ML17114A371

Errata for BWRVIP-271NP: BWR Vessel and Internals Project, Testing and Evaluation of the Browns Ferry, Unit 2, 120 Degree Capsule

ML17114A371
Person / Time
Site:	Browns Ferry, PROJ0704
Issue date:	04/20/2017
From:	McGehee A O Electric Power Research Institute
To:	Document Control Desk, Office of Nuclear Reactor Regulation
References
2017-046, BWRVIP-271NP
Download: ML17114A371 (72)

Text

ELECTRIC POWER RESE A RCH INSTITUTE 2 017-046 _______________

BWR Vessel & Internals Project (BWRVIP) April 20 , 2017 Document Control Desk U. S. Nuclear Regulatory Commission 11555 Rockville Pike Rockville , MD 20852 Attention:

Reference:

Joseph Holonich Project No. 704-Errata for BWRVIP-271NP:

BWR Vessel and Internals Project , Testing and Evaluation of the Browns Ferry Unit 2 120° Capsule l. BWRVIP-271NP

BWR Vessel and Internals Project , Testing and Evaluation of the Browns Ferry Unit 2 120° Capsule. EPRl , Palo Alto , CA: 2014. 3002000078.

2. BWRVIP Letter 2013-056 , " Project No. 704-BWRVIP-271NP

BWR Vessel and Internals Project , Testing and Evaluation of the Browns Ferr y Unit 2 120° Capsule", dated April 17 , 2013. 3. BWRVIP Letter 2014-043 , " Project No. 704-Errata for BWRVIP-271NP:

BWR Vessel and Internals Project , Testing and Evaluation of the Browns Ferr y Unit 2 120° Capsule ," dated April 1 , 2014. The purpose of this letter is to notify you of errata regarding BWRVIP-271NP

[1]. This report was transmitted to the NRC on April 17 , 2013 [2]. Earlier identified errata were corrected and transmitted to the NRC on April 1 , 2014 [3]. During an internal EPRl review , BWRVIP-271NP was discovered to contain the following editorial error:

• Section 3.3.1 , Page 3-20 -" Fluence values are also calculated and reported in Section 3.4.2 .... " should be " Fluence values are also calculated and reported in Section 3.3.2 ... " This errata is editorial in nature and has no impact on plant safety or on any evaluations or conclusions contained in this report. Further , this errata will have no impact on any plant specific evaluations which have made use of the integrated surveillance program (ISP) data contained in this report. Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 Hillview Avenue , Palo Aho , CA 94304-1395 USA* 650.855.2000 *Customer Se r vice 800.313.3774

• www.epr i.com BWRVIP 2017-046 Enclosed are five (5) corrected paper copies of BWRVIP-271NP.

The correction is reflected in page 3-20. As with the original transmittal , this report is being transmitted to the NRC for information only. Please note that the enclosed report is non-proprietary and is available to the public by request to EPRI. If you have any questions regarding this subject , please contact Drew Odell (Exelon , BWRVIP Integration Committee Technical Chairman) by telephone at 610.765.5483 or by e-mail at andrew.odell

@exeloncorp.com. Sincerely , Andrew McGehee , EPRI, BWRVIP Program Manager Tim Hanley , Exelon, BWRVIP Chairman c: D. Rudland , NRC D. Odell , Exelon N. Palm , EPRI R. Carter , EPRI A. McGehee , EPRI C. Wirtz , EPRI G. Haliburton , TV A 2 ELECTRIC POWER -=*-RESEARCH INSTITUTE 2013 TECHNICAL REPORT BWRVIP-271 NP: BWR Vessel and Internals Project Testing and Evaluation of the Browns Ferry Unit 2 120° Capsule PREPARED UNDER THE N U CLEAR

• PROGRAM ELECTRIC POWER RESEARCH INSTITUTE April 18 , 2017 TO: Recipients of EPRI 3002000078 (BWRVIP-271 NP , April 2013)

SUBJECT:

Correction to page 3-20 of EPRI 3002000078 , BWRVIP-271 NP: BWR Vessel and Internals Project , Testing and Evaluation of the Browns Ferry Unit 2 120° Capsule. Our records indicate that you received the subject EPRI product by order or download prior to April 10 , 2017. The following correction has been made to this technical report: In the originally published version of this report on page 3-20 , Section 3.3.1 , the second sentence reads: Fluence values are also calculated and reported in Section 3. 4. 2 for each of the capsule flux wires. The referenced section should have been Section 3.3.2. Fluence values a r e also calculated and reported in Section 3.3.2 for each of the capsule flux wires. Page 3-20 has been updated to reflect the correction and the technical report is available for download when you log into EPRl.com at: h tt p://epri.co/000000003002000078. Together ... Shaping the Future of Electricity PALO ALTO OFFICE 34 20 Hillv i ew A ve nu e, Pal o A l t o , CA 94304-1 338 US A

• 650.855.2000

• Custome r Serv i ce 800.3 1 3.377 4

• www.epri.c o m BWRVIP-271 NP: BWR Vessel and Internals Project Testing and Evaluation of the Browns Ferry Unit 2 120° Capsule 3002000078 Final Report , April 2013 EPRI Project Manager R. Carter Work to de velop th i s product was compl e ted under the EPRI Nuclear Qua l ity Assurance Program i n c omp l iance w it h 10 CF R 50 , App e ndi x Band 10 CFR 21 , 'NO ELECTR IC POW E R RESEARCH I NST ITU TE 3420 Hillview Avenue, Palo A l to , Califo rn ia 94304-1338

• PO Box 10412 , P a l o Alto , Cal i fornia 94303-0813 *U SA 800.3 1 3.3774

• 650.855.212 1

• askepr i@ep r i.com

• www.ep r i.com DISCLAIMER OF WARRANTIES AND LIMITATION OF LIABILITIES THIS DOCUMENT WAS PREPARED BY THE ORGANIZATION(S)

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OR (B) ASSUMES RESPONSIBILITY FOR ANY DAMAGES OR OTHER LIABILITY WHATSOEVER (INCLUDING ANY CONSEQUENTIAL DAMAGES , EVEN IF EPRI OR ANY EPRI REPRESENTATIVE HAS BEEN ADVISED OF THE POSSIBILITY OF SUCH DAMAGES) RES UL TING FROM YOUR SELECTION OR USE OF THIS DOCUMENT OR ANY INFORMATION , APPARATUS , METHOD , PROCESS , OR SIMILAR ITEM DISCLOSED IN THIS DOCUMENT.

REFERENCE HEREIN TO ANY SPECIFIC COMMERCIAL PRODUCT, PROCESS , OR SERVICE BY ITS TRADE NAME , TRADEMARK , MANUFACTURER , OR OTHERWISE, DOES NOT NECESSARILY CONSTITUTE OR IMPLY ITS ENDORSEMENT , RECOMMENDATION , OR FAVORING BY EPRI. THE FOLLOWING ORGANIZATION PREPARED THIS REPORT: Electric Power Research Institute (EPRI) MP Machinery

& Testing, LLC TransWare Enterprises Inc. THE TECHNICAL CONTENTS OF THIS DOCUMENT WERE PREPARED IN ACCORDANCE WITH THE EPRI NUCLEAR QUALITY ASSURANCE PROGRAM MANUAL THAT FULFILLS THE REQUIREMENTS OF 10 CFR 50 APPENDIX B , 10 CFR PART 21 , ANSI N45.2-1977 AND/ OR THE INTENT OF IS0-9001 (1994). CERTIFICATION OF CONFORMANCE CAN BE OBTAINED FROM EPRI. BEFORE THE CONTENTS OF THIS DOCUMENT CAN BE APPLIED TO FULFILL QUALITY PROGRAM REQUIREMENTS, CONTRACTUAL ARRANGEMENTS BETWEEN THE USER AND EPRI MUST BE ESTABLISHED. USE OF THE CONTENTS OF THIS DOCUMENT IN NUCLEAR SAFETY OR NUCLEAR QUALITY APPLICATIONS MAY ALSO REQUIRE FURTHER ACCEPTANCE REVIEWS/ACTIONS PURSUANT TO USER'S INTERNAL PROCEDURES. NOTE For further information about EPRI , call the EPRI Customer Assistance Center at 800.313.3774 or e-mail askepri@epri.com. Electric Power Research Institute , EPRI , and TOGETHER ... SHAPING THE FUTURE OF ELECTRICITY are registered service marks of the Electric Power Research Institute , Inc. Copyright© 2013 Electric Power Research Institute , Inc. All rights reserved.

ACKNOWLEDGMENTS T h e following organizations prepared this report: E l ectric Power Research Institute (EPRI) 3420 Hillview Ave Palo Alto, CA 94304 Principal Investigators T. Hardin M. O'Connor MP Machinery

& Testing, LLC 2161 Sandy Drive State College, PA 16803 Principal Investigator Dr. M. P. Manahan, Sr. Trans Ware Enterprises Inc. 1565 Mediterranean Drive Sycamore, IL 60178 Pr i ncipal Investigator E. N. Jones This report describes research sponsored by EPRI and its BWRVIP participating members. This publication is a corporate document that should be cited in the literature in the following manner: BWRVIP-27 JNP: BWR Vessel and Internals Proj e ct, Testing and Evaluation of th e Browns Ferry Unit 2 120° Capsule. EPRI, Palo Alto, CA: 2013. 3002000078.

111 PRODUCT DESCRIPTION In the late 1990s, a Boiling Water Reactor Vessel and Internals Project (BWRVIP) Integrated Surveillance Program (ISP) was developed to improve the survei ll ance of the U.S. BWR fleet. This report describes testing and eva lu ation of the Browns Ferry Unit 2 120° capsule. These result s wi ll be used to monitor embritt l ement as part of the BWRVIP ISP. Background The BWRVIP ISP represents a major enhancement to the process of monitoring e mbrittlement fo r the U.S. fleet of BWRs. The ISP optimizes surveillance capsule tests while at the same time maximizing the quantity and quality of data , thu s resulting in a more cost-effective program. The BWRVIP ISP provides more representative data that can be used to assess embrittlement in reactor pressure vessel beltline materials and improve trend curves in the BWR range of irradiation conditions. Challenges and Objectives Neutron irradiation exposure reduces the toughness of reactor vessel steel plates , welds, and forgings.

The objectives of this project were twofold:

• To document the results of neutron dosimetry and Charpy V-notch ductility test s for the surveillance materials (plate heat A0981-1 and weld heat BF2 ESW) in the Browns Ferry Unit 2 120° capsule

• To compare the resu lt s with the embrittlement trend prediction of the U.S. Nuclear Regulatory Commission (U.S. NRC) Regulatory Guide 1.99 , Rev. 2 Approach The Browns Ferry Unit 2 120° capsule had been irradiated in the reactor since plant startup. The surveillance capsule contained flux wires for neutron flux monitoring , Charpy V-notch impact test specimens, and tensile specimens.

The project team removed the capsule from the reactor in 2011 and tran s ported it to facilities for testing and evaluation.

The team used dosimetry to gather information about the neutron fluence accrual of spe cimens from the capsule. They then perfonned a neutron transport calculation in accordance with Regulatory Guide 1.190 and compared it to the results from the dosimetry.

Testing of C harp y V-notch specimens was performed according to the American Society for Testing and Materials (ASTM) standards.

Results and Find i ngs The report includes capsule neutron exposure and Charpy V-notch test results for Browns Ferry 2 surveillance plate heat A0981-1 and surveillance weld BF2 ESW (an electroslag weld of unknown heat number). The project compared irradiated Charpy data to unirr a diated data in order to determine the shifts in Charpy index temperatures for the surveillance plate and weld materials due to irradiation.

For the surveillance plate , results indicate a shift about 32% higher v than the prediction of Regulatory Guide 1.99, Revision 2, but within (predicted shift+ margin). For the weld, the shift was about 2.3 times higher than the predicted shift and about 15% higher than (predicted shift+ margin). Researchers also measured flux wires and determined fluence for the capsule. Applications, Value, and Use Results of this work will be used in the BWRVIP ISP that integrates individual BWR surveillance programs into a single program. The ISP provides data of high quality to monitor BWR vessel embrittlement.

The ISP results in significant cost savings to the BWR fleet and provides more accurate monitoring of embrittlement in BWR vessels. Keywords BWR Charpy testing Mechanical properties Radiation embrittlement Reactor pressure vessel integrity Reactor vessel surveillance program Vl CONTENTS 1 INTRODUCTION

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............... 1-1 1.1 Implementat i on Requirements

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1-1 2 MATERIALS AND TEST SPECIMEN DESCRIPTION

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2-1 2.1 Dosimeters

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..................... 2-1 2.2 Charpy V-Notch Specimens

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........................................................ 2-1 2.2.1 Capsule Loading Inventory

.................................................................................... 2-1 2.2.2 Material Descr i ption and Properties

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.............................. 2-4 2.2.3 Chemical Composition

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2-5 2.2.4 CVN Baseline Properties

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................................................................... 2-5 2.3 Capsule Opening ...........................................

.............................................................. 2-12 3 NEUTRON FLUENCE CALCULATION

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3-1 3.1 Description of the Reactor System ............................

.................................................... 3-2 3.1.1 Reactor System Mechanical Design ....................................................................... 3-2 3.1.2 Reactor System Material ....................

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.................................................... 3-4 3.1.3 Reactor Operating Data Inputs ....................

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................................................. 3-5 3.1.3.1 Core Load i ng ........................

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........................................... 3-6 3.1.3.2 Power History Data ..........................

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3-6 3.1.3.3 Reactor State-Point Data ................

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........................................ 3-8 Beginning of Operation through Cycle 16 State Points ............................................... 3-8 Projected Reactor Operat i on ..........................

............................................................ 3-8 Limitation of Fluence Projections

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............................................ 3-9 3.2 Calculation Methodology

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.......................... 3-10 3.2.1 Description of the RAMA Fluence Methodology

................................................... 3-10 3.2.2 The RAMA Geometry Model for the Browns Ferry 2 Reactor ............................... 3-11 3.2.2.1 The Geometry Model .......................................

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........... 3-14 3.2.2.2 The Reactor Core and Core Reflector Models .............................................. 3-15 V II _J 3.2.2.3 The Core Shroud Model ............................................................................... 3-16 3.2.2.4 The Downcomer Region Model .................................................................... 3-16 3.2.2.5 The Jet Pump Model .................................................................................... 3-16 3.2.2.6 The Surveillance Capsule Model .................................................................. 3-16 3.2.2. 7 The Reactor Pressure Vessel Model ............................................................ 3-17 3.2.2.8 The Vessel Insulation Model. ........................................................................ 3-17 3.2.2.9 The Inner and Outer Cavity Models .............................................................. 3-17 3.2.2.10 The Biological Shield Model ....................................................................... 3-17 3.2.2.11 The Above-Core Component Models ......................................................... 3-17 The Top Guide Model .............................................................................................. 3-17 The Core Spray Sparger Model. ................

............................................................... 3-18 3.2.2.12 The Below-Core Component Models .......................................................... 3-18 3.2.2.13 Summary of the Geometry Modeling Approach .......................................... 3-18 3.2.3 RAMA Calculat i on Paramete r s ............................................................................. 3-18 3.2.4 RAMA Neutron Source Calculation

...................................................................... 3-19 3.2.5 RAMA Fission Spectra ......................................................................................... 3-19 3.3 Surveillance Capsule Activation and Fluence Results ................................................. 3-19 3.3.1 Compar i son of Predicted Activation to Plant-specific Measurements

................... 3-20 3.3.1.1 Cycle 1 30° Flux Wire Holder Activation Analysis ......................................... 3-20 3.3.1.2 Cycle 7 30° Surveillance Capsule Activation Analysis ..................................

3-21 3.3.1.3 Cycle 16 120° Surveillance Capsule Activation Analysis .............................. 3-21 3.3.1.4 Surveillance Capsule Activation Analysis Summary ..................................... 3-22 3.3.2 Capsule Peak Fluence Calculations and Lead Factor Determinat i ons ................. 3-23 3.4 Capsule Fluence Uncertainty Analysis .........................................................................

3-23 3.4.1 Comparison Uncertainty

....................................................................................... 3-24 3.4.1.1 Operating Reactor Comparison Uncertainty

................................................. 3-24 3.4.1.2 Benchmark Comparison Uncerta i nty ............................................................ 3-24 3.4.2 Analytic Uncertainty

............................................................................................. 3-24 3.4.3 Combined Uncertainty

.......................................................................................... 3-25 4 CHARPY TEST DATA .............

