ML18139B520
| ML18139B520 | |
| Person / Time | |
|---|---|
| Site: | Surry  |
| Issue date: | 09/30/1981 |
| From: | Lozito E, Snow C VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.) |
| To: | |
| Shared Package | |
| ML18139B519 | List: |
| References | |
| VEP-FRD-44, NUDOCS 8109150136 | |
| Download: ML18139B520 (76) | |
Text
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*vepco SURRY UNIT 1, CYCLE i6 . .
- STARTu*:p .PHYSlCS TES.T REPOR.T
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. 8109150136 810909
[ PDR AOOCK 05000280
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* *: FUEL I ESOU*I CES D:E PA I TI EI T c,** : ~**--* _.: ..,.v I RC I Ill ELE CT11 C Po* WE I COI PI NY
VEP-FRD-4lJ SURRY UNIT 1, CYCLE 6
*STARTUP PHYSICS TEST REPORT BY vAY H. LEBERSTIEN 1 Reviewed By:
C. T. Snow, Nuclear Fuel Engineer Nuclear Fuel Operation Subsection Subsection Nuclear Fuel Operation Subsection Fuel Resources Department Virginia Electric and Power Co. Richmond, Va. September, 1981
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CLASSIFICATION/DISCLAIMER The data, techniques, information, and conclusions in this report have been prepared solely for use by the Virginia Electric and Power Company (the Company), and they may not be appropriate for use in situations otlier than those fo:r which they were specifically prepared. The Company therefore makes no claim or warranty whatsoever, express or irnplied,as to thei:r accuracy, usefulness, o:r applicability. In particular, THE COMPANY MAKES NO WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, NOR SHALL ANY WARRANTY BE DEEMED TO ARISE FROM COURSE OF DEALING OR USAGE OF TRADE, with respect to this report or any of the data, techniques, information, or conclusions in it. By making this
" report available, the Company does not authorize its use by others, and ~ any such use is expressly forbidden except with the prior written approval of the Company. Any such written approval shall itself be deemed to inco:rpo:rate the disclaime:rs of liability and disclaimers of warranties provided he:rein. In no event shall the Company be liable, under any legal theo:ry ~hatsoever (whether cont:ract, tort, wa:rzanty, or .strict or absolute liability), f6r any property damage, mental or physical injury o:r death, loss of use of property, or other damage resulting from or arising out of the use, authorized or unauthorized, of this repo:rt or the dat~, techniques, information, or conclusions in it .
i
ACKNOWLEDGEMENTS The author would like to acknowledge the coope:i:at~on of the Surry Powe:i: Station pe:i:sonnel in pe:i:forming the tests documented in this repo:i:t. Also, the autho:i: would like to exp:i:ess his g:i:atitude to Mr. C. T. Snow, and D:i:. E. J. Lozito fo:i: their aid and guidance in p:i:epa:i:ing this :i:epo:i:t. I ii I
' TABLE OF CONTENTS SECTION TITLE PAGE NO.
Classification/Disclaimer.................. i Acknowledgements ........... ,* . ~ ... .......... ii List of Tables. . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv List of Figures . . . . . . . . . . . . . . . . . . . . . . . *. . . . . v Preface. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vi Introduction and Summary . . . . . . . . . . . . . . . . . . . 1 2 Control Rod Drop Time Measurements ........ . 10 3 Reactor Coolant System Flow Measurement ... . 15 4 *control Rod Bank Worth Measurements ....... . 17 5 Boron Endpoint and Worth Measurements ..... . 22 6 Temperature Coefficient Measurements ...... . 26 7 Power Distribution Measurements . . . . . . . . . . . . 31 I 8 References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43 APPENDIX Startup Physics Test Results and Evaluation Sheets................ . . . . . . . . . . A. 1 iii
LIST OF TABLES TABLE TITLE PAGE HO. I.11 1. 1 Ch:ronology of Tests. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
- 2. 1 Hot Rod D:rop Time Summa:ry.. .. . .. .... ... . .. . .. ... . .. 12
- 3. 1 Reacto:r Coolant System Flow Measu:rement Summary.... .16
- 4. 1 Cont:rol Rod Bank Worth Summa:ry... ...... ... . .. . . . . .. 19
- 5. 1 Bo:ron Endpoints Summary............................ 24
- 6. 1 Isothermal Temperature Coefficient Summary......... 28
- 7. 1 Incore Flux Map Summary............................ 33 7.2 Compa:rison of Measured Power Distribution Pa:ram-eters With Thei:r Technical Specifications Limits... 34
- iv
LIST OF FIGURES FIGURE TITLE PAGE NO.
