1.14570E+01 1.28901E+01 '
9.75366E 01 1.500E+04 2.711E+04 1.217475+02 1.23100E+02 1.28901E+01 1.43223E+01 9.74574E 01 1.508E+04 2.711E+04 1.21747E+02 1.23180k+02 1.43223E+01 1.57545E+01 9.77741E 01 1.508E+04 2.711E+04 1.2174"E+02 1.22100E+02 1.57545E+01 1.71068E+01 9.00825E 01 1.500E+04 2.711E+04 1.217475+02 1.23390E+02 1.71868E+01 1.56190E+01 1.00624E+00 1.5085+04 ?.711E+04 1.21747E+02 1.731005+02 1.86190E+01 2.00512E+01 1.02999E+00 1.500E+04 2.711E+04 1.21747E+02 1.23180E+02 2.00512E+01 2.14035E+01 0.00000E+00 1.500E+04 2."11E+04 1.1J180E+02 1.24612E+02 0.00000E+00 1.43223E+00 1.13133E+00 1.500E+04 2.711E+04 1.23180E+02 1.24612E+02 1.43223E+00 2.86446E+00 1.12183E+00 1.500E*04 2.711E+04 1.23180E+02 1.24612E+02 2.864460+00 4.29669E+00 1.0s799E+00 1.500E+04 2.711E+04 1.23180E+02 1.24612E+02 4.29669E+00 5.72092E+00 1.02920E+00 1.500E+04 2.711E+04 1.23180E+02 1.24612E+02 5.72892E+00 7.16115E+00 1.00545E+00 1.500E+04 2.711E+04 1.23180E+02 1.24612E+02 7.16115E+00 8.5933OE+00 9.96742E.01 1.500E+04 2.711E+04 1.23100E+02 1.24612E+02 8.59338E400.1.00256E+01_9.99900E*01 1.500E+04 2.711E+04 1.23100E+02 1.24612E+01 1.00256E+01 1.145702401 1.00387E+00 1.508E+04 2.711E+04
'1'.231004+02 1.24612E+02 1.145785+01-1.28901E+01 9'98325E+01 1;500E+04:3.711Eo04 1.231COE+02 1.24612E+02 3.28901E+01 1.43223E+01 9.93575E 01-1.508t+04 2.711E+04 1.23180E+02 1.24612E+02 1.43223E+01 1.57545E+01 9.983253 01 1.500E+04 2.711E+04
-1.23180E+02 1.24612E+02 1.57545E+01 1.71860E+01 1.013372+00 1.500E+04 2.711E+04 1.23100E+02 1.24612E+02 1.71860E+01 1.86190E+01.1.03237E+00_1.500E+04 2.711E+04
-1.23180E+02 1.24612E+02 1.86190E+01 2.00512E+01 1.04424E+00 1.500E+04 2.711E+04
< 1.23100E+02 1.24612E+02 2.00512E+01 2.14835E+01 9.896165 01 1.508E+04 2.711E+04
% 4 aw a ; m N .< , . 7 gg,ee e 2 je W g ,
. ,a
%- h t _
, pQ
- 1F t#94+pswr WM A .sw , 4 , - ,,q:
Jmg gqgwqhygpgggg4 s,
.- - -_- .. - - _ _ _ - - - - - _ _ _ _ - - - = - - - - . - - -
Table 2.1.3.6 i Low Leakage Core LoadinE Pin Geometry, Power, and Burnup Distributions (cont'd) Assembly 6 Fin Power Set 13 Belative DOC EOC , Pin Burnup Surnup E+Left I+Eight Y Bot Y Top Power (pen) ) Nwp ) l 1.24612B+02-1.26044B+02 0.00000E+00 1.43223E+00 1.14003E+00 1.500E+04 2.711E+04 ' 1.24612E+03 1.26044B+02 1.43223B+00 2.064463+00 1.07900E+00 1.500E+04 2.711E+04 1.24613E+02.1.26044E+03 2.064465+00 4.296693+00 6.96690E*01 1.500E+04 2.711E+04 , 1.34613E+03 1.26044E+03 4.294695+00 5.72092E+00 1.06950E+00 1.500E+04 3.711E+04 i 1.34613E+03 1.26044E+03 5.73493B+00 7.14115E+00 1.04434E+00 1.500E+04 2.7115+04 1.24612E+03 1.36044E+03 7.161185+00 0.59330E+00 1.03474B+00 1.500E+04 2.711E+04 1.24612E+03 1.26044E+03 0.59330E+00 1.002563+01 1.039495+00 1.500E+04 2.711E+04 ; 1.24613E+03 1.26044E+01 1.00J865+01 1.14570B+01 6.59400E+01 1.500E+04 2.711E+04 1.24612E+03 1.26044E+03 1.14570B+01 1.209015+01 1.037915+00 1.500E+04 2.711E+04 1.24612E+02 1.26044E+03 1.20901E+01 1.43223E+01 1.03150R+00 1.500E+04 2.711E+04 1.24612E+02 1.26044B+02 1.43223E+01 1.57545E+01 1.03712E+00 1.500E+04 2.711E+04
, 1.24612E+02 1.26044E+02 1.57545E+01 1.71060B+01 1.05374E+00 1.50 E+04 2.711E+04 1.24612B+02 1.260448402 1.71060E+01 1.06190E+01 6.760905 01 1.500E+04 2.711E+04 '
1.24612E+02-1.26044E+03 1.06190B+01 2.00512E+01 1.000(2E+00 1.500E+04 2.7115+04 1.24611E+03 1.26044B+02 2.00512E+01 2.14035E+01 9.975333 01 1.5003+04 2.711E+04 1.26044E+02 1.27476E+02 0.00000E+00 1.43223E+00 1.17012B+00 1.500E+04 2.711E+04 1.26044E+02 7.174765+02 1.43223E+00 2.264465+00 1.11312E+00 1.506E+04 2.711E+04 1.26044E+03 1.274765+02 2.064465+00 4.296?!&+40 1.00304E+00 1.500E+04 2.7115,04 1.26044E+02 1.27474E+02 4.296698+00 5.72094E+00 1.127375+00 1.500E+04 2.711E+04 1.26044E+02 1.274763+02 5.72092E+00 7.16115E+00.1.11391E+00 1.500E+04 2.711E+04
- 1.26044E+02 1.27476E+02 7.16115E+00 0.59330E+00 1.10045E+00 1.500E+04 2.711E+04 1.26044E+02 1.274765+02 0.59330B+00 1.00256E+01'1.09412E+00 1.500E+04 2.711E+04 1.26044E+02 1.274765+02-1.002565+31 A.145704+01 1.09570E+00 1.500E+04 2.711E+04
- 1.26044E+02 1.274765+02 1.14570E+01 1.20901E+01 1.09254E+00 1.500E+04 2.711E+04 1.26044E+02 1.374763+03 1.209 01E+01 1. 63223 3301 1.09 6495+00 1.500E+04 ' 2.711E+04 1.26044E+02 1.374765+03 1.43223E+01 1.57545E+01 1.10600E+00 1.500E+04~2.711E404 '
1.26044B+02 1.274765+03 1.575459401 1.71060E+01 1.11075E+00 1.500E+04 2.711&+04 1.26044E+02 1.274765+02-1.71040&+01 1.06190E+01 1004020E+00 1.500E+04 2.711E+04' 1.26044E+02 1.274765+02 1.06190E+01 2.00512E+01 1.041015+00 1.500E+04 2.7J1E+04
~1.26044B+02 1.274763+02 2.00512E+01 2.14035E+01 1.02762E+00 1.500E+04 2.711E+04 1.274765+02 1.20900E+02 0.00000F+00 1 43223E+00 9 1.17646E+00 1.500E+04 2.711E+04 1.274765+03 ' 1.30900E+03 1.43223E+00 2.06444E+00 1.176465+00 1.500E+04 2.711E+04.
1.274765+03 1.209093+02 2.064463+00 4.296693+00 1.15033E+00 1.500E+04 2.711E+04 1.274765+03.1.24900E+02 4.296695+00 4.72092E+00 1.14162E+00 1.500E+04 2.711E+04 i 1.374765+02'1'.20900E+03 5.73092E+00 7.16115E+00 0.00000E+00-1.500E+04 2.7115+04 4 '
- 1i '4763+03 1. 30900E+03 + 7.1411SE+00 s S 480958Se90 t 1518840E*00 ct1990E*4413 s 711E+04 >
te <r1.374765+0311.30900E+02,0.59330E+00
'g ' "
1.003563+01'1.11313E+00 1.500E+04 2.7115+04 1; 374765+03 : 1'. 309003+03 ' 1; 002865401 - 1.14570E+01' 1'.110753400 ~- 1.500E+04 : 3 J113404 1.27474E+02 1.20900E+02 1.14570E+01'1.20901E+01 1.11233E+00 1.500E+04 2.711E+04
- 1.274765+02 1.20900E+02 1.209 01E+0111.43223B+01 1.12104E+00 1.500E+04 2.711E+04
=
1.274763+03.1.20900E+02 ' 1.43223E+01' 1.575455+01 0.00000E+00 -1.500E+04 2.711E+ 04
~
1.374763+03 1.30900E403 1.57545E+01 '1.71060E+01' 1.12420E+00 1.500E+04 2.711E+04 '
. , , 1.374765+03:1'.20900E+02.1.71060E+01 1.06190E+01ili11391E+00'1.500E+04 3.711E+04 r*** * 'M 1'.374763+03 : 1'. 309 00E+03 1. 0619 0E+01 3.00512E+ 01' 1.10203 E+ 00.1. 500E+04 3.711B+ 04 W. % M W a?47ss+03 4.sts00E+03;3.00513E+01 3.14035E+0 p .04345E+00 4.,sesg+o4ja a11E+043
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4 Tabk 2.1.3.7 Low Leakage Core Loading Asial Power Distributions Eone Radial Eone Asial Soundary 1 2 3 4 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 1' 1.3970E+01 2.00705 02- 2.0$045 02 1.96473+02 2.34728 02 2 2.73015+01 2.6350E 02 2.6696E+02 2.6007E 02 2.9040E.02 3 4.0792E+01 3.2677E+02 3.20565*02 3.25193 02 3.4631E*02 4 5.4204E+01 3.7477E*01 3.7560E 02 3.744;E 02 3. 0 015 E + 0 2 5 6.7615E+01 3.90375 02 3.9824'a+02 3.98795 02 4.0735E+02 6 0.10265+01 4.17973+02 4.1704E 02 4.1879E+02 4.2295E 02 7 9.44375+01 4.2797E+02 4.2640E 02 4.2871E*02 4.3079E 02 8 1.0785E+02 4.3677E 02 4.35125 02 4.37673 02 4.3743E*02 9 1.21265+02 4.41563 02 4.3976E.02 4.4262E 02 4.4079E 02 10 1.34675+02 4.4596E 02 4.4416E 02 4.4718Ea02 4.4303E*02 11 1.40085+02 ( 4.4876E 02 4.4600E*02 4.4990E 02 4.4519E+02 1 12 1.6149E+02 4.51565+02 4.4960E+02 4.5270E*02 4.4647E+02 13 1.7490E+02 4.53165 02 4.51365 02 4.5454E 02 4.4671E.02 14 1.0832E+02 4.55163 02 4.5320E*02 4.5630E*02 4.46075 02 15 2.0173R+02 4.55965 02 -4.5416E*02 4.57425 02 4.4639E+02 < 16 2.1514E+02' 4.5716E 02 4.55125 02 4.5854E 02 4.45675 02 17 2.2855E+02
<coxi. 4.5676E*02 4.54005 02 4.5006E*02',4.4367E+02
- it 2.41965+02 4.55965 02 4.54323 02 4.5750E*02 4.4159E.02 19 2.35373+02
.4.51564 02 4.5040E 02 4.5310E 02 4.3639E 02-20 2.6070E+02~ .
4.46365 02 4.4560E 02 4.4766E*02 4.3031E+02-21 2.8219E+02 4.3117E*02 4.3120E 02 4.3167E*02 4.16715,02-22 2.9561E+02- .
.' - g_2
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l T0ble 2.1.3.7 Low Leakage Core Loading Asial Power Distributions (cont'd) Eone Radial Zone Asial Boundary 1 2 3 4 22 2.9561E+02 4.11575 02 4.12723 02 4.1127E*02 3.9967E.02 23 3.0902E+02 3.62773 02 3.65605 02 3.6127E*02 3.58965 02 24 3.2243E+02 2.9678E*02 3.0120E 02 2.9343E 02 3.0304E 02 25 3.3584E402 t 2.30783 02 2.3672E*02 2.2567E*02 2.48725 02 , 26 3.4925E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 27 3.8211E+02 tone Radial Radial Eone Boundary 1 107.175 2 128.610 3 150.040 4 184.461
- s f f k '
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Tabb 2.1.3.8 Lcrw Leakage Core Loading Edit Locations
. *(en) t (me) 0(derroes).
. Thiusel shield capsules .
. Flus Spectrum and .
Peak Reactica Retse 203.25 195.76 20 . Pressure vessel Capsules
* . Flus Spectrum and .
. Peak Roastion kates 215.43 195.76 30 .
. Cavity Capsules /
. Flus Spectrum and .
. Peak mesetion aates 330.06 184.665 9.5 .
4
. Fluses and DFA Rates' 320.06 194.665 0 45 .
. Pressure vessel 0.Ts+ .
. (A) Asial peak Location .
. (al-B = 1.0 M*V 219.391 195.760 0 45 .
. (b) B > 0.1 MrY 219.393 195.750 0 45 .
. (c) DFA mates 219.393 195.760 0 48 .
. (d) Plum Spectrum $19.393 198.760 15.5 .
(s) Lower Wold Locatico 219.393 67.1040 0 45 .
. Pressure vessel 1/4 Ts .
. (A) Asial Peak Location 0 45 (a) I a 1.0 MrY 234.473 195.760 .
4 (b) E
- 0.1 punf 224.473 192.062 0 48 .
. lo) DFA sates 224.473 195 760 0*45 .
. (d) Flum Spectrum 224.473 195'.760 15.5 .
. (B) Lower weld Location 224.473 67.1048 0 45 .
. Pressure Vessel 1/2 To .
. (A) Asial peak Location .
. (a) S = 1.0 Mrv 229.070 195 760 0 45 .
. (b) E
- 0.1 bunf 229.070 192.062 0 45 .
. '(c) DPA Rates 229.470 192.062 0 45 .
(d) Flua Spectrum 229.070 195 760 15.5 . (3) Lower Wald Loestion 219.07C 67.1040 0*45 . o.................
. Pressure vessel 3/4 T .
. (A) Asial peak Location .
. (a) 3 = 1.0 mrv 23l.268 192.062 0 45 .
. (b) E > 0.1 NEY 235.268 192.062 0 48 .
. (c) DFA Rates 235.260 192.062 0 45 .
(d) Flua Spectrum 229.070 192.062 15.5 . (3) Lower weld Location 235.268 67.1048 0 45 .
. Preseure Vessel Outer T .
. (A) Asial Peak Location 0 45
. (a) R = 1.0 MWV 240.342 192.?62 .
. + . (b) 5 > 0.1 Msv 240.342 100.363 0 45 .
. (c) DFA Eates 240.342 100.363 0 45 .
(d) Flus Spectrum 240.342 198.760 15.5 .
. ,(3) . Lower Weld Location 240.342 67.1049 0 45 .
210.50 _195.76 0 45 .-
. . .. Downsomer _
-. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .......g..................................
'~t?
+The inner. wall (0.T) and venet outer. wall (T) edits were taken at the Center of the mesh blocks immediately laside the vessel. He vessel laternal edits were taken at mesh blocks centered about the required edit locatloa.
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1 Table 2,1 A.1 Partial Length Shield Assembly Core Loading Basic Design Data
. Reactor . . Material .
. Thermal Power . 2527.73 MW(TN) . .*
. Core Inlet Temp. . 536'F . ..
. Core Operating Pressure . 2010 psia . ..
.................................................................., 1
. Raffle Thickness . 1.5075 cm . 88 304 .
By* Pass e
. N 0 (560 F 3 .
.............................................................2010psia).
. Inner Radius of Core Barrel . 190.185 cm . ..
. Barrel Thickness . 3.01 cm 88 304
. Inner Inlet Thickness . 2.54 on . Mg0 ($36.F .
.............................................................2010psia).
Inner Radius of Thermal Shield. 196.535 cm . ..
. Thermal shield Thickness . 3.81 cm . 88 304 .
. Outer Inlet Thickness . 10.095 an . Ngo (53 6*F .
. . 2010 psia).
. Inner Radius of Liner Clad . 210.440 cm . ..
. Vessel Liner Clad Thickness . 0.635 cm . S8 304 .
. Vessel Thickness . 21.59 cm . SA.3023
. FY Insulation Air Thickness . 1.835 cm . Air .
. FV Insulation Thickness . 10.16'at . FV Insulatio6 .
. Cavity Thickness . 82.62 cm . Air. .
.. Immer, Radius of, . 335.200 em'
. Biological shield . . .
Bio shield Liner Thickness 0.635 cm SA 3023
,1, .
% 3., Bio? Shield;Thiehness .. N 213.3 6 - om ' .Y Comoreto b
...................................................(...........4.gW.
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- 3 -
. :*? ax e i $ E: , g + 1 4
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- 4 , '
a
Table 2.1.4.2 l Partial Length Shield Assembly Core Loading l Core and Fuel Assemblies n J 4
. Total Number of Fuel Assemblies 204 .
1 . .
. Number of Partial Length Fuel Assemblies 24 .
. Number of Rods per assembly (15x15) 216 fuel rods .
. O guide tubes .
. 1 instrument tube .
. Assembly Pitch 21.485 cm .
. Fin Pitch 1.43233 cm .
. Fuel Material Sintered UOg pellets .
. Cladding Material Er.4 .
. Fuel Active Length 335.28 cm .
. Fuel Active Length of 240.144 cm .
. Partial Length Assembly .
I Partial Length Shield Assembly Core Loading Basic Design Data Upper and Lower Reflectors 1
-- . Lower Reflector Thickness 13.97 on 88 304 + water (536*F) .
. . Upper Reflector Thickness 32.865 cm 88 304 + water (584*F) .
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Table 2.1.4.3 Partial Length Shield Assembly Core Loading Design specification asatorial compositions
. Histure Component Atos penetties .
(etos/baca) .
. N 2.825003 02 .
. 3 2.692005 05 .
. 0 1.412005 02 .
. C 2.581005 05 .
0 (fuell 1.20$003 02 .
. Al 3.560005 04 .
. Core Cr 1.608003 05 .
. Fe 2.20$005 05 .
. Ni 3.077003 05 .
. Er 5.440005 03 .
. U.235 1.120003 04 .
. U.230 6.030005 03 .
. Fu.239 , 2.200005 05 .
. Fu.240 7.120003 06 .
. Cr 1.85300E.02 .
. Beetle un 1.752003 03 .
. (38 304) Fe 5.00700E*02 .
. Ni 8.57400F.03 .
. Dypasa+ E 4.929005 02 .
. (560* F) 0 2.464005 02 .
. B 4.900005 06
. Cr 1.053005 02 .
. Core terrol Ha 1.752005 03 .
. (55 304) Fe 5.00700B+03 .
. NL 4.574003 03 .
.- talet Water Gep E 5.095005 02 .
. (53 6'F) 0 2.548005 02 .
. B 5 300003 06 .
. Cr 1.853005 02 .
. Thermal Shield aan 1.752003 03 .
. (88 304) Fe 5.007003 02 .
. Ni 8.574005 03
.............................Cr....................................
1.053005 02 .
. RFY Liner. Ha 1.752005 03 .
. (88 304) Fe 5.007005 02 .
. N1 4.574005 03 .
. C f.040005 04 .
. RFV Well 81 7.50900E*04 .
. (SA 3023) Ben - 1.391005 03 .
. Fo 4.103005 02 .
. No 3.140005 04
+This composition is also to be used la the water region between the fuel assembly and the core bame (see F"qure 2.4.1).
s6gn , le - AMNHugs-t 9, e sqf 7g " = Y m
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J
e Table 2.t4.3 Partial Length Shield Assembly Core Loading Design Specification Material Compositions (coct'd)
. Misture Component Atos Densities .
I (aton
..................................................../b*ca) .............,
Cr 3.43000E.04 . Mn 3.24000M.05 .
. RFV Fe 1.074004 03 .
. Insulation Wi 1.59000N.04 .
A1 1.30000E.04 . N 3.770003405 . 0 9.950005 05
. Cavity N 3.20000E.05 (Air)
O 8.00000E 06 . C 9.84000E.04
. Bio. shield Liner S1 7.589005 04 (SA 3023) Mn 1.391005 03 .
Fe 0.183005 02 . No 3.14000E 04 R 7.770005 03 . l C 1.150005 04 . 0 4.380005 02 . Na 1.0!C00E 03
. Bio Shield Ng 1.400003 04 (concrete) A1 2.39000E.03
.' si 1 580005 02 .
K 6.93000E 04 . Ca 2.29000E 03 ( . Fe 3.130005 04 .
. Cr 8.783003 03 .
Mn 0.30400E.04 . Fe 2.753005 02 .
. Shield NL 4.064005 03
. Aerembly N 2.88400E 02 0 1.34200E 02 .
3 10 2.572003 05 . Cr 4.53250E.03 . Mn 4.300005 04 . Lower Reflector Fe 1.45175E.02 .
. (Water Steel) Ni 2.143505 03 .
. (536*F) 5 3.822005 02 .
0 1.91100E 02 . B 3.825005 05 Cr 4.63250E.03 ., Me 4.380005 04
. Upper,Eeflector Fe 1.451753 02 (Water steel) Mi 2.143505 03 .
(584*F) ,E 3.553033 02 .
. O' 1.776565 02 .
r , '. B- 3.533935
.....'..............................s.~...".k.....'.;......t06. 4. .Y.ma;; .g.p- g v o eld ,
. =
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Table 2.1,4.4 Partial Length Shield Assembly Core Loading Axial zone Assignments
. zone Description .
. 1 Lower Reflector .
. 2,3 Active Core Fuel Assemblies .
. . 4 Upper Reflector .
. 5 Shield Assembly .
. 6 Core Baffle .
. 7 By. Pass .
. 8 Core Barrel .
. 9 Inner Inlet Water Gap .
. 10 Thermal Shield .
. 11 Outer Inlet Water Gap .
. 12 Reactor Pressure Vessel Liner .
. 13 Reactor Pressure Vessel .
. 14 Air Gap .
. 15 Pressure Vessel Insulation .
. 16 Cavity .
. 17 Biological Shield Liner .
. it Biological Shield .
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- 1%per Partial Assembly Core umMay pg y ' Ptsel n====hly Geometry, Power, and.Burnup Distr hanHons' e ,
'j
. f,'p 4 4
[ ., Relative' acc Buraup socOsa
- As===My One )
aurnup
)
Axial' Pan Peaking Power .- , 7$ ' Set' Factor 7 Power. i Assisably ' X.IMt X-Right> -.Y-Bot Y-Top-
'h In,suber 1.0000 0
- w. 1.0000
'2.14850E+01 .7.72900E-01 4.02000E+03 ~1.54200E+04 '0 F j) 11:!0.00000E+00.,2.14c50E+01 'O.00000E+000.00000E+00. 2.14850E+01 S.77600E-01 4.02000E+03 1.54280E+04 1.0000 0 T 12m 2.14850E+01> 4.29700E+01 0.00000E+00' 2.14850E+01 8.91400E-01 4.02000E+03. 1.54280E+04' 1.0000 0
% i ~3 4.29700E+011 6.44550E+01 2.14850E+01- 7.63500E-01 0.00000E+00' 1.21140E+04 1.0000 0
.t ;4- 6.44550E+01;-S.59400E+01 0.00000Et00 1.0000 13 i
5 8.59400E+01< 1.07425E*02 0.00000E+00 1.07425E+02 0.00000E+00= 0.00000E+00 2.14850E+01 0.00000E+00 8.77600E-01 8.20900E-01 0.00000E+00
-1.0000 1.46200E+04-14 1.43140E+04
'6 1.0000 2.81650E+04 15'
=7 1.28910E*02' 0.00000E+00 0.00000E+00 0.00000E+00 8.22400E-01 7.50500E+03.'2.09740E+04 h -
+ 1.0000' O
-8 1.50399E+02- 0.00000E+00' O 00000E+00 0.00000E+00 3.60000E-01 8.20900E-01.-4.02000E+03 1.54280E+04: 0.00000E+00 0 .3.43500E+03 1.0000-
/ 92.14850E+01C.44550E+61 4.29700E+01~ # 2.14850E+01.
2.14850E+01 4.29700E+01 4.29700E+01 7.52500E-01.-4.02000E+03~ 1.0000 1.5428CE+04 -0
'f 10 4.29700E+01 ' S.59400E+01'.2.14850E+01,.4.29700E+01 9.43000E-01 0.C9000E+00' 1.49700E+04 1.0000 0 11' 6.44550E+01~ 1.07425E+02 2.14850E+01,- 4.29700E+01 S.48400E-01 7.80200E-01 -S.52800E+03'-2.24750E+04
.0.00000E+00 1.18320E+04 1.0000' 10
-12 ;8.59400E+01' 0.00000E+00 1.0000 11 T- - 13: 1.0742SE+02' O.00000E+00 E2.14850E+01'2.14850E+01 0.00000E+00 8.49300E-01 1.21170E+04 1.0000' 12 2.60290E+04 i
14 :1.28910E+02 H0.00000E+00 4.58000E-01 0.00000E+00 .4.32600E+03' 1.0000 0
'151.50399E+02 0.00000E+00' 2.14850E+01: 0.00000E+00 8.13600E-01 -4.02000E+03~ 1.54200E+04 C T 1.0000: 0-5 *T 16."4.29700E+01' 6.44550E+01 4.29700E+01 6.44550E+01- 1.0000 0 17 6.44550E+01 S.59400E+01: 4.29700E+01' 6.44550E+01 7.67100E-01 'O.00000E+00 '1.20663E+0 1.0000 7 t IS- S.59400E+01 L1.0742SE+02 4.29700B+01 6.44550E+01 9.42300E-011.0000' 0.00000E+00 1.49243E+
I ' S 19 <1.07425E+02 'O.00000E+00 4.29700E+01 0.00000E+00 O.00000E+00 7.63400E-01 0.00000E+00 6.86000E-01' 1.26090E+04 2.47790E+04 3.61655E+04 d o 1.0000 9 W' s. 20 1.28910E+02' 0.00000E+00.- 4.29700E401' 1.0000 0 J % 21 1.50399E+02' O.00000E+00 8.59400E+01 6.44550E+014.29700E+01 0.00000E+00 8.59400E+01. 8.20900E-01 0.00000E+00 3.60000E-01 1.28990E+040.00000E+00' 1.0000 4 3.43500E+03 " Mi 1.0000 5 4" 7 L 22 :6.44550E+01': 8.59400E+01 0.00000E+00 6.44550E+01 0.00000E+00 7.31700E-01 2.08950E+04 3.30110E+04 1.0000 6 4[- ~ bP ~25: 2324.r1.07425E+02
'1.28910E+02: -0.00000E+00 0.00000E+00- 6.44550E+01 6.44550E+01 C.00000E+00 0.00000E+00 8.45500E-01' O.00000E+00 1.40180E+04 5.46200E-01 8.60900E-011.0000 0.00000E+00 1-0.00000E+00 1.0000 2
- 1.41
'8.91500E
~8.59400E+01 0.00000E+00 t i 26 '8.59400E+01,'0.00000E+00 1.0000 3.
S ' s' 27s1.07425E+02 O.00000E+00 0.00000E+00 0.59400E+01 S.59400E+01 0.00000E+00' 0.00000E+00 4.67600E-01 6.60800E-01 0.00000E+00 7.63500E+03 0.00000E+00 1.08970E ' i I.jf, 1 28 T1.28910E+02 fy~ 6 goe.: $ssemblies inel bnpowersetsdonothaverightortopre.1hese i data are included with the pin l uQ: 4 jp -
'$7 -houndaries spec geometry. data.
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....r ...,.i._. . , , _ _ _ . _ _ _ _ _ _ _ ____
.._...e -
y3 g. , I "2 - @ + , - % ~' a; . n
- N 7
< Table 2.1.4.6 _
Lower Partial Assembly Core Loading s Fuel Assembly Gecznetry, Power, and Burnup Distributions i Relative BOC Burnup EOC Burnup Axial Pin Assembly Assembly (MWD ) (MWD ) Peaking . Power Number X-Left X-Right Y-Bot Y-Top Power Factor Set 1 S.00000E+00 2.14850E+01 0.00000E+00 2.14850E+01 2.90100E-01 4.02000E+03 1.54280E+04 1.0000 0 2 2.14850E+01 4.29700E+01 0.00000E+00 2.14850E+01 3.29400E-01 4.02000E+03 1.54280E+04 1.0000 0 . 3 4.29700E+01- 6.44550E+01 0.00000E+00 2.14850E+01 3.34600E-01 4.02000E+03 1.54280E+04 1.0000 0 4 6.44550E+01 8.59400E+01 0.00000E+00 2.14850E+01 2.86500E-01 0.00000E+00 1.21140E+04 1.0000 0 5 8.59400E+01 1.07425E+02 0.00000E+00 2.14850E+01 3.29400E-01 0.00000E+00 1.43140E+04 1.0000 0 6 1.07425E+02 0.00000E+00 0.00000E+00 0.00000E+00 3.11100E-01 174 6200E+ 04 2.81650E+04 1.0000 11 7' 1.28910E+02 0.00000E+00 0.00000E+00 0.00000E+00 3.07600E-01 7.50500E+03 2.09740E+04 1.0000 12 9 2.14850E+01 4.29700E+01 2.14850E+01 4.29700E+01 3.08100E-01 4.0200DE+03 1.54280E+04 1.0000 0 10 4.29700E+01 6.44550E+01 2.14850E+01 4.29700E+01 2.82500E-01 4.02000E+03 1.54280E+04 1.0000 0 a 11 6.44550E+01 8.59400E+01 2.14850E+01 4.29700E+01 3.54000E-01 0.00000E+00 1.49700E+04 1.0000 0 12 8.59400E+01 L.07425E+02 2.14850E+01 4.29700E+01 2.92800E-01 0.00000E+00 1.18320E+04 1.0000 0 13 1.07425E+02 0.00000E+00 2.14850E+01 0.00000E+00 3.21500E-01 8.52800E+03 2.24750E+04 1.00J0 9 L 14 1.28910E+02 0.00000E+00 2.14850E+01 0.00000E+00 3.17700E-01 1.21170E+04 2.60290E+04 1.0000 10 16 4.29700E+01 6.44550E+01 4.29700E+01 6.44550E+01 3.05400E-01 4.02000E+03 1.54280E+04 1.0000 0 17 6.44550E+01 8.59400E+01 4.29700E+01 6.44550E+01 2.87900E-01 0.00000E+00 1.20663E+04 1.0000 0 18 8.59400E+01 1.07425E+02 4.29700E+01 6.44550E+01 3.53700E-01 0.00000E+00 1.49243E+04 1.0000 0
- 19 1.07425E+02 0.000002+00 4.29700E+01 0.00000E+00 2.60000E-01 2.47790E+04 3.61655E+04 1.0000 7 20 1.28910E+02 0.00000E+00 4.29700E+01 0.00000E+00 2.85600E-01 0.00000E+00 1.26090E+04 1.0000 8 22 6.44550E+01 8.59400E+01 6.44550E+01 8.59400E+01 3.08100E-01 0.00000E+00 1.28990E+04 1.0000 0 1.0000 4
- 3. 23 8.59400E+01. 0.00000E+00 6.44550E+01 0.00000E+00 2.77300E-01 2.08950E+04 3.30110E+04 1.0000 5 4 24 1.07425E+02- 0.00000E+00 6.44$50E+01 0.00000E+00 3.22100E-01 0.00000E+00 1.41970E+04 1.0000 6
'25 1.28910E+02 0.00000E+00 6.44550E+01 0.00000E+00 1.96800E-01 0.00000E+00 8.91500E+03 1
. m 26 8.59400E+01' O.00000E+00 8.59400E+01 0.00000E+00 3.20500E-01 0.00000E+00 1.40190E+04 1.0000 1.0000 2 s 27 1.07425E+02 0.00000E+00 8.59400E+01 0.00000E+00- 2.47100E-01 0.00000E+00 1.08970E+04 1.0000 3
; - 28 1.28910E+02 0.00000E+00 8.59&OOE+01 0.00000E+00 1.68400E-01 0.00300E+00 7.63500E+03
- Note: Assemblies including pin power sets do not,have right or top boundaries specified here. These data are included with the pin v- geometry data.
9 1
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s [ x. L [
...._._._.m. . . . , . . _ , . . - . . . . . . . . . , , , ..., . _
f I L Table 2A.4.7 Upper Partial Assembly Core Loading Pin Geometry, Power, and Eurnup Distributions Assembly 6 Pin Power set 13
- , Relative 30C EOC Pia surnup Burnup E Lett E Eight Y Bot Y Tol, Power (MWD ) (MWD )
1.07425E+02 1.088575+02 0.00000E+00 1.43223E+00 1.09062E+00 1.462E+04 2.815E+04 1.07425E+02 1.00857E+02 1.43223E+00 2.864465+00 1.07792E+00 1.462E+04 2.816E+0( 1.07425E+02 1.000575+02 2.96446E+00 4.29669E+00 1.03094E+00 1.462E+04 2.815E+04
- 1.07425E+02 1.000575+02 .4.296693+00 5.72092E+00 1.03163E+00.1.462E+04 2.8165+04 1.07425E+02 1.000573+02 5.72092E+00 7.16115E+00 0.00000E+00 1.462E+04 2.016E+04 1.07425E+02 1.00857E+02 7.16115E+00 0.593385+00 1.01093E+00 1.462E+04 2.816E+04 1.07425E+02 1.08057E+02 8.593385+00 1.00256E+01 9.09004E 01 1.462E+04 2.016E+04
- 1.07425E+02 1.009573+02 1.00256E+01 1.14578E+01 9.0169 6E 01 1.462E+04 2.8165+04 1.07425E+02 1.000575+02.1.14578E+01 1.20901E+01 9.04132E-01 1.462E+04 2.816E+04 1.07425E+02 1.00057E+02 1.28901E+01 1.43223E+01 9.98740E 01 1.462E+04 2.816E+04
-1.07425E+02 1.00857E+02 1.43223E+01 1.57545E+01 0.00000E+00 1.462E+04 2.816E+04 1.07425E+02 1.00857E+02 1.57545E+01 1.71868E+01 9.97530E-01 1.462E+04 2.816E+04 1.07425E+02 1.00857E+02 1.71060E+01 1.86190E+01 9.700423 01 1.462E+04 2.815E+04 1.07425E+02 1.00857E+02 1.86190E+01 2.00512E+01 9.70735E 01 1.462E+04 2.815E+04 1.07425E+02 1.00857E+02 2.00512E+01 2.14835E+01 9.195793 01 1.462E+04 2.816E+04
.1.09857E+02 1.10289E+02 0.00000E+00.1.43223E+00 1.13630E+00 1.462E+04 2.816E+04 1.00057E+02 1.102895+02 1.43223E+00 2.86446E+00 1.05043E+00 1.462E+04 2.016E+04 1.08857E+02 1.10289E+02 2.96446E+00-4.29669E+00 1.013365+00 1.462E+04 2.016E+04 1.088575+02 1.10289E+02 4.29669E+00 5.72092E+00 1.06200E+00 1.462E+04 2.816E+04
'1.080575+02.1.10289E+02.5.72892E+00 7.16115E+00 1.04990E+00 1.462E+04 2.016E+04 1.08857E+02 1.10289E+02 7.16115E+00 8.59338E+00 1.03205E+00 1.462E+04 2.816E+04 1.008575+02 1.10289E+02 8.59330E+00 1.00256E+01 1.02067E+00 1.462E+04 2.816E+04
- 1.00057E+02 1.10209E+02 1.00256E+01 1.14578E+01 1.01702E+00 1.462E+04 2.816E+04 1.08857E+02 =1.10289E+02 1.14570E+01' 1.289 01E+01 1.01500E+00 1.462E+04 2.816E+04 1.08057E+02 1.10289E+02 1.20901E+01 1.43223EiO1 1.02109E+00 1.462E+04 2.816E+04 1.00057E+02.1.102895+02 1.43223E+01 1.57545E+01 1.03042E+00 1.462E+04 2.816E404
,1.080575+02 1.10289E+02 1.57545E+01 1.71868E+01 1.02798E+00 1.462E+04 2.816E+04 1.008575+02 1.10209E+02 1.71860E+01 1.86190E+01 9.561193 01 1.462E+04 2.816E+04 1=000575+02 1.10289E+02 1.86190E+01 2.00512E+01 9.524655 01 1.462E+04 2.816E+04 1.080573+02 1.10289E+02 2.00512E+01 2.14335E+01 9.46375E-01 1.462E+04 2.815E+04 1.10289E+02 :1.11722E+02 0.00000E+00 1.43223E+00 1.13029E+00 1.462E+04 2.016E+04 1.10209E+02-1.11722E+02 1.43223E+00 2.86446E+00 1.047475+00 1.462E+04 2.816E+04 1.10289E+02 1.11722E+02 2.86446E+00 4.29669E+00 1.00727E+00 1.462E+04 2.816E+04 1.10289E+02 1.11722E+02 4.29 6695+00 -5.7209 2E+00 1.03042E+00 1.462E+04 2.815E+04
-1.102093+02:1.11722E+02 5.72092E+00 7.16115E+00 1.007275+00 1.442E+04'2.816E+04
~
1.10289E+02 1.11722E+02 7.16115E+00 0.59338E+00 9.9 6312E-01 1.462E+04 - 2.816E+04 1.10289E+02 1.11722E+02 0.59338E+00 1.00256E+01'9.930763-01 1.462E+04 2.016E+04 1.10209E+02 1.11722E+02 1.00256E+01 1.145785+01 9.09835E-01 1.462E+04 2.016E+04
'1.102895+02;1.11722E+02 1.1457BE+01;1.28901E+01 9.890045-01 1.462E+04=2.816E+04-1.102095+02 1k11722E+02 1 20901E+0111;43223E+01'9~.06560E 01'1.462E+04*3.816E+04 1.10289E+02 1.11722E+02 1.43223E+01 1.57545E+01 9.90220E-01 1.462E+04 2.816E+04 1.102895+02 1;11722E+02 1.57545E+01 1.71868E+01 9.98740E 01 l'.462E+04 2.816E+04
=1;102095+02-1.11722E+02;1.71860E+01 1.86190E+01 9.52465E 01 1.462E+04f2.816E+04
<:1.10289E+02'1.11722E+02 1.86190E+01 2.00512E+01 9 451575 01 1 462E+04h2.816E+04z 1.102895+02_1.11722E+02 2.00512E+01 2.14035E+01-9.42721E G1 1'.462E+0412.014E+04 y '#,F
-f ,
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- e suw'empa +
bh k N ,Mkh N k } % h M N $ d e ykyy .* m,4pg.. _.4 m , , ; g4 ,g 4 .
Table 2.1.4.7 Upper Partial Assembly Core Loading Pin Geometry, Power, and Burnup Distributions (cont'd) Assembly 6 Pin Power Set 13 Relative BOC EOC Pin Burnup Burnup X Left X Right Y Bot Y-Top Power (MWD ) (MWD ) 1.11722E+02 1.13154E+02 0.00000E+00 1.43223E+00 1.13638E+00 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.43223E+00 2.96446E+00 1.11689E+00 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 2.86446E+00 4.29669E+00 1.04869E+00 1.467 >04 2.816E+04 1.11722E+02 1.13154E+02 4.29 669 E+00 5.72 89 2E+00 1.00727E+00 1.4 6e >04 2.816E+04 1.11722E+02 1.13154E+02 5.72892E+00 7.16115t< 00 9.84132E-01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 7.16115E+00 8.59330E+00 9.74388E+01 1.4622+04 2.816E+04 1.11722E+02 1.13154E+02 8.59338E+00 1.00256E+01 9.71952E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.00256E+01 1.14578E+01 9.71952E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.14578E+01 1.28901E+01 9.68299E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.28901E+01 1.43223E+31 9.65863E-01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.43223E+01 1.57545E+01 9.68299E*01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.57545E+01 1.71868E+01 9.78042E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.71868E+01 1.86190E+01 9.92658E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.86190E+01 2.00512E+01 1.00727E+00 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 2.00512E+01 2.14835E+01 9.52465E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 0.00000E+00 1.43223E+00 0.00000E+00 1.462E+04.2.816E+04 1.13154E+02 1.14586E+02 1.43223E+00 2.86446E+00 1.11202E+00 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 2.86446E+00 4.29669E+00 1.03407E+00 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 4.29669E+00 5.72892E+00 9.92658E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 5.72892E+00 7.16115E+00 9.70735E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 7.16115E400 8.59338E+00 9.62209E-01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 8.59338E+00 1.00256E+01 9.58555E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.00256E+01 1.14578E+01 9.58555E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.14578E+01 1.28901E+01 9.56119E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.28901E+01 1.432'JE+01 . 9.53683E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.43223E+01 1.57545E+01 9.56119E-01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.575$5E+01 1.71868E+01 9.65863E-01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.71868E+01 1.8C190E+01 9.80478E 01 1.462E+04 2.916E+04 1.13154T+02 1.14586E+02 1.86190E+01 2.90512E+01 1.00484E+00 1.462E+04 2.816E+04 1.13154E+02 1.14596E+02 2.00512E+01 2.14835E+01 0.00000E+00 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 0.00000E+00 1.43223E+00 1.12420E+00 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.43223E+00 2.86446E+00 1.09741E+00 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 2.86446E+00 4.29669E+00 1.02433E+00 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 4.29669E+00 5.72892E+00 9.85350E 01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 5.72892E+00 7.16115E+00 9.64645E 01 1.462E+04 2.816E+04 1.14536E+02 1.16018E+02 7.16115E+00 8.59338E+00 9.56119E 01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 8.59338E+00 1.00256E+01 9.57337E-01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.00256E+01 1.14578E+01 9.58555E-01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.14578E+01 1.28901E+01 9.54901E-01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.28901E+01 1.43223E+01 9.50029E 01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.43223E+01 1.57545E+01 9.52465E-01 1.462E+04 2.816E+04 1.14586E+02'1.16018E+02-1.57545E+01 1.71868E+01 9.59773E 01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.71868E+01 1.86190E+01 9.74388E 01 1.462E+04 2.816E+04 1.14586E+02 1.16018E+02 1.86190E+01 2.00512E+01 9.95094E 01 1.462E+04 2.81Gl+04 1.14586E+02 1.16018E+02 2.00512E+01 2.14835E+01 9.48811E 01 1.462E+04 2.815E+04 b Y y ;y
- M $, *i i
w;4g.ggggggg,pyyj < ,
. . _ _ _ ~ _ _ . _ -. --m .- . - . - - - , . .- ..m -
4 Table 2.1 A.7 Upper Partial Assembly Core Loading [
- Pin Geometry. Power, and Eurnup Distributions (cont'd)
Assembly 6 Pin Power set 13 ,
=
Relative ROC EOC Fin Burnup turnup X Left E Right Y Bot Y Top Power (NWD ) (MND ) 1.160195+02 1.17451E+02 0.00000E+00 1.43223E+00 1.10349E+00 1.462E+04 2.816E+04 1.160185+02 1.17451E+02 1.43223E+00 2.86446E+00 1.08401E+00 1.462E+04 2.916E+04 1.160185+62 1.17451E+02 2.86446E+00'4.296695+00 1.02311E+00 1.462E+04 2,0162+04 1.160185+02 1.17451E+02 4.29669E+00 5.72O32E+00-9.92914E 01 1.462E+04 2.016E+04 11.16010E+02 1.17451E+02 5.72092E+00 7.16115E+00 9.622093 01.1.462E+04 2.816E+04-1.16010E+02 1.17451E+02 7.16115E+00LO.59330E+00 9.57337E 01 1.462E+04 2.016E+04 1.16010E+02 1.17451E+02 0.5933er+10.1.002S65+01 9.67081E-01 1.462E+04 2.816E+04 1.16010E+02 1.17451Et02 1.00256E+0i 1.14570E+01 9.75606E 01 1.462E+04 2.816E*04 1.160185+02 1.17451E+02 1.14578E+01 1.20901E+01 9.64645E 01 1.462E+04 2.816E+04 1.16018E+02 1.17451E+02 1.20901E+01 1.43223E+01 9.52465E 01 1.462E+04 2.816t+04 1.16010E+02 1.17451E+02 1.43223E+01 1.57545E+01 9.51247E*01 1.462E+04 2.8165+04 1.16018E+02 1.17451E+02 1.57545E+01 1.710605+01 9.59773E 01 1.462E+04 2.8162 04 1.16018E+02 1.17451E+02:1.71068E+01 1.86190E+01 9.75606E-01 1.462E+04 2.816E+04 1.16018E+02 1.17451E+02 1.86190E+01 2.00512E+01 9.07756E 01 1.462E+04 2.016E*04 1.16010E+02 1.17451E+02 2.00512E+01'2.14835E+01 9.32977E 01 1.462E+04 2.816E+04 1.17451E+02 1.13083E+02 0.00000E+00 1.43223E+00 1.09619E+00 1.462E+04 2.816E,04 1.17451E+02 1.18883E+02 1.43223E+00 2.86446E+00 1.00035E+00 1.462E+04 2.016E+04 1.17451E+02 1.18803E+02 2.86446E+00 4.29669E+00 9.41503E 01 1.462E*04 2.816E+04 1.17451E+02 1.19803E+02 4.29669E+00 5.72892E+00 9.81636E 01 1.462E+04 2.816E+04 1.17451E+02 1.10083E+02 5.72092E+00 7.16115E+00 9.59773E-01 1.462E+04 2.616E+04 1.17451E+02-1.19883E+02 7.16115E+00 0.59330E+00 9.57337E 01 1.462E+04 2.816E+04 1.17451E+02'1.18883E+02 t.59338E+00 1.00256E+01 9.7438BE 01 1.462E+04 2.916E+04 1.17451E+02 1.18003E+02 1.00256E+01 1.14570E+01 0.00000E+00-1.462E+04 2.W16E,04 1.17451E+02 1.19803E+02 1.14578E+01 1.20901E+01 9.71952E 01 1.462E+04 2.816E+04 1.17451E+02 1.18083E+02 1.28901E+01 1.43223Et"01 9.52465E-01 1.462E+04 2.816E+04 1.17451E+02 1.18083E+02 1.43223E+01 1.57545E+01 9.51247E 01 1.462E+04 2.916E+04 1.17451E+02 1.19883E+02 1.57545E+C1 1.7186BE+01 9.62269E-01 1.462E+04 2.816E+04 1.17451E+02 1.10003E+02 1.71868E+01 1.86190E+01 9.04963E 01 1.462E+04 2.016E+04 1.17451E+02 1.10083E+02~1.86190E+01 2.00512E+01 9.87786E 01 1.462E+04 2.816E+04 1.17451E+02 1.19883E+02 2.00512E+01 2.14835E+01 9.28105E 01 1.462E+04 2.816F.+04
-1.10083E+02 1.20315E+02 0.00000E+00 1.43223E+00 1.09741E+00 1.462E+04 2.Olst+04
- 1.18083E+02'1.20315E+02 1.43223E+00 2.06446E+00 1.07792E+00 1.462E+04 2.016E+04 1.18003E+02 1.20315E+02 2.06446E+00 4.29669E+00 1.01702E+00 1.462E+04 2.016E,04 1.18083E+02 1.203153+02 4.29669E+00 5.72892E+00 9.78042E 01 1.462E+04 2.m16E+04 1.18883E+02 1.20315E+02.5.72092E+00,7.16115E+00 9.57337E 01 1.462E+04 2.816E+04 4
-1.18803E+02.1.20315E+02 7.16115E+00 8.59332E+00-9.52465E 01,1.462E+04 2.816E+C4 L1.18003E+02 1.20315E+02 0.59330E+00 1.00256E+01'9.62209E 01 l'.462E+04:2.016E+04
.1;18803E+02 1.20315E+02 1.00256E+01 1.1457BE+01 9.719785 01.1.462E+04 2.911E+04 1.19903E+02 1.20315E+02.1.14578E+01 1.20901E+01 9.62209E1 01 1.462E+04 2.816E+04
, !1.10883E+02: 1.20315E+02 - 1.28901E+01 1.43223E+01 9.50029E 01 1.462E+04 2.616E+04
'1.10003E+02 1720315E+02.1.43223E+01'1.57545E+01 C 9;50029E 01"li462E+04'2.816E504' "1.18083E+02~1.20315E+02 1.57545E+01 1.7106CE+01=9.58555E-01 1.462E+04.2.816E+04 cl.18083E+02 1.20315E+02 1.71868E+01 1.86190E+01 9.75606E 01 1.462E+04 2.016E+04 "arH ear-1.19803E+02' 1.20315E+02 ; 1.8619 0E+0112.00512E+01- 9.87786E 01 1'.462E+04: 2.816E+04 ilh0 61;10003E+02 1.20315E+02.2.00512E+01 2.14835E+01;9.32977E-01'1.462E+04'2.816E+04 w pfl h n , ,e
.__.4 y uwmmu w n .w w.mmmwn -
6%QQQh r 4s 1
~ ~ g ,, +
s - W- ' + 9% th * %% % m&Q , %
. l }
--r - - . . .. .
'sJ
- Table 2.1.4,7 Upper-Partial Asucubly..dore Loading Pin Geometry, Power, and Burnup Distributions (cont'd)
Assembly 6 Fin Power Set 13 Relative ROC EOC Fin Burnup Burnup X Left E Eight Y Bot _Y Top Power DefD ) DefD ) 1.20315E+02 1.21747E+02 0.00000E+00 1.43223E+00 1.11000E+00 1.462E+04 2.016E+04 1.20315E+02 1.21747E+02 1.43223E+00 - 2.064463+00 1.00523E+00 1.462E+04 2.016E+04
- 1.20315E+02 1.217475+02 2.86446E+00 4.29669E+00 1.01458E+00 1.462E+04 2.016E+04
.1.20315E+02.1.217475+02 4.296695+00 5.72892E+00 9.756065 01 1.462E+04-2.016R+04 1.20315E+02-1.217475+02 5.72892E+0017.16115E+00 9.561193 0151.462E+04 2.0165+04
' 1.20315E+02 :1.217473+02 7.16115E+00 0.593395+00 9.500295 01 1.462E+04 2.816E+04 1.20315E+02 1.21747E+02 8.59330E+00 1.00256E+01 9.50C295 01 1.462E+04 2.816E+04 1.20315E+01 1.217475+02 1.09256E+01 1.14578E+01 9.52465E 01 1.462E+04 2.816E+04 1.20315E+02-1.21747E+02 1.145783+01 1.20901E+01 9.50029E 01 1.462E+04 2.0163+04 1.20315E+02 1.21747E+02 1.209 01E+01 1.43223E+01 9.46375E 01 1.462E+04 2.'816E+04 1.20315E+02 1.21747E+02 1.43223E+01 1.57545E+01 9.48811E 01 1.462E+04 2.816E+04 1.20315E+02 1.21747E+02 1.57545E+01.1.71068E+01 9.555555 01 1.462E+04 2.816E+04 1.20315E+02 1.21747E+02 1.71060E+01-1.86190E+01 9.74300E 01 1.462E+04 2.816E+04 1.20315E+02 1.21747E+02 1.86190E+01 2.00512E+01 9.961125 01 1.462E+04 2.816E+04 1.20315E+02 1.21747E+02 2.00512E+01 2.14035E+01 9.500295 01 1.462E+04 2.816E+04 1.21747E+02 1.23180E+02 0.00000E+00 1.43223E+00 0.00000E+00 1.462E+04 2.81EE+04 1.217475+02 1.23100E+02 1.43223E+00 2.86446E+00 1.09741E+00 1.462E+04 2.016E+04 1.21747E+02 1.23100E+02 2.06446E+00 4.296695+00 1.02067E+00 1.462E+04 2.915E+34 1.21747E+02 1.23100E+02 4.29669E*00 5.72892E+00 9.804785 01 1.462E+04 2.616E+04 1.21747E+02 1.23150E+02 5.72892E+00 7.16115E+00 9.59773E 01 1.462E+04 2.816E+04 1.21747E+02 1.23180E+02 7.16115E+00 8.59330E+00 9.524655 01 1.462E+04 2.0165+04 1.217475+02-1.23180E+02 8.59330E+00 1.00256E401-9.500295 01 1.462E+04 2.816E+04 1.21747E+02 1.23100E+02 1.00256E+01 1.14570E+01 9.51247E 01 1.462E+04 2.816E+04 1.21747E+02 1.23180E+02 1.14578E+01 1.20901E+01 9.500295 01 1.462E+04 2.516E+04 11.217473+02 1.23180E+02'1.20901E+01 1.43223Et01 9.500295 01 1.462E+04 2.816E+04 1.21747E+02 1.23180E+02 1.43223E+01 1.57545E+01-9.54901E 01 1.462E+04 2.016E+04 1.21747E+02 1.23100E+02 1.57545E+01 1.71868E+01 9.65043E 01.1.462E+04 2.816E+04 1.21747E+02 1.23180E+02 1.71060F+01 1.86190E+01 9.816965 01 1.462E+04 2.816E+04
=1.21747E+02 1.231SOE+02 1.86190E+01 2.00512E+01 1.007275+00-1.462E+04 2.816E+04 1.21747E+02 1.23100E+02 2.00512E+01'2.14835E+01 0.00000E+00 1.462E+04 2.816E+04 1.23180E+02 1.24612E+02 0.00000E+00 1.43223E+00 1.11811E+00 1.462E+04 2.816E+04
,1;23100E+02 1.24612E+02 1.43223E+00 2.06446E+00.1.10106E+00 1.462E+04 2.016E+04 1.23100E+02 1.24612E+02 2.06446E+00 4.29669E+00 1.03651E+00 1.462E+04 2.816E+04 1.23180E+02 1.24612E+02 4.29669E+00 5.72092E+00 9.975305 01 1.462E+04 2.816E+04
, 1.23100E+02"1.24612E+02 5.72892E+00 7.16115E+00 9.756065 01 1.462E+04 2.816E+04 c l.23180E+02'1.24612E+02 7.16115E+00_ O.59338E+00 9.65863E 01.1.462E+04 2.016E+04
^ "1123180E+02-1.24612E+02 0.59338E+00.1.00256E+01-9.65863E 01;1.462E+04'2.016E+04 1.23180E+02 1.24612E+02 1.002563+01 1.14570E+01'9.60299E 01L1.442E+04L2.016E+04 1.23180E+02 1.24612E+0211.14578E+01:1'.20901E+01 9165063E-01 1.462E+04 2.016E+04 yn .
1;23100E+02 1.24612E+02,1.28901E+01)1.43223E+01_9.658635 01 1.462E+04.2.816E+04
' 1.23100E+02-1124612E+02:1.43223E+01-1.57545E+01'9.719528 01*1".462E404 2.816E+04 1.22180E+02J1.24612E+02-1.57545E+01'1.71860E+01 9.82914E 01,1.442E+04 2.016E+04
' 1.23100E+02:1~.24612E+02 1.71868E+01'1.86190E+01.9.99966E 01 1.462E+04;2.816E404 j$%1.23100E+02<1'.24612E+02 1.86190E+01L2.00512E+01 1.014585+00>1.462E+0422.8165+04
.% d M9 $ M. Lw 3,3180E+02;1,;24412,E+02,2.005145+01.2.14835E+01'9.S9,7735
. 01-1.442E+04 y 2.0163+04 A M WMMU g . y l , hgggg, mmmmsv w mmenn x ammmy 344 .
- , , - . - . - . . . - - . - . - . - ~ ~ . . - - - - - - - . - - - - - -
Table 2.1.4.7 i Upper Partial Assembly Core Loading Pin Geometry, Power, and Burnup Distributions (cont'd) Assembly 6 Pin Power Set 13 L i Eelative ROC EOC Pin Burnup Surnup X Left X Right Y Bot Y Top Power (MND ) (MWD ) i 1.24612E+02 1.26044E+02 0.00000E+00 1.43223E+00 1.11446E+00 1.462E+04 2.816E+04 1.24612E+02 1.26044E+02 1.43223E+00 2.86446E+00 1.03772E+00 1.462E+04 2.816E+04 1.24612r+02 1.26044E+02 2.86446E+00 4.29669E+00 1.02189E+00 1.462E+04 2.816E+04 1.24612E+02 1.26044E+02 4.29669E+00 5.72892E+00 1.02798E+00 1.462E+04 2.816E+04 ! - 1.24612E+02 - 1.26044E+02 5.72892E+00 7.16115d+00 1.00727E+00 1.462E+04 2.816E+04 , 1.24612E+02 1.26044E+02 7.16115E+00 8.59338E+00 9.97530E 01 1.462E+04 2.816E+04 ! 1.24612E+02 1.26044E+02 8.59338E+00 1.00256E+01 9.97S30E 01 1.462E+04 2.816E+04 l 1.24612E+02 1.26044E+02 1.00256E+01 1.14578E+01 9.32977E 01 1.462E+04 2.816E+04 j 1.24612E+02 1.26044E+02 1.14578E+01 1.28901E+01 9.97530E 01 1.462E+04 2.816E+04 l 1.24612E+02 1.26044E+02 1.28901E+01 1.43223E+01 9.97530E 01 1.462E+04 2.816E+04
- 1.24612E+02 1.26044E+02 1.43223E+01 1.57545E+01 1.00484E+00 1.462E+04 2.816E+04
- 1.24612E+02 1.26044E+02 1.57545E+01 1.71868E+01 1.01702E+00 1.462E+04 2 616E+04 d-1.24612E+02 1.26044E+02 1.71868E+01 1.86190E+01 9.91440E 01 1.462E+04 2.816E+04 l 1.24612E+02 1.26044E+02 1.86190E+01 2.00512E+01 9.64645E 01 1.462E+04 2.816E+04
?- 1.24612E+02 1.26044E+02 2.00512E+01 2.14835E+01 9.60991E 01 1.462E+04 2.816E+04
- 1.26044E+02 1.27476E+02 0.00000E+00 1.43223E+00 1.12907E+00 1.462E+04 2.816E+04 i 1.26044E+02 1.27476E+02 1.43223E+00 2.86446E+00 1.06087E+00 1.462E+04 2.816E+04 1 1.26044E+02 1.27476E+02 2.86446E+00 4.29669E+00 1.02311E+00 1.462E+04 2.816E+04
- 1.26044E+02 1.27476E+02 4.29669E+00 5.72892E+00 1.07426E+00 1.462E+04 2.816E+G4 i 1.26044E+02 1.27476E+02 5.72892E+00 7.16115E+00 1.06452E+00 1.462E+04 2.816E+04 i 1.26044E+02 1.27476E+02 7.16115E+00 0.593385+00 1.05112E+00 1.462E+04 2.816E+04 1.26044E+02 1.27476E+02 8.59338E+00 1.00256E+01 1.04260E+00 1.462E+04 2.816E+04 1.26044E+02 1.27476E+02 1.00256E+01 1.14578E+01 1.04260E+00 1.462E+04 2.816E+04 1
1.26044E+02 1.27476E+02 1.14578E+01 1.28901E+01 1.04260E+00 1.462E+04 2.816E+04 i 1.26044E+02 1.27476E+02 1.28901E+01 1.43223E%01 1.05234E+00 1.462E+04 2.816E+04 j 1.26044E+02 1.27476E+02 1.43223E+01 1.57545E+01 1.06330E+00 1.462E+04 2.816E+04 j 1.26044E+02 1.27476E+02 1.57545E+01 1.71868E+01 1.06452E+00 1.462E+04 2.816t+04
- 1.26044E+02 1.27476E+02 1.71868E+01 1.86190E+01 9.95094E 01 1.462E+04 2.816E,04 1 1.26044E+02 1.27476E+02-1.86190E+01 2.00512E+01 9.91440E-01 1.462E+04 2.816E+04
- A.26044E+02 1.27476E+02 2.00512E+01.2.14835E+01 9.82914E 01 1.462E+04 2.816E+04
- 1.27476E+02.1.28908E+02 0.00000E+00 1.43223E+00 1.10715E+00 1.462E+04 2.816E+04 1.27476E+02 1.28908E+02 1.43223E+00 2.86446E+00 1.10106E+00 1.462E+04'2.816E+04 1.27476E+02 1.28908E+02 2.86446E+00 4.29 669E+00 1.06939E+00 1.462E+04 2.816E+04 I
1.27476E+02 1.28908E+02 4.29669E+00 5.72892E+00 1.06208E+00 1.462E+04 2.816E+04 i 1.27476E+02 1.28900E+02 5.72892E+00 7.16115E+00 0.00000E+00 1.462E+04 2.816E+04 1.274765+02 1.28908E+02 7.16115E+00 8.5933SE+00 1.04869E+00 1.462E+04 2.816E+04 1.27476E+02 1;28908E+02 8.59338E+00 1.00256E+01 1.03285E+00 'l.462E+04' 2.816E+04 1.27476E+02 - 1.289 08E+02 1.00256E+01 1.14578E+01 1.0042E+00 1.462E+04 2.816E+04
- 1. 27476E+02 1.289 08E+02 i l .1457 8E+01 1.289 01E+01 1. 03529 E+00 ' 1.462E+04 ,2. 816E+04
, 1.27476E+02.1.28908E+02 1.28901E+01 1.43223E+01 1.04990E+00 1.462E+04 2.816E+04 _
- l'.27476E+02 -1;28900E+02:1.43223E+01 1.57545E+01 0.00000E+00:1;462E+04 2.816E+04 -
3' 1.27476E+02 1.28908E+02 1.57545E+01 1.71868E+01 1.05599E+00 1.462E+04.2.816E+04
~ 1.27476E+02'1.28908E+02 1.71868E+01 1.86190E+01 1.04381E+00 1.462E+04.2.816E+04 '
- j. 1.27476E+02 1.28908E+02 1.86190E+01 2.00512E+0111.03651E+00 1.462E+04-2.816E+04 ~
1.27476E+02 1.289 08E+02 2.00512E+01 2.14435E+01 9.8169 6E 1.462E+04 2.816E+04 1-m' % if;n ,.- , r, , wy x( .Q,gq3,,3 i i l &%% % , "'l #w. JI.b km 4 n Mm
- n, m . .
no,, n , , amm amww
..m . . . . ... , . . . . . - ..
Ta'ole 2.1.4.8 Lower Partial Asambly Core Loading
.- Pin Geometry. PWer. and Burnup Distributions 4
Assembly 6 Fin Power Set l'. Relative ROC EOC Pin Burnup Burnup
-I Leit' . E Eight- Y Bot Y Top Power (MND ) DefD )
1.07425E+02 1.008575+02 0.00000E+00 1.43223E+00 1.098893+00 1.462E+04 2.816E+04 1.07425E+02.1'00857E+02 1.43223E+00 2.064465+00 1.07640E+00 1.462E+04 2.8165+04 1.07425E+02 1.088575+02 2.064465+00 4.29669E+00 1.041065+00 1.462E+04 2.016E+04 1.07425E+02-1.088575+02-4.29669E+00 5.72892E+00 1.03142E+00 1.462E+04 2.0165+04 1.07425E+02 1.098575+02 5.72092E+00 7.16115E+00 0.00000E+00-1.462E+04 2.016E+04 , 1.07425E+02 1.008573+02 7.16115E+00 0.593385+00 1.01214E+00 1.462E+04 2.816E+04 1.07425E+02 1.088575+02 8.59330E+00 1.00256E+01 9.89647E 01 1.462E+04 2.816E+04
-1.07425E+02 1.080573+02 1.002565+01 1.145785+01 9.80007E 01 1.462E+04 2.416E+04 1.07425E+02 1.00057E+02 1.14578E+01 1.28901E+01 9.83220E 01 1.462E+04 2.816E+04
-1.07425E+02 1.00857E+02 1.28901E+01 1.43223E+01 9.992063 01 1.462E+04 2.816E+04 1.07425E+02 1.00957E+02 1.43223E+01 1.57545E+01 0.00000E+00 1.462E+04.2.016E+04 1.07425E+02'1.08057E+02 1.57545E+01 1.71868E+01 9.96073E 01 1.462E+04 2.816E+04 1.07425E+02~1.08057E+02 1.71868E+01 1.06190E+01 9.80007E 01 1.462E+04 2.816E+04 1.07425E+02 1.08857E+02 1.86190E+01 2.00512E+01 9.70368E 01 1.462E+04 2.816E+04 1.07425E+02 1.00857E+02 2.00512E+01 2.14835E+01 9.159585 01 1.462E+04 2.816E+04
- 1.08857E+02 1.10289E+02 0.00000E+00 1.43223E+00 1.13745E+00 1.462E+04 2.016E+04 1.08857E+02 1.10209E+02 1.43223E+00 2.06446E+00 1.05712E+00 1.462E+04-2.816E+04 1.08857E+02 1.10289E+02 2.86446E+00 4.29669E+00 1.01535E+00 1.462E+04 2.816E+04 1.08857E+02 1.10289E+02 4.296695+00 5.72892E+00 1.06355E+00 1.462E+04 2.816E+04 1.00057E+02 1.102895+02 5.72092E+00 7.16115E+00 1.05070E+00 1.462E+04 2.015E+04 1.008575+02 1.10289E+02 7.16115E+00 0.59330E+00 1.03463E+00 1.462E+04 2.036E+04 1.00057E+02 1.10289E+02 8.5933 8E+00 1.00256E+01 1.02178E+00 1.462E+04 2.816E+04 11.08857E+02 1.10289E+02 1.00256E+01 1.14570E+01-1.01856E+00 1.462E+04 2.816E+04 1.00857E+02 1.10289E+02 1.14578E+01 1.28901E+01 1.01535E+00 1.462E+04 2.016E+04
.1.00857E+02.1.10209E+02 1.20901E+01 1.43223E&.01 1.021785+00 1.462E+04 2.916E+04 1.00857E+02 1.102695+02 1.43223E+01.l.57545E+01 1.02020E+00 1.462E+04 2.816E+04 1.088573+02 1.10289E+02 1.57545E+01-1.71864E+01 1.02020E+00 1.462E+04 2.816E+04 1.08857E+02-1.10289E+02 1.718685+01 1.86190E+01 9.57515E 01 1.462E+04 2.816E+04 1.00057E+02 1.102895+02 1.86190E+01 2.00512E+01'9.54302E 01 1.462E+04 2.016E+04 1.08857E+02 1.10289E+02 2.00512E+01 2.14835E+01 9.47876E-01 1.462E+04 2.816E+04 1.10289E+02 1.11722E+02 0.00000E+00 1.43223E+00;1.13102E+00 1.462E+04 2.816E+04 D1.10289E+02 1.11722E+02 1.43223E+00 2.86446E+00 1.04748E+00 1.462E+04 2.016E+04 1.10289E+02 1.11722E+02.2.86446E+00 4.296,69E+00 1.00571E+00 1.462E+04 2.816E+04 1.102893+02 1.11722E+02 4.29 669E+00 5.72892E+00 1.03142E+00 1.462E+04 2.816E+0d.
; 1.10289E+02 1.11722E+02 5!72892E+00 7.16115E+00 1.00093E+00 1.462E+04 2.816E+04 1110289E+02 1.11722E+02 7.16115E+00 8'.59330E+00 9.96073E 01 1.462E+04. 2.8165+04
~1'.10289E+02 1.11722E+02 8.59330E+00 1.00256E+01 9.92060E 01 1.462E+04 2.816E+04 1.102895+02 1'.11722E+02 1.002565+01 1.145785+0119.093185 01 -1.462E+04 : 2.816E+04
.1'.10289E+02 1~.11722E+02 1.14578E+01 1.20901E+01 9.89647E 01-1.462E+04.2.816E+04 x Vikl0289E+02 31111722E+02'1.28901E+01.1.43223E+014 9 6864335 01 1.462E+04 2.8165+04
-1.10289E+02 I1 11722E+02 1.43223E+01 1.57545E+01 9.89 647E-01 1.462E+04 2.816E+04 l'.10289E+02.1.11722E+02 1.57545E+01 1.7106SE+01L9.99206E 01:1.462E+04 2.816E+04'
%,1.10289 3+02 ,1' 11722E+02 . 1.71060E+01.1.0619 0E+01' 9.54302E 0111.46 2E+04 ; 2.816E+04 ~
. . D5 1.10289E+02'1.11722E+02 1.06190E+01 2.00512E+01.9.44663E 01:1.462E+04c2.816E+04 w % m is1020,s402 1.11722s+02 2.00512E+01(2.14835E+0t!s;41449a elft;4saswosisjstss+0,4j
.,.[ k 'tj8 *
.h ' -
t 1 y.f[ [ [, i A. n r.