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4-1 4.1 Charpy Test Procedure

................................................................................................. .4-1 4.2 Charpy Test Data .......................................................................................................... 4-2 V lll 5 CHARPY TEST RES UL TS .....................................................................

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5-1 5.1 Analysis of Impact Test Results ..................

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5-1 5.2 Irradiated Versus Unirradiated CVN Properties

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.............. 5-1 6 REFERENCES

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6-1 A APPENDIX A-DOSIMETER ANALYSIS ...........................................................................

A-1 A.1 Dosimeter Material Description

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.......................... A-1 A.2 Dosimeter Cleaning and Mass Measurement..

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A-1 A.3 Radiometric Analysis ..........

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........................................................ A-4 I X LIST OF FIGURES F i gure 2-1 Photog r aph of 120° capsule for Browns Fe rr y Unit 2 showing positive i dentification markings ...................................................................................................... 2-3 Figure 2-2 Schematic drawing showing the locations of test spec i mens in the Browns Ferry Unit 2 120° surveillance capsule ............................................................................. 2-4 Figure 2-3 Browns Ferry 2 plate A0981-1 (LT) unirradiated Charpy energy plot.. ..................... 2-8 Figure 2-4 Browns Ferry 2 weld BF2 ESW unirradiated Charpy energy plot .......................... 2-10 Figure 3-1 Planar view of Browns Ferry 2 at the core mid-plane elevation

............................... 3-3 Figu r e 3-2 P l anar v i ew of the Browns Ferry 2 RAMA quadrant model at the core mid-plane elevation

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............................................................ 3-12 Figure 3-3 Axial view of the Browns Ferry 2 RAMA model ..................................................... 3-13 Figure 4-1 Illustration of digital opt i cal comparator measurement of shear fracture area ......... .4-2 Figure 5-1 Irradiated plate A0981-1 (Browns Ferry 2 120° capsule) Charpy energy plot .......... 5-2 Figure 5-2 Irradiated plate A0981-1 (Browns Ferry 2 120° capsule) lateral expansion plot. ...... 5-3 Figure 5-3 Irradiated weld BF2 ESW (Browns F e rry 2 120° capsule) Charpy energy plot ........ 5-4 Figure 5-4 Irradiated weld BF2 ESW (Browns Ferry 2 120° capsule) lateral expans i on plot ................................................................................................................................... 5-5 Figure A-1 Packet G9 Cu dosime t er wire: prior to clean i ng (left); and after cleaning/coiling (right) ..........................................................................

............................ A-2 Figure A-2 Packet G9 Fe dosimeter wire: prior to clean i ng (left); and after cleaning/coiling (right) ...................................................................................................... A-2 Figure A-3 Packet G9 Ni dosimeter wire: prior to cleaning (left); and after cleaning/coiling (r ight) ..................................................

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............................................ A-2 Figure A-4 Packet G10 Cu dosimeter wire: prior t o clean i ng (left); and after cleaning/coiling (right) ................................................

...................................................... A-3 Figure A-5 Packet G10 Fe dosimeter wire: prior to cleaning (left); and after cleaning/coiling (right) ...................................................................................................... A-3 Figure A-6 Packet G10 Ni dosimeter Wire: prior t o cleaning (left); and after cleaning/coiling (right) ...................................................................................................... A-3 XI LIST OF TABLES Tabl e 2-1 Browns Ferry 2 1 20° surveillance c apsule specimen inventory

................................ 2-2 Table 2-2 Best estimate chemistry of Browns Ferry 2 surveillance plate A0981-1 .................... 2-5 Table 2-3 Best estimate chemistry of Browns Ferry 2 surveillance weld BF2 ESW .................. 2-5 Table 2-4 Unirradiated Charpy impact test data for surveillance plate A0981-1 (LT) ................ 2-6 Table 2-5 Un irrad i ated Charpy impact test data for surveillance weld BF2 ESW ...................... 2-7 Table 2-6 Baseline CVN properties

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................................................... 2-7 Table 3-1 Summary of material compositions by region for Browns Ferry 2 ............................. 3-5 Table 3-2 Summary of the Browns Ferry 2 core loading inventory

........................................... 3-7 Table 3-3 State-po i nt data for each cycle i n Browns Fe r ry 2 .................................................... 3-9 Table 3-4 Comparison of specific activities for Browns Ferry 2 Cycle 1 30° f l ux wire holder wires (C/M) .......................................................................................................... 3-20 Table 3-5 Compari s on of specific activities for Browns Ferry 2 cycle 7 30° surveillance capsule flux wires (C/M) ................................................................................................. 3-21 Table 3-6 Comparison of specific activities for Browns Ferry 2 cycle 1 6 120° surveillance capsule flux wires (C/M) ................................................................................................. 3-22 Table 3-7 Comparison of activities for Browns Fer ry 2 surveillance capsule flux wires ........... 3-22 Table 3-8 Lead fac t ors for Browns Ferry 2 30°, 1 20°, and 300° surve i llance capsules ........... 3-23 Table 3-9 Combined capsule fluence uncertainty for energy >1.0 MeV .................................. 3-25 Table 4-1 Irradiated Charpy V-Notch impact test results for base metal (heat A0981-1) specimens from the Browns Ferry 2 120° surveillance capsule ...................................

.... .4-3 Table 4-2 Irradiated Charpy V-Notch impact test results for weld metal (heat BF2 ESW) specimens from the Browns Ferry 2 120° surveillance capsule ....................................... .4-4 Ta b le 4-3 Irradiate d Charpy V-Notch impact test results for HAZ specimens from the Browns Ferry 2 120° surveillance capsule ....................................................................... .4-4 Ta b le 5-1 Effect of i rradiation (E>1.0 MeV) on the notch toughness properties

........................ 5-6 Table 5-2 Comparison of actual versus predicted embrittlement

.............................................. 5-6 Table 5-3 Percent decrease in upper shelf energy ................................................................... 5-7 Table A-1 Wire dosimeter masses .......................................................................................... A-4 Table A-2 GRSS specifications

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................................................ A-5 Table A-3 Counting schedule for the dosimeter materials

....................................................... A-6 Table A-4 Neutron-i n duced reactions of interes t ..................................................................... A-6 Table A-5 Results of the radiometric analysis ...................................................

...................... A-6 X lll 1 INTRODUCTION Test coupons of reactor vessel ferritic beltline materials are irradiated in reactor survei ll ance capsules to faci lit ate evaluation of vessel fracture toughness in vessel integrity evaluations. The key values that characterize fracture toughness are the reference temperature of nil-ductility transition (RT ND T) and the upper shelf energy (USE). These are defined in 1 OCFR50 Appendix G [1] and in Append i x G of the ASME Boiler and Pressure Vessel Code ,Section XI [2). Appendix Hof 10CFR50 [1] and ASTM E185-82 [3) establish the methods to be used for testing of surveillance capsu l e materials.

In the late 1990s the BWR Vessel and Internals Project (BWRVIP) initiated the BWRVIP Integrated Surveillance Program (ISP) [4], and the BWRVIP assumed responsibility for testing a n d evaluation of ISP capsules.

The surve illan ce plate and weld from the Browns Ferry Nuclear Plant Unit 2 (hereinafter, Browns Ferry 2 or BF2) were designated as "ISP representative surveillance materials" to be tested by the ISP according to an approved capsule withdrawal and test schedule. This report addresses the withdrawal and test of the Browns Ferry 2 120° capsule. The capsule was irradiated for 16 cycles of operation.

The capsule was removed in March 2011 and testing and evaluation was completed in September 2012. The surveillance capsule contained flux wires fo r neutron flux monitoring, Charpy V-notch impact test specimens , and tensile specimens.

The ca ps ule was shipped to MP Machinery

& Testing, LLC for opening and testing of the Charpy V-notch surveillance specimens. Evaluation of the fluence environment was conducted by Trans Ware Enterprises, Inc. Final evaluation of the Charpy test data and irradiated material properties and compilation of this report were performed by EPRI. The Charpy V-notch surveillance materials were tested per ASTM E185-8 2 , and the information and the associated evaluations provided in this report have been performed in accordance with the requirements of 10CFR50 Appendix B [5). This report compares the irradiated material properties of surveillance plate heat A0981-1 and surveillance we ld BF2 ESW to their baseline (e.g., unirradiated) properties.

The observed embrittlement (as characterized by is compared to that predicted by U.S. Nuclear Regulatory Commission (U.S. NRC) Regulatory Guide 1.99 , Rev. 2 [6). Other BWRVIP ISP reports wi ll integrate these shift results with the previous Browns Ferry 2 survei ll ance capsule results for a broader characterization of embritt l ement behavior.

1.1 Implementation Requirements The results documented in this report will be utilized by the BWRVIP ISP and by individual utilities to demonstrate compliance with 10CFR50, Appendix H , Reactor Vessel Material Surveillance Program Requirements.

Therefore , the implementation requirements of 1 OCFR50, Appendix H govern and the implementation requirements of Nuclear Energy Institute (NEI) 03-08, Guideline for the Management of Materials Issues [7], are not applicable. 1-1 I __j 2 MATERIALS AND TEST SPECIMEN DESCRIPTION The General Electric (GE) designed Browns Ferry Unit 2 (BF2) 120° surveillance capsule was removed from the plant for analysis and testing during the March 2011 refueling outage. The c a psule was a GE standard single basket design and contained a total of two Charpy packets and fo ur tensile tubes. Within each Charpy packet were a total of 12 Charpy V-notch specimens and three high purity dosimetry wires. Each of the tensile tubes contained two tensile specimens.

The 1 2 0° capsule is an original plant capsule, and has been irradiated in the plant since initia l startup. This is the second surveillance capsule to be removed from BF2 and tested. The 30° capsule was removed during the Fall 1994 outage and was tested by GE [8]. 2.1 Dosimeters The dosimetry wires were located along the ends of the Charpy specimens during irradiation.

Each of the two Charpy packets contained one high purity iron, copper, and nickel wire for fluence determination.

Further details on the exact wire locations during the irradiation are provided in the capsule opening discussion given in Section 2.3. A detailed discussion of the radiometric analysis of the capsule dosimetry wires is provided in Appendix A. 2.2 Charpy V-Notch Specimens The BF2 120° capsule Charpy V-notch and tensile specimen inventory, material descriptions , unirradiated (baseline)

Charpy impact data, and previously measured capsule data are summarized in this section of the report. 2.2.1 Capsule Loading Inventory The BF2 120° surveillance capsule inventory is provided in Table 2-1. A ll of the capsule specimens , which include tensile specimens , Charpy specimens, and dosimeters, were recovered from the capsule basket. Testing was only performed on the 24 Charpy specimens , and the do s imetry wires were counted and weighed to determine specific activities.

All eight of the tensile specimens (three base metal, three weld, and two RAZ) remain untested and are being held in reserve for future testing since there is no near-term use for tensile data. The technical advantage of storing the tensile specimens untested is that there will be options in the future for ho w these specimens wi ll be used to obtain useful data. For example, the tensile specimen geometry is conducive to fabrication of subsize Charpy as well as miniaturized Charpy V-notch specimens.

Further, research is currently underway to develop testing methods which wi ll enable the determination of plane-strain fracture toughness data from Charpy-sized specimens.

With these new technologies in view, there may be a need in the future for static and/or dynamic tensile data for use in the calcu l ation of fracture toughness from experimental data obtained from Charpy specimens.

Therefore, all of the tensile specimens have been placed into the archive storage so that they can be tested when necessary in the future. Similarly, the broken Charpy 2-1 Mat e rials and T es t Sp eci m en D escr iption specimen h alves h ave b een ad d ed to l ong-term archive storage for future u se in miniature mechanica l behav i or spec i men testing, chem i stry ana l ysis, and microstructural studies. As indicated in Table 2-1, there were a tota l of two C h arpy packets in the caps ul e, and each containe d three dosimetry wires (one Fe wire, one Cu wire, and one Ni wire) and 1 2 Charpy specimens.

Charpy packet 09 was fo u nd to contain all of the base metal test specimens as we ll as 4 we l d specimens.

Charpy packet G 10 contained the remaining four we l d specimens a l ong with all of the HAZ specimens. The capsule and a sc h ematic showing the position of the specimens within the capsule are shown in Figures 2-1 and 2-2, respective l y. 2-2 Table 2-1 Browns Ferry 2 120° surveillance capsule specimen inventory Charpy Specimens Flux Wires Vertical Position I I I I Base Weld I HAZ Fe Cu Ni -G9 8 4 0 1 1 1 Lowest in basket I G10 0 4 8 1 1 1 Hig h est in basket I I 1 The ca p sule included t e nsile s pecimens , but t he tens i l e spec im ens we r e not t ested. Four tensile specimens for th i s capsu l e were located at the lowest a x ial pos iti on below Cha r py pac k et G9 and four t ensi l e specimen s were l ocated betwe e n Charpy packets G9 a nd G10. 2 T he pack e t number s in t his tabl e a r e organiz e d by ax ia l pos i t i on i n th e c apsule wi t h p acket G 9 at the lowest e l evation i n the r e a ctor and packet G10 a t the h i ghes t.

Mat e ria l s a nd T es t Sp eci m e n D esc r ipti o n Figure 2-1 Photograph of 120° capsule for Browns Ferry Unit 2 showing positive identification markings Upper photograph shows the binary reactor code 26 in the upper left corner of the baske t. The lower photograph show s the GE drawing number engraved on the basket outer surface. The Side which Faced the Pressure Vessel in the Plant is Facing Down i n this Photograph.

2-3 Mat e rial s and T es t Sp e c i m en D e s c ription Figure 2-2 GI 0 Weld/HAZ Charpy 117C4058 Tensile Tuee (J) Tensile Tuee G8 (]) Base/Weld Charpy 117C4058 Tensile Tuee G7 Tensile Tuee G6 GI 0 fh)ilretry

\Vire Lcx::ation (J) fh)ilretry

\Vire Lcx::ation Schematic drawing showing the locations of test specimens in the Browns Ferry Unit 2 120° surveillance capsule 2.2.2 Material Description and Properties The material descriptions, chemical compositions, and unirradiated (baseline)

Charpy mechanical properties of the materials irradiated in the BF2 120°capsule are summarized below. The BF2 surveillance base metal specimens were machined from plate heat number A0981-1 in the longitudinal orientation (LT). Unirradiated baseline data are available for the plate , weld and HAZ materials.

All of the specimens were stamped on one end with the BF2 three-digit FAB codes assigned by GE. The weld Charpy surveillance specimens were made by the electroslag-weld (ESW) proces s according to Babcock and Wilcox Weld Procedure WR-12-4 and subsequently heat treated to simulate the core region plate treatments

[8]. The records regarding the identity of the weld wire heat number/flux lot combination used for the surveillance weld are not available

[8 , 9]; therefore, the surveillance weld is referred to as BF2 ESW. 2-4 Mat e rials and T es t Sp ec im en D e scription 2.2.3 Chemical Composition The best estimate chemical compositions of the surveillance plate A0981-1 and we ld BF2 ESW a r e shown in Tables 2-2 and 2-3, respectively.