- 1. 1 Co:re Loading Map. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 1.2 Beginning of Cycle Fuel Assembly Bu:rnups.. .. . . . . . . . . . .... 6
- 1. 3 Inco:re Inst:rumentation Locations......................... 7
- 1. 4 Bu:rnable Poison and Sou:rce Assembly Locations............ 8
- 1. 5 Cont:rol Rod Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . *. . 9
- 2. 1 Typical Rod D:rop T:race. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
- 2. 2 Rod D:rop Time - Hot Full Flow Conditions . . . . . . . . . . . . . ~... 14
- 4. 1 Bank B Integ:ral Rod Wo:rth................................. 20 4.2 Bank B Diffe:rential Rod Wo:rth........ . . . . . . . . . . . ... . . . . .. . 21
- 5. 1 Bo:ron Wo:rth Coefficient.................................. 25
- .,;
- 6. 1 Isothe:rmal Tempe:ratu:re Coefficient - HZP, ARO............ 29 6.2 Isothe:rmal Tempe:ratu:re Coefficient - HZP, B-Bank In...... 30
- 7. 1 Assembly Powe:r Dist:ribution - HZP, ARO................... 35 7.2 Assembly Powe:r Dist:ribution - HZP, B-Bank I n . . . . . . . . . . . . . 36 7.3 Assemb~y Powe:r Dist:ribution - I/E Cal. - Flux Map . . . . . . . . 37 7.4 Assembly Powe:r Dist:ribution - I/E Cal. - Flux Map . . . . . . . . 38 7.5 Assembly Powe:r Dist:ribution - I/E Cal. - Flux Map . . . . . . . . 39 7.6 Assembly Power Dist:ribution - I/E Cal. - Flux Map . . . . . . . . 40 7.7 Assembly Powe:r Dist:ribution - I/E Cal. - Flux Map . . . . . . . . 41 7.8 Assembly Powe:r Dist:ribution - HFP, Eq. Xenon . . . . . . . . . . . . . 42 V
PREFACE The purpose of this report is to present the analysis and evaluation of the physics tests which were performed to verify that the Surry 1, Cycle 6 core could be operated safely, and to make an initial evaluation of the performance of the core. It is not the intent of this
- report to discuss the particular methods of testing or to present the detailed data taken. Standard test techniques and methods of data analysis were used. The test data, results and evaluations, together with the detailed startup procedures, are on file at the Surry Power Station. The:refo:re, only a cursory discussion of these items is included in this report. The analyses presented includes a brief summary of each test, a comparision of the test results with design predictions, and an evaluation of the :results.
The Surry 1, Cycle 6 Startup Physics Tests Results and Evaluation Sheets have been included as an appendix to provide additional info:rmat~on on the startup test :results. Each data sheet provides the following information: 1) test identification, 2) test conditions (design), 3) test conditions (actual), q) test results, 5) acceptance criteria, and 6) comments concerning the test. These sheets provide a compact summary of the startup test results in a consistent format. The design test conditions and design values of the measured parameters were completed p:cio:c to startup physics testing. The entries for the design values were based on the calculations performed by Vepco's Nuclear Fuel Engineering G:coup.1 During the tests, the data sheets were used as guidelines both to verify that the proper test conditions were met and vi
to facilitate the preliminary comparison between measu~ed and predicted test results, thus enabling a quick identification of possible problems occuring during the tests .. The AppendiK to this report contains the final completed and approved version of the startup Physics Tests Results and Evaluation Sheets. vii
Section 1 INTRODUCTION AND
SUMMARY
On September 14, 1980 Unit No. 1 of the Surry Power Station was shutdown for its fifth refueling. During this shutdown, 76 of the 157 fuel assemblies in the core were replaced with fresh fuel assemblies. The sixth cycle core consists of 8 batches of fuel: four once-burned
- batches fr~m Cycle 5 of Unit 1 and Cycles 2 and 3 of Unit 2 (Batches 7A, 7B, S2/4A4, and S2/6B3), respectively, one twice-burned batch that is carried over from Cycles 4 and 5 (Batch 6C2), one thrice-burned batch that is carried over from Cycles 2, 3 and 4 (Batch 4C2), and two fresh batches (Batches 8A and 8B). The core loading pattern and the design parameters *for each batch are shown in Figure 1.1. Fuel assembly burnups are given in Figure 1.2. The incore instrumentation locations are identified in Figure 1.3. Figure 1.4 identifies the location and number of burnable poison rods and source assemblies for Cycle 6; and Figure i.5 identifies the location and number of control rods in the Cycle 6 core.