" W, % p .
e4Q& %$ y;Wyy ~
,q
. m yp&;Q. - y . Q&&9l ,
nNkh?k$dMM9tWM N$N a> MINQf *'NNNNN M i ~ A ;
Table 2.1.4.8 o Lower Partial Asambly Core Loading Pin Geosotry, Power, and Burnup Distributions (cont'd) Asstably 6 Fin-Power Set 11 Relative BOC EOC Pia Burnup Burnup X Left. E Right Y Ect Y-Top Power (MND ) (MND ) 1.11722E+02 1.13154E+02 0.00000E+00 1.43223E+00 1.1374fE+00 1.462E+04 2.016E+04 1.11722E+02 1.13154E+02 1.43223E+00 2.06446E+00 1.11496E+00 1.462E+04 2.016E+04 1.11722E+02 1.13154E+02 2.864463+00 4.29669E+00 1.05070E+00 1.462E+04 2.016E+04
,1.11722E+02 1'.13114E+02 4.296695+00 5.72092E+00 1.00893E+00 1.462E+04 2.016E+04 1.11732E+02:1.13154E+02 5.72092E+00 7;16115E+00 9.532203 01:1.462E+04 2.0165+04 1.11722E+02.1.13154E+02 7.16115E+00 8.59323E+00 9.735815 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 8.59330E+00 1.002565+01 9.73501E 01 1.462E+04 2.Ol6E+04 1.11722E+02 1.13154E+02 1.00256E+01 1.14578E+01 9.735815 01 1.462E+04 2.815E+04 1.11722E+02 1.13154E+02 1.145783+01 1.20901E+01 9.67155E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.28901E+01 1.43223E+01 9.63941E 01 1.462E+04 2.016E+04 1.11722E+02 1.13154E+02 1.43223E+01 1.57545E+01 9.671553 01 1.462E+04 2.816E+04
' 1.11722E+02 1.13154E+02 1.57545E+01 1.7106tE+01 9.767943 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.71068E+01 1.86190E+01 9.92860E 01 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 1.06190E+01 2.00512E+01 1.00571E+00 1.462E+04 2.816E+04 1.11722E+02 1.13154E+02 2.00512E+01 2.14835E+01 9.51089E 01 1.462E*04 2.816E+04 1.13154E+02 1.14506E+02 0.00000E+00 1.43223E+00 0.00000E+00 1.462E+04 2.816E+04
_1.13154E+02 1.14506E+02 1.43223E+00 2.86446E+00 1.11175E+00 1.462E+04 2.816E+04 1.13154E+02 1.14536E+02 2.86446E+00 4.29669E+00 1.03463E+00 1.462E+04 2.816E,04 1.13154E+02 1.14506E+02 4.29669E+00 5.72892E+00 9.92060E 01 1.462E+04 2.816E+04 1.13154E+02 1.14506E+02 5.72892E+00 7.16115E+00 9.70360E 01 1.462E+04 2.816E+04 1.13154E+02 1.145065+02 7.16115E+00 0.59330E+00 9.6072OE 01 1.462E+04 2.816E+04 1.13154E+02 1.14506E+02 8.59338E+00 1.00256E+01 9.57515E 01 1.462E+04 2.816E+04 1.13154E+02 1.14506R+02 1.00256E+01 1.14578E+01 9.57515E 01 1.462E+04 2.816E+04 1.13154E+02 1.14556E+02 1.145783+01 1.209 01E+01 9.54302E 01 1.462E+04 2.816E+04 1.13154E+02 1.14586E+02 1.209 01E+01' 1.43 223 E*D1 9.543 025-01 1.462E+04 2. 816t+04 1.13154E+02 1;14506E+02 1.43223Ei01-1.57545E+01 9.57515E 01 1.462E+04 2.816E+04
- 1.13154E+02 1.14506E+02 1.57545E+01 1.71060E+01 9.63941'E 01 1.462E+04 2.816E+04 1.13154E+02 1.145063+02 1.71860E+01 1.86190E+01 9.000073 01 1.462E+04 2.816E+04 1.13154E+02 1.145065+02 1.86190E+01 2.00512E+01 1.00571E+00 1.462E+04 2.816E+04 1.13154E+02 1.14506E+02 2.00512E+01 2.14835E+01 0.00000E+00 1.462E+04 2.816t+04 1.14506E+02 1.160183+02 0.00000E+00 1.43223E+00 1.12460E+00 1.462E+04 2.016E+04
-1.145063+02 1.16010E+02 1.43223E+00 2.86446E+00-1.09560E+00 1.462E+04 2.016E+04 1.14506E+02 1.16018E+02 2.864463+00 4.29669E+00 1.02499E+00 1.462E+04'2.816E+04 1.14586E+02 1.16018E+02-4.29669E+00 5.72092E+00 9.03220E 01=1.462E+04 2.816E+04 1.145065+03 1.160185+02 5.72892E+00.7.16115E+00 9.639415 01:1.462E+04 2.016E+04
'1.14506E+02 1.16010E+02.7.16115E+00ft.59338E+00-9.57515E 01_1.462E+04 2.016E+04-1114506E402'1.16018E+02l8.5933tJ+00 1.00256E+01-9.57515E-01'1.462E+04 2.816E+04 1.145965+02 1.160183+02 1.00256E+01 1.14578E+01 9.57515E 01 1.462E+04-2.016E+04 11'.145865402# 1;16018E+02 1114578E+01 1.28901E+01 9.54302E 01'1.462E+04!2.816E+04 11.14586E+02 1.16010E+02 1.28901E+01 1.43223E+01 9.51089E-01.1.462E+04 2.816E+04
'1114596EkO2'li16010E+02"l'.'43223E+01 1~.57545E+01 9;51009E 01 12462EdO41 2.816t+04 1.14506E+02'1.16018E+02 1.57545E+01 1.71868E+01 9.60728E 0111.462E+04 2.816E+04 1~14556E+02 1.16018E+02 1.71868E+01 l'.06190E+01 9.73581E 0111.462E+04 2.Ol6E+04 na n-41.145865+02<1.'160183+02-1.86190E+01 2.00512E+01 9.96073E-01 1.462E+04;2.816E+04 c dialdfi &'.L15065+02 51'.16010E+02 2.00512E+01 = 2.1403 5E+01, 9.478765 0111.462E+04 l 2.8165+04 -
iwwwgeww<nrw ww , s w; ,
- w , we wwgpw > w -
r S- . g 4 , h kh~S W 2 i 'I - = N, t c* ;r V, a
- 4 p%;GMysWW we L m p; '
'M Nw, J Wl 4; n 3Op&pg@;&ggn
_ _ _ _ _ _ _ _ _ . _ . _ _ _ _ _ _ _ _ _ _ . - - _ , _ _ - -- ~ C p l Table 2.1 A8 i [ Lower Partial Asembly Core Loading
- Pin Geometry, Power, and'Eurnup Distributions (cont'd)
I i Assembly 6 Pin Power Set 11 i l Relative BOC EOC
- i. . .
Fin Burnup Burnup l I Left X Right Y Sot Y* Top Power 04WD ) (MWD ) i-1.160185+02 1.17451E+02 0.00000E+00 1.43223E+00 1.10211E+00 1.462E+04.2.816E*04 1.16018E+02 1.17451E+02 1.43223E+00 2.86446E+00 1.082O3E+00 1.462E+04 2.816E+04 ; 1.16010E+02 1.17451E+02 2.86446F+00 4.29669E+00 1.02178E+00 1.462E+04 2.816E+04 ' l 1.160185+02 1.17451E+02 4.29669E+00 5.72892E+00 9.83220E 01 1.462E+04 2.016E+04 l 1.160185+02 1.17451E+02 5.72892E+00 7.161153400 9.607285 01 1.462E+04 2.816E+04 l 1.160185+02 1.17451E+02 7.16115E+00 0.59338E+00 9.57515E 01 1.462E+04 2.016E+04 l- 1.16018E+02 1.17451E+02 8.59330E+00'1.00256E+01 9.67155E 01 1.462E+04 2.816E+04 i- 1.16010E+02 1.17451E+02 1.002565+01 1.14578E+01 9.73581E 01 1.462E+04 2.816E+04 l 1.15010E+02 1.17451E+02 1.14570E+01 1.28901E201 9.639415 01 1.462E+04 2.816E+04 i
- _ . 1.16010E+02'1.17451E+02 1.20901E+01 1.43223E+01 9.510095 01 1.462E+04 2.816E+04
-1.160185+02 1.17451E+02 1.43223E+01 1.57545E+01 9.51009E 01 1.462E+04 2.816E+04 L1.16018E+02 1.17451E402 1.57545E 01 1.71068E+01 9.60720E 01 1.462E+04 2.816E+04 I
[ 1.160185+02 1.17451E+02 1.71068E+01 1.8619 0E+01 9.76794E-01 1.462E+04 2.816E+04 l 1.16018E+02 1.17451E+02 1.86190E+01 2.00512E+01 9.89647E 01 1.462E+04 2.816E+04 [ 1.16018E+02 1.17451E+02 2.00512E+01 2.14835E+01_9.31010E 01'1.462E+04-2.816E+04 1.17451E+02 1.18883E+02 0.00000E+00 1.43223E+00 1.09568E+00-1.462E+04 2.816E+04 i 1.17451E+02 1.19803E+02 1.43223E+00 2.06446E+00 1.07961E+00 1.462E+04 2.816E+04 lj 1.17451E+02 1.18883E+02 2.86446E+00 4.29669E+00 9.41449E 01 1.462E+04 2.816E+04 { 1.17451E+02 1.10083E+02 4.296693+00 5.72092E+00 9.03220E 01 1.e62E+04 2.016E+04 [- - 1.17451E+02 1.10003E+02 5.72892E+00 7.16115E+00 9.60728E 01 1.462E+04-2.816E+04 l 1.17451E+02 1.19803E+02 7.16115E+00 9.5933OE.', 9.57515E 01 1.462E+04 2.016E+04 - 1.17451E+02 1.18803E+02 0.59330E+00 1.00256E+01 9.73501E 01 1.462E+04 2.016E+04 1.17451E+02.1.18003E+02 1.00256E+01 1.14570E+01 0.00000E+00 1.462E+04 2.016E+04 l
-1.17451E+02 1.19803E+02 1.145785+01 1.20901E+01 9.73501E 01 1.462E+04 2.816E+04
- 1.174515+02 1.18883E+02 1.28901E+01 1.43223E+01 9.54302E 01 1.462E+04 2.816E+04 l
1.17451E+02 1.19803E+02 1.43223E+01 1.57545E+01 9.51089'E 01L1.462E+04 2.815E+04
-1.17451E+02 1.19803E+02 1.57545E+01 1.71860E+01 9.639415 01 1.462E+04 2.0165+04
- ~ 1.17451E+02.1.19883E+02 1.71068E+01 1.86190E+01 9.06105E=01 l'.462E+04 2.016E+04.
-1.17451E+02.1.10803E+02 1.86190E+01 2.00512E+01 9.86433E 01 1.462E+04 2.816E+04
--1.17451E+02 1.18083E+02 2.00512E+01 2.14035E+01 9.28597E 01 1.462E+04 2.816E+04 1.19803E+02 1.20315E+02 0.00000E+00 1.43223E+00 1.09560E+00'1.462E+04 2.816E+04 1.18083E+02 1.20315E+02 1.43223E+00 2.86446E+00 1.07640E+00=1.462E+04 2.816E+04 1.18883E+02 1.20315E+02 2.86446E+00'4.29669E+00 1.01535E+00 1.462E+04 2.016E+04 l 1.18003E+02 1.20315E+02 4.29669E+00 5.72892E+00 S 76794E 01 1.462E+04 2.816E+04 l .1.19803E+02 1.20315E+02 5.72892E+00'7.16115E+00 9.57515E 01 1.462E+04 2.816E+04 1.18003E+02 1.20315E+02 7.16115E+00 8.59338E+00 9.54302E 0111.462E+04 2.816E+04 1.18883E+02,1.20315E+02 5.59338E+00 1.00256E+01 9.63941E 01'1.462E+04 2.816E+04 1.18083E+02:1.20315E+02al.002565+01:1.14578E+0159.70368E 01*1".462E+04T21016E+04 1.18883E+02 1.20315E+02 1.14578E+01'1.28901E+01 9.60720E 01 1.462E+04 2.816E+04 ^
F 11118883E+02c1.20315E+02"1.20901E+01'1.43223E+01?9.478762-01'1$4625404 2'.816E+04 d ^ 1.18083E+02,1.20315E+02 l'.43223E+01 1~.57545E+01 9.47876E-01 1.462E+04 2.816E+04 1.10083E+02 1.20315E+02 1.57545E+01 1.71868E+01'9.57515E 01 1.462E+04 2.816E+04 i 11.19883E+02 1.20315E+02"1.71060E+01 1.86190E+01 9.73581E 01.1.462E+04-2.816E+04
- . . ~l1. 188035402 1. 20315E+ 02-1. 86190E+ 01 2 00512E+01 9_.09647E 01.1;462E+04'2.8165+04
- 90%%2isseesseos;1sa031sE+on 2 00512E+0t< a 14835E+014 9:3ses33-ott114623404*sse16EiO4"
!' .m .
- % OAINNQ sm1 14#f a $W . ,. m6 ,ye , dY u . , , ,
%gn%%;gM - m w % w@gpmnnymMsw@y _ ,_ _ u _ _ - _ _
, _ _ _ _ _ - _ . - - _ ..,.1 m ar _ e Table 2.1.4.8 Lower Partial Asemaly Coat Loading Pin Geometry, Power, and Burnup Distributions (cont'd)
. Assembly 6 Pin Power Set 11
, Relative ROC EOC Pin Burnur turnup Z-Left- Z Right Y Bot Y Top Power DOC 3 ) (NWD )
1.20315E+02 1.217475+02 0.00000E+00 1.43223E+00 1.11175E+00 1.462E+04 2.Ol6E+04 1.20315E+02 1'.217475+02 1.43223E+00 2.06446t+00 1.08604E+00 1.462E+04 2.816E+04
'1.20315E+02 1.217475+02 2.06446E+00 4.29669E+00 1.01535E+00 1.462E+04 2.816E*34 1.20315E+02 1.217473+02 4.296693+00 5.72892E+00 9.73501E 01 1.462Rt04 2.816E+04 1.20315E+02'1.21747E+02 5.72892E+00 7.16115E+00 9.54302E 01 1.462E+04'2.016F+04 1.20315E+02 1.217475+02 7.16115E+00 8.59338Et00 9.47876E 01 1.462E+04 2.816E+04
-1.20315E+02 1.217475+02 8.593385+00 1.002565+01 9.51009E 01 1.462E+04 2.816t+04 1.20315E+02 1.217475+02 1.00256E+01 1.14578E+01 9.510895 01 1.462E+04 2.0163404 1.20315E+02 1.21747E+02'1.14570E+01 1.28901E+01 9.47876E 01 1.462E+04 2.01EE+04 1.20315E+02 1.21747E+02 1.289011+01 1.43223E+01 9.47076E 01 1.462E+04 2.81CE+04 1.20315E+02 1.217475+02 1.43223E+01 1.J7545E+01 9.47076E 01 1.402E+04 2.816E+04 1.20315E+02 1.21747E+02 1.57545E+01 1.71068E+01 9.57515E 01 1.462E+04 2.816E+04 -
1.20315E+02 1.21747E+02 1.71060E+01 1.86190E+01 9.73581E 01 1.462E+04 2.81GE+04 1.20315E+02 1.21747E+02 1.06190E+01 2.00512E+01 9.96073E 01 1.462E+04 2.A16t+04 1.20315E+02 1.21747E+02 2.00512E+01 2.14835E+01 9.51089E 01 1.662E+04 2.816E+04 1.21747E+02 1.23180E+02 0.00000E+00 1.43223E+UO 0.000004+00 1.462E+04.2.916E+04 .
'1.217475+02 1.23180E+02 l'.43223E+00 2.06446E+00 1.09568t+00 1.462E+04 2.816E,04 1.21747E+02 1.23180E+02 2.86446E+00 4.29669E+00 1.02170E+00 1.462E,04 2.816E+C4 1.21747E+02 1.23100E+02 4.29669E+00 5.72892E+00 9.00007E 01 1.462E+04 2.816E+04 1.217475+02 1.23100E+02 5.72092E+00 7.16115E+00 9.607285 01 1.462E+04 2.816E+04 1.21747E+02 1.23100E+02'7.16135E+00 0.59338E+00 9.51089E-01 1.462E+04 2.816Et04 1.21747E+02 1.231SOE+02 0.59330E+00 1.00256E+01 9.51089E-01 1.452E+04 2.816E+04 1.21747E+02 1,23180E+02 1.00256E+01 1.14578E+01 9.510895 01 1.462E+04 2.816E+04 -
1.21747E+02 1.23100E+02 1.145785+01 1.289 01E+01 9.51089E 01 1.462E+04 2.816E+04 1.217475+02 1.23180E+02 1.28901E+01 1.43223E+11 9.51089E 01 1.462E+04 2.816E+04 1.21747M+02 1.23180E+02 1.43223E+01 1.57545E+01 9.543 02E 01 1.462E+04 2.816E+04 1.21747E+02 1.23180E+02 1.57545E+01 1.7186SE+01 9.639415 01 1.462Et04 2.816E+04 1.21747E+02 1.23100E+02 1.71868E+01 1.8619 0E+01 9.03 220E 01 1.462E+04 - 2.816E+04
-1.21747E+02 1.23100E+02 1.86190E+01 2.00512E+01 1.00093E+00 1.462E+04 2.816E+04 1.217475+02 1.23180E+02 2.00512E+01 2.14835E+01 0.00000E+00 1.462E+04,2.01GE+04 l'.23180E+02 1.24612Eo02 0.00000E+00 1.43223E+00 1.11017E+00 1.462E+04.2.816E+04 1.23100E+02-1.24612E+02 1.43223E+00 2.864465+00-1.10211E+00 1.462E+04 2.514E+04
'1.23180E+02.1.24612E+02 2.86446E+00 4.29669E+00 1.03704E+00 1.462E+04 2.816E+04 1.23180E+02 1.24612E+02 4.29669E+00 5.72892E+00 9.96073E 01 1.462E+04 2.816E+04
-1.23100E+02 1.24612E+02-5.72092E+00 7.16115E+00 9.76794E 01 1.462E+04'2.815E+04 1.23180E+02L1.24612E+02=7;16115E+00ft.59330E+00 9.671553-0111.462E+0412.816E+04-1.23100E+02 1.24612E+02 S.593385+00 1.00256E+01 9.67155E 01 1.462E+04'2.816E+04 1.231SOE+02 1.24612E+02 1.00256E+01 1.145785+01-9.671553 0121.462E+04 2.8163+04-1.23100E+02 1.24612E+02 1.14570E+01- 1.289 01E+01 9.57155E 01 1.462E+04. 2.016E+04 11.23180E+02'1.24612E+02 1.28901E+0111.43223E+01 9.67155E 0141.462E+0'4:2.016E+04 1.23100E+02 1.24612E+02 1.43223E+01.1.57545E+01 9.70368E 01 1.462E+04 2.816E+04
.1.23180E+02 1.24612E+02 1.57545E+011 1.71868E+01 9.83220E-01'1.462E+04_2.816E+04 11'.23180E+02 1.24612E+02 1.71868E+01 1.86190E+01 9.99286E 01 1.162E+04~2.816E+04 nl.23100E+02'1.24612E+02'1.86190E+01:2.00512E+01 1.01535E+00.1.462E+04'2.816t+04 -
W & gt.331895+ Sac 14246133402<2.00512E+01524149353401i91607288401i1i4685e640340143+041< a - n ,
+
+w> .
% $ M Mid t @ st [ q . ~
,)j Q- {khh >}k M WM - J ' -
v +
%e@WWW%$ @WWw
4 1-Table 2.1.4.8 , Lower Partial Asambly Core Loading i Pin Geometry, Power,'and Burnup Distributions (cont'd) n , [ . Assembly 6 Pin Power Set 11 i l Relative ROC EOC . Pin. Burnup Burnup l E-Left- 1 Right - Y Bot Y Top _ Power (MWD ) . DOG) ) i f- 1.24612E+02 1.26044E+02 0.00000E+00 1.43223E+00 1.11496E+00 1.462E+04 2.8164+04 ! 1.24612E+02 1.26044E+02 1.43223E+00-2 96446E+00 1.03704E+00 1.462E+04.2.016E+04 l 1.24612E+02 1.26044E+02 2.064465+00 4.2966fE+00 1.02170E400 1.462E+04 2.916E+04 l- -1.24612E+0211.26044E+02 4.29669E+00:5.72092E+00 1.02020E+00,3.4623404 2.816E+04 s1.24612E+02 1.26044E+02'S.72892E+00=7.16115E+00 1.00093E+00 1.462E+04'2.0163+04 ( 1.246125402 1.26044E+0217.16115E+00 0.59338E600 9.992865*01 1.462E+04 2.016E+04 l 1~.24612E+02 1.26044E+02 0.59330E+00 1.00256E+01 9.96073E 01 1.462E+04 2.016E+04 l 1.24612E+02.1.26044E+02 1.00256E+01.1.14570E+01 9.350235 01 1.462E+04 2.016E404 ! 1.24612E+02 l'.26044E+02 1.14570E+01 1.20901E+01 9.99206E 01 1.462E+04 2.016E+04 l 1.24612E+02 1.26044E+02 1.20901E+01 1.43223E+01.9.99206E 01 1.462E+04 2.016E+04 L l1.24612E+02 1.26044E+02 l'.43223E+01 1.57545E+01 1.00571E+00 1.462E+04 2.816E+04 ) . 1.24612E+02-1.26044E+02 1.57545E+01 1.71060E+01 1.01535E+00 1.462E404 2.816E+04 i 1.24612E+02 1.26044E+02 1.71068E+01 1.06190E+01 9.92060E-01 1.462E+04 2,616E,04 1 1-1.24612E+02 1.26044E+02 1.06190E+01 2.00512E+01 9.639415 01 1.462E+04 2.81GE*04 1.24612E+02 1.26044E+02 2.00512E+01 2.14835E+01 9.60720E 01 1.462E+04 2.816E+04 1.26044E+02 1.27476E+02 0.00000E+00 1.43223E+00 1.13102E+00 1.462E+04 2.016E404
-1.26044E+02 1.27476E,02 1.43223E+00 2.06446E+00 1.06034E+00 1.462E+04 2.816E+04
! II.26044E+02 1.27476E+02 2.06446E+00 4.29663E+00 1.J2499E+00 1.462E+04 2.816E+04 l 1.26044E+02 1.27476E+02 4.29669E+00 5.72892E+00 1.07640E+00 1.462E+04 2.016E+04 [ 1.26044E+02'1.27476E+02 5.72092E+00 7.16115E+00-1.06355E+00 1.462E+04 2.016E+04 1.26044E+02 1.27476E+02 ' 7.16115E+00. 0.5933 0E+00 1.05070E+00 1.4,*2E+C4 2.816E+04 ! 1.26044E+02:1.27476E+02 0.59338E+00 1.00256E+01 1.04106E+00 1.462E+04-2.016E+04 l l1.26044E+02 1.27476E+02 1.00256E601 1.14570E+01 1.04106E+00 1.462E+04 2.016E+04 l' 1.26044E+02.1.27476E+02 1.14570E+01 1.28901E+01 1.04427E+00 1.462E+04 2.816E+04 l 1.26044E+02 1.274763+02 1.209 01E+01.1.43223E+.61 1.05070E 600 1.462E+04 2.816E+04
.1.26044E+02 1.27476E+02 1.43223E+01 1.57545E+01 1.06355E+00 1.462E+04 2.8163+04 1.26044E+02 1.27476E+02 1.57F45E+01'1.71860E+01 1.06355E+00 1.462E+04 2.01GE+04 1.26044E+02 1.274765+02 1.71860E+01:1.8619 0E+01 ' 9.9 6073E 01 1.462E+04 2.016E+04 .
i 1.26044E+02 1.27476E+02 1.86190E+01 2.00512E+01'9.92060E 01 1.462E+04 2.816E+04 1;25044E+02~1.27476E+02 2.00512E+01 2.14035E+01 9.03220E-01 1.462E+04 2.016E+04
.1.27476E+02.1.20908E+02 0.00000E+0011.43223E+00 1.10532E+00~1.462E+04 2.016E+04 1 II.27476E+02 1.20900E+02:1.43223E+00 2.06446E+00 1.09889E+00 1.462E+04 2.018*M4 L 1.27476E+02 1.20900E+02-2.864463+00.4.29669E+00 1.06990E+30 1.462E+04 2.016m;0.;
~
.1.27474E+02 1.28900E+02 4.29669E+00 5.72092E400 1.06355E+00 1.462E+04 2.816E+04
. 1.27476E+02 1.20900E+02 5.72092E+00 7.16115E+00 0.00000E+00 1.462E+04 2.816E+04 1
1'.274763402 1.28900E+0217.16115E+00 8.59330E+00.1.04740E400+1;4622404 2.816E+04
~
l 1.274765+02 1;20900E+02 0.593385+00.1.00256E+01 1.03463E+00 1.462E+04 2.816E+04 L = 11.274763+02"1.20900E+0211'00256E+01il.145785+01 . 1.02020E+0041.462E+04 2.816E+04 i 1.27476E+02 1.20900E+02.1.14578E+01 1.20901E+01 1.03463E+00 1.462E+04 2.816E+04
- *s' 4 1'.'27476E402'1L20900E+02 I1'.289 01E+01* 1i43223E+01"1.050702400 t11462E404 2 5 016E+34 IT 11.27476E+02
- 1.20900E+02'1.43223E+01 1.57545E+01 0.00000E+00-1.462E+04 2.816E+04. '
l' yrs <1.27476E+02il.20900E+02 1.57545E+01 1.71860E+01 1.05391E400 1.462E+04 2.016E+04 L ,
;1,27476E+02;1.20900E+02'1.71060E+01 1.06190E+01 1.04427E+00-1.462E404 2.016E+04=
. .T a 1'.274763+0U 1.20900E+02 1.0619OE+01 2.00512E+01:1.03704E+00si'.462E+04.2.8163+04. ' 4@NMl OS94WWst2 1128900E+02? ? 2100512E+01Y211493SE+0119'.832203;4111*.'462S+04 4 2itT0t+04" i@ g ghAbgbMpA wp-e , - fJ, , , m m.x '< 'w yu dd[h[df%; 4 O GQd#MQ UIi a +;
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7 Table 2.1.4.9 l Upper Partial Asrserbly Core Loading Axial Power Distributions Zone Radial Zone Axial Boundary 1 2 3 4 0.0000E+00 0.0000E+00- 0.0000E+00 0.0000E+00 0.0000E+00
- 1. 1.3970E+01 0.0000E+00 0.0000E+0S 0.0000B>00 0.0000E,00 2- 2.7381E+01 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 3 4.0792E+01 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 4 5.4204E+01 0.0000E+00 0.0000E+00 0.0000E400 0.0000E+00 5 6.7615E+01 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 6 8.1026E+01 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 7 9.4437E+01 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E400 8 1.0785E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000W+00 9 1.0910E+02 S.4211E 02 5.3658E-02 5.4819E 02 4.2657E 02 10 1.2126E+02 5.9469E 02 5.882CE 02 6.0141E 02 6.0467E-02 11 1.3467E+02 5.9304E 02 5.8727E-02 5.9965E-02 6.0590E 02 12 1.4808E+02 5.9304E-02 5.8837E-02 5.9954E-02 6.0566E 02 13 1.6149E+02
- 5.9414E 02 5.9014E 02 6.0020E-02 6.0575E 02 14 1.7490E+02 5.9469E-02 5.9157E 02 6.0031E 02 6.0558E 02 15 1.8832E+02 5.9414E*02 5.9124E 02 5.9910E-02 6.0504E 02 16 2.0173E+02 5.9249E-02 5.8970E 02 5.9679E 02 6.0423E 02 17 2.1514E+02 5.9029E-32 5.8782E 02 5.9415E-02 6.0362E-02 18 2.2855E+02 5.8864E 02 5.8650E 02 5.9184E 02 6.0272E-02 19 2.4196E+02 5.8809E-02 5.8595E-02 5.8998E 02 6.0158E 02
-20: 2.55375+02 5.8699E 02 5.8540E-02 5.8723E-02 5.9670E 02 21 '2.6878E+02 5.8204E 02 5.8186E 02 5.8008E-02 5.8885E 02 22 2.8219E+02 w @rhi&#MA : a -
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, , . . , . . . . . . - . , . . g- .- -.. . . - -- -- i Table 2.1.4.9 Upper Partial Aussembly Core Loading Axial Power Distributions (Cont'd) Eone Radial Zone Axial Boundary 1 2 3 4 22 2.8219E+02 5.6829E 02 5.7083E 02 5.6458E 02 5.7019E 02 23 2.9561E+02 5.1133E 02 5.4667E 02- 5.34135 02 5.4180E-02 24 3.0902E+02 4.9512E 02 5.0375E 02 4.8445E 02 4.8655E 02 25 3.2243E+02
- 4.2235E02 4.3855E 02 4.1200E-02 4.1559E-02 26 3.3584E+02 '
3.3448E 02 3.4952E 02 3.1637E 02 3.2901E 02 27 3.4925E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 28 3.8211E+02
. Zone Radial Radial Zone Boundary 1 107.175 2 128.610 3 150.040 4 184.461 i
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l Table 2.1.4.10 Lower Partial Asssorr.bly Core Leading { Axial Power Distributions Zone Radial Zone Axial Roundary 1 2 3 4 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 1 1.3970E+01 9.5272E 02 9.87303-02 9.16573-02 8.3606E 02 2 2.7381E+01 i 1.2078E 01 1.2309E 01 1.1872E 01 1.1306E 01 i 3 4.0792E+01 1.3939E 01 1.4050E-01 1.3873E 01 1.3594E 01 4 5.4204E+01 1.5141E 01 1.5124E 01 1.5196E 01 1.5218E 01 3 6.7615E+01 1.5186E 01 1.5648E 01 1.5922E-01 1.6230E 01 6 0.1026E+01 1.6020E 01 1.5799E 01 1.6216E 01 1.6759E 01 1.6020E 01 1.573BE-01 1.6245E-01 1.6948E 01 0 -1.0785E+02 1.4890E 02 1.4594E 02 1.5188E 02 1.5039E 02 9 1.0910E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 10 1.2126E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 11 1.3467E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 12 1.4800E+02 0.0000E+00 0.0000E+00 0.0000E+00
- 0.0000E+00 13 1.6149E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 14- 1.7490E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 15 1.8832E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 16 2.0173E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 17 2.1514E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 18 2.2855E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 19 -2.4196E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E,00
~20 "2.5537E+02' O.0000E+0C 0.0000E+00 0.0000E+00 0.0000E+00 21 3.687OE+02
.' O.0000E+00 0.0000E+00 0.0000E+00 050000E+00 22 2. 8219E+02
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7 . . . . , . Table 2.1 A.10 Lower Partial Assstably Core Loading Axial Power Distributions (cont'd) Zone Radial Zone Asial Soundary 1 2 3 4 22 2.8219E+C2 0.0000E+00 0.0000E+00 0.0000E+00- 0.0000E+00 23 2.9561E+02 , r 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 24 3.0902E+02 0.0000E+00- 0.0000E+00 0.0000E+00 0.0000E+00 25 3.2243E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 8 26 3.3584E+02 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 ' 27 3.4925E+02 O.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 28 3.8211E+02 Zone Radial Radial zone Boundary 1- 107.175 2 128.610 -' e n- - u, . . -o. , s ' 150.040' 3-4 184.461
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Table 2.1.4.11 Partial Length Shield Assembly Core Loading Edit Locations
. Edit R (ca) E(ca) 9 (degrees) .
. Pressure Vessel Inner 0 d .
. Low Wold Location .
. - (a) Flumes and DPA Rates 219.393 67.1040 0-45 .
. (b) Reduction Factors 219.393 67.1040 0 45 .
l
+The inner wall (0 T) edit was taken at the center of the mesh block immediately laside the vessel.
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Assembly :"..E?.:
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i Os ' g , . :o Detail A PressureVessel .sr o.. Bklogical
?+
.[ Y-T@'
n ThermalShield
\e x *D.
Shield t
\ x x .. :::o. f (Concrete)
X-Left :- X-Right \ \ i: y Core B'~' %\ s .
.x x . -
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t Y-Bottom
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c3 N 03 (O G3 A N m i 4 -- Nele: AH Dimensionsin cm. ammmm m m 8 . e .. Low Leakage Core Loading Figure 2.1.3.1 , L s. e-m
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; n
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sules '".Q
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+ #. g ' y gqggg 3 y g
- y. Nels: All Dimensions in cm. gwmmm m m o 2 , ; ,
Location of Surveillance Capsules j y ;, Figure 2.1.3.3 W
, w -y y- - . m y - x . - - - - --- .1--- -m1 . . . . ,. , , ,
e i a O O1g Gjl.l g,Q - s.m w r
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, . " - - ' ~ s Surveillance Capsule-Figure 2.1.3.4
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- f. Detail A o -
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J.: Shield Thermal Shield 4 -- n .
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. /(Concrete)
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03 -%8 OD @ C43 A N un r: ;;; m m m m m = o w1-M Note: All Dimensions in cm.
.. ,et
- e. a e /-;s F
m Partial Length Shield Assembly Core Loading
- Figure 2.1.4.1 j
la Case 3 318 tuer
. . . = . .,
ReactorVessel N7 s-Thermal Shield >- Core Barrel > N, ?. =
= .
Core Baffle = l s i e >' I ll ll , '! s a
= r a .:
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= =
, = = .
= = ..
Shield Zone \
~"
s... i 9 -
\ . l l N .
i i- :[ N 4 . l if 109.102 cm
\ k! ! ! $$ Lower Girth
\ :((i ! (u ! h Weld
% s: i !
i
= =
67.1048 cm m
= =
w e s c s. Bottom of Core--> I '* a
!s j< -13.97 cm
. ys PLS Assembly \i s. g g:
NM Partial Length Shield Assembly Core Design - Figure 2.1.4.2 wMsh&gk.apiW;<j;W, mm A m cm e oqw,d% 9 yy c .mpyw p py~;< , , . my myy, n.jymy?.t;mn ;,
;w,gm
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382.115 -- 4 349.25 3 6 7 8 9 10 11 12 13 14 15 16 _17 18 109.102 2 5
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13.97 1
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- 6. - g g o -gy gm uG-Note:M Dimensionsin cm. 3E. .
. Partial Length Shield Assembly Core Loading Axial Geometry at 0=0*
Rgure2.1.4.3 L 'r T E l l'
.,. (
- Y + "
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Figure 2.2.2.1 BWR Planar Geometry Insulation f Y Top Ingatlon i ' . .. O, ppy l0; uner '. 6 . X Left * > X Right i o Outer Core
" Boundary Riser -
g, Y Bottom Inner Core .*. Jet . . Boundary \ Pump p
] Shroud Downcomer v {. $g5 th
{ (( Reflector gump 3. N k 000 ((C 0 Q) .
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aei ump . a u is @D -
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31 , s b '. < . MB -
@T 7116 7+ s Capsule / $ $
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Figute 2.2.2.2 BWR Axial Geometry SHROUD INSULATION o - 813.23
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CORE PLATE / v.'F 12.39 -.
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- 9 8 E RR n W RM E $
INLET a n a gp 88 WRW n g nM W
, m, NN
~%gr4m % m u.w u , 4 , -
-o RADIUS (cm)1 m .. .y
. wwe m Anolmunionsincm . ~ . n ,. o .~ , ,, n % ,
? ~+' .
_ . . . ;;: n , noi; (;; Tv%ijKwt73 j.3 . 'L~ '
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i , jc-- ;g ; ' t fg , 9
k Figure 2.2.2.3 Surveillance Capsule
< 3.10 cm >
/
. a Core E
o e Capsule = m. SS-304 Water N '[ f- 1h r '.t' % p'# 4" ^. ;T 4 I
- fp $8 h'gyh yrf[fyg/f i) Ap[ I f, {,{ g g3./ p 4 - x + F i. h '
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' . =
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Table 2.2.1.1
, Fraction of Fissions by Isotope as a Function of Raposure Raposure U+235 U+230 Fu.239 Fu241 (Nwd/T) 4.33 0.7651 0.0733 0.1566 0.
5.92 0.7190 0.0733 0.1936 0.0059 6.63 0.7005 0.0733 0.2096 0.0074 11.13 0.6153 0.0766 0.2014 0.0320 14.12 0.5630 0.0766 0.3330 0.0373 - 15.66 0.5370 0.0766 0.3400 0.0440 i 17.00 0.5070 0.0766 0.3500 0.0533
-j/O drf['M$f_tff g{ (,7 *. //,Q'M *# f - , h h- y - ' f f.4 ij g.,p *
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Table 2.2.2.1 Basic Design Data
. Reactor Parameter . Material .
! . Thermal Power 3833 MW(TN) .
. Core Inlet Temp. 270.9 C .
. Core Operatins Pressure 7.20 MPa .
. Core Saturated Temp. 207.7 C .
1 . Inner Radius of Shroud 270.2075 on . .. .
. Shroud Thickness 5.00 on . 88 304 .
4 321.31 om
. Inner Radius of Liner RFV .
. . Thickness of Liner 0.476 cm . 88 304 . l . ..................................................................,
. Inner Radius of RFV 321.706 cm .
. RFV Wall Thickness 16.129 on . Steel .
i . Inner Radius of Insulation Liner 351.79 on . 88 304
. Thickness of Insulation Liner 0.159 on . .
. Thickness of Insulation 0.571 cm . Al .
. Inner Radius of Concrete Shield 436.00 as .
. Thickness of Concrete Shield
- 40.62 on .
. Radius of Center of Jet Pump & . .
l l
. Riser to Core Center 293 on . .
l
. Number of Jet Pumps 24 .
. Location of Jet Pump Every 15 dog, of Circumference .
l ..................................................................., j . Location of Risers Every 30 dog. of Cirouaterance . I l . . Jet Pump ID 18.212 om . i - ...................................................................,
. Jet Pump Op 20.752 on .
= ,...................................................................
i . Riser ID 28.40 on .
. Riser 00 28.245 on .
y.g Capsule Total. Widths ,.,g 8.38,am y .;, . , , 3 e Ll g y .4.J : Radial Thioksess 3.10 as . Stool, _' .
++n.9tc;;............................................................ses...,< -
l
- *' The thiokness used ta~oalculation .
s .: .i , [ M k. h_. R 53 ( l-lh$dh MsQMkh h hED$1f"&Jk;ivbf}hd '4 'U'*' EI 'b4" 'Ad' -' # ihib bMO d
}
Table 2.2.2.2 Core and Fuel Assemblies
. Total Number of Fuel Assemblies 800 .
. Number of Fuel Rods per assembly (II8) 62 .
. Number of Water Rode 2 .
. Channel Boa Outer Width 13.8557 cm .
. Thickness of Channel 0.3040 cm .
. Som ,
. Assembly Pitch 15.25 cm .
. Fin Pitch 1.61544 cm .
. Cladding Mate'lal Er .
. Fuel Active Length 381.0 cm .
Basic Design Data Upper and Lower Reflectors .
. Region Neight Material .
. Lower Reflector .
. Inlet Region ,12.39 cm SS 304, Sat. water,Er .
. Core Plate 37.04 cm SS.304, Sat. water .
. Upper Reflector .
. Top Guide 37.03 cm 70% void water,Er .
. Upper Reflector 18.52 cm 88 304,70% void water,Er.
Steam separation a 327'.24,. ,om , 70% void wat,er
. =.
. gu 7 r . -
.. Dryer Regionf ' '
. ;_,,. .m,...........................................................,........c.+r-t g 4 is J 'h- v' h . .'
d
~
4 'h B 7 .f. 1,. ,% . ' f p. / ' ' t ' f 4 : . 7
e 4 e 1 i Table 2.2.2.3 j l Material Compositions '
. Misture Component Aton Densities .
. (aton/b* ca) .
. M 2.74760E+02 .
. 0 1.27300E+02 .
. Inner Core 1 0 (fuel) 1.44830E 02 .
. U 235 1.31490E*04 .
. U 238 7.10000E*03 .
. Er 4.95070E 03 .
. M 2.468205 02 .
. 0 1.23410E*02 .
. Inner Core 2 0 (fuel) 1.44830E 02 .
. U 235 1.314805 04 .
. U+230 7.10000E*03 .
. Er 4.950705 03 .
. M 1.76560E 02 .
. 0 0.820005 03 .
. Inner Core 3 0 (fuel) 1.44030E*02 .
. U.235 1.31480E 04 .
. U 230 7.10000E 03 .
. Er 4.958703 03 .
. M 1.32120E.02 .
. 0 6.60580E.03 .
. Inner Core 4 0 (fuel) 1.44030E.02 .
. U.235 1.31400E*34 .
. U 238 7t10000E*03 .
. Er 4.95870E*03 .
. M 1.0J110E*02 .
. 0 5.15540E 03 .
. Inner Core 5 0 (fuel) 1.44030E 02 .
. U 235 1.31400E 04 .
. U 238 7.100005 03 * .
. Er 4.95070E 03 .
. M 8.44790E+03 .
. 0 4.22400E*03 .
Inner Core 6' O (fuel) 1.440305 02 .
. U+235 1.314005 04 .
. -U 230 7.108805 03 .
. Er 4.95070E 03 .
Mpbyg. 4 -: t# , . o. ' ,
, <+4 a:-*Aa7e lo s %-J Ei! [y h 4 4 U< ,A ?- ~# ,- ** .'<
s - 4 a 5 ;y} , ( e j h., 3 4 Lg y .jh w ura, ~ c G' -- giQl 5%_.sLQ QV;kOf%$ki$f a n * ;-*
Table 2.2.2.3 Material compositions (Cont'd)
. Mixture Component Aton Densities .
. (ston/b*cs) .
. M 7.25039E 03 .
. 0 3.62520E 03 .
. Inner Core 7 0 (fuel) 1.440305 02 .
. U 235 1.31480E 04 .
. U 230 7.108605 03 .
. Er 4.95870E 03 .
. N 2.74760E.02 .
. 0 1.370905 02 .
. Outer Core 1 0 (fuel) 1.44030E 02 .
. U.235 1.314005 04 .
. U 239 7.10000E.03 .
. Er 4.950705 03 .
. N 2.74320E 02 .
. O 1.37160E 02 .
. Outer Core 2 0 (fuel) 1.44030E 02 .
. U 235 1.314007 04 .
. U 238 7.10080E 03 .
. Er 4.95570E 03 .
. H 2.514805 02 .
. 0 1.25740E 02 .
. Outer Core 3 0 (fuel) 1.44030E 02 .
. U 235 1.31400E 04 .
. U 230 7.100005 03 .
. Er 4.95870E 03 .
. H 2.10360E 02 .
. 0 1.05180E 02 .
. Outer Core 4 0 (fuel) 1.44830E 02 .
. U 235 1.31450E 04 .
. U 238 7'.10000E 03 .
. Er 4.95870E 03 .
. R 1.60310E 02 .
. O O.41550E 03 .
. Outer Core 5 0 (fuel) 1.448305 02 .
. U 235 1.314005 04 .
. U 230 7.108805 03 .
. Er ,
4.95070E 03 . 6 h N ~gf l , ~f ' h k { &-% ; Y N 9. p -- V l 4 j j Q-.[ s
.f? T- ^' ; & 4 9 ,
}. - .f w, t - p,b , 0 - g ;. ,,, , ,g y g-sypp y p ;g g;
, . 5 ,
'v,
)h 1-i , s a
. A ;., y , g ,q 7 4 -
-3 ee.cpe pp. e-c,. t _ r _ yg jg gpj,,qg g.,,gj pjg#p.p , .,,
Table 2.2.2.3 Material Compositions (Cont'd)
. Mixture Component Atom Densities .
. (atos/b* ca) .
. N 1.38750E 02 .
. 0 6.93850E+03 .
. Outer Core 6 0 (fuel) 1.44030E*02 .
. U 235 1.314805 04 .
. U 238 7.100005 03 .
. Er 4.95870E+03 .
. M 1.262605 02 .
. 0 6.31310E*03 .
. Duter Core 7 0 (fuel) 1.440305 02 .
. U 235 1.31480E+04 .
. U 238 7.10000E 03 .
. Er 4.958705 03 .
. Inner Core 1 M 3.79930Ba02 .
. Water Gap 0 1.89965E 02 .
. Er 1.03750E 02 .
. Inner Core 2 E 3.73870E 02 .
. Water Gap 0 1.86935E 02 .
. Er 1.03750E 02 .
. Inner Core 3 H 3.58630E 02 .
. Water Gap O 1.79315E 02 .
. Er 1.03750E 02 .
. Inner Core 4 E 3.48990E 02 .
. Water Gap 0 1*.744955*02 .
. Er 1.037505 02 .
. Inner Core 5 E 3.42690E 02 .
. Water Gap 0 1.713453 02 .
. Er 1.03750E 02 .
. Inner Core 6 N 3.38650E 02 .
.. Water Gap O 1.693255 02 .
. Er 1.037505 02 .
. Inner Core 7 M 3.360603 02 .
. Water Gap 0 1.68030E 02 .
. Er 1.03750E 02 .
. Outar Core 1 M 3.799305 02 .
. Water Gap 0 1.899653 02 .
s s a, R- .! f n Er 1.03750E 02 . guesw 4, sye < . wyv , .%*p,--a4 ,.- g g.g . l 4 N\ - f q fy ? 7 4 4 1 ,, I [ f
%Mih We +. + *' W O* W W A W N b4b$ ?Y?WNW" A
J Table 2.2.2.3 Material Compositions (Cont'd) l
................................................................., l
. Mixture Component Aton Densities .
f
. (atos/b*ca) .
. Outer Core 2 N 3.79830E 02 .
. Water Gap 0 1.099155 02 .
. Er 1.037505 02 .
1
. Outer Core 3 N 3.74880E 02 .
. Water Gap 0 1.874405 02 .
. Er 1.03750E 02 .
. Duter Core 4 N 3.659605 02 .
. Water Gap 0 1.029005 02 .
. Er 1.037505 02 .
. Outer Core 5 , N 3.56840E 02 .
. Water Gap 0 1.784203 02 .
. Er 1.037505 02 .
. Outer Core 6 N 3.50430E 02 .
. Water Gap 0 1.752153 02 .
. Er 1.03750E 02 .
. Outer Core 7 N 3.47720E 02 .
. Water Gap 0 1.73060E 02 .
. Er 1.037505 02 .
. N 4.928405 02 .
. Reflector 0 2.46420E 02 .
. Cr 1.74000E 02 .
. Mn 1.520005 03 .
. Shroud NL 0.550005 03 .
. (88 304) Fe 5.830005 02 .
. C 2'.37000E 04 .
. Si 8.93000E 04 .
. Cr 1.740005 02 .
. Me 1.520005 03 .
. RFV Liner Ni 8.550005 03 .
. (35 304) Fe 5.030005 02 .
. C 2.370005 04 .
. Si 8.930005 04 .
t ; k } 'f 4 k d [Iie t; {q .ip ' s -. B 4 ;. 4. . 4 f: 4 ,..y # F .[+ -- = li-- ,f
-- g ( g #
e . .
. ,"~i -
kN?i)fyM4Wdh$$t'htf (i U f i .; et 4 @ 4 g y@ pin @$jg(
- g; MSjt;Psid(%rphiliSMM-d
i l Table 2.2.2.3 Material Compositions (Cont'd)
. Mixture Component Atos Densities .
(stos/b* ca) .
. M 5.045505 02 .
. Downconer O 2.522803 02 .
. Cr 1.270005 04 .
. Mn / 1.12000E+03 .
. RFY Well Ni 4.440005 04 .
. (Steel) Fe 0.19000E+02 .
. C 9.810005 04 .
. Si 3.710005 04 .
. N 3.541505 02 .
.. O 1.770005 02 .
. Er 7.974705 03 .
. Cr 1.974905 03 .
. Inlet Region Mn 1.725205 04 .
. Fe 6.617055 03 .
. Ni 9.704253 04 .
. Si 1.01356E 04 .
. C 2.60995E 05 .
. N 4.66420E 02 .
. O 2.332105 02 .
. Cr 1.315445 03 .
. Core Flate Mn 1.14912E 04 .
. Fe 4.407403 33 .
. Ni 6.46380E 04 .
. Si 6 75100E 05 .
. C 1.791723 05 .
. M 1.21530E*02 .
. Top Guide 0 6.07670E 03 .
. Er 7.68960E 03 .
. E 9.822305 03 .
. 0 4.91120E 03 .
. Er 7.512505 03 .
Cr 2.015323 03.r ..
. Upper Reflector Mn 2.459365 04 .
. Fe 9.432945 03 .
. Ni 1.303395+04~ .
. 81 1.444075 04 .
. C 3.034665 05 .
'{ !
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i I l l Table 2.2.2.3 l l Material Compositions (Cont'd)
. Mixture Component Aton Densities .
. (s ton /b*ca) .
. N 1.478503 02 .
. Stoma Seperator/ Dryer 0 7.39260E*03 .
. Internal N 5.04550E*02 .
. Jet Pump Water 0 2.52280E*02 .
. Cr 1.55161E+02 .
. Jet Pump Nets 1 Fe 6.37862E.02 .
. Ni 6.895005 03 .
1
. Internal N 5.04550E 02 .
. Riser Water 0 2.52200E 02 . .
. Cr 1.551265 02 .
. Riser Metal re 6.524733 02 .
. Ni 6.894875 03 .
. Cavity 0 9.62000E 06 .
1.74000E 02
. Cr .
. Mn 1.520005 03 .
. Insulation Liner Ni 8.55000E+03 .
. (88+304)- Ps 5.8300PI 02 .
. C 2.370005 04 .
. Si 8.93000E*04 .
. Insulation A1 6,.06030E 03 .
. Concrete Wall .
. N 1.513675 02 .
. C 2.240325 04 .
. O O.53268E.02 .
. Na 2.045515 03 .
. Me 2.08319E*04 .
- . A1 4.655965 03 .
. Pi 3.077805 02 .
. K 1.350033 03, .
. Ca 4.461155 03 .
. Fa 6.097553 04 .
4 v 4 $ ': r Wh , 4 Ri h , ,
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+
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4 Table 2.2.2.3.1 Isotopic Fractions in Cr, Fe and Ni*
. Isofors . wr 4 . IsoTors . wr %' . IsoTops . WT % .
. Cr 50 . 4.345 . Fe+54 .. 5.9 . Ni+50 . 68.27 .
. . ..................................................s........
- . Cr 52 . 83.79 . Fe+56 . 91.72 . N1 60 . 26.10 .
d 1
. Cr.53- . 9.5 . Fe+57 . 2.1 . .N1 61 . 1.13 .
J
. Cr.54 .- 2.365 . Fe.50 . 0.20 . N1 62 . 3.59 .
i.
..... . ..... . ..... . ..... . wi.g4 . o,31 .
*Taken from Reference 4
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__- _ .m - _ . _ _ _ .____._____m _ Tabk 2.2.2.4 , l 1 Fuel Assembly Geometry and Power l Relative Asial Pin Assab. Assembly Burnup Peaking Power ! Number X Left I Right Y Bot Y Top Power + Group
- Factor set 1 1.15924 14.00176 1.15824 14.00176 5.0353e 030 1 1.000 0
)
2 16.39024 29.32176 1.15024 14.08176 1.0735e=02 1 1.000 0 3 31.63024 44.56176 1.15024 24.00176 1.0570e=02 1 1.000 0 ,
.4 46.07024 59.80176 1.15024 14.08176 1.1137e 02 1 1.000 0 5- 62.11024 75.04176 1.15824 14.00176 1.1007e 02 1 1.000 0 6 77.35824 90.20176 1.15024 14.00176 2.1072e 02 1 1.000 0 7 92.59024 105.52176 1.15024 14.08176 1.3563e 02 1 1.000 0 0 107.03024 120.76176 1.15824 14.00176 1.0017e 02 1 1.000 0 9 123.07024 136.00176 1.15024 14.00176 1.0795e=02 1 1.000 0 10 138.31024 151.24176 1.15024 14.00176 1.0763e=02 1 1.000 0 11 153.55024 166.40176 1.15024 14.09176, 1.3165e 02 1 1.000 0 12 168.79024 101.72176 1.15024 14.00176 1.0626e 02 1 1.000 0 13 104.03024 196.96176 1.15024 14.00176 1.1916e 02 1 1.000 0 14 199.27024 212.20176 1.15024 14.00176 8.2017e 03 1 1.000 1 15 214.51024 227.44176 1.15824 14.00176 6.0150e 03 2 1.000 12 16 229.75024 242.60176 1.15824 14.00176 3.2642a 03 3 1.000 23 17 16.39024 29.32176 16.39024 29.32176 6.46190 030 1 1.000 0 le 31.63024 44.56176 16.39024 29.32176 1.1217e 02 1 1.000 0 19 46.87024 59.00176 16.39024 29.32176 1.3327e 02 1 1.000 0 20 62.11824 75.04176 16.39024 29.32176 1.1004e 02 1 1.000 0 21 77.35824 90.28176 16.39524 29.32176 1.3504e 02 1 1.000 0 22 92.59024 105.52176 16.39024 29.32176 1.1164e 02 1 1.000 0 23 107.83024 120.76176 16.39024 29.32176 1.3234e 02 1 1.000 0 24 122.07024 136.00176 16.39024 29.32176 1.0701e 02 1 1.000 0 25 130.31024 151.24176 16.39824 29.32176 1.3192e 02 1 1.000 0 26 153.55824 166.40176 16.39024 29.32176 1.0950s 02 1 1.000 0 27 160.79824 101.72176 16.39024 29.32176 1.2077e 02 1 1.000 0 20 184.03034.196.96176 16.39024 29.32176 9.9145e= 03 - 1 - 1.000 0 29 199.27824 212.20176 16.39024 29.32176 9.9915e 03 1 1.000 2 30 214.51824 227.44176 16.39024 29.32176 5.5691e=03 2 1.000 13 31 229.75024 242.68176 16.39024 29.32176 3.2U11e 03 3 1.000 24
.32 31.63024' 44.56176 31.63024 44.56176 5.4259e 039 1 1.000 0 33 46.07024 59.00176 31.63054 44.56176 1.1137e 02 1 1.000 0 34 62.11024 75.04176 31.63824 44.56176 1.3600e 02 1 1.000 0 35 77.35024 90.20176 31.62024 44.56176 1.1276e+02 1 1.000 0 36 92.59024 105.52176 31.63024 44.56176 1.3441e 02 1 1.000 0 37 107.03024 120.76176 31.63024 44.56176 1.0870s 02. 1 1.000 0 30 123.07824 135.00176 31.63024 '44.56176 1.1092e*02 1- 1.000 0
+ The relative assembly power has been normalised so that the one eighth of the total core power aquals 1.0.
- The th: ee burnup groupe 1,2 and 3 correspond to assembly burnups of 13.031, 13.700,12.755 GND/T. ,
9 mote that the, assembly power for assemblies on the core disposal at 45 - is actually.one half of the. assembly power, since only half.of the assembly is
# e ne W M < i:
m e og ewo 'imenuded ta ~the estaat.- i
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e Table 2.2.2.4 Fus3 Assembly Goonstry and Power (cont'd) Relative Asial Pin Assab. Assambly Burnup Peaking Power Number X Left X Right Y Bot Y Top Power Group Factor Set 39 130.31024 151.24176 31.63024 44.56174 1.1050e 02 1 1.000 0 40 153.55024 166.40176 31.63024 44.56176 1.3296o 02 1 1.000 0 41 160.79024 101.72176 31.63024 44.56176 1.0577e 02 1 1.000 0 42 104.03024 196.96176 31.63024 44.56176 1.1744e 02 1 1.000 3 43 199.27024 212.20176 31.63024 44.F6176 7.9120e+03 2 1.000 14 44 214.51024 227.44176 31.63024 44.56176 5.4170s 03 3 1.000 25 45 46.07024 59.00176 46.07024 59.00176 6.7304e 030 1 1.000 0 46 62.11024 75.04176 46.07024 59.00176 1.1000e 02 1 1.000 0 47 77.35024 90.20176 46.07024 59.00176 1.3305e 02 1 1.000 0 40 92.59024 105.52176 46.07024 59.00176 1.0090e 02 1 1.000 0 49 107.03024 120.76176 46.07024 59.00176 1.1169e 02 1 1.000 0 50 123.07024 136.00176 46.07024 59.00176 1.0976e 02 1 1.000 0 51 130.31024 151.24176 46.07024 59.00176 1.3404e 02 1 1.000 0 52 153.55024 166.40176 46.07024 59.00176 1.0900e 02 1 1.000 0 53 160.79024 101.72176 46.07024 59.00176 1.2697e 02 1 1.000 0 54 184.03024 196.9617C 46.07024 59.00176 9.6007e 03 1 1.000 4 55 199.27024 212.20176 46.07024 59.00176 9.4040e 03 2 1.000 15 56 214.51024 227.44176 46.07024 59.00176 4.7132e 03 3 1.000 26 57 62.11024 75.04176 62.11024 75.04176 5.4676e 030 1 1.000 0 50 77.35024 90.20176 62.11024 75.04176 1.0032e 02 1 1.000 0 59 92.59024 105.52176 62.11024 75.04176 1.1061e 02 1 1.000 0 60 107.03024 120.76176 62.11824 75.04176 1.0950e 02 1 1.000 0 El 123.07024 136.00176 62.11024 75.04176 1.3430s 02 1 1.000 0 62 130.31024 151.24176 62.11024 75.04176 1.1080e 02 1 1.000 0 63 153.55024 166.40176 62.11024 75.04176 1.3175e 02 1 1.000 0 64 160.79024 101.72176 62.11024 75.0417C 1.0412e 02 1 1.000 0 65 104.01024 196.96176 62.11024 75.04176 1.1221e 02 1 1.000 5 66 199.27024 212.20176 62.11024 75.04176 7.3459e 03 2 1.000 16 67 214.51024 227.44176 62.11024 75.04176 4.3773e 03 3 1.000 27 40 77.35024 90.20176 77.35024 90.20176 6.6254e 039 1 1.000 0 69 92.59024 105.52176 77.35024 90.20176 1.1015e 02 1 1.000 0 70 107.03024 120.76176 77.35024 90.20176 1.3409e 02 1 1.000 0 l 71 123.07024 136.00176 77.35024 90.20176 1.1139e 02 1 1.000 0 72 130.31024 151.24176 77.35024 90.20176 1.3279e 02 1 1.000 0 13 153.55024 166.40176 77.35024 90.20176 1.0653e 02 1 1.000 0 74 160.79024 101.72176 77.35024 90.20176 1.2053e 02 1 1.000 0 75 104.03024 196.96176 77.35024 90.20176 0.9775a 03 1 1.000 6 L 76 199.27024 212.20176 77.35024 90.20175 0.3615e 03 2 1.000 17 l 77 214.51024 227.44176 77.35024 90.18176 3.9167e 03 3 1.000 20 1 l l l 9 4 y {-
+ 4 y Nh %.b% ,' d { #
't,
_'Nd((Q%f H6 __ _ .
7.._ __n .. . , , . _ _ . ,y __ ____ i 1 Table 2.2.2/, Fuel Assembly Geometry and Power (cont'd) Relative Aziel Pin Asamb. Assembly Burnup Peeking Power Number X Left X Right Y Bot Y Top Power Group Factor Set 78 92.59024 105.52176 92.59024 105.52176 6.7159e 030 1 1.000 0 79 107.03024 120.76176 92.59824 105.52176 1.1005e 02 1 1.000 0 to 123.07024 136.00176 92.59024 105.52176 1.3245e 02 1 1.000 0 81 130.31024 151.24176 92.59024 105.52176 1.0791e 02 1 1.000 0 02 153.55824 166.48176 92.59024 105.52176 1.2404e 02 1 1.000 0 83 168.79624 101.72176 92.59024 105.52176 9.4730e 03 1 1.000 0 94 104.03024 196.96176 92.59024 105.52176 9.7112e*03 1 1.000 7 05 199.27024 212.20176 92.59J24 105.52176 5.06419 03 2 1.000 18 86 214.51824 227.44176 92.59024 105.52176 3.2740e 03 3 1.000 29 07 107.03024 120.76176 107.03824 120.76176 5.4160e 038 1 1.000 0 08 123.07024 135.00176 107.83024 120.76176 1.0679e 02 1 1.000 0 89 138.31024 151.24176 107.03024 120.76176 1.2509e 02 1 1.000 0 90 153.55024 166.40176 107.03024 120.76176 9.7937e 03 1 1.000 0 91 160.79024 101.72176 107.03024 120.76176 1.0372e 02 1 1.000 0 92 104.03024 196.96176 107.03024 120.76176 6.6025e 01 2 1.000 19 > 93 199.27024 212.20176 107.83024 120.76176 4.2016e 03 3 1.000 30 94 123.07024 135.00175 123.07024 136.00176 6.2400e 036 1 1.000 0 95 130.31024 151.24176 123.07024 135.00176 9.9663e 03 1 1.000 0 96 153.55024 166.40176 123.07024 136.00176 1.0792e 02 1 1.000 9 97 160.79024 101.72176 123.07024 136.00176 7.3002e 03 2 1.000 20 13 104.03024 196.96176 123.07024 136.00176 4.0407e 03 3 1.000 31 99 138.31024 151.24176'130.31024 151.24176 2.72'23e 030 1 1.000 0 100 153.55024 166.40176 139.31024 151.24176 .7.8106e 03 1 1.000 10 101 168.79024 101.72176 138.31024 151.24176 6.0455e 03 2 1.000 21 102 104.03024 196.9C176 138.31024 151.24176 3.6073e 036 3 1.000 32 103 153.55024 166.(1176 153.55024 166.40176 3.1472e 03 1 1.000 11 104 168.79824 181.72176 153.55024 166.40176 4.6201e 03 2 1.000 22 105 184.03024 196.96176 153.55024 166.40176 2.6529e 03 3 1.000 33 106 160.79324 101.72176 360.79024 101.72176 1.6018e 030 3 1.000 34 1.
.y =
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T ab b 2.2.2.5 - Pia Geometry and Power Distribution Pia Pitch Set 1 nelative* Pia Pia Power Assemb. I Left X Right Y Mot Y Top Power Set Number , 1.99270s+02 2.05740B+02 1.15024B+00 7.62000E+00 2.664063 03 1 14 2.057405+02 2.12203E+02 1.15024E+00 7.62000B+00 2.707505 03' i 14 1.99270E+02 2.057405+02 7.620005+00 1.40010B+01 2.492045 03 1 14 2.051405+02 2.122023+02 7.62000B+00 1.40010E+01 2.36960B*03 1 14 1.99370E+02 2.05740E+02 1.639028+01 2.20600E+01 3.251055 03 2 29 2.057405+02 2.12202s+02 1.63902s+01 2.20600s+01 3.425213 03 2 29- } 1.99270B+02 2.057405+02 2.206005+01 2.93210B+01 5.057535 03 2 29 2.057402+02 2.122025+02 2.20600B+01 2.93210B+01 2.030165 03 2 29 1.040305+02 1.905005+02 3.16302E+01 3.01000E+01 3.712055 03 3 42 1.90500E+02 1.96962E+02 3.163025+01 3.010005+01 3.900435 03 3 42 1.040385+02 1.905005+02 3.01000B+01 4.45610E+01 3.698725 03 3 42 1.905005+02 1.969623+02 3.01000B+01 4.45610E+01 3.436025 03 3 42 1.040305+02 1.90500E+02 4.607025+01 5'.33400E+01 3.067393 03 4 54 1.90500E+02 1.96962B+02 4.60742E+01 5.33400E+01 3.225075 03 4 54 1.040305+02 1.905005+0% 5.334005+01 5.90010B+01 3.01263E 03 4 54 1.90500E+02 1.969625+02 5.33400E+01 5.90010E+01 2.060035 03 4 54 1.040385+02 1.905005+02 6.21102E+01 6.05000E+01 3.577765 03 5 65 1.905005+02 1.96962E+02 6.211025+01 6.05000E+01 3.737505 03 5 65 1.040305+02 1.905005+02 6.050005+01 7.50410E+01 3.530645 03 5 65 1.90500E+02 1.96962E+02 6.050003+01 7.50410B+01 3.257005 03 5 65 1.04030E+02 1.905005+02 7.735025+01 0.30300E+01 2.924793 03 '6 75 1.905005+02 1.969625+02 7.73502E+01 0.30300E+01 2.90730E 03 6 75 1.040305+02 1.905005+02 0.30200E+01 9.02010E+01 2.795043 03 6 75 1.90500B+02 1.969623+02 0.30200E+01 9.02010B+01 2.501595 03 6 75 1.04030E+02 1.905005+02 9.25902B+01 9.90600E+01 3.219315 03 7 04 1.905005+02 1.969625+02 9.259025,01 9.90600E+01 3.224105 03 7 to 1.04030E+02 1.90500E+02 9.90600s+01 1.055225+02 3.091365 03 7 to 1.905005+02 1.969625+02 9.90600B+01 1.05522E+02 2.677505 03 7 04 1.607983+02 1.752605+02 1.070305+02 1.14300E+02 3.400943 03 '0 91 1.75260B+02_1.01722B+02 1.07030E+02 1.14300E+02 3.416045 03 0 =91 , 1.60790E+02 1.752605+02 1.14300E+02 1.20762E+02 3.325993 03 0 91 1.75260B+0e 1.017225+02 1.14300E+02 1.20162E+02 2.099405 03 0 91 1.535503+02 1.60020E+02 1.23070B+02 1.295405+02 3.409955 03- 9 96
--1.60020B+02 1.664023+02 1.230705+02 1.295405+02 3.525205*03 -9 96
-1.535505+02 1.600205+02 1.295405+02 1'.36001E+02 3.405415 03 9 96 1.60020B+03 1.66402E+02 1.295405+02 1.360025+02 3.070775 03 9 96 1.53550E+02 1.600203+02-1.303105+02 1.447005+02 3.603103 03 10 100 1.60020E+02 1.664025+02 1.303105+02-1.44700B+02 2.525123 03.10' '100 1.53550B+02 1.60020B+02 1.447005+02 1.513425+02 2.507035 03 10 100
-1.600205+02 1.664025+02 1.447005+03'1.512425+02 2.104935 03'10: m 100 <
1.53550B+02 1.600205+02 1.535505+02 1.600203+02 2.273533 03 11- 103
-1.600205+02 1.664023+02 1.53550B+02'1.600205+03 1.931023 03 11; ~103 1.53550B+02 1.60020B+02 1.600203+02 1.664025+02 1.931035 03 11" 10J' 1.60020B+02 1.664025+02 3.600205+02 1.664025+02 1.779915 03 11 103
,v
, w e p p pga 945etDeat 1"is a SmS:assey.-+ s e n g Ep W 4 6is p e hJi pj d4 @ pyn 6h Q (p
~
- The pia powers have been normalised so that'one eighth of the total core 3, $qpesar equals 1.0. g,; , ; ,
q g wa
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I Table 2.2.2.5 Pin Geometry and Power Distribution (cont'd) O Pin Pitch Set 2 Relative Pin Pin Power As seeb. I.Left X Right Y Est Y Top Power 8et Number 2.14510F+02 2.17749E+02 1.15024E+00 4.30912E+00 5.504955 04 12 15 2.177495+02 2.20900E+02 1.15024E+00 4.30912E+00 5.507983 04 12 15 2.20900E+02 2.24211B+02 1.15024E+09 4.30912E+00 5.76430E 04 12 15 2.24211E+02 2.27442B+02 1.15024E+00 4.30912E+00 5.63C945 04 12 15 2.14510E+02 2.177493+02 4.30912E+00 7.62000E+00 5.053745 04 12 15 2.17749E+02 2.20900E+02 4.30912E+00 7.62000E+00 5.10042E.04 12 15 2.20900E+02 2.242115+02 4.30912E+00 7.62000E+00 3.74652E 04 12 15 2.24211E+02 2.27442E+02 4.30912E+00 7.62000E+00 5.201625 04 12 15 2.14510E+02 2.177495+02 7 62000E+00 1.005095+01 4.777155 04 12 15 2.177493+022.20900E+027)62000E+001.005093+013.33715504 12 15 2.20900B+02 2.142115+02 7.62000E+00 1.035095+01 4.652995 04 12 15 > 2.24211E+02 2.27442E+02 7.62000E+00 1.005095+01 4.5f190E 04 12 15 2.14510E+02 2.177495+02 1.005093+01 1.4n010E+01 4.16460E 04 12 15 2.177493+02 2.20900E+02 1.005095+01 1.40010E+01 4.27294E 04 12 15 2.20900E+02 2.24211E+02 1.005093+01 1.40010E+01 4.00670E 04 12 15 2.24211E+02 2.27442E+02 1.005095+01 1.40010E+01 4.12026E 04 12 15 2.14510E+02 2.17749E+02 1.63902E+01 1.96211E+01 5.60053I 04 13 30 2.17749E+02 2.20900R+02 1.63902E+01 1.96291E+01 5.14152E 04 13 30 2.20900E+02 2.24231E+02 1.63902E+01 1.96291L+01 5.44770E 04 13 30 2.24211E+02 2.27442E+02 1.63902E+01 1.96291E+01 5.40211E 04 13 30 2.14510E+02 2.177495+02 1.96291E+01 2.20600E+01 5.270095 04 13 30 2.177495+02 2.20900E+02 1.96291E+01 2.20600E+01 3.732543 04 13 30 2.20900E+02 2.24211E+02 1.9629?.E+01 2.20600E+01 5.011475 04 13 30 2.24211E+02 2.27442E+02 1.96291E+01 2.20600E+01 4.027505 04 13 30 2.14510E+02 2.177495+02 2.20600E+01 2.60909E+01 4.53200E 04 13 30 2.177497+02 2.20900E+02 2.20600E+01 2.40909E+01 4.571073 04 13 30 2.20900E+02 2.24211E+02 2.20600E+01 2.609095+01 3.214975 04 13 30 2.24211E+02 2.27442E+02 2.20600E+01 2.60909E+01 4.49760E 04 13 30 2,14510E+02 2.177493+02 2.609095+01 2.93210E+01 4.035073 04 13 30 2.177495+02 2.20900E+02 2.609093+01 2.93210E+01 3.924335 04 13 30 2.20900E+02 J.24211E+02 2.60909E+01 2.93210E+01 4.041425 04 13 30 J.14211E+02 2.27442E+02 2.609093+01 2.93310E+01 3.94603E 04 13 30 1.99270E+02 2.C25093+02 3.16302E+013.40691E+017.120605 04 14 43 2.02509E+02 2.05740E+02 3.16302E+01 3.40691E+01 7.226595 04 14 43 2.05740E+02 2.00971E+02 3.16302E+01 3.40691E+01 d.902025 04 14 43 2.00971E+02 2.12202E+02 3.16302E+01 3.40691E+01 6.97070E 04 14 43 1.99270E+02 2.025095+02 3.40691E+01 3.01000E+01 6.912913 04 14 43 2.035095+02+2.05740E+02 3.40691E+01 3.01000E+01,4.069553 04 14 43 2.05740E+02 2.00971E+02 3.406915+01 3.01000E+01 6.645515 04 14 43 2.009715+02 2.12202B+02 3.40691E+01-3.01000B+01'6.407435 04 14 43
.1.99270E+02 2.02509E+02 3.01000E+01 4.133095+01 6.220263 04 14 43 2.025095+02 2.05740B+02 3.01000E+01 4.133093+01'6.21690E 04 14 3 -43 2.05740E+02 2.009715+02 3.01000E+01 4.13309E+01 4.466535 04 14 43 2.00971E+02 2.12202E+02 3.01000E+01.4.133095+01 6.301445 04 14 43 1.99270E+02 2.025093+02 4.13309E+01 4.45610E+01 5.073445 04 14 43 2.025095+02 2.05740R+02 4.133093+01 4.45610E+01 5.700575 04 14 43
' t* 04h1 s*s 24957495+02-24009715+02 4.133095+01 4.45610E+01 5.070415 04 14 43 2.00971E+02 2.12202E+02 4.13309D+014.45610E+015.606695 04 14 43
[ -p # Pim P,1 % Set is a 4x4 array.