Chemica l compositions are presented in weight percent. If multiple measurements exist for a sing l e s pecimen , those measureme nt s are first a v erage d to yie ld a sing l e va lu e for that specimen, and then the different specimen averages are a v erage d to determine the best estimate for the s urveillance heat. Table 2-2 Best estimate chemistry of Browns Ferry 2 surveillance plate A0981-1 I I I I Cu Ni p s Si I (wt%) I I Specimen ID Source (wt%) (wt%) I (wt%) (wt%) I 0.14 0.55 0.007 0.011 0.19 N/A I Refs. 8 and 9 0.14 0.55 0.007 0.011 0.19 +-Best Estimate Average Table 2-3 Best estimate chemistry of Browns Ferry 2 surveillance weld BF2 ESW I Cu Ni p s Si Specimen ID Source (wt%) (wt%) (wt%) (wt%) (wt%) 0.20 0.33 0.010 0.011 0.09 N/A Refs. 8 and 9 0.20 0.33 0.010 0.011 0.09 +-Best Estimate Average 2.2.4 CVN Baseline Properties As noted above, the Browns Ferry 2 surveillance plate Charpy specimens are longitudinal (LT) specimens. Table 2-4 provides the unirradiated (base lin e) Charpy test data for the A0981-1 surveillance plate material and Table 2-5 provides the unirradiated data for the we ld [8]. T h e baseline test data were fit to a hyperbolic tangent curve using the computer program CVGRAPH [10]. F i gures 2-3 and 2-4 show the fitted Charpy energy data curves for the unirradiated plate and we ld , respective l y. Table 2-6 summar i zes t h e baseline (unirradiated)

Charpy V-notch properties (index temperatures) of plate heat A0981-1 and weld heat BF2 ESW. In this table and throughout this report, T 3 0 is the 30 ft-lb ( 41 J) transition temperature; T 50 is the 50 ft-lb (68 J) transition temperature; T 3 sm iI is the 35 mil (0.89 mm) lateral expansion temperature; and USE is the average energy absorption at full shear fracture appearance. 2-5 Mat e r ials a nd T es t Sp ec im e n D esc ription Table 2-4 Un irradiated Charpy impact test data for surveillance plate A0981-1 (LT) E7J -39.5 21.92 15.0 11.7 (-39.7) (29.72) (0.38) E7C 6.3 23.08 20.5 20.8 (-14.3) (31.29) (0.52) E63 40.1 73.68 54.0 38.2 (4.5) (99.90) (1.37) E75 64.0 99.02 72.5 58.8 (17.8) (134.25) (1.84) E74 97.2 107.05 70.5 60.3 (36.2) (145.14) (1.79) E62 174.7 140.88 92.0 100.0 (79.3) (191.01) (2.34) E5K 327.9 144.72 93.5 100.0 (164.4) (196.21) (2.37) *All spec i men IDs have a dot over t he middle alphanumeric character. 2-6 Mat e rials and T es t Sp ec im en D esc ripti on Table 2-5 Unirradiated Charpy impact test data for surveillance weld BF2 ESW Specimen Temperature CVN LE Percent Shear ID" °F (C) ft-lb (J) mils (mm) 11 (%) EBJ -49.7 I 5.47 6.5 I 4.6 (-45.4) (7.42) (0.17) EAL 14.4 28.06 21.5 12.7 (-9.8) (38.04) (0.55) EAE 50.0 47.89 40.0 22.5 (10.0) (64.93) (1.02) EC3 81.3 22.40 25.0 28.3 (27.4) (30.37) (0.64) EBU 119.1 83.90 63.5 50.3 (48.4) (113.75) (1.61) EB6 204.3 102.15 79.0 79.3 (95.7) (138.49) (2.01) EAK 301.6 113.53 88.0 100.0 (149.8) (153.92) (2.24) EAD 373.8 110.62 84.5 100.0 (189.9) (149.98) (2.15) *All specimen IDs have a dot over the m i ddle alphanumeric character. Table 2-6 Baseline CVN properties A0981-1 Browns Ferry 2 -46.7 -14.8 -25.4 137.8 (LT) Surveillance Plate (-43.7) (-26.0) (-31.9) (186.8) BF2 ESW Browns Ferry 2 -52.5 -19.5 -29.5 116.0 Surveillance Weld (-46.9) (-28.6) (-34.2) (157.3) _J_ 2-7 Mat e ri als and T es t Sp e cim e n D esc ription 2-8 PLATE HEAT A0981-1 (BF2) CVGRAPH 5.0.2 Hyperbolic Tangent Curve Printed on 09/0 9/2002 08:29 AM Page l 300 Coefficients of Curve 1 A= 70.15 B = 67.65 C = 84.96 TO= 11.25 D = O.OOE+OO Equation is A+ B * (Tanh((T-To

)/(C+DT))] Upper Shelf Energy= 13 7 .8(Fixed)

Lower Shelf Energy=2.S(Fixed)

Temp@30 ft-lbs=-46.7 Deg F Temp@SO Deg F Plant: Browns F e rry 2 Material: SA302BM Heat: A0981-I Orientation:

LT Capsule: UNIRRA Fluence: 0.0 n/cm" 2 I . i I . -i ____ _,__I 1 * + I 250 t----1-->----'---

---

L---; I I i I : I -'------ ----1*-----_, -I ! . 200 -:-----f---I -----g i f c:

• Go l ---------r w z ' > 100 . ------i------i-----lp' -(.) I 9 ' -------j-----+---

I I I 50 --. ----t----L--+---I I I I ------1----1 i *1 I I I '. I I I I I I . 0 I ! I I . o -* -*-

-300 -200 -100 0 100 200 300 400 500 600 Temperature in Deg F Charpy V-Notch Data Temperature InputCVN Co mputed CVN Diff e r ential Figure 2-3 -8 0. 0 0 -6 0. 0 0 -40. 00 -20.00 . 0 0 2 0. 0 0 4 0. 0 0 8 0. 0 0 100. 0 0 12 0. 0 0 200. 00 8. 5 0 1 7. 5 0 3 5. 5 0 4 0. 0 0 9 7. 0 0 6 8. 0 0 7 3. 0 0 104. 5 0 137. 0 0 134. 5 0 146. 5 0 16. 6 4 23. 8 0 3 3. 6 6 4 6. 3 3 6 1. 2 4 7 7. 0 9 9 2. 2 I 1 I 5. 4 2 12 2. 9 0 I 2 8. 0 9 1 3 6. 2 3 Browns Ferry 2 plate A0981-1 (LT) unirradiated Charpy energy plot -8. 14 -6. 3 0 I. 8 4 -6. 3 3 3 5. 7 6 -9. 09 -I 9. 2 I -1 0. 9 2 1 4. 1 0 6. 4 1 1 0. 2 7 Mat e rial s and T e st Sp ec im en D e scripti o n Tern perature 300. 00 PLATE HEAT A0981-1 (BF2) Page 2 Plant: Bro wns Ferry 2 Material:

SA302BM Heat: A0981-1 Orientation

LT Capsule: UNIRRA Fluence: 0.0 n/cm" 2 Charpy V-Notch Data JnputCVN Computed CVN I 3 3. 0 O 13 7. 6 5 Correlation C o efficient= .956 Figure 2-3, continued Browns Ferry 2 plate A0981-1 (LT) unirradiated Charpy energy plot Diff e rent i al -4. 6 5 2-9 Mat e rial s and T es t Sp eci m e n D escr iption Figure 2-4 WELD HEAT ESW (BF2) CVGRAPH 5.0.2 Hyperbolic Tangent Curve Printed on 09/09/2002 08:23 AM Page l Coefficients of Curve l A= 59.25 B = 56.75 C = 81.22 TO= -6.21 D = O.OOE+OO Equation is A+ B * [Tanh((T-To)

/(C+DT))] Upper Shelf Energy= 116.0(F ixed) Lower She l f Energy=2.5(Fixed)

Temp@30 ft-lbs=-52.5 Deg F Temp@50 ft-lb s=-19.5 Deg F Plant: BROWNS FERRY 2 Materia l: ESW Heat: ESW Orientatio n: NA Capsule: UNIRRA F l uence: 0.0 n/cm" 2 + I I ' t t 250 ... -* -* --t""-*. ---------+------'

---; I ' I I i I ! I i i 200 !-, I +---J -r----t--t--

-*: 150 t --r---+---+-J-

-r---* -

Jl ' I l l i I ! : z 1* + -'1 0 0 i (j) ' ; t; 100 ----I : --1----'------1 ----50 I I ; --L-1-I l , L : I ! : ' I I .L -.. -* ----;*-----*-4---4------.....__ -----I , I 0 --_,_ ---30 0 -200 -10 0 0 100 200 300 400 500 600 Temperature in Deg F Charpy V-Notch Data Temperature Input CVN Computed CVN Differential

-8 0 -0 0 3. 5 0 I 8. 3 7 -I 4. 8 7 -60. 00 3 7' 0 0 2 6' 3 4 I 0. 66 -40. 00 5 4. 00 3 6. 9 I I 7. 0 9 -20.00 3 0. 0 0 49' 70 -I 9. 70 '00 4 3. 5 0 6 3. 5 8 -20.08 20' 00 l 06' 00 7 6' 9 5 2 9. 0 5 40. 00 9 3' 5 0 8 8. 4 5 5. 0 5 6 o. 0 0 I 0 7. 5 0 97. 4 I IO. 09 8 0. 0 0 8 2' 00 l 0 3' 8 7 -21. 87 I 2 0. 00 9 7' 5 0 I I I. I 4 -I 3 _ 6 4 2 00. 00 l 0 7' 5 0 l I 5. 3 0 8 0 Browns Ferry 2 weld BF2 ESW unirradiated Charpy energy plot 2-10 Mat e rials and Test Specimen D esc ription WELD H E AT E S W (BF2) Page 2 Plan t: BROWNS FERRY 2 Material: ESW Heat: ESW Orientat i on: NA Capsu l e: UNIRRA F lu e n ce: 0.0 n/cm"2 Temperature 300. 00 Figure 2-4 (cont i nued) C harp y V-N ot c h Data lnputCVN l 4 3. 0 0 Correlation Coefficient

= .891 Compute d CVN l I 5. 94 Browns Ferry 2 weld BF2 ESW unirradiated Char p y energy plot Di ffere ntial 2 7. 06 2-1 1 Mat e rial s and T es t Sp ec im en D esc ription 2.3 Capsule Opening The surveillance capsule was opened on Apri l 11 , 2012. As shown in Figure 2-1, the 120° capsule consisted of a single basket attached to the lead tube. The outside of the capsule had identification markings which could be clearly read. The capsule was marked with the correct binary reactor code number 26 , which agrees with the markings reported on GE Drawing 129B3578 entitled, "Surveillance Program Number Identification of GE Reactors." The capsule basket was also engraved with drawing number 117C4060B007, Part Number 7, and this marking is consistent with the markings observed on the 30° capsule basket described in [8]. As indicated in Figure 2-2 , the capsule basket contained two Charpy packets and four tensile tubes. Referring to Figure 2-1, the lead tube is positioned on the top surface of the basket in the photograph. Therefore , the surface that is facing down in the photograph was facing the vessel during irradiation.

The hook at the top of the photograph is the vessel lower attachment hook , and it was on the bottom of the capsule when the capsule was insta ll ed in the plant. The Charpy packet end tabs are on the right side in Figure 2-1. Moving up from the bottom of the capsule, the first item in the capsule was tensile tube G6 , then tensile tube G7, followed by Charpy packet G9. Above Charpy packet G9, the remaining two tensile tubes G8 and G9 were loaded with Charpy packet G 10 at the highest elevation in the plant. Attention was paid to the l ocation of the Charpy specimens and the dosimetry wire locations during disassembly of the Charpy packets. Each packet was found to contain one Fe , one Cu , and one Ni dosimetry wire along the ends of the Charpy specimens at the locations shown in Figure 2-2. The wire locations along the ends of the Charpy specimens were on the top side of the Charpy packets when the capsu l e was in the plant. Therefore, the wires were irradiated in a horizontal position in the reactor. The identifications assigned to the dosimetry wires indicate the Charpy packet from which they were recovered.

The wires and Charpy specimens were placed in individually marked containers for positive identification throughout the work. 2-12 3 NEUTRON FLUENCE CALCULATION The Browns Ferry 2 120° capsule was irradiated for 16 cycles of operation.

The survei ll ance capsule was placed in the reactor's 120° capsule holder prior to cycle 1 and was removed following cycle 16 for a total irradiation period of 22.9 effective full power years (EFPY). The surveillance capsule included copper, iron, and nickel flux wire dosimetry specimens.

Evaluation of the survei ll ance capsule specimens requires knowledge of the neutron irradiation environment.

The neutron flux density , neutron energy spectrum , and neutron fluence are required at the surveillance capsule location.

The NRC has established guidelines in Regulatory Guide 1.190 [ 11] for determining best estimate values of flux, energy spectrum, and fluence for RPV damage assessments using particle transport methods. These guidelines are not specifically intended for use in surveillance capsu l e evaluations; however, they do provide a suitable framework to support the development of accurate neutron transport analysis models for surveillance capsule evaluations.

This report documents the application of the modeling and analysis guidelines provided in [11] to determine the surveillance capsule accumulated irradiation and capsule specimen neutron fluence of the Browns Ferry 2 120° ISP capsule flux wires. Additionally, the accumulated irradiation for the 30° capsule, removed at the end of cycle 7, and the 30° flux wires, removed at the end of cycle 1, were determined.

The neutron fluence was also calculated for the 300° ca ps ule at the projected time ofremoval, and for the 120° capsule at the end of cycle 16 and at the end of the reactor's extended design life of 54 EFPY. The fluence and activation values presented in this report were calculated using the RAMA Fluence Methodology

[12] (hereinafter referred to as "RAMA"). The specific activities predicted by RAMA are compared to the activity measurements reported in Appendix A. RAMA was developed for the Electric Power Research Institute, Inc. (EPRI) and the Boiling Water Reactor Vessel and Internals Project (BWRVIP) for the purpose of calculating neutron flu e nce in Boiling Water Reactor (BWR) components.

As prescribed in Regulatory Guide 1.190 , RAMA has been benchmarked against industry standard benchmarks for both pressurized water reactor (PWR) and BWR designs. In addition , RAMA has been compared with several specific dosimetry measurements and reported fluence from several commercial operating rea c tors. The results of the benchmarks and comparisons to measurements show that RAMA accurately predicts specimen activities, RPV fluence, and vessel interna l component fluence in all light water reactor types. Under funding from EPRI and the BWRVIP , the RAMA me t hodology has been reviewed by the U.S. NRC and subsequently given generic approval for determining fast neutron fluence in BWR pressure vessels [13] and vessel internal components that include the core shroud and top guide [14]. 3-1 N e utron Fluen c e Calculation 3.1 Description of the Reactor System This section provides an overview of the reactor design and operating data inputs that were used to develop the Browns Ferry 2 reactor fluence model. All reactor design and operating data inputs used to develop the model were plant-specific and were provided by Tennessee Valley Authority (TV A). The inputs for the fluence geometry model were developed from design and as-built drawings for the reactor pressure vesse l , vessel internals, fuel assemblies, and containment regions. The reactor operating data inputs were developed from core simulator data that provided a historical accounting of how the reactor operated for cycles 9 through 16. Core simulator data was not available for cycles 1 through 8. Data for these cycles was approximated using information from the following sources: 1) cycle summary reports, 2) spreadsheet data , and 3) cycle 9 data for axial power shapes, water densities , and fuel assembly orientation.

Projections for cycle 17 to the end of the reactor's extended operating life were based on the reactor's operating history for cycle 16. 3. 1. 1 Reactor System Mechanical Design Browns Ferry 2 is a General Electric BWR/4 class reactor with a core loading of 764 fuel assemblies. Browns Ferry 2 began commercial operation in 1975 with a design rated power of 3293 MWt. At the beginning of cycle 11 the rated power was increased to 3458 MWt. At the time of this fluence analysis , Browns Ferry 2 had completed 16 cycles of operation.

Figure 3-1 illustrates the basic planar configuration of the Browns Ferry 2 reactor at an axial elevation near the reactor core mid-plane.

All of the radial regions of the reactor that are required for fluence projections are shown. Beginning at the center of the reactor and projecting outward, the regions include: the core region, including control rod loc ations and fuel assembly locations (fuel locations are shown only for the 0 to 90 degree quadrant);

core reflector region (bypass water); central shroud wall; downcomer water region including the jet pumps; reactor pressure vessel (RPV) wall; cavity between RPV and insulation; insu l ation; cavity region between the insulation and biological shield; and biological shield (concrete wall). The mechanical design inputs that were used to construct the Browns Ferry 2 fluence geometry model included as-built and nominal design dimensional data. As-built data for the reactor components and regions of the reactor system is a lwa ys preferred when constructing specific models; however, as-built data is not always available.

In these situations, nominal design information is used. 3-2 Ne utron Flu e nc e Calculati o n Figure 3-1 300* 240* Noles: Ttos ilnlwOig is nol lo sc81e. F = Fud-loc-.S. (Loe&lions stm .. only fo<tlle

+ = ("'Jdml md kM:Hlions Reactor Nollh Ste West O" 180" Planar view of Browns Ferry 2 at the core mid-plane elevation Suivellance CapsoJe Jet Pimp Assembly Core Relecf:or Reactor PressuR! Vessel and Clad Vessel lnsw.tion andaad Biological Shield an<1aa<1 For the Browns Ferry 2 fluence model, the predominant dimensional information used to construct the fluence model was nominal design d ata. As-built data was availa bl e for the fo llo wing dimensions:

• Jet pump mixer p ip e radial l ocation

• Reactor pressure vessel cladding inner radius Another imp ortant component of the fluence analysis is the accurate description of the surveillance capsu l es in the reactor. It is shown in F igur e 3-1 that three surveillance caps ul es were in i t iall y installed in the Browns Ferry 2 reactor. The capsules were attache d radia ll y to the ins i de s urfac e of the RPV (looking outward from the core region) at the 3 0°, 120°, and 3 00° az i m uths. Surve ill ance capsules are u se d to monitor the ra di ation accumu l ated in th e reactor over a p er iod of time. The importance of surveillance capsules influence analyses is that they contain flux wires that are irradiated during reactor operation.