On July 6,* 1981 at 1700, the sixth cycle core achieved initial criti9ality. Following criticality, startup physics tests were performed as outlined in Table 1.1. A summary of the results of these tests follows: 1.*The drop time of each control rod was confirmed to be within the 1.8 second limit of the Surry Technical Speci:fications.z
- 2. The reactor coolant system flow rate was confirmed to be 1
greater than the minimum limit specified in the Final Safety Analysis Report 3 *
- 3. Individual control rod bank worths for all control rod banks were measured using the rod swap technique~ and were found to be within 5.5% of the design predictions. The sum of the individual control rod bank worths was measured to be within 1.6% of the design prediction. These results are within the design tolerance of +/-15% for individual bank worths (+/-10% for the rod swap reference bank worth) and the design tolerance of +/-10% for the s~m of the individual control rod bank worths.
- 4. Criti~al boron concentrations for two control bank configurations were measured to be within 4 ppm of the design predictions. These results were within the design tolerances and also met the accident analysis acceptance criterion.
- 5. The boron worth coefficient was measured to be within 4.3%
of the design prediction, which is within the design tolerance of +/-10% and met the accident analysis criterion.
- 6. Isothermal temperature coefficients for two control bank corifigurations were measured to be within 1.7 pcm/°F of design predictions. These results are within the design tolerance of +/-3 pcm/°F and also met the accident analysis acceptance criterion.
- 7. Core power distributions at HZP indicated measured assembly-wise power values to be somewhat larger than the established 2
design tolerance. These higher-than-expected power values were accompanied by a quadrant power tilt ratio CQPTRl which at hot-zero-power, was measured to be approximately 2.8%, but decreased to 1. 1% at full power. Core power distributions for various at-power conditions were generally within 5% of the predicted power distributions. These deviations of power distribution at HZP had no adverse consequences since, for all maps, the hot channel factors were measured to be within the limits of the Technical Specifications. In summary, all startup physics test results were acceptable.
- Detailed results, together with specific design tolerances and
,., acceptance criteria for each measurement, are presented in the appropriate sections of this report. 3
Table 1.1 SURRY 1 - BOL CYCLE 6 PHYSICS TESTS CHRONOLOGY OF TESTS Reference Test Date Time Power Procedure Hot Rod Dz:op-Hot Full Flow 7/5/81 0400 HSD PT-7 Reactivity Computez: Checkout 7/6/81 2257 HZP PT28.11CB) Boron Endpoint-ARO 7/7/81 0817 HZP PT28.11CC) Tempez:ature Coefficient-ARO 7/7/81 1402 HZP PT28.11CD) Flux Map-ARO 7/7/81 1630 HZP OP-57, PT28.2 Bank B Woz:th 7/7/81 2130 HZP PT28.11CE) Boz:on Endpoint-B In 7/8/81 0320 HZP PT28.11CC) Tempez:ature Coefficient-B In 7/8/81 0410 HZP PT28.11CD) F.lux Map-B In 7/8/81 0735 HZP OP-57,