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Tabb2.2.2.6 Fin Geometry and Power Distribution (cont'd) Pin Pitch fst 2
- Relative Pin Pin Power Assemb.
I.Left . .lght Y. Bot Y Top Power Set Number 1.99J70E+02 2.025095+02 4.60702E+01 5.01091E+01 0.507765 04 15 f4 2.025093+02 2.05740E+02 4.60702E+01 5.01091B+01 5.501455 04 15 59 2.05740E+02 2.009715+02 4.60702B+01 5.010915+01 0.659605 04 15 55 2.00971B+02 2.12202E+02 4.50702E+01 5.0?091E+01 0.226095 04 15 55 1.99270E+02 2.025095+02 5.01091E+01 5.33400B+01 0.047715 04 15 55 2.025095+02 2.05740B+02 5.01091E+01 5.33400E+01 6.003355 04 15 55 2.05740B+02 2.00971E+02 5.010915+01 5.33400E+01 7.656855 04 15 55 2.00971E+02 2.12202E+02 ".010915+01 5.33400E+01 0.004055 04 15 55 1.99270E+02 2.025095+02 5.33400E+01 5.657095+01 7.656055 04 15 55 2.025095+02 2.05740E+02 5.33400E+01 5.657J95+01 7.133675 04 15 55 2.05740B+02 2.00971E+02 5.33400B+01 5.657095+01 5.534745 04 15 55 i 2.00971E+02 2.12202E+02 5.33400E+01 5.657095+01 7.307295 04 15 55 1.99270E+02 2.025095+02 5.657095+01 5.00010E+01 6.67236E.04 15 55 2.025095+02 2.05740B+02 5.657095+01 5.90010E+01 6.933305 04 15 55 2.05740E+02 2.00971E+02 5.657095+01 5.90010B+01 6.703395 04 15 55 2.00971B+02 2.12202E+02 5.657095+01 5.90010E+01 6.309215 04 15 55 1.99270E+02 2.025095+02 6.21102E+01 6.534915+01 6.001605 04 16 66 2.025095+02 2.05740E+02 6.21102E+01 6.53491E+01 6.061235 04 16 66 2.05740E+02 2.00971E+02 6.21102E+01 6.53491E+01 6.407245 04 16 66 2.00971E+02 2.12202E+02 6.21102B+01 6.53491E+01 6.400515 04 16 66 1.99270E+02 2.025095+02 6.53491E+01 6.05000E+01 6.534945 04 16 66 2.025095+02 2.05740E+02 6.53491E+01 6.05000E+01 4.579715 04 16 66 2.05740E602 2.00971E+02 6.53491E+01 6.05000E+01 6.10021E*04 16 66 2.00971E+02 2.12202E+02 6.53491E+01 6.05000E+01 5.977495 04 16 66 1.99270E+02 2.025093+02 6.05000E+01 7.101095+01 5.003075 04 16 66 2.025085+02 2.05740E+02 6.05000E+01 7.101095+01 5.76004E.04 16 66 2.05740E+02 2.009715+02 6.05000E+01 7.101093+01 4.099903 04 16 66 2.00971E+02 2.12202E+02 6.05000E+01 7.181095+01 5.745075 04 16 66 1.99270E+02 2.025095+02 7.101095+01 7.50410B+01 5.370915 04 16 66 2.025095+02 2.05740E+02 7.101095+01 7.50410E+01 5.212105 04 16 66 2.05740E+02 2.009715+02 7.101095+01 7.50410E+01 5.334495 04 16 66 2.009715+02 2.12202E+02 7.101095+01 7.50410E+01 5.116465 04 16 66 1.99270E+02 2.025095+02 7.73502E+01 0.050915+01 7.933055 04 17 76 2.025095+02 2.05740E+02 7.73502E+01 0.050915+01 7.707955 04 17 76 2.05740E+02 2.00971E+02 7.73502E+01 0.05091E+01 7.792745 04 17 7C i l 2.00971E+02 2.12202B+02 7.73502E+01 0.014915+01 7.240095 04 17 75 1.99270E+02 2.025095+02 0.05091E+01 0.30200E+017.317055 04 17 76
- 2.025095+02 2.05740E+02 0.05091E+01 0.30200B+01 5.497325 04 17 76 2.05740E+02 2.00971E+02 0.05091E+01 0.30200E+01 6.010155 04 17 76 2.00971E+02 2.12202E+02 0.05093E+01 0.30200B+01 7.064195 04 17 76 1.39370E+02 2.025095+02 0.30200E+01 0.705095+01 6.932213 04 17 76 2.025095+02 2.05740E+02 0.30200E+01 0.705095+01 6.379055 04 .17 76 l
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_ _ _ _ . _ _ _ . ,. . _ . _ _ _ _ __ m _ _m _, _m_______ Table 2.2.2.5 Fin Geometry and Power Distribution (cont'd) Pin Pitch Set 2 Relative Pin Pin Power Assemb.
. I+Left I+Right Y Ect Y Top Power Set :tumber 2.05740B+02 2.00971E*02 0.30200B+01 0.705095+01 4.060625 04 17 76 2.00971E+02 2.12202E+02 0.30200E+01 0.70509E+01 6.36492E*04 17 76 1.99274E+02 2.025095+02 0.705098+01 9.02010E+01 5.920343 04 17 76 2.025095+02 2.05740E+02 0.105093+01 9.02010E+01 6.115045 04 17 76 2.057405+03 7.009715+02 0.705095+01 9.02010E+01 5.001155 04 17 76 2.00971E+02 2.12202E+02 0.705095+01 9.020195+01 5.31500E*04 17 76 1.99270E+02 2.025095+02 9.2b902E+01 9.50291E+01 5.043325 04 10 05 2.025095+02 2.05740E+02 9.25902E+01 9.50291E+01 5.773165 04 10 L5 2.05740B+01 2.00971E+02 9.25902E+01 9.50291E+01 5.240513 04 10 05 2.009715+02 2.12202E+02 9.25902E+01 9.58291E+01 4.96764E 04 it 85 1.99270E+02 2.025095+02 9.50291E+019.90600E+015.577595 04 10 35 ,
2.025095+02 2.05740E+02 9.50291E+01 9.90600E+01 3.014375 04 10 -85 2.05740E+02 2.00971E+02 9.502915+01 9.90600E+01 4.926255 04 10 95 2.00971E+02 2.12202E+02 9.50291E+01 9.90600E+01 4.472775 04 10 05 1.99270E+02 2.025095+02 9.90600E+01 1.02291E+02 4.053323 04 10 05 2.025095+02 2.05740E+02 9.90600E+01 1.02291E+02 4.60500E 04 le 65 2.05740E+02 2.00971E+02 9.906005601 1.02291E+02 3.16077Ea04 le 05 2.00971E+02 2.12202E+02 9.90600E+01 1.02291E+02 4.21234E 04 10 45 1.99270E+02 2.025095+02 1.02291E+02 1.05522E+02 4.357445 04 it 85 2.025093+02 2.05740E+02 1.02291E+02 1.05522E+02 4.002375 04 10 05 2.05740E+02 2.00971E+02 1.02291E+02 1.05522B+02 4.02155E*04 it 85 2.00971E+02 2.12202E+02 1.02291E+02 1.05522E+02 3.74724E 04 it 85 1.04030E+02 1.072693+02 1.07030E+02 1.11069E+02 6.500935 04 19 92 1.072693+02 1.90500E+02 1.07030E+02 1.110695+02 6.45467E 04 19 92 1.90600E+02 1.93731E+02 1.07030E+02 1.110693+02 5.906063 04 19 92 1.937315+02 1.96962E+02 1.07030E+02 1.110695+02 5.670365 04 19 92 1.04030B+02 1.072693+02 1.110695+02 1.14300E+01 6.239415 04 19 92 1.072695+02 1.90500E+02 1.110695+02 1.14300E+02 4.20217E*04 19 92 1.90500E+02 1.937315+02 1.110695+02 1.14300E+62 5.50bO7E*04 19 92 1.93731E+02 1.96962E+02 1.11069E+02 1.14300E+02 5.125705 04 19 92 1.04030E+02 1.072695+02 1.14300E+02 1.17531E+02 5.535605 04 19 92 1.072695+02 1.90500B+02 1.14300E+02 1.175315+02 5.375365+04 19 92 1.90500B+02 1.93731B+02 1.14300E+02 1.17531E+02 3.615965 04 19 92 1.937313402 1.96962E+02 1.14300E+02 1.17531E+02 4.002525-04 19 92 1.04030E+02 1.072695+02 1.175315+02 1.20752E+02 5.106605 04 19 92 1.072695+02 1.90:00E+02 1.175315+02 1.20752E+02 4.750205 04 .19. 92 1.90500E+03 1.937315+02 1.175315+02 1.20762E+02'4.666255 04 19 92~ 1.93731E+02 1.96962E+02 1.17531E+02 1.20762E+02 4.411635 04 19 92 "1'.607983+02 1.720295+02 1.23070E+02 1.263095+02 6.972545 04- 20 97' 1.720295+02 1.75260E+02 1.23070Lt03 1.263095+02 6.069505 04 20 97
-1.75260E+02 1.704915+02 1.23070E+02 1.263095+01 6.296235 04 -20 -97 1.70491E+02 1.01722E+62 1.23070E+02 1.263093+02 6.131693 04 '20 97 1.60790E+02 1.720293+02 1.253095+02 1.29540E+02 6.01911E+04 20 -97 n' '1.720295+03 1.75260B+02 1.263095+02 1.29540E+02 4.635995-04 20 97-1'.75260E+02 1.70491E+02 1.263095+02 1.29540B+03 6.060704 04 -20' 97-
'1.70491E+03 1.61722E+02 1.263093+02 1.29540E+03 5.69205d 04 20 '97' 1.607995+02 1.720295+02 1.29540E+02 1.32171E+03 6.17030E 04 20 97
- % N1.720295+02.1.15260B+02 1.29540E+02 1.32771E+02-5.934613 04s 20 w A7Qe e-w w ~ ;1.75260B+02 1.78491E+02 1.29540B+021.327715+02 3 4'.059623 04X2041971 %,
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Table 2.2.2.5 Fin Geometry and Power Distribution (coct'd) Pin Pitch Set 2 Relative Pin Fin Power Assemb. I Left X Right Y Bot Y Top Power Set Number 1.704915+02 1.01722E+02 1.29540E+02 1.327715+02 5.543205 04 20 97 1.6079 0E+02 1.720295+02 1.12771E+02 1.36002E+02 5.059405 04 20 97 1.720295+02 1.75260E+02 1.327715+02 1.36002B+02 5.472555 04 20 97 1.75260E+02 1.70491E+02 1.327715+02 1.36002E+02 5.396335 04 20 97 1.704915+02 1.017225+02 1.32771E+02 1.36002E+02 4.995095 04 20 97 1.60790E+02 1.720295+02 1.30313E+02 1.415495+02 5.057195 04 21 101 1.720295+02 1.75260E+02 1.30310E+02 1.415495+02 5.507675 04 21 101 1.75260E+02 1.704915+02 1.30310E+02 1.415495+02 5.454435 04 21 101
,1.70491E+02 1.01722E+02 1.30310E+02 1.415495+02 5.069045 04 21 101 1.6&P90E+02 1.720295+02 1.415495+02 1.44700E+02 5.401943 04 21 101 1.720295+02 1.75260E+02 1.415495+02 1.44700E+02 5.240935 04 21 101 1.75260E+02 1.70491B+02 1.415493+02 1.44700B+02 3.602135 04 21 101 1.704915+02 1.01722E+02 1.415493+02 1.44700E+02 4.004615 04 21 101 1.60790B+02 1.720293+02 1.44700B+02 1.40011B+02 5.213605 04 21 101 1.720293+02 1.75260E+02 1.44700E+02 1.40011E+02 3.495395 04 21 101 1.75260E+02 1.704915+02 1.44700E+02 1.40011E+02 4.562605 04 21 101 1.70491E+02 1.01722E+02 1.44700E+02 1.40011E+02 4.320095 04 21 101 1.607983+02 1.720295+02 1.40011E+02 1.51242B+02 4.671115 04 21 101 1.720295+02 1.75260E+02 1.403115+02 1.51242E+02 4.50220E+04 21 101 1.75260E+02 1.70491E+02 1.40011E+02 1.51242E+02 4.155553 04 21 101 1.70491E+02 1.01722Ee02 1.40011E+02 1.51242E+02 4.00540E 04 21 101 1.60790E+02 1.720295+02 1.53550B+02 1.567895+02 4.756493 04 22 104 1.720295+02 1.75260E+02 1.53550E+02 1.567895+02 4.504635 04 22 104 1.75260E+02 1.704915+02 1.53550E+02 1.567895+02 4.064775 04 22 104 1.70491E+02 1.01722E+02 1.53550E+02 1.567895+02 3.745035 04 22 104 1.60790E+02 1.720293+02 1.567895+02 1.60020E+02 4.544005 04 22 104 1.720295+02 1.75260E+02 1.56789E+02 1.60020E+02 3.010995 04 22 104
.1.75260E+02 1.70491E+02 1.567895+02 1.60020E+02 3.009135 04 22 104 1.70491E+02 1.017223+02 1.567895+02 1.60020E+02 3.376035 04 22 104 1.60790E+02 1.720295+02 1.60020E+02 1.63251E+02 3.965045 04 22 104 W30295+02 1.75260E+02 1.60020E+02 1.632515+02 3.724045 04 22 104 4.?F260E+02 1.704915+02 1.60020E+02 1.63251E+02 2.451565 04 22 104 t.90491E+02 1.01722E+02 1.60020E+02 1.63251E+02 3.195645 04 22 104 1.647995+02 1.720295+02 1.63251E+02 1.66402E+02 3.590333 04- 22 104 1.720295+02 1.75260E+02 1.63251E+02 1.66402E+02 3.277153 04 22 104
-1.75260E+02 1.70491E+02 1.632515+02 1.66402E+02 3.152745 04 22 104 1.704915+02 1.01722E+02 1.63251E+02 1.66402E+02 2.041035 04 22 104 i
v m Yh'- , _) f f - l WT ,- c y J7 4 - 4 2 y . 7 4
*r.! ,{ g , j -M , }
Op % , c4 ' ( b /j , (}4 W' 4 'M s i 9:e 14 _b ghg g.;gfyy4M h @{N@ #U MOQi-db
Table 2.2.2.5
- Pin Goosotry and Power Distribution (cont'd)
+
Fin Pitch Set 3 Relative Pin Pin Power Assemb. X+Left X*Eight Y Bot Y Top Power Est Number 2.29750E+02 2.31374E+02 1,15024E+00 2.773685+00 9.060545 05 23 16 2.31374B+02 2.329995+02 1415024E+00 2.77360E+00 0.02605E.05 23 16 2.329095+02 2.3460$E+02 1.15024B+00 2.77360E+00 0.663325 05 23 16 2.34605E+02 2.36220E+02 1.15024E+00 2.77360E+00 0.402635 05 23 16 1.36220E+02 2.3703%5+02 1415024E+00 2.77360B+00 0.443513 05 23 16 2.37035E+02 2.39451E+02 1.15024E+00 2.77360E+00 0.546905 05 23 16 2.39451E+02 3.410665+02 1.15024E+00 2.77360E+00 0.620245 05 23 16 2.410665+02 2.42602E+02 1.15024E+00 2.77360E+00 0.765025*05 23 16 2.29750E+02 2.31374E+02 2.77360E+00 4.30912E+00 0.30572E+05 23 16 2.31374E+02 2.329095+02 2.77360E+00 4.30912E+00 7.603155*05 23 16 2.329995+02 2.34605E+02 2.77360B+00 4.30912E+00 7.t0970B+05 23 16
. 2.34605E+02 2.36220E+02 2.77360B+00 4.30912E+00 7.349275 05 23 16 2.36220E+02 2.37035E+02 2.773685+00 4.30912E+00 7.294013 05 23 16 2.37035E+02 2.394515+02 2.773685+00 4.30912E+00 7.37703E+05 23 16 2.394515+02 2.410665+02 2.77360E+00 4.38912E+00 7.466625 05 23 16 2.410665+02 2.42602E+02 2.77360E+00 4.30912E+00 0.044535 05 23 16 2.29750E+02 2.31374E+02 4.30912E+00 6.004565+00 7.713435 05 23 16 2.31374E+02 2.329095+02 4.30912E+00 6.004565+00 7.03761E*05 23 16 2.32909E+02 2.34605E+02 4.30912E+00 6.004565+00 6.790393 05 23 16 2.34605E+02 2.36220E+02 4.30912E+00 6.004565+00 6.77309E 05 23 16 2.36220E+02 2.37035E+02 4.30912E+00 6.004565+00 6.63131E*05 23 16 4
2.37035E+02 2.39451E+02 4.30912E+00 6.004565+00 6.579325 05 23 16 2.39451E+02 2.410665+02 4.30912E+00 6.004565+00 6.010403 05 23 16 2.41066E+02 2.42602E+02 4.30912E+00 6.00456E+00 7.352555 05 23 16 2.29750B+02 2.31374E+02 6.004565+00 7.62000E+00 7.031005 05 23 16 2.31374E+02 2.329095+02 6.004565+00 7.62000E+00 6.41655E 05 23 16 2.329095+02 2.34605B+02 6.004565+00 7.62000E+00 6.317125 05 23 16 2.34605E+02 2.36220E+02 6.004565+00 7.62000E+00 0.00000E+00 23 16 2.36220E+02 2.37035E+02 6.004565+00 7.62000E+00 6.37339E.05 23 16 2.37035B+02 2.39451E+02 6.004565+00 7.62000E+00 6.090075+05 23 16 2.39451E+02 2.410665+02 6.004565+00 7.62000E+00 6.191695 05 23 16 2.410665+02 2.42602E+02 6.004565+00 7.62000E+00 6.676233 05 23 16 2.29750E+02 2.31374E+02 7.62000E+00 9.23544E+00 6.500415 05 23 16 2.31374E+02 2.329093+02 7.62000E+00 9.23544E+00 5.949175 05 23 16 - 2.329095+02 2.34605E+02 7.62000E+00 9.23544E+00 5.775005 05 23 16 2.34605E+02 2.36220E+02 7.62000E+00 9.23544E+00 5.95321E*05 23 16 2.36220E+02 2.37035E+02 7.62000E+00 9.23544B+00 0.00000E+00 23 16 2.37035B+02 2.39451E+02 7.62000E+00 9.23544B+00 5.74501R+05 23 16 2.39451E+02 2.410665+02 7.62000E+00 9.23544E+00 5.745015 05 23 16
=2.410665+02 2.42602E+02 7.62000E+00 9.23544E+00 6.164105 05 23 16 2.29753E+02 2.31374E+02 9.23544E+00 1.005095+01 6.18?.345 05 23 16 2.31374E+02 2.339095+02 9.23544E+00 1.00509E+01 5.670145 05 23 16 2.329095+02 2.34605E+02 9.23544E+00 1.005095+01 5.434665 05 23 16 2.34605E+02 2.36220E+02 9.23544B+00 1.005095+01 5.40306E 05 23 16
.3.34220B+02 2.37035E+02 9.23544E+00 1.005095+01 5.447735 05 23' 16 2.37035E+02 2.39451E+02 9.23544E+00 1.005095+01 n.301115 05 16 2.39451E+02 2.41064E+02 9.23544E+00,1 005095+01 5.4a3255 05,L231<m16 r m ,^ .,
2.410665+02 2.42602E+02 9.23544E+00 1'.005095+01 5.049995 05 23 ' ~ 16 ' ' . , _ >, , + Pia'Pittsh set 3'is'a Ost array - ,
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e Table 2.2.2.5 Pin Geometry and Power Distribution (cont' d) Pin Pitch Set 3 Relative Pin Pin Power Assemb. X*Left Z Right Y Bot Y Top Power Set Number 2.297505+02 2.31374E+02 1.005095+01 1.24663E+01 5.99405E+05 2J 16 2.31374E+02 2.329895+02 1.005095+01 1.24663E+01 5.572145*05 23 16 2.329995+02 2.34605E+02 1.00509E+01 1.24663E+01 5.40020E 05 23 16 2.3460$3+02 2.36220E+02 1.00509E+01 1.24663Et01 5.37202E.05 23 16 2.36220E+02 2.37835E+02 1.08509E+01 1.24663E+01 5.342753 05 23 16 2.37835E+02 2.394515+02 1.08509E+01 1.24663E+01 5.372785 05 23 16 2.39451E+02 2.410665+02 1.005095+01 1.24663E+01 5.30262E 05 23 16 2.410665+02 2.42602E+02 1.00509E+01 1.24663E+01 5.683945 05 23 16 2.297585+02 2.31374E+02 1.24663E+01 1.400185+01 6.114473 05 23 16 2.31374E+02 2.329092+02 1.24663E+01 1.40018E+01 6.152033 05 23 16 2.329095+02 2.34605E+02 1.24663E+01 1.40910E+01 6.121795 05 23 16 2.34605E+02 2.36220E+02 1.24663E+01 1.40010E+01 6.030605 05 23 16 2.36220E+02 2.37835B+02 1.24663E+01 1.40010E+01 6.00040E*05 23 16 2.37835E+02 2.394515+02 1.24663B+01 1.408153+01 6.02412E 05 23 16 2.39451E+02 2.410665+02 1.24663E+01 1.40018E+01 5.97542E.05 23 16 - 2.410665+02 2.42682E+02 1.24663E+01 1.408195+01 5.05227E 05 23 16 2.29750E+02 2.31374E+02 1.63902E+01 1.801375+01 0.734005 05 24 31 2.31374E+02 2.32909E+02 1.63992E+01 1.80137E+01 8.41002E 05 24 31 2.32909E+02 2.3460$E+02 1.63982E+01 1.801375+01 8.100385 05 24 31 2.34605E+02 2.36220E+02 1.63902E+01 1.80137E+01 0.002975 05 24 31 2.36220E+02 2.37835E+02 1.63982E+01 1.80137E+01 0.03005E 05 24 31 2.37035E+02 2.39451E+02 1.63982E+01 1.001373+01 8.35223E.05 24 31 2.394515+02 2.410665+02 1.63982E+01 1.001375+01 8.07014E.05 24 31 2.410665+02 2.42602E+ 02 1.63902E+01 1.001375+01 9.06233E.05 24 31 2.29750E+02 2.31374E+02 1.801375+01 1.9 6291E+01 0.072875 0F 24 31 2.31374E+02 2.32909E+02 1.001375+01 1.96291E+01 7.32716E 05 24 31 2.329895+02 2.34605E+02 1.001375+01 1.96291E+01 7.10660E*05 24 31 2.34605E+02 2.36220E+02 1.001375+01 1.96291E+01 6.94383E 05 24 31 3.36220E+02 2.37035E+02 1.80137E+01 1.96291E+01 6.906235 05 24 31 J.37035E+02 2.39451E+02 1.80137E+01 1.96291E+01 7.259025 05 24 31 2.39451E+02 2.410663+02 1.001375+01 1.96291E*01 7.70243E.05 24 31 2.410665+02 2.42602E+02 1.80137E+01 1.96291E+01 9.32178E 05 24 31 2.29750E+02 2.33374E+02 1.r$291E+01 2.124465+01 7.376125 05 24 31 2.31374E+02 2.329093402 1.96291E+01 2.12446E+01 6.68264E*05 24 31 2.329095+02 2.34605E+02 1.96291E+01 2.124465+01 6.32059E 05 24 31 2.34605E+02 2.36220E+02 1.96291E+01 2.124465+01 6,29023E.05 24 31 2.36220E+02 2.37835E+02 1.96291E+01 2.12446E+01 6.404045 05 24 31 2.37835E+02 2.39451E+02 1.96291E+01 2.124465+01 6.52543E 05 24 31 2.394515+02 2.41066E+02 1.96291E+01 2.12446E+01 7.10332E*05 24 31 2.410665+02 2.42682E+02 1.96291E+01 2.124463+01 0.62902E*05 24 31 2.297585+02 2.31374E+02 2.12446E+01 2.28600E+01 6.669525 05 24 31 2.31374E+01 J.329895+02 2.124465+01 2.20600E+01 6.044435 05 24 31 N\ .'- 7 .' s , . . % M h $' :
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Table 2.2.2.5 Pia Geometry and Power Distribution (coat' d) Pia Pitch Set 3 , Relative Pia Pia Power Assemb. 5+b9ft 5+Right Y Sot Y Top Power Set Number 3.339095+02 2.34605E+03 2.134465+01 2.20600E+01 5.029435*05 24 31 3.34605E+03 2.363305+02 2.134465+01 2.206005+01 6.00052E+05 24 31 2.363305+03 3.37035B+03 2.134465+01 3.20600B+01 0.000005+00 24 31 3.370385+03 2.394515+03 2.134465+01 2.206005+01 6.006005 05 24 31 3.394515+08 3.410645+03 3.134465+01 3.306005+01 6.435345 05 24 31 3.410665+03 2.436035+02 3.334465+01 3.306003+01 7.054005*05 24 31 3.397505+03 3.313745+03 3.306005+01 3.44754B+01 6.11350s.05 24 31 3.313743+03 3.339093+03 3.206005+01 1.44754B+01 5.564965 05 24 31 3.339093+03 f. 346055+03 3.20600B+01 1.44754B+01 5.444335 05 24 31 2.34605B+03 3.363305+02 2.30600E+01 2.441545+01 0.00000E+00 24 31 2.363305+02 2.37035E+03 2.20300B+01 2.44754B+01 5.509445+05 24 31 2.370?SB+02 2.394515+02 2.20600E+01 2.44754B+01 5.421625 05 24 31 2.394515+02 2.410665+02 2.20600B+01 2.44754s+01 5.004695 05 24 31 2.410665+02 2.43602B+02 2.30600B+01 2.447545+01 7.210145+05 24 31 2.29750B+02 2.31374E+02 2.44754B+01 2.609093+01 5.760205 05 24 31 2.313745+02 2.329093+02 2.44754E+01 2.609095+01 5.26044E+05 24 31 2.329095+02 2.34605E+02 2.44754E+01 2.609093+01 5.066554+05 24 31 2.34605B+02 2.362205+02 2.44754E+01 2.609093+01 5.041575 05 -24 31 2.36320B+02 2.37035F+02 2.447545+01 2.609093+01 4.950295+05 24 _31 2.370385+02 2.39451B+02 2.447545+01 2.609095+01 5.045365 05 24 ~ 31 2.394515+02 2.41064E+02 2.44754E+01 2.609095+01 5.534673 05 24 31 2.410665+02 2.42602E+02 2.44754B+01 2.609093+01 6.73311E*05 24 31 2.297505+02 2.31378%+02 2.609093+01 2.770435+01 5.505905 05 24 31 2.31374s+02 2.329093+02 2.609093+01 2.770635+01 5.106421 05 24 31 2.339095+03 2.34605B+02 2.609095+01 2.770635+01 5.074005+05 24 31 2.34605B+02 2.362305+02 2.609093+01 2.77063B+01 4.953503 05 24 31 2.363305+02 3.370385+03 3.6C9095+01 2.77063E+01 4.939025 05 24 31
, _2.370355+02 2.39451E+02 3.609095+01 2.77063B+01 5.050403 05 24 31 3.394515+03 2.410465+02 3.609095+01 2.77063E+01'5.330525 05 .24 31 2.410665+03 2.426025+02 2.509095+01 2.77063B+01 6.200393 05 24 31 2.397505+02 2.31374E+02 2.770633+01 2.933105+01 5.023075.C5 24 31 2.313745+03 3.339095+03 3.770635+01 3.93310B+01 5.066035 05 24 31 2.339095+02 2.346055+02 2.77063E+01 3.932105+01 5.031353 05 24 31 2.34605E+02 2.363305+03 2.770635+01 3.933105+01 5.496495 05 24 31 .
3.363305+03 3.370355+03 3.770635+01 2.932105+01 5.630903 05 24 31 3.37035E 93.3.394515+03 - 3.770635+01 2.93310B+01 5.674735 05 24 31 2.394515+03 3.410665+03 2.770635+01'3.933105+0125.735055J05 24 31 2.410665+03 2.434035+03 3.770435+01-3.93310B+01 5.904303 05- 34 31 3.145105+03 3.161345+03 3.163085+01 3.335375+01'1.350435 04 28 44 2.161345+03 2.177495+03 3.163035+01 3.335375+01 1.332953 04 25 44
~ 3.17746 5+03 3.193655+03 3.163033+01 3.325375+01 1'.263795 04 25 44 2.19365E+03 3.30900E+03 3.163035+01 3.335373+01 1.294035 04_ 25 44
--_3.209008+03 3.335955+03 3.163035+01 3.335375+01 1.206165+04 25 44
<# t r-- 3.335955+03 3.343115+03 3.163085+013.335375+01 1.303575 04 25 44-
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- W9% 3k999999+43!8&874485+08 3.193035+0143'.885975001i1'.308893 04% 35:b 444 3.145105+03 3.16134B+03 3.335375+01-3.406915+01 1.375335 04: 25 44 3.16134B+03 3.177495+fi 3.325375+01 3.406915+01 1.197005 04x 25 % d da g a.177495+03;3.193655+03L3.335375tt1,3.406915+01-1.,135705 4 64y 35 g 44 g g y
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Table 2.2.2.5 - Pia Seametry and Power Distribution (cont' d) Pin Ditch set 3 melative tin tin power Assemb. E.Left X R& Bht Y Bot Y Top Power Set Number 2.19365E+02 2.20900E+02 3.325375+01 3.406915+01 1.222643 04 25 44 2.20900E+02 2.22595E+02 3.325373+01 3.40691B+01 1.219315 04 25 44 2.12595E+02 2.24211E+02 3.325373+01 3.40691E+01 1.242755 04 25 44 2.242115+02 2.250265+02 3.325375+01 3.406915+01 1.165505 04 25 44 2.250263+02 2.27442B+03 3.325375+01 3.406915+01 1.230135 04 25 44 3.145105>02 2.16134B+02 3.406915+01 3.640465+01 1.164525 04 25 44 2.161345402 2.177495+02 3.40691E+01 3.640465+01 1.005015 04 25 44 2.177493+02 2.19365E+02 3.406915+01 3.640465+01 1.137275 04 25 44 2.19365E+02 2.209005+02 3.404915+013.640463+01 1.125533 04 25 44
. 2.20900E+02 2.225955+02 3.406915+01 3.640463+01 1.141903 04- 25 44 2.225955+02 2.242115+02 3.406915+013.640465+019.664475 05 25 44 2.242115+02 2.250265+02 3.406915+01 3.640465+01 1.174293 04 25 44 2.250265+02 2.274435+02 3.406915+01 3.440465+01 1.101935 04 25 44 2.145103+02 2.16134B+02 3.640465+01 3.01000B+01 1.130305 04 25 44 2.16134E+02 2.177495+02 3.640465+01 3,01000E+01 1.115513 04 25 44 2.177495+02 2.19365E+02 3.640465+013.01000E+01 1.073595 04 25 44 2.19365E+02 2.209005+02 3.640465+013.01000E+01 1.059265 04 25 44 2.20900B+02 2.22595E+02 3.640465+01 3.01000B+01 0.000005+00 25 44 2.23595E+02 2.242115+02 3.640465+01 3.01000B+01 1.070593 04 25 44 2.242115+02 2.250263+02 3.640465+01 3.01000E+01 1.079373 04 25 44 2.250263+02 2.27442E+02 3.640465+01 3.01000E+01 1.091743 04 25 44 2.14510E+02 2.16134B+02 3.010005+01 3.97154E+01 1.003513 04 25 44 2.16134E+02 2.177495+02 3.01000E+01 3.97154E+01 1.066023 04 25 44 2.177493+02 2.19365E+02 3.01000E+01 3.97154E+01 1.044125 04 25 44 2.19365E+02 2.209005+02 3.01000E+01 3.971545+01 0.00000E+00 25 44 2.20900E+02 2.22595E+02 3.01000E+01 3.971545+01 1.034035 04 25 44 2.22595E+02 2.242115+02 3.01000E+01 3.97154E+01 9.906435 05 25 44 2.24211E+02 2.250263+02 3.01000E+01 3.97154E+01 1.01570E 04 25 44 2.250263+03 2.27442E+02 3.01000E+01 3.97154E+01 1.027035 04 25 44 2.14510E+02 2.16134E+02 3.97154E+01 4.133095+01 1.064093 04 25 44 2.16134E+02 2.177495+02 3.97154E+01 4.133095+01 1.056015 04 25 44 2.177495+02 2.19365E+02 3.971545+01 4.133095+01 0.602235 05 25 44 2.19365E+02 2.20900E+02 3.97154B+01 4.133095+01 9.993505 05 25 44 2.20900E+03 2.22595E+02 3.971545+01 4.133095+01 9.644993 05 25 44 2.22595E+02 2.242115+02 3.97154B+01 4.133095+01 9.567745 05 25 44
' 2.242115+02 2.250265+02 3.97154E+01 4.133095+01 0.967555 05 25 44 2.250263+02 2.27442E+02 3.97154B+01 4.133095+01 9.453703 05 25 44
.2.145185+02 2.16134E+02 4.133093+01 4.294635+01 1.040943 04 25 44 2.16134E+02 2.177495+02 4.133095+014.29463E+019.935715 05 25 44 12.177495+02 2.19365E+03 4.133095+01 4.29453E+01 1.051543 04 25 44 2.193655+01 2.20900E+01 4.133093+01 4.39463B+01 1.014575 04' 25 44 2.209005+03 2.235955+02 4.133095+014.29463E+019.965743 05 25 44
' 2.225955+02 2.242115+CJ 4.133093+01 4.294635+019.039323 05 25 44
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I l Table 2.2.2.5 Pin Geometry and Power Distribution (cont' d) Pin Pitch set 3 Belative Pin Pin Power Assemb. I Left I 11tht Y Bot Y Top Power Set Number 2.242115+02 2.250265+02 4.133095+01 4.29463E+01 9.269735 05 25 44 2.250265+02 2.27442E+02 4.133095+01 4.29463E+01 9.564405 05 23 44 2.14510E+02 2.16134E+02 4.29463E+01 4.45610E+01 1.10070s.04 25 44 2.16134B+02 2.177495+02 4.29463E+01 4.45610B+01 1.105165 04 25 44 2.177495+02 2.19465E+02 4.29463B+01 4.45610E+01 1.122535 04- 25 44 2.19365E+02 2.20900E+02 4.29463E+01 4.45610E+01 1.091995 04 25 44 2.20900E+02 2.22595E+02 4.29463E+01 4.45610E+01 1.074005 04 25 44 2.22595E+02 2.242115+02 4.09463E+01 4.45610E+01 1.01015E 04 25 44 2.24211E+02 2.250263+02 4.29463B+01 4.4561F5+01 1.024663 04 25 44 , 2.250265+02 2.27442E+02 4.29463E+01 4.45610E+01 9.950345 05 25 44 2.14510E+02 2.16134B+02 4.60702B+01 4.049375+01 1.269175 04 26 56 2.16134E+02 2.177495+02 4.60702E+01 4.049375+01 1.230103 04 26 56 2.177493+02 2.19365E+02 4.60702E+01 4.049375+01 1.204393 04 26 56 2.19365E+02 2.20900E+02 4.60702E+01 4.049375+01 1.175575 04 26 56 2.20900E+02 2.22595E+02 4.60702E+01 4.049375+01 1.166943 04 26 56 2.22595E+02 2.24211E+02-4.60702E+01 4.049375+01 1.10062E 04 26 56 2.24211E+02 2.250263+02 4.60702E+01 4.049375+01 1.190113 04 26 56 2.250263+02 2.27442E+02 4.60702E+01 4.04937E+01 1.232405 04 26 56 2.14510E+02 2.16134E+02 4.049375+01 5.01091E+01 1.101353 04 26 56 2.16134B+02 2.17749E+02 4.049373+01 5.01091R+01 1.070075 04 26 56 2.17749E+02 2.19355E+02 4.049375+01 5.01091E+01 1.049475 04 26 56 2.19355E+02 2.20900E+02 4.049375+01 5.01091E+01 1.023105 04 26 55 2.20900E+02 2.22595B+02 4.049375+01 5.01091E+01 1.014393 04 26 56 2.23595E+02 2.24211E+02 4.049373+01 5.01091E+01 1.026603 04 26 56 2.242115402 2.250265+02 4.049375+01 5.01091E+01 1.043045 04 26 56 2.250265+02 2.27442E+02 4.049375+01 5.01091E+01 1.139995 04 26 56 2.14510B+02 2.16134E+02 5.01091E+01 5.172465+01 1.097425 04 26 56 2.16134E+02 2.177495+02 5.01091E+01 5.172465+01 9.97062E 05 26 56 2.177495+02 2.19365E+02 5.01091E+01 5.172465+01 9.593535 05 26 56 2.19365E+02 2.20900E+02 5.01091E+01 5.172463+01 9.519595 05 26 56 2.20900E+02 2.22595E+02 5.01091E+01 5.172465+01 9.303025 05 26 56 2.22595E+02 2.24211E+02 5.01091E+01 5.172465+01 9.213353 05 26 56 2.24211E+02 2.250263+02 5.01091E+01 5.172465+01 9.617255 05 26 56 2.250265+02 2.27442E+02 5.010915+01 5.172465+01 1.052323 04 26 56 2.14510E+02 2.16134E+02 5.172465+01 5.33400E+01 1.012025 04 26 56 2.16134E+02 2.17749E+02 5.172465+01 5.33400E+01 9.197845 05 26 : 56 2.177495+02 2.19365E+02 5.172465+01 5.33400E+01 9.009073 05 26 56 2.19365E+02 2.20900E+02 5.172465+01 5.33400E+01 0.00000E+00 26 56 . 2.20900E+02 2.22595B+02 5.172465+01 5.33400E+01 9.01400E 05 26 56 2.22595E+02 2.24211E+02 5.172465+01 5.33400E+01 0.657295 05 26 56 2.242115+02 2.250265+02 5.172465+01 5.33400B+01 0.030995 05 26 56 2.250265+02-2.27442E+02 5.172465+01 5.334095+01 9.675005 05 26 56 2.14510E+02 2.16134E+02 5.33400E+01 5.49554E+01 9.505715 05 26 56 2.16134E+02 2.177495+02 5.33400E+01 5.49554E+01 0.63635E 05 26 56 of w. y 12.177495+02 2,19365E+02.5.33400E+01;5,49554E+01-0.349678 05 26 5 0E+02'5.334003401'5.49554E+01'0'.56215EJ05" 26 *5684Bilnisj 1
~
2.20900E+02 2.22595E+02 5.33400E+01 5.49554E+01 0.00000B+00 26 56 2.22595E+02 2.24211E+02 5.33400E+01 5.49554E+01 0.267405 05. 26 56~ M%Am%. '3.242&15+022.25024E+025.33400E+015.49594B+310.31304305226b'i560 Spm L - . . , ,y , ,4>49 * -
%# .e- #ppfMWn, 4 o
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Table 2.2.2.5 i Pia Geometry and Powei O'.stribution (cont'd) l 1 Pin Pitch Set 3 i
- Relative Pia !
i Pin Power Assemb.
- I.Left I*Right Y=Det Y Yop Power Set Number j 2.250265+02 2.27443E+02 5.334005+01 5.49554B+01 9.072675 05 26 56 2.*4510B+02 2.16134E+02 5.49554B+01 5.657095+01 9.160495 05 26 56 2.161345+02 2.177495+02 5.495541+01 5.657095+01 0.375665 05 26 56 !
! 2.177495+02 2.193655+02 5.49554N+01 5.657095+01 7.901745 05 26 56 4 2.19365B+03 2.20900B+02 5.495545+01 5.657095+01 7.919915 05 26 56 I 2.20900B+02 2.225955+02 5.49554E+01 5.657095+01 7.976105 05 26 56 t 2.22595F+02 2.24211R+02 5.49554B+01 5.657095+01 7.095435 05 26 56 l . 3.242115+02 2.250265+03 5.495545+01 5.657)95+01 0.067295+05 26 56 i '2.280265+02 2.27443B+02 5.495545+01 5.657095+01 0.745125 05 26 56 i ! - 2.145105+02 2.161345+02 5.657095+01 5.01063B+01 9.040075 05 26 56
- 2.16134B+02 2.177495+02 5.657098+01 5.01063B+01 0.304755 05 26 56 l l' 2.177495+02 2.193655+02 5.657093+01 5.01063B+01 0.224285+05 26 56 !
i 2.19365E+02 2.20900B+03 5.657095+01 5.01063E+01 0.043565 05 26 56 1 2.20900B+02 2.225955+02 5.657095+01 5.010635+01 7.993055 05 -26 56 I 2.225955+02 2.342115+02 5.657093+01 5.81063E+01 0.05341E*05 26 56 l 2.242115+02 2.260265+02 5.657095+01 5.010635+01 0.092525 05 26 56 j 2.250265+02 2.274435+02 5.657095+01 5.01063E+01 0.623905 05 26 56 ! 2.145105+02 2.16134E+02 5.01043B+01 5.900105,01 9.430005 05 26 56 2.161345+02 2.177495+02 5.01063E+01 5.90010E+01 9.435553 05 26 56 2.177495+02 2.19365E+02 5.01063B+01 5.900105+01 9.300295 05 26 56 2.193655+02 2.20900B+02 5.010635+01 5.900105+01 9.232165 05 26 56 l 2.209005+02 2.22595E+02 5.01063E+01 f.10010s+01 9.170335 05 26 56 l 2.225955+02 2.242115+02 5.01063B+01 5.900105+01 9.20043E+05 26 56 i 2.342115+02 2.250265+02 5.01063B+01 5.900105+01 9.134495+05 26 56 4 2.250263+02 2.27442B+02 5.01863B+01 5.900103+01 0.990405 05 26 56 L 2.145105+02 2.161345+02 6.211025+01 6.373375+01 1.237615 04 27 67 != 2.161345+02 2.177495+02 6.311025+01 6.373375+01 1.105505 04 27 67 1 2.177495+02 2.193655+02 6.211035+01-6.373375+01 1.147168 04 27 67 i' 2.19365B+02 2.209005+02 6.211025+01 6.373375+01 1.112095 04 27 67 l' 2.209005+02 2.22595B+02 6.311023+01 6.373375+01 1.101015 04 27 67 j 2.225955+02 2.242115+02 6.31103E+01 6.373375+01 1.109395 04 27 67 1 2.242115+02 2.250265+02 6.31102B+01 6.373373+01 1.116405 04 27 67 ! 2.250265+02 2.274435+02 6.21103E+01 6.373375+01 1.135535 04 ~27 47 i 2.14510B+02 2.161345+02 6.373375+01 4.534915+01 1.141465 04 27 67 2.161345+02 2.177493+02 6.373375+01 6.53491B+01 1.027675 04 27 67 [ i 2.177495+02 2.193655+02 6.373375+01 6.534915+01,9.916125 05 27 67 i 2.19365B+02 2.209005+02 6.373375+01 6.534915+01'9.604205 05 27 67
. 2.209005+02 2.22595E+02 6.373375+01 6.534915+01'9.505033 05 27 67 l 2.225955+02 2.242115+03 6.373375+01 6.534915+01 9.570215 05 27 67
'2.242115+02 2.250265+02 6.373375+01 6.534915+01 9.607995 05 27 67 l- 2;250265+02 2.274435+02 4.373375+01 6.534915+01'1.045575 04* 277 67 2.145105+02 2.141345+02 6.534915+01 6.696465+01 1.050465+04 27 - :67 i 2.161345+0313.177495+02'6.534915+01'6.696465+01 9.430005*05 27 ' 67-t i -
_f ] , i ! :eihp'6OYM @h4{ Wp II :M 4 i iti- r i {
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4 i
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4841 HK Table 2.2.2.5
. Pin Geometry and Power Distribution (cont' d)
Pin Pitch Set 3 Relative Pin Pia Powei Assemb. X Left X Right Y* Bot Y Top Power Set Number 2.17749E+02 2.19365E+02 6.53491E+01 6.69646E+01 8.90013E 05 27 67 2.19365E+02 2.20980E+02 6.53491E+01 6.69646E+01 8.76486E 05 27 67 2.20980E+02 2.22595E+02 6.53491E+01 6.69646E+01 8.79843E 05 27 67 2.22595E+02 2.24211E+02 6.53491E+01 6.69646E+01 8.69319E 05 27 67 2.24211E+02 2.258265+02 6.53491E+01 6.69646E+01 8.08549E 05 27 67 2.25026E+02 2.27442E+02 6.53491E+01 6.69646E+01 9.62136E 05 27 67 2.14518E+02 2.16134E+02 6.69646E+01 6.85800E+01 9.62136E 05 27 67 2.161342+02 2.17749E+02 6.69646E+01 6.85800E+01 8.63465E 05 27 67 2.177493+02 2.19355E+02 6.696465+01 6.85800E+01 0.29195E*05 27 67 3 2.19365E+02 2.20980E+02 6.696465+01 6.85800E+01 8.46279E 05 27 67 2.20980E+02 2.22595E+02 6.69646E+01 6.85800E+01 0.00000E+00 27 67 , a 2.22595E*02 2.24211E+02 6.696461+01 6.85800E+01 8.11933E 05 27 67 2.24211E+C2 2.25826E+02 6.69046E+01 6.85800E+01 0.13069E 05 27 67 2.258265+02 2.27443E+02 6.69646E+01 6.85800E+01 0.79515E 05 27 67 2.14518E+02 f,3C s 39'+02 6.85800E+01 7.01954E+01 0.979875-05 27 67 2.16134E+02 i>U14sid'92 6.85800E+01 7.01954E+01 8.07946E 05 27 67
.?.17749E+02 2.1$* a6E+01 6.85800E+01 7.01934E+01 7.800102 05 27 67 2.19365E+02 2.20980E+02 6.85800E+01 7.01954E+01 0.00000E+00 27 67 2.20980E+02 2.22595E+02 6.85800E+01 7.01954E+01 7.04023E 05 27 67 2.22595E+02 2.24211E+02 6.85800E+01 7.01954E+01 7.48440E 05 27 . 67 2.24213E+02 2.25826E+02 6.05800E+01 7.01954E+01 7.58787E 05 27 67 2.25826d+02 2.27442E+02 6.85800E+01 7.01954E+01 8.19832E 05 27 67 2.14518E+02 2.16134E+02 7.01954E+01 7.18109E+01 8.6013tE 05 27 67 2.16134E+02 2.17749E+02 7.01954E+01 7.18109E+01 7.78875E 05 27 67 2.17749E+02 2.19i35E+02 7.01954E+01 7.18109E+01 7.47.857E 05 27 67 2.19365E+02 2.20s00E+02 7.01954E+01 7.181095+01 7.40542E 05 27 67 2.20980E+02 2.22595E+02 7.01954E+01 7.18109E+01 7.20429E 05 27 67 2.22595E+02 2.24211E+02 7.01954E+01 7.18109E+01 7.11495E 05 27 67 2.24211E+02 2.25826E+02 7.01954E+01 7.18109E+01 7.31835E 05 27 67 2.250265+02 2.27442E+02 7.01954E+01 7.18109E+01 7.85014E-05 27 67 2.14518E+02 2.16134E+02 7.18109E+01 7.34263E+01 8.42216E-05 27 67 2.16134E+02 2.177495+02 7.181095+01 7.34263E+01 7.74736E 05 27 67 2.17749E+02 2.19365E+02 7.18109&+01 7.34263E+01 7.56743E-05 27 67 2.19365E+02 2.20980E+02 7.18109E+01 7.34263E+01 7.37211E-05 27 67 2.20980E+02 2.22595E+02 7.16109E+01 7.34263E+01 7.27848E-05 27 67 2.22595E+02 2.24211E+02 7.18109E+01 7.34263E+01 7.30447E 05 27 67
~2.24211E+02 2.25026E+02 7.18109E+01 7.34263E+01'7.307005-05 27 67' 2.258265+02 2.27442E+02 7.18109E+01 7.34263E+01 7.73424E 27 67
'2.145185+02 2.16134E+02 7.34263E+01 7.50418E+01 8.72020E 05 27 67:
2.16134E+02 2.17749E+02 7.34263E+01 7.50418E+01 8.66972E-05 27 67
;2.177495+02 k.19355E+02 7.34263E 01 7.504185+01 8.58493E-05' 27 67 2.19365E+02 2.20980E+02 7.34263E+01 7.50418E+01 8.40828E 05 .27 67 2.20980E+02 2.22595E+02 7.34263E+01 7.50418E+01,8.330305 05 27; , 67
+ ' 2t 22575E+02 2.24211E+02 7.34263E+01 7.504185+01- 8.32770E-05 ' 27 67
~4 2.24211E+02 2.258263+02 7.34263E+01 7.504185+01 8.238955 05 27, 67.
hui M22280SSE+02 2.27442E+02 7.34263E+01^7.804185+01E 8!006025 05"127 _1474W ' v o 2.145185+02 2.16134E+02 7.73582E+01 7.89737E+01 1.115563 04 28 77.
.2.16134E+02 2.17749E+02 7.73582E+01 7.897375+01 1.07887E 04 28 77-
2;177495+02 2.19365E+02 7.73582E+01 7.09,737,5701_1.04907E
, 7 0( .2y; 7733
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. ._. ,_ _ .._. _ .c. v._ __
L Table 2.2.2.5 Fin Geometry and Power Distribution (cont' d) Pin Pitch Set 3 Relative Pin Pin Power Assemb. X Left X Right Y Bot Y Top Power Est Number 2.19365E+02 2.20980E+02 7.73502E+01 7.897375+01 1.01611E 04 28 77 2.20980E+02 2.22595E+02 7.73502E+01 7.897373+01 9.99000E 05 20 77 2.22595E+02 2.24211E+02 7.73502E+01 7.89737E+01 9.99177E-05 20 77 2.24211E+02 2.258265+02 7.73582E+01 7.89737E+01 1.00039E 04 20 77 2.250263+02 2.27442E+02 7.73502E+01 7.897375+01 1.01268E 04 20 77 2.14510E+02 2.16134E+02 7.097375+01 5.05091E+01 1.03019E 04 28 77 2.16134E+02 2.17749E+02 7.097375+01 0.05091E+01 9.374515 05 28 77 2.17749E+02 2.19365E+02 7.097373+01 0.05091E+01 9.07259E 05 20 77 2.19365E+02 2.20900E+02 7.097375+01 8.05091E+01 0.78122E 05- 28 77 2.20900E+02 2.22595B+02 7.897375+01 0.04091E+01 b.624765 05 28 77 2.22595E+02 2.24211E+02 7.897375+01 0.05091E+01 0.63056E 05 20 77 2.24211E+02 2.25026E+02 7.897375+01 0.05091E+01 8.651765 05 20 77 1.250263+02 2.27442E+02 7.097375+01 0.05091E+01 9.29476F 05 20 77 2.145185+02 2.16134E+02 0.05091E+01 8.22046E+01 9.482013 05 28 77 2.16134E+02 2.17749E+02 8.05091E+01 S.220465+01 8.59540E-05 28 77 2.177495+02 2.19365E+02 8.05091E+01 S.22046E+01 8.216193 05 20 77 2.19365E+02 2.30900E+02 0.05091E+01 8.220465+01 8.10389E 05 20 77 2.20980E+02 2.22595E+02 8.058915+01 0.22046E+01 7.84750E-05 28 77 2.22595E+02 2.24211E+02 8.05891E+01 0.22046E+01 7.71956E 05 20 77 2.24211E+02 2.25826E+02 0.05091E+01 8.22046E+01 7.90529E 05 28 77 2.25026E+02 2.27442E+02 8.05891E+01 8.22046E+01 8.50186E 05 20 77 2.145185+02 2.16134E+02 8.220465+01 8.38200B+01 0.65832E 05 28 77 2.16134E+02 2.17749E+02 0.22046E+01 8.30200E+01 7.04902E-05 20 77 2.17749E+02 2.19365E+02 0.22046E+01 8.38200E+01 7.64965E 05 20 77 2.19365E+02 2.20900E+02 8.22046E+01 8.30200E+01 0.00000E+00 20 77 2.20980E+02 2.22595E+02 8.22046E+01 8.38200E+01 7.54392E 05 28 77 2.22595E+02 2.24211E+02 8.220465+pl 8.38200E+01 7.15554E 05 28 77 2.24211E+02 2.258263+02 8.220465+b1 0.38200E+01 7.20601E 05 28 77
. 2.258265+02 2.27442E+02 8.22046E+01 0.30200E+01 7.74656E 05 20 77 2.145185+02 2.16134E+02 0.30200E+01 8.54354E+01 0.047623-05 28 77 2.16134E+02 2.17749E+02 0.38200E+01 8.54354E+01 7.28904E 05 28 77 2.17749E+02 2.19365E+02 8.38200E+01 8.54354E+01 7.00968E 05 20 77 2.19365E+02 2.20980E+02 8.38200E+01 0.54354E+01 7.15479E 05 20 77 2.20900E+02 2.22595E+02 8.38200E+01 0.54354E+01 0.00000E+00 28 77 2.22595E+02 2.24211E+02 S.30200E+01 8.54354E+01 6.765655 05 28 77 2.24211E+02 2.250265+02 0.30200E+01 S.54354E+01 6.712663-05 28 77 2.258265+02 2.27442E+02 8.38200E+01 0.54354E+01 7.19617E 05 28 77 2.145185+02 2.16134E+02 8.54354E+01 8.705093+01 7.675655-05 28 77 2.16134E+02 2.177493+02 8.64354E+01 8.70509E+01 6.98545E-05 28 77 2.177495+02 2.19365E+02 S.54354E+01 0.70509E+01 6.618283 05 20 77 2.19355E+02=2.20980E+02 0.54354E+01'8.70509E+01 6.526925 05' 20+ 77 2.20980E+02 2.22595E+02 8.54354E+01 8.705095+01 6.520623-05 28 77 2.22595E+02'2.24211E+02 8.54354E+01 8.70509E+01 6.38384E-05' 28 77
. gy ,
n ikh'l& & :M r j. . ;g 4" - s:
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Table 2.2.2.5 Fin Geometry and Power Distribution (cont' d) Pin Pitch Set 3 Relative Pin Pin Power Assemb. I Left I Right T Bot T Top Power Set Number 2.242115+02 2.250265+02 0.$?354B+01 0.705093+01 6.442393 05 20 77 2.250265+02 2.2's 442E+02 0.54354E+01 0.705095+01 6.072405 05- 20 77 2.14510E+02 2.16134E+02 0.705095+01 0.06663E+01 7.491605 05 20 77 2.16134E+02 2.177493+02 0.705095+01 0.06663E+01 6.900663 05 20 77 r2.177495+02 2.19365E+02-0.705095+01 0.066635+01.6.725705 05 20 77 2.19365B+62 2.20900E+02-0.705093+01 0.06663E+01 6.532735 05 20 77 2.20900E+02 2.22595E+02 0.705095+01 0.06663E+01 6.447435 05 20 77 2.22595E+02 2.242115+02 0.705095+01 0.06663E+01 6.434315 05 20 77 2.24211E+02 2.250265+02 0.705095+01 0.06663E+01 6.393435 05 20 77 2.250265+02 2.27442E+02 0.705095+01 0.06663E+01 6.722505 05 20 77 2.14510E+02 2.16134E+02 0.06663E+01 9.02010E+01 7.72940E-05 20 77 2.16134E+02 2.177495+02 0.06463E+01 9.02010E+01 7.669095 05 20 77 2.177495+02 2.19365E+02 0.06663E+01 9.02010E+01 7.560143 05 20 77 2.19365E+02 2.20900E+02 0.06663E+01 9.02010E+01 7.399025 05 20 77 2.20900E+02 2.22595E+02 0.06663E+01 9.02010E+01 7.301915 05 20 77 2.22595E+02 2.24211E+02 0.06663E+01 9.02010E+01 7.275925 05 20
- 77 2.242115+02 2.250265+02 0.06663E+01 9,02010E+01 7.157065 05 20 77 2.250263+02 2.27442E+02 0.06463E+01 9.02010E+01 6.969015 05 20 77 2.14510E+02 2.16134E+02 9.25902E+01 9.421375+01 9.796315 05 29 06 2.16134E+02 2.177493+02 9.25902E+01 9.421373+01 9.232295-05 29 06 2.177493+02 2.19365E+02 9.25902E+01 9.421375+01 0.730055-05 29 06 2.19365E+02 2.20900E+02 9.25902E+01 9.421373+01 0.267525-05 29 06
'2.20900E+02 2.22595E+02.9.25902E+01 9.421375+01 0.027533 05 29 06 2.22595E+02 2.24211E+02 9.25902E+01 9.421375+01 0.053523 29 06 2.24211E+02 2.250265+02 9.25902E+01 9.421373+01 0.31060E 05 29 06
'2.250265+02 2.27442E+02 9.25902E+01 9.421375+01 9.053115-05 29 06
~2.14510E+02 2.16134E+02 9.421375+01 9.50291E+01 9.076045 05 29 06 2.16134E+01 2.177495+02 9.421375+01 9.50291E+01 0.060923 05 29 36 2.177493+02. 2.19355E+02 9.421375+01 9.502915+01 7.621993 k 05 29 06 3 2.19365E+02 2.20900E+02 9.421373+01 9.50291E+01 7.210903-05' 29 06 2.20900E+02 2.22595E+02 9.421373+01 9.50291E+01 7.001695 05 29 . 86 2.22595E+02 2.242115+02 9.421373+01' 9.502915+01 7.015573 05 29 06 2.24211E+02 2.250265+02 9.421373+01 9.50291E+01 7.266425-05 29 06 2.250263+02 2.27442E+02 9.421375+01 9.502915+01 0.444935 05 29 06 2.14510E+02 2.16134E+02 9.502915+01 9.744465+01 0.304375-05 29 06
, 2.16134E+02 2.177495+02 9.50291E+019.744465+0117.379475-05 29 06 "2'.177493+02 = 2.19365E+02 ' 9 '.50291E+01 91744463+01" 6 ; 325005h 05 ' ' 29 ' ,"06' 2.19365E+02 2.20900E+02 9.50291E+019.744465+01 6.567895 05 29 06 2;20900E+02 ' 2.22595E+02 9.50291E+01 9.744463+01 = 6.462153-05 '29 ) 106-2.22595E+02 - 2.242115+02 9.50291E+01 9.744465+01 6.346325 05 29- 86 2.242115+02 2.250263+02-9.50291E+01 9.744465+01 6.656465-05 '29 :06 t 2.250265+02 = 2.27442E+02 9.502915+01 9.744463+01 7.796125-05.' ' 29 06 2.14510E+02 2.16134E+02 9.744465+01 9.90600E+01 7.514403-05 29~
06
;2.16134E+02 2.177495+02 9.744465+01.9.90600E+01 6.60750E-05.1 294, l66 A 2.177495+02 2.19265E+02 9.744465+01' 9.90600E+01 - 6.294333 05 : 29b ' 2 06 > -
wnW" qp2MHSS40f 2120900E+02' 9.7444634019190600E+01'6;207015 F OSM29R k TOG J 2.20900E+02 2.22595E+02 9.744465+01 9.90600E+01 0.00000E+00 29 Or 2.22595E+02 2.242115+02 9.744465+0L 9.90600E+015.,077425-05e29y W 86 n. ., j% j, 9g86Sg[g . @&hh, % {2.343115+02. R05 N$$h, 2.250263+03 n& Qpg o;9.744465+01 Q pgyycgg 9.90600E+01; , 6.052575 ,-
t. L Table 2.2.2.5 1 Pia Geometry and Power Distribution (cont' d) Pin Pitch Set 3 I-Relative Pin Pin Power Assemb. X Left X Right Y Bot Y Top Power Set Number 2.250265+02 2.27442E+02 9.744463+01 9.90600E+01 7.115005 05 29 06
-2.14510E+02 2.16134E+02 9.90600E+01 1.006755*02 6.090225 05 29 06 2.16134E+02 2.177493+02 9.90600E+01 1.00675E+02 4.163105 05 29 06 2.177A *P a *2 2.19365E+02 9.90600E+01 1.00675E+02 5.496115 05 29 06 2.193v. 02-2.20900E+02 9.90600E+01 1.00675E+02 0.00000E+00 29 06 2.20900E+02 2.22595E+02 9.9.0600B+01 1.00675E+02 5.629113 05 29 06 2.22595E+02 2.24211E+02 9.90600E+01 1.00475E+02 5.342695 05 29 06
- 2.24211E+02 2.250263+02 9.90600E+01 1.00675E+02 5.503693 05 29- 86
- 2.250263+02L2.27442E+02 9.90600E+01 1.00675E+02 6.500763 05: 29' 06 2.14510E+02-2.16134E+02 1.00675E+02 1.022915+02 6.493693 05 29 06 2.16134E+02 2.177495+02 1.00675E+02 1.02291E+02 5.034205 05 29 06 2.177495+02 2.19365E+02 1.00675E+02 1.02291E+02 5.492335 05 29 06 2.19355E+02 2.20900B+02 1.00675E+02 1.02291E+02 5.323255 05 29 06 2.20900E+02 2.22595E+02 1.00675E+02 1.022915+02 5.003775 05 29- 86 2.22595E+02 2.242115+02 1.00675E+02 1.022915+02 4.9967CE 05 29 06 2.24211E+02 2.250265+02 1.00675E+02 1.02291E+02 5.296255 05 29 06
-2.250265+02 2.27442E+02 1.00675E+02 1.02291E+02 6.194145 05 29 06 2.14510E+02 2.16134E+02 1.02291E+02 1.039065+02 6.200535 05 29 06 2.16134E+02 2.177493+02 1.02291E+02 1.039063+02 5.719465 05 29 06 2.177493+02 2.19365E+02 1.02291E+02 1.039065+02 5.40274E-05 29 06 2.19365E+02.2.20900E+02 1.022915+02 1.039065+02 5.231903 05 29 06 2.20900E+02 2.22595E+02 1.02291E+02'1.039065+02 5.070095-05 29 06 2.22595E+02 2.24211E+02 1.02291E+02 1.039065+02 5.053735 05 29 06 2.24211E+02 2.250265+02.1.02291E+02 1.039065+02 5.154605 05 29 06 2.250265+02 2.27442E+02 1.02291E+02 1.039065+02 5.051445-05 29 86 2.145185+02 2.16134E+02 1.03906E+02 1.05522E+02 6.513305 05 29 06 2.16134E+02 2.177495+02 1.039065+02 1.05522E+02 6.39700E 05 29 96 2.177495+02-2.19365E+02 1.039065+02 1.05522E+02 6.211305 05 29 48 a 2.19365E+02 2.20900E+02 1.039065+02 1.05522E+02 5.950193 05 29 26 2.20900E+02 2.22595E+02 1.039065+02 1.05522E+02 5.707093 05 29 06 2.22595E+02 2.24211E+02 1.03906E+02 1.05522E+02 5.69'674E 05 29 86 2.242115+02 2.250265+02.1.039065+02 1.05522E+02 5.617005-05 29 06-2.250263+02 2.27442E+02 1.039065+02 1.05522E+02 5.631643 05 29 06 1.99270E+02 2.00094E+02 1.07030E+02 ?s.69454E+02 1.196735 04 30- 93 .