When a caps ul e is removed from the reactor, the irradiated flux wires are evaluated to obtain activity measurements.

T h ese measurements are used to validate the fluence model. Three sets of flux wires have been removed from the Browns Ferry 2 reactor and analyzed. (See Section 3.4, which presents a comparison of the calcu l ated-to-m easured capsule resu lt s.) 3-3 Ne utron Fluence C al c ulati o n 3. 1.2 Reactor System Material Each region of the reactor is comprised of materials that include reactor fuel, steel, water, insulation, concrete, and air. Accurate materia l information is essential for the fluence eva l uation as the material compositions determine the scattering and absorption of neutrons throughout the reactor system and, thus , affect the determination of neutron fluence in the reactor components. Table 3-1 provides a summary of the materials for the various components and regions of the Browns Ferry 2 reactor. The material attributes for the steel, insulation , concrete, and air compositions (i.e. material densities and isotopic concentrations) are assumed to remain constant for the operating life of the reactor. The attributes of the fuel compositions in the reactor core region change continuously during an operating cycle due to changes in power level, fuel burnup, contro l rod movements, and changing moderator density levels (voids). Because of the dynamics of the fuel attributes with reactor operation , severa l state-point data sets are used to describe the operating states of the reactor for each operating cycle. The number of data sets used in this analysis is presented in Section 3 .1.3 .3. 3-4 Ne utr o n Flu e n ce Ca l c u l ati o n Table 3-1 Summary" of material compositions by region for Browns Ferry 2 Region Control Rods and Guide Tubes Core Support Plate Fuel Support Piece --------+-

Fu e I Assembly Lower Tie Plate Reactor Core Reactor Coolant I Moderator Core Reflector Fuel Assembly Upper Tie Plate Top Gu i de Core Spray Sparger Pipes Core Spray Sparge r Flow Areas Shroud Downcomer Region Jet Pump Riser and Mixer Flow Areas Jet Pump R i ser and Mixer Metal Jet Pump Riser Brace and Pads Surve i llance Capsul e Speci m ens Reactor Pressure Vessel Clad Reactor Pressure Vessel Wall Cavity Reg i ons Ins u lat i on Clad I n sulation Biolog ic al Shi el d Clad ..__ ______ _ Biologi c al Sh i eld Wall 3. 1.3 Reactor Operating Data Inputs Material Composition S t ainless Steel , s.c Stainless Steel Sta i nless Stee l Stainless Steel , Z i rcaloy , lnconel Water W a ter Stainless Steel , Zircaloy , lnconel Stainle s s Stee l Stainless Steel Wa t er Stainless Steel Water Water Stainles s Steel Stainless Steel Carbon Steel S t ainless Steel Carbon Steel Air (Nitrogen)

Stainle ss Ste e l A l uminum Fo i l Carbo n S t e e l Re i nforced Concre t e An accurate eva lu ation of reactor vesse l and component fluence requires an accurate accounting of t h e reactor's operating history. The primary reactor operat i ng parameters that affect the determinat i on of fast neutron fluence in light water reactors include reactor power le v e l s , core power distributions , coolant water density distributions , and fu e l material (isotopic) distributions.

3-5 Ne utron Fluence Ca l c ulation 3.1.3.1 Core Loading It is common in BWRs that more than one fuel assembly design may be loaded in the reactor core in any given operating cycle. For fluence evaluations, it is important to account for the fuel assembly designs that are loaded in the core in order to accurately represent the neutron source distribution at the core boundaries (i.e. peripheral fuel locations and the top and bottom fuel elevations).

Eleven different fuel assembly designs were loaded in the Browns Ferry 2 reactor during the period included in this evaluation.

Table 3-2 provides a summary of the fuel designs loaded in the reactor core for each evaluated operating cycle. The cycle core loading provided by TV A was used to identify the fuel assembly designs in each cycle and their location in the core loading inventory. (Note that fuel loadings for cycle 12 were divided into three individual periods, identified as 12A , 12B and 12C.) For each cycle, appropriate fuel assembly models were used to build the reactor core region of the Browns Ferry 2 RAMA fluence model. 3.1.3.2 Power History Data Reactor power history is the measure of reactor power levels and core exposure on a continual or periodic basis. For this fluence evaluation, the power history for the Browns Ferry 2 reactor was developed from power history inputs provided by TV A. The power history data showed that Browns Ferry 2 started commercial operation with a design rated thermal power of 3293 MWt for cycles 1 through 10 and implemented a measurement uncertainty recovery (MUR) power uprate of 3458 MWt at the beginning of cycle 11. It was assumed in this analysis that all future cycles would operate at the 3458 MWt power level. The power history data for Brown s Ferry 2 included daily power levels for most cycles. When daily power histories were not available, average power levels were constructed based on exposure accumulation using the core simulator codes. This data was used to calculate the capsule and vesse l fluences.

Periods of reactor shutdown due to refueling outages and other events were also accounted for in the model. The power history data was verified by comparing the calculated energy production in effective full power years with power production records provided by TV A. Table 3-3 lists the accumulated EFPY at the end of each cycle for this fluence evaluation.

3-6 Ne utron Flu e n ce Cal c ulation Table 3-2 Summary of the Browns Ferry 2 core loading inventory Cycle 7x7 Designs 8x8 Designs 9x9 Designs 10x10 Designs Dominant Peripheral GE3 GE4 GE5 GE6 GE7 QUAD+1 GE9 GE11 GE13 GE14 ATR-10 Design 764 GE3 2 632 132 GE3 3 364 168 232 GE3 1 232 1 240 r 4 168 GE3 5 123 153 488 GE4 6 l 70 4 GE? [ 7 212 388 4 160 GE? 8 4 580 4 176 GE? 9 348 216 200 GE? 10 l I 148 200 200 216 I GE9 11 48 200 516 GE11 12A L 764 GE13 128 764 GE13 I 12C 49 715 GE13 13 111 281 372 GE11 14 I T 149 335 280 GE13 15 I 111 653 GE14 16+2 764 ATRIUM-10 1 Due to lack of detailed information on QUAD+ design , these lead test assemblies (L TAs) were modeled as GE6 bundles. 2 Cycles 17 and beyond use cycle 16 data for projecting fluence to the end of the extended plant license period. 3-7 Ne utron Flu e n ce C al c ulation 3.1.3.3 Reactor State-Point Data Cycles 1 through 8 of Browns Ferry 2 were derived from Cycle Summary Reports and plant data spreadsheets, which contained bundle average exposures. Radial power shapes were calculated based on this bundle average exposure data. Data from cycle 9 was used to provide axia l power shapes, water densities, and fuel assembly orientation for cycles 1 through 8. This represented the best available information for these cycles. Core simulator data was provided by TV A to characterize the historical operating conditions of Browns Ferry 2 for cycles 9 through 16 and cycle projections.

The data calculated with core simulator codes represents the best-available information about the reactor core's operating history over the reactor's operating life. In this analysis , the core simulator data provided by TV A was processed by Trans Ware to generate state-p oint data files for input to the RAMA fluence model. The state-point files included three-dimensional data arrays that described core power distributions , fuel exposure distributions , fuel materials (isotopics), and coolant water densities. A separate neutron transport calculation was performed for each of the state points tallied in Table 3-3. The calculated neutron flux for each state point was combined with the appropriate power history data described above in order to provide an accurate accounting of the fast neutron fluence for the reactor pressure vessel. Fluence projections to the end of the reactor's design life and extended design life were performed using projected equilibrium cycles. Equi librium cycles are discussed below. Beginning of Operation through Cycle 16 State Points A total of 170 state points were used to represent the operating history for the first 16 operating cycles of Browns Ferry 2. These state points were selected from hundreds of exposure points that were calculated with the core simulator code. The hundreds of exposure points were eva luat ed and grouped into a fewer number of exposure ranges in order to reduce the number of transport calculations required to perform the fluence evaluation.

Several criteria were used in the determination of the exposure ranges, including eva luation s of core thermal powers , core flows , core power profiles, and control rod patterns.

In determining exposure ranges , it is assumed that there will be at le ast one exposure step in that range that would accurately represent the average operating conditions of the reactor over that range. This single exposure step is then referred to as the "state point". Table 3-3 shows the number of state points used for each cycle in this fluence evaluation.

Projected Reactor Operation Projections of plant operations beyond cycle 16 are represented with an "equilibrium" cycle that incorporates the best-available information on expected cycle length, fuel bundle lo ading, and operating strategies for future cycles. Cycle 16, at a thermal power level of 3458 MWt, is used as the equilibrium cycle for this analysis to project fluence to the end of the extended plant design life of 54 EFPY. 3-8 N e utron Flu e n c e Ca l c ulation Tab l e 3-3 State-point da t a for each cycle in Browns Ferry 2 Cycle Number Number of State Rated Thermal Accumulated Points Power 1 (MWt) Effective Full Power Years (EFPY) 3 3293 t 1.3 2 3 3293 2.0 3 3 3293 3.0 4 3 3293 4.4 5 t 3 3293 5.5 6 3 3293 6.8 7 3 3293 8.1 8 3 3293 9.4 9 20 3293 10.7 10 17 3293 12.2 -+--11 19 3458 14.0 12 17 3458 15.7 13 21 3458 17.6 14 19 3458 19.4 15 17 3458 21.3 16 16 3458 22.9 17+ 2 16 3458 54.0 1 The rated thermal power is listed for each cycle. The actual power levels were used for the individual state-point calculations for cycles 1-16. 2 Cycles 17 a n d beyond use cycle 16 data for projecting fluence to the end of the extended plant license. Limitation of Fluence Projections Some of the fluence values presented in thi s report are based on projections of the operation of Browns Ferry 2 beyond the current operating cycle. Projections are performed usin g an assumed equilibrium cycle. The significance of the equi librium cycle is that it defines the flux profiles that are used to project fluence into the future. Providing that the design ba sis for the equilibrium cy cl e does not change appreciably, projections based on the equilibrium cycle should remain bounding through 54 EFPY to support licensing , in-service inspection , and flaw evaluation acti v ities. 3-9 Neutron Fluence Calculation If the design basis for the equilibrium cycle changes at any point in time that would result in a significant change to the flux profiles for the equilibrium cycle, then a new evaluation is needed. Operating conditions, if changed, that could impact the validity of the equilibrium cycle include power uprates, introduction of new fuel designs, changes in projected cycle lengths, changes in core loading strategies, changes in reactor flow, or other changes that could alter the flux profiles used in the fluence projections.

3.2 Calculation Methodology The Browns Ferry 2 capsule evaluation was performed using the RAMA Fluence Methodology software package [12]. RAMA and the application of RAMA to the Browns Ferry 2 reactor are described in this section. 3.2.1 Description of the RAMA Fluence Methodology The RAMA Fluence Methodology (RAMA) is a system of computer codes, a data library, and an uncertainty methodology that determines best-estimate fluence in light water reactor pressure vessels and vessel components.

The primary codes that comprise the RAMA methodology include model builder codes, a particle transport code, and a fluence calculator code. The data library contains nuclear cross sections and response functions that are needed for each of the codes. The uncertainty methodology is used to determine the uncertainty and bias in the estimate fluence calculated by the software.

The primary inputs for RAMA are mechanical design parameters and reactor operating history data. The mechanical design inputs are obtained from plant-specific design drawings, which include as-built measurements when available.

The reactor operating history data is obtained from reactor core simu l ator codes, system heat balance calculations, daily operating logs, and cycle summary reports that describe the operating conditions of the reactor over its operating lifetime.

The primary outputs from RAMA calculations are neutron flux, neutron fluence, dosimetry activation, and an uncertainty eva lu ation. The model builder codes consist of geometry and material processor codes that generate input for the particle transport code. The geometry model builder code uses mechanical design inputs and meshing specifications to generate three-dimensional geometry models of the reactor. The material processor code uses reactor operating data inputs to process fuel materials , structural materials, and water densities that are consistent with the geometry meshing generated by the geometry model builder code. The particle transport code performs three-dimensional neutron flux calculations using a deterministic, multigroup, particle transport theory method with anisotropic scattering.

The primary inputs prepared by the user for the transport code include the geometry and material data generated by the model builder codes and numerical integration and convergence parameters for the iterative transport calculation. The transport solver is coupled with a general geometry modeling capability based on combinatorial geometry techniques.

The coupling of general geometry with a deterministic transport solver provides a flexible, accurate , and efficient tool for calculating neutron flux in light water reactor pressure vessels and vessel components.

The primary output from the transport code is the neutron flux in multigroup form. 3-10 Neu tron Flu e n ce Calculation T he fluence calculator code determines fluence and activation in the reactor pressure vessel and vessel components over specified periods of reactor operation.

The primary inputs to the fluence calculator include the multigroup neutron flux from the transport code, response functions for the various materials in the reactor , reactor power levels for the operating periods of interest , the specification of which components to evaluate , and the energy ranges of interest for evaluating neutron fluence. The fluence calculator includes treatments for isotopic production and decay that are required to ca l culate specific activities for irradiated materials.

The reactor operating history is genera ll y represented with several reactor state points that represent the various power levels and core power shapes generated by the reactor over the life of the plant. These detailed s t ate points are combined with the daily reactor power levels to produce accurate estimates of the fluence and activations accumulated in the plant. The uncertainty methodology provides an assessment of the overa ll accuracy of the RAMA Fluence Methodology.

Variances in the dimensional data, reactor operating data, dosimetry mea s urement data , and nuclear data are evaluated to detennine if there is a statistically significant bias in the calculated results that might affect the determination of the best-estimate fluence for the reactor. The plant-specific results are also weighted with comparative results from experimental benc h marks and other plant analyses and ana l ytical uncertainties pertaining to the methodology to determine if the plant-specific model under evaluation is statistically acceptable as defined in Regulatory Guide 1.190. The RAMA nucle a r data library contains atomic mass data, nuclear cross-section data , and response functions that are needed in the material processing, transport , fluence , and reaction rate calculations.

The cross-section data and response functions are based on the BUGL E-9 6 nuclear data library [15] and the VITAMIN-B6 data library [16]. The RAMA Fluence Methodology is described in the Theory Manual [17]. The genera l procedures for using the methodology are presented in the Procedures Manual [ 18]. 3.2.2 The RAMA Geometry Model for the Browns Ferry 2 Reactor Section 3.1 described the design inputs that were provided by TVA for the Brown s Ferry 2 reactor fluence evaluation.

These design inputs were used to develop a plant-specific, dimensional computer model of the Browns Ferry 2 reactor with the RAMA Fluence Methodology. Figures 3-2 and 3-3 provide general illustrations of the primary components, structures and regions developed for the Browns Ferry 2 fluence model. Figure 3-2 shows the planar configuration of the reactor model at an elevation corresponding to the reactor core mid-plane elevation. Figure 3-3 shows an axial configuration of the reactor model. Note that the figures are not drawn to scale. They are intended only to provide a perspective for the layout of the model , and specifically how the various components , structures, and regions lie relative to the reactor core region (i.e., the neutron source). Because the figures are intended only to provide a general overview of the model , they do not include illustrations of the geometry meshing developed for the model. To provide such detail is beyond the scope of this report. 3-11 Ne utr o n F lu e n ce Ca l c ul atio n 43 5.61 (171.50")

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• E 0 CD ID c ID <( a. .. E ::JI rn n.. "CJ a; ::J ..., e .c: rn Axial view of the Browns Ferry 2 RAMA model Ne utron Flu e n ce Ca l c ulation c (ij 0 ?:-'ii ?:-32 > 'S > Q) as II) as :c 0 .5 0 Q; U) Q; "ii <ti c II) :5 0 £ II) 0 *a, 0 Ci ili The followi n g subsections provide an overview of the computer model s that were developed for the va rious components, structures , and coo l ant flow regions of the Browns Ferry 2 r eac tor. 3-13 Neutron Flu e n ce Calcu l ation 3.2.2.1 The Geometry Model RAMA uses a generalized three-dimensional geometry modeling system that is based on a combinatorial geometry technique, w hich is mapped to a Cartesian coordinate system. In this analysis, an axial plane of the reactor model is defined by the (x,y) coordinates of the modeling system, and the axial elevation at which a plane exists is defined along a perpendicular z-axis of the modeling system. Thus, any point in the reactor model can be addressed by specifying the (x,y,z) coordinates for that point. Figure 3-1 illustrates a planar cross-section view of the Browns Ferry 2 reactor design at an axial elevation corresponding to the reactor core mid-plane elevation.