. PT28.2 Bank D Worth - Rod Swap 7/8/81 1025* HZP PT28.11CF)
Bank C Worth - Rod Swap 7/8/81 1104 HZP PT28.11CF)
'* Bank A Worth - Rod swap 7/8/81 1137 HZP PT28.11CF)
Bank SB Worth - Rod Swap 7/8/81 1241 HZP PT28.11CF) Bank SA Worth - Rod Swap 7/8/81 1205 HZP PT28.11CF) Flux Map - NI Calibz:ation 7/8/81 1853* 32% OP-57, PT28.2 Flux Map - NI Calibration 7/9/81 1525 47% OP-57, PT28.2 Flux Map - NI Calibz:ation 7/13/81 2008 57% OP-57, PT28.2 Flux Map - NI Calibration 7/14/81 0024 65% OP-57, PT28.2 Flux Map - NI Calibration 7/14/81 1 121 85% OP-57, PT28.2 Flux Map - HFP, Eq. Xenon 7/21/81 0949 100% OP-57, PT28.2 RCS Flow Measurement 8/6/81 1345 100% ETA-60002 fl 4
FIGURE 1.1 SURRY UNIT 1 - CYCLE 6 CORE LOADING MAP R p N M L K J H G F E D C 8 A I 7A 88 7A I OA3 ) 1C6 I OA8 I 1 1_ _ 1_ _ 1_ _ 1
,-4-C-2-.,...1_8_8_1 88 I *683 I 88 ,-e-s-~,-4-C2-I I D29 ) 5C4 I 3CO I Wl4 I OC2 I 3C5 I Dll ) 2
_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ I 7A I 88 I 88 I 78 I 78 I 7B I 88 I 88 I 7A I I 1A6 I 1C4 I 4CO I 3A9 I 3A6 I SAl I scs I ocs I 1A7 I 3 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ I 7A I 78 I 88 I 78 I 8A I 78 I 8A I 78 I 88 I 7B I 7A I I 2AO I 2A3 I 4C9 I 2A6 I 188 I 4A3 I OB8 I 3A2 I lCS I 4A8 I 1A3 I 4 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ , _ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ I 4C2 I 8B I 88 I 78 I 8A I 7B I 8B I 78 I 8A I 78 I 88 I 88 I 4C2 I I D38 I OC9 I 5C6 I SAO I OBS I 4A6 I 2C9 I 4A7 I 082 I 5A3 I 4C3 I sco I D20 I 5
, _ _ 1_ _ 1_ _ 1_ _ , _ _ , _ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1
,~ loo 17B IM 17B , ~ I n loo 17B IM 17B , ~ , ~ I
_ _ ,I_ 4CS_ ,f _OC4_ ,I_5A9_ 1f _180_ 1I _ 2A8_ ,f _1C7_ 1f _OA4_ ,I_ 4C7_ 1f_3A8_ ,I_ 086_ 1I _SA4_ ,f _ 2C3_ ,f _3C4_ 1f _ _ 6
) 7A I 88 f 7B I 8A f 78 f 88 f 6C2 f 8A I 6C2 I 88 ) 78 I 8A f 7B I 88 I 7A f I lAO I 4C2 I 3AO I 1B4 I SAS I 4C6 I Jl5 I 064 I J09 I 5C2 I 5A6 I 166 I 4A9 I 2C5 I OA2 I 7
- , _ _ , _ _ , _ _ , _ _ , _ _ , _ _ , _ _ 1_ _ , _ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ , _ _ 1 I 88 I *6B3 I 78 I 76 f 88 I 7A I 8A I *4A4 I 8A I 7A I 88 I 7B I 78 I *6B3 I SB I I 1C9 I Wl8 I 2A7 I 3A5 I 1C2 I 1A4 I 1B5 I S20 I 089 I !Al I 3C8 I 5A7 I 3A4 I W31 I 4Cl I 8 1_ _ 1_ _ 1_ _ 1_*_1 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1
- I 7A I 88 I 7B I 8A I 78 I 88 I 6C2 I 8A I 6C2 I 88 I 78 I 8A I 78 I SB I 7A I I OAl I OC6 I 4A5 I 187 I SAS I lCl I J42 I 1B2 I J03 I OC7 I 2A9 I 1B9 I 6AO I 2Cl I OAS I 9