2.00094E+02 2.025093+02 1.07030E+02 1.09454E+02-1.116553-04 30 93 2.035093+02 2.04125E+02:1.070385+02 1.09454E+02 1.057375-04 30- 93 2.04125E+02 2.05140E+02 1.07030E+02 1.09454E+02'1.002915-04 30 93 2.05740E+02-2.07355E+02 1.07030E+02 1.02454E+02 9.755575 05 30 93 J2.07355E+02 2.009715+03 1.07030E+02-1.09454B+02.9.032793-05 30 93 2.009715+02 2.105063+02-1.07030E+02 1.09454E+02.1.020005-04 130 93 2.105063+02 2.12202E+02 1.070385+02 1.09454E+02 1'.123243 04 30 '93
-1.99370E+02 2.00094E+02 1.09454E+02 1.110695+02 1.103275-04 30 93-
-2.00094E+02 2.025095+02-1.09454E+02 1.110693+02 9.062325 05' 30' 93
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y 1 Table 2.2.2.5 i Pin Geometry and Power Distribution (cont'd) j- Pin Pitch Set 3 l ll Relative Pin Pin Power Assemb. X Left X Right' Y-Bot _ Y Top Power Set Number i ! 2.025093+02 2.04125E+02 1.09454E+02 1.110693+02 9.342215 05 30 93 i 2.04125B+02 2.05740E+02 1.09454E+02.1.110695+02 0.06240E 05 30 93 ! 2.05740E+02 2.07355E+02 1.09454E+02'1.110695+02 0.64596E 05 30 .93 l 2.07355E+02 2.00971E+02 1.09454E+02 1.110695,02 0.720995 05 93 12.009715+02.2.105065+02 1.09454E+02 1.110695+02-9.136043 05 30 93 l _2.105063+02 2.12202E+02 1.09454E+02 1.110695+02 1.077233 04 '30 93 I 1~.99270E+02'2.00094E+02 1.110695+02 1.12605E+02 1.02660E 04 30 93 l 2.00094E+02 2.025093+02 1.11069R+02 1.12605E+02 9.100965 0C 30 93 , 2.025093+02 2.04125E+02 1.110693+02 1.12605E+02 0.513225 05 30 93 2.04125E+02 2.05740B+02 1.110695+02 1.126055+32 0.230043 05 30 93 i 2.05740E+02 2.07355E+02 1.110695+02:1.12605E+02 0.134695 05 30 93
- l. 2.07355E+02 2.00971E+02 1.110695+02 1.12605E+02 0.051665 05 30 93
- 2.00971E+02 2.105065+02 1.110695+02 1.12605E+02 0.534425-05 30 93 i 2.105065+02 2.12202E+02 1.110695+02 1.12605E+02 1.010135 04 30 93 l 1.992785+02 2.00094E+02 1.12605E+02 1.14300E+02 9.520453 05 30 93
! 2.00094E+02 2.025093+02 1.12605E+02 1.14300E+02 0.534425-05 30 93 ! 2.025095+02 2.04125E+02 1.12605E+02 1.14300E+02 0.050235 05 30 93 l 2.04125E+02 2.05740E+02 1.12605E+02 1.14300E+02 0.065545 05 30 93 l 2.05740E+02 2.07355E+02 1.12605E+02 1.14300E+02 0.00000E+00 30 93 ( 2.07355E+02 2.009715+02 1.12605E+02 1.14300E+02 7.611303 05. : 30 93
- . 2.00971E+02 2.105063+02.1.12605E+02 1.14300E+02 7.914135 30 .93 i 2.105065+02 2.12202E+02 1.12605E+02 1.14300E+02 9.472173-05 30 93
' 1.99270E+02.2.00094E+02 1.14300E+02 1.15915E+02 9.035095-05 30 93 2.00094E+02 2.025095+02 1.14300E+02-1.15915E+02 f.125105 05 30 93 l= 2.025093+02 2.04125E+02 1.14300E+02 1.15915E+02 7.778365 05 30 93 l 2.04125E+02 2.05740E+02 1.14300E+02 1.15915E+02'O.00000E+00 30- 93 !' 2.05740E+02 2.07355E+02 1.14300E+02 1.15915E+02 7.41775E-05 30 93 i '2.07355E+02.2.03971E+02 1.14300E+02 1.15915E+02 7.07900E 05__30 93 j, 2.00971E+02 2.105063+02 1.143CDE+02 1.15915E+02 7.447705-05 30 93 i 2.105065+02 2.12202E+02 1.14300B+02 1.15915E+02 0.090323-05 30 93 l 1.99270E+02 2.00094E+02 1.15915E+02'1.17531E+02 0.069005-05 30 53 , 2.00094E+02 2.025093+02 1.15915E+02-1.17531E+02.7.991605 05 30. 93 l 2.025095+02 2.04125E+02'1.15915E+02'1.175315+02 7.502293 05 30 93 l 2.04125E+02 2.05740E+02 1.15915E+02 1.17531E+02 7.239333-05. 93 l :2.05740E+02.2.07355E+02 1.15915E+02 1.175315+02 6.090403-05 30 93
- i. _2.07355E+02 2.009715+02.1.15915E+02 1.17531E+02 6.704333-05 30 93 i_ 2.00971E+02 2.105065+02:1.15915E+02'1.17531E+02 7.190705 05 30' 93-2.105063+02;2.12203E+02 1.15915E+02 1.175215+02 9.407235-05; 30 _
93 !- -1'99270E+02-2.00094E+02:1.175315+02 1.191465+02 0.907905-05-~30'
. 93
- 2.00094E+02 2.025093+02 1.175315+02 1.191465+02 0.15041E 05 30 93 3 '2.025095+02 2.04125E+02'1.175315+02 1.191463+02 7.760195 05 30. '93 j '2.04125E+02 2.05740E+02 1.175315+02 1.191465+02 7.33775E-05 30 93
- 2.05740E+02 ?2 L 07355B+02 1'.175315+02 r l'.191465+0S if s089403-05 " 30 ? w : 93 -
l_ vn - 4 - 2.07385E+02 2.009715+02 1.17531E+02 1.191465+02L6.997575-05' 30 s 93< - j- <
- 2.009715+02 2.105063+02 1.175315+02 :1.191465+02 7.110965 05 !,30f '93) l- 2.105063+02 2.12202E+02 1.17531E+02 1.191465+02't.103393 05' 30- -
93! _ ' 1.99270E+02 2.00094E+02 1.191465+02 1.20762B+02 9.739175-05 30 93 i' 1 ; 3,
- j. g, J M 7;;n2.00094E+02 2.025093+02 1.191463+02:1.20762E+02.9.463345-05 30 W,k 9 I $ $ $g6 e NNW ;4: , , 97 m p% nQgs@ppe:
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Table 2.2.2.5 4
- Pin Geometry and Power Distribution (cont' d)
Pin Pitch Set 3 Relative Pin ! Pin Power Assemb. ! Z Left X Right Y Bot Y Top Power Set Number I 2.04125E+02 2.05740E+02 1.19146E+02 1.20762E+02 8.60302E-05 30 93 l 2.05740E+02 2.07355E+02 1.191465+02 1.20762E+02 0.23487E 05 30 93 2.07355E+02 2.08971E+02 1.19146E+02 1.20762E+02 8.02000E 05 30 93 . 2.08971E+02 2.105065+02 %.19146E+02 1.20762E+02 7.84751E 05 30 93 2.105865+02 2.12202E+02 1.1914EE+02 1.20762E+02 7.834393-05 30 93
- 1.04030E+02 1.85654E+02 1.23070E+02 1.24694E+02 1.36159E 04 31 98 i 1.05654E'+02 1.87269E+02 1.23070E+02 1.24694E+02 1.29068E-04 31 98
- 1.872695+02 1.08885E+02 1.23078CbO2 1.246945&O2 1.23022E 04 31 98
! '1.88845E+02 1.90500E+02 1.230785+02,1.24694R+02 1.170135 04 31 98 l 1.90500E+02 1.92115E+02 1.23078E+02 1.24694E+02 1.13260E 04 31 98 l 1.92115E+02 1.93731E+02 1.23070E+02 1.24694E+02 1.11436E 04 31 98 1.93731E+02 1.953465+02 1.23070E+02 1.24694E+02 1.09743E 04 31 98 f 1.95346E+02 1.96962E+02 1.230785+02 1.24694E+02 1.090975 04 31 98 ! 1.840383+02 1.05654E+02 1.24694E+02 1.263093+02 1.265045-04 31 98 ! 1.85654E+02 1.07269E+02 1.24694E+02 1.26309E+02 1.133085 04 31 98 l 1.87269E+02 1.08805E+02 1.24694E+02 1.263095+02 1.07911E-04 31 90 j 1.00805E+02 1.90500E+02 1.24694E+02 1.26309E+02 1.026365 04 31 98 1 1.90500E+02 1.92115E+02 1.24694E+02 1.26309E+02 9.942125 05 31 98 ! 1.92115E+02 1.93731E+02 1.24694E+02 1.26309E+02 9.79298E 05 31 98 l 1.93731E+02 1.95346E+02 1.24694E+02 1.26309E+02 9.69300E 05 31 98 3 1.95346E+02 1.96962E+02 1.24694E+02 1.26309E+02 1.02914E 04 31 90 1.84030E+02 1.85654E+02 1.26309E+02 1.27925E+02 1.18290E 04 31 98 1.85654E+02 1.872695+02 1.26309E+02 1.27925E+02 1.05818E-04 31 98 ! 1.07269E+02 1.08805E+02 1.26309E+02 1.27925E+02 9.86137E 05 31 98 l 1.00085E+02 1.90500E+02 1.26309E+02 1.27925E+02 9.54643E 05 31 98 1.90500E+02 1.92115E+02 1.263095+02 1.27925E+02 9.37457E 05 31 98 , 1.92115E+02 1.93731E+02 1.26309E+02 1.27925E+02 9.05007E 05 31 98 1.93731E+02 1.95346B+02 1.26309E+02 1.27925E+02 9.06140E 05 31 98 ! 1.953465+02 1.96962E+02 1.26309E+02 1.27925E+02 9.65317E 05 31 98 1.840385+02 1.05654E+02 1.27925E+02 1.29540E+02 1.10792E-04 31 98 1.05654E+02 1.87269E+02 1.27925E+02 1.29540E+02 9.90301E 05 31 98 1.87269E+02 1.08885E+02 1.27925E+02 1.29540E+02 9.300455 05 31 98 i 1.88805E+02 1.90500E+02 1.27925E+02 1.29540E+02 9.40561E 05 31 90 } 1.90500W+02 1.92115E+02 1.27925E+02 1.29540E+02 0.00000E+00 31 90 } 1.92115E+02 1.93731E+02 1.27925E+02 1.29540E+02 8.62583E 05 31 98 i 1.93731E+02 1.953465+02 1.27925E+02 1.29540E+02 8.45145E 05 31 SS 1.95346E+02 1.96962E+02 1.27925E+02 1.295402602 8.99603E 05 31 98 1.84030E+02 1.05654E+02 1.29540E+02 1.31155E+02 1.06340E 04 31 98 1.85654E+02 1.072695+02 1.29540E+02 1.31155E+02 9.50983E-05 31 98 1.87269E+02.1.08085E+02 1.29540E+02 1.31155E+02 9.139375 05 31 98
-1.88085E+02 1.90500E+02 1.29540E+02 1.31155E+02 0.00000E+00 31 98 1.90500E+02 1.92115E+02.1.29540E+02 1.31155E+02 8.70153E 05 .31 98 1.92115E+02 1.93731E+02 1.29540E+02 1.31155E+02 0.10875E-05 31~ 98 1
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1 Table 2.2.2.5 Pin Geometry and Power Distribution (cont'd) Pin Pitch Set 3 Relative Pin Pin Power Assemb. I Left X Right Y Bot Y Top Power Set Number 1.93731E+02 1.953465+02 1.29540E+02 1.31155E+02 0.038045 05 31 90 1.95346E+02 1.96962E+02 1.29540E+02 1.31155E+02 0.54507E 05 31 90 1.040385+02 1.05654E+02 1.31155E+02 1.32771E+02 1.05291E 04 31 90 1.05454E+02 1.072693+02 1.31155E+02-1.32771E+00 9.435645 05 31 90
.1.072695+02 1.00005E+02 1.31155E+02 1.32771E+02 0.095095 05- 31 90 1.00005E+02 1.90500E+02 1.31155E+02 1.32771E+02 0.606903 05 71 90 1.90500B+02 1.92115E+02 1.31155E+02 1'.32771E+02 0.166543 05 31 90 1.92115E+02 1.93731E+02 1 71155E+02 1.32771E+02 7.062195 05 3 . 90 1.93731E+02 1.953465+02 1.31155E+02 1.32771E+02 7.90207E 05 31 90 1.953465+02 1.96962E+02 1.31155E+02 1.32771E+02 0.32931E 05 31 90 1.04030E+02 1.05654E+02 1.32771E+02 1.34306E+02 1.069195-04 31 90 1.05654E+02 1.072695+02 1.32771E+02 1.343063+02 9.664535 05 31 90 1.07269E+02 1.00005E+02 1.32771E+02 1.34306E+02 9.21036E 05 31 90 1.00005E+02 1.90500E+02 1.32771E+02 1.34306E+02 0.75024E 05 31 SS 1.90500E+02 1.92115E+02 1.32771E+02 1.343065+02 0.40754E 05 31 90 1.92115E+02 1.93731E+02 1.32771E+02 1.34306E+02 0.215495 05 31 90 1.93731E+02 1.95346E+02 1.32771E+02 1.34306E+02 0.020935 05 31 90 1.953465+02 1.96962E+02 1.32771E+02 1.34306E+02 0.31719E 05 31 90 1.04030E+02 1.05654E+02 1.343063+02 1.36002E+02 1.145005 04 31 90 1.05654E+02 1.072695+02 1.343065+02 1.36002E+02 1.106793-04 31 90 1.072695+02 1.00005E+02 1.343063+02 1.36002E+02 1.064955 04 31 90 1.00005E+02 1.90500E+02 1.34306E+02 1.36002E+02 1.01374E-04 31 90 1.90500E+02 1.92115E+02 1.34306E+02 1.36002E+02 9.76371E 05 31 90 1.92115E+02 1.93731E+02 1.343065+02 1.36002E+02 9.499245 05 31 90 1.93731E+02 1.95346E+02 1.343065+02 1.36002E+02 9.15901E-05 31 90 1.95346E+02 1.96962E+02 1.343063+02 1.36002E+02 0.770003 05 31 90 1.040385+02 1.05654E+02 1.30310E+02 1.39934E+02 1.066403 04 32 102 1.05654E+02 1.07269E+02 1.30310E+02 1.39934E+02 1.014725-04 32 102 1.072693+02 1.00005E+02 1.30310E+02 1.39934E+02 9.60560E-05 32 102 1.00005E+02 1.90500E+02 1.30310E+02 1.39934E+02 9.197043 05 32 102 1.90500E+02 1.92115E+02 1.30310E+02 1.39934E+02 0.060915-05 32 102 1.92115E+02 1.93731B+02 1.30310E+02 1.39934E+02 0.69713E-05 32 102-1.93731E+02 1.953465+02 1.30310E+02 1.39934E+02 0.562005 05 32 102 1.95346E+02 1.96962E+02 1.30310E+02 1.39934E+02 0.53609E 32 102 1.04030E+02 1.05654E+02 1.39934E+02 1.415495+02 9.975305-05 32. 102-1.05654E+02 1.072695+02 1.39934E+02 1.41549E+02 0.00211E-05 32 - 102 1.072693402 1.00005E+02 1.39934E+02 1'.415493+02 0.40591E-05 32' 102 1.00005E+02 - 1.90500E+02 1.39934E+02 1.415493+02 7.96051E 05 . 32 102 1.90500E+02 1.92115E+02 1.39934E+02'1'.415493+02 7;65693E-051232< '102 1.92115E+02 1.937315+02 1.39934E+02 1.415493+02 7.514605-05 32 102
-1.93731E+02 1.953465+02'1.39934E+02 1.415495+02 7.41109E 32 ~102 1.953465+02 1.96962E+02 1.39934E+02 1.415495+02 ^ 7.062055-05 . 32 102 1.04030E+02'1.05654E+02 1.415495+02L1.43165E+02:9.295443 321 102 V
1.05654E+02 1.072693+02'1.415493+02 1.43165E+02.0.220943-05, 32 l102 s +
/1.072693+02-1.00005E+02 1.415493+02 1.43165E+02'7.676363-05' 325 i102 -
1.00005E+02 1.90500E+02 1.415495+02 1.43165E+02 7.400533-05d 3S N 101 * > @ % 1.90500E+02 1.92115E+02 1.415493+02 1.43165E+02 7.00000E-05 32 102 x L1.92115E+02 1.93731E+02 1.415493+02 1^43165E+02
. 6.757203-051 32( 102q
' " ]{
~~
] ] .937315+02 1.953463+02 1.415495+02:1.43165E+0{
s 6.,007005-05j SS g 14)2l , y RgWQy w -? J- c
+ M' b\ MHkh y$$M%%,
. . c. . . . = . = _ . . , _a - .- -.~
Table 2.2.2.5 Fin Geometry and Power Distribution (cont' d) Pin Pitch Set 3 Relative Pin Pin Power Assemb. X Left X Right Y Bot Y Top Power Set Number i 1.95346E+02 1.96962E+02 1.41549E+02 1.43165E+02 7.23920E 05 32 102 1.04030E+02 1.05654E+02 1.43165E+02 1.44700E+02 8.505045 05 32 102 1.85654E+02 1.072695+02 1.43165E+02 1.44780E+02 7.58702E 05 32 102 1.072693+02 1.00005E+02 1.43165E+02 1.44700E+02 7.21405E 05 32 102 1.00005E+02 1.90500E+02 1.43165E+02 1.44700E+02 0.00000E+00 32 102 1.90500E+02 1.92115E+02 1.43165E+02 1.44780E+02 6.80145E 05 32 102 1.92115E+02 1.93731E+02 1.43165E+02 1.44700E+02 6.31466E 05 32 102 1.93731E+02 1.953465+02 1.43165E+02 1.447)0E+02 6.25031E 05 32 102
=1.953465+02 1.96962E+02 1.431655+02 1.44700E+02 6.640195 05 32- 102 i 1.840385+02 1.05654E+02 1.44780E+02 1.46395E+02 8.057415 05 32 102 1.85654E+02 1.07269E+02 1.44780E+02 1.46395E+02 7.11235E 05 32 102 1.072695+02 1.80005E+02 1.44700E+02 1.46395E+02 6.67527E 05 32 102 1.00805E+02 1.90500E+02 1.44700E+02 1.46395E+02 6.65306E 05 32 102 1.90500E+02 1.92115E+02 1.44700E+02 1.46395E+02 0.00000E+00 32 102 1.92115E+02 7.93731E+02 1.44780E+02 1.46395E+02 6.02975E 05 32 102 1.93731E+02 1.953465+02 1.44700E+02 1.46395E+02 5.075053 05 32 102 1.95346E+02 1.96962E+02 1.44780E+02 1.46395E+02 6.21927E 05 32 102 1.84030E+02 1.05654E+02 1.46395E+02 1.40011E+02 7.73591E 05 32 102 1.05654E+02 1.87269E+02 1.46395E+02 1.40011E+02 6.86403E 05 32 102 1.07269E+02 1.00005E+02 1.46395E+02 1.48011E+02 6.34948E 05 32 102 1.00005E+02 1.90500E+02 1.46395E+02 1.40011E+02 6.12409E 05 32 102 1.90500E+02 1.92115E+02 1.46395E+02 1.40011E+02 5.98908E 05 32 102
-1.92115E+02 1.93731E+02 1.46395E+02 1.40011E+02 5.74012E 05 32 102 1.93731E+02 1.953465+02 1.46395E+02 1.40011E+02 5.695135 05 32 102 1.95346E+02 1.96962E+02 1.46395E+02 1.48011E+02 5.99290E 05 32 102 1.84030E+02 1.85654E+02 1.40011E+02 1.49626E+02 7.56911E-05 32 102 1.05654E+02 1.072695+02 1.48011E+02 1.496265+02 6.012055 05 32 102 1.872693+02 1.00005E+02 1.40011E+02 1.496265+02 6.50014E 05 32 102 1.08805E+02 1.90500E+02 1.40011E+02 1.496265+02 6.19747E 05 32 102 1.90500E+02 1.92115E+02 1.40011E+02 1.49626E+02 5.90811E 05 32 102 1.92115E+02 1.93731E+02 1.40011E+02 1.49626E+02 5.06370E 05 32 102 1.93731E+02 1.953465+02 1.48011E+02 1.496263+02 5.72516E 05 32 102 1.95346E+02 1.96962E+02 1.40011E+02 1.496265+02 5.923763-05 32 102 1.840385+02 1.85654E+02 1.496263+02 1.51242E+02 7.70790E 05 32 102 1.05654E+02 1.072695+02 1.496265+02 1.51242E+02 7.58450E-05 32 102 1.072695+02 1.80885E+02 1.496265+02 1.51242E+02 7.35562E-05 32 102 1.88805E+02 1.90500E+02 1.49626E+02 1.51242E+02 7.07071E-05 32 102 1.90500E+02 1.92115E+02 1.49626E+02 1.51242E+02 6.067315-05 32 102 1.92115E+02 1.93731E+02 1.496265+02 1.51242E+02 6.73306E 05 32 102 1.93731E+02 1.953465+02 1.496265+02 1.51242E+02 6.507455 05 32 102 l '1.953465+02 1.96962E+02 1.496265+02 1.51242E+02 6.21447E-05 32- 102 1.840385+02 1.85654E+02 1.53550E+02 1.55174E+02.8.267393 05 33 105 1.85654E+02 1.872695+02 1.535595+02 1.55174E+02 7.718775 05 33 105 l
! m
+e -
m , .
? , y hn @ {:Q', > ,
g yy , , ,; , fic + r afk y;3 ,,, n l .
.- vm . c - . . nn . um hhktfib4kh@%MhDh?
- b '
? N I 'U b "
Table 2.2.2.5 Pin Geometry and Power Distributione (cont'd) Pin Pitch Set 3 Relative Pin Pia Power Assemb. E Left X Right Y Bot- T Top Power Set Number L 1.872695+02 1.80905E+02 1.535585+02 1.55174E+02 7.220625 05 33 105 1.00005E+02 1.90500E+02 1.53550E+02 1.55174E+02 6.764625 05 33 105 1.90500E+02 1.92115E+02 1.53550E+02 1.55174E+02 6.496113 05 33 105 1.92115E+02 1.937315+02 1.53550E+02 1.55174E+02 6.434295-05 33 105
.1'.93731E+02 1.953465+02 1.535385+02 1.55174E+02 6.535235 05 ' 33 105-1.953463+02 1.96962B+02 1.53550E+02 1.55174E+02 7.003355 05 33 105 '
1.04030E+02 1.85654B+02 1.55174E+02 1.567893+02 7.665703 05 33 105 1.05654E+02 1.072693+02 1.55174E+02 1.567895+02 6.69547E*05 33 105 1.072695+02 1.00085E+02 1.55174E+02 1.567895+02 6.246205 05 33 105 3 1.80005E+02 1.90500E+02 1.55174E+02 1.567895+02 5.043275 05 33 105 1.90500E+02 1.92115E+02 1.55174E+02 1.567895+02 5.605555 05 33 105 , 1.92115E+02 1.93731E+02 1.55174E+02 1.56789E+02 5.540525 05 33 105 1.93731E+02 1.953463+02 1.55174E+02 1.56789E+02 5.67066E 05 33 105 1.953465+02 1.96942M+02 1.55174E+02 1.56789E+02 6.533463 05 33 105 1.04030E+02 1.05654E+02 1.56789E+02-1.58405E+02 7.035905 05 33 105 1.05654E+02 1.87259E+02 1.56789E+02 1.50405E+02 6.12094E 05 33 105 1.072695+02 1.00005E+02 1.567895+02 1.58405E+02 5,50764E 05 33 105 1.80805E+02 1.90500E+02 1.56789E+02 1.50405E+02 5.310005 05 33 105 1.90500E+02 1.92115E+02 1.567895+02 1.58403E+02 5.163435 05 33 105 1.93115E+02 1.93731E+02 1.567893+02 1.584b5E+02 5.003943 05- 33 105 1.93731E+02 1.953463+02 1.567895+02 1.58405E+02 5.187153 05 33 105 1.953465+02 1.96962E+02 1,567895+02 1.50405F+02 6.029765 05 33 105 1.04030E+02 1.05654E+02 1.56405E+02 1.60020E+02 6.395175 05 33 105 1.05654E+02 1.072695+02 1.58405E+02 1.60020E+02 5.570405 05 33 105
'1.072693+02 1.00085E+02 1.50405E+02 1.60020E+02 5.166715 05 33 105 1.08805E+02:1.90500E+02 1.50405E+02 1.60020E+02 5.090325 05- 33 105 1.90500E+02 1.92115E+02 1.58405E+02 1.60020E+02 0.00000E+00* 33 105
, ,1.92115E+02 1.937315+02 1.58405E+02 1.60020E+02_4.639295-05 33 105
=1.93731E+02 1.953460,02 1.58405E+02 1.60020E+02-4.716513 05 33 105 1.953465+02 1.969622+02 1.58405B+02 1.60020E+02 5.508655 05 33 105 1.840385+02 1.85654E+02 1.60020E+02 1.61635E+02 5.098545 05 33 105-1.05654E+02.1.972695+02 1.60020E+02 1.61635E+02,5.156115-05 33 105 1.872693+02 1.08805E+02 1'.60020E+02 1.61635E+02 4.053293 05 33-105 1.80805E+02 1.90500E+02-1.60020E+02 1.61635E+02 0.00000E+00 33 105 1.90500E+02 1.92115E+02 1.60020E+02 1.61635E+02 4.513075-05 33- ,105
.1.92115E+02 1.937315+02 1.60020E+02 1.61635E+02 4.220135 05- 33, ._10 5 ,
1.937315+02 1.953465+02 1.60020E+02 1.61635E+02# 4;355895-059 33 1105' 1.953468+02 1.96962E+02 1.60020E+02 1.61635E+02-5.104135-05 33 .105
' 1.04030E+02 1'.05654E+02 1.61635E+02 1.63251E+02 5;569723 05: . 331 '105 1.05654E+02fl.072695+02;' 61635E+02 1.63251E+02 4.880365-05 . 33 - 105 1.072695+02 1.80805E+P2 1.61635E+02 11632515+02 4.521193 05~:33< 105 1.00005E+02 1.90500E+02 1.6163SE+02 1.63251E+02 4.326623 05 33- 105z
[ 1.90500E+02.1.92115E+02 1.61635E+02 1.632515+43fes073753-854 33 W itS % W x fy?!1,93115E+02.1.93731E+02:1.61635E+02 1.632515+02:3.953145-05lJ33 105
** i1.937315+02 '1.953465+02 1.61635E+02 1.632515+02 4.139373 405 ~ 33J 11051 1.953465+02 1.96962E+02 1.61635E+02'1.632515402.4.014935-05 "331 1054'
-1.040383+02 1.05654E+02 1.63251E+02 1.640663+02 5.379195 05 33 .105
- 1.85654E+02 1.072693+02 1.63251E+02 1.640665+02.4.783383 05 33' 105; o Qg M1.078693+4311'00085S+03.1.633515+03}1.648663+03$511345(05,{33g105 f
mev+ .
~wwwww wwgwwu
Tabb 2.2.2.5 Pin Geometry and Power Distribution (cont'd) Pin Pitch Set 3 Relative Pin Pin Power Assemb. I Left X Right Y Sot Y Top Power Set Number 1.00005E+02 1.90500E+02 1.63251E+02 1.640665+02 4.24536E 05 33 105 1.90500E+02 1.92115E+02 1.63251E+02 1.640665+02 4.063675 05 33 105 1.92115E+02 1.937315402 1.63251E+02 1.64966E+02 4.00335E 05 33 105 1.93731E+02 1.9534ES+02 1.63251E+02 1.648665+02 4.044245 05 33 105 1.953465+02 1.96962E+02 1.63251E+02 1.648663+02 4.564345 05 33 105 1.040385+02 1.85654E+02 1.64866E+02 1.66402E+02 5.523293 05 33 105 1 85654E+02 1.07269E+02 1.64066E+02 1.66482E+02 5.32620E 05 33 105 1.W72695+02 1.08805E+02 1.648665+02 1.66402E+02 5.10009E 05 33 105 1.00085E+02 1.90500E+02 1.640665+02 1.66402E+02 4.834613 05 33 105 1.90500E+02 1.92115E+02 1.540665+02 1.66402E+02 4.64736E 05 33 105 1.92115E+02 1.93731E+02 1.648663+02 1.66402E+02 4.54163E 05 33 105 1.93731E+02 1.953465+02 1.640665+02 1.66482E+02 4.44144E 05 33 105 1.95346E+02 1.96962E+02 1.64066E+02 1.66482E+02 4.424285-05 33 105 1.68790E+02 1.70414B+02 1.68790E+02 1.70414E+02 8.013003 05 34 106 1.70414E+02 1.72029E+02 1.68798E+02 1.70414E+02 8.36696E 05 34 106 1.720293+02 1.73645E+02 1.687985+02 1.70414E+02 7.66050E 05 34 106 1.73645E+02 1.75260E+02 1.68790E+02 1.70414E+02 7.548853 05 34 106 1.75260E+02 1.76075E+02 1.687985+02 1.70414E+02 7.19469E 05 34 106 1.76075E+02 1.78491E+02 1.68790E+02 1.70414E+02 7.07403E-05 34 106 1.78491E+02 1.801065+02 1.68790E+02 1.70414E+02 6.90945E 05 34 106 1.80106E+02 1.81722E+02 1.60790E+02 1.70414E+02 7.31156E 05 34 106 1.687985+02 1.70414E+02 1.70414E+02 1.72029E+02 8.36696E 05 34 106 1.70414E+02 1.72029E+02 1.70414E+02 1.72029E+02 7.61801E 05 34 106 1.72029E+02 1.73645E+02 1.70414E+02 1.72029E+02 6.93267E 05 34 106 1.73645E+02 1.75260E+02 1.70414E+02 1.72024E+02 7.182575-05 34 106 1.75260E+02 1.76075E+02 1.70414E+02 1.72029E+02 6.86982E 05 34 106 1.76875E+02 1.78491E+02 1.70414E+02 1.720295+02 6.80065E 05 34 106 1.70491E+02 1.80106E+02 1.70414E+02 1.72029E+02 6.'344515 05 34 106 1.80106E+02 1.01722E+02 1.70414E+02 1.72029E+02 7.06098E-05 34 106 1.687985+02 1.70414E+02 1.72029E+02 1.73645E+02 7.66850E 05 34 106 1.70414E+02 1.72029E+02 1.720295+02 1.73645E+02 6.93267E 05 34 106 1.720295+02 1.73645E+02 1.72029E+02 1.73 645E+02 6.90467E-05 34 106 1.73645E+02 1.75260E+02 1.72029E+02 1.73645E+02 C.60452E-05 34 106 1.75260E+02 1.76875E+02 1.72029E+02 1.73645E+02 6.44751E-05 34 106 1.76875E+02 1.78491E+02 1.72029E+02 1.73645E+02 5.24418E 05 34 106 1.78491E+02 1.801065+02 1.720295+02 1.73645E+02 6.44978E 05 34 106 1.001063+02 1.81722E+02 1.72029E+02 1.73645E+02 6.88824E 05 34 106 1.687985+02 1.70414E+02 1.73645E+02 1.75260E+02 7.54885E-05 34 106 1.70414E+02 1.720295+02 1.73645E+02 1.75260E+02 7.18257E 05 34 106 1.72029E+02 1.73645E+02 1.73645E+02 1.75260E+02 6.60452E 05 34. _106 1.73645B+02'1.75260E+02 1.73645E+02'1.75260E+02 6.49143E 05 13 4 106
- 1.75260E+02 1.76875E+02 1.73645E+02 1.75260E+02 0.00000E+00 34 106 1.76075E+02 1~.78491E+02 1.73645E+02 1.75260E+02 5.87096E 05 34 '106 en aae~ -
+
. 7pp e 3 + -
q u(;
, y fi @ yst gv_.
i ,
& $ **r
% k-} i i, # ; .-
W4E6% hIS46M W % + w > 96mS:.edw h . - * ' ' > W u I H Mht.c &
Table 2.2.2.5 Pia Geceetry and Power Distributions (cont'd) Pin Pitch Set 3 Relative Pia Pia Power Assemb. l
' I Left X Right Y Bot Y Top Power Set Number '
'1.70491E+02 1.001065+02 1.73645E+02 1.75260E+02 5.94164E 05 34 106 1.001063+02 1.01722E+02 1.73645E+02 1.75260E+02 6.406365 05 34 106 1.60790E+02 1.70414E+02 1.75260E+02 1.76075E+02 7.194693 05 34 106 1.70414E+02 1.720293+02 1.75260E+02 1.76075E+02 6.069025 05 34 106
-1.720295+03 1.73645E+02 1.75260E+02 1.76075E+02 6.447513-05 34 106 1.73645E+02 1.75260E+02 1.75250E+02 1.76075E+02 0.00000E+00 34 106 1.75260E+02 1.76075E+02 1.75260E+02 1.76075E+02 5.64701E 05 34 106 1.76075E+02 1.70491E+02 1.75260E+02 1.76075E+02 5.411795 05 34 106 1.70491E+02 1.001063+02 1.75260E+02 1.76075E+02 5.501933 05 34 - 106 1.001068+02 2.01722E+02 1.75260E+02 1.76075E+02 6.042365 05 34 106 1.60790E+02 1.70414E+02 1.76075E+02 1.70491E+02 7.074033 05 34 106 1.70414E+02 1.720295+02 1.76075E+02 1.70491E+02 6.000655 05 34 106 1.720295+02 1.73645E+02-1.76075E+02 1.70491E+02 5.24410E 05 34 106 1.73645E+02 1.75260E+02 1.76075E+02 1.70491E+02 5.070965 05 34 106 1.75260E+02 1.76075E+02 1.76075E+02 1.70491E+02 5.411795 05 34 106 1.76075B+02 1.70491E+02 1.76075E+02 1.704915+02 5.193455 05 34 106 1.70491E+02'1.001065+02 1.76075E+02 1.70491E+02 4.071105 05 34 106 1 9010!M+02 1.01722E+02 1.76075E+02 1.7t491E+02 5.492025 05 34 106
-1.60790E+02 l'.70414E+CJ 1.70491E+02 1.001065+02 6.909455 05 34 106 1.70414E+02 1.7202sE+02 1.78491E+02 1.001063+02 6.344513 05 ' 34 106 l'720295+02 1.73645E+02 1.70491E+02 1.001065+02 6.44970E-05 24
. 106 1.73645E+02 1.75260E+02'1.70491E+02 1.00106E+02 5.541645-05 34 106 1.75260E+02 1.76075E+02 1.704915+02 1.001065+02 5.501933 05 34 106 1.76075E+02 1.704915+02 1.70491E+02 1.001063+02 4.071105 05 34 106 1.70491E+02 1.001063+02 1.70491E+02 1.001065+02 4.902675 05 34 106
'1.001065+02 1.01722E+02 1.70491L+02 1.001063+02 5.413015 05 34 106 1.60790E+02 1.70414E+02 1.00'065+02 1.01722E+02 7.311563-05 34 106 1.70414E+02 1.720295+02 1.001065+02 1.017223402 7.069905-05 34 106 1.720295+02 1.73645E+02 1.001065+02 1.01722E+02 6.000243 05 34 106 1.73645E+02 1.75260E+02 1.001065+02 1.01722E+02 6.406365 05 34 106 1.75260B+02 1.76075E+02 1.00106E+02 1.01722E+02 6.042365 05 34 106 1.76075E+02 1.70491E+02 1.001065+02 1.01722E+02 5.492025-05 34 106 1.70491E+02 1'.001065+02 1.001063+02 1.01722E+02 5.413015 05 34 106
'1.001065+02 1.01722E+02 1.001063+02.1.01722E+02 5.255295 05 34 106 i_ f f f I.
I { %. -x 4
- y-
$ l m Y _W % -- ? . , .O f '. '_ y 7 ,upM M iy g a
s m q% 3 . w% Ln-
~ e n.3-dvRNkWi%9- iv
-i s
gg,
}-T GNr (h@zdNOf M4dM hidMQ
~
i Table 2.2.2.6 Arial Power Distributions t E*** Eadial Zone Axial Roundary(cm) 1 2 3 0.000E+00
. .0000 1 4.9430E+01..
. .00H 2- 6.4670E+01 3 7.9910E+01
. .0340 4 9.5150E+01
- 319 0.0430 0.0372 5 1.1039E+02
* . 9 .0383 6 1.2563E+02 7 1.4087E+02 8 1.5611E+02
* * . OS 9 1.7135E+02 10 1.0659E+02 0.0430 11 2.0183E+02
. . 0.0M3 12 2.1707E+02
* . .0457 13 2.3231E+02 1$ 2.4755E+02
* . 0.0488 15 2.6279E+02
* .50 16 2.7803E+02
. 0.05H 17 '2.93275+02 0.0516 18 3.08515+02
. 0.0516 19 3.2375E+02-ww a e.,,. 4 e U -
0.0430 0.0470 0.0507~ , ,
. ' . . 0.0412 0.0450 0.0491 ;. a g;,
~
,21:'3.5423E+02 0.0374 0.0414 0.0462 22 3.69473+02
,c
. , vyr,t: ::3 :: 4; ,, , __
@muan
^-Y +
sip _
,,h, <
,. . aggb. ~ . .
\ " * ^ '~
^' '
idyg'd ' 4.. :(p ,; W '4 + t jy i ,.g.gg 4g.g, 3 [ _
- I
l l Table 2.2.2.6 l Axial Power Distributions (cont'd) Lone Rcdial Eone Asial Bo mdary (cm) 1 2 3 22 3.69475+02 0.0340 0.0373 0.0415
- 25. 3.0471E+02-0.0293 0.0309~ 0.0347 24 3.9995E+02 0.0214 0.0226 0.0258 25 4.15195+02 0.0091 0.0090 0.0112 26 4.3043E+02 0.0000E+00 0.0000E+00 0.0000E+00 27 8.1323E+02 Eona Radial Radial-Eone Boundary (cm) 1 220.282 2 234.074 3 259.530 t
?
+ .- Fy ,e -; w ) 't if f. k
< a:t,
+
p [ r. -- . 9 h Y-{ [' ( , , 4. * * - a p' g', ;
,,@. -{ [ E
, rv, a'
,pp . - t 't 'h--,
s-F up. - dikw sc; -
., a, 4,;p jg g. gl'4g y),, _ -
w, I
%dQ:t'J
, yg .r p;. J ,. . , :.a; JQ.uqiic5];$q.u:.61, .
Table 2.2.2.7 Edit Locations
. R (cm) E (ca) 8(degrees).
. Pressure Vessel Capsules .
. Fluz Spectrum and .
. Peak Reaction Rates 319.195 306.605 3 .
. Pressure Vessel 0T .
. (A) Axial Peak Location .
. (a) E > 1.0 MIV 321.786 306.605 0 45 .
. (b) E > 0.1 NEY 321.786 306.605 0 45 .
. (c) DFA Rates 321.786 306.605 0 45 .
. , (d) Flux Spectrum 322.286 306.605 42.51 .
. (E) At the Axial Core Midplane .
.- (a) E > 1. 0 MIV 321.786 239.93 0 45 .
. (b) E > 0.1 MBV 321.786 239.93 0 45 .
. (c) DPA Rates 321.786 239.93 0 45 .
. Pressure vessel 1/4 T: .
. (A) Axial Peak Location .
. (a) E > 1.0 MIV 325.818 306.605 0 45 .
. (b) E > 0.1 DGnr 325.818 302.795 0-45 .
. (c) DPA Rates 325.818 298.985 0-45 .
. (d) Fluz Spectrum 325.818 306.605 42.51 .
. (E) At the Axial Core Kidplane .
. (a) E > 1.0 MIV 325.818 239.93 0 45 .
. (b) ED 0.1 DGnr 325.818 239.93 0 45 .
. (c) DPA Rates 325.818 239.93 0-45 .
. Pressure vessel 1/2 T .
. (A) Axial Peak Location .
. (a) E > 1.0 MIV 329.851 306.605 0 45 .
. (b) E > 0.1 MIV 329.851 306.605 0-45 .
. (c) DPA Rates 329.851 306.605 0-45 .
. (d) Plum Spectrum 329.851 306.605 42.51 .
. -(E) At the Axial Core Midplane .
. (a) E > 1.0 MIV 329.851 . 239.53 0-45 .
. (b) E > 0.1 MIV 329.851 239.93 0-45 .
. (c) DFA Rates 329.851 239.93 0 45 .
. Pressure vessel 3/4 T .
. (A) Axial Peak Location .
. (a) E > 1.0 MIV -333.883 302.795 0 45 .
. (b) E > 0.1 N37 333.883 302.795 0-45 .
. (c) DPA Rates 333.883 298.985 0 45 .
. - (d) Flux Spectrum 333.883 302.795 42.51 .
. .(E) At the Axial Core Midplane .
. (a) E > 1.0 MIV 333.883 239.93 0 45 .
.. (b) I > 0.1 MIV 333.883 239.93 0 45 .
. -(c) DPA Rates 333.883 239.93 0-45 .
D /y 4 p *5 * " " '- , S' (N , t
*l lM Mfl ~ r
+
14 & l: + . _ j g :_ m Q _ s . +., . i$w
, 4gg M &: > '
ar - >
,3 i, s gygy : gpygg a
I Table 2.2.2,7 Edit Locations (cont'd)
.- R (ca) E(ca) 8(degrees).
. Pressure Vescel T .
. (A) Axial Peak Location .
. (a) E > 1.0 NEY 337.5L5 302.795 0 45 ..
. . (b) E > 0.1 MBV 337.215 302.795 0 45 .
. (c) DFA Rates - 337.915- 298.985 0 45 .
. (d) Flux Spectrum 337.032 302.795 42.51 .
. (3) At the Axial fore Midplane . ,
. (a) E > 1.0 MIV 337.915 239.93 0 45 .
. (b) E > 0.1 MIV 337.915 239.93 0-45 '
. (c) DPA Ratte 337.915 239.93 0 45 .
. DowuComer ,
. (A) Azial Peak Location .
. (a) E > 1.0 MEV 278.100 30C.605 0 45 .
. (b) E > 0.1 MIV 278.100 306.605 0 45 .
. (c) DFA Rates 278.100 306.605 0 45 .
. (d) Flux Spectrum 278.100 306.605 23.5 .
. (E) At tho' Axial Core Midplane .
. (a) E > 1.0 MCV 278.100 239.93 0 45 .
. (b) E > 0.1 MIV 278.100 239.93 0 45 .
. (c) DPA Rates 278.100 239.93 0-45 .
. Cavity .
. (A) Azial Peak Location .
. (a) E > 1. 0 MIV - 397.700 282.602 0-45 .
. (b) E > 0.1 MIV 398.700
- 279.554 0 45 .
. (c) DPA Rates 398.700 279.554 0 45 .
. (d) - Flum Spectrum 398.700 282.602 44.975 .
'f h 'f,
- g 4 1 '4 5 h.4 4 ',( .
' ' ' ,- g -N f ,._
N ( .' -' w, e,d } M 4. j$ hle % *F k( 5' '- . *5 . I 3
'5
^
C -I I 4 ^ l' ~
.h g--
.A -. 1 m
). .
F c , .
- - ' ', b .
l 5 b' il .v' $- ~ ,
a s l 1 L . i
. 3 DORT CALCULATIONAL METIIODOLOGY 1
6 3.1 Introduction 3.3 Core Neutron Source
- The methodology used to perform the pressure vesse.1 The benchmark calculation of the core neutron source i Guence benchmark problems follows the methods and includes the effect of the strong pin-wise variations of i approach described in the pressure vessel fluence the power distribution in the fuel assemblies located near
! , ' caLulationandmeasurementmethodsRegulatoryGuide- the core boundary. The MESH code was used to allocate i 1053. The modeling and aumerical i wwd e.used in the pin-wise power to the individual (r, 0) mesh blocks.
- these calculatmas are based on well established state-of. - This allocation was performed by a numerical integration , the art techniques and, except for nuclear data - of the power distribution, defined on the (x,y) pin-wise j uncertainties, are believed to provide a flux solution mesh, over the (r,0) mesh block. This numerical 1
accuracy of a few percent, it is intended that the flux integration typically employed 2100 integration mesh per ,
- solutions to thsee h= h= ark problems will be updated - iWil P in and was shown to be securate to withm sl% for .
- 'as signiacant improvements are made in the basic ' each (r,0) mesh block.'-
- _ mohads and in the nuclear data sets.
The magnitude of the core neutron source increases with ' }i The nuclear cross sections, determination of the core fuel burnup due to the higher number of neutrons '
- l. neutron source, transport calculations, synthesis Produced per MeV of energy by a Pu fission. This was approach, and the dosimetry cross sections are described taken into account by calculating the number of neutrons E in the following sections, per MeV, vAc [ neutrons /MeV1, using the fbel burnup
! d-uwt isotopic fission fractions. In addition, the } fission spectrum was also considervd to be d- +t ou 3.2 the fuel burnup in order to account rer the harder more Neutron Cross Sections and , peaetrating neutron spectnan charactenstic of the Pu Fission Spectra fissions in the high burnup fuel, his exposure dep-imne was included in both the radial (r,0) and The BUGLE 93 47 group cross section Hbrary was used exial(r,z) source distributions. in the benchmark calculations. The BUGLE-93 library
.was determined . by. callapsing the ENDF/B VI VITAMIN-B6 Anc-group cross 'section set using 3.4 Neutron Transport Calculations spatially dependent spectra calculated for a typical PWR -
. conAguration. . The BUOIA93 library includes the The neuuan transport calculations for the bencinark ENDF/B-VI versons of the iron, hydrogen and oxygen probians wwe performed with the ORNL DORT cross marcia== which are known to have a signiBcant discrete ordinates tianaport code using the 47-group
.e8bct on presasse vessel Duence pr=h-BUGLE-93 library, including the ENDF/B-VI fron, oxygen and hydro-gen cross sections. The ca'culations The Sision spectra for U-235, U 23g, PU-239 and were p.1 d in a fixed source mode for a radial (r,0)
Pu-241 are provided in Table-3.2.1 and were used in the plane, an axial (r,z) plane, and in a one dimenmonal (r) MESH, 5) calculations of the core neutron geometry, The PWR radial (r,0) calailarians were7
""'88-performed in a two step " boot strap" fashion in which an inner oeo eighth 45' nia=*h=1 sector was first cakadated. A second outer = ?h core 45' annular da :V$ ,
sector was then calculated using the Bux on the inner : surface of the annulus, calculated in the Srst inner 14hs ENDPS VI Aselon spects for U-235, U-238, Po 239.' calantarian as an input boundary anadiriaa ' A ~15 cm
~and P0-241 were processed wkh NJOY (Reference.6) and radial overlap-region between the inner and outer
=l=het== wese perfenmed wkh both the ENDP/B-VI and cannilaela== was maintainai to insmo that the neglect of hbis 3.2.1 spectra.- Dese calculadcas lahah the the outer geoenetry in the inner problem had a negligible l> 1.MeV and >0.10 MeV fluences ngreed to within
. eSect (s0.5%) on the vessel fluemme calml=ela== :In the i 51.0% {~
, 3-1 ,
. NURBO/CR-6115) aaw 4 gf : n+: , ,
+ -
n- n e? bhY m.wmye%%
.' w muwm%imen W ? m; t@M@ issNO Mnaim MOW 9' %MUNNNN MbY
--- . . . . . - - .---- - - . .... - .. - _ - .. - ~._ ~ - . - _ - . - .- - .
- 3. DORT Calculational Methodology - j BWR calculations, the butstrap method was not ud 3.5 Flux Synthesis and the solution on the full radial (r, 0) geometry was
&ned in one step.
The vessel Duxes were determined by combining the DORT (r,0) and DORT (r,z) calculated fluxes. The flux JThe calculations were performed using an S. quadrature 1 at the (r,0,z) location was determined by the relation and a P 3 angular decomposition of the scattering cross- ( sections tti in the PWR calculation, the (r,0) mesh s included 61 angular mesh intervals, and 108 and 102
$,(r,6,1) = $/r,6)($,(r,ry$,(r)], (1) radial mesh intervejs in the inner and outer bootstrap calculations, respectively, la the BWR calculation, the
' (r,0) mesh included 61 angular mesh intervals, and 222 where $,(r,6), 4,(r,r) and $,(r) are the group-g radial mesh intervals. '!he angular (0) and radial (r) mesh fluxes calculated in the indicated geometry, The
,goctive core radius R.,used in the cylindrical geometry Mties wue incresW at material interfaces where the (r,z) and (r) calculations was determined so that the Dux geometry was changing rapidly and at the capsule above 1 MeV (y at the vessel inner-wall satisfies the -
locations. The radial mesh used in the axial (r,z) calculations was amantinity identical to that used in the caddon , (r,0) calcula: ions. The spatial mesh used in the i calculations is given in Chapter 4 with the calculated 3*
- 1 resuks.
@ >'i(r;Rc)g @ >i(r,e)dB. (2) o Vacumn boundary conditions were used on the outer
' radial and axial boundaries ofthe pt oblems and reflecting The radial source distribution in these cylindrical :
boundary conditions were used on the internal 0 = 0' and calculations was determined as an azimuthal average of 0 = 45' azimuthal boundaries. A pointwise flux- the (r,0) source distribution. convergence of103was used together with anintegrated Aux convergence criteria of104 In the case of the PWR partial length shield assembly
- core design, equation (2) was applied separately to the In a' nier to validate the numencal methods used in theseaxial core regions above and below the partial length
~t~iah. DORT _ sensitivity calculations ,were shield material interface at z = 109,102 cm.
performed for selected numerical input parameters. The sensavitycalculations included an increase in the angular quadratum Aom S to Si, an inemm in the angular repe==aatariaa of the scattering crees sections hem P3 to - 3.6 Dosimetry Cross Sections P3 , and a factor of 10 increase in the flux pointwise - convergence *The results of these calculations am g g , ,,, ,,, ,,jm pneonted in Table 3.4.1, and indicate that the >l MeV using ENDF/B-VI cross sections. The cmss section data and >0.1 MeV fluxes vary by less than 2% at all (r,0) were collapsed to the 47-group structure using NJOY,
,lhe calculated reaction rates are for dosunster matenals a henthenumericatinputparsinesenamW w
having a 90% response range above 0.1 MeV, and include those reactions that are typically used to =
' determine the pressure vessel fluence above 0.1 McV.
'lhe specific donimear reas, response ranges and cornoponding halflives are given in Chapter 4 with the hanchmarer caimineian results ntWhde the BWR (r,0) sad (r) aal-lan=== were -
perfonned using an S, quadrature, the BWR (r, z) , nal=1= aman were performed using an Su quadrature. .
., , ,, ,2 s, ,. w , .
ygm,
>;) U 3 '
} ff 4
4 qu m.pn.- us m.6,; : m, y . . gg wnM, , WQdWg4g49 g%W
- ggy,j u
-- . p. y ; ,3 o .
hh %hh Jh7 d- E * ' " " I# ' _ u
I Tabb 3.2.1 Benchmark Problem Pission Spectrum by Isotope Group U 235 U 238 Pu 239 Pu 240 Pu 241 lu-242 1 5.01790E 05 2.55580E 05 5.62080E 05 1.59837E 04 1.11229E 04 9.41379E 05 2 2.01670E 04 1.38950E 04 2.26770E 04 4.24436E 04 3.33440E-04 2.935732-04 3 1.14600E 03 9.23970E 04 1.29210E 03 1.90310E 03 1.62701K 03 1.461tBE 03 4 2.52230E 03 2.30120E 03 2.93940E 03 3.67560E 03 3.33202E 03 3.05379E 03 5 5.65690E 03 5.39710E 03 6.47000E-03 7.23358E 03 6.020213 C3 6.35974E 03 6 1.61470E 02 1.59700E 02 1.81090E 02 1.8326bE-02 1.7s f 42E 01 1.70033E 02 7 3.07130E 02 3.13400E 02 3.40160E 02 3.19116E 02 3.22692E 02 3.09993F 02 0 .8.05130E 02 8.35720s 02 8.77920E 02 7.78502E-02 8.08065E 02 1.86116E 02 9 7.67500E 02 7.07770E 02 0.12310E 02 7.04721E 02 7.41343E 02'1.313365 02 10 4.40110E 02 4.45130E 02 4.55610E 02 3.95926E-02 4.17697E 02 4.14407c 02 11 4.66870E 02 4.67790$ 02 4.765F0E 02 4.15580E-02 4.38337E C2 4.36?16E-C2 12 2.00290E 02 1.99590E 02 2.02720E 02 1.78618E 02 1.08091E 02 1.87651C 02 13 4.02620E-03 4.00560E 03 4.04740E 03 3.46967E 03 3.65159E 03 3.C457CE 13 14 2.43450E-02 2.41820E 02 2.45230E 02 2.17653E-02 2.2P679E-02 2.2670U:-02 15 7.35500E 02 7.28080E 02 7.34400E 02 6.58307E 02 3.89709E 03 6.910d*4E 02 16 7.19480E 02 7.11800E 02 7.12330E 02 6.52904E-02 6.7946:E 02 d.93101I 02 17 8.94980E 02 6.88220E 02 8.80130E 02 8.3G931E-02 8.629042 02 t.7C231E 02 18 1.15030E 01 1.14380E 01 1.11580E-01 1.14986E-01 1.13412E 01 1.14737T-01 19 6.26870E 02 6.21080E 02 5.98610E-02 6.61640E 02 6.31523E 02 6.40114E 02 20 2.72400E 02 2.68800E 02 2.57760E C2 2.93997E 02 2.773163 32 2 01294F-02 21 4.68520E 02 4.60320E-02 4.39290E 02 5.13975E-02 4.20479E 02 4.876470-c2 22 3.76160E 02 3.68060E 02 3.49500E 02 4.21326E 02 3.91602E 02 *s.96966E-02 7 23 4.17720E 02 4.10120E-02 3.88410E 02 4.79967E 02 4.44999E C2 4.50850C-02 l 24 2.13900E 02 2.12210E-02 2.02000E 02 2.51519E-02 2.3354 8E 02 2.3(67EE 02 25 3.00470E 02 3.028605-02 2.96650E 02 3.60326E-02 3.38053E 02 3.42313E 02 26 1.54080E 02 1.58020E-02 1.50480E 02 1.87262E 02 1.80121E 02 1.82293E-C2 27 7.42510E-03 7.72090E 03 7.49710E-03 8.99821E 03 8.92036E 03 9.03624E 03 l 28 3.54620E 03 3.72200E-03 3.55110E 03 4.24394E 03 4.31820E-03 4.363312 03 1 29 9.98080E 04 1.05290E-03 9.96940E-04 1.18278E 03 1.23205E C3 1.24343E 03 30 5.69770E 04 6.02400E 04 5.63780E 04 6.71909E .04 7.10591E 04 7.* 46UOE 34 31 1.73370E 04 1.83510E 04 1.74090E 04 2.C3574E-04 2.17201E 04 2.1SC432 04 32 2.03050E-04 2.15060E 04 2.12840E 04 2.38119E 04 2.55417E-04 2.56065E 04 33 5.40380E-04 5.73110E-04 5.30120E-04 6.32934E-04 6.90362E-04 6.88273E 04 34 4.84200E-04 5.1466CE 04 5.19380E-04 5.59177E 04 6.22162E 04 6.19155E 04 35 1.57460E-04 1.67660E 04 1.57790E 04 1.78267E 04 2.00672E-04 2.00929E 04 36 5.11560E 05 5.45120E-05 5.33090E-05 5.76396E 05 6.58773E 05 5.62128E-05 37 2.08270E 05 2.21990E-05 2.19810E 05 2.35810E-05 2.84631E-05 2.7634SE 05 38 2.54840E-06 2.71460E 06 2.65010E-06 2.95265k C5 3.76926E 06 3.55021E 06 39 8.27310E-07 8.80310E-07 8.62760E 07 9.93296E 07 1.34411E-06 1.21832E 0G l 40- 3.09000E 07 3.28840E 07 3.14170E 07 3.97077E-07 3.76995E C7 4.99475E-07 41 6.00000E-08 7.96970E-08 6.14480E 08 1.14164E 07 1.82060E-07 1.4855BE-07 42 5.40660E-12 9.55630E 09 2.176555-11 1.93115E 0S 3.30303E-08 2.572672 08 43- 0.00000E+00 2.67170E-09 8.29070E-12 4.59724E 09 9.115503 09 4.77114E 09 44 . 0.00000E+00 2.16310E 11 6.85750E 13 1.54375E 09 2.79927E C9 1.4G516E 09 i 45 0.00000E+00 0.00000E+00 0.00000E+00 8.08059E-10 1.32100E-09 6.91426E *0 46 0.00000E+00 0.00000E+00 0.00000E+00 7.18356E 10 8.97226E 10 4.69930E 10
. 47 0.00000E+00 0.00000E+00 0.000002 00 5.2210'7E-10 2.85903E-10 l'.45644E 10 l
, qq
{)9% 4
'Nd-
[ 4 7{ t j % 47 +
, s. W , 39; 5- , 2
); Table 3.4.1 A
Sensitivity of the DORT Calculated Hux to Nummerical Input W+
; Sandard Problesa (r,0) Cale dans==
i , 14caden r=201.25 m r=215.43 cum r=219.393 ces r=224.473 cum r =229.870 can r=235.2ES cm r=240.342 can r=320.06 ces - 0 -20* 8 = 28' 9 = 15.5* 8 = 15.5* 8-15.5* p = 15.5* 8 - 15.5* 8=9.5* E > 1.0 MeV _ _ BASE CASE
- 2.74340(+ 11)** 4.82786(+ 10) 3.70878(+10) 2.07115(+ 10) 9.87759(+09) 4.49649(+09) 1.87858(+09) 1.18914(+09)
NEGFIX = 1 2.74341(+11) 4.82769(+ 10) 3.70878(+ 10) 2.07116(+ 10) 9.87756(+09) 4.49645(+09) 1.87854(+u9) 1.18908(+09)
, 5 M. 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 .
I MODE 0 - 0.3 2.74782(+11) 4.88035(+10) 3.75722(+ 10) 2.10279(+10) 1.00388(+ 10) 4.57132i+09) 1.90718(+09) 1.19941(+0s
% M. +0.16 +1.09 + 1.31 +1.53 +1.63 +1.60 +1.52 +0.86 -
2 NO.DIR.s = 16 2.77494(+11) 4.90304(+10) 3.77070(+ 10) 2.09948(+ 10) 1.00378(+ 10) 4 57470(+09) 1.91243(+09) 1.19121(+09) I
% M. + 1.15 +1.56 +1.67 +1.37 +1.62 +1.74 + 1.80 +0.17 l EPSPTWISS = 2.74340(+11) 4.82786(+10) 3.70878(+10) 2.07115(+ 10) 9.87760(+09) 4.49649(+09) 1.87858(+09) 1.18914(+ 09) ^
9; ' , 0.0151
$- % mr. 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 } ~
P5 CASE 2.74121(+11) 4.82110(+ 10) 3.71238(+ 10) 2.07133(+ 10) 9.87417(+09) 4.49647(+09) 1.87945(+09) 1.18945(+09) 4 _- 5 M. 0.1 -0.1 + 0.1 0.0 0.0 0.0 +0.1 0.0 sb. g ;;e (f %G: y; , >-
- y. A &
k b' y 1 a p+_ Q.wl[ ym Y . Q >. ! . N ',.
~
y- i y _ a<
i y,
.J n q
=. .
~
- Taide 3.4.1 (Cast'd.)
~
h== leav ity of the DOItT Calculeled Hex to Nummerical Input Par == ans+ '
*a=8==1R Preldeas (r,0) Cam t es== r=2EL25 cum r=215.43 as r=219.393 cua r=224.473 cum r=229.879 cm r=235.2ES am r=248342 cua r=320.06 cm j 8=23* 8=20' 8 = 15.5* 8 = 15.5" 8=15.5* 8 =13.5* 8 = 15.5* 8 - 9.5*
E > 0.l MeV 7.10406(+ 10) 5.07562(+ 10) 3.26105(+ 10) 1.68486(+ 10) 1.18751(+ 10) BASE CASE
- 633036(+11) 9.60304(+10) 8.54595(+ 10)
I I NEGHX = 1 633037(+11) 9.60282(+10) 8.54591(+ 10) 7.10403(+ 10) 5 07555(+ 10) 3.26699(+ 10) 1.68482(+ 10) 1.18746(+ 10) 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
% diK.
MODE 8=03 634654(+11) 9.71702(+ 10) 8.65981(+ 10) 7.20723(+ 10) 5.15099(+ 101 3.31450(+10) 130503(+ 10) 1.19674(+ 10)
+ 0.26 +1.19 +133 +1.45 +1.48 +1.45 +1.20 + 0.78
% diK.
NO.DIR.s = 16 639342(+11) 9.75237(+ 10) 8.69504(+ 10) 7.19877(+ 10) 5.14835(+10) 331332(+10) 130851(+ 10) 1.19170(+ 10) - i
% diK.' +1.00 +1.56 +1.74 +133 +1.43 +1.42 1.40 +035 EPSIrIWISE = 633036(+1I) 9.60304(+10) 8.54595(+10) 7.10408(+ 10) 5.07562(+10) 3.26702(+10) 1.68480(+ 10) 1.18744(+ 10) 0.0001 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
% diK.
s PS CASE 6.32864(+11) 9.59391(+10) 8.55101(+10) 7.10480(+ 10) 5.07512(+ 10) 3.26692(+ 10) 1.61W92(+ 10) 1.18752(+ 10)
~
% dig. 0.0 4.1 + 0.1 0.0 0.0 0.0' O.0 0.0
[ .$ - Q 9J ;) + .'the DORT Numericalarma== are as fogows: NEGFIX is de orgative source fix. MODE is the 8-weighted flux extrapolamon. NO.DGLs is the ===d=* of angular _ - and EPSPTWISE is the flus poima wise convergence.
^
,17 i yj~ i . : S i--
f
@ * : BASE CASE.~ NEGFIX = 0. MODE 8 = 0.0. NO.DIR s = 8. EPSPTWISE = 0.00I
$:h ?
.) L$ i A. " Read as 2.74340x10*" assernes/(cm'-sec).
i$, S -
. L 2p }. ,
n-
+
, n J.j s b: '
; 1 y ;
E G . Table 3.4.2
^
- Semskivity of the DORT Calculated Hex to S, Quadrature PartialIangth M A% (r, z) Cale=a=*ia= (at 0=e*)
i AsialFemk r=282.3 cue r=215.43 cum r=219393 can r=224.473 cui r=229.370 cui r=235.2dB cum r=248.342 cui r=338.06 can I =cee8== = 1 N .3 0 can z=192.062 can z=195.761 cas z=199.459 csm =199.459 can z=283.155 ces =206.856 can z=221.65 can E > 1.0 MeV S8 CASE I.93804E+11 5.62798E+10 2.55168Et t0 1.44130E+ 10 6.94778E+09 3.17615E+09 1.26196E+09 6.84196E +08 ' S16 CASE ' l.94670E+11 5.68005E+ 10 2.59528E + 10 1.45900E + 10 ?.05053E+09 3.22510E+09 1.28726E+09 6.86218E+09
% diff.* +0.4 + 0.9 + 1.7 + I .3 + 1.5 + 1.5 + 2.0 0.3 Azimi Punk r=201.25 cum r=215.43 ees r=219.393 can l r=224.473 cui r=229.379 cia r=235.2dB can r=240.342 cum r=320.e6 cui Incatise z=1N.363 can x=192.062 can z =199.459 cum z=283.155 can ze=203.158 can x=206.356 can z=210.555 cui :=221.65 cui a
E > 0.1 MeV S8 CASE 4.31404E+ 11 1.01910E+ 11 5.87544E+ 10 4.93831E+ 10 3.53358E+10 2.23169E+10 1.07'tm + 10 5.76909E +09 S16 CASE 4.34119E +11 1.02fME+ 1d 5.97682E +10 4.99973E+ 10 3.58176E + 10 2.26348E+10 1.04519E+10 5.79595E +09
% diff.* +0.6 +C.9 + 1.7 + 1.2 + 1.4 + 1.4 +2.2 + 0.5 O
a k i 4-r - h A I
;. ~
r I
45 y ' g;-
? . ?
w -
- p y
{. .. TaNe 3.4.2 (Cont'd.)
.S - Lesleivity of the DORT Calculated Hux to S Quadrature
- Partiallength Shidd Asseenbly (r, z) Calculation (at 8=0*)
1 ' Imwer Weld r=281.25 ces r=215.43 ces r=219.393 can r=224.473 can r=229.879 can r=235.2ER cm r=248.342 cui r=328.96 ces I memel== s=67.145 ces z=67.1948 ces z=67.1948 can z=67.1988 can x=67.It48 :ma z=67.1988 ces z=67.1988 cas =67.1948 ces , E > 1.0 MeV ,
^ 58 CASE 2.93827E+09 1.34748E+09 8.77387E+08 5.41246E+08 2.97191E+08 1.67741E+08 1.22672E+08 2.43208E+08
+
S16 CASE 2.93118E+09 1.35314E+09 4.89447E+08 5.50882E+ 08 3.02727E+08 1.71633E4 08 1.27715E +08 2.48526E +08
% diK.* 0.2 + 0.4 + 1.4 + 1.2 + 1.9 +2.3 +4.1 + 2.2 ,
{7
% E > 0.1 MeV -!
S8 CASE 6.05030E+09 2.27455E+n9 2.34299E+09 2.50280E+09 2.303465+09 2.00939E+09 1.71868E+09 2.43826E+09 S16 CASE 6.07039E+09 2.28721E+09 2.38497E +09 2.54234E+09 2.34933E+09 2.06107E+09 1.79908E+09 2.50080E+09 "h
? l
% diK.* +0.3 + 0.6 + 1.8 + 1.6 + 2.0 +2.6 +4.7 + 2.6 k ~
I* j h-1r
%diff = (516 CASE - 38 CASE) a 100fS$ CASE 4 ** Cmes earesane used in h are frees BUG 12-93 e .
5 L .]
,~ .N -
d - g,> w I i t i
-. -- ,.,---n - - - ,., ,,_ =,n. , = = -. - - - -. -
f 4 DORT BENCHMARK PROBLEM CALCULATION RESULTS 4.1 PWRi Benchmi Problem d) the downcomer and cavity fluxes and dpe rates at the radii of 210.50 s;tn and 320.06 cm, respectively, and Calculation Resas e) the flux spectmm at the pressure vessel peak flux 4.1.1 Calculated Flux, Reaction Rates and location and at the capsule locations. The benchmark solution for the standard code loading, The scalar neutmn flux or fluence rate &(t,E) [n/cm8 sec- the low leakage core loading and the PLSA core are MeV) is the Amdanantal quantity of interest in the giwn in Secums . 4.1.2 4.1 A, rapec6vdy. pressure wesel benchmark calculations. The neutron flux has been =t=w throughout the problem geometry on a doorme spent and ansre d=p=ad==* moh.1 The 4.1.2 Standard Core Leading Benchinark
=l=lan=t Aux is an average over the three dunensional Problesa (Ar, A6, Az) spatial mesh block and is labeled by the _
coordmates of the center of the mesh block. The The calculated > 1 MeV and >0.10 MeV fluxes [n/cm' s] calculated youp-wise solution is an integral over each
~
and dpa rates [dpa/s] for the standard core loading sugy smup. The (r,6,z) solution spatial mesh are given benchmark problem are given in Tables 4.1.2.1 4.1.2.3, in Tables-4.1.1.1 and 4.1.1.2. The energy mesh is given respectively. The Guxes and dpa rates are given for the in Table-4.1.1.3. Both the group wise and energy wssel inner wall and four selected vessel internal
- integreed >l MeV and >0.1 MeV flux solutions are locations, as a Ametion of the azimuthacal (0) location.
provided with the benchmark results. The calculated The flux edit is taken at the axial (z) location where the reaction rates ' for surveillance capsule - dosimeter Gux or dpa rate peak occurs which is soon to increase as materials typically used for measuring the fast neutron - the vessel radial location increases The same data is fluence are included, together with the iron displacement. presented in Tables 4.1.2.4 - 4.1.2.6 for the vessel axial
- per stom reaction rates. The nuclear parameters lor the location of the circumferential weld. The vessel inner-neutron aux monitors are given in Table 4.1.1 A. For wall data at the circumferential weld location will be comparison the dosuneter reactma rates have been used to determine the relative reduction factors of Table-calculated using both the SAILOR (Reference 7) and 4.1.4.3 resulting from the PLSA core loading.
ORNL TM Il476 (Keference 8)- dosimetry cross secuans, as well as the ENDF/B VI donirretry cross The fluxes and dpa rates are presented in Table 4.1.2.7 sechons given in Table 4.1.1.5. In addition to the group- for a location near the conter of the downcomer and in wise flux, the neutma spectrum at the surveillance Table 4.1.2.8 for a cavity location close to the biological capsule locahons and several vessel locahons is also - ahield. These edits are taken at the axial location
. prtmded. corrseponding to the peak of the >1-MeV flux. The r-downmmar Duxes are calculated with the thermal shield The benamd problem calculated results include: capsule included in the model and the vessel capsule -
removed. a) the ari==Aal distribuhon of the E > l-MeV flux, E :
> 0,10 MeV flux and dpa rate at the premure venel ; The neutron Aux spectrum at the >1 MeV peak axial peak 6=eian at the inner wall, T/4, T/2,3T/4 amin =dallaxial location is provided in Table 4.1.2.9 for and oueur surfeos 1==*===
the vessel inner-wall and four selected vessel internal
~
lameia== - 1he five spectra are also given in Figures
- b)f the axial peakL reachon rates of the neuemn 4.1.2.1 - 4.1.2.5.
da===d==s at the espsuls la=*=ng
- The neutron flux spectrum for the thermal shield, c) the'. PLSA core-to-standard core flux and dpa- pressus vessel and cavhy capades at the axial locadon reduchon factors (e.g., PLSA Bux/SCL Rux) at the of the mavimum >1-MeV Gux is provided 'in Table -
lower circumferential weld at O' for the partial length shield ansablycareloadas. . w Khfx$d$hgy * +
- b kk$h* ^
4 hl
- h i s Mg - *
- tJ -
+ ' =MNMWe b b "
a, Mgm J .-. .
. :~
- ~
+ .e#W %#:>
- 4. Benchmark Problem Cahulreion Results 4.1.2.10. Th se spectra are also giver.in Figures 4.1.2.6 locations. The five spectra are also given in Figures
- -4.1.2.8. 4.1.3.14,1.3.5.
- De calculated reaction rates for the dosameter meterials The neutron Dux spectrum for the thermal shield, of Table 4.1.1.4 are given in Tables 4.1.2.11 4.1.2.13 pressure vessel and cavity capsules at the axial location for the thermal shield, pressure vessel anJ cavity of the maximum >l McV Dux is provided in Table capsules, respectively."" The axiallocations correspond 4.1.3.10. These spectra are also ghen in Figures 4.1.3.6 to the peak >l.MeV flux larmelana for each capsule. For - 4.1.3.8.
user convenience, the _ reaction rates have been delarndeed using each of the dnsimeter cross sa: tion sets ne calculated reaction rates for the doHmeter materials given in Table 4.1.1.5 and are provided in the Tables, ofTable 4.1.1.4 are given in Tables 4.1.3.11 4.1.3.13, for the thermal shield, pressure vessel and cavity. capsules, respectively, The axial locations correspond to 4.11 Lew-Leskase Core Losding' the peak >1 MeV finn laratiana ibr each capsule For Benchmark Problem um coannience, the paction utes hass ' ben - determined using each of the dosimeter cross section .eets given in Table 4.1.1.5 and are provided in the Tables. The calculated > 1-MeV and >0.10 MeV fluxes [n/cm' s]
- and dpa rates [dpa/s] for the low leakage core loading hanchmark problem are givoit in Tables 4.1.3.1-4.1.3.3, respectively De finxes and dpa rates are given for the 4.1.4 Partial Length Shield Assembly Core vesset inner wall and four selected vessel internal Leading Benchmark Problem taratiana, as a function of the azimuthal (0) location.
The Bux edit is taken at the axial (z) location where the The calculated >1 MeV and >0.10 MeV fluxes [n/cm s] 3 flux or dpa rate peak oa:urs which is seen to increase as and dpa rates for the partial length shield assembly core the vessel radial location increases The same data is loading benchmark problem are given in Table 4.1.4.1. preaantad in Tables 4.1.3,4 4.1.3.6 for the vessel axial The lluxes and dpa rates are given for the vessel inner-location of the circumferential weld. wall at the lower circumferential weld se a ibaction of the azimuthal (0) location. The same data is also given in The fluxes and dpa rates are presented in Table 4.1.3.7 Figures 4.1.4.1 4.1.4.3. for a location near the center of the downcomer and in Talde 4.1.3.8 for a cavity location close to the biological : The vessel inner wall neutron Bux spectnan at the lower shield. These edits are taken at the axial location circumferential weld is given in Table 4.1.4.2, for the 6 corresponding to the peak of the >l-MeV flux. The = 0' azimuthal location. This spectrum is also given in dowarr==ar fluxes are calculated with the thermal shield Figure 4.1.4.4. . capsule included in the model and the vessel capsule removed. The vessel inner wall flux and dpa reduction factors RF defined, for the Gux, as
- ne' neutron flux spectrum at the >1-MeV peak -
m,1==what/ axial location is provided in Table 4.1.3.9 for RF = PLSA flux /SCL flux , (3) the vessel inner wall and four selected vessel internal - - are pr== entad in Table 4.1.4.3. These RFs are calculanad for the circumferential weld as a - fbaction of the
~
nruninhal lacahan and are based on the SCL results of Section 4.1.2.
' ""It le : A that the desmesters with tiu==handa 7-MeV wose thund to be seasierve to the ausenal esame oesties repe=== man of the penpheral assemblies in the radial eslaulmass. Inessening the ease eteenve radium R,,by ~12
- eat for the SC14LifL) sueuhad la a-30% (5%) reduction in
' these donnester :==ra====
~
Chhl' . IWRBGCR4115 14-2 ~ Q-, gg,ygg % y .& s, s ,. D% , n A W ., . _ , _
. , g ns gw h$$p$
? ys , 9-gr_, W ~-
k e5% N kk d ! N U' k M N $ M y $ JN W N ^4 W A J@ DhMMM@h,gMMMNdd M Td N NNkfdiNn?
- 4. Benchmark Problem Calculation Results l
4.2 - BWR -Benchmark Problem d) the flux spectrum at the pressure vessel peak flux location, cavity peak flux location and at the capsule Calculation Results - ioce e ,. The benchmark solution for the BWR benchmark 4.2.1 Calculated Fulux, Reaction Rates and problem is given in the following section.. , Spectra -
"he scalar neutron flux or fluence rate $(I,E) [n/cm2 - 4.2.2 BWR Benchmark Problem Results sec-MeV) is the ihndamental quantity ofinterest in the pressure vessel benchmark calculations. The neutron Thecalculated>1 MeVand>0.10MeV8uxes[n/cm'-s)
Sax has been' calculated throughout the problem and dpa rates [dpa/s] for the BWR benchmark problem geometry on a discrete spatial and energy dependent are given in Tables 4.2.2.14.2.2.3, a.,,,,thay. The mesh. The calculated Gux is an average over the three Saxes and dpa rates are given foe the vessel inner wall ~ dimanalaani (Ar, 40, Az) spatial mesh block and is and four selected vessel internal locations, as a function labeled by the coordinates of the center of the mesh of the azimuthacal (0) location. The aux edit is taken at block. The calculated group-wise solution is an integral the axial (z) locanon where the flux or dpa rate peak over each energy group. The (r,0,z) solution spatia! . occurs which is seen to generally decrease as the vessel mesh is given in Table 4.2.1.1, and the energy mesh is radial location increases lhe same data is presented in given in Table-4.2.1.2. Both the group wise and energy Tables 4.2.2.4 - 4.2.2.6 for the core axial midplane integrated >1-MeV and >0,1 MeV flux solutions are location. provided with the benchmark results. The calculated
-reaction rates for surveillance capsule dosimeter - The fluxes and dpa rates are presented in Tables 4.2.2.7 materials typically used for measuring the fast neutron and 4.2.28 for a location naar the center of the fluence : are included, together _ with the iron downcomer at the peak axial location and at the core displacen ent-per atom reaction rates. The nuclear axial midplane location, respectrvely, in Table 4.2.2.9, parameters for the neutron flux monitors are given in the corresponding data is presented for the casity at the Table 4.2.1.3. The dosimeter reaction rates were peak axial location close to the biological shield. These calculated using the BUOLE-93 ENDF/B VI dosimetry edits are taken at the axial location corresponding to the
- cross sections given in Table 4.2.1.4. In addition to the peak of the >1-McV flux, group-wiseflux,theneutron.,,eb matthesurveillana _
capsule, cavity and several wssel locations is also The neutron flux .,,m,U-- at the >1 MeV peak provided. nriminhallaxiallocation is presided in Table 4.2.2.10 for ' the vessel inner wall and four selected vessel internal Tbc benchmark problem calenlatal results include: locations. The five spectra are also given in Figures 4.2.2.14.2.2.5. a) 7 the animinhal distribution of the E > l McV Gux, E
> 0.10 MeV flux and dpa rate at the pressure vessel The neutron flux spectrum for the downcomer, pressure axial peak and core midplane locations at the inner- vessel capsule and the casity at the location of the wall, T/4, T/2, 3T/4 and outer surfam ic,:strons, manmum >l-MeV flux is provided in Tr.ble 4.2.2.11, The spectra for the capsule and cavity lara*wis are also b)? the axial peak reaction rates of the neutron given in Figures 4.2.2.6 and 4.2.2.7, respectively.
da=i==a-a at the capsule lar=*iaa, . _ The calculated reaction raess for the dosimeter matenals c) the downcomer and cavity fluxes and dpa rates at - of Table 4.2.1.3 are given in Table 4.2.2.12 for the the radii of 278.1 cm and 398.7 cm, . - , : 4, - pressure vessel capsule.1he axial locations -.v.,,end and to the peak >l-MeV flux lanatiana for the capsule.