It is shown for this one elevation that the reactor design is a complex geometry composed of various combinations of rectangular, cylindrical, and wedge-shaped bodies. When the reactor is viewed in three dimensions, the varying heights of the different components, structures, and regions create additional geometry modeling complexities.

An accurate representation of these geometrical complexities in a predictive computer model is essentia l for calculating accurate , best-estimate fluence in the reactor pressure vesse l , the vessel internals, and the surrounding structures.

Figures 3-2 and 3-3 provide general illustrations of the planar and axial geometry complexities that are represented in the Browns Ferry 2 fluence model. For comparison purposes, the planar view illustrated in Figure 3-2 corresponds to the same core mid-plane elevation illustrated in Figure 3-1. The computer model for Browns Ferry 2 assumes azimuthal quadrant symmetry in the planar dimension.

Figure 3-2 illustrates the quadrant geometry that was modeled in this analysis.

In terms of the modeling coordinate system, the " northeast" quadrant of the geometry is represented in the model. The 0° azimuth, which has a "north" designation, corresponds to the 0° azimuth referenced in the plan drawings for the reactor pressure vessel. Degrees are incremented clockwise.

Thus , the 90° azimuth is designated as the "east" direction.

All other components, structures, and regions have been appropriate l y mirror reflected or rotated to this quadrant based upon their relationship to the pressure vesse l orientation to ensure that the fluence is appropriately calculated relative to the neutron source (i.e., the core region). Although symmetry is a modeling consideration, the results presented in this report for the different components and structures are given at their correct azimuths in the plant. Figure 3-3 illustrates the axial configuration of the primary components, structures , and regions in the fluence model. For discussion purposes, the same components , structures, and regions shown in the planar view of Figure 3-2 are also illustrated in Figure 3-3. Figure 3-3 shows that the axial height of the fluence model spans from a lo wer elevation just below the jet pump riser inlet to above the core shroud head flange. This axial height covers all areas of the reactor pressure vesse l that are expected to exceed a fluence threshold of 1.0E+ 17 n/cm 2 at 54 EFPY. As previously noted, Figures 3-2 and 3-3 are not drawn precisely to scale. They are intended only to provide a perspective of how the various components, structures, and regions of the reactor are positioned relative to the reactor core region (i.e., the neutron source) and each other. The following subsections provide details on the modeling of individual components, structures, and regions. Please refer to the figures for visual orientation of the components and regions described in the following subsections.

3-14 Ne utron Flu e n ce Cal c ulati o n 3.2.2.2 The Reactor Core and Core Reflector Models The reactor core contains the nuclear fuel that is the source of the neutrons that irradiate all components and structures of the reactor. The core is surrounde d by a s hroud structure that serves to channe l t he reactor coolant through the core region during reactor operation. The region between the core and the core shroud is the core reflector , and it contains coolant. The reactor core geometry is rectangular in design and is modeled with rectangular e l ements to preserve its shape in the analysis.

The core reflector reg ion interfaces w ith the rectangular shape of the core region and the curved shape of the core shroud. It is, therefore, modeled using a combination of rectangular and cylindrical elements. The core region is centered in the reactor pressure vessel and is characterized in the analysis with two fundamenta l fuel zones: interior fuel assemblies and peripheral fuel assemblies.

The peripheral fuel assemblies are the primary contributors to the neutron source in the fluence calculation. Becau s e these assemblies are loaded at the core edge where neutron l eakage from the core is greatest , there is a sharp power gradient across these assemblies that requires consideration.

To a ccount for the power gradient , the peripheral fuel assemblies are sub-meshed with add itional rec t ang ul ar elements th at preserve the pin-wise details of the fuel assemb l y geometry and power distribution.

The interior fuel assemb li es make a lesser contribution to the reactor fluence and are, therefore , modeled in various homogenized forms in accordance with their contributions to the reactor fluence. For computational efficiency , homogenization treatments are used in the interior core region primarily to reduce the number of mesh regions that must be so l ved in the transport calculation.

The meshing configuration for each fue l assemb l y l ocation in the core region is determined by parametric studies to ensure an accurate estimate of fluence throughout all regions of the reactor system. Each fue l assembly design , whether lo a d ed in the interior or peripheral locations in the core , is represented with four axial material zones: the lower tie plate/end plug zone , the fuel zone, the fuel upper plenum zone, and the upper tie plate/end plu g zone. The structural materials in the top and bottom nozzles for each unique assembly design are repre s ented in the model to address the shielding effects th a t these materials have on the components above and below the core region. The fuel zone contains the nuclear fue l and structura l materials for the fuel a s semb li es. The materials for each fuel assembly are unique during reactor operation and are incorporated into the model using reactor operating data from core simu l ator codes. The upper plenum region captures fission gases during reactor operation.

The Browns Ferry 2 reactor core region has a nominal elevation for the bottom of active fuel at 549.43 cm (216.31 in.) and an active fuel height of 381.00 cm (150 in.). Browns Ferry 2 loaded fuel designs with active fuel heights ranging from 146" to 150". The core simulator codes used by Browns Ferry 2 mode l ed the core as 150" in all situations , so this value was also used in the RAMA model. Since the predominant peripheral fuel d e signs throughout Browns Ferry 2's history were 150" in height , the effect of this approximation on the component fluence will be negligible.

From an isotopic standpoint, the core is modeled using quadrant symmetry. For the 30° and 120° capsule eva lu atio n s, as well as the peak RPV fluence calcu l ations, the NE fuel quadrant was used. 3-15 N e utron Flu e nc e Calculation 3.2.2.3 The Core Shroud Model The core shroud is a canister-like structure that contains the reactor core and channels the reactor coolant and steam produced by the core into the steam separators. Axially the shroud extends from the lower shroud wall to the top of the shroud head rim in the model. The core shroud is cylindrica l in design and is modeled with pipe elements.

3.2.2.4 The Downcomer Region Model The downcomer region lies between the core shroud and the reactor pressure vessel. It is basically cylindrical in design, but with some geometrical complexities created by the presence of jet pumps and surveillance capsules in the region. The majority of the downcomer region is modeled with pipe segments.

The areas of the downcomer containing the jet pumps and specimen capsules are modeled with the appropriate geometry elements to represent their design features and to preserve their radial, azimuthal, and axial placement in the downcomer region. These structures are described further in the following subsections.

3.2.2.5 The Jet Pump Model There are tenjet pump assemblies in the downcomer region of Browns Ferry 2, which provide the main recirculation flow for the core. The jet pumps are modeled at azimuths 30 , 60, and 90° in the downcomer region. When symmetry is applied to the model, the 30° location represents the jet pump assemblies that are positioned azimuthally at 30, 150, 210, and 330°; the 60° location represents those at 60, 120, 240 , and 300°; and the 90° location represents the jet pump assemblies at 90 and 270°. Note that there are no jet pumps present at the 0-and 180° azimuths of the reactor. The jet pump model includes representations for the riser, mixer, and diffuser pipes; nozzles; rams head; riser inlet pipe; and riser brace yoke , leafs, and pads. The jet pump assembly design is modeled using cylindrical pipe elements for the jet pump riser and mixer pipes. The riser pipe is correctly situated between the centers of the mixer pipes. The riser brace assembly model includes two leaf structures that attach to the yoke and pad elements.

3.2.2.6 The Surveillance Capsule Model Section 3.1 describes the three surveillance capsules installed in the Browns Ferry 2 reactor. The surveillance capsules are installed near the inner surface of the pressure vessel wall. The surveillance capsules are rectangular in design. Because of this shape, the capsules are not easily implemented in the otherwise cylindrical e lem ents of the downcomer region model. With reference to Figure 3-1, it is observed that the capsules are of small dimensions in the planar geometry and they reside a long distance (view factor) from the core region. Based on these factors , the otherwise rectangular shape of the surveillance capsules can be reasonably approximated in the model with arc elements.

The surveillance capsule model also includes a representation for the downcomer water that surrounds the capsule on all sides. The surveillance capsules are correctly modeled behind the jet pump riser pipes at the 30-and 60° azimuths.

When symmetry is applied to the model, the 30° location represents the capsule installed at 30°, while the 60° lo cation represents the capsules at 120 and 300°. 3-16 N e utron Flu e nc e Calculation The surveillance capsules are modeled at their correct axial position and height relative to the core region. The surveillance capsules cover about nine percent of the total core height. 3.2.2. 7 The Reactor Pressure Vessel Model The reactor pressure vessel and vessel cladding lie outside the downcomer region and each is cylindrical in design. Both are modeled with pipe elements.

The cladding-pressure vessel interface is a key location for RPV fluence calculations and is preserved in the model. This interface defines the inside surface (OT) for the pressure vessel base metal where the RPV fluence is calculated.

Browns Ferry 2 has cladding only on the inside surface of the pressure vessel wall. 3.2.2.8 The Vessel Insulation Model T h e vessel insulation lies in the cavity region outside the pressure vessel wall. The insulation is cylindrical in design and follows the contour of the pressure vessel wall. It is modeled with pipe e l ements. 3.2.2.9 The Inner and Outer Cavity Models The cavity region lies between the pressure vessel and biological structures.

As previously described , the vessel insulation lies in the cavity region; thus creating two cavity regions. The inner cavity region lies between the vessel and the insulation. The outer cavity region lies between the vessel insulation and biological shield cladding.

The boundaries of the cavity regions follow the contours of the pressure vessel, vessel insulation , and biological shie ld. The cavity regions are essentially cylindrical in design and are modeled with pipe segments. 3.2.2.1 0 The Biological Shield Model The biological shield (concrete) defines the outer most region of the fluence model. The biological shield is basically cylindrical in design and is modeled with pipe segments.

There is cladding on the inside and outside surface of the biological shield. 3.2.2.11 The Above-Core Component Models Figure 3-3 includes illustrations of other components and regions that lie above the reactor core region. The predominant above-core components represented in the model include the top guide and core spray spargers. The Top Guide Model The top guide component lies above the core region. The top guide is appropriately modeled by including representations for the vertical fuel assemb l y parts and top guide plates. The upper fuel assembly parts that extend into the top guide region are modeled in three axial segments:

the fuel rod plenum, fuel rod upper end plugs, and fuel assembly upper tie plate. The fuel assembly parts and top guide plates are modeled with rectangular elements. 3-17 Ne utron Flu e n ce C al c ulati o n The Core Spray Sparger Model The core spray spargers include upper and lower sparger pipes and a vertical inlet pipe. The core spray spargers are appropriately represented as torus structures in the model. The sparger pipes resi d e inside the u pper shroud wa ll above the top guide. The spargers are modeled as pipe-like structures and include a representation of reactor coolant inside the pipes. 3.2.2.12 The Below-Core Component Models Figure 3-3 includes illustrations of other components and regions that lie below the reactor core region. The fuel support piece, core support plate , and core inlet regions appropriately include a representa tion of the cruciform control rod below the core region. The lower fue l assemb l y parts inc lud e representations for the fuel rod l ower end p lu gs, lower tie plate , and nose piece. The below-core components are mode l ed with rectangu l ar elements with the exception of the core s upp ort plate. The core support plate is modeled using both rectangular and cy lindri ca l e l ements to provide an appropriate representation of that component.

3.2.2.13 Summary of the Geometry Modeling Approach To summarize the reactor mode li ng process , there are severa l key features of the RAMA code system that allow the reactor design to be accurately represented for RPV and capsule fluence eva lu ations. Following is a summary of some of the key features of the model.

• Rectangular, cylindrical, and we d ge bodies are mixed in the model in order to provide an accurate geometrica l representation of the components and regions in the reactor.

• The reactor core geometry is mode l ed with rectangular bodies to represent its actual shape in the reactor. The fuel assemblies in the core region are also sub-meshed with a d ditional rectangular bodies to represent the pin cell regions in the assemblies.

• A com bi nation of rectangular and cylindrical bodies is used to describe the transition parts between the rectangular core reg ion and the cy lind rical outer core regions.

• Cyli ndr ica l and wedge bo di es are u sed to model the components and regions that extend outward from the core region (core shrou d , downcomer, RPV, etc.).

• The survei ll ance capsules are mode l ed at their correct radial , azimuthal , and elevational positions behind the jet pumps in the downcomer region.

• The above-core region includes accurate representations of the top guide and core spray spargers.

• The below-core region includes appropriate representations for the fuel support piece, core support p l ate, core inlet regions, cruciform co ntrol rods, and contro l rod drives.

• The biological shie ld is appropriate l y represented as a cylindrical body. 3.2.3 RAMA Calculation Parameters The RAMA transport code uses a three-dimensional deterministic transport method to calculate the neutron flux. The accuracy of the transport method is based on a numerical integration technique that u ses ray-tracing to c h aracter i ze the geometry, anisotropy treatments to determine 3-18 Neutro n Fluence Calculation t h e directional flow of particles, and convergence parameters to determine the overall accuracy o f the flux solution between iterates.

The code allows the user to specify values for each of these parameters.

The primary input parameters that control the ray-tra cing calculation are the distance between parallel rays in the planar and axial dimensions , the depth that a particle is tracked when a reflective boundary is encountered, and the number of equally spaced angles in polar coordinates for tracking the particles. Plant-specific values are determined for each of the parameters.

The RAMA transport calculation employs a treatment for anisotropy that is based on a Legendre expansion of the scattering cross sections.

By default , the RAMA transport calculation uses the maximum order of expansion that is available for each nuclide in the RAMA nuclear data li b rary. For the actinide and zirconium nuclides, a P 5 expansion of the scattering cross sections is used. For all other nuclides, a P 7 expansion of the scattering cross sections is used. T h e overall accuracy of the neutron flux calculation is determined using an iterative technique to converge the flux iterations.

The convergence criterion used in the evaluation was determined by p a rametric study to provide an asymptotic solution for this model. 3.2.4 RAMA Neutron Source Calculation RAMA calculates a neutron source distribution for each tran sport calculation using the in p ut relative power density factors for the fuel region and data from the RAMA nuclear data library. The source distribution changes with fuel bumup; thus, the source is determined using core-specific three-dimensional bumup distributions at frequent intervals throughout a cycle. For the fluence model , t he peripheral fuel assemblies are modeled to preserve the power gradient at the core edge that i s formed from the pin-wise source di str ibutions in these fuel assemblies.

3.2.5 RAMA Fission Spectra RAMA calculates a weighted fission spectrum for each calculation that is based on the relati ve contributions of 235 U, 238 U, 239 Pu , 240 Pu , 2 41 Pu, and 24 Pu isotopes.

The fission spectra for these isotopes are derived from the BUGLE-96 nuclear data library. 3.3 Surveillance Capsule Activation and Fluence Results This section documents the fluence and activation results for the Browns Ferry 2 reactor. The act i vation results also form the basis for the validation and qualification of the application of the RAMA Fluence Me t hodology to the Browns Ferry 2 reactor in accordance with the requirements ofU. S. NRC Regulatory Guide 1.190 (Reg. Guide 1.190). Reg. Guide 1.190 requires fluence calculational methods to be validated by comparison with measurements from operating reactor dosimetry for the specific plant being analyzed or for reactors of similar design. Three flux wire activation ana l yses were performed for the Browns Ferry 2 reactor. Flux wires were removed from the 30° capsule flux wire holder and analyzed at the end of cycle 1 (irradiated for 1.3 EFPY); surveillance capsule flux wires were removed at the end of cycle 7 from the 30° capsule (irradiated for 8.1 EFPY); and surveillance capsule flux wires were removed at the end of cycle 16 from the 120° capsule (irradiated for 22.9 EFPY). Details of the dosimetry specimens and analysis are presented below. 3-19 Ne utron Flu e n ce C al c ul a ti o n Peak fluence was calculated for each of the two removed capsules and the 30° capsule flux wire holder. A ddition a ll y, peak flue nc e was calculated for the 300° capsu l e sti ll in the reactor in support of l ead factor calcu l ations. Lead factors are determined and reported for all capsu l es. 3.3.1 Comparison of Predicted Activation to Plant-specific Measurements The comparison of predicted activation for the Browns Ferry 2 cycles 1 , 7 , and 16 flux w ir es to measurements is presented in this subsection.