, _ _ , _ _ 1_ _ , _ _ 1_ _ 1_ _ , _ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ , _ _ 1 100 ,~ 17B IM 17B ,~ In loo 17B IM 17B loo loo I I 2C6 I 3C7 I 2Al I 2BO I 4A2 I lCS I OA7 I 3C6 I 2A5 I 1Bl I 4A4 I 3Ci I 2C7 I 10
, _ _ 1_ _ , _ _ 1_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I 4C2 I 88 I 88 I 7B I 8A I 78 I 88 I 78 I 8A I 7B I 8B I 8B I 4C2 I I D24 I 4C4 I 2CO I 3A3 I 083 I 2A4 I 2C2 I 6A2 I OB1 I 3A7 I SCl I 1C3 I 037 I 11 1_ _ 1_ _ 1_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ , _ _ , _ _ 1_ _ 1_ _ 1_ _ 1 In 17B ,~ 17B IM 17B IM 17B ,~ IIB In I I 1A2 I 6A4 I 3C3 I 6Al I 183 I 6A3 I 087 I 2A2 I lCO I 5A2 I OA9 I 12
, ___ 1___ 1___ 1___ 1___ 1___ 1___ 1___ 1___ 1_ _ 1___ 1 In loo I ~ IIB Im Im 100 loo I n I I 1A5 f OC3 I 5C3 I 4Al I 3Al I 4AO I 4C8 I 3C9 I OA6 I 13 1_ _ 1_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I 4C2 I 88 I 88 I *663 I 8B I 88 I 4C2 I I 030 I OCl I OC8 I Wl5 I 3C2 I 2C8 I D23 I 14 1___ , ___ 1___ 1___ 1___ 1_.__ 1___ 1 I 7A I 88 I 7A I
,--f--> BATCH 1
I 1A9 I 2C4 I 1A8 I _ _ 1 _ _ , _ _ 1 15 I 1--> ASSEMBLY ID FUEL ASSEMBLY DESIGN PARAMETERS BATCH 4C2 6C2 7A 7B SA 8B S2/4A4 S2/6B3 Initial Enrichment (w/o U235) 3.33 2.90 2.90 3.39 3.22 3.40 2.61 3.20. Burnup at BOC-6 (MWD/M'l'U) 25,619 21,534 17,158 15,425 0 0 11,042 10,951 Assembly Type 15X15 15Xl5 lSXlS lSXlS 15X15 15X15 15X15 lSXlS Number Of Assemblies 8 4 20 44 20 56 1 4 Fuel Rods per Assembly 204 204 204 204 204 204 204 204
*Transferred from Surry 2.
5
FIGURE 1.2 SURRY UNIT l - CYCLE 6 BEGINNING OF CYCLE FUEL ASSEMBLY BURNUPS R p N M L K J H G F E D C B- A OA3 1C6 I OA8 I 163121 o I 165381 ____...,....____ 1___ 1____ 1____ 1__________ l I D29 I 5C4 I 3CO I Wl4 I OC2 I 3C5 I Dll I I 256701 o I o I 109151 o I o I 257011 2 ____ 1_*___ 1____ 1___ 1____ 1____ 1____ 1____ 1___ I 1A6 I 1C4 I 4CO I 3A9 I 3A6 I 5Al I 5C5 I ocs I 1A7 I I 174041 o I o I 151911 134921 1s2111 o I o I 174931 3
~ 1 ____ 1____ 1____ 1____ 1___ 1____ 1____ 1___ 1___ 1___
I 2AO I 2A3 I 4C9 I 2A6 I 1B8 I 4A3 I OB8 I 3A2 I 1C8 I 4A8 I 1A3 I I 177031 104951 o. I 152981 o I 177521 o I 157291 o I 108441 174461 4 ____ 1____ , ____ , ___ , ___ , ____ 1___ 1___ 1___ 1___ 1____ 1____ 1____ I D38 I OC9 I 5C6 I SAO I OBS I 4A6 I 2C9 I 4A7 I OB2 I 5A3 I 4C3 I sco I 020 I I 256851 o
, ____ , ___ I o I 134901 o I 173751 o I 173551 o I 134931
. _, ____ 1____ 1____ , ____ , ____ 1____ 1____ 1____ 1____ , ____ , ____ , o I o I 256021 5 I 4C5 I OC4 I 5A9 I 1BO I 2A8 I 1C7 I OA4 I 4C7 I 3A8 I OB6 I 5A4 I 2C3 I 3C4 I I o I o I 154101 o I 174321 o I 11aasl o I 173151 o I 155611 o I o I
____ , ____ 1____ 1_.___ 1____ 1____ 1____ 1____ 1____ 1____*1 ____ 1____ 1____ 1____ 1____ 6
. I lAO I 4C2 I 3AO I 1B4 I SAS I 4C6 I JlS I OB4 I J09 I SC2 I 5A6 I 1B6 1. 4A9 I 2C5 I OA2 I . I 165041 o I 153261 o I 175441 o I 214041 o I 215531 o *I 173111 o I 152301 o I 166141 7 , 1___ 1____ 1_ _ , ___ , ____ 1____ , ___ , ____ 1____ 1____ 1___ 1___ 1____ 1____ 1____ 1 I 1C9 I Wl8 I 2A7 I 3A5 I 1C2 I 1A4 I 1B5 I 520 I 089 I lAl I 3C8 I 5A7 I 3A4 I W31 I 4Cl I