~ .- ~
~-
_ f '- 2
^ '-'
&.jM4%pgn - ,
,, ~
gx . - mw ?& un m ~ "
, ,w +fama c
,y.
dW91 NRMd?h R E* -
/
Table 4.1.1.1 Mesh Used in DORT Cal::ulation (Inner Model) R (ca) E(cc) 8(revolution) 1 0.00000 0.00000 0.00000E+00 2 5.00000 4.44500 6.94400E 04 3 10.0000 6.50125 2.08300E 03 4 15.0000 B.55750 4.86100E 03 5 20.0000 10.6138 7.63900E 03 6 2E.0000 12.6700 1.04170E 02 7 30.0000 13.9700 1.31940E 02 8 35.0000 16.2200 1.66670E 02 40.0000- 18.4700 2.01390E 02 9 10 45.0000 20.7200 2.22220E 02 11 50.0000 22.9700 2.50000E-02 12 56.0000 3 25.2200 2.77780E 02 13 60.0000 27.4700 3.05560E 02 14 65.0000 29.7200 3.33330E 02 15 70.0000 31.9700 3.61110E 02 16 75.0000 34.2200 3.88890E 02 17 80.0000 36.4700 4.16670E 02 le 85.0000 38.7200 4.44440E-02 19 90.0000 40.9700 4.68750E 02 20 95.0000 43.2200 4.75690E-02 21 100.000 45.4700 5.00000E 02 22 107.106 47.7200 5.13890E-02 23 114.320 .49.9700 5.35410E 02 24 120.040 52.2200 5.37770E 02 25 124.320 54.4700 5.41760E 02 26 128.610 56.7200 5.51140E 02 27 132.900 58.9700 5.60520E-02 28 137.180 61.2200 5.69900E-02 29 141.470 63.4700 5.73890E-02 30 144.330 65.7500 5.76250E 02 31 147.190 68.4595 5.94720E 02 32 150.040 71.1690 6.11110E-02 33 151.470 73.8785 6.25000E-02 , 34 152.628 76.588'O 6.38890E 02 35 153.687 79.2975 6.52700E-02 36 154.745 82.0070 6.66670E-02 37 155.886 84.7165 6.94440E 02 38 156.944 87.'4260 7.22220E 02 39 158.002 90.1355 7.50000E-02 40 159.063- 92.8450 7.77700E 02 41 160.119 95.5545 8.05560E 02 42 161.177 98.2640 8.29860E-02 m >;; - - ., s s .-g
, . . s , g 4 -
g njip MQ .- I EhANkhff. 6"sM$M , 6 c: 5f- ' -ly di ##h ;- - (:sp (% h,jg M vy! r N-$ N ' < EI ' ' ? O '
Table 4.1.1.1 Mesh Used in DORT Calculation (cont'd) (Inner Model) R (ca) E(ca) 0(revolution) l 43 162.236 100.973 0.36910E 02 44 163.294 103.683 8.611105 02 45 164.352 106.393 8.00990E 02 4J 165.411 109.102 9.131904-02 47 166.469 111.012 9.201405 02 40 166.990 114.521 9.444405 02 49 167.527 117.230 9.72220E 02 50 160.057 119.940 ,. 1.000003 01 51 168.506 123.639 1.0130PE 01
- 52 -169.115 '127.337 1.02770E 01
- 53. 169.644 131.036 1.04861E 01 54 170.173 134.734 1.06944E 01 55 170.702 138.433 1.09028E 01 56 171.232 142.131 1.111115 01 57 171.761 145.830 1.138095 01 58 172.290 149.520 1.159723 01 59 172.019 153.227 1.19750E 01 60 173.340 156.925 1.2C3335 01 61 173.878 160.624 1.229175 01 62 174.407 164.323 1.25000E 01 63 174.936 160.021 64 175.465 171.720 '
65 175.994' 175.418 66 176.523 179.117 67 177.053 182.815 68 177.582 186.514 69 178.111 190.212 70 178.640 193.911 71 -179.169 197.610 72 179.690- 201.308 73 .180.220 205.007
- 74 100.757 208.705 75 101.286 212.404 76 101.015 216.102 77 102.344 219.801 70 182.873 227.499 79 183.403 22?.190 SO 183.932 230.896 81 104.461 234.595 82 184,990 238.294'
'83 105.319 241.992 84 106.570 245.691
&#(qwQLp -
1.m - e s .
.- m - , , ,
4 i
?
31 . i f 7 -1. <.[ ^ l * - 4 2. a s, , a .o s tM Sk) * / ' L 4,t% y ,
, 3 -#p g , 4 _
Tabk 4.1.1.1 i Mesh Used in DORT Calculation (cont'd) (Inner Model) R (ca) E(ca) i 05 187.636 249.389
-86 188.694 253.000 87 109.753 256.706 GB 190.185 260.485 89 190.820 264.183 90 191.455 267.002 91 192.090 271.581 92 192.725 275.279 ,
- 93. 193.360 270.970 94 193.995- 282.676
- 95 194.630 206.375 96 195.268 290.073 97 196.535 293.772 3 98 197.070 297.470 99 199.000 301.169 ~
100 200.34b 304.867 101 200.66J 308.566 102 201.295 312.265 103 201.932 315.963 104 202.568 319.662 105 203.205 323.360 106 203.840 327.059 107 204.155 330.757 100 205.000 334.456 109 '206.000 338.154 110 341.853 111 345.551 112 349.250 113- 350.528 114 352.520 115 355.895
- 116' 359.261 117 362.628 110 365.994 119 367.994 120 369.415
-121 370.715 122 372.715 123 375.840 124 378.982
- 125= 302.115 3 --
i , t y*J - b N -- ' ' _1 _
+) , 4-95 i
'u hi:~ C
~
E+ #b, Y brqQ9p ' +:1 e .1 n,Myor, >
, . s.
4pl;Qj:fy;g gigfM{j[gQffgy-
Table 4.1.1.2 Mesh Used in DORT Calculatica (Outer Model) i R (ca) 5(ca) 0 (revolution) 1 190.185 0.00000 0.00000E+00 2 190 820 4.44500 6.94400E+04 3 191.455 6.50125 2.08300E 03 4 192.090 0.55750 4.86100E*03 i 5 192.725 10.6138 7.63900E*03 l 6 193.360 12.6700 1.04170E*02 7 193.995 13.9700 1.31940E 02 0 194.630 16.2200 1.66670E 02 9 195.250 18.4700 2.013905 03 80 196.535 20.7200 2.22220E*02 1 197.870 22.9700 2.50000E 02 12 199.000 25.1200 2.777005.02 13 200.345 27.4700 3.05560E*02 14 200.660 29.7200 3.33330E 02 35 201.295 31.5700 3.61110E 02 16 201.932 34.2200 3.800903 02 17 202.568 36.4700 4.16670E 02 10 203.205 35.7200 4.444405 02 , 19 203.840 40.9700 4.68750E 02 20 204.155 43.2200 4.75690s 02 21 205.000 45.4700 5.000005 02 22 206.000 47.7200 5.138905 02 23 207.000 49.9700 5.354103 02 24 200.000 52.2200 5.377705 02 25 209.000 54.4700 5.417603 02 26 210.000 56.7200 5.51140E 02 27 211.000 50.9700 5.60520E 02 20 212.000 61.2200 5.69900E.02 29 212.750 63.4700 5.738905 02 30 213.210 65.7500 5.76250E 02 31 213.525 68.4595 5.94720s 02 32 213.845 71.1690 6.111105 02 23 214.470 73.8705 6.25000s.02 34 215.112 76.5000 6.30090E 02 35 215.748 79.2975 6.527003 02 36 216.302 82.0070 6.66670E 02 37 217.015 94.7165 6.94440E.02 38 217.335 87.4260 7.22220E 02 39 217.090 90.1355 7.50000E 02 40 210.440 92.9450 7.777005 02 41 219.075 95.5545 0.05560s.02' 42 219.710 98.2640 8.29860E+02 1 v= F v t k, } f _h'
, , T t ( :
9, 1IlE a+ 1 . ' t ph I k h 553 bI7 t' *#" *
- . _ - - - . . _ . _ - - ~ . - . . - . - - ~ . . . . . _ - - . ~ - - . - - . ~ _ - _ .
l Table 4.1.1.2 ) Nesh Used in DORT Calculation (cont'd)
, (Outer Model)
It (ca) 2(ca) 0(revolution) 43 .20.694 100.973 8.360105 02 44 221.774 103.683 8.611105 02 45 222.053 106.393 0.00890E 02 46 223.933 109.102 9.131905 02 47 225.012 112.812 9.201405 02 40 226.092 114.521 9.44440E 02 49 227.171 117.230 9.72220E 02 50 220.251 119.940 1.000005 01 51 229.330 123.639 1.013895 01 53 230.410 127.337 1.02770E 01 ! 53 231.489 131.036 1.040615 01 54 232.569 134.734 1.069445 01 55 233.640 139.433 1.09020E*01 56 234.720 142.131 1.111115 01 57 215.007 145.830 1.13009E*01 58 236.807 149.520 1.159725 01 - 59 237.966 3t3.227 1.18750E 01 60 239.046 156.925 1.208335*01 61 240.020 160.624 1.22917E*01 62 240.665 164.323 1.25000E+01 63 242.500 168.021 64 245.000 171.720 65 240.000 175.418 66 252.660 179.117 67 257.000 102.015 68 262.500 106.314 69 269.240 190.212 70 279.400 193.911 71 200.000 197.610 72 300.000 201.300
- l 73 315.000 205.007 74 325.120 208.70b 75 330.200 212.404 76 334.010 216.102 77 335.200 219.801 70 335.915 223.499 .
79 336.750 227.198 90 338.000 230.896 el 339.750 234.595 82 341.500 238.294 03 343.250 241.992 e4- 345.000 245.691 l
,,. . n 9. .
h kNhh$bfM4MMKWh F" :0?4# , _ , . , tu , ,
,x . ,
,, . x % , %- 2 .
;g.an%,ggw, . , . ,
e Table 4.1.1.2 Mesh Used in DORT Calculation (cont'd) (outer Model) R (cm) E(cm) 05 346.750 249.309 86 348.500 253.000 87 350.250 256.786 SO 352.000 260.405 09 353.750 264.103
. 90 355.500 267.802
-91 357.250 271.501 92 359.000 275.279 93 361.000- 270.970 94 363.000 202.676 95 365.000 206.375 96 367.000 290.073 97 369.000 293.772 98 371.000 297.470 99 373.000 301.169 100 375.000 304.867 101 377.000 308.566 102 37P.000 312.265 103 301.000 315.963 104 319.662 105 323.360 106 327.059 107 330.757 100 334.456 109 338.154 110 341.853 111 345.551 112 349.250 113 350.528 114 352.520 115 355.895
- 116 359.261 117 362.628 lit 365.994 119 367.994 120 369.415 121 370.715 122 372.715 123 375.048 124 378.982
' 125 382.115 .y g f y- (,. j s y,
e t I i '. +h p_
- j ._
' ' p <: ssp! .r g'-- n qpi ), ; ; ,, ,
- , , rv o
Tabb 4.1,1.3 47*0roup Energy structure of SA1LCR Cross.2ection LLbrary Group Lower anergy Group Lower Energy (Movi (Nov) 1 1 14.19* 26 1.03:10 ' 1 2 12.21 26 1.11a10 2 3 10.00 27 6.76a10 2 4 0.61 20. 4.09:10
*2 5 7.41 29 3.10a10
*2 4 6.07 30 2.61a10"*
*2 7 4.97 31 2.43 10 2
8 3.60 32 2.19:10 3 9 3.01 33 1.50 10 3 10 2.73 34 7.10:10 3 11 2.47 35 3.34s10 3 12 2.37 36 1.59a10 4 . 13 2.35 37 4.54a10 I 4 14 2.23 30 2.14:10 4 15 1.92 39 1.01x10 5 16 1.65 40 3.73a10
. 5 17 1.35 41 1.07:10 6
18 1.00 42 5.04:10 1 5 19 8.21a10 43 1.06:10 . 1 7 20 7.43a10 44 9.76s10 1 7 21 -4.08 10- 45 4.14:10 1 7 22 4.90a10 46 1.0010 1 23 3.69a10 47 0.00 1- ' 24 2.90a10
- The upper energy of group 1 to 17.33 Nov .
, c63 n. e gg m( , ., ,
i ,,,.,p...,_, , . , u ,, .. e - 4 s
,~gg ~g ggQ
)k.M,%jgghk.Ik[fii 14rgyf f : . < ' <
3.q u . c .g ,j. ggg,4jpgggggg, g;g%., . , _
Table 4.1.1.4 Standard Core Loading Nuclear Parameters For Neutron Flus Monitors
. , . Reaction of . + . Product .
. Monitor . Interest . Response Range . Half life .
. .63 60 . . .
. Copper . Cu (n,oD Co . 6.13Mov = E < 11Mov . 5.27 y .
. .54 54 . . .
. Iron . Fe(n p) Mn . 2.47Mov < E < 7.0Mov. 312.2 d .
. .50 58 . . .
. Nickel . Ni(nep) Co . 2.09Mov < I < 7.6Mov. 70.88 d .
. .230 137 . . .
. U 238 . U(n, f) Cs . 1.51Mov < E < 6.7Mov. 30.17 y .
. .237 137 . . .
. Np.237 . Np (n, f) Ca. 0.67Mov < E < 5.7Mev. 30.17 y .
. .27 24 . .
. Aluminium . A1 (n,M Wa . 6.5Nev < E < 12Mov . 14.96 h .
. .32 32 . . 14.28 d .
. Sulfur . S(nep) F . 2.29Mov < E < 7.4Mev. .
. .56 56 . g .
. Iron . Fe (n,p) Mn . 5.44Mov < E < 11Mov . 2.570 h .
. .65 64 . * . .
. Copper . Cu(n.2n) Cu. E > 10.5 Nov . If.70 h .
. .46 46 . . ..
. Titanium . Ti(nep) Sc . 3.86Mov < E < 9.4Mev. 83.81 d .
. .115 115 . . .
. Indium . .In(n,n') In . 1.16Mov < E < 5.9May. 4.486 h .
+ The upper and lower' limits of the energy range are defined such that 95% of-the detector response occurs above the. lower energy and 5% detector response occurs above the upper energy..
- Effective threshold used for proup averaged cross sections .
m; V : .:, . < v; , y , si . Q- gn, w . u. r.a m 3.< o_ y
- a f + O . $_= c ** *
>e .W_ g 3
[~ , .'g ggdghgg. .
-~ _- _ _ _
i
\
l Table 4.1.1.5 Desimeter Activation Cross Sections (EUGLE93) 27 32 46 oroup dpa 4 (n t) s (n.p) T1 (n.p) 1 2.92800E+03 L t *4 80E.01 1.99690s.01 2 2.69300E+03 2.399505 01 1 26s205 01 3.21560E.01 2.664905 01 3 2.45500E+03 1.046005 01 3.81900E.01 2.609208 01 4 2.24500E+03 7.47109E.02 3.40150E.01 2.35990E.01 5 2.09200E+03 3.983605 02 3.17920E.01 2.04500E.01 6 1.97100E*03 9.67520E.03 3.06550E.01 1.54930E.01 7 1.79200E+03 3.574303 04 2.486103 01 9.755605 02 0- 1.60000E+03 3.165505 07 9 2.766705 01 4.002203 02 1.36900E+03 0.P0000E+00 1.062503 01 10 1.26500E+03 5.25430E.03 0.00000E+00 9.96220E.02 4.641905 04 11 1.19000E+03 0.00000E+00 6.07660E.02 6.0$$70E 06 12 1.24600E+03 ' O.00000E+00 7.23790E 02 1.06920E.06 13 1.16600E+03 0.00000E+00 6.64600E 02 - 3.771602 07 14 1.09600E+03 0.00000E+00 6.10960E.02 3.42230E.57 15 1.03600E+03 0.00000E+00 2.12780E.02 2.33440R 07 16 8.19000E+02 0.00000E+00 3.79620E.03 7.94750E 06 17 9.15000E+02 0.00000E+00 5.72e10s.04 8.39500E.10 19 6.32000E+02 0.00000E+00 5.48290E.05 0.00000E+00 19 2.67000E+02 0.00000E+00 1.43450E 07 0.00000E+00 20 5.16000E+02 0.00000E+00 0.00000E+00 0.00000E+06 21 4.00000E+02 0.00000E+00 22 0.00000E+00 0.00000E+00 2.69000E+02 0.00000E+00 0.00000E+00 23- 3.00000E+02 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00 24 2.24000E+02 0.00000E+00 25 0.00000E+00 0.00000E 00 1.78000E+02 0.00000E+00 0.00000E+00 26 1.92000E+02 0.00000E+00 0.00000E+00 0.00000E*00 0.00000E+00 27 1.34000E+02 0.00000E+00 0.00000E+00 0.00000E+00 20 7.54000E+01 0.00000E+00 29 0.00000E+00 0.00000E+00 7.14000E+01 0.00000E+00 0.00000E+00 30 2.94000E+02 0.00000E+00 0.00000E+00 0.00000E+00' O.00000E+00 31 6.00000E+01 0.00000E+00 32 Ov00000E+00 0.00000E+00 3.61000E+00 0.00000E+00 0.00000E+00 33 7.73000E+00 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00 34 1.19000E+01 0.00000E+00 0.000C0E+00 0.00000E+00 35 7.36000E+00 0.00000E+00 34 0.00000E+09 0.00000E+00 3.82000E*00 0.00000E+00 0.00000E+00 0.00000E,00
- 37 1.17000E+00 0.00000E+00 0.00000E+00 0.00000E+00 38 9.300005 02 0.00000E+00 39 0.00000E+00 0.00000E+00 1.360005 01 0.00000E+00 0.00000E+00 40, 2.06000E.01 0.00000E+00-0.00000E+00 0.00000E+00' O.00000E+00 41- 1.100003 01 0.00000E+00 42 0.00000E+00 0.00000E+00 6.090005 01 -0.00000E+00 0.00000E+00 43" 9.25000E.01 0.00000E.00 0.00000E+00 0.00000E+00 0.00000E+00
. 44- 1.47000E+00 0.00000E+00 45 0.00000E+00 0.00000E+00 2.12000E+00 0.00000E+00 0.00000E+00-
' 46 3.30000E+00 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E 00
- 47 7.65000E+00 'O.00000E+00-
*: 0.00000E 0.000COR+00
........................................... ..+00-
- dpa'is from Reference 4 and not from BUCLE-93+
N%%S , . 3, . - - u- i. f+ e,- .
+ sw .a;:w
( - -j 14 yg) V - c-x_= - r ; f n .; CiM i % t%k@ d *
- r
- UN N * ^
4 Table 4.1.1.5 Dosimeter Activation Cross factions (EUGLE93) (cont *d) 54 56 50 63 Group Fe (sep) Fe (n.p) 51 (n.p) Cu (aaW) 1 2.61610E*01 9.079505 02 2.60050E*01 3.54140E+02 3 4.041203 01 1.13440E+01 4.70450B+01 4.33760B+02 , :3 4.696905 01 0.09050E*02 5.923005 01 3.63770E+02 4- 4.932505 01 -5.600705 02 6.23120E+01 2.67930B+02 5 4.023405 01 4.00910E+02 6.25410E+01 1.00500E+02 6 -- '4.70150E+011 2.30500E+02 f 6.040405 01 9.06020E+03 7 4.33950E+01- 5.34250E+03 5.00050E+01 ,3.25320E+03 i
-0 3.12030E+01 11.74960E+04 3.01490E+01 5.750503 04 9- 1.93220B+01- 1.25600E+07 2.44540E+01 4.45250E+05 10 1.326305 01 6.55290E+10 1.710005 01 -0.13620E 06 11- 7.07050E+02 0.00000E+00 1.24950E+01 2.99060B+06 12 5.655205 02 0.00000E+00 9.65570E+02 9.393705 07 13 5.120105 02 0.00000E+00 0.05450B+02 0.17650E 07 14 4.49420E+03 0.00000E+00 7.91190B+02 6.744305 07 15 2.934003 02 0.00000E+00 5.065705 02 2.472603 07 16 0.07320E+03 0.00000E+00 2.702605 02 1.374905 00 17 2.90200E+03 '0.00000E+00- 1.46240E+02 0.00000E+00 10 7.32000E+04 0.00000E+00 5.61440B+03 0.00000E+00 A9 8.694005 05 0.00000E+00 , 1.29440E+03 0.00000E+00 20 6.56090E+06 '0.00000E+00 0.92400E+04 0.00000E+00 2.636105 07 21 0.00000E+00 5.21060E+04 0.00000E+00 22 0.00000E+00 0.00000E+00 1.76550B+04 0.00000E+00 23 0.00000E+00 0.00000B+00 -0.00000B+00 0.00000E+00 24 0.00000B+00 0.00000E+00 0.00003E+00 0.C0000E+00 25- 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00 26 0.00000E+00 0 90000E+03 0.00000E+00 0.00000E+00
- 27. 0.00000E+00 0.d0000E+00 0.00000B+00 0.00000E+00 at 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00
~29 '0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00 30 0.00000E+00 0.00000E+00 0.00000E+00: 0.00000E+00 31' -0.00000B+00' O.00000E+00- 6100000E+00 -0.00000B+00 32 0.00000E+00' O.00000E+00 0.00000E+00- 0.000005600 33 0.00000E+00 .0.00000B+00 0.00000E+00 0.00000E+00 34 .0.00000E+00 0.00000E*00 -0.00000E+00 0.00000E+00 35 0.00000E+00 0.000005+00 0.00000B+00 0.00000B+00
, 36 0.00000B+00 0.00000E+00- 0.00000E+00 0.00000E+00
=37 .0.40000E+00- 0.00000E+00 0.00000E+00 0.00000E+00 30 'O.00000B+00' O.00000E+00' '0.00000E+00 0.00000E+00 30- te.00000E+00- ~0.00000E+00- = 0.00000E+00 ' ' O.000003400-
!40 0.00000E+00- 0.00000B+00- :0.00000B+00- -0.00000E+00 L- .
, 11. 0.000005 00 .0.00000E+00- 0.000005 00 ,0.000005 00 L 142 0.00000E+00 0.0000CE+001 -0.00000E+00 0.00000E+00
"- 0.00000E+00
;43= 0.00000E+001 0.00000E+00; 0.00000E+00:
444 0.00000E+00 0.00000E+00: ,0,00000E+00 -;0.00000E+00
~45' 0.00000E+00 0.00000E+00 0.00000E+00- 0.00000E+00 L .
. :46' O.00000E+00 0.00000B+001 0.00000E+00 0.00000E+00-O@RL
/
t V , ;47- z0.00000E+00 444##p9i@NdewQn; , hMwwi% 9
,.0.00000E+00; -0.00000B+00f :0400000E+001 y W ONMwstWW174W9@o 4
, wpggy%ww-M#M$@?@NW e, st a ' e +dMOSMWA -MtJM-nNWM*nW
, - 1 m W m e e p mM WFM e m
, -/
hNhlkN %h7kiMIN'" $ --4 ;
$MNN[" M N M %N[fNfdN@ NkNh$hbNUM , l
Table 4.1.1.5 Dosimeter Activation Cross Sections (F7GLE31) (cont'd) 65 115 238 237 Group Cu (n,2n) In (n.n') U (n, f) Np (n,f) 1 9.908805 01 6.07760E+02 1.20300E+00 2.20000E+00 2 7.19280E+01 9.42420E*02 1.03450E+00 2.08210E+00 3 1.38520E 01 2.03630E*01 9.84680E*01 2.10550E+00 4 0.00000Ee00 2.70850E+01 9.95010E*01 2.17530E+00 5 0.00000E+00. 2.95180E 01 9.911405 01 2.23870E+00 6 0.00000E+00 3.23850s.01 8.30640E 01 1.95600E+00 7 0.00000E+00 3.312005 01 5.59790E+01 1.49180E+00 0 0.00000E+00 3.15650E+01 5.46370E*01 1.531105600 9 0.00000E+00 3.313305 01 5.25280E 01 1.60980E+00 10 0.00000E+00 3.355305 01 5.23280E 01 1.65070E+00 11 0.00000E+00 3.329905 01 5.32720E*01 1.66340E+00 1 12 0.00000E400 3.23410E*01 5.36910E 01 1.66060E+00 13 0.00000E+00 3.19360E*01 5.37700E+01 1.66980E+00 14 0.00000E+00 3.12010E+01 5.38310E 01 1.68260E+00 - 15 0.00000E+00 2.73260E 01 5.30140E 01 1.68220r+00 16 0.00000E+00 2.09410E 01 4.74430E*01 1.64620E+00 17 0.00000E+00 1.669803 01 3.16460E 01 1.58540E+00 18 0.00000E+00 9.10700E*02 4.08720E*02 1.47170E+00 19 0.00000E+00 4.84140E*02 1.23000E 02 1.33850E+00 20 0.00000E+00 2.50700E*02 3.76100E*03 1.193405 00 21 0.00000E+00 1.247503 02 1.40440E*03 9.21250E*01 22 0.00000E+00 3.863103 03 6.25180E*04 6.14430E*01 23 0.00000E+00 1.746605 03 3.78530E 04 2.63980E*01 24 0.00000E+00 9.51840E+05 1.52050Ea04 9.18460E*01 25 0.00000E+00 0.00000E+00 7.91640E*05 4.62870E.02 26 0.00000E+00 0.00000E+00 1.07100E 04 2.33250E+02 27 -0.00000E+00 0.00000E+00 3.699705 05 1.46710E+02 ' 28 0.00000E+00 0.00000E+00 9.15930E.05 1.18920E*02 29 0.00000E+00 0.00000E+00 2.904205 05 1.068603 02 30 0.00000E+00 0.00000E+00 5.28370E*05 1.01340E 02
- 31. '0.00000E+00 0.00000E+00 2433180E 05 - 9.90910E.03 32 0.00000E400 0.00000E+00 2.53650E 05 9.77C70E 03 33 0.00000E+00 0.00000E+00 1.44660E*04 9.54510E 03 34 0.00000E+00 0.00000E+00 5.26090E 04 9.14010E*03 35 0.00000E+00 0.00000E+00 1.27240E*05 8.80730E.03 36 0.00000E+00 0.00000E+00 5.90660E 09 9.33510E 03 37 0.00000E+00 0.00000E+00 1.033103 03 1.36970E 02 38 0.00000E+00 0.00000E+00 1.150103 05 2.60970E*02 39 0.00000E+00 0.00000E+00 1.705405 05. 3.08330E*02 40 0.00000E+00 0.00000E+00 2.88680E 05 6.26140E.02 41 0.00000B+00 0.00000E+00 1.42830E 04- - 2.468703 02
-42 0.00000E+00 0.00000E+00 7.566705 05 8.151005 03 43 0.00000E+00 0.00000E+00 1.74680E+06' 3.95390E 03 44 0.00000E+00 0.00000E+00 1.84880E*06 1.10250E 02' 45 0.00000E+00 0.00000E+00 2.47760E 05 7.11220E 03
, 46- 0.00000E+00 0.00000E+00- 3.77770E 06 14.98640E 03 4 47 0.00000E+00 0.00000E+00 '7.845403 06? 1.13480E 02-
, emeymdm ae % +
sn , t .mq -.
.g, ,g n ,ry g .g .mg
- > i. .,
I f A 9 ' y 3 x V , g 5 f , rgM p3 J' , W h p W y. s em , , pA j zp dify g dg Qg ;-p
Table 4.1.2.1 Standard core Loading Flus (E=1.0 MEV) At Pressure Vessel s 125.480em 125.400cm 129.186cm 129.186cm 140.282cm 8 0T 1/4 T 1/2 T 3/4 T T 1 3.14799E+10 1.78931E+10 0.69114E+09 4.00968E+09 1. 6's O 67 E
- 09 2 3.14939E+10 1.70948E+10 8.69181E+09 4.01204E+09 1.63590E+09 3 3.15515E+10 1.79309E+10 0.71023E+09 4.01916E+09 1.63546E+09 4 3.10090E+10 .1.807075+10 8.77347E+09 4.04600E+09 1.64438E+09 5 3.22104E+10 1.82947E+10 0.07711E+09 4.09152E+09 1.65943E+09 6 3.27523E+10 1.05911E+10 9.01599E+09 4.15139E+09 1.67925E+09 7 3.346693+10 1.89355E+10 9.20569E+09 4.23439E+09 1.70600E+09 8 3.44603E+10 1.954275+10 9.45942E+09 4.34323E+09 1.741175+09 9 3.54574E+10 2.00747E+10 9.70318E+09 4.44796E+09 1.77511E+09 10 3.63728E+10 2.05806E+10 9.93677E+09 4.54712E+09 1.80693E+09 11- J'.74744E+10 2.11727E+10 1.02041E+10 4.66105E+09 1.84307E+09 12 3.05964E+10 2.17730E+10 1.04749E+10 4.77398E+09 1.87884E+09 13 3.96873E+10 2.23491E+10 1.07300E+10 4.88026E+09 1.91205E+09 14 4.06840E+10 2.20693E+10 1.09581E+10 4.97269E+09 1.94069E+09 15 4.15400E+10 2.33066E+10 1.11436E+10 5.04551E+09 1.96229E+09 16 4.22000E+10 2.36185E+10 1.12659E+10 5.08990E+09 1.W7516R,09 17 4.25965E+10 2.37640E+10 1.13064E+10 5.09949E+09 1.97593E+09 18 4.25005E+10 2.36066E+10 1.12453E+10 5.06920E+09 1.96689E+09 19 4.21634E+10 2.34630E+10 1.11362E+10 5.02312E+09 1.95418E+09 20 4.20061E+10 2.32440E+10 1.10309E+10 4.98065E+09 1.93s13E+09 21 4.11917E+10 2.27246E+10 1.00174E+10 4.90050E+09 1.91354E+09 22 4.02185E+10 2.21933E+10 1.06133E+10 4.82491E+09 1.89446E+o9 23 3.88038E+10 2.17186E+10 1.04642E+10 4.77406E+09 1.88876E+09 24 3.82263E+10 2.15915E+10 1.04226E+10 4.75069E+09 1.88401E+09 25 3.73962E+10 2.12952E+10 1.03327E+10 4.726 0 0E +49 1.86609E+09 26 3.67420E+10 2.09653E+10 1.02152E+10 4.68137E+09 1.05169E+09 127- 3.63552E+10' 2.07451E+10 1.01082E+10 4.63723E+09 1.63997E+09 20- 3.64033E+10 2.06613E+10- 1.00430E+10 0.60702E+09 1.83573E+09 29 3.65714E+10 2.06166E+10 1.00083E+10 4.59093E+09 1.83048E+09 30 3.70498E+10 2.05760E+10 9.92402E+09 4.54562E+09 1.80541E+09 31 3.60078E+10 2.0425BE+10 9.81075E+09 4.48443E+09 1.78065E+09 32 3.62594E+10 2.02359E+10 9.70994E+09 4.43473E+09 1.76407E+09 4
A
..pb 7 44 g g IV Afd v
- N ,
+ s. ,
, ,s . ,i,,,., +, -
. - w- 4 m , g p g q;,_ c 4 s 1+ TV').
<hj h _j f r_M , = g; a y_~g;i _
, j){, .y , ,
d NfNh%(hjM kf'NN b ihF -
*M 3 fp 4 t- M , * *h?QDbGj[Mif j% e
. _ - .. . _. - _ - . - = - _ _ _ _ . . - - . _ . _ . -- _-
Table 4.1.2.1 Standard Core Loading Flux (E31.0 MEV) At treasure vessel (cont'd) s 125.488cm 125.485cm 129.186cm 129.186cm 140.282cm
't 0T' 1/4 T 1/2 T 3/4 T T 33 3.56841E+10 2.00119E+10 9.60770E+09 4.38845E+09 1.74834E+09 34 3.50515E+10 1.97443E+10 9.49650E+09 4.34081E+09 1.73226E+09 35 3.44059E+10 1.94493E+10 9.37791E+09 4 29200E+09 1.71536E+09 36 3.34183E+10 1.89984E+10 9.20303E+09 4.22263E+09 1.69156E+09 37 3.25664E+10 1.85583E+10 9.01527E+09 4.14578t+09 1.66606E+09 38 3.20601M+10 1.02674E+10 8.87729E+09 4.08568E+09 1.64576E409 39 3.18527E+10 1.01151E+10 0.79206E+09 4.04422E+09 1.63026E+09 40 3.18881E+10 1.80834E+10 8.75314E+09 4.01860E+09 1.61088E+09 41 3.20596E+10 1.81229E+10 0.74310E+09 4.00349E*09 1.61190E+09 42 3.21762E+10 1.81522E+10 8.73745E+09 3.99398E+09 1.60844E+09 43 3.22997E+10 1.81744E+10 0.72901E+09 3.983062+09 1.G0099E+09 44 3.24275E+10 1.81670E+10 0.69442E+09 3.95756E+09 1.500SOE+09 45 3.22800E+10 1.80303E+10 8.61449E+09 3.91564E+09 1.57376E+09 46 3.18627E+10 1.78479E+10 0.52620E+09 3.87575E+09 1.56143E+09 47 3.17519E+10 1.77103E+10 8.44757E+09 3.83815E+09 1. 5 4 64 9 E'+ 0 9 48 3.11006E+10 1.73353E+10 8.26056E+09 3.75861E+09 1.51796E+03 49 3.00742E+10 1.60012E+10 0.02813E+09 3.65574E+09 1.48481E+09 50 2.90423E+10 1.629475+10 7.80654E+09 3.56252E+09 1.45554E+09 51 2.83755E+10 1.59367E+10 7.64313E+09 3.49306E+09 1.43270Et09 52 2.75587E+10 1.54926E+10 7.44140E+09 3.40697E*09 1.40336E+03 53 2.640175+10 1.49294E+10 7.19011E+09 3,30096E+09 1.368G6E+09 54 2.536195+10 1.43443E+10 6.93103E+09 3.19288E+09 1.33392E+09 55 2.42393E+10 1.37501E+10 6.67180E+09 3.09487E+09 1.29944E+09 56 2.29862E+10 1.31122E+10 6.38859E+09 2.96794E+09 1.26188E+09
, 57 2.19661E+10' 1.25603E+10 6.14181E+09 2.86499E+09 1.22943E+09 58 2.10252E+10' 1.20735E+10 5.92692E+09- 2.77596E+09 1.20064E+09 59 2.04426E+10 1.17442E+10- 5.77594E+09 2.71222E+09 1.18071E+09
. 60 -2.00603E+10 1.15420E+10 5.68379E+09 2.67354E+09 1.16813E+09 61 1.98790E+10 1.14396E+10 5.63730E+09 2.65300E+09 1.16185E+09
.v, - a ;
* ' -' \' f^ # E '" .f h , ?-. ' f- j A
5
.l [ ,
! ^f' 5 % _
y .t - -. ogfyg g g g y.ggg g p m g 9R 1 4
,9 3 - ;ff pqp dv. gW pdFrA .m
f Table 4.1.2.2 Standard Core Londing j i Fluz (E>0.1 May) At Pressure Vessel a 125.400cm 129.106cm 132.005cm 140.202cm 162.474cm 0 0T 1/4 7 1/2 T 3/4 T T 1 7.20410E+10 6.21982E+10 4.52033E+10 2.910063+10 1.40176E+10 2 7.20005E+10-- 6.22313E+10 4.53040E+10 2.91970E+10 1.39967E+10 3 7.30665E+10 6.24103E+10 4.54201E+10 2.92636E+10 1.39959E+10 4 7.36611E+10 6.20935E+10 4.57407E+10 2.94435E+10 1.405375+10 5 7.46130E+10 6.36510E+10 4.62541E+10 2.97305E+10 1.41500E+10 6 7.50764E+10 6.46632E+10 4.69303E+10 3.01121E+10 1.42744E+10 7 7.75947E+10 6.60499E+10 4.70559E+10 3.06333E+10 1.443975+10 0 7.99122E+10 6.70797R+10 4.90610E+10 3.13046E+10 1.46527E+10 9 0.21982E+10 6.96247E+10 5.01974E+10 3.19367E+10 1.40555E+10 10 0.43711E+10 7.13121E+10 5.129465+10 3.25410E+10 1.50467E+10 11 0.69307E+10 7.32503E+10 5.25412E+10 3.32270E+10 1.52606E,10 12 0.95420E+10 7.52202E+10 5.37077E+10 3.39031E+10 1.54725E+10 - 13 9.20020E+10 7.70904E+10 5.49640E+10 3.45375E+10 1.56693E+10 14 9.44203E+10 7.07976E+10 5.601275+10 3.50960E+10 *1.58406E+10 15 9.64313B+10 0.022775+10 5.50746E+10 3.55449E+10 1.59753E+10 ' 16 9.79835E+10 0.12714E+10 5.74001E+10 3.50499E+10 1.60646t+10 17 9.09511E+10 0.19442E+10 5.77752E+10 3.59065E+10 1.60947E+10
..10 9.914365+10 G.19592E+10 5.77209E+10 3. 59 3 8 5 r.+10 1.60624E+10 !
19 9.06822E+10 0.15371E+10 5.74971E+10 3.30115E+10 1.60510E+10
- 20 9.04400E+10 0.10906E+10 5.71075E+10 3.56443E+10 1.590565+10 21 9.74095E+10 0.01506E+10 5.66104E+10 3.53451E+10 1.507265+10 9.63065B+10 7.90716E+10 5.59722E+10 3.50055E+10 1.57931E+10
. 22 23 ~ 9.47901E+10' 7.01654E+10 . 5.54007E+10 3.47522E+10 1.57011E+10 24 p.42130E+10 7.70701E+10 5.53140E+10 3.46670E+10 1.57511R+10 25 9.33731E+10 7.725073+10' 5.49700E+10 ' 3.44913E+10 1.56547E+10 26 9.23160E+10 7.64440E+10 5.45007E+10 3.42406E+10 1.55553E+10 27' 9.114573+10 7.56013E+10 5.40363d+10 3.39067E+10 1.54099E*10
- 20. 3.03402E+10 7.51700E+10 5.36943E+10 3.37974E+10 1.54654E+10 l 29 9.00590E+10 7.49149E+10 5.35160E+10 3.36973E+10 1.54319E+10
- 30 4.94794E+10 7.42427E+10 5.30312E+10 3.34214E+10 1.52719E+10
, 31 0.75027E+10. 7.30066E+10 5.22060E+10 3.29555E+10 1.50935E+10 l l 47 jh A s 1 . , 3, . t s. , , . . . ;
- b '
N f R - k -
^
$ 4 m 1 M .p -
i 76*i . N8f NII.M 51'bh b N 9IN*[%* ~ *
' N N h i U'N 'l kN! h I'M N f 4 *'
,th l
YQ pV j )' . .i L Q _ , . l , s - - ,
~ N 35&' .. -~ ~ ++~m a h W9 6G(l6-- \00 yhhhykh
- Ws%2*iN) % , 1 -- gl- k/ 7 ' ': V< m hln- (1)l% f }*ygQyQ.yf y -h;
~ ., - - - . , - --. --- , . . ..- - ~ . -
. . ..2 . - .
Table 4.1.2.2 Standard Core 1.osding Flus (E>0.1. alev) ' At : Pressure Vessel - (cont'd). s- 125.400am _ 129.106am 132. 005 es . 140.202em 162.474cm 0 0T 1/4 T 1/2 T 3/4 T T 32 .0.56464E+10 7.19420B+10 5.14634E+10 3.25402E+10 1.49675E+10-33 0.393075+10 7.07202E+10 5.07601E+10 3.21531E+10 1.40426t+10 34 0.225673+10 6.95934E+10 5.007775+10 3.17723E+10- 1.47160E+10 35 0.043265+10- 6.04715E+10 4.939665+10 3.14011E+10 1.450575+10 36 -7.04725E+10 6.49094E+10 4.050193+10 3.09112E+10 1.44115E+10 37 .7.64705E+10 6.54450E+10' 4.752065+10 3.03604E+10' 1.42241E+10 30 7.521475+10 6.43021E+10 4.675465+10- 2.99072E+10 1.40690E+10 39 7.461415+10 6.37040B+10 4.62042E+10 2.95553E+1C' 1.39304E+10 40 7 4i5763+10 6.337315+10 4.50352E+10 2.92072E+1C 1.30290E+10 41 .7.40192E+10 6.32593E+10 4.55930E+10 '2.90035E+10 1.37526E+10 42 7.503675+10~ 6.321065+10 4.54564E+10 2.09624E+10 1.37153E+10
- 43. 7.52560E+10 6.31725E+10 4.53142E+10 2.00360E+10- 1.36440E*10 44 7.54531E+10 8.29092E+10 14.50231E+10 2.06065E+10 1.353945&10
-45 7.51745E+10 6.25220E+30 -4.459073+10 2.03105E+10 1.34303E+10 46 7.452565+10- 6.20101E+10 4.42120E+10 2.00735E+10 .1.13661E+10 47- 7.409975+10 6.147465+10 4.37911E+10 2.70130E+10 1.32503E610 40 .7.26630E+10 6.02641E+10 4.294575+10 - 2.73140E+10 1.30735E+10 49- 7.04374E+10 5.057245,10 4.10301E+10 2.660515+10 1.20675E+10
'50 6.024415+10 5.700375+10 4.003075+10 2.61276E+10 1.24931E+10 St. 6.643773+10 :5.57971E+10 4.005975+10 2.56953E+10 1.25494E+10 52 - - 6.4639 63+10 5.42043E+10 3.90913E+10: 2.515065+10 1.23630E+10 531: 6.211195+10 L 5.24200E+10 - 3.79124E+10- 2.45094E+10 1.21485E+10-54 -5.94916E+10 -5.05040E+10 -3.67100E+10 2.30535E+10 1.193773+10-55,c5.607295+10 4.04011E+10 3.55210E+10 2.32071E+10 1.17295E+10
== _ 56L15.40304E+10- 4.65561E+10 3.42530E+10. 2.25211E+10: 1.150765+10 57 L5.16124E+10 4.47535E+10 3.312575+10. 2.190975+10 :1.13142E+10; s d5 50 94;9494'4E+10 ; 4.322603410 " 3;217675+10' ' 2.139663+1051'.11471E+10 -
, an 59;ci4.009'40E+10 u4.21135E+10 o 3.14690E+10 n 2.10120B+10 n 1 10271010 ,
~ " 40 M 4;M664E+10 C 4.14401E+10' - 3.104763+10L 2.07026E410H 1.09524E+10 " ' ~
61 4. '4719 4E+10 ' ' 4.11122E+10 - 3.00350E+10: 2.06665E+10 1.09151E+10
>y r
~
+~' -f ^ J 'f -
4 3L:... =au . , h --[ ' 4 g 4 4 )' 'y ,h '[y f8F4[ j thy f ( b T5 d_
. - . .' f ,,
r 7 ., ' ,
-.'T -
M k , .
.u <
r . . -
< h - a si *
*l$5&h 4* ,4_ -
u .wg , Q . _ If ,
@ % d 5 & &s h % , WJ t t? -ww - - w m;wQQgyyggqig.ygf&QQkyw u
,7 ,__7.,. .. ... _m
; ; u,. , ,
- m. - -~
s Table 4.1.2.3 Standard Core Loading DPA Este At Pressure Vessel a 125.400em 129.196cm 132.005cm 136.504em 150.77Sem
-0 ' O.T 1/4 7 1/2 T 3/4 T T '
l i
, i1 4.076423 11--2.it???Ba11 1.905275311=-1.00096E*11' 5.031178 12~
-2 4.07791E+11 3.170573 111=1.905045 11 1.00955E+11. 5.01373E+12-3 4.00673E+11 3.195075+11' -1.910425*11 1.091038*11 5.01329E*12 ,
4 4.925005 11 3.210225 11 1.923095 11 1.090645 11 5.035243 12 l 5 4.907615 11~ 3.240735 11 1.945305 11 1.109675+11 5.071928 12
- 6. 5.060545*11' 3.29972E+11 1.974125 11 1.124303 11 5.11961E.12 ,
7 5.176035+11 3.36921E*11 2.01331E*11 1.14433E*11 5.193295 12 0 5.326105 11 3.46223E 11 2.064965 11 1.170315 11 5.26576E 12 ' 9 5.475313 11 3.55201E+11 2.1140GE*11 1.19495E*11 5.34471E*12 10 5.61310E+11 3.637633 11 2.16120E 11. 1.21040E+11 5.41009E*12 11 .5.770023*11 3.73731E+11- 2.214975 11 1.245325 11 5.502293 12 12 5.945723*11 3.037075 11 2.260923 11 1.27149E*11 5.50401E 12 13 6.100225 11 3.93400E*11 2.319793 11 1.296235+11 5.661275 12 , 14 6.256673+11' 4.020773 11 2.365015 11 1.31700E 11 $.727515 12
, il 6.303605 11 4.093473 11- 2.401943 11 1.335135 11 5.770575 12
- 16 6.400973 11 4.14573E.11 2.42713E+11 1.34637E 11 5.011045 12
- 17 6.539425 11 4.171753 11~ 2.437545 11 1.350475+11 5.010423-32 it '6.539723*11' 4.163025 11 -2.430395 11. 1.34653E 11 5.0060CE+12
- 13 6.403535 11 4.133425 11. 2.41465E+11 1.339215 11 5.70759E 12 20- 6.463375 11 4'10309t . ;1 2,397775 11 1.33140E+11 5.75003E 12
- 21. 6.35107E+11 4.030133 11 2.364005 11 1.316055*11 5.707442 12 22- 6.220973 11' 3'.953615 11 2.32979E 11 1.30102E 11 5.67123E*12
- 23^ 6.027225=11 3.004623 11 2.30420E+11 1.29120E+11 5.663645 12
- 24 5.945143 11 3.065775+11 ~2.296663 11 1.207023 11 5.652005 12
' 255 5.025095+11' 3.020943 11' 2.20030E*11 '1.20070E 11: 5.614763 12 261 5.73072E+11 3.769273 11' 2.25043E.11 1.27069E+11 5.57632E 12
, ;27 .5.671055 11 3.731575 11 2.237355 11- 1.26057E 11 5.55011E 12 20i 5.675773 11 -3.714293 11 2.223425 11.- 1.25331E+11- 5.540265 12'
'29 5.696193+11- 3.704745 11. 2.215965 11 1.242463+11 -5.52720E+12
_30_l5.755015+11: 3.690265 11 2.19732E+11 L1.230625 11 5.466353 12 31 5.704125 11- 3.652775 11.x2.16062L 11; 1.222095+11 5.401678 12-4: , _
's u 4 m % ,
) F
- >-dyg g d < ; & _
%&p tw 8 * *
; . :;z [3 'V-] W % y
. N M M & B t W e e W M e q C e M W W W m e e M @
- W Mr MMt*WH@N" ,Q "e
~
. {_ .[ g . s , ~ v.
M eQ429p ihdddb:- mg p i + 1 - x + mvr. a(VT*Swe - tY $M.j-i*m ,%ytykfw eWM
.;;L , , khMI Mahf4[$sAhhdNNN%iN h
- E 9 @ _44Id $ d 6 s-; h N D T N758 N b-; M dI h k NfN3 M Y N "
._.._. _ _ . ~ . . - . - ..- _ _. _ ~_ _ _ . _ _ _ _ . . _ , - . _ _ _ _ . _ _ _ . _ - . _ . _ _ _ . _ , _ _ . . _ - -
l l l 1 i Table 4.1.2.3 i Standard Core Loading DPA Este At Pressure Vessel (cont'd) s; 125.400am 129.106am' 132.005cm 136.504cm ^150.775cm : 0- 0*T 1/4 T 1/2 T 3/4 T T-f 32- 5.61350E+11 3.610795+11 2.142598+11 1.20700E+11 5.35609E+12 , 33 5.520325 11- 3.565475 11 2.117243 11 1.19439E 11 5.31329E.12 34 5.421535 11 3.01507E 11 2.09090s 11 1.10096E 11 5.260593+12 35 5.322643+11 3.462005 11 2.06401E+11 1.16759E+11 5.222213 32 36 5.17570E+11 3.305165 11 2.02667E 11 '1.14944E+11 5.150013 12 37 5.046043 11 3.30045E.11 1.905973+11 1.12904E+11 5.09023E 12 30 4.96701E+11 3.25547E 11 1.954735 11 1.11244E+11 5.03300E*12 39 4.93221E+11 3.22450E+11 1.933253 11 1.09907E+11 4.90731E 12 40 4.93173E+11 3.21242E*11 1.92015E 11 1.09072L 1L 4.949352 12 41 4.951395 11 3.21101E+11 1.912613 11 1.00400E 11 4.023173 12 42 4.965425 11 3.21229E 11' 1.90010E+11 .1.079925 11 4.90996E 12 43 4.900025 11 3.212113 11 1.903453 11 1.075625 11 4.805435 12 44 4.99290E+11 3.205005 11 1.09239E 11 1.06736E.11 4.04728E.12 45- 4.96740E+11 3.17970E+11 1.073765 11' 1.05601E 11 4.000J0E+12-46 4.905993+*1 3.14766E+11 - 1.05590E+11 1.04643E+11 4.77875E 12 47 4.005163+11- 3.12207E+11- 1.030465 11 -1.03659E 11 4.73000E*12 40 4.70500B+11 3.05771E+11 1.00152E+11 1.01720E.11 4.66001E.12 49 4.61161E+11- 2.967073 11 1.753013+11 9.92603E 12 4~.500245 12 p 50 _4.4'19375 11 2.00300E+11 1.700965 11 9.70734E+12 4.51975E 12 t 51 54.370265+11 2.W2291E+11 1.675695 11 9.540475 12 4.46403E+12 52 4.25340s 11 2.747123 11 1.63449E*11 9.33402E 12 4.39303E.12 53- 4.091895 11 2.65219E+11 1.50391E+11- 9.00277E+12 4.31144E+12 i 54 3.924005 11 2.554365+11 1.532113 11 0.02050E 12 4.23002E+12 55' 3.757975 11 2.456025 11 1.400735 11 0.57667E 12 4.14943E.12 L '_56 3.572635 11 - 2.35027E+11 1.425195 11 0.307465 12 4.06296E.12
- 57 ;3.420045 11 2.25040E.11- 1.37642E+11. 0.060035 12 =3.90701E+12 l . 50 '3.201685 11 2.170243 11 1.334553 11'-7.06603E+12 '3.922273+12'
- 59;l3.19432E+11' 2.12273E 111.1.304335 11 7 7.71609E;12__3.07507E+12;
' 60 3;130325 11 2.000093 11; 1.206053 11 7.62730E+12'~3.046915 12 -
61_.-3.11003E+11;-2.07175E+11._1.276045 11: 7.50101E+12: ,3. 83 234E ?l2_-- g
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i TsWe 4,1.2.4 ; I Standard Core Loading l Flus (E>1.0 MEV) At Pressure vessel Lower Wold l (s 67.1040es)- 6 3/4 T T 0 0*T , -1/4 T 1/2 T / 1* i 1 2.701065+10 1. 53 0475+1'O 7.40090E+09 3.40212E+09 1.37703E+09 ! 2 2.702375+10 1.53062E+10 7.409463+09 3.40413E+09 1.37470E+09 3 2.70722E+10 1.53371E+10 7.425175+09 3.410165+09 1.37433E+09 4 2.72932E+10- 1.545675+10 7.47900E+09 3.43301E+09 1.30103E+09 5~ 2.76444E+10 1.56403E+10 7.56744E+09 3.471565+09 1.394475+09 6 2.010295+10 1.590195+10 7.60504E+09 3.522365+09 .1.41113E+09 7 2.01163E+10 1.62470E+10 7.047575+09 3.59279E+09 1.43360E+09 8 2.95690E+10 1.67160E+10- 0.06300E+09 3.60514B+09 1.46317t+09 9 3.042495+10 1.71711E+10 0.27170E+09 3.77401E+09 1.49169E+09 10 3.121075+10 1.760395+10 9.47005E+09 3.05015E+09 1.51042E+09 11 3.21563E+10 1.01104E+10 0.69870E+09 3.95402E+09 1.54000E+09 4 12 .3.31195E+10 1.06240B+10 0.92960B+09 4.05064E*09 1.57006E+09 il 3.40559E+10 1.911693+10 9.14701E+09 4.140W4E+09 1.60677E+09 14 3.49123E+10 1.95620B+10 9.34163E+09 4.21925E+09. 1.63003E+09 ; 15' 3.56472E+10 .1.99362E+10- 9.49970E+09' 4.20104E+09 1.C4090E+09 + 16 3.62132E+10 2.02030E+10 9.60402E+09 4.31070E+G9 1.699795+09 17 3.655375+10 2.03275E+10 9.630595+09 4.32604E+09 1.66043t+09
'10 3.65402E+10' 2.02614E+10 9.50645E+09 4.30120E+09 1.65202E+09-19 -3.61025B+10. 2.007015+10' 9.49345E+09 4.26202E+09 1.64213E+09 20 3.60475E+10 1.90020E+10 9.403665+09 1.225975+09 1.62947E+09 21 3.53490E+10 1 94305E+10 9.22160E+09 4.15794E+09 1.60796E+09 22 3.45140B+10 1.09040E+10 9.04761E+09- 4.093795609 1.59191E+09 4.05063E+09_ 1.50712E+09 1231-3.330075+10
' 24 0 3.200573+10 1.04692E+10 1.057793+10. 0.920495+09 . 4.037595+09' 1'50313B+09
.0.005015+09 . i 25 3.20941E+10: 1.021.SE+10 0.000305409- 4.00905E+09 1.56975E,09 l
26 3.153295+10 .1.793363+10 0.700165+09 3.97190E+09 1.555975+09 . s 27 - 3.120065+10 - 1.77452E+10 0.617015+09. 3.93453E+09. 1.54612E+09 20 3.12411E+10 1.76735E+10 0.56130E+09 3.900095+09 1.542568+09 its: 3.130495+10 1.76353E410 0.53170E+09- 3.09524E+09 1.53015E+09
'30-:3.17941E+10 1.76004E+10 0.46064B+09.;3.05679E+09._ 1.517075+09 i #31143.150575+10 1.74710E>10; 0.36340E+09 3.00400E+09; 1.49620E+09.-
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Table 4.1.2,4 Standard Core Loading Flux (E>1.0 MEV) At Pressure Vessel Lower Wald (cont'd) (s=67.1048cm) 0 0T 1/4 T 1/2 T 3/4 T T 32 3.11147E+10 1.73093E+10 8.27746E+09 3.76273E+09 1.48435E+09 33 3.062075+10 1.711765+10 0.19031E+09 3.72347E*09 1.46914E+09 ' 34- 3.00777E+10 1.68887E+10 0.09551E+09 3.68306E+09 1.45563E+09 35 2.95235E+10 1.66363E+10 7.99442E+09 3.64164E+09 1.44144E+09 36 2.867 DOE +10 1.62506E+10 7.84532E+09 3.58279E+09 1.42144E+09 4 37 2.7944'1 10 1.58741E+10 7.68525E+09 3.51758E+09 1.39997E+09 30 2.75101E+10 1.56253E+10 7.56763E+09 3.46659E*09 1.38296E+09 39 2.73322E+10 1.54950E+10 7.49499E+09 3.43142E+09 1.36994E+09 - 40 2.73627E+10 1.54679E+10 7.46182E+09 3.40969E+09 1.36037E+09 41 2.75101E+10 1.55018E+10 7.45329E+09 3.39687E+09 1.35451E+09 42 2.76104E+10 1.55269E+10 7.44840E+09 3.388voE+09 1.35160E+09 43 2.77165E+10 1.55459E+10 7. 4413 0 E+ 09 3.37954E+09 1.34534E409 44 2.78265E+10 1.55397E+10 7.41183E+09 3.35791E+09 1.33484E+09 45 2.77002E+10 1.54297E+10 7.34371E+09 3.32234E+09 1.32244E+09 46 2.73425E+10 1.52669E+10 7.26945E+09 3.28849E+0s 1.31208E+09 47 2.72474E+10 1.51492E+10 7.20142E+09 3.25659E+09 1.29952E+09 48 2.66006E+10 1.48284E+10 7.04881E+09 3.18910E+09 1.27555E+09 49 2.500784+10 1.43715E+10 6.84384E+09 3.10181E+09 1.24769E+09 50 2.49222E+10 1.39302E+10 6.65492E+09 3.02271M+0p 1.22309E+09 51 2,43498E+10 1.36320E410 6.51561E+09 2.96377E+09 1.20389E 09 52 2.36487E+10 1.32520E+10 6.34370E+09 2.89073E+09 1.17924E+09 53 2.27241E+10 1.27702E+10 6.12940E+09 2.00078E+09 1.15009E+09 54 2.17628E+10 1.22697E+10 5.30851E+09 2.70907E+09 ' 1.12090E+09 55 2.07991E+10 1.17681E+10 5.68750E+09 2.61742E+09 1.09132E+09 56 1.97233E+10 1.12155E+10 5.44603E+09 2.51820E+09 1.06035E+09 57 1.88476E+10 1.07433E+10 5.23563E+09 2.43084E+09 1.03309E*09 58 1.80399E+10 1.03268E+10 5.05243E+09 2.35530E+09 1.00889E+09 59 1.75397E+10 1.00451E+10 4.92370E+09 2.30122E+09 9.92144E+08 60 1.72183E+10 9.87210E+09 4.84514E+09 2.26839E+09 9.81573E+08
- El 1.70558E+10 9.78452E+09 4.80550E+09 2.25171E+09 9.76293E+08
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Table 4.1.2.5 Standard Core Loading Flux (E> 0.1MEV) At Pressure Vessel Lower Wald
, (s=67.1049es) j 8 0T 1/4 7 1/2 T 3/4-T T 1 6.22826E+10 5.27904E+10 3.81521E+10 2.43557E+10 1.14706E+10 2 6.23225E+10 5.28185E+10 3.51703E+10 2.43694E+10 1.14535E+10 3 6.24740E+10 5.29703E+10- 3.82741E+10 2.44250E+10 -1.14528F+10 4 4.29832E+10 5.33005E+10 3.05442E+10 2.45752E+10 1.15002E+10 5 f.37973E+10 5.40242E+10 3.89703E+10 2.48150E+10 1.15794E+10
$ 6.48777E+10 5.48829E*10 3.95403E+10 2.51330E+10 1.168165+10 7 6.63471E+10 5.60602E+10 4.03205E+10 2.55694E+10 1.18175E+10 8 6.832915+10 5.76'.J7E+10 4.13365E+10 2.61304E+10 1.19925E+10 9 7.02O42E+10 5.)0954E+10 4.22947E+10 2.66587E+10 1.21593E+10 10 7.21425E+10 6.05282E+10 4.32197E+10 2.71637E+10 1.23164E+10 11 7.43316E+10 6.21807E+10 4.42700E+10 2.77370E+10 1.24923E+10 12 7.65649E+10 6.38467E+10 4.53218E+10 2.83021E+10 1.26665E+10 13 7.07301E+10 6.54416E+10 4.63136E+10 2.OO324E+10 1.28203E+10 14 0.07373E+10 6.68045E+10 4.719798+10 2.92992E+10 1.29692E+10 15 8.24573E+10 6.00909E+10 4.79246E+10 -2.*6743E+10 1.30798E+10 16 8.37850E+10 6.89551E+10 4.84350E+10 2.99291E+10 1.31532E+10 17 8.46125E+10 6.94711E+10 4.IE034E+10 3.00430E+10 1.31778E+10 le 0.47767E+10 6.94830E+10 4.86369E+10 3.00023E+10 1.31675E+10 19 8.43811E+10 6.92002E+10 4.84472E+10 2.)S956E+10 1.31420E+10 20 8.41741E+10 6,88280E+10 4.81855E+10 2.9755CE+10 1.30875E+10 '
21 '8.33506E+10 6.80341E+10 4.77043E+10 2.95049E+10 1.29945E+10 22 8.23442E+10 6.71009E+10 4.71585E+10 2.92206E+10 1.29290E+10 23 8.10439E+10 6.63375E+10 4.67434E+10 2.50086E+10 1.29189E+10 24 8.05490E+10 6.60064E+10 4.66035E+10 2.89374E+10 1.2R942E+10 25 7.98343E+10 6.55661E+10 4.63199E+10 2. 879 05 E +'10 1.28150E+10 26 7.89243E+10 6.487365+10 4.59232E+10 2.8580DE+10 1.27333E+10 27'.7.79238E+10 6.42261E+10 4.55249E+10 2.83687E+10 1.26796E+10 29 7.72430E+10 6.37933E+10 4.52366E+10- 2.82105E+10 1.26594E+10
-29 7.69969E+10 6.35764E+10 4.50870E+10 2.81268E+10 1.263195+10 30 7.65040E+10 6.30071E+10 4.467795+10- 2.78963E+10 1.25006E+10 31 7.48847E+10 6.19597E+10 4.39537E+10 2.75072E+10 1.23542E+10 j g t 1 g>
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i l 1 Table 4.1.2.5 Standard Core Loading Flux (E> 0.1MEV) At Pressure Vessel Lower Wald (cont'd) (s=67.1048ca) 0 0+T 1/4 7 1/2 T 3/4 T T l 32 7.32302E+10 6.09725E+10 4.33577E+10 2.71605E+10 1.22507E+10 ) 33 7.177073+10. 6.00200E+10 4.27723E+10 .2.60374E+10 1.21483E+10 34 7.033265+10 5.90653E+10 4.219075+10 2.65195E+10 1.20444E+10 35 6.09440E+10 5.01132E+10 4.16170E+10 2.62096E+10 1.19375E+10 36 6.70963E+10 5.68540E+10 4.08630E+10 2.5000$E+10 1.17945E+10 37 6.53943E+10 5.55609Ee10 4.00361E+10 2.53406E+10 1.16400E+10 38 6.43107E+10 5.46420E+10 3.93900E+10 2.49623E+10 1.151365+10 39 6.37975E+10 5.40670E+10 3.09274E+10 2.46686E+10 1.14065E+10 40 6.37499E+10 5.37071E+10 3.86172E+10 2.44451E+10 1.13170E+30 41 6.39743E+10 5.36914E+10 3.84144E+10 2.42754E+10 1.12544E+10 42 6.41607E+10 5.36575E+10 3.02991E,13 2.41745E+10 1.12239E+10 43 6.43487E+10 5.36190E+10 3.81797Ii+10 2.40693E+10 1.11662E+10 44 6.45179E+10 5.34641E+10 3.793495+10 2.38778E+10 1.10799E+10 45 6.42000E+10 5.30606E+10 3.75707E+10 2.36307E+10 1.09969E+10 46 6.37247E+10 5.26333E+10 3.72521E+10 2.34328E+13 1.09376E+10 47 6.33609E+10 5.217875+10 3.69968E+10 2.32152E+10 1.00491E+10 48 6.21315E+10 5.11510E+10- 3.61842E+10 2.27990E+10 1.06974E+10 i 49 6.02280E+10 4.97144E+10 3 $2503E+10 2.22728E+10 1.05202E+10 50 5.83543E+10 4.83021E+10 1 44076E+10 2.18069E+10 1.0384eE,10 51 5.69700E+10 4.73576E+10 A.37509E+10 2.14456E+10 1.02668Et10 52 5.52703E+10 4.60732E+10 3.29345E+10 2.09971E+10 1.01136E+10 53 5.31085E+10 4.44910E+10 3.19406E+10 2.04546E+10 9.93734E+09 54 5.00674E+10 4.28632E+10 3.09267E+10 1.39064E+10 9.76416E+09 55 4.86276E+10 4.12474E+10 2.99240E+10 1.93662E+10 9.59302E+09 56 _4.61963E+10 3.95106E.10 2.88549E+10 1.87927E+10 9.41060E+09 57 4.41202E+10 3.79790E+10 2.79043E+10 1.82017E+10 9.25162E+09 50 ~ 4.23165E+10 3.66832E+10 2.71039E+10 1.78527E+10 9.11422E+09 59 4.10856E+10 3.57379E+10 2.65070E+10 1.75313E+10 9.01$66E+09 60 4.03256E+10 3.517293+10 2.615195+10 1.73396E+10 8 95435E+09 61 3.99433E+10 3.48877E+10 2.59726E+10 1.72425E+10 0.92357E+09
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l l i Table 4.1.2.6 Standard Core Loading a DPA Eates At Pressure vessel Lower Wold I (s=67.1048cm) 0 0T 1/4 T 1/2 T 3/4 T T 1 4.175665+11 2.70640E+11 1.61195E 11 9.13123E+12 4.13311E 12 2 4.176933 11 2.70709E*31 1.61243E+11 9.13615E 12 4.12695E.12 3' 4.194495 11 2.71329E.11 1.61630E 11 9.15522E 12 4.12658E 12 4 4.217965+11 2.73403E.11 1.62770E 11 9.21237E.12 4.14475E.12 5 4.270913 11 2.76684E+11 1.64509E*11 9.30504E 12 4.17511E 12 6 4.34023E*11 2.8102SE*11 1.67022E*11 9.42784E*12 4.21459E 12 7 4.43301E 11 2.06947E 11 1.70339E*11 9.59604E 12 4.26732E*12 0 4.56095E+11 2.94873E 11 1.74712E 11 9.81418E 12 4.33563E 12 9 4.68871E 11 3.02523E 11 1.78069E 11 1.00211E.11 4.40103E 12 10 4.806535 11 3.09810E 11 1.02861E 11 1.02180E*11 4.46247E.12 11 4.94005E*11 3.18311Eo11 1.07413E.11 1.04425E 11 4.53157E*12 12 5.09173E+11 3.26879E.11 1.91982E 11 1.06640E 11 4.59992E.12 13 5.23095E 11 3.35077E.11 1.96290E+11 1.08718E 11 4.66326E.12 14 5.35816E+11 3.42465E.11 2.00118E 11 1.10536E*11 4.71813E*12 15 5.466913 11 3.48659E 11 2.03245E*11 1.11984E 11 4.760403 12 16 5.55035E.11 3.53112E.11 2.05377E 11 1.12920E 11 4.787243 12 17 5.600453 11 3.55328E 11 2.06257E*11 1.13270E 11 4.79325E+12 10 5.60071E.11 3.54647E 11 2.05646E*11 1.1293CE+11 4.78350E.22 19 5.55258E 11 3.52050E 11 2.04307E 11 1.12316E*11 4.76734E.12 20 5.5352OR*11 3.49459E*11 2.02074Ea11 1.11659E 11 4.74278E*12 21 5.439735 11 3.43231E 11 2.00012E.11 1.10432E 11 4.70072E 12 22 5.32750E.11 3.367003 11' 1.97102E*11 1.09167E*11 4.67059E 12 23 -5.161473 11 3.308103 11 1.94930E 11 1.08274E*11 4.66423E*12 24 .5.09117E 11 3.292025 11 3.94291E 11 1.07990E 11 4.654645 12 25 4.90036E 11 3.25376E 11 1.929125 11 1.07391E 11 4.62376E.12 26 4.907515 11 3.20970E 11 1.91051E 11 1.06550E+11 4.59193E 12 27 4.85707E 11 3.17758E.11 1.09265E 11 1.05699E 11 4.57020E 12 28 4.860405 11' 3.16290E*11 1.00087E*11 1.05090E*11 4.56206E 12 29 '4.87789E 11 13.15477E.11 1.07456E 11 1.04767E*11 4.55134E*12 30 4.92526E 11 3.14252E.11 1.85879E 11 1.03856E*11 4.50090E 12
> 31 4.884725 11' 3.11070s.11 1.03456E 11' 1.02470E 11 4.44746E 12 4
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Table 4.1.2.6 Standard Core Loadir.g
-DPA Estes At Pressur, Vessel Lower Wold wont'd)
(s=67.1040es) 0- "0=T 1/4 7 1/2 T 3/4 T T
- 32 D 4.007145 11' ' 3.075035 11 - 1'.01250E +11 .1.012735 11 . 4.410805 12 33! 4.72734b 11 3.036473+11' 1.791163 11 1.00150E 11' 4.374523 12 34 4.642723 11--2.993503 11' 1.760095 11 9.90246E-12 4.337643*12 35- 4.550015 11: 2.940405 11--1.746165 11 9.79030E+12 4.299355 12 36 4.432135*11 2.002925 11 1.714563 11 9.630055 12 4.246975 12 37 4.321755 11- 3.017503 11 1.600135 11- 9.466965 12. 4.19033E+12 30 - 4.254073+11 . 2.7734 0E
- 11 1.65370E+11 9.327753 12 4.14373E+12 39 4.22360E+11 .2.746135 11 - 1.435565+11 9.222493 12 4.10530E.12 40 4.223245 11 2.73500E+11 1.624505-11 9.14576E 12 4.07411E 12 41 4.24013E+11 -2.735425 11 1.610165 11 9.00972E*13 4.05255E*12 42 4.252195+11 2.735075 11 1.61444E+11 9.05559E+12 4.041675+12 43- 4.264735 11 3.735745 11 1. 6104 5E + 11 - 9 . 019 67 E.12 4.021465 12 44 4.275025*11 2.729795+11. 1.601125-11 0.950425 12 3.909905 12
'45 4.254103 11 2.700265 11 1.505365-11 0.055295 1* 3.95766E*12 46 4.201465 11 -2.600005 11 1.570395 11 0.774723 12, 3.933253 12 47 4.193645 11 2.659105 11- 1.555475 11 0.69210E*12 3.900305 12-40 4.097005 11_ 2.60427E*11 1.524205 11 0.529343 12 3.041665 12-49 :3.96640E*11 2.52771E+11 1.403135 11 0.322795 12 3.77562E+1*
' 50 = -3.036073 11 - 2.456135 11 = 1.44502E+11 0.139113 12 3.710913 12
-51 3.749455 11- 2.404193 11 1.417658 11 7.999995 12 3.67345E.12
'52 3.643575 11. 2.339623 11 ' 1.30270B+11 -7.025653 12 3.61469E+12
'53 13.504125 11 =2.250743 11 1.339953 11 .7.614665 12 3.546405 12 54 3.360665 11. 2.175305 11 1.296095 11 7.40112E*12 3.479075 12
- = 55 3i21002E+11 2.092265=11. 1.242503 11 7.199605 12 3.412343 12 56L3.059225 11' 2.001465 11 1.205545 1116.96346E.12 13.340725 12'
'57' 2.929155 11 1.923173 11 1.164245 11 6.763025 12 3.270495-12
- 50 '2'.009925 11 1.054043 11 1.12070E*31. 6.592643+12 3.224105 12 59 - 2.735065 11 1.007675 11 1.103203 11- 4.467395 12: 3.105765 12 60 2.607005 11 1.778735 11 1.007723*11 6.39213E 12 3.161703 12 2.662045 11 1.76412E+11' 1.07991E 11 6.353923 12 3.149715 12 a r .