Fluence v alues are also calculated and reported in Sectio n 3.3.2 for eac h of the capsule flux wire s. 3.3.1.1 Cycle 1 30° Flux Wire Holder Activation Analysis Copper and iron flux wires were i rra diat ed in the Browns Ferry 2 s ur vei llanc e capsule flux w ir e holder at the 30° azimuth during the first cycle of operation. The wires were removed after being irra di ate d for a total of 1.3 EFPY. Activation measurements were performed fo llo wing irradiation for the following reactions

[1 9]: 6 3 Cu (n , a) 6°Co and 5 4 Fe (n,p) 5 4 Mn. The precise location of the individual wires withi n the surveillance capsule flux wire holder is not known , therefore, the activ a tion calcu l ations were performed at the center of the holder. Table 3-4 provides a comparison of the RAMA calc ul ated specific activities and the measured specific activities for the flux wire specimens.

The cycle 1 total flux wi r e average measured (C/M) value is 0.91 with a standar d deviation of +/-0.02. Table 3-4 Comparison of specific activities for Browns Ferry 2 Cycle 1 30° flux wire holder wires (C/M) Flux Wires Measured Calculated Calculated vs. Standard (dpslmg) (dpS/mg) Measured Deviation Iron I Fe-1 58.11 54.05 0.93 I Fe-2 58.80 54.05 0.92 Fe-3 57.44 54.05 0.94 Average 58.12 54.05 0.93 0.01 Copper Cu-1 3.198 2.808 0.88 Cu-2 3.130 2.808 0.90 Cu-3 3.053 2.808 0.92 Average 3.127 2.808 0.90 0.02 Total Flux Wire 0.91 0.02 Average -----3-20 Ne utron Flu e n ce Cal c ulation 3.3.1.2 Cycle 7 30° Surveillance Capsule Activation Analysis Copper, iron, and nickel flux wires were irradiated in the Bro wns Ferry 2 survei ll ance caps ul e at t h e 3 0° azimuth during th e first 7 cycles of operation.

T h e wires were removed after b ei n g irradiate d for a total of 8.1 EFPY. Activatio n meas ur ements we r e performed following irradi at ion for the fo llo wing reactions

[8): 6 3 Cu (n,a) 6°Co, 54 Fe (n , p) 5 4 Mn , an d 5 8 Ni (n,p) 58 Co. Table 3-5 provide s a comparison of the RAMA ca lcul ated specific activ iti es and the m easure d s p ecific activities for th e surveillance capsu l e flux wire specime n s. The cycle 7 capsule total flux wire average C/M value is 1.20 wit h a stan d ard d eviation of +/-0.06. It is noted t h at the EOC 7 capsu l e comparison shows significant l y more conservatism than the two other do simetry e v aluations at EOC 1 and EOC 16. It was noted in the original capsule eva lu ation [8] that the evaluators also showe d a simi l ar ove re stimate that could impl y t ha t some other circumstance exists ou t side both pre di ctive models that ca u sed the capsu l e to experience l ess activation than predicted , such as a dislocation o f the capsu l e container.

A 20% change in activity can be ca u sed by as little as a 114" variation in radia l positioning of the capsule. Table 3-5 Comparison of specific activities for Browns Ferry 2 cycle 7 30° surveillance capsule flux wires (C/M) Flux Wires Iron Average 1 Copper ---Average 1 Nickel Average 1 Total Flux Wire Average I Measured (dps/g) 6.05E+04 5.62E+03 Calculated (dps/g) 7.74E+04 6.49E+03 1.26E+06 Calculated vs. Measured 1.28 1.15 1.18 1.20 I Standard Deviation 0.06 I 1 The source document for the flux wire measurements only provided an average activity that represents the average of three wires for each wire type. 3.3.1.3 Cycle 16 120° Surveillance Capsule Activation Analysis Copper , iron, and nickel flux wires were irradiated in the Browns Ferry 2 survei llan ce capsule at the 120° azimuth d uring the first 1 6 cycles of operation.

The wires were removed after being irradiated for a total of 22.9 EFPY. Activation measurements were performed fo ll owing irradiation for the following reactions: 63 Cu (n,a) 6°Co, 54 Fe (n , p) 5 4 Mn , and 58 Ni (n , p) 58 Co. Table 3-6 provides a comparison of the RAMA calc ul ated specific activit i es and the measured specific activities for the surve ill ance capsule flux wire s pecimens.

The cycle 16 capsule total flux wire average C/M va lu e is 1.08 with a standard deviation of +/-0.07. 3-2 1 Ne utron F lu e nc e Ca l c ul a tion Table 3-6 Comparison of specific activities for Browns Ferry 2 cycle 16 120° surveillance capsule flux wires (C/M) Fe-G9 Fe-G10 Average Copper Cu-G9 Cu-G10 Average Nickel Ni-G9 Ni-G10 Total Flux Wire Average 80.04 91.95 85.15 91.95 82.60 91.95 13.71 13.70 13.74 13.70 13.73 13.70 1076.30 1226.63 1120.09 1226.63 1098.20 1226.63 3.3.1.4 Surveillance Capsule Activation Analysis Summary 1.15 1.08 1.11 0.05 1.00 1.00 1.00 0.00 1.14 1.10 1.12 0.03 1.08 0.07 Table 3-7 presents a summary of the total average calculated-to-measured result of specific activities for all Browns Ferry 2 flux wires. Combining all flux wires (copper, iron, and nickel), the total average C/M is 1.08 with a standard deviation of +/-0.13. Table 3-7 Comparison of activities for Browns Ferry 2 surveillance capsule flux wires Dosimeter Number of Calculated vs. Standard Measurements Measured Deviation 30° Flux Wire (EOC 1) 6 0.91 0.02 30° Capsule (EOC 7) 9 1.20 0.06 __,. 120° Capsule (EOC 16) 6 1.08 0.07 ----Total 21 1.08 0.13 3-22 Ne utron Flu e nc e Calculati o n 3.3.2 Capsule Peak Fluence Calculations and Lead Factor Determina t ions Peak fast neutron (E > 1.0 MeV) fluences were calculated for each of the capsules originally i n stalled in the Browns Ferry 2 reactor. Of the three original capsules, two have been removed , t h ose being the 30-and 120-degree capsules.

The third capsule, l ocated at 300°, remains in the reactor. The peak fluences for the 30-degree capsule are reported at the time of their respective removal, while the 120-degree capsule has fluence reported at the end of cycle 16 , and at the end of the reactor's extended operating life of 54 EFPY. Additionally, the lead factor for each capsule is calculated by dividing the peak capsule fluence by the respective peak RPV fluence at a given reporting time. The results of these calculations are presented in Table 3-8. Note that since the 300° capsule has not yet been removed , the lead factor and fluence are estimated.

It is observed in Table 3-8 that the lead factors vary between cycles and capsules.

In theory, a p l ant running with a consistent fuel loading pattern and a symmetric power shape will have similar lead factors for all capsules, since the capsules usually reside in symmetric locations.

In the case of Browns Ferry 2, the decreased lead factor between the EOC 7 30° capsule and the EOC 16 120° capsule can be attributed to changing fuel designs, as seen in Table 3-2. Like other fluence predictions , any future changes in any of t h e items l isted in "Limitations of Fluence Projections" will impact the 300° capsule l ead factor predictions.

Table 3-8 Lead fa c tors fo r Browns Ferry 2 30°, 120°, and 300° surveillance capsules Capsule Time of EFPYat Capsule RPVPeak Lead Factor Removal Removal Fluence F lu ence (n/cm 2) (n/cm 2) 30° EOC 7 8.1 EF PY 2.40E+17 2.29E+1 7 1.0 5 I 1---1 20° EOC16 22.9 E FPY 6.4 4 E+17 6.30E+17 1.02 300° E O X L' (est.) 54 EFP Y 1.60E+18 1.58E+1 8 1.01 1 E O X L re prese n ts t he e n d of t h e exte nd ed d esign l ife , which i s ass u med t o rep r ese n t 54 E FP Y. 3.4 Capsule Fluence Uncertainty Analysis Th i s section presents the combined uncertainty analysis and bias determination for the Browns Ferry 2 capsule fluence evaluation.

The combined uncertainty is comprised of the comparison uncertainty factors and an analytic uncertainty factor developed in this section. When combined, these components provide a basis for determining the overall uncertainty (lcr) and bias in the capsule fluence for this a n alysis. The requirements fo r determining the combined uncertainty and bias for light water reactor fluence evaluations are provided in Regulatory Guide 1.190. The method implemented for determining the combined uncertainty and bias for reactor component fluence is described in the RAMA Theory Manual [ 17]. Regarding the determination of a bias in the fluence, Regulatory Guide 1.190 prov i des that an adjustment to the calcu l ated fluence for bias effects is needed if a statistically significant bias exists in the fluence computation.

3-23 Neutron Fluen c e Calculation The results presented in this section show that the combined uncertainty for the Browns Ferry 2 capsule fluence evaluation is 12.2% and that no adjustment for bias effects is required to t h e calculated capsu l e fluence reported in Section 3.3 of this report. The following subsections describe the comparison uncertainties determined in Section 3.3, the determination of the analytic u ncertainty, an d t h e determination of the overall combined uncertainty and bias for t h e Browns Ferry 2 capsule fluence evaluation.

3.4. 1 Comparison Uncertainty Comparison uncertainty factors are determined by comparing calcu l ated activities with activity measurements.

For caps u le fluence eva lu ations, two comparison uncertainty factors are considere d: an operating reactor comparison uncertainty factor and a benc h mark comparison uncertainty factor. The determination of a comparison uncertainty factor based on measurements involves t h e combination of two measurement components.

One component is the variation in the comparison of the calculate d-to-measure d (C/M) activity ratio and the other accounts for t h e uncertainty intro du ced b y the measurement process. 3.4.1.1 Operating Reactor Comparison Uncertain ty The operating reactor, or plant-specific, comparison uncertainty for the Browns Ferry 2 reactor is d etermine d by combining the standard d eviation for t h e act i vity comparisons wit h the measurement uncertainty for t h e plant-specific activ i ty measurements.

3.4.1.2 Ben c hmark Comparison Uncertainty T h e benc h mark comparison uncertainty used in the Browns Ferry 2 uncertainty analysis is based on a set of ind u stry standard s i mulation benc h mark comparisons.

3.4.2 Analytic Uncertainty The calc ul ationa l models use d for fluence analyses are comprised of numerous analytical parameters that h ave associated uncertainties in the i r values. The uncerta i nty in these parameters needs to be tested for its contr i bution to the overa ll fl u ence uncertainty.

The uncertainty values for the geometry parameters are based upon uncertainties in the dimensional data used to construct the plan t geometry model. The uncertainty values for the material parameters are based upon u ncertainties in t h e materia l densities for the water and n u clear fuel materials and the compositiona l makeup of typical steel materials.

The uncertainty values for the fission source parameters are base d upon uncertainties i n the fuel exposure and power factors for the fuel assemblies l oaded on the core periphery. The transport method u sed in the fluence ana l ysis employs a fission source calculation that accounts for the re l ative contributions of the uranium and p lu toni u m fissi l e isotopes in the fuel and the relative power density of the fuel in t h e reactor. Both fission source parameters are derived directly from informa ti on calculated b y three-dime n siona l core s i mulator codes. The u ncerta in ty va l ues for the n u clear cross-section parameters are based u pon uncertainties in t h e number densities for the predominant nuclides that make up t h e reactor materials. 3-24 N e utron F lu e n ce C al c ulat io n T he uncertainty parameters for the fl u ence model inputs are based upon geometry mes hin g and n umerical integration parameters used in the neutron flux transport calcu l atio n. The process for d etermining the geometry meshing and numerical integration parameters invo l ves an exhaustive sensitivity study that is described in the RAMA Procedures Man u al [ 18]. 3.4.3 Combined Uncertainty The combined uncertainty for the capsule fluence evaluat io n is determined with a weighting function that combines the ana l ytic, plant-specific comparison, a nd benchmark comparison uncertainty factors developed in Sections 3.4.1 an d 3.4.2. Table 3-9 shows that the combined u ncerta inty (lcr) determined for the Browns Ferry capsule fluence is 12.2% for energy> 1.0 MeV. Table 3-9 also shows that , in accor d a n ce with Regulatory Guide 1.190 , no bias term ex i sts an d it is not necessary to adjust the RAMA predicted capsu l e fluence in this analysis for bias effects. It is also demonstrat e d in Tab l e 3-9 that the combined uncertainty is within the limits prescribed in U.S. NRC Regulatory Guide 1.190 (i.e. :S 20%). Table 3-9 Combined capsule fluence uncertainty for energy >1.0 MeV Uncertainty Tenn Value Combined Uncertainty (1 o) 12.2% Bias None 1 1 The bias terms are less than the ir constituent uncertainty values , concluding that no statistically significant bias ex ists. 3-25 __J 4 CHARPY TEST DATA 4.1 Charpy Test Procedure Charpy impact tes t s were conducted in accordance with American Society for Testing and Materials (ASTM) Standards E 185-82 and E23-02. The 1982 version of E 185 has been reviewed and approved by NRC for surveillance capsu l e testing applications.

This standard references ASTM E23. The tests were conducted using a Tinius Olsen Testing Machine Company, Inc. Model 84 impact test machine with a 300 ft-lb (406.75 J) energy capacity. The Model 84 is equipped with a dial gage as well as the MPM optical encoder system for accurate absorbed energy measurement.

The machine is also equipped with an instrumented striker, so a total of three independent measurements of the absorbed energy were made for every test. In all cases, the optical encoder measured energy was reported as the impact energy. The optical encoder energy is much more accurate than the analog dial. The optical encoder can resolve the energy to within 0.04 ft-lbs (0.054 J), whereas, for the dial, the resolution is approximately 0.25 ft-lb s (0.34 J). The impact energy was corrected for windage and friction for each test performed. The velocity of the striker at impact was nominally 18 ft/s (5.49 m i s). The MPM encoder system measures the exact impact velocity for every test. Calibration of the machine was verified as specified in ASTM E23, and verification specimens were obtained from the National Institute for Standards and Technology (NIST) and tested in accordance with the standard.

The ASTM E23 procedure for specimen temperature control using an in-situ heating and cooling system was followed.

The advantage of using the MPM in-situ heating/cooling technology is that each specimen is thennally conditioned right up to the instant of impact. Thermal losses associated with liquid bath systems, such as those resulting from transfer from a liquid bath to the test machine, are completely eliminated. Each specimen was held at the desired test temperature for at least 5 minutes prior to testing , and the fracture process zone temperature was held to within+/- l .8° F (+/- 1° C) up to the instant of strike. Precision calibrated tongs were used for specimen centering on the test machine. Lateral expansion (LE) was determined from measurements made with a lateral expansion gage. The lateral expansion gage was calibrated using precision gage blocks which are traceable to NIST. The percentage of shear fracture area was determined by integrating the ductile and brittle fracture areas using t he MPM Digital Optical Comparator (DOC) image analysis system. As shown in Figure 4-1 , each fracture surface image is captured, outlined to delineate the brittle area, and outlined to define the outer ductile fracture region. The DOC software then performs a pixel area integration and automatically calculates the shear fracture area. This method for shear area determination is the most accurate method given in ASTM E23 and is far superior to the commonly used photograph comparison method. The number of Charpy specimens for measurement of the transition region and upper shelf was limited. Therefore , the choice of test temperatures was very important.