- ~ I o I 1oaas1 136741 176151 o I 179161 o I 110431 o I 177911 o I 177801 138271 11oosl o I 8 1____ 1___ 1____ 1____ 1___ 1____ 1____ 1____ 1____ 1____ 1____ 1____ 1___ ._1 ____ 1____ 1 I OAl I OC6 I 4A5 I 1B7 I SAS I lCl I J42 I 1B2 I J03 I OC7 I 2A9 I 1B9 I 6AO I 2Cl I OAS I I 167221 o I 153801 o I 174881 o I 216541 o I 215281 o I 174781 o I 156251 o I 165421 1____ 1____ 1____ 1____ 1___ 1____ 1___ 1___ 1____ 1____ 1____ 1_____ 1____ 1__.__ , ____ ,
9 I 2C6 I 3C7 I 2Al I 2BO I 4A2 I lCS I OA7 I 3C6 I 2A5 I 1Bl I 4A4 I 3Cl I 2C7 I I o I o I 154001 o I 178711 o I 175691 o I 177151 1___ 1___ 1_____ 1___ 1___ 1___ 1___ 1___ 1____ , ____ 1____ , ___ 1____ , o I 1s11s1 o I o I 10 I D24 I 4C4 I 2CO I 3A3 I OB3 I 2A4 I 2C2 I 6A2 I 081 I 3A7 I 5Cl I 1C3 I D37 I I 255981 o I o I 142601 1 0 I 112s11 o I 173881 o I 136301 o I o I 256981 11 1____ 1____ 1___ 1____ 1___ 1____ 1___ 1___ 1___ 1_ _ 1___ 1___ 1___ 1 I 1A2 I 6A4 I 3C3 I 6Al I 1B3 I 6A3 I 087 I 2A2 I lCO I SA2 I OA9 I I 174011 105931 o I 154791 o I 176011 o I 152911 o I 109661 173621 12 1___ , ___ 1___ 1___ 1___ 1____ 1____ 1___ 1____ , ____ 1___ 1 I lAS I OC3 I SC3 I 4Al I 3Al I 4AO I 4C8 I 3C9 I OA6 I I 112201 o I o I 157731 134981 151641 o I o I 173801 1____ 1___ 1___ 1____ 1____ 1___ 1___ 1____ 1____ 1 I D30 I OCl I OC8 I Wl5 I 3C2 I 2C8 I D23 I I 255731 o I o I 110001 o I o I 254271 14 1____ , ____ 1____ 1____ 1____ 1____ 1____ 1 I 1A9 I 2C4 I 1A8 I
,----!-->*ASSEMBLY IO II____
166871, ___ o I, ___ 166711, 15 I !--> ASSEMBLY BURNUP
, ___ I 6
FIGURE 1.3 SURRY UNIT l - CYCLE 6 INCORE INSTRUMENTATION LOCATIONS R p N M L K J H G F E 0 C B A I I I I l11DITCI _ _..,.....__ 1_ _ 1_ _ 1_ _ 1_ _..,.....__ l I I I I I _ _ 1I_ _ 1I_ _ 1I_TC_ 1I_ _ 1I___ TC 1I_MD_ 1I_ _ 1I___ 2 IMO! I I 11101 I I IMDI I TC I I TC I MD I TC I I TC I I TC I 3 ___ 1___ 1___ 1~_1 _ _ 1_ _ 1___ 1_ _ 1_ _ 1_ _ 1___ I I I I I I I I I I I I I TC I I .MO I ___ 1___ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1I I MO I I MD 1_ _ 1___ 1___ 1I_ _ I TC I I 4 I I I I I I I I . I I I MD I I ND I I I MO I I MD I TC I MD I TC I I TC I 110 I TC I I TC I 5 1_ _ 1___ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_._1 ___ 1_ _ 1_ _ 1_ _ 1___ 1 I I I I MD I I I I I I I I I I I I TC I I TC I I I MD I TC I MD _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1___ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ I I I I I 6 I 1* I I I I I I I I I - I I I I - I 1I_TC_ 1I_TC_ 1I_MD_ 1I_ _ 1I_ _ 1I_ _ ,I_MD_ 1I_ _ 1I_
- MD_ ,I___ 1I_TC_ 1I_HD_ 1I___ 1I___ HD 1I___ 1I 7 I I INDI IMDI I I I I I I IMDI I I 1I_MD_ 1I_TC_ 1I___
TC 1I___ 1I_TC_ 1I_TC_ 1I_ _ 1I_TC_ 1I_TC_ 1I___ MD 1I___ TC 1I_ _ 1I___TC 1I___ HD 1I_TC_ 1I 8