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- . : .. ~.=.: x ..:.:. .. v.- .
..:.... . . . e. - . . .-- - -
Table 4.1.2.7 standard Core 1.oading Downconer Fluxes and DPA Estes (r=210.50cm.s=121.7 pen) FLUE FLUE DPA/s 4 (E>1.0 MEv) (E=0.1 MEv) - 1 6.69557E+10 1.19710E+11 1.01187E 10 2 6.69299E+10 1.19608E+11 1.01150E 10 3 6.70314E+10 1.19961E+11 1.01324E 10 4' 6.76476E+10 1.21097E+11 1.02248E 10 5 1.85990E+10 1.22900E+11 1.03679E 10 6 6.9OO58E+10 1.25380E+11 3.05616E 10 7 7.16070E+10 1.20773E+11 1.08224E 10 0 7.40597E+10 1.33554E+11 1.11935E 10 9 7.65923E+10 1.38414E+11 1.15733E 10 10 7.891275+10 1.43033E+11 1.19257E 10 11 8.10024E+10 1.49743E+11 1.23634E 10 12 8.48495E+10 1.54802E+11 1.28253E 10 13 0.78962E+10 1.60935E+11 1.32885E 10 14 9.00014E+10 1.66890E+11 1.37322E 10 15 9.33791E+10 1.72303E+11 1.41274E 10 16 9.54602E+10 1.76843E+11 1.44507E 10 17 9.689275+10 1.80188E+11 1.46770E 10 10 9.72561E+10 1.81678E+11 1.47462E 10 19 9.62308E+10 1.809BOE+11 1.46166E-10 20 9.61728E+10 1.80991E+11 , 1.46048E 10 21 9.36431E+10 1.70056E+11 1.42538E 10 22 9.12471E+10 4 1.74052E+11 1.39068E 10 23 0.7W276E+10 1.70559E*11 1.34282E*10 24- 8.73276E+10 1.69624E+11 1.33561E 10 25 0.56507E+10 1.67236E+11 1.31066E 10 26' 8.36407E+10 1.64010Ew11 1.20088E 10 27 8.22150E+10 1.61057K+11 1.25909E 10 28 0.16417E+10 1.59223E+11 1.24984E 10 ' 29' 8.12521E+10 1.50249E+11 1.24333E 10
~30' 8.10532E+10- 1.56061E+11' 1.23826E 10 '
31 7.99106E+10 1.51556E+11 1.21809E 10 32 7.85587E+10 1.47340E+11 1.1952SE 10
) W i . }I .g '.
;.Q-I t[ n ' {- f M t. i ,' ~% ' .k - A .k
- J4^y
- 2 #4'i'N 4A , h 5fy 39 * ' t 4 h f' $ 'F ( .
4 '*-
,.4~- i l
~
. . , ~ ~ q -
) s 'h
- l ,, Rj ell L' y,s g
&f }lw k kKi? .f Nl hik fe jbh*WlMs -5 : "*r -+
a ' k %l - v ,
.?hf$ bN$hN Y4
. 5 -e,(
, , , , . .. , , , , __ , __7-._ , ,, , .
l t i i i Table 4.1.2.7 - Standard Core Loading l Downcomer Flumes and DPA Estes (Cont'd) (r=210.50ca,s=121.79em) FLUE FLUE DFA/s 0 (E 1.0 serv) (E>0.1 serv) 33 7.70202E+1p 1.43255E+11 1.170275+10 34 7.53040E+10 1.39254E+11 1.14400E+10 35 7.37100E+10 1.35372E+11 1.11761E+10 36 7.10300E+10 1.30034E+11 1.07710E+10 37 6.910063+10 1.25912E+11 1.046975 10 30 6.01046E+10 1.23951E+11 1.03242E*10 39 6.01982E+10 1.239965+11 1.03236E+10 40 6.09345E+10 1.25613E+11 1.043545 10 41 7.01030E+10 1.20214E+11 1.06143E+10 42 7.09500E+10 1.30150E+11 1.07439E+10 43 7.17176E+10 1.31995E+11 1.00654E+10 44 7.293193+10 1.34039E+11 1.10542E+10 45 7.353665+10 1.36659E+11 1.11531E 10 46 7.20144E+10 1.36276E+11 1.10610E.10 47 7.31290E+10 1.36700E+11 .1.110213 10 40' 7.19644E+10 1.340375+11 1.09144E+10 49 6.91960E+10- 1.30100E+11 1.05151E+10 50 6.61544E+10 1.24561E+11 1.00666E+10 51' 6.430778+10 1.207465+11 9 .7010 0 E +:.1 52 6.19640E+10 1.15797E+11
- 9.41604E+11 53 S.07934E+10 1.09279Et11 0.93163E+11 54 5.55210E+10 1.02537E+11 0.43140E+11 55 5.22970E+10 9.59097E+10 7.939025 11 56 4.07310E+10 0.07261E+10 7.39040E+11 57 4.59419E+10 0.20002E+10 6.96950E+11 50 4.33020E+10 7.76001E+10 6.572005 11 59 4.17339E+10. 7.43051E+10 -6.33090s.11 60 , 4.06050E+10 7.21070E+10- 6.171445 11
, , 61 4.01560E+10. ,7.11196E+10 6.00971E*11;
; p f. 4 g g.j y_ y ,-
~
W} h tdy; 4n- ~ %y gj , ?_ n,- g_ %l-y s_ f q yNp ; , _ g,y lg . 'g_ _ r -m
-;- r i 2, ; y. j _,
bH .hk ':, ip~ k-
*/ .Q . # , g: < <
l .,.k? $hf - ypwun. . . . 4 m<
*ommwqvacape. w a
Table 4.1.2.8 Standard Core Loading Cavity Fluxes and DPA Rates (r=320.06cm s=177.27ca) FLUE FLUX DFA/s 8 (E>1.0 MEv) (E>0.1)tEv) i 1 1.02943E+09* 9.01502E+09 3.23295E.12 2 1.02944E+09 9.01542E+09 3.23302E 12 3 1.02804E+09 9.00099E+09 3.23017E 12 4 1.02813E+09 9.00762E+09 3.229492 12 5- 1.02837E+09 9.00607E+09 3.22971E 12 6' 1.028785+09 9.00456E+09 3.22964E+12 7 1.02897E+09 9.00078E+09 3.228892 12 8 1.03016E+09 9.00052E+09 3.22981E 12 9 1.03135E*09 9.00128E+09 3.23097E*12 10 1.03097E+09 8.99529E*09 3.22910E 12 11 1.03047E+09 8.98847E+09 3.22685E 12 12 1.02956E+09 8.98104E+09 3.22405E*12 13 1.02790E+09 8.97178E+09 - 3.22013E*12 14 1.02565E+09 8.96029E+0$ 3.214952 12 15 1.02265E+09 8.34605E+09 3.20846E 12 16 1.01929E+09 8.92877E+09 3.20095E 17 17 1.01584E+09 8.90796E+09 3.19262E 12 18 1.01287E+09 8.88662E+09 3.18475E 12 19 1.01059E+09 8.86927E+09 3.17858Eal2 20 1.01040E+09 8.86274E+09 3.176762 12 21' 1.00840E+09 8.84412E+09 3.17058E.12 22 1.007065+09 8.83167E*09 . 3.16624E*12 23 1.00604E+09 8.82245E+09 3.16300E 12 24 1.00605E+09 8.82129E+09 3.16279E*12 25 1.00582E+09 8.81787E+09 3.16173E 12 26 1.00505E+09 8.81120E+09 3.15936E*12 3.155!5R 12 27 1.00355E+09 8.80142E+09 28 1.00211E+09 8.79281E+09 3.15210E*12 29 1.00127E+09 8.78804E+09 3.15015E 12
-30 9.99412E+08 8.77755E+09 3.14530E*12 .
, 31 _9.96954E+08 8.76228E+09 3s1396PE 12 5
h .-. 32' 9.94791E+08 8.74939E+09 3.13444E.12
'33 9.92102E+08 8.73482E+09 3.12830E.12
,, g ? . A .* 4e
*^ A^. .ht i d ,, 'fd 5 T 'jY ' k h.
' h l 'I f 2
< { f % *k .- s ' k'~ d d-- p flI 9 ;[i 1 F %'
,. 4 '!! a
.._ kg+', 4 5 -l ,
+. "A +
1
, .g, e ,3 f gg,s +;t p hi [k ( *!I( hh / .Q.4 'r" *h j g [y55h' N f f f);6 }ghikkdO!! f h Ibj (h(# I. [ . p f i,dM*, ' , ( d t
. .. .. . . . . . . . 7.; :: .~ ~. ~ ~.~ :
~^ "
. Table 4.1.2.8 Standard Core Loading Cavity F1bzes and DPA Rates (cont'd)
(r=320.06ca.s=177.27ca) i FLUE FLUE DPA/s 1 8 (E>1.0 mrv) (E>0.1 NEV) , i l 34 9.89077t+08 8.71871E+09 3.12148E.12 - l 35 J.85241E+08 8.69836E*09 3.11207E.12 36 9.786585+08 8.66429E+09 3.09840E.12 37 9.71692E+08 8.62215E+09 3.08174E+12 8 38 9.64724E+08 8.57789E+09 3.06466E.12 39 9.57418E+08 8.532075+09 3.04689E.12 ' 40 9.49384E+00 0.48433E+09 3.02793E 12 41 9.41926E+08 8.44180E+09 3.01070E*12 42 9.37228E+08 8.41580E+09 3.00005E 12, 43 9.31896E+08 0.38662E+09 2.98805E*12 44 9.23716E+00 8.34163E+09 2.96959E 12 45 9.16185E+00 8.29952E+09 2.95244E 12 46 9.11425E+08 8.27302E+09 2.941693 12 47 9.07294E+08 8.24855E+09 2.93193E*12 48 9.00514E+08 8.20079E+09 2.91606E 12 49 8.93901E+08 8.16985E+09 2.90062E 12 50 8.90101E+08 8.14608t+09 2.89140E*12 51 8.87471E+08 0.12907E+09 2.88477E 12 52 8.84169E+00 8.10909E+09 2.87705E*12 53 8.00975E+0g 8.00973E+09 2.86920E 12 54 8.70105E+08 8.07109E+09 2.86202E*12 55 8.75496E+08 8.05440E+09
- 2.85558E+12 56 8.71876E+08 0.03293E+09 2.84705E+12 57 '8.70113E+08 0.02070E+09 2.84247E+12 58 8.67167E+00 8.00366E+09 2.83569E 12 59 8.66773E+08 7.99914E+09 2.83424E 12 60 8.66015E+08 -7.99392E+09 2.83230E 12 61 8.65740E+08 7.99194E+09 2.83157E*12 l' .
y~ 2 v <! .j. - 5 ypdg4 -j~5 f
, 1, **s , -t; e y t ;n ig h y'; -
O 4 ? gM , t '1 . . * , - w k et . .-- ,p a + [ y- fdk e p{gkdQpg.kgg pp j-+
. fl 1 3?u ,
i jag 4j,df 9p$apj g-Qg fl g. A 8
Table 4.1.2.9 Standard Core Loading Flux Spectrum At Pressure Vessel (PressuIre Vessel Capsule In) 8 15.5' .125.488cm Group 0T 1/4 T 1/2 T 3/4 T T 1 2 1.34004E+07 6.03020E+06 2.54426E+06 1.06968E+06 4.65023E+05 3 4.20813E+07 1.86479E+07 7.70275E+06 3.15887E*06 1.33379E+06 4 1.75195E+08 7.77592E+07 3.17580E+07 1.27914E+07 5.30266E+06 5 3.39395E+08 1.51262E+08 6.10609E+07 2.41801E+07 9.83754E+06 6 5.90665E+08 1.58392E+08 1.00967t+08 3.86032E+07 1.51169E+07 7 1.54113E+09 6,46641E+08 2.39974E+08 8.72151E+07 3.23568E+07 8 2.27942E+09 9.40904E+08 3.43468E+08 1.23041E+08 4.44146E+07 4.17926E+09 9 2.94717E+09 1.72441E+09 6.31242E+08 2.27138E+08 0.02326E+07 10 1. 2 6 9 8 ,'E+ 0 9 4.84919E+08 1.80883E+08 6.38869E+07 11 2.16745E+09 9.814582,08 3.83223E+08 1.44961E+08 5.12002E+07 2.46760E+09 12 1.22373E+09 1.16140E+09 4.64842E+08 1.79066E+08 6.28895E+07 13 5.84109E+08 2.36458E+08 9.18980E+07 3.23944E+07 14 3.15611E+08 1.59021E+08 6.70858E+07 2.69577E+07 1.00840E+07 15 1.55286E+09 7.96555E+08 3.41000E+08 1.38897E+08 5.15699E+07 16 3.98671E+09 2.15949E+09 4.15372E+09 2.49334E+09 9.58512E+08 4.00040E+08 1.45036E+08 1.20167E+09 17 5.75809E+09 3.68149E+09 1.86892E+09 5.35826E+08 2.03143E+08 18 8.73523E+09 8.69067E+08 3.38535E+08 19 6.61604E+09 3.86360E+09 2.00538E+09 8.18435E+08 20 5.56635E+09 4.68957E*09 3.05523E+0) 1.75235E+09 7.89423E+08 21 2.86008E+09 2.20627E+09 1.38858E+09 7.74542E+08 3.28518E+08 7.95371k 19 8.09916E+09 22 6.03883E+09 3.78933E+09 6.39531E+09 6.54231E+09 5.09178E+09 3.32359E+09 1.70351E+09-23 1.53636E+09 24 7.09089E+09 7.37463E+09 5.83849E+09 3.76972E+09 1.54915E+09 25 7.22374E+09 8.79679E+09 7.70684E+09 5.34731E+09 2.38270E+09 8.92968E+09 26 9.14224E+09 7.58075E+09 5.19241E+09 2.440492+09 8.65439E+09 9.59941E+09 8.38386E+09 27 5.92608E+09 2.78120E+09 28 6.02155E+09 6.12114E+09 5.25983E+09 3.70188E+09 1.72611E+09 29 4.73095E+09 4.45339E+09 3.70920E+09 2.56747E+09 1.16605E+09 30 1.65571E+09 1.19812E+09 9.57109E+08 6.57726E+08 3.15729E+08 31 8.18351E+0B 4.08395E+08 3.23962E+08 2.22161E+08 1.28353E+08 2.07212E+09 2.27206E+09 32 1.99328E+09 1.48555E+09 8.43522E+08 33 1.21342E+09 1.29224E+09 1.16184E+09 8.84812E+08 5.06656E+08 2.39033E+09 2.08344E+09 34 1.71712E+09. 1.27142E+09 7.41995E+08 35 4.19607E+09 2.41134E+09 1.66284E+09 1.15857E+09 7.21073E+08 36 5.23504E+09 3.65217E+09 2.47138E+09 1.60971E+09 8.35726E+08 37 4.69929E+09 2.85953E+09 1.83504E+09 1.15592E+09 6.19866E+08 38 7.68285E+09 4.43931E+09 2.65387E+09 1.60042E+09 8.84664E+08 39 4.2490FE+09 1.96302E+09 1.10425E+09 6.55982E+08 4.04734E+08 40 4.66985E+00 2.37076E+09 1.26143E+09 7.22978E+08 4.25704E+08 41 6.05506E+09 2.92646E+09 -1.47803E+09 8.14790E+08 4.94604E+08 i 42 7.63070E+09 3.66787E+09 1.77643E+09 9.34762E+08 5.62218E+08 43 14.41493E+09 1.97298E+09 9.18737E+08 4.71662E+08 2.96609E+08 44 5.92169E+09 2.39279E+09 1.03252E+09 5.12118E+08 3.53170E+08 45 4.47157E+09 1.60795E+09 6.31627E+08 3.02245E+0B 2.38733E+08
. / 46" 3.82771E+09 7.61855E+08 2.19882E+08 1.04247E+08 1.66904E+08
( '8.29237E+09 9.88803E+08 1.50504E+08 7.33782E+07 3.16178E+08
, ,( 47}y , , 3. 8 8 610E +10 ; - 1.19 4 8 6 E+ 09 - 3.61846E+07 2".63903E+07 7.03751E.08 i - h [4
- Q + %>&gfMMt$1%W '
,, % ,- A 9M
Table 4.1.2.10 standard Core Loading Flua Spectrus At Capsule Location Group Thermal Bhleid Prosaure Vessel Cavity 1 4.267115+07 1.60000E+07 2.06720E+05 2 1.45534B+00 5.109165+07 0.06094E+05 3 6.00301E+00 2.19393E+00 3.12212E+06 4 1.43540E+09 4.20001B+00 5.66333E+06 5 2.75610B+09 7.500473+00 0.519575+06 6 7.415778+09 1.97003B+09 7 1.79233B+07 1.23333B+10 2.903215+09 2.45560E+07 0 = 2.69703E+10 5.614165+09 4.42734B+07-9 2.26943E+10 4.04130B+09 3.495298+07 10 1.736378+10 2.96103E+09 -2.707065+07 11 2.02292E+10 3.33300E+09 3.451073+07 12 9.915565+09 1.64260B+09- 1.776175+07 13 2.627573+09 4.376565+00 14 5. 53974B+06
- 1.32935B+10 2.09754B+09 2.73430E+07 15 3.57601B+10 5.26555B+09 7.43913E+07 16 3.99955E+10 5.355793+09 17 1.04204E+00 5.95111E+10 7.377065*09 1.700115+00 10 1.00036E+11 1.038598+10 19 4.19930E+00 6.476563+10 6.26002B+09 4.002168+00 20 3.40231E+10 3.49051E+09 2.03052E+00 21 0.40700E+10 7.40525E+09 22 0.59070E+00 6.90710E+10 6.262065+09 0.37963B+00 23 7.59062E+10 7.032065+09 24 0.61022B+00 6.45J915+10 5.72732E+09 1.243963+09 25 9.69050E+10 9.311215+09 26-1.601165+09 0.00710B+10 0.20525B+09 1.70632E+09 27 6.92903B+10 '6.65551E+09 1.12321E+09 at 5.71735B+10 5.59012B+09 0.11510E+00 29 2.277175+10 2.354075+09 30 2.54354B+00 1.490695+10 1.63042E+09 1.181065+00 31 1.443515+10 1.31003E+09 32 4.10315E+00 1.15322E+10 1.05062E+09 2.75023B+00 33 2.700095+10 2.96005B+09 5.69065E+00 34 5.00010E+10 35 6.470665+09 .- 4.34430E+00 6.91935E+10 7.30020E+09 6.49900E+00 36 6.67670E+10 6.960695+09 5.20495E+00 37 1.03094B+11 1.09990B+10 7.76450E+00 30 6.06505E+10 6.62742E+09 3.704765+00 39 6.24260E+10 6.70022E+09 3.02704E+00 40 0.323275+10 9.004573+09 4.530793+00 41 1.023175+11 1.137415+1J 42 5.16374E+00.
5.96955B+10 6.777785+09 2.79154E+00 43 7,01260E+10 9.22740B+09 3.440075+00
- 44. 5.77013E+10 7.10653E+09 2.43411E+00 45- .5.414995+10- 7.091998+09 2.017393+00 46 1.14442E+11 1.67072E+10 4.10005E+00 47.. 2.925575+11- 0.37771E+10 1.09560B+09 Thermal Ehleid capsule flua spectrum is at r=203.25ca. s.121.79am. 4 20' ~
Pressure vessel capsule flua spectrum is at r=215.43es, s 121.79am. 0 3( . Cavity Capsule Elus spectrum is at r=320.06ca, s.177.27am, . 0 9.5*.a
;(
s y :i&iMe k%dWim < 3 !1 - 5 .- _
~
j;l{ '[ -s &
' -4 ,
M u& O; Q M & n e M v. m . > y wy ggggyggg&g&39 g3
r--- . . . . . . _ _ . . . . . .._ ._.. Table 4.1.2.11 Standard Core Loading ( Effect of Selected Cross Sections on the Calculated Reaction Rates Axial Peak Reaction Rate (reactions /sec*atos) I o Thermal Shield Capsule (r=202.25ca, s=121.79cs,0 20 )
. Detector .
. SAILOR .
. Material BUGLR93 .
. INDF/B.IV . ORNL
.........................................................../TM.11476 27 ...............
. . 16 . 16
.Al (n,A) 3.00239X10
. 4.03820x10 .
. 32 . 14 . 14
.8 (n,p) 2.44909x10
. 2.52759x10 .
46 . 15 . 15
.Ti (n,p) . 4. 699.19 X10 . 4.54495x10 54 . 14 . 14
.Pe (n.p) . 3.09914X10 . 3.12051x10 14 .
. 3
. 56 . 16 . 16 07175x10 ................
va (n,p) 5.12145x10
. 5.54759x10 .
50 . 14 . 14
,Ni (n.p) 4.19745x10
. 14 .
. 4.17753xA0 . 4
. 63 . 16 10360x10 ...............
.Cu
. 16 .
(naX) . 2.51129x10 . 1.96732x10
. 65 . +16 . 16
.Cu (n,2n) 2.42305x10'
. 2.99767x10 *
. 115 . 14 14
.In (n,n') . 0.72960210
. 0.50503x10
. 237 .
13 . 13
.Wp (n,f) l.98422x10
+13 .
. 9.46386x10 .
238 _ . 13 9.36238x10 .................
.V (n,f). . 13 . +13
. 1.40695x10 . 1.40763x10 . 1
.......................................................... 41495x10. ................
. SAILOR used a flat weighting spectrum to collapse the cross sections. :
+ - BUGLE 93 used a pressure vessel 1/4T weighting spectrum to collapse the -
m .,cr,oss sections.. mt A 2 = f $h V i
,g-bt , ,
~
# s . . Ay -
.p ,
-v;q hn,-l9,9
* /(:
'V .
's. , i ** O ' ' Y?Yb i
. . . ' ' Y y ls ____ - ---
Table 4.1.2.12 Standard Core Loading Effect of Selected Cross Sections cte the Calculated Reaction Rates Axial Peak Reaction Rate (reactions /sec* atom) Pressure Vessel Capsula (r=215.43ca, s=125.49em,0 20* )
. Detector . . SAILOR . .
. Material . SUGLE93 . ENDF/3 IV . ORNL/TM 11476 .
. 27 . . 16-
. 16 . .
.Al (n,e() . 1.13574X10 . 1.17933x10 . .
. 32 . - 15
. 15 . .
.5 (nep) . 5.08199x10 . 5.20401x10 . .
. 46 . - 15
. *15 . .
.Ti (n,p) . 1.17613x10 . 1.14241x10 . .
. 54 . + 15 . . 15 . . 15 .
.Fe' (n,p) . 6.57302K10 . 6.78698x10 . 6.50612x10 .
. 56 .
- 16 . 16 . .
.Fe (n p) . 1.43009x10 . 1.54390x10 . .
. 50 . + 15
. 15 . -15 .
.Ni (n,p) . 8.62894x10 . O.68697x10 . 8.45897x10 .
. 63 . 17 . 17 . .
.Cu (n .t<) . 6.06179X10 . 5.63029x10 . .
. 65 . 16 . +16 . .
.Cu (n.2n) . 8.29140110 . 1.01544x10 . .
. 115 . + 14
. 14 .
.In (n,n') . 1. 0141x10 . 1.33060x10. .
. 237 . - 13
. 13 . - 13
'. Np (n, f) . 1.18077x10 . 1.27145x10 . 1.22359x10 .
. 230 . + 14 . 14 . - 14 .
.U (n, f) . 2.37573x10 . 2.39417x10 . 2.38418x10 .
BUGLE 93 used pressure vessel 1/4T weighting sp3ctrum to collapse cross sections. SAILOR used flat weighting spectrum to collapse cross sections. 1 ,
,y m , ,
4% . n- y ,% , . p y, m. %.gnm %. t, . E t [k f } M"' ._' 4 ' yi . " '
'-4 .
- m. _ _ . ... .. .. .. __ -- . .-- .. . -
Table 4.1.2.13 Standard Core Loading Effect of Selected Cross Sectiens on the Calculated Reaction Rates Axial Peak Reaccion Rate (reactions /sec* atom) o Cavity Capsule (r=320.06ca, s=177.27ca,0=9. 5 )
. Detector . . SAILOR . .
. Material . BUGLE 93 . ENDF/B.IV . ORNL/TM 11476 .
. 27 . 1% . 18 . .
.Al (n.s() . - 1.40434110 . 1.45241x10- . .
. 32 - , 17 . 17 .
.8 (n,p) . 4.70800x10 . 4.88722x10 .
. 46 . 17 . 17 .
.Ti (n.p) . 1.13189x10 . 1.10318x10 .
. 54 . 17 17
. . 17
.Fe (n,p) . 6.14379X10 . 6.25252x10 . 6.08292x10
. 56 . 18 . 18 .
.Fe (n.p) . 1.59444110 , 1.71283x10 .
................................... 1.....................................
. 58 . 17 17 17
.Ni (n.p) . 8.63266L10 . 8.52622x10 . 8.60783x10
. 63 . 19 . 19 .
.Cu (n,0() . 7.48370x10 .- 6.63479x10 .
65
. . 18 .
18 . .
.Cu (n,2n) . 1.29640x30 . 1.56898x10 . .
. 115 . 16 . 16 .
.In- (n.n') . 2.31850x10 . 2.28786x10 .
. 237 -15 15
. . . -15 .
. Np - (n,f) . 4.32775x10 . 4.55761x10 . 4.62433x10 .
. 238 . 16 16
. . 16 .
.U (n,f) . 3.22105x10 . 3.18192x10 . 3.24756x10 -
BUGLE 93 used pretsure vessel 1/4T weigeting spectrum te collapse cross sections.. SAILOR used flat weighting spectrum to collapse cross sections. g fl- ' [ s k ,i ,..f g p.
.I' g- g " C
+ -
5-Ws 4 t i >( ) IA 'i us&hw . - ' i W W o' *. % % wd k M u w
1 Table 4.1.3.1
- Low Leakage Core Loading Flux (E>1. 0 ME'D ht Pressure Vessel s 195.760cm 195.760cm 121.760cm 192.062cm 192.062em 8 0T 1/4 T 1/2 T 3/4 T T 1 1.53440E+10 0.77316E+09 4.28603E+09 1.99076E+09 8.23397E+08 2 1.53465E+10 8.77444E+09 4.28683E+09 1.99228E+09 8.22090E+08 3 1.53800E+10 8.00021E+09 4.30069E+09 1.99800E+09 8.22556E+08 4 1.55703E+10 8.90427E+09 4.34861E+09 2.01860E+09 8.29407E+08
'S 1.58767E+10 9.07218E+q9 4.42652E+09 2.05268E+09 8.40659E+08 6 1.62824E+10 9.29594E+09 4.53086E+09 2.09764E+09 8.55525E+08 7 1.68219E+10 9.59862E+09 4.67203E+09 2.15909E+09 8.75460E+08 '
3 1.75564E+10 1.00013E+10 4.85784E+09 2.23875E+09
- 01185E+08 9 1.82704E+10 1.03835E+10 5.03303E+09 2.31405E+09 9.25666E+08 10 1.89160E+10 1.07406E+10 5.19834E+09 2.38465E+09 9.48505E+08 11 1.96779E+10 1.11528E+10 5.38592E+09 2.46500E+09 9.74243E+08 12 2.04448E+10 1.15664E+10 5.57393E+09 2.54425E+09 9.99594E+08 13 2.11853E+10 1.19619E+10 5.75164E+09 2.61885E+09 1.02321E+09 14 2.18621E+10. 1.23200E*10 5.91054E+09 2.68456E+09 1.04386E+09 15 2.24440E+10 1.26233E,10 6.04233E+09 2.73773E+09 1.06007E+09 16 2.28961E+10 1.28465E+10 6.13457E+09 2.77331E+09 1.07080E+09 17 -2.31802E+10 1.29663E+10 6.17690E+09 2.78773E+09- 1.07424E+09 18 2.32153E+10 1.29529E+10 6.15850E+09 2.77813E+09 1.07143E+09 19 2.30083E+10 1.28464E+10 6.10690E+09 2.75654E+09 1.06545E+09 20 2.29534E+10 1.27433E+10- 6.05719E+09 2.73661E+09 1.05837E+09 21 2.25502E+10 1.24785E+10 5,94840E+09 2.69583E+09 1.04510E+09 12 2.20532E+10 1.22022E+10 5.~ 84253 E+09 2.65651E+09 1.03514E+09 23 2.12926E+10 1.19476E+10 5.76314E309 2.62921E+09 1.03195E+09 24 2.09762E+10 -1.18797E+10 5.74106E+09 2.62093E+d9 1.02934E+09 25 2.05278E+10 1.17203E+10 5.6928PT 99 2.60318E+09 1.02052E+09
" 26 ~ 2.01735E+10 l'15437E+10 5.62920E+09 2.57844E+09 1.01120E+09 27 1.99720E+10 1.14270E+10 5.57020E+09 2.E5336M+09 2.00427E+09 28 2.00115E+10 1.13828r+10 5.53295E+09 2.53564E+09 1.00139E+09 29 2.01135E+10 1.13576E+10 5.51286E+09 2.52611E+09 9.98167E+08 30 2.03881E+10 1.13347E+10 5.46461E+09 2.49951E+09 9.83678E+08 31 2.02263H+10 1.12338E+10 5.39127E+09 2.46027E+09 9.67816E+08 32 1.98781E+10 1.11019E+10 5.32140E+09, 2.42591E+09 9.56042E+08 33 1.95098E+10 1.09463E+10 5.24838E+09 2.39232E+09 '9.44384E+08 3 4 ' "1.910 04E+10 ' 1.07601E+10 5.16669E+097 2.35630E+09 '9.31959E+08 "9h lyf hliyk%fd h , d:j p'% i td 'i(% JN /;N ] y p yrks tQ 4 . L -Y
^
< "h-tN { h bNygp * *
,4>,
1 y 4 o s t y
.. . >.it
- f i,(V.S Ed e w t n
y y dQ p[ Q - s , <^: .3 * % QNhyg $ j M ,
, *C C. 3 .
Table 4.1.3.1 Low Leakage Core Loading Fluz (E>1.0 MEV) At Pressnes vessel (cont'd) s 195.760cm 195.760cm 195.760cm 192.062cm 192.062cm 8 0T 1/4 T 1/2 T 3/4 T T
. s
-- 3 5 1.8673SE+10- 1.055165+10 5.07709E+09 2.31783E+09 9.19423E+08 6 36 1.00366E+10 1.02334E+10' 4.94250E+09 2.26129E+09 8.98905E+08 37 1.73041E+10 -9.84269E+09 4.76751E+09 2.18682E+09 8.73824E+08 38 1.66555E+10 9.40091E+09 4.59813E+09 2.11312E+09 8.49110E+08 39 1.60820E+10 9.15020E+09- 4.43900E+09 2.04247E+09 8.24875E+08 40 1.55741E+10 8.85210E+09 4.29191E+09 1.97554E+09 0,01495E+08 41 1.51352E+10 8.59263E+09 4.16180E+09 1.91534E+09 7.80872E+08 42 1.48690E+10 8.43455E+09 4.08174E+09 1.87822E+09 7.68619E+08 43 1.46073E+10 8.27503E+09 4.00094E+09 1.84044E+09 7.54258E+08 44 1.41865E+10 8.02084E+09 3.87306E+09 1.78133E+09 7.32955E+08 45 1.37151E+10 7.74946E+09 3.74090E+09 1.72135E+09 7.127h2E+08 46 '1.33673E+10 7.56416E+09 ?.65350E+09 1.68243E+09 7.00233E+08 47 1.30799E+10 7.38977E+09 3.56792E+09 1.64378E+0S 6.85980E+08 48 1.25494E+10 7.09495E+09 3.42879E+09 1.58211E409 6.64330E+08 49 1.19600E+10 6.77711E+09 3.28135E+09 1.51753E+C9 6.42842E+08 50 1.15097E+10 6.53434E+09 3.16804E+09 1.46838E+0) 6.26879E+08 51 1.12010E+10 6.36387E+09 3.08883E+09 1.43340E+0f 6.15041E+08 52 1.08357E+10 6.16252E+09 2.99506E+09 1.39239E+09 6.00677E+08 53 1.04211E+10 5.93579E+09 2.88987E+09 1.34649E+09 5.85150M+08 54 1.00285E+10 5.72101E+09 2.79046E+09 1.30341E+09 5.70782E+08 55 9.66131E+09 5.52110E+09' 2.69816E+09 1.26330E+09 5.57406E+08 56 9.27224E+09 .5.31364E+09 2.60333E+09 1.22253E+09 " 43730E+08 -
57 8.969275+09 5.14457E+09 2.52498E+09 1.18853E+D9 5.32574E+08 58 8.69695E+09 5.00024E+09 2.45921E+09 1.16033E+09 5.23063E+08 59 8.53277E+09 4.9051CE+09 2.414285+09 1.14066E+09 5.16687E+08 60- 8.42832E+09 4.84754E+09 2.38730E+09 1.12900E+09 5.12768E+08 61 8.37590E+09 4.81074E+09 2.37389E+09 1.12311E+09 5.10808E+08
- 1. 4 7 'M . ,' -' k* h : .i - -- , N d 'af
/ ( I'
- i > 'j ,
o
' v i.; * ' V g, 4 4 ' ~ -
s
%- sr p 3 7 pgjm (f, ,
4 g 7c 4 W;s W #Mgga% g A;ppea j m pm ,, i Asa @ dgiv M ydQnd QQgefjpbg%sy
_ _. . . _ , - . _ . . . - . . _ . _ . _ _ _ . _ . _ . _ . . , . , _,,_s_.-- . . _ _ , . . . _ _ .y_; _ Table 4.1.3.2 Low Leakage Core Loading. Flux (E>0.1 NEV) At Pressure Vessel s- 195.760cm 192.062cm 192.062cm 192.062cm 108.3 63 cm
'8 0-T 1/4 T 1/2 T 3/4 T T 1b3.51282E+10. 3.02704E+10 2.22113E+10- 1.44301Eh10 6.99700E+09
- 2 :3.51500E+10 l3.02935E+10' 2.22270E+10' 1.44413E+10 6.98036E+09 3- 3.52711E+10 3.04196E+10 2.231575+10 1.44002E+10 6.99290E+09 4 3.57027E+10 3.07600E+10 2.25403E+10 1.46211E+10 7.03531E+09 ,
5 3.63970Ft10 3.13109E+10- 2.291395+10 1.40203E+10 7.10412E+09 6 -3.73249E+10 3.20535E+10 2.34021E+10 1.51032E+10 7.19375E+09 7 3.85758E+10 3.30529E+1D 2.40649E+10 1.54750E+10 7.31254E+09 . 0 4.02351E+10 3.43540E+10 2.49191E+10 .1.59510E+10 7.46377E+09 9 4.18353E+10 3.55701E+10 2.57160E+10 1.63950E+10 7.60631E+09 10- 4.33325E+10 3.67440E+10 -2.64770E+10 1.60172E+10 7.74061E+09 11 '4.50607E+10 3.00754E+10 2.73363E+10 1.72920E+10 7.09009E+09 12 4.'68104E+10 3.94053E+10 2. 8189 8E+10 1.77602E+10 8.03751E+09 13 4.05070E+10 '4.06732E+10 2.899465+10 1.01990E+10 0,17467E+09 14L-5.00550E+10 4.10215E+10 2.97159E+10 1.05807E+10 8.29526E+09 15 15.13083E+10 4.279575+10 3.03100E+10 1.89000E+10 0.39252E+09 16 .5.24290E+10 4.352F3E+10- 3.076085+10 1.91393E+10 8.46120E+09 17 5.31071E+10 4.39722E+10 3.10136E+10 1.92662E+10 0.49342N+09 10 .5.33204E+10 4.40791E+10- 3.10528E+10 1.92783E+10 8.49710E+09 19 5.31259E+10 4.39562E+10 3.09660E+10 1.92279E+10 .8.48454E+0.4
-20 5.30582E+10 4.37594E+10 3.00260E+10 1.91510E+10= 0.45294E+0J 21:-5.26165E+10 4.32996E+10 '3.05414E+10 1.899965+10 8.39262E + C9 22 5.203265+10 4.27383E+10 3.02019E+10' 1.00162E+10 8.34843E+09 23 5.12279E+10 4.22550E+10 2.99359E+10 1.06754E+10 8.33878E+09 24 5.09146E+10 ,4.20965E+10 2.90451E+10 1.06275E+10 8.32144E+09-25 5~.04631E+104.17654E+10 2.96591E+10 -4. 0527 0 E+10 0.26662E+09 26 4.90965E+10 4.13215E+10 2.93951E+10 1.83020E+10 0.20816E+09 27- 4.92754E+10 4.09019E+10 -2.91246E+10 1.02318E+10 0.16732E+09
- 28. 4.08595E+10' 4.06166E+10 2.09240E+10 1.81105E+10 0.14907E+09 29.-4.87143E+10 4.0470CE+10 2.881995+10 1.00575E+10 8.12772E+09 30 4.04120E+10 4.00830E+10- 2.05206E+10 1.78870E+10 8.03335E+09
- 31 ; 4.732465+10 3.933775+10 2.80150E+10x 1.75097E+10. 7.91877E+09< +
.32 4.61745E+10 3.86068E+10 2.75316E+10'.1.73121E+10 7.83062E+09 I33 ' t 4'.51261E+10 '3.70836E+10 2.706173+10- 1.70433E+10" 7;74107Ei19' i34 -4i40606E+10 3.71215E+10. 2.65755E+10 1.67672E+10 7.64717E+09:
oy :r m s
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[ 0 & h ( Q ?^, 3 - , & # W4k & % & L & ,,G N OG$ h ' - 4$ 5{hY %%% o-L - i b 9 & sa M 9 %$ % 2 W r#5 % M ki$ $ ? SbY
.. _ . . . . , _ . . . _ . .m . _ _ . . . - . _ _ .._ . ._
3 1 Table 4.1.3.2 Low Leakage Core Loading Flux (E>0.1 MEV)' At Pressure Vessel (cont'd) a 195.760cm 192.062cm 192.062em 192.062cm 188.363cm 8 0T 1/4 T 1/2 T 3/4 T T 35 4.29928E+10 3.633593+10- 2.60734E+10 1.64844E+10 7.54705E+09
'36 4.15235E+10 3.52380E+10 2.53707E+10 1.60876E+10 7.40745E+09 37- 3.98175E+10 3.38989E+10 2.44t50E+10 1.55824E+10 7.23521E+09 38 3.83011E+10 -3.265675+10 2.36356E+10 1.50896E+10 7.06796E+09 39 3.69579E+10 3.15146E+10 2.28361E+10 1.46187E 10 6.90420E+09 40 3.57727E+10 3.04739E+10 2.20894E+10 1.41716E+10 6.74600E+09 41 3.47560E+10 2.95591E+10 2.14233E+10 1.37682E+10 6.60829E+09 42 3.41401E+10 2.90021E+10 2.10144E+10 1.35201E+10 6.52740E+09 43' 3.35318E+10 2.84515E+10 2.06084E+10 1.32718E+10 6.43057E+09 44 3.25757E+10 2.75887E+10 1.99771E+10 1.28889E+10 6.28995E+09 45 3.15486E+10 2.66975E+10 1.93417E+10 1.25076E+10 6.16164E+09 46 3.08280E+10 2.61107E+10 1.89330E+10 1.22649E+10 6.08359E+09 47 3.01550E+10 2.55299E+10 1.85216E+10 1.20206E+10 5.99025E+09 48 2.89910E+10 2.45803E+10 1.78677E+10 1.16368E+10 5.OS211E+09 49 2.76990E+10 2.35556E*10 1.71760E+10 1.12353E+10 5.71654E+09 50 2.66928E+10 2.27626E+10 1.66431E+10 1.09280E+10 5.61674E+09 51 2.59685E+10 2.21913 E+10 1.62585E+10 1.07070E+10 5.54076E+09 52 2.51160E+10 2.15200E+10 1.58102E+10 1.04496E+10 5.44866E+09 53 2.41484E+10 2.07621E+10 1.53063E+10 1.0160BE+10 5.34973E+09 54 2.32216E+10 2.00390E+10 1.48272E+10 9.88800E+09 5.25839E+09 55 2.23494E+10 1.93633E+10 1.43812E+10 9.63410E+09 5.17291E+09 56 2.14467E+10 1.86736E+10 1.39284E+10 9.37780E+09 5.08597E+09 57 2.07062E+10 1.80885E+10 1.35425E+10 9.1587BE+D9 5.01388E+09
;58 2.00750E+10 1.76088E+10 1.32283E+10 8.98124E+09 4.95316E+09 l
59 1.96533E+10 1.72653E+10 1.29992E+10 8.85108E+09 4.91117E+09 l 60 1.93961E+10 1.70632E+10 1.28644E+10 8.77485E+09 4.88541E+09 61 1.92676E+10 1.69621E+10 1.27974E+10 8.73658E+09 4.87254E+09 l
- l. . o 4 ,
' 947+_- -45sv+ 4,i c.- g m - .-
l
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. . . - - . - . _ . . . . . - . . . . . , - - . , - ,, a : . .= = , , . ., , , . , . , _ . _
Table 4.1.3.3 - Low Leakage Core Loading DFA Rates At Pressure vessel
.s 195.760cm 195.760csi 192.062cm 192.062cm 100.363cm 0- 0 T. 1/4 T 1/2 T 3/4 7 T 1.12.304005 11 :1.559553 11- 9.393633 12 :5.403615 12 2.516545 12 2 =2.304225 11- 1.560095 11 9.397905 12 5.407573 12 2.51310E-12 3 2.309595 11 1.565215 11- 9.431293 12 5.42461E 12 2.51469E 32 4 '2.410325 11- 1.00313E 11 9.53091E 12 5.47507E 12 2.531073 12 5 2.46440E 11 1.6117?I 11 9.609453 12 5.55601E 12 2.557775 12 6 -2.575773 11 -1.649735 11 9.901205 12' 5.663175 12- 2.59272E 12 7 2.60725E 11 1.70115E 11 1.010763 11 5.000535-12 2.63917E 12 0 2.71750E 11 1.760993-11 1.056043 11 5.99534E 12 2.690615 12 9- 2.02433E 11 1.033123 11- 1.09096E 11 0.17030E-12 2.75470E 12 10- 2.921485 11 1.093265-11 1.124065 11- 6.33545E 12 2.007465 12 11- 3.03556E 11- 1.96244E 11 1.16153E 11 6.52236E 12' 2.066333 12 12 3.15020E 11 - 2.03159E 11 1.190045-11 6.70611E 12 2.92430E 12 13 3.26076E 11 '2.097563 11 1~.23403E 11 6.07070E-12 2.97020E 12 14- 3.36165E-11 2.15719E 11 1.26551E 11 7.03136E 12 3.02544E 12
-15 3.440175-11: 12.207645 11 1.291663 11 7.155965-12 3.063055 12
.16= 3.5152!I-13 2.24506E 11 1.310465 11 7.243165 12 3.000095 12 17--3.55740E-11 2.266135 1~320175 11' 7.206425 12 3.09935E-12 10" 3.56417E 11 2.26669E-11 1.31923E 11' 7.20019E-12 3.09740E 12 19 '3.536325 11 2.25261E 11 1.31215E 11- 7.24700E 12 3.00063E-12 20- 3.529993-11 2.230675-11 1.30431E 11. 7.21147E-12 3.07454E 12
~ 21 - 3.474745 11 2.201553-11 1.207175-11 7.136983 12 3.04771E-12
-22:-3.407055 11 2.16161E 11' 1.269205-11 7.05717E 12 3.02007E-12
.- 23 3.30276E-11 2.12429E-11 l.255445 11 6.99004E 12- 3.023095-12 24 3.257323-11_ 2.114165 11.1.251333 11 6.900135 12 3.01640E 12
~ 25 ' 3.19110E 111' 2.089023 11 1.24244E 11 -6.940293 12 2.99542E 12 226 3.140205 11' - 2.06107E 11 1.23030E-11 6.00322E 12 2.97302E 12 L27- 3.10954E-11 .2.04160E-11 1.210415-11 6.02410E-12 2.95691E 12
^20 3.11401E 11 2.03227E 11- 1.210333-11. 6.700555-12 2.949005 12.
29 3.12701E 11 2.026025-11 1.20595E-11 6.757195-12 -2.94164E-12 30' 3.16166E-11~ 2.010575 11 1.194093-11 6.691543 12 2.90502E-12 31 ' 3.129603-11-- 1.99466E-11 1.176555 11;,6.50513E 2.064005-12' 32-':3.072755-11 1.96674E 11 1.15910E 11, 6.407945 12 2.032415 12
~
'33sl3 013535-11 l'.93605E-11 l'.14154E 111L6.39306E*12: 2.00057E 12
_34. 2.949635 11LL1.901333 11 1.12250E-11_ 6.29390E-12 2.766015-12' k 4 w 2 : f'* y * h
;(qh @(; .
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3 .< < apg&Mk%@$%@[a # -
< W 'M @ M % d O N N M N TN D N N b.MM*WM
. . ;.. =
- a- w e. :. - - - - - - - -
- -lj 4-l Table 4.1.3.3 Low Leakaga Core Loading i
DPA Rates At Pressure Vessel (cont' d) s 195.760cm 195.760cm 192.062cm 192.062cm 188.363cm 0 0T. 1/4 T 1/2 T 3/4 T T 35 2.8(;,8E-11 1.86300E 11 1.10248E 11 '6.19058E-12 2.73052E 12 { 36 2.787>6E-11 1.00855E 11 1.07342E 11 6.04316E 12 2.67923E 12 37 2.67692E-11 1.74071E-11 1.03619E-11 5.85272E-12 2.61479E 12 38 2.57775E 11 1.67755E*11 1.00023E 11 5.66564E-12 2.55170E 12 39 2.48937E-11 1.61941E 11 9.66302E 12 5.48621E 12 2.48977E-12 40 2.41041E-11 1.566425 11 9.34644E 12 5.31566E 12 2.42983E-12 , 41 2.34184E-11 1.51989E 11 9.06421E-12 5.16162E-12 2.37729E 12-42 2.30022E 11 1.49147E-11 8.89053E-12 5.06666E-12 2.34620E 12 43 2.25905E-11 1.46309E 11 8.717015-12 4.97125E-12 2.30949E 12 44 2.19312E 11 1.41807E 11 8.44480E-12 4.823195 12 2.25563E 12 45 2.12060E 11 1.37072E-11 0.16765E-12 4.67478E 12 2.20575E 12 46 2.06797E 11 1.33889E-11 7.98755E-12 4.5797BE 12 2.17518E 12 47 2.02303E 11 1.30858E-11 7.80901E-12 4.48482E 12 2.13953E-12 , 48 1.94187E 11 1.25806E-11 7.52283E-12 4.33502E 12 2.08621E-12 49 1.85272E 11 1.20384E 11 7.22083E 12 4.17851E 12 2.03375E 12 50- 1.78502E-11 1.16250E 11 6.99004E-12 4.05933E 12 -1.99505E 12 51' 1.73789E-11 1.13316E 11 6.82481E 12 3.97391E-12 1.96598E 11 52 1.68195E 11 1.09859E 11 6.63156E-12 3.87432E 12 1.93071E 12 I 53 1.61920E-11 -1.05979E 11 6.41541E 12 3.76283E-12 1.89281E-12 54 1.55998E-11 1.02315E 11 6.21092E-12 3.65801E-12 1.85783E 12 55 1.50479E 11 9.89088E 12 6.02144E-12 3.56054E-12 1.82520E 12 56 1.44661E-11 9.54003E-12 5.82796E-12 3.46205E-12 1.79201E 12 57 1.40107E-11 9.25079E 12 5.66607E 12 3.37875E 12 1.76468E 12
- 58. 1.36042E 11 9.00690E-12 5.53201E-12 3.31068E 12 1.74160E 12 59 1.33559E-11 8.84186E 12 5.43758E 12 -3. 26174 E- 12 1.72582E-12 60 1.31982E 11 8.74286E 12' 5.38139E-12 3.23297E-12 1.71617E-12 61 1.311925 11 8.69328E-12 5.35346E-12 3.21847E-12 1.71132E 12 4
-~.'
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=-
Table 4.1.3.4 Low Leakage Core Loading Fluz (E>1.0 MEV) At Pressure Vessel Lower Wold (s=67.1040ca) 9' ,0TI 1/4.T 1/2 T 3/4 T .T 6 . Q,, , 1 1 <1.28711E+10. 7.33657E+09 -3.57204E+09 1.65025E+09 6.74094E+08 2 11. 20733 E+10 ' 7.337651-09 3.57271E+09 1.65152E+09 6.73025E+08 3 1.290215+10 7.35922E+09 3.584275+09 . 1.65625E+09 6.73405E+00 4: 1.30611E+10 7.446265+09 3.62421E+09 1.67333E+09 6.79015E+08 5 '1.33103E+10 -7.50671E+09 3.68915E+09 1.?O150E+09 6.082275+08 6 1.36500E+10 7.773093+09 3.77612E+09 1.73086E+0S 7.003985+08 7: 1.41116E+10--0.02708E+09- 3.09380E+09 1.70901E+09 7.167193+08 0 1.47280E+10-.8.36394E+09 4.048695+09 1.85585E+09 7.37781E+0B
- 9 1.53273E+10 9.68363E+09 4.19472E+09 1.91027E+09 -7.57825E+08 10 1.50692E+10 0.98236E+09 4.33252E+09 1.97601E+09 7.76523E+08 11 1.65088E+10 9.32720E+09 4.480895+09 2.04342E+09 7.97593E+08 12 .1.71525E+10 -9.673163+09 4.64562E+09 ' 2.10913E+09 8.18351E+00 13 1.77741E+10 1.00040E+10 4.79375E+09 2.17090E+09 8.37686E+08 14=.l.03422E+10- 1.030365+10 4.92622E+09 2.22545E+09 8.54590E+08
, 15- 1.80307E+10 1.05574E+10 5.03609E+09 2.26953E+09 8.67061E+08 16 1.92103E+10 1.07441E+10 5.112983+09 2.29903E+09 8.76649E+00 li- 1.94409E+10 .1.00444E+10=-5.14820E+09 2.31099E+09 8.79459E+08 18 .1.94705E+10 1.00332E+10' 5.132963+09 2.30303E+09 8.77152E+00 19s - 1.93051E+10 1.07442E+10 5;00997E+09 2.20513E+09 8.72255E+00 ! 20 1.92590E+10 '1.06500E+10' 5.04853E+09 ~ 2.26041E+09 0.66450E+08 21" 1.09210E+10 1.04346E+10 4.957065+09 2.234795+09 0.55582E+08 ' 22 1.05042E+10 1.02055E+10 4.86962E+09 2.202195+09 0.47429E+08
^
; 23, - 1.78667E+10- 9.99265E+09 4.00344E+09 2.17955E+09 0.448175+00
- . .24 1.76017E+10.'9.935095+09 4.78504E+09'-2.17269E+09' 8.42677E+08
-- 2 5 - 1.72228E+10 9.00265E+09 4.744893+09. 2.15797E+09- 8.35460E+08 26 1.69291E+10, 9.65495E+09 4.69180E+09 2.137465+09 8.270295+08 4:
27'=1.67590E+10 9.557365+09 4.64261E+67 '2.11667E+09- 8.221573+00 + 20- 1.67921E+10 '9.52031E+09' 4.611565+09; 2.10197E+09 0.19795E+00 29.-l'.60773E+10 -9.49922E+09 '4.5P482E+09 2.09400E+09 8.17157E+0S
=30< 1.710663+10' 9.47987E+09 4.554595+09.=2.07202E+09- 0.05294E+08
, .311.1.697015+10_-9.39520E+09 -4.49343E+09 12.03950E+09 .7.92311E+08 7.02675E+0B-133 - }L 1~.63604E+1032} 9.15470E+09 1%667763+10'-9.20489E+09' 4.37430E+09- 1.98317E+09- 7.73134E+08 '4.43524E+09-2.0
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4
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}
Table 4.1.3.4 Low Leakage Core Loading
'Fluz (551.0 MEV) At Pressure vessel Lower Weld (cont'd)
(s= 67.1040 cm) 8- 0 T I- 1/4 T - 1/2 7 3/4 T T 34- 1.60247E+10 0.990065+39 - 4.306195+09 1.95330E+09 7.62965E+08
- 35L 1.566673+10 ;8.82449M+99i 4.231515+09 1.92141E+09= 7.510865+00 36 1.513173+10 0.55025E+09 4.11931E+09 1.07454E+09 7.35910E+08
-37, 1.45170E+10 8.23144E+09 3.97345E+09 1.01281k+09 7.15377E+00 38 -1.397265+10 7.92884E+09 3.83226E+09 1.75171E+09 6.95144E+08
- 39. 1.34914E+10 7.65224E+09 3.69963E+09 1.69314E+09- 6.75303s+00
'40- 1.30653E+10 7.40293E+09 3.57704E+09 1.637663+09 6.56161E+00 41 1.26972E+10 -7.19595E+09 3.46860E+09l-1.50776E+09 6.39276E+08 42 1.247395+10. 7.05376E+09 3.40188E+09 -1.55698E+09 6.29244E+08 43 1.22544E+10 6.92036E+09 3.33454E+09 1.52564E+09 6.17486E400 44 1.19015E+10 6.70781E+09 3.227975+09 1.47666E+09 6.00044E+00 45 1.15061E+10 6.40000E+09 3.11782E+09 1.42694E+09 5.83502E+08 46 . 1.12144E+10 .6.32593E+09 3.04490E+09 1.39468E+09 5.73252E+08 47 1.09733E+10 -6.18010E+09 2.97365E+09 1.36264E+09 5.61582E+00 40- 1;05283E+10' 5.93354E+09- 2.85770E+09 1.31152E+09 5.43856E+C8
-.49- 1.00330E+10 5.66771E+09 -2.73480E+09 1.25790E+09- 5.26263E+08 50 ' 9.65500E+09 5.46464E+09 2.64103E+09 1.21723E+09 5.13194E+08 51 9.39684E+09 5.32206E+09 2.57433E+09 - 1.18023E+09 5.03501E+00 52 9.09020E+09-_5.15364E+09 2.49619E+09 1.15423E+09 4.91741E+08 53 T8.74234E+09 i 4.963985+09' 2.408493+09. 1.11618E+09 4.79030E+0B 54 0.412765+09 4.78431E+09 -2.32563E+09. 1.00047E+09 -4.67267E+00 55 0.10445E+09 4.61705E+09 2.24069E+09 1.04721E+09 4.56317E+08
-7.77782E+09 4.443495+09 2.16963E+09 1.01341E+09 4.45120E+0S
'57- 7.52341E+09 4.30203E+09 2.10431E+09 9.85220E+D8 4.35908E+08 58 7.294795+09 4.18120E+09-:.2.04940E+09 9.610385+00 4.28201E+00.
59 - 7.15689E+09 4.101665+09 -2.01203E+09 -O'.4 5 53 0E+00. ,4. 229 02E+0 8
'60 17.06918E+09' 4.05350E+09 -1.90953E+09 9.35064E+00 4.19773E+00
- . 61 .7;025163+09 4.02940E+09- 1.97935E+09 9.309875+08 4.18169E+00
-' '3 c-5 %
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~ -.7g - ;y=;.anwa .w.7 .y.; w ,x a x _ a ; = ;;; = e w.7; m w.. = ,.
~ - .-
j I b Table 4.1.3.5 ' Low Leakage Core Loading Flux (Er 0.1MIV) At Pressure Vessel Lower Weld (s=67.1040ca) 0 0T 1/4 7 1/2 T 3/4 T T 1 2.93710E+10 2.51101E+10 1;02041E+101 l'.175093+10 5.50424E+09 2: 2.930995+10 2.51373E+10,'1.02970E+10--1.17600E+10 -5.57663E+09 3- 2.94905E+10n 2.52419E+10 1.03700E+10- 1.179905410 5.50032E+09 - 4 2.90514E+10 2.553173+10 1~. 0 56165+10 1.190665+10 5.61423E+09 5l _ 3.04322E+10 2.59004EQ0 1.00620E+10 1.20755E+10 5.66936E+09 6 3.12002E+10. 2.65902E+10 1.92649E+10 1,22997E+10 5.74110E+09-3.22544E+10 2.74279E+10 1.90110E+10_ 1.26035E+10 5.03637E+09 ' 0' 3.36423E+10 2.05000E+10 2.051475+10---1.299175+1R 5.95759E+09 9 = 3.49007E+10. 2.95244E+10 2.11713E+10 .1.33530E+10- 6.07104E+09 10 3.623295+10 3.04924E+10 2.17983E+10 1.36975E+10 6.17947E+09-11 3.76051E+10 3.15970E+10 2.25063E+10 1.40054E+10 6.29929E+09 12 3.91407E+10 3.27020E+10 2.32095E+10 1.44666E+10 6.41746E+09
- 13. 4.05611E+10 3.37540E+10' 2.30727E+10' 1.40245E+10 6.52740E+09 14 4.19560E+10 3.47002E+10 2.44670E+10 1.51424E+10--6.62407E+09 15 4.29712E+10 3.55171E+10 2.49631E+10 l'. 54 03 4 E +10 6 70202E+09 16 4.30410E+10 3.61253E+10 2.53270E+10 1.55913E+10 6.75704E+09 17 4.44090E+10. 3.64937E+10 .2.55359E+10 1.56947E+10 6.78203E+09-10 . .4.45072E+10. 3.65019E+10~ 2.55670E+10 1.57043E+10 6.70575E+09 19 4.44242E+10 ~ 3.64792E+10 2.54950E+10 1.566293+10 6.77550E+09
=20 4.43473E+10 3.63153E+10 2.53001E+10 1.560000+10 6.750173+09 21 74.39971E+10 3.59323E+10 2.514495+10 1.54755E+10 6.701785+09
-22 :4.35074E+10- 3.54652E+10 2.'4064 0 E+10 1.53265E+10 6.66630E+09 23 4.20330E+10: 3.50631E+10 ,2.46453E+10= 1.52116E+10 6.65040E+09' 24 4.25705E+10. 3.49313E+10 2.45704E+10 1.51725E+1D 6.64461E+09 l
i
~"
25 4.21924E+10 3.46559E+10 2.44171E+10' 1.50912E+10 6.60072E+09
'26 4.17102E+10 3.42071E+10 2.4199 5E+10 .1.49729E+10 6.55390E+09
- 27 4.11989E+10 - . 3.39300E+10 2.39766E+10 1.405065+10 6.52110E+09 20 4.00515E+10 3.37023E+10' 2.30121E+10_'1.47575E+10 6.50656E+09
-29: 4.07304E+10 3.35011E+10 .2.372575+10 1.47077E+10 6.40947E+09 30.14.04793E+10 3.32602E+10 2.34059E+10 1.45694E+10 6.41396E+09 31 -3.95703E+10 3.264275+10 -2.30633E+10: 1.43265E+10 6.32220E+09' 32 3.06091E+10 3.20360E+10 2.266563+10 1.41004E+10- 6.25174E+09~
>33f;3.773275+10 ;3;14371E+10_- 2.227093+10 l.30014E+107 6.10010E+09 l y -l3,0 j 3 604193+10 3 3.00050E+10 -'2.19700E+10 1.36565E+10:'6.10490E+09-1:
l s i 4 7 .I
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l Table 4.1.3.5 Low Leakage Core Loading Flux (E> 0.1MEV) At Pressure Vessel Lower "Aeld (cont'd) (s= 67.1048 ca) 0 0T 1/4 T 1/2 T 3/4 T T
'35- 3.59489E+10 3.01531E+10 :2.14655E+10 f1.34261E+10 6.02487E+09
;36.'3.47201E+109 2.92419E+10 2.088593+10, 1.310285+10 5.91316E+09 i
.37 3.32933E+10--2.81305E+10" 2.01575E+10 1.26911E+10 5.77532E+09
'38- 3.20252E+10 2.70996E+10 1.94580E+10 1.22894E+10 5.64145E+09 39 3.09021E+10 -2.615175+10 1.87997E+10 1.19057E+10 5.51038E+09 40- 2.99111E+10 2.52881E+10 1.81849E+10 1.15413E+10 5.38378E+09 41 2.90611E+10 2.45290E+10 1.76364E+10 1.12126E+10 5.27356E+09 42 2.85462E+10 2.406695+10- 1.72997E+10 1.10104E+10 5.20081E+09 43 2.803765+10 2.36099E+10 1.69655E+10 1.00081E+10 5.13132E+09 44 2.72383E+10 2.28939E+10 1.64456E+10 1.04960E+10 5.01877E+09 45 2.63794E+10 2.21542E+10. 1.59223E+10 1.01852E+10 4.91604E+09 46 2.57768E+10 2.16671E+10 - 1.55856E+10 .9.98731E+09 4.85354E+09 47 2.52141E+10 2.11851E+10 1.524683+10 9.78816E+09 4.77883E+09 48 2.42407E+10 2.03968E+10 1.47082E+10 9.47526E+09 4.66822E+09 49__ 2.31608E+10 1.95461E+10 1.41384E+10 9.14794E+C9 4.55968E+09 50 2.23185E+10 .1.888783+10 -1.36995E+10 8.89740E+09 4.47975E+09 51 2.17128E+10 : 1.841365+10 1.338283+10 8.71725E+09- 4.41892E+09 52--2.099995+10 1.78564E+10= 1.30134E+10 S.50741E+09 4.34517E+09
'53.-2.019065+10 1.72273E+10 1.25984E+10 8.27198E+09 4.26595E+09 54 1.94156E+10 1.66270E+10 1.22037E+10 8.0495BE+09 4.19281E+09
'55 1.06861E+10 1.60662E+10 -1.18364E+10 7.84258E+09 4'.12436E+09 56 .1.79310E+10 1.54936E+10'.1.14634E+10 7.63362E+09 4.05474E+09 57 -1.73116E+10 1.500795+10 l'.11455E+10 7.45507E+09 -3.99701E+09 58 -1.67035E+10 1.46097E+10 1.088605+10 7.31032E+09' 3.94830E+03
- 59. 1.643095+10 1.43246E+10 1.06900E+10 7.20422E+09 3.91477E+09
'60~ 1;62159E+10 1.41568E+10 ' 1.05871E+10 7.14200E+09 3.89414E+09 61 1.61084E+10 1.40729E+10 1.053183+10 7.110885+09 3.88383E+09 i
i i
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2
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r h Tabla 4.1.3.S Low Lestage Core Loading
- bFA Estes At Pressure vessel Lower Weld (s = 67.104 0 ca) 0 0T 1/4 T 1/2 T 3/4 T T
-1' 1.995323-11 1.298235 11- 7.764015 12 4.420093 12 2.01856E 12 2 1.99544E 11 1.29867E 11 7.76039E-12' 4.42412E 12 2.01579E 12 '
-4 1.999955 11 1.30293E 11 7.79590E 12 4.43806E 12 2.01706E-12 3
5-2.02400E 11 1.31786E-11 7.87029E 12 4.47940E 12 2.030283 32 , 6-2.06267E 11 -1.341653-11 0.00945E 12 4.54573E 12 2.05181E 12 2.11399E 11 1.37332E 11 8.18464E 12 4.63356E 12 2.00002E 12 7 2.182235 11 1.416153 11 8.421595 12 4.75270E 12 2.11750E 12 ,
, v' O - 2.27456E-11 1.47266E 11 .8.73003E 12 4.90502E-12 2.16547E 12 9 2.36404E 11 1.52608E-11 9.019033 12 5.04925E 12 2.21001E 12 10 2.44541E 11 1.57617E 11 9.292065 12 5.10462E 12 2.253323 12
- 11. 2.54095E-11 -1.63380E 11 9.60200E 12 5.33784E 12 2.30084E 12 12 2.637043-11 1.69140E 11 9.91163E 12 5.48848E-12 2.34764E-12 13 2.72959E 11 1.74635E-11 1.02028E 11 5.629973 12 2.39114E 12 14 2.81410E 11 1.79603E 11 1.046333 11 5.75511E-12 2.42927E-12 15 2.88659E 11 1.83806E-11 -1.06797E 11 5.85723I 12 2.45961E 12 16 2.94278E-11 1.86923E 11 1.083525 11 5.92066E 12 2.480453 12 17 2.97010E 11. 1.00670E 11 1.09155E-11 5.96402E 12 2.48089E-12 18 19 :- 2.98379E 11 1.887221 11 1.09075E 11 5.95873E 12 2.48722E 12 2.96049E-11 1.87547E 11 1.00405E 11 5.93199E 12 2.48005E 12 20- 2.95517E 11 1.86303E 11- 1.07035E-11 5.90210E 12 2.46866d 12 21' 2.90092E 11 1.83286E 11 1.06412E 11 5.84082E 12 2.44696E-12 22 2.852063 1.79954E 11 1.049223 11 5.7752EE-12 2.43106E 12 '
23' 2.76439E-11 1.76041E 11 1.03702E 11 5.72741E 12 2.42701E 12. 24 2.72680E-11 1.75997E 11. 1.034415 11' 5.71207E-12 2.42169E-12 725~ 2'67157E 11 1.739675 111 .1.02706E 11 fr.67940E-12 2.40471E 12 26 2.62825E 11 1.71638E 11 1.01701E 11 5.63261E 12 2.30665E-12 27 2.603195-11 1.69950E 11 1.00717E-11 5.58416E 12 2.37366E 12 28 2.60687E-11 1.69174E-11 1.000493-11 '5.54040E 12 2.36793E 12 29- 2.61771E-11 1.60722E 11 9.960675 12 5.52934E-12 2.36137E 12 30 2.64664E 11 1.60037E-11 9.87730E-12' 5.475573 12 2.332493 12
-31'12.61978E 11 1.66050E 11 9.726675-12. 5.30851E 2.29889E 12'
,32. : 2.57217E 11 1;63729E 11 9.58245E 12 5.30903E-12 .2.27341E-12
- 7 33
~ 2.522595 110- 1~.61176E 11' 9.43677E-12T 5.23144E 12 ?2.24700E-12'
, 0 ' e, ' '
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Table 4.1.3.6 Low Leakage Core Loading DPA Rates At Pressure Vessel Lower Weld (cont'd) (s=67.1040ca) 0 0T 1/4 T 1/2 T 3/4 T T 34 2.46900E 11 1.58286E 11 9.28015E-12 5.150313 12 2.22065E 12
,35
2.414P95 11 1.55153E 11' 9.11402E 12 5.06576E 12 2.19144E 12 36 2.333675 11 1.50562E 11 0.07380E 12 4.94508E 12 2.15014E-12 37 2.24060E 11 1.44913E 11 8.56597E 12 4.78915E-12 2.09024E-12 30 2.15764E 11 1.39654E 11 0.26850E-12 4.63594E 12 2.04741E 12 39 2.08365E 11 1.34813E 11 7.98004E 12 4.48900E-12 1.99753E-12 40 2.01756E-11 1.30402E 11 7.72628E 12 4.34933E 12 1.94924E 12 41 1.96017E 11 1.26520E-11' 7.49295E-12 4.22319E 12 1.90690E 12 42 1.92534E 11 1.24163E 11 7.34935E 12 4.145425 12 1.88185E 12 43 1.89008E-11 1.21800E 11 7.20558E-12 4.06728E 12 1.852275-12 44 1.83572E 11 1.100535-11 6.98077E 12 3.946005 12 1.80887E-12 45 1.77502E 11 1.141105-11 6.75156E 12 3.82442E 12 1.768661-12 46 - 1.73090E 11 1.11460E-11 6.60257E-12 3.74650E 12 1.74401E 12 47 1.69336E 11 1.08936E-11 6.45491E-12 3.66878E 12 1.71527E-12 48 1.62543E 11 1.04729E 11 6.218153 12 3.54604E-12 1.67229E-12 49 1.55079E 11 1.002135 11 5.968353 12 3.41780E-12 1.63000E-12 50 - 1.49410E-11 9.677035 12 5.777445 12 3.32015E 12 1.59879E 12 51 .1.45464E 11 9.432705 12 5.64077E-12 3.25017E-12 1.57536E-12 52 1.40780E 11' 9.14481E-12 5.48092E-12 3.16857E 12 1.54694E 12 53 1.35525E-11 8.82172E 12 5.30212E 12 3.07722E 12 1.51630E 12 54 1.30564E-11 0.51653E 12 5.13298E 12 2.99135E 12 1.4 8818E 12 55 - 1.25941E 11 0.23284E 12 4.97624E 12 2.91150E 12 1.46180E 12 56 1.21068E-11 7.940605-12 4.81620E 12 2.83000E 22 1.43513E-12 57 1.17252E-11 7.699703-12 4.68229E-12 2.76256E-12 1.41310E 12
-50 1.138463 11. 7.496555 12 4.57139E 12 2.70670E 12 1.39450E 12 59 ' 1.11765E-11 7.35909E 12 4.49330E-12 2.66670E 12 1.38178E 12 60: 1.10445E 11 7.27G65E 12 4.44683E 12' 2.64313E 12 1.37400E-12 C1:~1.09782E-11 7.23535E-12 4.42372E 12 2.631265 12 1.37010E 12
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i Table 4.1.3.7 Low Leakage Core Loading Downcomer Fluzes and DPA Rates (r=210.50cm,s=195.76ca) FLUX FLUI DPA/s 8 (E>1.0 MEV) (E>0.1 NEV) 1 3.19651E+10 5.60212E+10 4.83206E 11 2 3.10411E+10 5.60045E+10 4.029453 11 3 3.18950E+10 5.61790E+10 4.83900E-11 4 3.23444E+10 5.70009E+10 4.9064#.I 11 5 3.30580E+10 5.83302E+10 5.01300E 11 6- 3.40324E+10 6.01477E+10 5.16032E 11 7 -3.532723410 6.26006E+10 5.35612E-11 8 '3.71271E+10 6.60010E+10 5.62794E-11 9 3.89175E+10 6.93465E+10 5.89651E 11 10 4.05292E+10 7.24619E+10 6.14050E 11 11 4.24824E+10 7.62165E+10 6.435723-11 12 4.44983E+10 E.01112E+10 6.740515 11
.13 4.64001E+10 8.39766E+10 7.04070E-11 14 4.83429E+10 8.76671E+10 7.32390E-11 15 4.99792E+10 9.09645E+10 7.57330E-11 16 5.12922E+10 9.37011E+10 7.77541E 11 17 5.21975E+10 9.57035E+10 - 7.91657E 11 18 5.24664E+10 9.66256E+10 7.964175-11 19- 5.19313E+10 9.62961E+10 7.89526E-11 20 5.19369E+10 9.63712E+10 7.89530k-11
~21 5.06161E+10 .9.489065+10 7.71096E-11 22 4'.93955E+10 9.330775+10 7.53354E 11 23 4.76592E+10 9.11678E+10 7.28551E-11 24 4.74112E+10 9.07090E+10 7.25207E 11
-25' 4.65370E+10 8.94933E+10- 7.122105-11
-26 4.55225E+10 8.78947E+10 6.97135E 11 27- 4.483C5E+10 8.64330E+10 6.86578E 11
'28 4.45762E+10 8.55402E+10 6.825175 11
, 29- 4.43745E+10- 8.50526E+10l - 6.79163E '
30' 4;43231E+10- it:399373+10 M; 6.77442E - 1 . g- a a & k- , A v - + as a 4 a y i I iQ,.. .Mi k 8[ 4 v - j ,~ YF .', $
' j '\ i .A;ukhh4[> :l si -
i i - " c -L ~ G &~-d b i <x - w n M?"k % i; fed +A +k& 'NM ga s + - y47 %%es&gshscs%gew&ws . fnw%%$rM w w
I Figure 4.1.3.7 Low Leakage Core Loading i Downcomer Fluxes and DPA Rates (cont' d) (r=210.50cm.s=1W5.76ca) FLUX FLUX DPA/s 8 (E>1.0 MEV) (E>0.1 MIV) 31 4.37137E+10 0.165085+10 6.66917E+11 32 4.29418E+10 7.93698E+10 6.54131E 11 33 4.206185+10 7.71129E+10 6.39939E 11 34 4.10899E+10 7.48318E+10 6.24558E 11 35 4.00509E+10 7.25322E+10 6.08455E 11 36 3.84513E+10 6.92870E+10 5.84054E 11 37 3.67752E+10 6.59132E+10 5.58178E-11 38 3.53559E+10 6.31654E+10 5.36466E-11 39 3.41932E+10 6.10148E+10 5.18752E 11 40 3.32277E+10 5.93237E+10 5.04129E-11 41 3.24444E+10 5.80441E+10 4.92320E 11 42 3.20013E+10 5.73483E+10 4.85610E 11 43 3.15354E+10' 5.66412E+10 4.787683 11 44 3.00166E+10' 5.55360E+10 4.68020E 11 45 2.99768E+10 5.42423E+10 4.55506E-11 46 2.92380E+10 5.313 63 E+10 4.44744E-11 47 2.87002E+10 5.22066E+10 4.36479E 11 48 2.75257E+10 5.02271E+10 4.18811E 11 49 2.61091E+10 4.77301E+10 3.97461E 11 50 2.49621E+10 4.56059E+10 3.00329E 11 51 2.42073E+10 ' 4. 413 43 E+10 3.68774E 11 52 2.32986E+10 4.23330E+10 3.54820E-11 53 2.22364E+10 4.02029E+10 3.386165-11 54 2.12117E+10 3.81266E+10 3.22988E 11 55 2.02471E+10 3.61638E+10 3.08309E 11 56 1.92168E+10 3.40970E+10 2.92691E-11 57 1.84344E+10 3.24515E+10 2.00702E 11 58 1.77035E+10 3.10056E+10 2.69749E 11 59 1.72778E+10 3.00773E+10 2.63223E 11 60 1.69920E+10 2.94950E+10 2.588825-11 61 1.68483E+10 2.92019E+10 2.56643E-11 f 4 9
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a i Table 4.1.3.8 '
- Low Leakage Core Loading Cavity Fluzes and DPA Eates (r=320,06cm,s=184.66Sca)
FLUI FLUE DPA/s 0' (E>1. O _ SERV); (E>0.1 SERV) - 1 5.37593E+00 4.610265+09 1.66455E 12 2 5.37704E+00 4.61094E+09 1.66479E 12 3 5.360015+00 4.607065+09 1.663073 12
.4 5.36931E+08 4.605963+09 1.66284E 12 5 5.370565+08 4.604495+09 1.662585 12-6 5.37306E+08 4.602985+09- 1.662425 12
-7 5.37364E+08 -4.59961E+09 1.66163E 12 0 5.30072E+00 4.59022E+09 1.661095 12 9 5.38778E+00 4.59740E+09- 1.66230E 12
-- 10 5.30455E+08 4.592365+09 1.66072E 12
-11 5.30037E+08 '4.58633E+09 1.650015 12
- 12 5.373775+00 4.57974E+09 1.656515 12 13 5.36326E+00- 4.57193E+09 1.653523-12 14 ~ 5.340585+08 4.56272E+09 1.649795 12 15 5.33004E+08- 4.55177E+09 1.64526E 12 16 5.30911E+08 4.53875E+09 1.64005E 12 17 5.28670E+00 4.52323E+09- 1.634155 12 18 5.25545E+00 4.50604E+09 1.620243 12 19 5.247265+00 '4.493275+09 1.62335E 12 20- 5.24433E+08 4.40750E+09 1.62166E 12 21 5.22500E+08 4.47190E+09 1.616143 12
- 22 5.211895+08 4.46080E+09 1.612233 12
'23T ~ 5.20004E+08 4.45244E+09 1.609175-12 '
24' 5.199895+00 4.45110E+09 1.60075E 12 25- 5.19622E+00 4.44759E+09 1.607555 12-26_ 5.19784E+08 4.44132E+09 1.60522E-12 27 5.17376E+00 4.432613409 1.601785-12 20 5.16059E+00 4.42505E+09' 1.59870E-12
' 29. ' 5.15304E+00 4.42091E+09 1.59699E-12_
30 : 5.13781E+08- 4.41222E+09~ . 1.5p3423-12
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. Figure 4.1.3.8 Low Leakage Core Loading Cavity Fluzes and DPA Rates (cont'd)
(r=3 2 0. 0 6 cm, s =104. 6 6 5 cm) FLUE FLUX DPA/s 0, (E>1.0 MIV) (E>0.1 NEV) 31 5.11393N+00 4.39020E+09 1.507723 12 32 5.093105,00- 4.306295+09- 1.502025 12 33 5.06999E+00- 4.37300E+09 1.57756E 12 34 5.04530E+00 4.36056E+09 1.57199E 12 35 5.01353E+00 4.34372E+09 1.56400E 12 36 4.96574E+00 4.31030E+09 1.55422E 12 37 4.90774E+00 4.20456E+09 1.54063E 12 30 4.05004E+00 4.24941E+09 1.52601E 12 39 4.79160E+00 4.21363E+09 1.51279E 12 40 4.73001E+00 4.17713E+09 1.49033E-12 41 4.67506E+00 4.14400E+09 1.40540E 12 42 4.643093+00 4.12560E+09- 1.47772E 12 43 4.60506E+00 4.10416E+09 1.46899E 12 44 4.54669E+00 4.07103E+09 1.45554E 12 45 4.49120E+00 4.039175+09 1.442665 12 46 4.459073+00 4.02030E+09 1.435153 12 47 4.42390E+00 4.00035E+09 1.42702E 12 40 4.371173+00 3.96979E+09 1.41473E 12 49 4.310295+00 3.93070E+09 1.40230E 12 50 4.20690E+00 3.91921E+(9 1.39469E-12 51 4.26250E+00 3.90450E+09 1.30009E 12 52 4.23627E+00 3.009375+09 1.30276E 12 53 4.20722E+00 3.07197E+09 1.37584E 12 54 4.17937E+00 3.05523E+09 1.36920$*12 55 4.15400E+00 3.040675+09 1.363?93 12
- 56 4.12520E+00 3.02357E+09 1.35640E 12 57 4.10654E+00 ~3.01214E+09 1.3519OE-12 50 4.00426E+00 3.79940E+09 1.346055-12 59 4.07563E+00 3.79392E+09 1.34469E-12 60- 4.06010E+00 3.70941E+09 1.34290E-12 61 4.06494E+00 '3.70753E+09 1.342155 12
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.i Table 4.1.3.9 Low Leakage Core Loading Flux Spectrum At Pressure Vessel (Pressure Vessel Capsula In) 8 =15. 5 * =195.760cm Group 0T 1/4 T 1/2 T 3/4 T T 1
8.95971E+06 4.04639E+06 1.71127E+06. 7.204465+05 3.13552E+05 2 2.66720E+07 1.18582E+07 4.91037E+06 2.01695E+06 8.52613E+05 3 4 1.06687E+08 4.748775+07 1.94349E+07 7.83696E+06 3.25155E+06 2.04944E+00 9.15840E+07 3.70330E+07 1.46790E+07 5.97526E+06 5 3.49216E+00 1.53135E+08 5.99373E+07 2.29414E+07 8.98942E+06 6 8.99565E+00 3.70206E+00 1.40533E+08 5.11175E+07 1.89706E+07
'7 1.30087E+09 5.379983+0S= 1.96720E+08 -7.05024E+071 2.54068E+07 8
2.31851E+09 9.50891E+08 3.52000E+08 1.27042E+08 4.49000E+07 9 1.614475+09 6.90629E+0S 2.67952E+00 1.00362E+08 3.54585E+07 10 1.17790E+09 5.35940E+00 2.10237E+08 7.98665E+07 2.82120E+07 11 1.33508E+09 6.31525E+08 2.54021E+08 9.82945E+07 3 . 4523 8 E + 0,7 12 6.60471E+0B 3.16891E+08 1.20904E+08 5.03147E+07 1.77265E+07 13 1.70214E+08 8.61210E+07 3.64668E+07 1.47036E+07 5.49417E+06 14 8.37224E+0B 4.31467E+08 1.05441E+08 7.57869E+07 2.81014E+07 15 2.14839E+09 1.17028E+09 5.21746E+00 2.18524E+08 7.91228E+07 16 2.23472E+09- 1.34924E+09 6.52857E+08 2.91964E+08 1.10470E+08 17 3.09285E+09 1.98870E+09 1.01350E+09 4.72548E+08 1.03599E+08 18 4.69342E+09 3.57421E+09 2.09348E+09 1.06842E+09 4.42641E+08 19 2.99026E+09 2.53073E+09 1.65250E+09 9.48778E+08 4.25846E+08 20 1.53302E+09 1.18983E+09 7.511463+0B 4.19502E+08 1.77012E+08
'21 4.26216E+09 4.35878E+09 3.25634E+09 2.04435E+09 9.14851E+00 22 3.42242E+09 3.51560E+0S 2.74099E+09 1.78949E+09 8.22432E+08
~23 3.79426E+09 3.96428E+09 3.14348E+09 2.02927E+09 8.28609E+08 24 3.86580E+09 4.72220E+09 4.14134E+09 2.87263E+09 1.27340E+09 25 4.76833E+09 4.90140E+09 4.06939E+09 2.78572E+09 1.30129E+09 26 4.61586E+09 5.13492E+09 4.488695+09 3.17051E+09 1.47962E+09 27 3.205775+09 3.26790E+09 2.01039E+09 1.97630E+09 9.16890E+08 28 2.51505E+09 2.37374E+09 1.97864E+09 1. 3 68,2 O E+ 09 6.19772E+08 29 8.79362E+00 6.30401E+00 5.10448E+00 3.50385E+08 1.67033E+08 30 4.34403E+08 2.17634E+00 1.72010E+08 1.18340E+08 6.84491E+07 31 1.10068E+09 1.20020E+09 1.06011E+09 7.89183E+00 4.46329E+08 32 6.44102E+08 6.86094E+08 6.16769E+00 4.69131E+08 2.67381E+08 33 1.26761E+09 1.10466E+09 9.10021E+0B 6.73229E+08 3.92060E+08 34 2.22481E+09 1.27925E+09 8.82025E+08 6.13543E+00 3.82035E+08 35 2.77412E+09 1.93564E+09 1.30094E+09 8.51121E+08 4.43179E+08 36 2.48875E+09 1.51446E+09 9.71059E+08 6.10536E+08 3.29150E+08 37 .4.06557E+09 2.34878E+09 -1.402383+09 0.44043E+08 4.70063E+08 30 ;2.247283+09 1.03870E+09 5.83287E+09. 3.45706E+08;:2.15568E+08-P 39c 12.46853E+09 1.25322E+09 ; 6.65027E+08 ' l 3.00715E+08 2.26521E+00 40 -3.19962E+09 1.54584E+09 .7.79807E+0S 7 4.28626E+08 - ( 2.63301E+00 41 .'4.02753E+09 -1'.93545E+09 9.354863+08 4.90924E+082.99183E+08-42 2.32885E+09 1.04054E+09 4.03561E+08 7.2.47461E+08 1. 57 8 9 3 E+ 3 8..