Prior to testing, the 4-1 C h a rp y T es t Dat a Charpy energy-temperature curve was predicted using embrittlement models and previous data. The first test was then conducted near the middle of the transition region, and test temperature decisions were then made based on the test results. Overall, the goal was to perform two tests on the upper shelf, and to use the remaining specimens to characterize the 30 ft-lb (41 J) index. This approach was successful and the transition region and upper shelf energy are well defined. Figure 4-1 Illustration of digital optical comparator measurement of shear fracture area First, the Brittle Fracture Area is outlined (within green line). Next , the Outer Ductile Fracture Area is outlined (within red line). Finally, the software integrates the areas and calculates the Percent Shear Fracture Area. 4.2 Charpy Test Data A total of eight irradiated base, weld , and HAZ metal specimens, respectively , were tested over the transition region temperature range and on the upper shelf. The data are summarized in Tables 4-1 through 4-3. In addition to the energy absorbed by the specimen during impact, the measured lateral expansion values and the percentage shear fracture area for each test specimen are provided in the tables. The Charpy energy was acquired from the optical encoder and has been corrected for windage and friction in accordance with ASTM E23. The impact energy is the energy required to initiate and propagate a crack in the Charpy specimen. The optical encoder and the dial cannot correct for tossing energy or losses in the test machine, and therefore this small amount of additional energy, if present, may be included in the data for some tests. The instrumented striker energy does not include tossing energy or machine vibration energy since 4-2 Charp y T e st Data t h e energy, in t h is case, is measured only du ring a few mi ll iseco nd s of contact b etwee n the s tr iker a nd specimen. Base d on co mp arison b etwee n the instrumented striker e n ergy and the o p tica l e n co d e r ene r gy, it has bee n s h own t h at the t ossi n g energy, an d o th er l osses, are sma ll for m ost t es t s. T h e latera l expansio n is a measure of the transverse plast i c deformation prod u ce d by t h e contact e d ge of the striker during the impact event. Latera l expansion is d etermined by meas u ring the maxim u m cha n ge of s p ecime n thickness a l ong the sides of the specimen. Latera l ex p a n sion is a m eas u re of t h e du c ti l i t y of t h e speci m en. T h e nuclear in du stry t racks t h e em b r ittl eme nt s h ift using t h e 35 mil (0.89 mm) l atera l expansio n in d ex. In accorda n ce wit h ASTM E23, t h e latera l expans i on for some specimens, whic h cou ld be broken after the impact test, s h ou l d not be reporte d as broken si n ce the l atera l expans i on of th e unbroken specime n is less than t h at for t h e b roken specimen. Therefore, when th ese co nd itions exist, t h e va lu e listed is t h e u nbroken measureme nt a nd a footnote is inc l u d e d to i d e n tify t h ese specimens. A ll of the 1 20° caps u le specime n s that di d n ot separate during the test co uld be b roken by hand under t h e ASTM E23 r e q uirements. The percentage of shear frac tu re area is a d irect q u an t ifica t ion of t h e transition i n the fracture m odes as the temperature increases.

A ll meta l s wit h a body centered cu b ic lattice structure , s u ch a s ferritic pressure vesse l materials, u n d ergo a transition in fracture modes. At l ow test temperatures , a crack propagates in a b ritt l e manner and cleaves across t h e gra i ns. As t h e te m pera ture i n creases, t h e perce n tage of shear (or du cti l e) fractu r e increases. T hi s temperature ra n ge i s r eferre d to as the tra n sitio n region a nd the fracture process i s mixe d mo d e. As t h e temperature increases further, t h e fracture process is event u ally complete l y ducti l e (i.e., no br i tt l e component) an d th i s temperature ra n ge is referred to as the upper shelf region. Table 4-1 Irradiated Charpy V-Notch impact test results for base metal (heat A0981-1) specimens from the Browns Ferry 2 120° surveillance capsule -105.3 (-76.3) 4.33 (5.8 7) 5.0 (0.1 3) 3.7 E7J -39.5 (-3 9.7) 21.92 (29.72) 1 5.0 (0.38) 11.7 E7C 6.3 (-14.3) 23.08 (31.29) 20.5 (0.52) 20.8 E63 40.1 (4.5) 73.68 (99.90) 54.0 (1.37) 38.2 E75 64.0 (17.8) 99.02 (134.25) 72.5 (1.84) 58.8 ---.--I E74 97.2 (36.2) 107.05 (145.14) 70.5 (1. 79) 60.3 E62 174.7 (79.3) 140.88 (191.01) 9 2.0 (2.34) 1 00.0 E5K 327.9 (164.4) 1 44.72 (196.21) 93.5 (2.37) 100.0 1 All s pecimen IDs have a dot ove r the m i ddle alphanum er i c cha ra cter. 4-3 Charpy T e st Data 4-4 Table 4-2 Irradiated Charpy V-Notch impact test results for weld metal (heat BF2 ESW) specimens from the Browns Ferry 2 120° surveillance capsule -49.7 I (-45.4) 5.47 (7.42) 6.5 (0.17) 4.6 EAL 14.4 (-9.8) 28.06 (38.04) 21.5 (0.55) 12.7 EAE 50.0 (10.0) 47.89 (64.93) 40.0 (1.02) 22.5 EC3 81.3 (27.4) 22.40 (30.37) 25.0 (0.64) 28.3 EBU 119.1 (48.4) 83.90 (113.75) 63.5 (1.61) 50.3 EB6 204.3 (95.7) 102.15 (138.49) 79.0 (2.01) 79.3 ---+ 113.5 3 I (153.92) 1-8 8.0 EAK 301.6 (1 4 9.8) (2.24) 100.0 EAD 373.8 (189.9) 110.62 (149.98) 84.5 (2.15) 100.0 1 All specimen IDs have a dot over t he middle alphanumeric character. Table 4-3 Irradiated Charpy V-Notch impact test results for HAZ specimens from the Browns Ferry 2 120° surveillance capsule 109 5 ( 78 6) 217 (2 94) 05 (0 01) 5 1 --I I EDK -70.6 (-57.0) 22.95 (31.12) 14.0 (0.36) I 15.7 I I I I I EEL -12.5 I (-24.7) I 45.17 (61.24) 35.5 (0.90) 23.6 EE6 23.5 (-4.7) 62.35 (84.53) 48.0 (1.22) 35.8 I I EEJ 47.3 (8.5) 92.68 (125.66) 70.0 (1.78) 5 3.0 I I i I I ED5 72.0 (22.2) 112.58 (152.64) 76.5 (1.94) 80.7 I 1 122.64 : (166.28) I I EEA 181.6 (83.1) 84.5 I (2.15) I 100.0 EET 300.9 (149.4) 141.24 (191.49) 91.5 (2.32) 100.0 1 All specimen IDs have a dot over the m i ddle alphanumeric ch a racte r. Note: HAZ test results are not used in t he BWRVIP ISP.

5 CHARPYTEST RESULTS 5.1 Analysis of Impact Test Results For ana l ysis of the Charpy test data , the BWRVIP ISP has selected the hyperbolic tangent (tanh) function as the statistical curve-fit tool to model the transition temperature toughness data. A hyperbolic tangen t curve-fitting program named CVGRAPH [10] was used to fit the Charpy n o tch energy and lateral expansion data. Analysis methodology (e.g., definition of upper fixed shelf and lower shelf) followed the BWRVIP conventions established for analysis of all ISP data [2 1 , 22]. The imp ac t energy curve-fits from CVGRAPH are provided in Figures 5-1 (plate A0981-1) and 5-3 (weld BF2 ESW), and the lateral expansion curve-fits are s hown in Figures 5-2 (plate A0981-1) and 5-4 (weld BF2 ESW). Because HAZ results are not used in the BWRVIP ISP, that data was not fit. For the analysis of Charpy energy test data , lower shelf energy was fixed at 2.5 ft-lbs (3.4 J). Upper shelf energy was fixed at the average of all test energies exhibiting shear greater than or equal to 95%, consistent with ASTM Standard E185-82 [3]. For analysis of the l ateral expansion te s t data, the lower shelf was fixed at 1.0 mils; the fixed upper shelf was defined as the average of the lateral expansion test data points at the same test temperatures used to define the fixed upper shelf energy. 5.2 Irradiated Versus Unirradiated CVN Properties Table 5-1 summarizes the T 30 [30 ft-lb (41 J) Transition Temperature], T3 s miI [35 mil (0.89 mm) Lateral Expansion Temperature], Tso [50 ft-lb (68 J) Transition Temperature], and Upper Shelf Energy for the unirradiated and irradiated materials and shows the change (shift) from baseline values. The unirradiated values of T 3 0 and T s o were taken from the CV GRAPH fits provided in Figures 2-3 and 2-4; the unirradiated values ofT 3 s miI were previously determined in [21, 22]. The irradiated values are from the index temperature s determined in Figures 5-1 through 5-4. Table 5-2 provides a comparison of the measured shifts to predicted shifts for plate heat A0981-1 and weld heat BF2 ES W. Predicted shift is based on the formula provided in Reg. Guide 1.99 Rev. 2 [6] and shown in Note 2 to the table. The fluence was input as 6.44 x 10 17 n/cm 2 , as reported in Section 3 for the 120° capsule. For surveillance plate heat A0981-1, the measured shift is within the value expected (e.g., the measured shift is l ess than predicted shift+ margin); however, the measured shift for weld heat BF2 ES W is about 15% greater than the predicted shift + margin. Measured percent decrease in USE is presented in Table 5-3 and compared to the percent decrease predicted by Figure 2 of Reg. Guide 1.99, Rev. 2. For both the surveillance plate and weld, the measured percent decrease is les s than the predicted percent decrease.

5-1 C harp y Test R es ult s 5-2 Irr a diat e d Plat e H e at A 0981-1 CVE (BF2-120) C V G RAPH 5.0.2 H yper b o li c Ta n ge n t Cur ve Print ed o n 0 9/23/2 01 2 01: 1 9 P M P age 1 300 250 .! 'T 200 0 0 u. 150 l!! w z () 100 50 0 -300 Temper a ture -1 0 5.30 -3 9. 5 0 6. 3 0 4 0. 1 0 6 4. 00 9 7. 2 0 1 74.70 3 2 7.9 0 Figure 5-1 Coeff i c i e nt s of C ur ve 1 A = 72.65 B = 70.1 5 C = 69.29 T O= 45.34 D = 0.0 0 E+OO E qu a ti on is A+ B * [T anb ((T-To)/(C+D n)J U pp e r S h e lf E n e r gy=14 2.8(F i xe d) L ower S h e l f Energy=2.5(F i xed) Te mp@3 0 ft-l b s=-3.5 D eg F T e mp@50 ft-l b s=22.2 D eg F P lan t: BRO WNS FE RRY 2 Ma t e ria l: SA302BM Hea t: A098 1-1 Ori en t a ti o n: L T Ca p s u l e: 1 20 DE F lu e n c e: n/cm" 2 -n / A I I _:Yo -200 -100 0 100 200 300 400 500 600 Temperature in Deg F C h a rp y V-N otch D ata InputCVN Com pu t ed C VN Differ e nti a l 4. 3 3 4. 2 9 . 04 2 1. 9 2 13. 6 6 8. 2 6 2 3. 0 8 3 6. 8 4 -13.7 6 7 3. 6 8 6 7. 3 6 6. 3 2 99. 0 2 9 I. 1 0 7. 9 2 107. 05 1 1 7. 14 -1 0. 0 9 1 4 0. 88 1 3 9. 5 3 1. 3 5 144. 7 2 14 2. 7 6 1. 9 6 Corre l a t i on C o efficien t= .9 8 9 Irradiated plate A0981-1 (Browns Ferry 2 120° capsule) Charpy energy plot C harp y T est R esu lt s Irradiated Plate Heat A0981-1 LE (BF2-120)

C VGRAPH 5.0.2 Hyperb o li c T a n ge nt Curv e Printed o n 09 12 3/2 01 2 01:25 PM P age 1 200 150 JQ E c .2 ! !. 100 d1 -e 50 0 -300 Temperature

-105.30 -39. 50 6. 30 40. 1 0 64. 00 9 7. 2 0 174.70 327.90 Figure 5-2 Coe ffi c i e nts o f C ur ve 1 A = 46.88 B = 45.88 C = 69.83 TO = 34.81 D = 0.00E+OO E quati o n is A+ B * [T anh ((T-To)/(C

+D 1))] U pp e r S h e lf L.E.=92.8(Fixe d) Lowe r S h e lf L.E.=1.0(F i xe d) T em p.@L.E. 35 mils=l 6.4 D eg F P l ant: BR OWNS FE RRY 2 Ma t e ri a l: SA302 B M H ea t: A098 1-l O ri e nt a ti o n: LT Caps ul e: 1 20 DE F lu e n ce: n/cm"2 -r v Jo 0 300 Temperature in Deg F Char p y V-Notch Data Input L.E. Comp u ted L.E. 5. 00 15. 00 20. 50 5 4. 00 7 2. 50 7-0. 50 9 2. 00 9 3. 5 0 Corre l at i on Coefficient=

.986 2. 6 3 1 0. 7 6 2 9. 1 2 50. 34 6 5. 0 I 7 9. 59 9 1. 11 9 2. 7 3 600 Diffe r ential 2. 3 7 4. 24 -8. 6 2 3. 66 7. 4 9 -9. 0 9 . 8 9 . 7 7 I rradiated plate A0981-1 (Browns Ferry 2 120° capsule) lateral expansion plot 5-3 C harp y T est R esu lt s 5-4 Irradiated W e ld He at B F2 ESW CVE (B F2-1 20) CVGRAPH 5.0.2 H yper bolic Tangent Curve Printed o n 09123/2012 01:27 PM P age 1 3 00 2 5 0 .! 'j' 200 0 if 150 ! w z (; 100 50 0 -300 Temperature

-49.70 14. 40 50. 00 8 1. 3 0 119.1 0 204.30 30 1. 60 373. 80 Figure 5-3 Coefficients of Curve 1 A = 5 7.29 B = 54.7 9 C = 99.55 TO= 94.15 D = O.OOE+OO Eq u atio n is A+ B * [Tanh((T-To)/(C+

D T))] Uppe r S h e lf Energy=l 12. l (F i xed) Lower She l f Energy=2.5(Fixed)

Tem p@30 ft-l b s=39.8 De g F Temp@5 0 ft-lb s=80.9 Deg F Plant: BROWNS FERRY 2 Material: ESW Heat: ESW Orientation

NA Caps ul e: 1 20 DE F lu e n ce: n/cm" 2 " :: ....--v / ----V o -200 -100 0 100 200 300 400 500 600 Temperature in Deg F C h ar p y V-Notc h Data Input CVN Com puted CVN Differential

5. 4 7 8. 2 7 -2. 8 0 2 8. 0 6 20. 87 7. 1 9 4 7. 8 9 34. 4 7 13. 42 2 2. 40 50. 26 -2 7. 8 6 8 3. 9 0 7 0. 7 4 13. 16 1 02. 15 101. 28 . 8 7 11 3.53 110.41 3. 1 2 110.62 111. 68 -1. 0 6 Corre l ation Coefficien t= .954 Irradiated weld BF2 ESW (B r owns Ferry 2 120° capsule) Charpy energy plot C harp y T e st R es ults Irradiated Weld Heat BF2 ESW LE (BF2-120)

C VGRAPH 5.0.2 Hyperbolic T a n ge nt Curve Prin t ed o n 09/23/201 2 01:29 PM P age 1 200 150 .IQ E c .2 I! ! 100 di 1! 50 0 -300 Tem p erature -49. 7 0 14. 40 50. 00 81. 3 0 119.1 0 204. 30 301. 60 373. 80 F igure 5-4 Coefficients of Curve 1 A = 43.63 B = 42.63 C = 108.46 TO= 85.22 D = 0.00E+OO E quati o n is A+ B * [Tanh((T-T o)/(C+Dn)] U pp e r Shelf L.E.=8 6.3(Fixe.d) L owe r S h e lf L.E.=l.O(Fixed) T em p.@L.E. 35 mil s=63.0 D eg F Plant: BROWNS FE RRY 2 M ate rial: ESW Heat: ESW Ori e ntati o n: NA Ca p s ul e: 1 20 DE F lu e n ce: t> *y-/ __/ 0 300 Temperature in Deg F Charpy V-Notch Data Input L.E. 6. 50 21. 5 0 4 0. 00 25. 00 63. 50 7 9. 00 8 8. 0 0 8 4. 5 0 Corre lati o n Coefficien t = . 967 Computed L.E. 7. 54 19. 1 7 3 0. 25 42. 09 56. 5 2 7 7. 7 1 8 4. 7 0 8 5. 8 4 n/c m" 2 600 Differential

-1. 04 2. 3 3 9. 7 5 -17.0 9 6. 9 8 1. 2 9 3. 3 0 -1. 3 4 I rradiated weld BF2 ESW (Browns Ferry 2 120° capsule) lateral expansion plot 5-5 Cha rp y T est R esu lt s 5-6 Table 5-1 Effect of irradiation (E>1.0 MeV) on the notch toughness properties Irradiated OF (OC) OF (OC) OF (O C) OF (OC) A0981-1 -46.7 -3.5 43.2 1 -14.8 22.2 J 37.0 -25.4 16.4 41.8 137.8 142.8 (LT) (-43.7) (-19.7) (24.0) (-26.0) (-5.4) (20.6) l (-31.9) (-8.7) (23.2) (186.8) (193.6) BF2 ESW -52.5 39.8 92.3 -19.5 80.9 100.4 -29.5 63.0 92.5 116.0 112.1 (-46.9) (4.3) (51.3) (-28.6) I (27.2) (55.8) (-34.2) I (17 .2) (51.4) (157.3) (152.0) Table 5-2 Comparison of actual versus predicted embrittlement A0981-1 Browns Ferry 2 Plate (SA533B-1) 6.44 43.2 1 32.7 } 65.43 (LT orientation)

(24.0) (18.17) (36.35) BF2 ESW Browns Ferry Unit 2 surveillance weld 1 6.44 92.3 40.24 80.45 (51 1}_ (22.36) (44.72) Notes: 1. See Table 5-1 , il T30. 2. Predicted shift= CF x FF , where CF is a Chemistry Factor taken from tables from USN RC Reg. Guide 1.99, Rev. 2 (6], based on the material's Cu/Ni content , and FF is Fluence Factor, f0.28-0.10 log f , where f = fluence (10 19 n/cm 2 , E > 1.0 MeV) specified.

l 3. Margin Term is defined as 34°F for plate materials and 56°F for weld materials , or margin equals shift (whichever is l ess), per Reg. Guide 1.99 , Rev. 2 (6]. 5.0 (6.8) -3.9 (-5.3)

Table 5-3 Percent decrease in upper shelf energy Identity A0981-1 BF2 ESW Notes: Material Browns Ferry 2 Plate A0981-1 Browns Ferry 2 ESW Fluence (x10 17 n/cm 2) 6.44 6.44 Cu Content (wt%) 0.14 0.20 C h a rp y T est R es ult s Measured Predicted Decrease Decrease in In USE 2 USE 1 (%) (%) -3.63 12.0 r 3.36 17.8 1. Calculated from Table 5-1 , (Change/Un irradiated

)* 100. A positive number indicates a decrease in USE; a negative number indicates the USE increased over the unirradiated value. 2. Based on extrapolation of and interpolation between the curves given in Figure 2 of Reg. Guide 1.99 Rev. 2 [6]. 5-7 6 REFERENCES

1. 10 CFR 50, Appendices G (Fracture Toughness Requirements) and H (Reactor Vessel Material Surveillance Program R equire m ents), Federal Register , Volume 60, No. 243, dated December 19 , 1995. 2. American Soc i ety of Mechanica l Engineers (ASME) Boiler and Pressure Vessel Code (Code),Section XI, "Rules for Inservice Inspection of Nuclear Power Plant Components," Nonmandatory Appendix G, Fracture Toughness Criteria for Protection Against Failure. 3. ASTM E185-82, Standard Practice for Conducting Surveillance Tests for Light-Water Cooled Nuclear Power Reactor Vessels, E706 (IF), ASTM Standards, Section 3, American Society for Testing and Materia l s, Philadelphia, PA, 1993. 4. BWRVIP-86 , Revision 1-A: BWR Vessel and Internals Proj ect, Updated BWR Int egra ted Surveillance Program (IS P) Implementation Plan. EPRI, Palo Alto, CA: 2012. 1025144. 5. 10 CFR 50, Appendix B, "Quality Assurance Criteria for Nuclear Power Plants and Fuel Reprocessing Plants." 6. U.S. NRC Regulatory Guide 1.99, "Radiation Embrittlement of Reactor Vessel Materials," Revision 2, May 1988. 7. "Guideline for the Management of Materia l s Issues," NEI 03-08, Nuclear Energy Institute , Washington, DC , Latest Edition. 8. " Browns Ferry Steam Electric Station Unit 2 Vessel Surveillance Materials Testing and Fracture Toughness Analysis", C. Oza, GE Nuclear Energy, GENE-B 1100639-01, Revision 1, August, 1995. 9. Letter from R.H. Shell (TVA) to USNRC , "Browns Ferry Nuclear Plant , Sequoyah Nuclear Plant, and Watt s Barr Nuclear Plant-Response to Generic Letter 92-01 (Reactor Vessel Structural Integrity)," Tennessee Valley Authority , dated July 7 , 1992. 10. CVGRAPH, Hyperbo l ic Tangent Curve Fitting Program, Developed by EPRI, Version 5.0.2, Revision 1 , 3/26/02. 11. "Ca lculationa l and Dosimetry Methods for Determining Pressure Vessel Neutron Fluence," Nuclear Regulatory Commission Regulatory Guide 1.190, March 2001. 12. BWRVIP-126:

BWR Vessel Int erna ls Proj ect, RAMA Fluence M ethodo logy Software, Version 1.0. EPRI, Palo Alto, CA: 2003. 1007823. 13. Letter from William H. Bateman (U.S. NRC) to Bill Eaton (BWRVIP), Safety Evaluation o f Proprietary EPRI Reports BWRVIP-114, -115, -117, and -121 and TWE-PSE-001

-R-001. dated May 13, 2005. 6-1 R e f e r e n ces 14. Letter from Matthew A. Mitchell (U.S. NRC) to Rick Libra (BWRVIP), "Safety Evaluation of Proprietary EPRI Report B WR Vessel and Internals Project, Evaluation of Susquehanna Unit 2 Top Guide and Core Shroud Material Samples Using RAMA Fluenc(f Methodology (BWRVIP-145)," dated February 7, 2008. 15. " BUGLE-96: Coupled 47 Neutron, 20 Gamma-Ray Group Cross Section Library Derived from ENDF/B-VI for LWR Shielding and Pressure Vessel Dosimetry Applications," RSICC Data Library Collection, DL2C-185, March 1996. 16. "VITAMIN-B6:

A Fine-Group Cross Section Library Based on ENDF/B-VI Release 3 for Radiation Transport Applications

, RSICC Data Library Collection, DL2C-l 84 , December 1996. 17. BWRVIP-114-A:

BWR V e ssel and Int e rnals Proj e ct , RAMA Fluen ce Methodolo gy Th e ory Manual, EPRI, Palo Alto , CA: 2009. 1019049. 18. BWRVIP-121-A

BWR V es s e l and Int e rnals Proj e ct , RAMA Fluen ce M e thodolo gy Pro ce dur e s Manual, EPRI , Palo Alto , CA: 2009. 1019052. 19. Analysis of the Vessel Wall Neutron Dosim e ter from Browns Ferry Unit 2 Pressu r e Vessel, Southwest Research Institute , 02-4884-002 , Rev. 0, September 1979. 20. ASTM Standard E23, 2002, "Standard Test Methods for Notch Bar Impact Testing of Metallic Materials," ASTM International , West Conshohocken , PA , 2002 , DOI: 1O.l520/E 0023-02 , www.astm.org. 21. BWRVIP-135 , R e vision 2: BWR V e ss e l and Int e rnals Proj ec t, Int eg rat e d Surv e illan ce Program (ISP) Data Sourc e Book and Plant Evaluation

s. EPRI , Palo Alto , CA: 2009. 1020231. 22. BWRVIP Letter 2010-238 , Errata for BWRVIP-135 , Rev. 2 , October 15 , 2010. 6-2 A APPENDIX A -DOSIMETER ANALYSIS A.1 Dosimeter Material Description The 120° Browns Ferry Unit 2 (BF2) surveillance capsule primary dosimeter materials are pure metal wires which were located within the surveillance capsule Charpy packets. The wire types provided for the Browns Ferry Unit 2 surveillance program are copper, iron , and nickel. Each wire is about three inches (7 .62 cm) long w ith one of each type included in the two Charpy specimen packets. A.2 Dosimeter Cleaning and Mass Measurement At the time the Charpy packets were opened, the dosimeter wires were cleaned with wipes that were wetted with acetone to remove loose contamination.

Upon receipt at the radiometric lab , the wires were visually inspected and cleaned with a lab wipe soaked in pure ethanol. The wire segments were then examined under a low magnification optical microscope.

There was evidence of oxidation indicating the need for chemical etching and further cleaning.

This was accomplished by soaking the Fe wire segments in a 4N solution of hydrochloric acid until the oxidation was etched from the surface. Similarly , the Ni and Cu wires were immersed in a 2N solution of nitric acid solution.

The wires were then rinsed with distilled water, wiped once more with ethanol , and then allowed to dry in air at room temperature.

The wires then exhibited a clean, shiny appearance.

Figures A-1 through A-6 show low-power magnifications of the dosimetry wires as they were found prior to cleaning , and after cleaning and coiling. In general , the iron and copper wires had experienced the most oxidation , while the nickel wires were relatively clean at the time of recovery from the Charpy packets. The tota l mass of each wire was measured using a Mettler Toledo XS 105DU ana l ytical digital balance. Table A-1 lists the results of these measurements, as well as the identification assigned to each dosimeter.

The dosimeters identifications were assigned as the Charpy packet numbers fo ll owed by the type of dosimeter material.

As previously mentioned, the wires were tightly coi l ed for subsequent counting and weighing. Each wire was wrapped around a thin metal rod to form a coil of approximately 0.5 inch (12.7 mm) diameter or less, w hi ch yields a reasonable approximation to a point source geometry at the distance the dosimeter wires are placed from the gamma detector.

The coiled wire segments were pressed firmly against a hard surface to flatten the coil to yield the best counting geometry A-1 Appendix A -Dosimeter Analysis G9Cu G9Cu Figure A-1 Packet G9 Cu dosimeter wire: prior to cleaning (left); and after cleaning/coiling (right) G9Fe G9Fe 0 Figure A-2 Packet G9 Fe dosimeter wire: prior to cleaning (left); and after cleaning/coiling (right) G9Ni G9Ni Figure A-3 Packet G9 Ni dosimeter wire: prior to cleaning (left); and after cleaning/coiling (right) A-2 Appendix A -Dosi m eter A n a l ysis GlOCu GlOCu Figure A-4 Packet G10 Cu dosimeter wire: prior to cleaning (left); and after cleaning/coiling (right) GlOFe GlOFe Figure A-5 Packet G10 Fe dosimeter wire: prior to cleaning (left); and after cleaning/coiling (right) GlONi GlONi Figure A-6 Packet G10 Ni dosimeter Wire: prior to cleaning (left); and after cleaning/coiling (right) A-3 App e ndix A -Do s im e ter An a l ys is Table A-1 Wire dosimeter masses Wire Dosimeter ID Mass (mg) G9 Cu 361.65 G9 Fe 159.02 G9 Ni 320.05 G10 Cu 360.86 G10 Fe 160.34 G10 Ni 318.77 A.3 Radiometric Analysis Radiometric ana l ysis was performed using high resolution gamma emission spectroscopy.

In this method, gamma emissions from the dosimeter materials are detected and quantified using state gamma ray detectors and computer-based signa l processing and spectrum analysis.

The specifications of the gamma ray spectrometer system (GRSS) are listed in Table A-2. The GRSS features a hyper pure germanium (HPGe) detector that is housed in a lead-copper shield to reduce background count rates. Standard background subtraction procedures were used. GRSS calibration was performed using a National Institute for Standards and Technology (NIST) traceable mixed gamma quasi-point source. The Canberra analysis software provides the capability for energy resolution and efficiency ca l ibration using specified standard source information.

Calibration information is stored on magnetic disk for use by the spectrographic ana l ysis software package. Since detector efficiency depends on the source-detector geometry , a fixed, reproducible geometry must be selected for the gamma spectrographic analysis of the dosimeter materials.

For the dosimeter wires, the counting geometry was that of a quasi-point source (coiled wire) placed five inches (12.7 cm) vertically from the top surface of the detector shell. In this way , extended sources up to 0.5 inch (1.27 cm) can be analyzed with a good approximation to a point source. The coi l ed wires were well within the area needed to approximate a point source geometry.

The HPGe detector was calibrated for efficiency using the NIST traceable source. The accuracy of the efficiency calibration was checked using a gamma spectrographic analysis of the NIST traceable mixed gamma source. The isotopes contained in the s ource emit gamma rays which span the energy response of the detector for the dosim e ter mat e rials. These measurements show that the efficiency calibration is providing a valid mea s urement of source activity. The acceptance criteria for these measurements are that the software must yie ld a valid isotopic identification , and that t h e quantified activity of each correctly identified isotope must be within the uncertainty specified in the source certification.

Validation of system performance was performed prior to starting the counting tasks , an d upon completion of all counting work for BF2. The counting system p e rformance was acceptable in each case, indicating that the counting system properties did not change during the course of the counting procedure.

A-4 Appendix A -Dosim e t er Analysis Table A-3 shows the counting schedule established for this work. There was no requirement for order of counting, since the dosimeter materials still contained sufficient quantities of activation products to allow accurate radio assay. Counting times were more than sufficient to achieve the d e sired statistical accuracy for gamma emissions of interest in all cases. N eutrons interact with the constituent nuclei of the do simeter materials, producing radionuclides i n varying amounts depending on total neutron fluence , its energy spectrum, an d the nuclear properties of the dosimeter materials.

Table A-4 lists the reactions of interest and their resultant ra dionuclide prod u cts for each element contained in the dosimeters.

These are threshold reactions involving an n-p or n-a interaction. F i nally, Table A-5 presents the primary results of interest for flux and fluence detennination.

The s p ecific activity units are in dps/mg, which nonnalizes the activity to dosimeter mass. The a c tivities are speci fi ed for a useful reference date/time , w hich in this case is the BF2 plant shutdown date and time. This reference date/time was spec ifi ed as February 26, 2011, at 1 2:00:00 AM EST. Table A-2 GRSS specifications S ystem Component Description and/or Specificati o ns Detector Canberra Mode l GC1518 Energy Resolut i on 1.8keV @ 1.33 MeV Detector Efficiency (relative to a 3 inch x 3 inch 15% at 1.3 MeV (7.62 cm x 7.62 cm) Nal crystal) Amplifier/Multichannel Analyzer Canberra DAS-1000 Computer System Intel i5-2500 CPU at 3.30 GHz ,, 2.91 GB Main Memory , 931 GB Hard Disk , 17-inch Monitor , HP Laser Jet Printer Software Canberra Apex v 1 .2 A-5 A pp e n dix A -Do s im e ter Analys i s Table A-3 Counting schedule for the dosimeter materials Dosimeter ID Count Start Date Count Start Time (ET) Count Duration (Live Time Seconds) G9 Cu 08/18/12 2: 04 PM 86 , 400 G9 Fe 08/17/12 1:34 PM 86,400 G9 Ni 08/20/12 6: 51 AM 86,400 G10 Cu 08/22/12 8:05 AM 86 , 400 G10 Fe 08/21/12 7:48 AM 86,400 G10 Ni 08/23/12 8:47 AM 86,400 Table A-4 Neutron-induced reactions of interest Dosimeter Material Neutron-Induced Reaction Reaction Product Radionuclide Iron Fe 54 (n , p)Mn 54 Mn 54 Copper Cu 6 3{ n , a )Co 60 Co so N i ckel Ni 58 (n.p)Co 58 Co ss Table A-5 Results of the radiometric analysis Activity at Specific Reference Activity at Activity Dosimeter ID Isotope ID Date/Time*

Reference (IJCi) Date/Time* Uncertainty(%) (dps/mg) G9 Cu 60Co 1.34E-01 13.71 1.90 G9 Fe 54Mn 3.44E-01 80.04 2.56 G9 Ni 58Co 9.31 E+OO 1076.30 2.74 G10 Cu 60Co 1.34E-01 13.74 1.90 G10 Fe 54Mn 3.69E-01 85.15 2.56 G10 Ni 58Co 9.65E+OO 1120.09 2.76 *February 26 , 2011 at 12: 00: 00 AM EST is the reference date and time. A-6 Export Control Restriction s Access to and use of EPRI Intellectual Property is granted with the cific understanding a n d req ui rement tha t responsibi li ty for ensuring full compliance with all applicable U.S. and foreign export laws and regulations is being undertaken by you and your company. This includes an obliga t ion to ensure that any individual receiving access hereunder who is not a U.S. cit i ze n or permanent U.S. resident i s permitted access under applicable U.S. and foreign expor t l aws and regulations.

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