3.12152E+09 '1.26120E+09 '5.42939E+08 '2.60401E+00~:14881775+08 44 2.35583E+09 -8.46985E+08- 3.31096E+08 .1.58293E+08ill'.27369E+0B-45 -2.01571E+09' 4.01121E+08 1.15435E+00':5.462275+071+0:94442E+07-
>1- w 46i 4.36504E+09- 5.20484E+08 7.91024E+07/ f 3.86040E+07 ' '1.69931E+08 4
- 47. 2.040363+10- 6.29138E+08 1.87944E+07-- l'.41357E+07. 3.79490E+00' 1
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Table 4.1.3.10 Low Leakage Core Loading Flux Spectrum At Capsule Location Group Thermal Shield Pressure Vessel Cavity
'. 1 2.86233E+07 1.00290E+07 1.80102E+05 2 9.25192E+07 3.28134E+07 5.00176E+05 3 4.21285E+08 1.34860E+08 1.85392E+06 4 8.72079E+00 2.625673+08 3.32626E+06 5 1.63932E+09 4.54603E+00 4.08952E+06 6 4.357565+09 1.169975+09 1.01250E+07 7 7.05957E+09 1.72212E+09 1.35494E+07 8 1.48779E+10 3.1423rt+09 2.37664E+07 9 1.22241E+10' '2.22680E+09 1.85033E+07 '
10 9.33050t+09 1.61970E+09 1.47019E+07 11 1.08100E+10 1.81467E+09 1.01245E+07 12 5.30090E+09 8.92312E+00 9.29061E+06 13 1.41170s+09 2.32396E+08 2.88943E+06 14 7.120173+09 1.13812E+09 1.42535E+07 15 1.9002O5+10 2.84974E+09 3.87701E+09 16 2.11101E+10 2.80950E+09 5.41140E+07 17 3.12948E+10 3.96978E+09 9.25220E+07 18 5.22985E+10 5.56405E+09 2.16581E+00 19 3.37349E+10 3.36514E+09 2.09905E+08 20 1.81129E+10 1.07476E+09 1.04103E+08 21 4.35261E+10 4.00287E+09 4.40184E+08 22 3.569775+10 3.34595E+09 4.27577E+08 23 3.93046E+10 3.75960E+09 4.'38445E+0B 24 3.33019E+10 3.059575+09 6.33305E*05 25 4.99846E+10 4.97060E+09 8.118485+08 26 4.53695E+10 4.41779E+09 8.63564E 05 27 3.56713E+10 3.546965+09 5.67060E+08 28 2.94159E+10 2.98244E+09 4.08944E+08 29 1.17175E+10 1.25426t+09 1.27929E+08 30 7.67403E+09 8.67024E+08 5.93436E+07 31 7.414263+09 6.95390E+08 2.06075E+0E 32 5.92500E+09 5.63288E+08 1.38458E+08 33 1.430093+10 1.50100E+09 2.05779E+0B 34 3.02036E+10 3.44303E+09 3.18109E,08 35 3.55670E+10 3.80496E+09 3.25683E+08 36 3.42967E+10 3.69890E+09 2.60552E+0S 37 5.33232E+10 5.04162E+09 3.88550E+0B 38 3.11189E+10 3.51722E+09 - 1.85291E+08 39 3.20001E+10 -3.59640E+09- 1. 913 9 0 E+ 08 40 4.26472E+10 4.81535E+09 2.26942E+08 41 5.23847E*10 6.02390E+09 2.58066E+0B 42 3.05480E+10 3.58744E+09 1.39480E*00 43 3.99628E+10 4.88106E+09 1.72279E+08
~44 2.950783+10' 3.75736E+09 1.21621E+08=
'45 ,2.76915E+10 3.74894E+09 1.00072E+08 46- 5.053095+10 0.83175E+09 2.09488E+08 47 1.50116E+11 4.41768E+10 5.40801E+08 Thermal Shield Capsule flum spectrum is at r=202.25cs, s 195.76ca. 8 20' Pressure Vessel Capsule flux spectrum is at r=215.43ca. =195.76es.'8 20*.
-Cavity Capsula flux spectrum is at r=320.06en, s=184.665am, 8=9.5*
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$bhi$hhhhWO-O%o > i P. ' * *
^ *Oi*Y"W + YWYkYYkYW$$h$tV
Table 4.1.3.11 Low Leakage Core Leading Effect of Selected Cross Sections on the Calculated Reaction Rates Axial Peak Reaction Rate (reactions /sec* atom) o Thermal shield capsule (r=202.25ca,s=195.76ca,t=20 ) Detector .
. SAILOR .
,. Material BUGLE 93
. . INDF/B.IV . ORNL/'m.1147
. 27 '. . 16 . 16 .
6 .......
.Al (n,o0 - 2.34084x10 .
. 2.43356x10 .
32 . 14 . 14
.8 (n,p) . 1.35902x10 . 1.40130x10 4
. 46 . 15 . 15
.Ti (n,p) . 2.71072Z10 . 2.62811x10
. 54 . 14 . 14 14
.Fe (n,p) . 1.72762X10 1.74803x10
. 1.71228x10
. 56 . 16 . 16 .
.Fe -(n.p) 3.04757x10 .
. 3.29786x10 .
. 50 . 14 . 14 14
.Mi (n,p) . 2.33009x10 2.32339x10 2.27883x1
................................................................. 0 63 ........
. . 16- . 16
.Cu (n,eO 1.48520x10
. 1.17917x10 .
65 .
. 16 . 16
.Cu (n,2a) 1.53266x10 .. .
. 1.80725x10 ,
. 115 . 14 . 14 .
.In (n n') . 4.68765110 . 4.56521x10 .
. - 237 . 13 -. 13 13
.Mp (n, f) 4.75353x10
.- 5.00191x10 . 4.94987x
. 238- . 14 . 14 10 .........
.U 14
, (n. f) -. 7.60617x10 . 7.51544x10
.. 7.647
.........~................................................... 51x10 BUOLE93 used pressure vessel 1/4T weighting spectrum -to collapse cross
, .9. , . sections .
1 AMW'used^ flat weighting spectrum to collapse cross sections.
#gw- 4 cw yL
,2 i WyC&, ,w, 4 yAs e -
A- 4
? t.1 M d tt= G ivn m -t: WMdhikM@$'
=
; .Nf_RW % P 5' 1 f '-
g M;*- Qr+. Q. mp-y Q h y % : 9p y r -t , - i%MW 19% hi! a NNhN 1M N ~ 3
.. . . . m . _._- n-r. m. ..m...-- .a . - , .. .-,c.7- - - - - -
. - ~
?
Table 4.1.3.12 Low Leakage Core Loading Effect of Selected Cross Sections on the Calculated Reaction Rates Axial Peak Reaction Rate (reactions /sec*ston) o Pressure Vessel Capsula (r=215.43ca,s=195.76ca
...............................................,.D.20
. Detector .
)
SAILOR
.. Material
. BUGLE 93 . ENDF
........................................../B.IV
. 27- .
17
. ORNL/TM.11476
.Al (n af) 17 .
. 6.90977X10 . 7.17096x10 l
32 . 15
.S (n.p) .
15 .
. 2.87891x10 . 2.94648x10
. 46 . 16 16
.Ti (n p) . 6.89007x10
. 6,69567x10
. 54 .
15 15
.Fe (n.p) . 3.74169X10
. 15 .
. 3.87673x10 3.70166x10 56 .
17 .....................
.Fe (n,p) .
-17 .
. 0.59219x10 . 9.26725x10
. 58 .. 15 15
.Ni (n,p) 4.89663x10
. 15 .
. 4.93634x10 4.80096x10
. 63 . 17 ....................
. Cu . (n, )
17 .
. '4.10297Z10 . 3.40917x10 -
. 65 .
17 . 17
.Cu (n,2n) 5.30130X10 .
. 6.46168x10
~
. 115 . 15 . 15
.In {n,n') 7.61418x10
. 7.37723x10
. 237 . 14 . 13
.Np (n,f) . 6.44534x10
. 13 .
. 6.92798x10 .
. 2381 . 14 6.67566x10 . ................
. 14 .. =
14 4U? .( n,f) 7. - 1.31794x10 '
. 1.32889x10 '
........................................................ 1.32237x10 . ................
_ _. e BUGLB93 used pressure vessel 1/4T weighting spectrum to collapse cross
~
A sections.. . t. ,
~78 AIL 0EL' used flat weighting spectrum to collapse cross sections
-A m , , .m x mwite,n+mns ,.gh. y% %a w ym- n o= s w'w' mwn. > - e4. 4. n , e
- %Q.W~ M?,t44y?N,N6/5MNb'N
+h 1[k,I Dh -
, ,r e m p 3; ; i, 4-.
, y,.- - -9 p ne
.f ..w.
1 ik$NY?Wh.:? ?O ^ U. 2is;*,
,e" , mm n a 4- s[ m.,s[
4 g
..O -hM_ J. .
[ (N $
- ~ -
.,;....- a :. ' . .
- --: = =.=..:..,_u:r z "...r.: . .- - - --
Table 4,1.3.13 Low Leakage Core Loading Effect of Selected Cross Sections on the Calculated Reaction Rates Axial Peak Reaction Rate (reactions /sec* atom) o Cavity Capsule (r=320.06ca,s=184.665ca,8 9.5 )
. Detector .
. SAILOR .
. Waterial BUGLE 93
. ENDF/B.IV . ORNL
.........................................................../TN.11476
. 27. 19 ...............
.Al (n, eh . .
. . 19 .
. 8.23690210 . 8.51363x10 .
. 32 . 17 . 17
.8 (n p) . 2.56430x10 . 2.65870x10
. 46 . 18 . 18
.Ti (n,p) . 6.393 83x10 . 6.23519x10 54' . 17 . 17 17
.Pe (n,p) . 3.35862110 3.43927x10
. 3.32502x10
. 56 . 19 . 19
.Fe (n,p) . 9.24108110 . 9.91762x10
. 58 . 17 . 17 17
'.Ni (n,p) . 4.69114x10 4.64371x10
. 4.67184x10
. 63 . 19 . 19
.Cu (n.o4 4.31875x10
. 3.86573x10 .
65 . 19 . 19
.Cu (n,2n) 8.02959x10
. 9.66674x10 .
. 115 . 16 16
.In (n,n') . 1.21393x10
. 1.19735x10
. 237 . 15 . 15 . 15
.Np (n,f) . 2.23060x10 2.34751x10
. . 2.38177x10
. 238 . 16 . 4
- 16 .- 16 .
.U (n, f) 1.70382x10
. . 1.68464x10. .. 1.71748x10 BUGLE 93 used pressure: vessel 1/4T weighting spectrum to collapse cross sections.
EAILORL used flat weighting spectrum to collapse cross sections. omsywMsa!#ifGM*wvMwv A W U uMJuniuf M MSMWMN14NW$#6y y< s
;A =
s
, , b r 1
- 6. - 14 ; i Ti e G v N' 3 . ekS[ N
- ft ~ j 'i , = gg y gg ; g. .
' , ,N. IjM [YI
,' .k Y k > I
._ m . ;. ._ .
I Table 4.1.4.1 Partial Length Shield Assembly Core Loading Fluzes and DPA Rates I Pressure vessel Inner Wall at Lower Weld (s=67.1048 cm) FLUX FLUX DPA/s 6 (E>1.0 MIV) (E>0.1 MIV) 1 2.233795+09 5.38276E+09 3.62020E 12 2 2.234185+09 5.38504E+09 3.62030E 12 3 2.23845E+09 5.40259E+09 3.62731E 12 4 2.26291E+09 5.46318E+09 3.66640E 12 5 2.30312E+09 5.56249E+09 3.73053E 12 6 2.35724E+09 5.69822E+09 3.81720E 12 7 2.43213E+09 5.88913E+09 3.93721E 12
- 8. 2.54093E+09 6.157975+09 4.11042E 12 9 2.65700E+09 6.43975E+09 4.29478E 12 10 2.76892E+09 6.72406E+09 4.47400E 12 11 2.917544+09 7.09340E+09 4.71104E 12 12 3.09111E+09 7.52352E+09 4.98762E 12 13 3.29411E+09 8.02449E+09 5.310525 12 14 3.53195E+09 8.60001E+09 5.68827E 12 15 3.81302E+09 9.29202E+09 6.13329E-12 16 4.14606E+09 1.00976E+10 G.65903E 12 17 4.54195E+09 1.10492E+10 7.28119E 12 18 4.98766E+09 1.21176E+10 7.98068E 12 19 5.33654E+09- 1.29364E+10 8.52741E 12 20 5.62173E+09 1.37063E+10 8.98314E 12 21 6.07852E+09 1.48724E+10 9.70165E 12 22 6.46491E+09 1.599175+10 1.03184E 11 23 6.72432E+09 1.67994E+10 1.07272E-11 24 6.81068E+09 1.70941E+10 1.08657E 11 25 7.01473E+09 1.76814E+10. 1.11807E-11 26 7.41520E+09 1.85605E+10 1.17893E 11 27 7.877875+09 1.94505E+10 1.24861E 11 28' 8.30629E+09 2.01528E+10 1.31337E-11 293 8.54121E+09' 2.05372E+10 1.34880E-11 30 8.987665+09 2.13749E+10 1.414415 11 31 9.74142E+09 2.20030E+10 1.52631E 11
- J '; *j I h' mmw+v -
, e + . N; A ).1 bflh ' E khT dki (h. + i L; Y ' i *
*)
- N %d [ h h* 'I
^
Table 4.1.4.1 Partial Length Shield Assembly Core Loading Fluxes and DPA Rates (cont'd) Pressure Vessel Inner Wall at Lower Wald (s=67.1048 cm) l FLUX FLUE DPA/s 8 (E>1.0 MIV) (E>0.1 MIV) 32 1.04062E+10- 2.42896E+10 1.62611E 11 33 1.10525E+10 2.56920E+10 1.723113 11 l 34 1.172385+10 2.71705E+10 1.82430E 11 35 1.243065+10 2.87461E+10 1.93101E 11 36 1.34318E+10 3.09832E+10 2.08249E-11 37 1.48678E+10 3.41484E+10 2.29840E-11 38 1.63700E+10 3.74935E+10 2.52387E 11 39 1.78870E+10 4.08966E+10 2.751125 11 40 1.93876E+10 4.42734E+10 2.975075-11 41 2.07336E+10 4.73207E+10 3.17566E 11 42 2.14759E+10 4.90930E+10 3.28684E-11 43 2.22616E+10 5.08257E+10 3.40339E-11 44 2.33053E+10 5.31482E+10 3.557525-11 45 2.39822E+10 5.47C06E+10 3.65907E-11 46 2.40271E+10 5.52326E+10 3.66894E 11 47 2.43035E+10 5.58794E+10 3.72053E 11 48 2.44085E+10 5.59965E+10 3.72478E 11 49 2.40220E+10 5.52536E+10 3.669973 11 50 2.34054E+10 5.40702E+10 3.582113-11 51 2.30299E+10 5.31671E+10 3.52632E-11 52 2.25583E+10 5.19755E+10 3.45514E 11 , 53 2.18412E+10 5.02990E+10 3.349213-11 54 2.10390E+10 4.84424E+10 3.23133E 11 55 2.01911E+10 4.64943E+10 3.10704E-11 56 1.92011E+10 4.42950E+10 2.96250E 11 57 1.83672E+10 4.23688E+10 2.83993E-11 58 1.75780E+10 4.06419E+10 2.72450E-11' 59- 1.70842E+10 3.94581E+10 2.651355-11 60 1.67637E+10 3.87197E+10 2.603893 11-61 1.66007E+10 3.834685+10 2.57980E 11 e % 7
>5 ?' l'tT
- s. Y% f, 5y~ N4- * $, (':
1 y A b- ~^
.jv
+ j Q%) b; [=l [ fl )' ) u 4 p t .4v4 4 <
- red $4@?6^ m - i (, . , qhwpih eu. ') , . e , ,
#N hh M Niii.e D A3J* t I'
di-7 u N : ~ d?gp4dk{dhgigkd4 15ygrsk '
--- - J
Table 4.1.4.2 Partial Length Shield Assembly Core Loading Flus Spectrum Pressure Vessel Inner Wall at Lower Weld (s.67.104 ton 0 0*) Group Total 1 1.941363+06 2 5.41025E+06 3 1.94000E+07 4 3.44440E+07 5 5.211473+07 6 1.17603E+00 7 1.50194E+00 0 2.371595+08 9 1.54074E+0E 10 1.07761E+05 11 1.19241E+08 12 5.796185+07 13 1.497495+07 14 7.36260E+07 15 1.90632E+00' 16 1.98391E+0B 17 2.73455E+0B 18 4.252485+00 19 2.790685+08 20 1.394893+08 21 4.16800E 05 22 3.42922E+08 23 3.79122E+08 24 4.36742E+08 25 5.17911E+08 26 5.55939E+08 27 3.84285E+00 . 20 2.919965+0S 29 9.45355E+07 30 4.41074E+07 31 1.65994E+00 32 1.05050E+0B 33 1.77714E+08 34 2.49331E+00 35 3.130095+00 36 2.68347E+08 37 4.25142E+08
.2.266665+0S 39 2.47554E+08
' '~
40 3.14975E+08:
.41 3.893563+08
- 42 2.21554E+00 l- 43 2.910475+04 2.15918E+08-
.45 1.80784E+0B i~ 3.85360E+08 46 47 1. 617663+09 i
i i i
>* s /;)hy75$Ag p % , g g. i 1
,e ,, ,, ; . gg
+ ; .?: . . .
JT pCf r r{ nyyJ9 t 5 ,.9 e s ___ _ i
-:lfk Y ?l_1 lsW \ ^y\;?Q Q < r , :: uy[
,s[ b a .. ,, l;: m , g . . y-Q_ _--_g
' fjfh: , _ __ _.
/
1 Table 4.1.4.3 Partial Length Shield Assembly Core Loading Reduction Factors of Fluxes and DFA Rates Pressure Vessel Inner Wall at Lower Weld (su67.1048 cm) FLUX FLUX DPA/s 8 (E>1.0 MIV) (E>0.1 MIV) 1 - 1.2093+01- 1.1575+01 1.153E+01 2 1.210E+01 1.1575+01 1.154E+01 3 1.209E+01 1.1563+01 1.154E+01 4 1.206E+01 8 1.153E+01 1.150E+01 5 1.200E+01 1.147E+01 1.145E+01 , 6 1.192E+01 1.139E+01 1.1373+01 7 1.181E+01 1.127E+01 1.126E+01 8 1.164E+01 1.110E+01 1.110E+01 9 1.145E+01 1.091E+01 1.092E+01 10 1.127E+01 1.073E+01, 1.074E+01 11 1.102E+01 1.048E+01 1. 0 5 0 E + 0?. 12 1.071E+01 1.018E+01 1.021E+C1 13 1.034E+01 9.812E+00 9.850E+00 14 9.885E+00 9.3795+00 9.420E+00
- 15. 9.349E+00 8.874E+00 8.914F;+00 16 8.734E+00 8.298E+00 8.335E+00 17 0.048E+00 7.658E+00 7.692E+00 18 7.326E+00 6.996E+00 7.038E+00 19 6.780E+00 6.523E+00 6.511E+00 20 6.412E+00 6.141E+00 6.162E+00 21 5.815E+00 5.605E+00 5.407Et00 22 5.339E+00 5.149E+00 5.163E+00 23 4.952E+00 4.824E+00 4.812E+00 24 4.0175+00 4.712E+00 4.686E+00 25 4.575E+00 4.515E+00 4.462E+00 26 4.252E+00 4.252E+00 4.163E+00 27 3.961E+00 4.006E+00 3.890E+00 28 3.761E+00 3.833E+00 3.701E+00 29 3.675E+00 3.749E+00 3.616E+00 30 3.538E+00 3.579E+00 3.484E+00 T
9 M\ 'g * (
^
) -
7
, J. ? u ' ' - k(
E g [- 4 [ J i s.s i %; > ,
, X* , '
- 0N$?$1 n;M n
- C; p nr U g 4dyd T W +' N ' '
W ' * ' DN ' WNWWNMD@N MW *
'-J
= . -
- a ........,- .:;.-- ~- n ~ . .v , n . , , , . - - . - _
Table 4.1.4.3 Partial Length Shield Assembly Core Loading
' Reduction Factors of Fluxes and DPA Rates (cont'd)
Pressure vessel Inner Wall at Lower Weld (s.67.1040 cm) FLUE FLUE DFA/s 0 (E>1.0 MIV) (E>0.1 MIV) 31 3.242E+00 3.273E+00 3.200E+00 32 2.990E+00 3.015E+$0 2.9565+00 33 2.770E+00' 2.793E+00 2.743E+00 i 34 2.566E+00 ' 2.5895+00 2.545E+00
- 35 2.375E+00 2.390E+00 2.360E+00 36 2.135E+00 2.1665+00 2.1285+00 37 1.800E+00 1.915B+00 1.800B+00 30 1.681E+00 1.715E+00 1.606E+00 39 1.524E+00 1.560E+00 1.535E+00 40 1.411E+00 1.440E+00 1.420E+00 41 1.3275+00 1.352E+00 1.335E+00 42' 1.206E+00 1.3073+00 1.294E+00 43 1.245E+00 1.2663+00 1.253E+00 44 1.194E+00 1.214E+00 1.202E+00 45 1.155E+00 1.173E+00 1.163E+00 46 1.130E+00 1.154E+00 1.145E+00 47 1.117E+00 1.134E+00 1.124E+00 48 1.093E+00 1.110E+00 1.100E+00 49 1.074E+00 1.090E+00 1.001E+00
- 50 1.065E+00 1.0795+00 1.071E+00 51 1.0575+00 1.072E+00 1.063E+00 52 1.040E+00 1.063E+00 1.054E+00 53 1.040E+00 1.0565+00 1.0465+00 54 1.034E+00 1.050E+00 1.040E+00 55 1.030E+00 1.046E+00 1.D365+00 56 1.0275+00 1.043E+00 1.033E+00 57 1.0265+00 1.042E+00 1.031E+00 58 1.026E+00 1.041E+00 1.031E+00 59 1.0273+00 1.041E+00 1.032E+00 60 1.0273+00 1.041E+00 1.032E+00 61 1.027E+00 1.042E+00 1.032E+00 p .- 4 i
IE f gi '* \
.l )
,,q
;3 -
[, ,,5 GAMejTI;+'l? L Mb# * '+ 4 ' *Jk- W N 5. 42 %Ik N k 7 + - S f ph$} [ d4 0 ' Y )% 1-i 2, < . - . . lI '{ Q &Q i If'<' N8 #f"b I 't" ; # ' 'O ' ' , inhK0NVd@h4W" h "a " ; 'N *'* M NO ' D #WhN0WNW
- k,si Qi Y' g:
~
'R n E.; Il..%)?. .
.gya j;; f.9 * ' %* }
+t , - , ;.
- s s - a .. ,
- y. ,
4 + w .,. P. ' ~ ~
~
. Standard Core Loading Pressure Vessel Flux Spectrum At The 0-T Location ,
_ i i iii i i iii i i iii . , i ni . i iii i n ii i . . i i i iii . .i i nii .i i i iiir ml -
..'..j. . j 3
1010 = _ =_
- % : -A 1
- - ;g _ p -
... g
.. _ _ r u
- a. - -
1_. , a4 1-:.: c 1- ~r"");10g
- .c :
l
.. m .
qv a a. rm - w - _- ,i 79
+w ,- w _ -
p t_ n'>
.h ,
3 a. - - h5" n, ,, , _
- 108 ,
h y ,k, ? .,. ~1 t il! I t ill I t ill i 11ll 1 IllI I IllI I fil! I til! I fili I IllI I Ill! I tilI ~ j; I wf* 104 10-2 100 102 10 4 106
$ L +g :
4P+ yy: Energy (eV) _ y
.. .s > *- P- -
Figure 4.1.2.1 ; e..
- e_ 3 , t F
. I t
_ , i
.h : D'"< . _ ,
? ;' _ :
- i. <_ ^l .I
- .s5- y .
9 g * %. $$
^
Standard Core Leading Pressure Vessel Flux pectrum " At The T/4 Location ,
._. ny . .., . og . og i un og . un i os i un nu i ns e us_ '
. - i _
f - a 10 \ 10 ._
= 1 s _ : i e
as 4 J' 55
/ - tJ -
!r - _ - , a
- p e s- -
c310g ti
= ;;
[- u - e t= -
; ca - _ -
,- x _
tj 2, 2 =3 . ka: e.. ir _ - l . 1 .! k b p. > ', 2;e 108
= ,
o : - 1 i
~, ; .
A . _ r
- '1
. ,; ~ -
I fld I IIE I IIE I IId I IId I IId I Itd t ttd ttd t ttd t ttd t ttd {( [j(( 10 4 10-2 100 102 104 106 [j t..r er -
.m .
Energy (eV)
'? #' '4..'
) ?' ~ Figure 4.1.2.2 -
,2 ~
- i !
f i
}
1
eiy -
+' . g. 1.
- s.e +a - .
I _,\,. w
.Q , e, t : ^
. Standard Core Loading Pressure Vessel Flux Spectrum ;
AtThe T/2 Location ; (( _i sig i sig i sig i >>g i >>>i i sig i sig i > >9 i sig i sig i sig i iiii_ _ f _ . 2 1010 g 3
- =
y . . 1 . , g; : g i :
& es
.c w -
/
=
Is- 5 a 108 =-
= .= ; = : _ .
g c _ a ; y- - , s = -
- u. I '
8 '= g 10 r .
,a c .
n-s - 10 7
= _
- m. : #+ .+
.k ?; #.. .
id i nid i u nd n vis : ind i tid a nid i und i i J e and i and r und - l EI" -
$ 10-4 10-2 100 102 104 108 ;
EJ ' a Energy (eV) s: _ 3, Figure 4.1.2.3 4 4
x
. ' h 2..
3 :.; . 9- 7 3 # fy .: !- , T _e a.
. ~
$- Standard Corn Leading Pressure Vessel Flux Spectrum [
c*:. AtThe 3T/4 Location a [ _5 IIq 5 55q 5 555 4 IEq 5 lig 5 IIq 5 tiq 5 IIq 5 liq 5 55g 5 Igq 5 lig _ i u ,
+ ;. .
-[
~
1018 r .l
=
t
- - . i,
- - . o -
i l - M - . 2_ 108 =
._r, J '
=-
I 3 E E {[ c - - D - - .j es 8 . A e . n- 10 - - x
- s E
; G- - -
fi i - f cy '71 . . 10 7 r.
-: d
-> ?:- -
1 .w.* - _
- y. -
, 10 02 10 10 10 10 eo 7 . ; 4sO 3:
Energy (eV) i . ! y Figure 4.12.4 e ,, k? - .s - f ,' .s l i [ r T-4
3vu a: e , v.~
.:s .
r j-n =. f~h -'
,e., a...
I
- o. .
+'a + l
~
Standard Core Loading Pressure Vessel Flux Spectrum py - - AtThe 1-T Location d
+
2 o 10 10_'"'""'"""'"""
" ' ' ' 4-' " ' ' " ' ' _
1 Ji _
.s .
w _ ; w _ 4
. is 109 r r J'- : i
= _
.c _
g- _ t 1 a:: _ i C 3 1
' 8 -
E' 10 5 5 i x u _ 10 7 r
~
j . i
- t _ _
1 f p'. - t tid I tid I tid I tid I tid t fld I tid I tid I tid t tid I tid t tid 4
=5 E 10-4 10-2 100 102 10 4 106 j s
Energy (eV) . 7. y . =.
-kk$. Figure 4.1.2.5 .
2
' > t t
l
t; v 2-t
.3 - e ++
$ 's ,
A., + 4ff ,
,m ~ ,
Y#
- A
.:sr h, m
- Standard Core Loading Thermal Shield Capsule .
t< E Flux Spectrum - a
,; _...,.,...,.i3...,...,.., ..,...,...,..,..3_ l
- u. .
2 y . IT 1011 = - m -
=
x _ _ cm m . _
?' @
.. .- .c
,~ . -
a 3g = ,
. ~
- _ =_
c _ _ ,
- . m
- :
- I-m x _ _
I 4 [; %&. he - 108 = c t:, _ n.' k. 7, s# t tid'tIld Itid Ifld Itid Itid Itid Itid Iffd Ifld Itid Itid I' . ' 0$ E* 10 4 10-2 100 102 104 106 p:,::p. Energy (eV)
?m . -
*f:
,. v,* Figure 4.1.2.6 GYc .,
4, m .s
+-+..
?
k-
1 I ' ' ' ' ' lll l l 4 lIlli i I I . i;;l l i e m
- 2_
O. , , .
- . " o e =
E E : : _ m
, .. e 9 -
8 IE i E r 3 oi va : l
- 5 a _ _ e, e
- s u= _
=
._ o w au o
_ =_ a - . r = E q _ . _ ~. u =
- e_ _
'E _ _
= , ,
y : _ y _ _ o _ =_
.. , , , i iii. . . . iiiiii . . ini i
'o.
o o. 40 Jet l1871lun J8d xnu 4 6
'I
.s
',p,.
< 4;p.
- 4- , 1 e -3, ,
r [kM;ikk95h4pek?$$jO5['[s -fi .4.f.l'9 2 rF h fi 4.h j 6 i . + , g,3i df[p;pp Qtj@fQ,'gh4ps,;jjgdKl3((h;4J;f,gg i .. ' . 3{
' . i _. h., %.+ . 4
- y P -
1
.m 6 1 ,
e ?b? ~ ' n,.S. p,,,s
*g y_
*,.T4 -
r wk I ?.d'y w .
; : Standard Core Loading Cavity Capsule Flux Spectrum i
_a sig a sig a ssq s sig a asy a ssq a saq * *si 8 asi 8 88"I 8 884 8 884 ,- f
~
_- [ 10g- _
- E~
~ ,a r E
[ 2 .
. C . .y.
g
- n r y .
r
, :- >c~
=a8 IU r- ?-
o _- - ,
, w N e - _
_ Q. - -
; .. y .- . j !
x
- s -
, . Lt. * '
- 5- -
107 = E g ., V
' =
- 5. . .
_ 5 , r - _ S , x s . - 3;- f -c g; , _ ._ .- g q , m; 1 - ,
--- V ned d i and and e ind sid tid a vid and vid and t tid ;
$Y a 744
#N,
. . u. .
10-4 10-2 100 102 104 106 , p: : ' Energy (eV) : A ga; 3Y A i.w 5 s' Figure 4.1.2.8 % v. w?,u. y, j 4 *
. . . ;.. . .._ . . ~ . . . . . . .. . . . . . _ . . . . . . . . . . .. .. . . .
I ll5 3 3 5 I I 4 ]II II I ' I Y Y r
. i- -
E - m r
; L-1
>3 l3 . ~
.a O N
- k.
n s W - V O- r
- i @
E -
% w- L
- J :
R ,
. ~
, o Pm .
- . y a r
- i.
A
, iii . , , , , , ii...,,, , i...,-
o
- <= .
o o o t 40Jaylalilun Jed xnu T # 4 'l ; 4 e f lit
^
% *' 7 -. T t- i.
r s t
'7- - .
>' >,k: .y c
fr- 'A
% b'; K _ t .
. fN f ~hI F b z y 6, a ., 5
, 4,4 , ,,,k _.
l-I 4 $Nf:f$ k- . , f k. Q ' . h h
&- s-M6 nim 6h[dN[hdfsfhgmp_Q;.* N ,(c;ty gtgp444y1 '/DI!IdNIb k:hfhhh$h/ fbbfd3k)bM[N" ' -
~5
l l 1 1 l E
,i v..... . .....,,, . ,,
- i-
'S" u ?
e r
=.
u - r o
~
>5 -
- ~ ~
o a r
=
=
m "ks. ri d, r u - F : : F 1- - m, 3 ~ 3 r
- - y e ., o w-
- y
;- , ,, o a : :
. iiiii i i i i iiiii i i i i i., i ,i i i o m a n o
o o- o 40Jeylelilun Jed xntj e , .< - . 4 9
, e - j f [.k e i a.
g.
>- - > y xze y4 ,
[hdjih(.\ J
- r i+ -f, i g
-4'*
g, f, y
- ; y ; N .' g.:fj g..; d p I 3 4,Q 4 ff.4 hQpyt;$![ehdt ANN $i@t, 3
erM L f4Lgh>d46p: b m-J, -
'; T t, i; .
7 ( -_ ,
,Ti'g .if @r-fgghkiQ S-> ~
- ,. ~y 8 7 b p l % d,; ,.a f 6 9 ; 4 gg.g+;y g ;yj;7-u p y $Q) f;g a n QQs 3 ; Qt(
e
, t
,c . - , r , *c < ; ,S+ f.,> q _s .Q" .
+
l
. l g.
l' Low-Leakage Core Loading Pressure Vessel Flux Spectrum AtThe T/2 Location i sig i ing i asu a sig a sig i sig i ses a sig i ing a sig i ><g _ a ses_ ,
~
1010 r = .
- _=
_ N. _ D- 109 = = tis : = 6 : J _ l_ 22 _ - c -
- ) ;
y 7
- 103 e-
=
O. - ( . x - s . -i d E . -l w.: - 107 1_ _ r . y,D-I .
'i - ,.+v .-
7 y , -< ~r - 3; ~
.w. - .' - - a and vid a sad e tid s ned a tid a tid i tid s tid e and and e sud .
106 10 4 10 4 i
~
if". 3y. . s 10-2 100 102 106 2 3. - : 7 x- Energy (eV) wi~ . f;y. Is A . Figure 4.1.3.3
-Y _w.. <
a
,-4 i-
- yI
'~
, - - - a
.s .~ ,
e . 2 - W N,i 3.g6 #r :
- s. r, ,
.Se _w w#
t ___ Y y
}; : Low-Leakage Core Loading Pressure Vessel Flux Spectrum At The 3T/4 Location r . , . . . y i n . . 9 . 9 . . . .i . . . .i . . . .i . . . .i . . .i . . . .i . . . .i 's 160 _r ; - e : :
- y.
- s c .
is; 109 m r-
,_l L i i_
p_ y ' 'b 0 c=
^
_ Y ^ mm 108 =--
= -
g - _
- a. -
r
. x _ _,
~. . => -
~
c _ _, r 107 =
=- - ,.. 7 ,.i -
s a h ? ill! ! ll1l I fld I fld I Ild I Ill! I flN I II!I I Ill! I fld 1 Ild I fld 10 4 10-2 100 102 5: "." .
., 104 106 ;
if f 7 .
+
Energy (eV)
, b* % e * =
7: x
,,,y __ _ . _ _ _ _ _ _ __-_.-___-.___.__----..a
4: y W m [C'..v p
- w.
- sy ,
1, -
~
> e 'ep s., .f-.-' ~
g
~,.,. _
E' e
. .. i:
~ . .
1 Low-Leakage Core Leading Pressere Vessel Flux Spectrum [ At The 1-T Location _ . 3 .. g ..., .. , og i , ..., .i ,..., i . , . . i g . . ,_ , 7 109 _= 3 s _=_ g - e - e.
.c
- n. .
es - J ' 1 g 10 8 r T 7o. 2 m
- n. . _
e a. _ t - x _
,r
- = *
'l . ~,
# ,' 107 --
5 5 g,. - _
- a. .
+ h '.
A.. n. Y, ? 4' t std 1 tid e tid I tid t tid a tid 1 tid a tid a tid a ned a tid t tid , 106 4 4 10 10-2 100 102 10 106 ; b.%._ . s t fil . - Energy (eV) m-n o w . u .a.s :
? ' ,_
pt ae
.A s . ,E; . a x,,
n 6 . .
=
e I lll4 l l l 1 I .111.L' ' ' iieii iI 4 3 W
- i- ,-
r 3, - 3 I eens . y l E y o M .
?. w g .
r a e E
. I
- N r
u o$ g F q M w y b y N.
+==
g g . w gM . - G Bemm e.
.a. w b . .
g . .
.e m.
O r O gg . 1 w-- 3a : . : e W :: - J . . T o t' ?.
~
?.
~
w-= l lisai t t I I ll1911 I i 1 littl 1 1 I i o eo m o
=
o
, 40Jeyle1)lun Jed xnt:1 w g . ' s -4 6 I n i s irs , i / 7($ 4 > ,9 ; ( > a . . c_..i / $net E %lt # Jd s
, . , .'N' Y i).[ }.p q 4 '///$ g// 4yy _i? g4;; . d.4 4 sj . i fM*4,Nkkd%hYO'NI[5 i I t '"' I # "
'l' 5' '
5"
" i k b '# - *
' D -E biNEY dMd*- 8I5YNN NM Nd$
g p: A m.
.4-j%
- _f g -
7 ,
- g 9' 7-h, &
Low-Leakage Core Leading Pressure Vessel Capsule
~
Flux Spectrum
- ~ _...,......,...,..................,.....,, ...- .:4f-4 -
e e 1010 : _ q
~ fx 6>,.
O u x g . g
% :,-- e Q - .- a ,
1 M c i a 10g :- E 3,
-e
.ue O.
K ll V
+ . :. x -
_ =s - y ' f- . [I- - s'?. g';. -
.we - p .: . y ,- . =Fi. 108 - + _ +,
r-
;5: , . ~nvid as.d esad atidtsad aned itid a ned a sad a ned a tid e tid' I$i sz 10-4 10-2 100 102 10 4 108
& Energy (eV) 2., : ?;- 3'
'- Figure 4.1.3.7 4 7 ~
't i y .i ; t y:. n: r-
r ,. Eg ~~;I.,.; A - 4.L/t.
. . . -i sg s
'en s . .,
,s9 :.~;. .r ;-
a,m r-s. g_
.A
. g. Y.
i ( , Low-Leakage Core Leading Cavity Capsule 1:~ Finz Spectrum _a..ii i un i ug 4 un i nii i un i un a un i un i un i og i us-2- _ _
; 108 _r
., ; [ 2_
. p. w
+
.y
.c li; 108
= _= :
+, a - -
x ;x - - 1% , y .
,c - _
g- - - 4: . .e s A. w 81. !
+ x =. = .w -
, w #. . u_
,y. _ _ ,
a, - . - , s. n - t
.4-
- y+..
.# , 10g =.- m .* ; .e. 3 . -- -
- n ; x -
' It Y 1. ~
-s 'and a sid 's and a ud a nad a tid a tid a tid a tid : and a sad e red-
!kM.. 10 4 n 2 10~2 100 102 104 106 ( [ ., 2... Eriergy (e9
. . . b . l' fjif Figure 4.1.3.8 w 3 . 4; ,. ,
I
".[g -a 1 (4 ~.I % s k.- "*4[ -
.) Mf :. j 5
- 1. . ,
e i I _ ._ _i
m
; c, -
e nw U. - - I y) N i,Q '#, 1 > W-ra : s ,. :
% ._ 7 ,'M-
{,.'- - .T-; 'x-2 : -
~
T1 -
' ' Flux >1.0 MeV At The Pressure Vessel Weld Surface 8 .
M i i I i i i I 4 i l
'28 -
r
, , O - ?, E 24 - -
en . i 2 OJ - ^3 & ho 20 3 - r
.i I
. c :
i -;. w o. s. F i j r# 3 i cy g 1 Y C-4, .
+
i *P
.o.
12 - 3 v-A: 4
>< 8 j e: - 3 - !
i - - E I i f('f E - - A.
- 4 -
,': +-
t t
$n 3.!. 1 I I I I I i 1 O
Te&. 0 5 10 15 20 25 30 35 40 45 l d. %<-14 Angle (deg) l
.n kI e 7- k' Figure 4.1.4.1 ,
.M n 8 8 4: 4 6 ..
-$ gy ,
v 3,+- i . $ :e
+
b - g 1 1
n 5
, ' . a.
r an , i
+ , .
t P i .' '4 Y I 2'j
- 5 4,4- '* $M% ., N- #
- ' . ,- . ",1,$- # '
r' #
.c y g A7 e_
a r .n.. . . . ,,. -
,%_ -(. r: ;,% . , .a +p ,
4 .e . .. . y i :
. Flux >0.1 MeV At The Pressure Vessel Weld Surface '
..z w .
~
8 i i i i i i i i ; 7 - - O e .
~
.=e 6 - -
a E ' R5 - - ' I C ! o w 4.,a. . 54 - - i- ' C (
.L -
v o vo 3 - - [
. ' x . i , a..- _m_ 2 - -
x u. .
.r :
1 .
- 1 . t 5, o & : - t l .1 I I I I f i
, av 4- U ;
##' 0 5 10 15 20 25 30 35 40 45 i i
4 i _ Angle (deg) ; Figure 4.1.4.2 ; v > s i
e: Tr #- 4
- 4 r
~ . T#
w . .
,,,~_~..-
- kl ." V#p r a -
A een R,--
$_p' x.>
i;~ Displacements Per Atom At The Pressure 4 Vessel Weld Surface 8 i i : : i i
.r7 T"o -
,- 6 -
X E 2 5 - u .
, , e -
x n. a y 4 _ a c .
.: , , e c _
E e 3 -
.s. .
u
. t13
- q. c2 .
v_ 2. _m_ o 2 -
? 1 y., -
i i i i i i i r
- 2. :: 0 M 0 5 10 15 20 25 30 35 40 45 ,
- -est , } ; '^ ~ Angle (deg)
; renn V..
n yn ., l
}
l p I ' lIl i i i ii i i p i i I i. e
'S-
- 1 u .
m i H _ i li
- ,o E :
.(
t/)
=
e ass N O -
. . - ., v
- u. -
a- -
+
u , ER
. l -
i . eg., e m M r b i
, o g . .
e i
- :y I ,
T , iii i i i ,i i iiii i i , i i iiii i i ai, o cm ao b. O O O A0Jeytell!un Jed xnij 9 h
\{ ' q -_
9-VAy g4_; h f 1_h'g : 3cvd-M- m . 1 + ,4
~
a )44 #1( ' ~,4k 5 8 '
- m. [c f. g + s
- pIM$d sNQffqd[fnN /(t-y(g.gggf pg j_g4 4 g .(;g:4 47ygg:-j - a ;- *
+ i:* *Wj$ - iW " 6)? 1 5
+ w 6 6 [I:ka- ' '[4 h ""~ r
Table 4.2.1.1 Mesh Used in DORT Calc'J1stion R(ca) E(ca) 0(revolution) 1 0.00000 0.00000 0.00000E+00 i 2 7.50000 3.09750 6.247225+03 3 15.0000 6.19500 7.638095 03 4 22.5000 9.29250 9.027705 03 5 30.0000 12.3900 1.041945 02 6 37.5000 15.4767 1.378895+02 7 45.0000 10.5633 1.531673 02 0 52.5000 21.6500 1.79556E.02 1 9 60.0000 24.7357 1.95444E.02 10 67.5000 27.8213 2.003895 02 11 75.0000 30.9100 2.065565 02 12 02.5000 33.9967 2.153093 02 13 90.0000 37.0033 2.362783 02 14 97.5000 40.1700 2.37944E 02 15 105.000 43.2567 2.479445 02 16 112.500 46.3433 2.63556E 02 17 120.000 49.4300 3.065005 02 18 127.500 52.4700 3.392705 02 19 135.000 55.5260 3.098335 02 20 142.500 50.5740 4.15722E.02 21 150.000 61.6220 4.45309E 02 22 157.500 64.6700 4.71270E+02 23 165.000 67.7100 4.94056E 02 24 172.600 70.7660 5.260333 02 25 100.000 73.8140 5.565005 02 26 102.602 76.0620 5.678895 02 27 185.560 79.9100 6.120565 02 28 196.709- 82.9500 6.37944E.02 29 187.705 06.0060 6.676115 02 30 109.897 89.0540 6.002225 02 31 109.782 92.1020 6.004443 02 32 190.616 95.1500 ' 7.013095 02 33 191.625 98.1990 7.162225 02 34 192.706 101.246 7.212783 02 35 193.369 104.294 7.54611E*02 36 194.000 107.342 7.76833E+02 37 194.782 110.390 7.95444Ea02 38 195.444 113.439 9.046113 02 39 196.207 116.406 8.203095 02 40 190.098 119.534 - 8.321115 02 41 190.025 122.582 0.40778W 02 42 199.500 125.630 , 8.601675 02 1 43 200.562 128.670 8.759445 02
- vi t 4 . ,,
dhh*j. i- Jj 1 (,j(q l g ,- 7
! 1 l k -y [: ,
^j k f).W Gj 3 p 3
, # h- i g g j h; m@j pd/D <h hg = ,rr / ,
, , , , . , , , _ _ _ _ _ _ _ - . , _ , , - _ _ , .___. _ _ - _ _ _ _ _ _ _ . __ _ . _ _ _ _ _ _m Table 4.2.1.1 Mesh Used in DORT Calculation (cont'd)
R(en) 2(ca) 4(revolution) 44 201.416 131.726 0.000565 02 45 202.450 134.774 9.037225 02 46 203.446 137.022 9.296115 02 47 204.500 140.070 9.420565+02 40 205.506 143.910 9.71270E 02 49 206.520 146.966 9.064455 02 50 207.440 150.014 1.01506E.01 51 200.610 153.062 1.05650E.01 52 209.491 156.110 1.096093 01 53 210.474 159.150 1.112065 01 54 211.606 162.206 1.123205 01 55 212.505 165.254 1.153725 01 56 213.795 160.302 1.173563+01 57 214.611 171.350 1.100115 01 50 215.643 174.390 1.222225 01 59 216.300 177.446 1.23611E+01 60 217.732 100.494 1.240615 01 El 210.310 103.542 1.250005 01 62 215.403 106.590 63 220.202 109.630 64 221.543 192.606 65 222.394 195.734 66 223.735 190.702 67 225.040 201.030 60 226.423 204.070 69 227.237 207.926 70 220.431 210.974 71 229.450 214.022 72 230.719 217.070 73 231.344 220.110 74 232.630 223.116 75 233.095 226.214 76 234.074 229.262
- 77 235.625 232.310 70 236.176 235.430 79 237.220 230.430 00 230.470 241.430 81 239.300 244.430 02 240.227 247.550 83 240.703 250.590 to 241.770 253.646 05 242.570 256.694 06 243.672 259.742.
qq p + . - 4: > r I , y. .2-, ; ! 4.
"d,
$fl ,
f n 394M,;, y ,- p Mfng; f, , . n;. . 1O
! pod 4 W n- , 4 q 3 44 ,
we - w ;** E " Mtv;dps? W i M >
. . . - . = .
s Table 4.2.1.1 Mesh Used in DORT Calculation (cont'd) R(os) E(en) 87 244.461 262.790 et 244.974 265.830 39 245.616 260.006 90 247.540 271.934 91 240.091 274.902 92 249.019 270.030 93 250.597 201.078 94 251.140 284.126 95 251.560 287.174 96 252.267 290.222 97 254.077 293.270 98 255.593 297.000 99 257.727 300.090 100 250.519' 304.700 101 259.530 300.510 , 102 260.326 310.430 103 261.122 313.430 104 261.910 316.430 105 262.715 319.430 106 263.511 323.750 107 264.307 326.798 108 265.103 329.846 109 265.099 332.894 110 266.695 335.942 111 267.491 330.990 112 268.208 344.070 113 269.557 349.150 114 270.020 354.230 115 272.090 359.310 116 273.357 364.390 117 274.073 369.470 lig 274.778 374.550 119 275.484 379.630 120 276.109 304.710 121 276.995 309.790 122 277.600 394.070 123 270.600 399.950 124 270.878 405.030 125 279.627 410.110 126 200.376 415.190 127 201.125 420.270 128 201.875- 425.350 4
- , . . s a
5- -, e s-y g . * * - ' '
* ""5 * #
b '' i O f Y$[k NN +
-Y Ik h 4@ f (II'$(IdN f hMIb@NhA_hikh/Yi' *
. % -m a.nm , _
) , ,.y . _1 1 A$h N +
- m 4 0l + Qsg. 44 47 g -:
3 ,l4 [ ; 5 ' g,,
Table 4.2.1.1 l Mesh Used in DORT Calculation (cont'd) R(cm) E(cm) 129 282.624 430.430 130 203.454 436.603 131 204.284 442.777 132 205.114 440.950 133 205.944 455.123 134 206.774 461.297 135 287.604 467.470 136 200.435 473.643 137 209.265 479.017 138 290.095 485.790 139 290.925 ' 495.637 ' 140 291.755 505.204 141 292.505 514.931 142 293.415 524.578 143 294.245 534.225 144 295.075 543.072 145 295.905 553.519 146 296.735 563.166 147 297.565 572.814 140 290.396 502.461 149 299.226 592.108 150 300.056 601.755 101 300.886 511.402 152 301.716 621.049 153 302.546 630.696 154 303.376 640.343 155 304.125 649.990 156 304.875 659.637 157 305.624 669.204 158 306.373 670.931 159 307.122 680.578 160 307.919 698.225 , 161 300.716 707.072 162 309.513 717.519 163 310.310 727.166 164 311.156 736.813 165 312.002 746.461 166 312.84E 756.108 167 313.695 765.755 168 314.541 775.402 169 315.387 705.049 170 316.233 794.696 t
,,, n. , "
., : . 154 ,
i g ' 'A4 *: {; ]: Q*- r* 7 ,
k' s ,
4,. h- } s'[ ,;( _ f .b r ^f,
'$t /_.Y # p 'j -r
= .
03 be OA; > %:, - .a -
< ;O+ '
1 ;#- m ? ij- t , si.I hr-E& hip'iO VP ,g < $3}fgi' j ; 4h 5 6 . , ng { Q /e
- i 4dh{pi;i(,y r c h; sl4 1$!ddy,J >
.c - _ . - _ _ _ _ _ _ _ _ -
Tabh 4.2.1.1 Mash Used in DORT Calculation (cont'd) R (cm) E(cm) 171 317.079 804t343 172 317.925 813.990 173 318.772 174 319.610 175 320.464 176 321.310 177 321.786 170 322.706 170 324.500 ' 100 325.318 101 326.310 . 102 327.034 103 329.351 184 330.351 1 185 331.867 106 333.303 187 334.333 - 180 336.149 109 337.915 190 340.790 191 346.290 192 351.790 193 351.949 194 354.006 195 357.663 196 360.520 197 365.611 198 370.701 195 375.792 200 300.003 201 305.973 202 391.064 a 203 396.155 204 401.245 205 406.336 206 411.427 207 416.517 208 421.600 209 426.699 210 431.709 211 436.080
' '212 437.500
'213- 441.500
>214 445.500 215 449.500
!: 4
=216' 453.500 217- 457.500 218 461.500
, 4 219 465.500 220 469.500 221 473.500 222 477.500 4:a ; , e p (! ? , 3; 1
< - , c tw-6 2 ,ji, l;g s lo 3.6 991 y c,, _
,_ , 4g-g, @f fg,j.q'ju d;,y , .
% t ) ;:k k $. f i ,r- ,_. t {f6'(^f a fwff\ lpl&yk(f fi--i[4Mg {h
Table 4.2.1.2 47-Group Energy Structure of Cross-Section Library lower Energy 14wer Energy Group (Mev) Group (Mev) 1 14.19' 25 1.83x10' 2 12.21 26 1.l ix10 3 10.00 27 6.76x10-8 4 8.61 28 4.09x10'8 5 7.41 29 3.18x104 6 6.07 30 2.61x10'8 7 4.97 31 2.42x10'8 8 3.68 32 2.19x10-8 9 3.01 33 1.50x10~8 10 2.73 34 7.10x10 8 II 2.47 35 3.36x10~8 12 2.37 36 1.59x108 d 13 2.35 37 4.54x10 14 2.23 38 2.14x10d 15 1.92 39 1.0lx10d 4 16 1.65 40 3.73x10 17 1.35 41 l.07x10-8 18' l.00 42 5.04x10d 19 8.21x104 43 1.86x104 4 20 7.43 x10 44 8.76x10 21 6.08x10-' 45 4.14x104 4 2 C < - l i 22 : 4.98x104 - .46 1.00x10 3.69x104 47' O.00 . t
. 24 2.98x104 t'Ihe upper energy of group i is 17.33 Mev.
_-l5 e s s % .II .
'1 i .
f 4 h '[#
- _-[ _- 'h
i) - D' 46 m.. . , n, , , .x . w x gwp ,.m e:w
< +> w/+Weva*+ = > d !"si " d '#7 * ' ;
4edj%: ag- s', % '
Table 4.2.1.3 Nuclear Paraneters For Neutron Flux Monitors
. . Reaction of . + . Product .
. Monitor . Interest . Response Range . Ralf life .
. .63 60 . . .
. Copper . Cu (n,0() Co . 6.13Mov < E < 11Mov . 5.27 y .
. .54 54 . . .
. Iron . Fe(ne y) Mn . 2.47Mov < E < 7.0Mov. 312.2 d .
. .50 58 . . .
. Nickel . Ni(n.p) Co . 2.09Mov < E < 7.6Mov. 70.88 d .
. .230 137 . . .
. U+230 . U (n, f) Cs . 1.51Mov < E < 6.7Mov. 30.17 y .
. .237 137 . . .
. Np*237 . Np (n, f) Ca. 0.67Mov < E < 5.7May. 30.17 y .
. .46 46 . . .
. Titanium .
- Ti(n e p) Sc . 3.06Mov < E < 9.4Mov. 83.81 d .
1 j + The upper and lower limits of the energy range are defined such that 95% of the detector response occurs above the lower energy and 5% detector response occurs above the upper energy .
- Etfactive threshold used for group averaged cross sections .
?_
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o Table 4.2.1.4 Dosimeter Activation Crosa Sections (EUGLE93) 54 58 46 Group dpa (n,p) Ni (n,p)
.............................................................p)
Fe Ti (n. 1 2.92000E+03 2.616105 01 2.60050E 01 2.39950E 01 2 2.68300E+03 4.04120E*01 '4.70450s.01 2.66490E 01 3 2.45500E+03 4.696905 01 5.92300E 01 2.60920E*01 4 2.24500E+03 4.02250E 01 6.23120s.01 2.359903 01 5 2.09200E+03 4.82340E*01 6.254105 01 2.045505 01 6 1.97100E+03 4.781505 01 6.040405 01 1.54930E 01 7 1.79200E+03 4.33950E.01 5.00050E 01 9.755603 02 8 1.60000E+03 3.128205 01 3.014903 01 4.00220E.02 9 1.36900E+03 1.93220E 01 2.445405 01 5.25420E+03 10 1.26500E+03 1.32630E 01 1.710005 01 11 4.641905 04 1.19000E+03 7.07050E 02 1.24950E*01 6.85070E 06 12 1.24600E+03 5.65520E 02 9.655703 02 13 1.069203 06 1.16600E+03 5.120104 02 8.854507 02 3.77160E*07 14 1.09600E+03 4.49420E 02 7.91190;.02 15 3.42230E 07 1.03600E+03 2.93400E.02 5.06570E.02. 2.334405 07 16 8.19000E+02 8.87320E 03 2.782605 02 17 7.947503 00 9.15000E+02 2.90280E.03 1.46240E 02 0.395005 10 18 6.32000E+02 7.32000E 04 5.614405 03 0.00000E+00 19 2.67000E+02 0.69400E*05 1.294405 03 0.00000E+00 l 20 5.16000E+02 6.56090E.06 0.92600E 04 0.00000E+00 21 4.00000E+02 2.63610E 07 5.21060E 04 0.00000E+00 22 2.69000E+02 0.00000E+00 1.76550E 04 0.0)000B+00 23 3.00000E+02 0.00000E+00 0.00000E+00 0.00000E+00 24 2.24000E+02 0.00000E+00 0.00000E+00 0.00000E+00 25 1.78000E+02 0.00000E+00 0.0A000E+00 0.00000E+00 26 1.92000E+02 0.00000E+00 0.00000E+00 0.00000E+00 27 1.34000E+02 0.00000E+00 0.00000E+00 0.00000E+00 20 7.54000E+01 0.00000B+00 0.00000E+00 0.00000E+00 29 7.14000E+01 0.00000E+00 0.00000E+00 0.00000E+00 30 2.94000E+02 0.00000E+00 0.00000E+00 31 0.00000E+00 6.08000E+01 0.00000E+00 0.00000E+00 0.00000E+00 32 3.61000E+00 0.00000E+00 0.00000E+00 0.00000E+00 33 7.73000E+00 0.00000E+00 0.00000E+00 0.00000E+00 34 1.19000E+01 0.00000F+00 0.00000E+00 0.00000E+00 35 7.36000E+00 0.00000E+00 0.00000E+00 0.00000E+00 36 3.02000E+00 0.00000E+00 0.00000E+00 0.00000E+00 37 1.17000E+00 0.00000E+00 0.00000E+00 0.00000E+00 38 9.300005 02 0.00000E+00 0.00000E+00 0.00000E+00 39 1.36000E 01 0.00000E+00 0.00000E+00 40 ' 0.00000E+00 2.060005 01 0.00000E+00 0.00000E+00 0.00000E+00 41 1.100005 01 0.00000E+00 0.00000E+00 43^ 0.00000E+00 6.090005 01 0.00000E+00 ~0.00000E+00 0.00000E+00 43 9.25000E 01 0.00000E+00 0.00000E+00 0.00000E+00 44 1.47000E+00 0.00000E+00 0.00000E+00 0.00000E+00. 45 2.12000E+00 0.00000E+00 0.00000E+00. 0.00000E+00 46 3.30000E+00 0.00000E+00 0.00000E+00- 0.00000E+00: 47 7.65000E+00 0.00000E+00 0.00000E+00 0.00000E+00
..................................................................n
* @ a is not from Bugle 93.
. w, e , ,.. : v+ G M,+5 %:M W" i-v,9 Q g a in iv( 1- . '
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_ _ _,.,me _ ,, - - , .- _ _._ .. ~ .,.- _...-_ - . _ _ . Table 4.2,1.4 Dosimeter Activation Cross 5setions (EUGLB93) (cont' d) i
................................................................. )
63 230 237 eroup cu (n,at) U (n, f) wp (n, f) - 1 3.541405 02 1.20300E+00 2.20000E+00 2 4.337605 02 1.03450E+00 2.00210E+00 3 3.63770E+02 9.04600E+01 2.10550B+00 4 2.679305 02 9.95010E+01 2.17530E+00 5 1.005005 02 9.911405 01 2.23070E+00 6 9.06020B+03 0.306405 01 1.95600E+00 7 3.25320E+03 5.59790E+01 1.49100B+00 0 5.75050E+04 5.46370B+01 1.531105+00 9' :f.452505 05 5.252005 01 1.60900B+00 10 0.136203 06 5.232005 01 1.65070E+00 11 2.990603 06 5.32720E+01 1.66340E+00 12 9.393705 07 5.369105 01 1.66060E+00
.13 0.17650B+07 5.377003 01 1.66900E+00
- 14. 6.744305 07 5.303105 01 1.60260E+00 15 2.472605 07 5.30140E+01 1.60220E+00 16 1.374905 00 4.744305 01 1.64620E+00 17 0.00000E+00 3.16460E+01 1.50540E+00 it 0.00000E+00 4.007203 02 1.47170E+00 19 0.00000B+00 1.23000E+02 1.33050E+00 20 0.00000E+00 3.76100E+03- 1.19340E+00 21 0.00000B+00 1.404405 03 9.212505 01 22 0.00000E+00 6.251005 04 6.14430E+01 23 0.00000E+00 2.705305 04 2.63900B+01 24 0.00000E+00 1.520505 04 9.10400E+02 25 0.00000B+00 7.91640E+05 4.620705 02 26 0.00000B+00 1.07100E+04 2.332505 02 27 0.00000E+00 3.699703 05 1.46710E+02 20 0.00000E+00 9.159305 05 1.19920E+02 2P 0.00000E+00 2.904205 05 1.060605 02 30 0.00000B+00 5.203705 05 1.013405 02 31 0.00000B+00 2.331003 05 9.90910E+03 32 0.00000E+00 2.536503 05 9.770705 03
, 33 0.00000E+00 1.446605 04 9.545105 03 34 0.00000E+00 5.260905 04 9.14010B+03 35 0.00000R+00 1.272405 05 0.007303 03 36 0.00000E+00 5.906603 09 9.33510E+03 l 37- 0.00000E+00' 1.033105 03 1.36970E 02 i 30 0.00000E+00 1.150103 05 2.60970E+02 39- 0.00000E+00 1.705405 05 3.003305 02 l _
,40 0.00000B+00 2.00600E+05 6.261403 02 L 41. 0.00000B+00 1.42030E+04 2.46070E+02i ,
y ' *
- 42e 10.00000B+00-- :7.56670E+05 - 8.151003'03c # ', "NN 43' 'O.00000E+00 1.746003 06 3.953905 03
-44 0.00000E+00 1.040005 06 1.10250E+02-45- 0.00000E+00 3.477603-06 - 7.112203 03' 46 .0.000005600 3.777705 06 4.90640E*03, j -_47 . ' O.00000E+00 7.045405 06 1 1.134005 02-L a
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Table 4.2.2.1 Flux (E>1.0 3GfV) At l*ressure Vessel s 306.605cm 306.60ica 306.605cm 302.7f3ca 302.795cm 8 0T 1/4 T 1/2 T 3/4 T T A 6.047045+00 5.392415+C0 3.20670E+00 1.00936E+08 0.53931E+07 l 2 7.51923E+08 --4.06441e 00 2.94913E+00 1.69523E+00 0.241665+07 1 3 7 304065+08 4.627595+00. 2.820095+00 1.64414E+00 8.061295+07 4- 7.144575800 4.59403E+00. 2.77362Ee00_ 1.595585+00 7.92064E+07
- 5 ~7.04935E+08- 4.61510E+00 2.75164E+00 1.573195+00 .7.772295+07 ~
6 ~6.75790E+00 4.574365+00 2.73660E+00 1.554293+00 7.660965+07 7 C.35754E+00 4.36763E+00 2.646195+08 1.510063+00 7.57000E+07 8 6.03704E+00 4.14114E+00 2.53652B+00- 1.46902E+00 7.41660B+07 9 5.84700E+00 -4.06232E+00 2.456365+00 1.440473+00 7.335375+07 10 .5.72970E+08 -3.975215+00- 2.45363E+00 1.42000E+00 7.289165+07 11 5.64775E+00' 3.92097E+0s 2.41072B+00 1.42073E+00 */.26591E+07 12 5.64012E+00 3.89864E+00 2.39961E+00 1.39633E+08 7.21474E+07 13 5.69041E+08 -3.09601E+00 2.39032E+08 1.364793+00 7.173595+07 14 5.71479E+00 3.91101E+00 2.35730E+00 1.39215E+00 7.11394E+07 15 5.75902E+00 3.90400E+00 2.37740E+00 1.360995+00 7.091265+07 16 5.64153E+00 3.03472E+00 2.32050E+00 1.34002E+00 7.01720E+07 17 5.53714E+00 3.75614E+00 2.20(975+00 1.32995E+00 6.95022E+07
. it ' 5.400365+00 ' 3.71960E+'st 2.26994E+00 1.32548E+08 7.00560E+07 19 5.390695+00 3,72041E+00 2.2948FE+00 1.34961E+00 7.125615+07
~20 5.62990E+00 3.89091E+00 2.39074N+00 1.40500R+00 7.300263+07 21 6.204193+00 4.25224E+00 2.60021E+08 1.51224E+00 7.705775+07 22.'6.001385+00 4.62021E+00. 2.70695E+00 1. 59 4093 + 08 .- 0.02247E+07
'23 7.10103E+00 4.04072E+00 2.91483E+00 1.67431E+00 0.29602E+07 24 7.466595+08 5.027675+00 3;02462E+00 1.72620E+00 8.54600E+07 25 .7.59540E+00 5.13003E+00 3.06972E+00 1.77024E+00 0.607215607
-26 7.602R65+00 5.13336P+08 3.145375+00 1.006383+00 A.924993+07 27 .7.670015+08 5.302532+08 3.23542E+00 1.87423E+00 .s.25041E+07 20 0.00205E+00 5.55070E+08 3.30661E+08 1.94037E+00 9.52940E+07 29 8.534795+00. 5.02031E+08- 3.51052E+00- 2.01290E+00- 9.70004E+07 30 0.775073+08 -5.94074E+00- 3.50735E+00 2.053365+00 9.09335E+07 31 0.95443E+00 6.06070E+08 3.654393+00 2.00140E+00 1.004273+08
. 32 9.15604E+08 6.200404+00 3.73060E+08 2.131365+00. 1.02240E+00 33 =9.32874E+08 6.290015+00 3.00233E+002.16443E+00 1.03531E+09 4
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4 Table 4.2.2.1 Flux (E>1.0 lirV) At Pressure Vessel (cont'd) s 306.605cm 306.605cm 306.605cm 302.795cm 302.795cm 0 0T 1/4 T 1/2 T 3/4 T T 34 9.60023E+00 6.532595+00 3.92472E+08 2.23152E+08 1.06081E+00 l , 35. 9.906365+00 6.79690E+00 . 4.00384E+00 2.321475+00 1.09543E+08 36 '1.01103E+09 - 6.072995+00 4.15113E+08 2.36182E+00 1.115595+08
. 37 1.01494E+09 6.900973+00 4.17490E+08 2.30269E+00 1.12341E+08 30 1.02032E+09 6.95353E+00 4.199375+00 2.300275+00 1.13152E+00 g
-39 1.01705E+09 6.93485E+08 4.20905E+00 2.403363+00 1.13613E+08 40 1.01342E+09 6.946975+00 4.20275E+08 2.406493+00 1.14403E+08 ,
.41 1.01590E+09 6.93365E+00 4.217765+00 2.411063+06 1.140095+00 42 1.02131E+09 6.99027E+00 4.23064E+0S 2.43304E+08 1.15531E+00 43 1.02973E+09 '7.05702E+00 4.26405E+08 2.45224E+08 1.160965+00 44 1.04670E+09 7.13300E+08 4.314265+00 2.46550E+00 1.16697E+08 45 1.06991N+09 7.25504E+08 4.36796E+00 2.40372E+08 1.17136E+00 46 1.07300E+09 7.27117E+00 4.TF053E+0B 2.49995E+08 1.10294E+00 47 - 1.06300E+09 7.24919E+08 4.58525E+00 2.50546E+00 1.19203E+08 40 1.06000E+09 7.25573E+00 4.40045E+08 2.52216E+08 1.20492E+08 49 1.07420E+09 7.36789E+08 4.402275+08 2.57372E+00 1.22505E+00 50 1.13609E+09- 7.003273+08 4.73935E+00 2.710275+08 1.27020E+00 51 1.250093+09 8.56192E+00 5.156595+00 2.92440E+08 1.34781E+08
' 52 1.36002E+09 9.140695+00 5.445775+00 3.05590E+08 1.395003+08
'53 - 1.39142E+09 9.30604E+00 5.53277E+00 3.11440E+00 1.40012E+00 54 1.41713 E+09 9.47705E+08 5.63703E+00 3.16262E+08 1.43170E+00 55 1.43720E+09 9.63974E+00 5.73200E+08 3.22041E+00 1.45093E+08 56 1.44114E+09 9.67931E+08 5.77174E+00 3.23511E+08 1.45892E+00 57 1.390765+09 9.47376E+00 5.69035E+08 3.213D7E+00 1.45722E+00 58 1.34542E+09 9.20414E+08 5.50133E+00 3.17121E+08 1.45039E+08 59- 1.326285+09 9.10632E+00 5.52710E+04 3.1510nE+08= 1.44557E+00 60 1.32311E+09 9.00093E+08 5.49483E+00 3.18404E+00 1.43199E+00 1 -
f1
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L Table 4.2.2.2
, Flus (E=0.1 MET) At Pressure Vessel s 306.605cm 302.795am 306.605cm 302.795cm 302.795am 6 . 0 2- 1/4 T. 1/2 T 3/4 T T 1 1.56025E+09 1.411093+09 1.09493E+09 7.64354B+08 4.060065+00
,2n 1.634295+09- 1.37310E+09- 1.061053409_ 7.43910E+00 4.00694E+08 3 1.635053409 '1.34334B+09 1.03032E+09 7.31504B+00':3.96432E+00-4 1.560575+09 1.316115409 1.019295+09 7.170065+00 3.924363+0S 5 1.41304E+09 1.26330E+09 9.84322E+08 6.96896E+08 3.05355E+08 6 1.29754E+09 1.20310E+09 9.405375+08 6.74410E+08 3.704595+08 7 1.22910E+09 1.14630E+09 1.11404E+08 6.54010E+08 3.72593E+00 ,
) 8 1.17013E+09 1.093495+0' .76533E+08 6.34540E+00 3.665295+08 9 -1.139065+09 -1.07362E+C 8.56435E+00 6.250402+00 2.64000E+08 10 1.122195+09 1.057685+09 8.527465+0B 6.20391E+08 3.622395+08 R11 1.10833E+09 1.04751E+09 8.43410E+00 6.16015E+08 3.609783+00 12' 1.10015E+09 1.033675+09 8.33000E+08 6.077785+0e 3.586115+08 13 1.09694E+09- 1.026063+09 3.27923E+08 5.99594E+08 3.56510E+0S 14 1.10110E+09 1.026475+09 8.217075+00 6.00909E+00 3.55974E+00 15- 1.10400E+09 1.02094E+09 8.177765+08- 5.96337E+00 3.54532E+08 , 16 1.083995+09 *1.055683+09 0.04601E+08 5. 887'26E + 00 3.52772E+00 R17 1.06665E+09 9.09202E+00 7.94615E+00 - 5.833963+08 3.51606E+00
--18. 1.05111E+09- 9.872515+00 7.96262E+00 5.861273+08 .3.34055E+08 19 1.060665+09 9.99992E+08 8.11102E+00 5.98443E+08 3.60605E+0S
--20 -1.10505E+09 1.043965+09 8.43533E+08 6.19693E+00 3.69237E+00 "21 '1.200493+09 1.117685+09 0.93451E+08 6.49633E+00 3.796993+08 22 1.295365+09 1.199965+09 9.412775+08 6.76471E+00 3.90113E+00 23 1.36942E+09 1.24964E+09 9.03863E+00 7.05213E+00 . 4.00655E+08 24 1.42700E+09- 1.30043E+09 1.023275+09 7.29924E+08 4.11571E+00
'25--1.455915+09 1.32887E+09 1.04323E+09 7.464065+08 4.18120E+08 4
26 1.46965E+09 1.35410E+09 1.07114E+09 7.64695E+00 ,4.27632E+08 27' 1.49910E+09 1.395563409 1.10730E+09 7.92174E+08 4.40165E+00 20 1.560915+09 1.452063+09 1.150785+09 8.198165+00 4.531393+08
- 29. 1.64205E+09 1.51061E+09 1.10641E+09 8.41910E+00 4.60450E+08 30 -1.60121E+09 '1.53635E+09 1.207775+09 sis 4100E+00 4.64700E+08 31 '1.714495+09 1.564773+09 1.226595+09 8.65961E+08 4.69052E+08
-321 1.75231E+09 1.59010E+09 1.25090E+09 8.52115E+00 4.76242E+08
._ ,,33]1.70205E+09 1.62172E+09 1.26951E+09 0.93700E+08 ' =- 4.809785+08
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Table 4.2.2.2 1 Flux (E>0.1 Nev) At Pressure Vessel (cont'd) s 306.605cm 302.795cm 306.605cm 302.795cm 302.795cm 8 0 T. 1/4 T 1/2 T 3/4 T T 34 1.037173+09 1.66330E+09 'li30169E+09 9.14092E+08 4.89150E+08 ' 35 1.09057E+09 1.723365+09 1.343065+09 9.41422E+00 5.004895+08 36 1.914875+09 1.74621E+09 1.36401E+09 9.55991E+08 5.07620E+08 37 1.92263E+09 1.75706E+09 1.37415E+09 9.64183E+08 5.11446E+00 30 1.93322E+09 1.76700E+09 1.38119E+09 9.69470E+00 5.14780E+08 39 1.93224E+09 1.77081E+09 1.30930E+09 9.75447E+08 5.10003E+08 40 1.93296E+09 1.77829E+09 1.39397E+09 9.80786E+08 5.214675+08 . 41 1.94006E+09 1.78245E+00 1.401765+09 9.85511E+08 5.24542E+08 42 1.9 51995+09 1.79604E+09 1.40985E+09 9.92960E+08 5.27723E+08 43 1.96736E+09 1.80835E+09 1.41847E+09 9.9788PE+08 5.30363E+0B 44 1.99227E+09 1.82534E+09 1.43002E+09 1.00514E+09 5.33493E+08 45 2.03125E+09 1.85358E+09 1.44907E+09 1.016185+09 5.39414E+08 46 2.04414E+09 1.06627E+09 1.45960E+09 1.02575E+09 5.43715E+08 47 2.04555E+09 1.87766E+09 1.47355E+09 1.03565E+09 5.49602E+08 40 2.05525E+09 1.09537E+09 1.49000E+09- 1.04960E+09 5.56204E+08 49 2.09347E+09 1.93421E+09 1.52332E+09 1.071465+09 5.65411E+0B 50 2.21614E+09 2.04201E+09 1.60256E+09 1.12133E+09 5.83898E+08 51 2.43274E+09 2.21413E+09 1.71960E+09 1.19166E+09 6.07884E+08 52 2.6045BE+09 2.34074E+09 1.80079E+09 1.23864E+09 6.23027E+08 53 2.66457E+09 2.30385E+09 1.83107E+09 1.25770E+09 6.29953E+03 54 2.71879E+09 2.43007E+09 1.06545E+09 1.27903E+09 6.379475+08 55 2.760475+09 2.47111E+09 1.89570E+09- 1.29057E+09 6.45252E+08 SF 2.76594E+09 2.48029E+09 1.90513E+09 1.30520E+09 6.40093E+08 F1 2.70341E+09 2.45294E+09 1.89554B+09 1.30312E+09 6.49094E+08 58 2.64411E+09 2.41673E+09 1.87993E+09 1.29795E+09 6.48772E+08 59 2.62005E+09 2.40287E+09 1.07200E+09 1.29446E+09 6.48475E+08 60 2.61399E+09 2.39932E+09 l'.86895E+09 1.29896E+09 6.46926E+08
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Table 4.2.2.3 DFA Rate At Pressure vessel u 306.605cm 298.905cm 306.605cm 298.985cm 298.985cm
..0 0T 1/4 7 1/2 T 3/4 T T 1 1.266165 0.940665 13 '5.057505 13 3.636425-13 1.05131E 13 2 1.180243 12 0.19774E 13 5.476855 13 3.46251E-13 1.003063 13 3 1.148195 12 7.84016E 13 5.20927E 13 3.37831E 13 1.77393E 13 4 1.124695 12 7.779103-13 5.190753 13. 3.29444E 13 1.74999E 13 5 1.11291E 12 -7.755175 13 5.112635-13 3.231483-13 1.71007E-13 6 1.066095 12 7.635265 13 5.040103 13 3.171483 13 1.695955 13 7 1.00064E-12 7.27669E 13 4.863435 13 3.09166E 13 1.67421E 13 8 9.52544E 13 6.900475 13 4.663145-13 2.99320E 13 1.64447E 13 9 9.207545 13 6.77194E 13 4.53233E 13 2.94955E 13 1.630115 13 10 9.026735 13 6.632535 13 4.51974E 13 2.917915 13 1.62151E 13 11 0.899085 13 6.55229E-13 4.46295E-13 2.89876E 13 1.61675E-13 12 0.087075-13 6.50300E-13 4.41800E 13 2.05654E 13 1.60536E 13 13 8.905395 13 6.501495-13 4.40647E 13 2.00778E 13 1.59559E 13 14 9.029235 13 '6.521925 13 4.36890E-13 2.03611E 13 1.500935 13
- 15. 9.09732E 13 6.509515 13 4.360535-13 2.803313-13 1.58301E 13 16 8.905275 13 6.380725-13 4.276975 13 2.762555-13 1.57090E-13 17 0.745005 13 6.26816E 13 4.21885E-13 2.73301E 13 1.56256E-13 it 0.54713E 13 6.22202E-13 4.206093 13 2.73477E-13 1.574735-13 19 0.527013 13 6.23290E-13. 4.25694E 13 2.78531E-13 1.59980E-13 20 8.878205 13 6.512605-13 4.435005 13 2.80707E-13 1.64502E-13 21 9.771053 13 7.008465-13 4.760443-13 3.07104E-13 1.70440E 13 22 1.06975E-12 7.65022E 13' -5.07653E 13 3.21669E-13 1.76064E 13 23- 1.12715E 12 0.004075 13 5.293405 13 3.35878E 13 1.81150E-13 -
24 - 1.169433 12 . 8.20003E 5.485415 13 3.46332E-13 1.059915 13 25 .1.19120E 12 8.465653-13 5.577655-13 4.283333 13 2.20392E-13 26 1.190425-12 0.562033 13 5.71692E 13 4.400145 13 2.253515-13 27 1.200605-12 8.764955-13 5.08991E 13 4.561735-13 2.31405E 13 28 1.264413 12- 9.166295-13 6.146415 13 4.63074E 13 2.353225-13 29 1.336405 12 9.606955-13 6.360985 13 4.67748E-13 2.370453-13
.30 1.373773 12= 9.709225-13. 6.404675-13 4.696205-13 2.38593E-13 31 1.400073-12 9.971093-13:'6.596765 13..'4.725193 13 2.390975-13 32" 1.431355-121.019013-12 6.727293-13 4.73944E-13 2.414073-13 33- 1.450043-12-jl.034275-12;-6.041695-13 4.283333 13 .-l.009063-13 L ,-
- 4. [N
,.- s 7
< }b; '
l?
. + s ?Q v: ; , ,.
@-J A ,
dyiMe _rf " ].p]Q V: .j f j?p:j kj ? g 7 + 4 , - p ,
, s - s, A . ' b.g,%6 g 1> '
,94W# sn u *
, ,, -y _ q qqpWp3 py%hg
Table 4.2.2.3 DPA Rate At Pressure Vessel (cont'd) s 306.605cs 298.985cm 306.605cm 298.985cm 298.985cs 0 0T 1/4 T 1/2 T 3/4 T T 34 1.51410E 12 1.07226E 12 7.053423 13 4.400145 13 1.93551E-13 35- 1.563005 12 1.11550E 12 7.32687E-13 4.561735 13 1.99886E 13 36 1.58230E 12 1.128265 12 7.44668E 13 4.63074E 13 2.052175 13 37 1.59011E*12 1.134975 12 7.692482 13 4.67748E-13 2.09954E 13 38 1.59850E 12 1.14243E 12 7.52537E 13 4.69620E 13 2.119633 13
, 39 1.59319E 12 1.140785 12 7.56490E 13 '4 72519E 13 2.146333-13.
40 1.58715E-12 1.142233 12 7.56210E 13 4.73944E 13 2.17967E 13 41 1.590575 12 1.14004E 12 7.59049E 13 4.75326E-13 2.42528E-13 42 1.59925E-12 1.14985E 12 7.63188E 13 4.79320E 13 2.43978E 13 43 1.611523 12 1.16038E 12 7.67949E 13 4.825625 13 2.45215E 13 44 1.63945E-12 1.17343E-12 7.76344E 13 4.855995 13 2.46488E-13 45 1.67645E-12 1.19318E-12 7.86051E 13 4.89858E 13 2.48776E 13 46 1.60007E-12 1.19624E-12 7.08904E 13 4.93348E-13 2.50246E 13 47 1.66302E-12 1.19310E 12 7.91396E 13 4.957385 13 2.52380E 13 48 1.65563E-12 1.19469E 12 7.955513 13 5.000425 13 2.54998E 13 49 1.67625E 12 1.213363 12 8.10496E 13 5.099495-13 2.59050E-13 50 1.76802E-12 1.28157E-12 8.54123E-13 5.34821E-13 2.68535E 13 51 1.95400E-12 1.39958E 12 9.23120E 13 5.72184E-13 2.80885E-13 52 2.10860E-12 1.489803-12 9.704495 13 5.95508E-13 2.890375 13 53 2.15576E-12 1.51397E-12 9.84946E 13 6.052345 1? 2.91590E 13 54' 2.19300E 12 1.54031E 12 1.00267E-12 6.14616E 13 2.957113-13 55 2.22526E 12 1.56716E-12 1.01967E 12 - 6.25147E-13 2.99388E-13 56 2.23280E-12 1.575725 12 1.027095 12 6.286453-13 3.00993E-13 57 2.15436E-12 1.54497E 12 1.01598E-12 6.260313 13 3.01090E 13 58 2.00265E 12 1.50421E-12 9.99383E 13 6.19985E-13 3.00254E-13 59 2.05333E 12 1.48852E-32 9.91360E-13 ' 6.16801E-13 2.99529E 13 60 2.045045-12 1.48526E-12 9.85301E-13 6.212545-13 2.97762E-13 5 Y 4 g1 [f!
- i*" ~
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1n n ~ % Ly + g
, n
, pg m , 3 p 9 g y;, .9.; gy . C- W ;.inin dQk.; ">atyyty n <r
Table 4.2.2.4 Flux (E>1.0 MIV) At Pressure Vessel At the Axial Core Midplane s=239.93cm 8 0T 1/1 T 1/2 T ' 3/4 T T 1 7.26704E+08 4.86030E+08 2.90146E+00 1.641375+00 7.91649E+07 2 6.70030E+00 4.39211E+08 2.66826E+00 1.53785E+08 7.64112E+07 3 6.59431E+00 4.17809E+08 2.558700+00 1.4bl50E+08 7.47423E+07 4 6.45000E+00 4.16865E+00 2.50942E+00 1.44745E+08 7.35144E+07 5 6.36571E+08 4.16730E+08 2.40963E+08 1.42714E+00 7.206375+07 6 6.103175+08 4.13000E+09' 2.47613E+00 1.41000E+00 7.11014E+07 7 5.73601E+08 3.94400E+08 2.39434E+00 1.37786E+00 7.01097E+07 8 5.452775+08 3.73949E+00 2.29509E+00 1.333375+00 6.87598E+07 9 5.28103E+00 3.66032E+08 2.222565+08 1.31400E+00 6.80072E+07 10 5.174195+00 3.58961E+00 2.22000E+00 1.29550E+08 6.75791E+07 11 5.10015E+00 3.54700E+08 2.10049E+00 1.20804E+06 6.73620E+07 12 5.09342E+00 3.52051E+00 2.17120E+00 1.26671E+08 6.60091E+07 13 5.13915E+00 3.51822E+00 2.17007E+00 1.23009E+08 6.65083E+07 14 5.16125E+00 3.53182E+00 2.14202E+08 1.26290E+00 6.59555E+07 15 5.20206E+00 3.52554E+00 2.15121E+00 1.24192E+00 6.57453E+07 16 5.C9513E+08 3.46291E+08 2.09973E+08 1.222893+08 6.50590E+07 17 5.00004E+08 3.39195E+00 2.06931E+00 1.20649E+00 6.45136E+07 10 4.00430E+0S 3.35093E+08 2.05390E+00 1.20245E+00 6.49543E+07 19 4.07540E+00 3.35954E+00 2.07640E+08 1.22433E+00 6.60669E+07 20 5.00415E+00 3.52067E+00 2.17030E+00 1.27465E+00 6.04265E+07
- 21. 5.60294E+00 3.04009E+08 2.35273E+00 1.37185E+08 7.14415E+07 22 6.14253E+00 4.17224E+08 2.52171E+00 1.44610E+08 7.43763E+07 23 6.48517E+00 4.37043E+00 2.63736E+08 1.51885E+00 7.69204E+07
'24 6.74203E+00 4.53900E+00 2.73663E+00 1.56591E+08 7.92334E+07 25 6.05914E+00 4.63403E+08 2.77745E+00 1.60585E+00 0.05424E+07 26 6.06551E+00 4.60038E+08 2.84587E+00 .1.63864E+00 0.27465E+07 27 6.92577E+00 4.70705E+00 2.92733E+08 1.70010E+08 0.576175+07 28 7.29799E+00 5.01200E+08 3.06412E+00 1.76745E+00 8.83402N+07 29 - 7.70715E+08 5.26277E+08 3.17626E+00 1.82605E+00 9.0745's+07' 30 7.924265+00 .5.36431E+00 3.24576E+00 1.86267E+00 9.17224E+07 31 0.00620E+00 5.47266E+00 3.306393+08 1.800183+08 9.31068E+07 32 0.260175+00 5.59075E+00 3.37534E+08 1.93342E+00 9.47064E+07 33 8.42415E+00 5.68601E+00 3.44022E+08 1.96341E+08 9.60769E+07
? q y n b
f n #%Q.= _
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Table 4.2.2.4 i; ' i-l Flua (Em1.0 MEV) At Pressure Vessel (cont'd) At the Azial Core Midplane s=239.93cm .. 'O 0T 1/4 T 1/2 T 3/4 T T l ! 34 8.741063400 5.090775+00 3.55101E+08 2.02420E+00 9.03445E+07
- c 35, z 9.018483+00 6.137685+08 3.695065+08 ,2.105095+00- 1.01550E+08 1
! 36 -9.13042E+08" 6.206315+08 3.755965+08 '2.14250E+08.'1.034175+0B 4 , 37 .p.16505E+08 6.23800E+08 3.777465+00 2.16143E+08 1.04142E+00 ! 38 9.21437E+0S 6.279065+08 3.790565+00 2.16649E+00 1.04094E+08 . 39 9.104795+00 6.262173+08 3.009075+08 2.19019E+00 1.05321E+08 ! - 40 9.15174E+08 6.27300E+00 3.002621N00 2.18302E+00 1.06055E+00 1 41 9.17400E+0E- 6.26092E+00 3.016175+0B 2.107095+0B 1.06432E+08 l 42 9.22295E+08 6.31204E+08- 3.83500E+08 2.207095+08 1.07101E+00 43 9.29095E+08 6.37234E+08 3.05009E+08' 2.22450E+00 1.07625E+08
- 44 9.453073+00 6.44104E+C0 3.90353E608 .2.23655E+00 1.00103E+08
! 45 9.66213E+00: 6.551985+08 3.95210E+08 2.25300E+0g 1.09140E+08 } 46 9.68985E+0S 6.56573E+08 3.96164E+00 2.26779E+00 1.09667E+00 !- 47 9.60701E+00 6.54567E+08 '3.96764E+0B 2.27278E+00 1.10587E+00 48 9.57141E+08 '6.55136E+08 3.98133E+00 2.28792E+08 1.11710E+00 49' 9.69930E+08 6.652515+08L 4.05530E+09 2.33467E+00 1.13652E+08 l 50 1.025773+09 7.04546E+0S 4.287065+0F 2.45853E+08 1.18512E+00 51 1.13593E+09 7.73041E+00 4.66530E+08 2.65280E+08 1.249575+00 52" 1.22790E+09 8.26015E+08 4.92690E+00 2.772075+08 1.29333E+00 l- 53 1.25631E+09 0.40203E+08 5.00555E+08 2.82503E+08 1.30551E+00
- ' 54 1.27951E+09 8.55711E+08 5.10056E+08 2.968785+00 1.32746E+08 l 55 1.29763E+09 8.70334E+08 5.185063+08 2.92120E+00 .1.34520E+08 i 86 1.30121E+09 8.73920E+08 5.22180E+08 2.93455E+08 1.352595+08
- 57 1.25565E+09 0.55344E+08 5.14014E+00 2.915395+0S 1.35102E+09 I 50- 1.214665+09 - 8.30975E+08 5.04942E+00 2.87660E+08 1.344715+08 i 59 1.19735E+09 0.221293+08 5.00030E+08 2.85833E+08 1.34027E+08 l 60 1.194473+09 8.19035E+08 4.97111E+00 2.00090E+08 1.32770E+08 i
i i-u 4 .,= t 4 s ,
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T 5- S i'}Y I. .e ,, , + .
- ?* '* '
Pr J ' 2 *
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- n, .yp W ,fQ flu,if^
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1 Table 4.2.2.5 Flus (E>0.1 MEV) At Pruseuce Vessel At the Asial Core Midplane s=239.93an 8 0-T- 1/4 T 1/2 T 3/4 T T 1- 1.410663409 1.200375+09 9.97952E+00 7.02140E+00 '3.842965+00 2 1.47760E+09 1.24540E+09 9.67224E+08 6.834875+00 3.78504E+00 3 1.47902E+09. 1.210485+09 9.46472E+08 6.72133E+08 3.745115+00 4 1.410965+09 1.193763+09 9.29223E+00, 6.50921E+00 3.707575+08
- 5 1.27932E+09 .1.14503E+09 8.97289E+00 6.40341E+00 3.64115B+08 6 1.17315E+09 1.091075+09 8.645975+00 6.19642E+00 3.575773+00 7 1.110375+09 1.03954E+09 8.30740E+08 6.01633E+08 3.52043E+08 0 1.057963+09 9.91669E+00- 7.90965E+08 5.03014E+08 3.46335E+00 9 1.029063+09 9.73654E+00 7.00676E+00 5.75023E+08 3.43967E+08 10 1.01460E+09 9.592063+08 7.77301E+08 5.70039E+08 3.42302E+00 11 1.00200E+09 9.49900E+08 7.60008E+00 5.66012E+00 3.41114E+08 12 9.94602E+08 .9.37430E+08 7.59303E+00 5.504593+00 3.30803E+08 13 '9.917973+00 9.31250E+08- 7.54660E+08' 5.50969E+00 3.36903E+00 14-.9.95572E+08 '9.300863+00 7.490165+00' 5.522073+08 3.36411E+00 15: 9.90194E+00 9.25073E+08 7.45411E+08 5.47955E+08 3.35053E+08 16 9580096E+00 9.12032E+00 7.334975+00 5.40973E+00 3.33406E+08 17 9.64423E+08 0.97103E+08 7.243295+08 5.36091E+08 3.32397E+08 10 9.50374E+08 8.95354E+08 7.258575+08 5.38622E+00 3.35394E+08 19 9.50994E+00 9.06920E+00 7.393965+08: 5.49939E+00 .3.40020E+00 20 9.990395+04- 9.46702E+08 7.609365+00 5.685195+00 3.40943E+00 21 -1.00541E+09 1.01350E+09 _8.14370E+08 5.96871E+08 3.58702E+08 22 .1'.17110E+09- 1.07900E+09 8.57903E+08 6.21401E+00 3.68570E+00 23 1,23811E+09 1.133173+09 0.96696E+08 6.470485+00 3.70500E+00 24 1.29015E+09 1.17922E+09' 9.326085+08 6.705483+00 '3.88000E+08
-25 1.31630E+09 l1.20502E+09 9.50006E+00 6.85747E+00 3.949773+00 1.32870E+09 1.22793E+09- 9.762465+00 7.02402E+00 4.03941E+00 27: 1.35531E+09 1.26553E+09 1.00930E+09 7.27712E+00 4.15740E+00 24 1.41042E+09 -1.317475+09 1.04801E+09- 7.521575+00 4.260875+08
.29: 1.405293+09 1.36901E+09 1.001275+09 7.733515+08 4.34061E+08 30 1.519965+09 1.39314E+09 1.10070E+09; 7.045265+08 4.30933E+00.
. 31 -: .1.55005E+09 ; 1.410895+09.-1.11784E+09J 7.954063+08 4.437075+00s "32 sl~.58423E+09 1.44910E+09 1.140065+09,l0.10210E+08 -4.497225t08 533? 1.61111E+09 -1;47051E+09 1.15693E+09 30.200463400 4'.541795+08
h g 7 . A &
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l 1 Table 4.2.2.5 Flux (E>0.1 Blev) At Pressure Vessel (coot'd) At the Axial Core Midplane s 239.93cm 0- 0 T- 1/4 T 1/2 T- 3/4 T T 34 1.660965+09 1. 5127,2 E + 09 1.19623E+09 0.39530E+00 4.610675+00 35 1.70925E+09 1.56263E+09 1.223 09E+09 0.64595E+00 4.72535E+00 36 1.73122E+09 -1.50335E+09 1.24290E+09 0.77964E+00 4.79249E+00 ' 37 1.73025E+09 1.59320E+09 1.25222E+09 0.05407E+00 4.02059E+00 30 1.74703E+09 1.60301E+09 1.25065E+09 8.90353E+00 4.06004E+00 39 1.74693E+09 1.605695+09 1.26604E+09 0.95043E+00 4.09052E+00 40 1.74750E+09 1.612475+09 1.27032E+09 9.00761E+00 4.92320E+00 41 1.75399E+09 1.61626E+09 1.27743E+09 9.05111E+00 4.95229E+00 42- 1.76470E+09 1.62053r+09 1.20400E+09 9.119475+00 4.90230E+00 43 -1.770675+09 1.63974E+09 1.29266E+09 9.16450E+00 5.00722E+00
.44 1.001195+09 1.65514E+09 1.303175+09 9.23132E+00 5.036775+00 45 1.03645E+09 1.60074E+09 1.32053E+09 9.33202E+00 5.09272E+00 46 -1.04009E+09 1.692265+09 1.33015E+09 9.42003E+00 5.13340E+00 47 1.04934E+09 1.70261E+09 1.34209E+09 9.51200E+00 5.19902E+00 40 1.05000E+09 '1.71070E+09 1.35064E+09- 9.64043E+00 5.25212E+00 49 1.09261E+09 1.75394E+09 1.3002SE+09 9.04100E+00 5.33016E+00 50 2.00340E+09 1.052375+09 1.46046E+09 1.02907E+09 5.51214E+00 51 2.19925B+09 2.00762E+09 1.56710E+09 1.09435E+09 5.73702E+00 52 2.354595+09 2.12235E+09 1.64094E+09 1.13745E+09 5.00700E+00 53 2.40000E+09- 2.16142E+09 1.56053E+09 1.15492E+09 5.94556E+00 54 2.45779E+09 2.20405E+09 1.69904E+09 1.3.7451E+09 -- 6.020765+00 55 2.49540E+09 2.24054E+09 1.72740E+09 1.19243E+09- 6.00954E+00 56 -2.50045E+09 2.240073+09 1.73599E+09 1.19052E+09 6.116273+00-57 2.44390E+09 2.22414E+09 1.72731E+09 1.19664E+09 6.12501E+00 50 '2.390275+09 2.191375+09 1.71315E+09 '1.191965+09 6.12293E+00 59 2.36051E+09 2.17002E+09 1.70660E+09 1.10076E+09 6.12025E+00 60 2.36302E+09 2.17561E+09 1.70319E+09 1.19206E+09~ 6.10507E+00 I b
'x i
' h- ; E h j - h ( $ '( . ' 5 9 #
,; i Il .
1* h ( <T ~I"' k~ @ U
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+ c . 44te '
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' QGY'd$!.Yhk: Y lWW h ' WH
t Table 4.2.2.6 DPA Este At Pressure Vessel l At the Asial Core.Mi@ lame.,s=239.93ca 0T 1/4 1 1/2 T 0 --3/4 T T 1 ~ 1.145005 12 0.107925 13 5.322405 13 3.32735E 13 1.734125 13-2 1.067055 12- 7.420005-13 4.977253 13 3.169025 13 1.690133 13 3 -1.030045 7.104205 13 4.00709E 13 3.092245 13 1.66236E 13 o 4 1.016043 12. 7.049005 13 4.717595 13 3.015695 13 1.64010E 13 5 1.006295 12 7.027015 13 4.646275 13 2.957015 13 1.611015 13 6 9.641145 13 6.910175 13 4.500005 13 2.902535 13 1.509435 13 ' I ~7 9.049135 13 6.593223 13 4.419405 13 2.029403 13 1.569023 13 ! . 0.614305-13 6.252365 13 4.237455 13 2.739425 13 1.54120E-13 9 0.32650E 13 6.135923 13 4.110745 13 - 2.699433 13 1.527913 13 10- 8.162043 13 6.009635-13 4.107245 13 2.670563 13 1.519893-13 11 0.047353 13 ,5.936005 13 4.055675-13 2.653645-13 1.515435-13 12 0.C35743 13 5.092295-13 4.014705 13 2.614465 13 1.504795 13 13 -0.126155 13 5.090905-13 ~4.004275-13 2.56997E 13 1.495675 - 14 0.165973 13 5.909515 13 '3.97025E-13 2.595633 13 '1.409535 13 15 0.22775E-13 5.090305-13 3.96975E 13 2.565705 13 1.404005 13 16 0.053945 13: 5.706793-13 3.006603-13 2.520535 13 1.472773-13
; 17 7.909025 13. 5.679613-13 3.033095 13 2.501573 13 1.465063-13
- 10' 7.7k901E*13- 5.637073-13 3.022453-13 .2.503313-13 1.476503-13 19 7.711213-13 5.64771E 13 3.060695 2.549603 13 1.499933 13 20- 0.026005-13 5.$01003-13 4.031125-13 2.642615-13' 1.542005 13-i 21:10.836325-13 6.422653-13' 4.333065 13 2.010525 13 '1.597455 13
- 22: 9.674493-13' - 6.93147E 13 4.612715 2.943555-13 1.649075-13 23- 1.019323-12 .7.25102E-13 4.009633-13 3.073413 13 1.697305-13 24 _1.057525-12 7.50094E 13 24.904015-13'_3.169125 13 1.742605 13 1
25- 1.077205 12 7.669063-13 5.067915-13 3.242563 13 1.76996E-13
- 26.l1.076435 12 7.75795E-13 :5.194435-13 3.31677E-13 1.013353-13 27 -1.005005 12 7.94100E-13 5.351603-13 "3.436933-13 1.072473-13 2001;143303f12-L0.304503 5.504565-133.563145-13 sl'.922265 13 5
'seiT29]'1.200523 12 0.703753-13 4 5.779423 13" 3.669593-13 1.966473 . , 'q{ 30 3 11.242253-12.- 0.060093 13 .5.091605-13 ;3.734093-13 x1.905253 13 2
~ 31- 1'.265755;12i.9.034263-13 5.993425-13 3.703263-13 -2.010153 13'
- 32 1.294305 12 9.23101E 13 _6.111953 13 ' 3.061503 13 -2.041245-13 n a4 .J33h 1.310435 121.9.370033 13 _ '6.215745-131_3.910675-13 ;2.063073-13 ,
w - c p! , ~l . 'Y ' h '{ l - 5 _ ?
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4 Table 4.2.2.6 DFA Este At Pressure Vessel (coot'd) At the Asial Core Midplane s.239.93cm 4- 0T 1/4 T -1/2 T T 3/,4 T
'34 1.369175 12 9.714205 13 6.400013 13 4'.025333 13 '2.107265-13 35 1.413433-12 -1.010605 12 6.656333 13 4.172865-13 2.16710E 13 36 1.430875 12 1.02217E 12 6.765153-13 4.243243-13 ~2.20296E-13 37 1.437955 12 1.028255 12 6.80670E 13 4.278675 13 2.219073 131 30 1.445545 12 1.035015 12 6.836725-13 4.29594E-13 2.233563-13 39 1.440723 12 1.033525-12 6.872715 13 4.32239E-13 2.245795-13 40 1.435235 12 1.034025-12 =6.870195 13 4.33552E 13 2.25994E-13 '
41 1,43031E 12 1.033573-12 6.89597E 13 4.34024E 13 2.27040E 13
!42 1.446153-12 1.041723 12 6.933625-13 4.30473E 13 2.28405E 13 43 1.457245 1.051275 12 6.976915 13 4.41430E 13 2.295603 13 44 1.482535 12 1.063095-12 7.053103 13 4.442145 13 2.30756E 13 45 1.51602E 12 1.00099E 12 7.141305 13 4.48120E-13 2.329045-13
-46 1.51925E 12 1.003765-12 7.167313 13 4.513225 13 2.342905-13 47 1.504485 12 1.000913 12 7.190065 13 4.53529E 13- 2.362985-13 40 1.496995-12 1.002345 7.22793E 13 4.574065-13 2.307555-13 49 1.51550E-12 1.099253 12 7.363715-13 4.665495 13 2.425465-13 50 1.599213 12 1.16100E 12 7.75902E-13 4.892013-13 2.51394E-13 51 1.766613 12 1.26747E-12 8.30611E 13 5.234053 13 2.62913E 13 52 ~1.90640E-12 1.349555 12 8.015693-13 5.44720E-13 2.70510E-13 53 -1.949013-12 1.371443-12 8.947325-13 5.53603E 13 2.72909E-13 54- 1.982725-12 1.395285 12 9.10820E-13 5.621095-13 2.767545 13 55 2.011025-12 1.419615 12 9.262725 13 5.7101'0E-13 2.80184E-13
- 56 2.01067E-12 1.42739E 12 9.33010E-13' 5.75011E-13 2.81678E 13 571 1.947665 12- 1.399545 12 9.229545-13 5.72639E-13 2.017033 13 1.002725-12 1.36263E-12 9.079005-13 5.671443-13 .2.01007E 13 59 1.056195 12 1.340413 12 9.006265-13 5.642453-13 2.003415-13
'60 l1.84939E 12 1.34545E 12 8.960443 13- 5.68200E-13 2.707075 13 t
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d - 4 f .i ' m&W%&m% ~ w, - +. . ;,, a - , , %,uMgQgy%g:np nhS%WMqNQM:W .s r .. g , ,
- n Mp&asydf {pp%cty;cbl$%dQg;ggd
Table 4.2.2.7 Downconer Fluzes and DPA Rates (r=278.10am, s 300.605ca)
-FLUE FLUE DPA/s 8 (E>1.0 hEV) (E>0.1 MIV) 1 7.25624E+10 1.J2820Ee11 1.105025 10 2 7.295983+10- 1.32613E+11 1.110025-10--
3- 7.26404E+10 .1.317263+11 1.10644E-10 4 7.16205E+10 1.29700E+11 1.089793 10 5 6.77477E+10 -1.23602E+11 1.03104E 10 6- 6.39683E+10 1.17110E+11 9.744305-11 7 6.167995+10 1.12612E+11 9.390325-11 8 5.90013E+10 1.07374E+11 0.98694E 11 9 5.847605+10 1.05921E+11 8.097525 11 10 5.013295+10' 1.047975+11 8.84450E-11 11 5.71350E+10 1.020675+11 8.69997E 11 12 5.56754E+10 9.96783E+10 8.47665E 11 13 5.41220E+10 -9.705G4E+10 8.256023-11 14 5.30990E+10 9.48583E+10 8.098175 11 15 5.14766E+10 9.19491E+10 7.86062E 11 16 4.01467E+10 -8.60722E+10 7.364873 11 17 -4.60001E+10 B.30222E+10 7.153785 11 10 4.95016E+10 0.85162E+10 7.515185 11 19 5.31465E+10 9.54570E+10 0.029593 11 20 5.65551E+10 1.02120E+11 8.54056E 11 21- -6.191065+10 1.11952E+11- 9.34593E 11 22 6.705065+10 1.21153E+11 1.014525 10 23 7.200485+10 1.30025E+11 1.095615 10 24 7.020115+10 1.43204E+11 1.19>004E 10 25 0.325415+10 1.53070E+11 1.265663 10
- 26, 9.04047E+10 1.66423E+11 1.373665-10
- 27. 9.06623E+10 1.01314E+11 -1.49569E 10 28 :9.91442E+10 1.841365+11 1.505345 10 29 9.790383+10 1.827073+11 1.40854E-10 30 9.76924E+10 1.82694E+11 1.40610E 10 31 9.70467E+10 1.01053E+11 1.470385 10 32 9.76712E+10 1.807075+11 1.48630E 10
+
33 '- c 9.747995+10 1.796995+11 1.40537E-10'
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Table 4.2.2.7 Downconer Fluxes and DPA Rates (Cont'd) (r= 27 8.10 cm, = =3 06 . 6 05 ca) 3 FLUX FLUX DPA/s 8 (E31.0 serv) (E>0.1 MEv) 34 9.61024E+10 1.75665E+11 1.46186E-10 35 9.06185E+10 1.65623E+11 1.37976E 10 36 8.48232E+10 . .1.55773E+11 1.29350E 10 37 8.16531E+10 1.503295+11 1.24532E-10 38 7.95092E+10 1.46334E+11 1.21408E-10 39 7.90791E+10 1.44564E+11 1.20598E-10 40 7.87170E+10 1.43282E+11 1.201515-10 41 7.98183E+10 1.44043E+11 , 1.217475-10
. 42 8.02073E+10 1.44508E+11 1.22321E-10 43 8.00899E+10 1.44332E+11 1.22175E-10 44 8.15130E+10 1.470875+11 1.24256E-10 45 8.432375+10 1.53396E+11 1.28692E-10 46 8.817473+10 1.61410E+11 1.34585E-10 47 9.58350E+10 1.76402E+11 1.46028E-10 48 1.05302E+11 1.95758E+11 1.60424E-10 49 1.17721E+11 2.20651E+11 1.79092E-10 50 1.40142E+11 2.66256E+11 2.13342E-10 51 1.68364E+11 3.22637E+11 2.56196E-10
'52 1.83158E+11 3.54577E+11 2.79363E-10 53 1.87330E+11 3.64740E+11 2.86302E 10 54 1.95986E+11 3.81241E+11 2.99061E-10 55 2.05900E+11 3.99845E+11 3.126913-10 56 2.11886E+11 4.11390E+11 3.199175-10 57 2.14478E+11 4.16842E+11 3.22964E-10 58 2.13838E+11 4.17023E+11 3.22D38E-10 59 , 2.11683E+11 4.14384E+11 3.19146E-10
-60 -2.12178E+11 4.15588E+11 3.19652E-10 9A ?$ gj);gjp ' , M J -.Q[g "
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f Table 4.2.2.8 Downcener Flumes and DPA Rates (At the Axial Core Midplane r=278 10ca,s=239.93ca) 7 FLUX PLUX DPA/s 8 .(E>1.0 MEv) (E>0.1 NEv) 1 6.37689E+10 1.16516E+11 9.71895E-11 2 4.41228E+10 1.16341E+11 9.77082E 11 3 6.38515E+10 1.15566E+11 9.732775-11 4 6.29473E+10 1.13795E111 0.58d24E 11 5 5.95411E+10 1.08433E+11 9.07593E-11 6 5.62185E+10 1.02737E+11 8.57088E-11 7 5.42094E+10 9.87932E+10 8.25989E 11 8 5.18584E+10 9.42019E+10 7.9056SE-11 9 5.13990E+10 9.29299E+10 7.82730E-11 10 5.10988E+10 9.19465E+10 7.78113E 11 11 5.02236E+10 9.025585+10 7.65435E 11 12 4.89432E+10 8.74614E+10 7.458395 11 13 4.75803E+10 8.51574E+10 7.26460E 11 14 4.668175+10 8.32354E+10 7.12585E 11 15 4.52557E+10 8.06837E+10 6.91700E 11 16 4.232885+10 7.55272E+10 6.48082E-11 17 4.12225E+10 7.35531E+10 6.29520E-11 18 4.35905E+10 7.76722E+10 6.61346E-11 19 4.67210E+10 8.37578E+10 7.06555E-11 20 4.97133E+10 8.95987E+10 7.514345-11 21 .5.44260E+10 9.82231E+10 8.22257E-11 22 5.89434E+10 1.06295E+11 8.92547E 11 23 6.33574E+10 1.14776E+11 9.63790E-11 24 6.87252E410 1.25626E+11 1.04739E-10 25 7.31611E+10 1.34275E+11 1.11311E-10 26 7.94440E+10 1.45987E+11' 1.20808E 10 27 8.66980E+10 1.59048E+11 1.31537E 10 28 8.71147E+10 1.61513E+11 1.32371E-10 29 8.60210E+10 1.60324E+11- 1.30G865-10 30 8.58352E+10 1.60242E+11 1.30678E-10 31 0.52711E+10 1.50007E+11 1.29997E-10 32 0.58240E+10 1.58580X+11 1.307102-10 33 8.56617E+10 1.57633E+11 1.306323-10 M Vy&J& @ ~ T d i Lifl fN ' ' '
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_. _. . u . <.m_-.- . . .-_ . . . . . . - - - - 1 l Table .4.2.2.8 i l Downconer Fluxes and DPA Rates j 1 (At the Azial Core Midplane r=278.10cm,m=239.93ca) FLUI FLUX DPA/s 8 (E>1.0 MEV) (E>0.1 NIV) 34 8.44549E+10 1.54101E+11 1.285725 10 35 7.96374E+10 1.45294E+11 1.213545 10 36 - 7.45f)15+10 1.36650E+11 1.137645 10 37 7.17556E+10 1.31872E+11 1.09524E 10 38 6.987365+10 1.28369E+11 1.06779E 10 39 6.94984E+10 1.26821E+11 1.06073E 10 40 6.91849E+10 1.25703E+11 1.05689E 10 41 7.01579E+10 1.263775+11 1.071035 10 42 7.05008E+10 1.267975+11 1.07610E-10 43 7.03974E+10 1.26632E+11 1.07481E-10 44 7.16462E+10 1.29047E+11 1.09300E 10 45 7.41121E+10 1.34575E+11 1.132015 10 46 7.74922E+10 1.41600E+11 1.183765-10 47 8.42162E+10 1.54741E+11 1.28425E 10 48 9.25277E+10 1.71709E+11 1.410705 10 49 1.03429E+11 1.93529E+11 1.57465E-10 50 1.23113E+11 2.335085+11 1.87548E 10 51 1.470875+11 2.82931E+11 2.251865-10 52 1.60869E+11 3.10922E+11 2.45522E-10 53 1.G45283+11 3.19827E+11 2.51609E 10 54 1.72128E+11 3.34293E+11 2.62819E-10 55 1.80833E+12 3.50605E+11 2.74798E-10 56 1.860065+11 3.60724E+11 2.811465-10 57 1.88362E+11 3.65503E+11 2.83826E 10 58 1.87798E+11 3.656585+11 2.83'009E 10 59 1.85903E+11 3.63339E+11 2.80460E 10 60 1.86334E+11 3.64391E+11 2.80901E-10 L- ,
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Table 4.2.2.3 Cavity Fluxes and DPA Rates r=398.70cm 4 FLUE FLUX DPA/s 8 (R>1.0 MEv) (E=0.1 NEv) s=282.602cm s=279.554cm s=279.554cm 1 $.19479E+07 2.54473E+08- 1.159635 13
- 2 5.231485+07 2.54803E+08 1.16678E 13 3 5.25180E+07 2.547165+08 1.16829E 13 l 4 5.25311E+07' 2.54611E+08 1.16871E 13
, 5 5.22965E+07 2.543475+08 1.16500E 13 i 6 5.191175+07 2.54130E+08 1.159323 13 7 5.16546E+07 2.54200E+08 1.155615 13 8 5.15872E+07 2.54302E+08 1.15476E-13 9 5.16924E+07 L.54459E+08 1.156665 13 10 5.17694E+07 2.54532E+08 1.15798E 13 11 5.19453E+07 2.547065+08 1.16085E 13 12 5.21545E+07 2.549485+08 1.16451E-13 13 5.21079E+07 2.55045E+08 1.16495E-13 14 5.22074E+07 2.55037E+08 1.16583E 13 l 15 5.21325E+07 2.55065E+08 1.164283 13 16 5.19375E+07 2.554175+08 1.16169E-13 17 5.20797E+07 2.56622E+08 1.165423-13 18 5.30672R+07 2.59465E+08 1.18321E-13 , 19 5.41511E+07 2.62516E+08 1.203015 13 l 20- 5.46691E+01 2.64710E+08 1.21318E 13 i 21 5.535075+07 2.67316E+08 1.22525E-13 l 22 5.571465+07 2.69311E+08 1.23,285E-13 23 5.63417E+07 2.72255E+08 1.24544E 13 24 5.76811E+07 2.76394E+08 1.26972E-13 25 5.86674E+07 2.79530E+08 1.28817E-13 26 5.99887E+07 2.83705E+08 1.31185E-13 27 6.14913E+07 2.889085+08 1.33943E-13 28 6.265573+07 2.93103E+08 1.36141E 13 29 6.356375+07 2.96182E+08 1.37841E-13 30 6.39799E+07 2.97893E+08 1.38675E-13 31 6.43432E+07 2.933475+08 1.39383E-13
+
324 - 6.482875+07: o i 3.01374E+08 - 1.40330E-13 33 6.52671E+07 3.02902E+08 1.41128E-13 !~ 3 .
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J Tabb 4.2.2.9 , Cavity Fluzes and DPA Rates (cont'd) r=398.70cm FLUI FLUE DPA/s z 283.602cm s=279.554cm s=279.554cm 8 (E>1.0 MIV) (E>0.1 MEV) 34 6.60600E+07 3.059565+08 1.426395 13 35 6.73731E+07 3.10LW2E+0B 1.45063E 13 36 6.85195E+07 3.14241E+08 1.47140E 13 37 6.929785+07, 3.16764E+08 1.48588E 13 38 7.00342E+07 3.19020E+08 1.49946E 13 39 7.08230E+07 3.21431E+08 1.51384E 13 40 7.14632E+07 3.23735E+08 . 1.52599E 13 41 7.20260E+07 3.25909E+08 1.53666E 13 42 7.24539E+07 3.27801E+08 1.544843-13 43 7.28179E+07 3.29240E+08 1.55127E 13 44 7.30954E+07 3.30948E+08 1.55744E 13 45 7.38825E+07 3.34326E+08 1.57261E 13 46 7.45634E+07 2.37075E+08 1.58548E 13 47 7.56717E+07 3.40485E+08 1.60521E 13 48 7.692373+07 3.44192E+08 1.627725 13 49 7.802993+07 3.47575E+08 1.647213 13 50 7.91807E+07 3.51918E+08 1.66792E-13 51 8.00746E+07 3.55983E+08 1.68482E 13 52 8.05541E+07 3.5810SE+08 1.69392E 13 53 8.06036E+07 3.58805E+08 1.69537E 13 54 8.00069E+07 3.60049E+08 1.699545 13 55 0.12391E+07 3.61605E+08 1.70733E*13 56 8.170685+07 3.62700E+08 1.71549E-13 57 8.25914E+07 3.64401E*08 1.73009E 13 58 8.32210E+07 3.65700E+08 1.74101E-13 59 8.33420E+07 3.659995+08 1.74314E 13 60 8.36596E+07 3.66444E+08 1.74711E 13
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1
l 1 Table 4.2 A10 ' Fluz Spectrum At Pressure vessel 4 42.51' s 306.605cm s=306.605cm =306.605cm s=302.795cm s=302.795cm Group 0T 1/4 T 1/2 T 3/4 T T 1 1.45144E+06 8.51140E+05 4.55280E+05 2.40675E+05 1.45519E+05
, 2 3.98221E+06 2.31806E+06 1.22421E+06 6.36146E+05 3.78330E+05 3 1.38250E+07 0.07480E+06 4.24131E+06 2.180185+06 1.28286E+06 4 2.429495+07 1.43174E+07 7.48060E+06 3.80477E+06 2.21551E+06 5 3.66752E+07 2.14025E+07 1.09403E+07 5.435585+06 3.10342E+06 6 0.05306E+07 5.02178E+07 2.46778E+07 1.17776E+07 6.51670E+06 7 1.10113E+0B 6.15821E+07 2.99427E+07 1.41802B+07 7.758995+06 0 1.62710E+C8 9.10256E+07 4.47425E+07 2.14402E+07 1.16773E+07 9 1.012565+08 -5.89232B+07 -3.0[845E+07 1.499375+07 8.21885E+06 ,
10 6.86134E+07 4.220075+07 2.23501E+07 1.13156E+07 6.170163+06 11 7.33791E+07 4.620CSE+07 2.49657E+07 1.28534E+07 7.03824E+06 12 3.506765+07 2.24949E+07 1.23057E+07 6.381375+06 3.51085E+06 13 0.65360E+06 5.77535E+06 3.26255E+06 1.73874E+06 9.03372E+05 14 4.33860E+07 2.93996E+07 1.67870E+07 9.01552E+06 5.06771E+06 15 1.12498E+08 7.99966E+07 4.72184E+07 2.581965+07 1.43668E+07 16 1.15850E+08 8.92594E+07 5.62290E+07 3.22770E+07 1.83726E+07 17 1.549775+08 1.24302E+08 8.12742E+07 4.80871E+07 2.792810+07 18 2.39865E+08 2.18249E+00 1.580865+08 1.00680E+08 5.98535E+07 19 1.45214E+08 1.36801E+00 1.04883E+08 7.100785+07 4.46924E+07 20 7.61680E+07 7.03784E+07 5.35826E+07 3.57649E+07 2.20858E+07 21 2.23453E+08 2.53669E+08 2.20689E+08 1.59703E+08 9.84222E+07 22 1.47690E+0B 1.54698E+08 1.33078E+08 9.02825E+07 6.50064E+07 23 1.89661E+08 2.16406E+08 1.92411E+08 1.39829E+08 8.37832E+07 24 1.81696E+08 2.21221E+08 2.09219E+08 1.59934E+08 9.98713E+07 25 1.91614E+08 1.91157E+08 1.65710E+08 1.24799E+08 8.53724E+07 26 2.04774E+00 2.31926E+08 2.14825E+0B 1.65236E+08 1.07721E+08 27 1.517985+08 1.70517E+08 1.59753E+08 1.22859E+08 7.91146E+07 28 9.13819E+07 7.00000E+07 6.47475E+07 4.84103E+07 3.30616E+07 29 3.36533E+07 2.28332E+07 1.75979E+07 1.28947E+07 8.89195E+06 30 2.21608E+07 1.23030E+07 9.40842E+06 5.89944E+06 6.27014E+06 31 4.314365+07 4.53749E+07 3.99941E+07 3.148065+07 2.24942E+07 32 2.331475+07 2.36310E+07 2.12C53E+07 1.70020E+07 1.21623E+07 33 4.82868E+07 3.97948E+07 3.19665E+07 2.47100E+07 1.86002E+07 34 7.98184E+07 3.97861E+07 2.53249E+07 1.896195+07 1.81539E+07 35 1.21562E+08 9.64862E+07 6.91251E+07 4.67343E+07 3.13456E+07 36 1.054275+00 7.91381E+07 5.57745E+07 3.72227E+07 2.47032E+07 37 1.57190E+08 1.041275+08 6.808365+07 4.46165E+07 3.22886E+07 38 9.41541E+07 5.92006E+07 3.72325E+07 2.40360E+07 1.75710E+07 39 9.61211E+07 6.22106E+07 3.84200E+07 2.421995+07- 1.72371E+07 40 1.272S1E+00' 8.251965+07 5.04327E+07. 3.11393E+07 2.17334E+07
~
41' 1.53565E+08 ' 9.53296E+07 5.65150E+07 '3.41860E+07' 2.418485+07 42' 8.80941E+07 5.14179E+07 2.94949E+07- 1.75775E+07 1.28650E+07
-43 1.12239E+08 5.66321E+07 2.93236E+07 1.72131E+07 1.40101E+07
'44 0.17431E+07 3.54910E+07 1.63386E+07 9.37243E+06 8.66707E+06 45 7.43535E+07 2.38461E+07 8.91602E+06 5.00614E+06 6.29555E+06 46 1.575075+00 3.28214E+07 7.809085+06 4.51151E+06 1.14895E+07
- 47 1.08202E+09 7.03264E+07 4.63913E+06 2.21562E+06' 2.713575+07:
,e , , N -y-N $ph ,
9 up*- 3 x 3% . . < gg r* q.4, * ,(N , , ,.. g , 4 $ Q[kfe
.O Whjf*
- diT/i i U nA4 5 '* 6 ' ' - N T-df d) d s r -
k / $ M%: d['
Table 4.2.2.11 Flux Spectrum at the Downcomer, Capsule and Cavity Group Downcomer Pressure Vessel Cavity Capsule 1 3.06440E+07 1.20397E+06 8.82735E+04 2 9.94113E+07 3.21690E+06 2.22049E+05 3 4.34619E+0B 1.06770E+07 7.27237E+05 4 8.69995d+08 1.84146E*07 1.22673E+06 5 1.57902E+09 2.71738E+07 1.67074E+06 6 4.24337E+09 6.54588E+07 3.42529E+06 7 6.44469E+09 8.01483E+07 4.00089E+06 8 1.18478E+10 1.15285E+08 5.85934E+06 9 8.28758E+09 7.12901E+07 4.01597E+06 10 5.72389E+09 4.74982E+07 2.94413E+06 11 6.28604E+09 5.03231E+07 3.34623E+06 12 3.01237E+09 2.38313E+07 1.71368E+06 13 7.812765+08 5.80002E+06 4.71627E+05 14 3.72442E+09 2.93640E+07 2.34469E+06 15- 8.89692E+09 7.66362E+07 6.17582E+06 16 8.93241E+09 7.85537E+07 7.88597E+06 4 17 1.19526E+10 1.03870E+08 1.22991E+07 18 1.59615E+10 1.57156E+08 2.50803E+07 19 1.00176E+10 9.33834E+07 1.96089E+07 - 20 5.75172E+09 4.87374E+07 1.08405E+07 21 1.06772E+10 1.36337E+08 3.84548E+07 22 9.47762E+09 8.96021E+07 3.03620E+07 23 1.05198E+10 1.14643E+0B 3.41054E+07 24 8.27485E+09 1.05726E+08 4.09960E+07 25 1.52337E+10 1.14367E+08 4.93562E+07 26 1.28278E+10 1.20772E+08 5.058485+07 27 1.08677E+10 8.91329E+07 3.761395+07 28 9.59758E+09 5.37322E+07 2.22784E+07 29 4.47478E+09 1.89532E+07 7.16805E+06 30 3.46514E+09 1.08276E+07 7.45577E+06 31 1.28394E+09 2.57457E+07 1.00461E+07 l 32 1.69532E+09 1.37871E+07 6.53739E+06 33 6.21169E+09 3.12861E+07 1.40931E+07 34 1.19938E+10 4.56788E+07 1.82946E+07 35 1.17352E+10 7.63772E+07 2.03678E+07 36 1.17072E+10 6.39967E+071 1.76332E+07 37 1.951275+10 9.43503E+^' 2.58626E+07 38 1.18174E+10 5.64554E+07 1.41391E+07
-39 1.18917E+10 5.81865E+07 1.35024E+07 40 1.59635E+10 7.70609E+07 1.68843E+07 41 2.01242E+10 9.25460E+07 1.92489E+07 ~
42 1.21640E+10 5.27821E+07 z 1.06510E+07 43 1.70609E+10 6.63114E+07 _1.27264E+07 44 1.36351E+10 4.76412E+07 ~ 8.62314E+06' 45 1.49940E+10 4.14.8975+ 07 7.54572E+06 46 4.18799E+10 0.56534E+07 1.71394E+07 47 7.26301E+11 5.95337E+08 5.50658E+07 Downoomer flux spectrum is at r=278.10can,s=306.605ca,8=23.5.3 y + -Pressure vessel Capsule flux' spectrum,is at r=319.195ca,s=306.605ca,t=3.-
. Cavity flux spectrum'is at r=398.70cm.s=282.602ca,8=44.975..
, + < n y.gf y ; % .
. .p ,
3 , .
~
11 ' '
< y, n;f 4 < - : . % Q Q @!M6 ,* %> i y9 j g , ,g g g,g ,, 4 ,
t Table 4.2.2.12 Calculated Reaction Rates (reactions /sec* atom) at the Capsule
. Detector . . . . .
. Material . r=318.348cm . r=319.195cm . r=320.041cm . r=320.887cm .
. 46 . -17 . 17 . -17 . 17 .
.Ti (n.p) . 4.19811110- . 3.70240x10 . 3.22615x10 . 2.78949x10 .
. 54 . -16 . 16 . -16 . 16 .
.F3 (n,p) . 1.81953I10
. 1.61912x10 , 1.41706x10 . 1.22869x10 .
.- 58 , -16 . - -16 . 16 .- -16 ..
.ti (u,p) . ' 2.32589110 . 2.07686x10 . 1.82386x10 . 1.58472x10 .
. 63 . 18 . ' 18 . 18 . 18 .
.Cu (n s(), . 2.89411x10 . 2.54905x10 . 2.22507x10 , 1.92927x10 .
. 237 . -15 . -15 . 15 . -15 .
.Np (n, f) . 2.10361x10 . 2.03505x10 . 1.90963x10 . 1.76904x10 .
. 238 . -16 . -16 . -16 . 16 .
.U (n f) . 5.04572x10 . 4.65176x10 . 4.17612x10 . 3.71114x10 .-
CUGLE93 used pressure vessel 1/4T weighting spectrum to collapse cross ( costions. l 46 Te (n,p) axial peak reaction rate at s=302.795cm l ' l 54
- Fa - -(n p)- axial peak reaction rats at: s=302.795cm 58 C1 (n p) axial peak reaction rate at s=302.795cm 63 Cu (n e() axial peak reaction rate at s=302.795cm 237 Mp (n,f) axial peak reaction rate at n=306.605cm 238. m -- . . ,.
- i U -(n,f)1 axial peak reaction rate at s=306'605cm .
, pb ,
s
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F%ure 4.2.2.1 PRESSURE VESSEL 0-T FLUX SPECTRUM
. m _. . . . . . . ...........m. ...m. .....m. . . .... . . . . . . . . . . . . . . ..m.. .....m. . . ....m.
1d . . y . m
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gs . 8 4 c- 4
,,. gegg , pn ,, e s 3:f sg.m dQgJggs. g, 7.x
, c,h u.w; c9.; ;
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- hi. / -'e
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y
f a Figure 4,2.2.2 PRESSURE VESSEL 4 T FLUX SPECTRUM
, , ,,,i., , , , . . . , . ,,,,,,,m ,.....m ,,,,,m, , . . . . . . , , , , , . . . . , , , , , , , , , , , , , , . , , , , , , , , , , . , , , , , , , , , , , , , , , , , ,
e 1d- - 1
- Lr :
[ 1 1 y - I
~
. Q id-. . -
ti 2 I J - I 16 - - 3+10' , , . . . . , , ,,,,,,,,,,,,,..,, ,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,m,, ,,,,,,,,,,,,,,,,,
' 10-' 10-' ,,,,,,,,*,,,,,,,,,',,,,,,,s?
-10~ - 10~ ' 10- =18; .1d . 16: -16 16' 16 1d . 16
+ - < >
4 . ,. - , 9 1 + h ,- +.. , a 'h (
' 8
. - ._ ' j ,"
a
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,,_9, _3_
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.~ ._ j,(;
- < , g . a- ;~,>,.
- ri t h x fg,.,
,r. > > ; :+- n, ,. . __
u
Figure 4.2.2.3 PRESSURE VESSEL 2 T FLUX SPECTRUM
. . .. . . . . .....m.. . . o m.m ..oom . . o o.. . . o . . e. . . o m .. ...om- i . . " .e . > > o .m. . . o "a ....u-..
18 : : 3 - ( - 7 b 1d: _
~
9 3 . J .
. @ 16: .
s2._
- 16. :
4 10' . . . ' .". ..~s - . ""m '"m - * ' 4 1g* m 11"d." . . . 10,
", 3 "16, ' " ."10-' 16 ' " ,16 " " ,d 1 e 11 6 1d ""1Cf - ' ""6 -1 ' ' " "'6
-1
. .c gggy g h . -{ '
2-4
^
- s-4-f 6
# (- -
. . - I -,
x
' ' ~
f . at % ,
+
M@ Wow -
.m .g+am ,
_ a' e ::Hipahdigegsar ppg % y:jf$pssdfdwrip- . '< 1;v > + *
- Mi@ ibilimi#s # 4 W hM$t.$ M M R 4 t W '
m .
Figure 4.2.2.4 PRESSURE VESSEL 3 4 T FLUX SPECTRUM 1d y , o . u m. , , , , o m. , o mo. , , m o ... . . . . u m. .o...... . o o.e . u mm. . o u mi , o o .m. , o o m., . o o..m _ g - 11 : - 7- - 8 E N 3 d ' 10': : R p 16 _ : S > 2 10 .
. . . . . , " . ....,*.. mms *....~...'..."".. . . " . . . . ."~i .
- 10-* 10 10- 1G- 10- 16 . . o . ,d 1
1d'. . " ",6 1
. . ",6 1 - 16- . " 1. "@ . " " ."61-a -
ggg -
~ t i t ?
._.y;_ .g
/ %
f'- p' k_ % ( e,*d 4 y*
- il} %* s j '
[4 fi *e ;
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