.., I I I I I I I I I I ND I I I I I I I1___ 1I_ _ 1I_ _ 1I___ TC 1I_MD_ 1I_ _ 1I_ _ 1I_TC_ 1I___ MD 1I___ TC 1I_ _ 1I___ 1I___ 1I___ 1I_MD_ 1I 9 I I MD I I I I MD I I I . I I I I MD I 1I_ _ 1I___
TC 1I_ _ 1I___ 1I_ _ 1I___ TC 1I___ 1I_ _ 1I___ 1I_ TC _ 1I_MD_ 1I_ _ 1I___ TC 1I 10 I I I I I I I MD I I MD I I I I I I1_ _ 1I_ _ 1I_TC_ 1I_MD_ 1I_TC_ 1I_ _ 1I___ TC 1I_ _ 1I_ TC _ 1I_MD_ 1I_ _ 1I___ 1I_ _ 1I 11 I I I I I MD I I I I I I HD I I MD I I TC I I TC I I I I TC I MD I TC I 12 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1___ 1_ _ 1_ _ 1_ _ 1___ 1 I I I I I MD I I MD I I I 1I___ 1I_ _ 1I_ _ 1I_ _ 1I_TC_ 1I_ _ 1I_TC_ 1I_ _ 1I_ _ 1I 13 I MD I I I I I I I I1_TC_ 1I_ _ 1I_ _ 1I_ _ 1I_MD_ 1I_ _ 1I_TC_ 1I 14
'MO - MOVABLE DETECTOR I I I I TC - THERMOCOUPLE I MO I TC I TC I 15 1_ _ 1_ _ 1_ _ 1 II 7
FIGURE 1.4 SURRY UNIT 1 - CYCLE 6 BURNABLE POISON AND SOURCE ASSEMBLY LOCATIONS R p N 11 L K J H G F E D C B A I I I ss I I _________ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_________ l I PS I I I I I I 12 I I 12 I I I 2 _ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ __ _ I I I I I I I I I I I I a I 16 I I ss I I 16 I a I I 3 _ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ __ _ I I I I I I I I I I I
- I I I I 16 I I 16 I I 16 I I 16 I I I 4
____ 1____ 1____ 1_ _ _ _ 1_ _ _ _ 1____ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ __ _ I I I I I I I I I I I I I I I I 8 I 16 I I 16 I I 20 I I 16 I I 16 I a I 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1 I 5 I I I I I I I I I I . I I I I I I 16 I I 16 I I 16 I I 16 I I 16 I I 16 I I 6 _ _ _ _ 1_ _ _ _ 1_ _ _._1 _ _ _ _ . 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ __ _ I I I I I I I I I I I I I I I I I I 12 I I 16 I I 16 I I 12 I I 16 I I 16 I I 12 I I 7 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1
*,.; I I I I I I I I I I I I . I I I I I I I I I 20 I I 12 I I 12 I I 20 I I I I I 8 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_._ _ _ 1_ _ _ _ 1_ _ _ _ 1 I I I I I I I I I I I I I I I I I I 12 I I 16 I I 16 I I 12 I I 16 I I 16 I I 12 I I 9 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1 I I I I I I I I I I I I I I I I 16 I I 16 I I 16 I I 16 I I 16 I I 16 I I 10 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1 I I I I I I I I I I I I I I I I a I 16 I I 16 I I 20 I I 16 I I 16 . I a I 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1 I 11 I I I I I I I I I I I I I I I 16 I I 16 I I 16 I I 16
- I I I 12 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ 1 I I I I I I I I I I I I a I 16 I I ss I I 16 I a I 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1 I 13 I I I I I PS I I I I I I 12 I I 12 I I I 14 1 _ _ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ 1_ _ _ _ 1_ _ _ _ 1_ _ _ _ 1 I I I I 992 FRESH BURNABLE POISON ROOS I I I I 15 SS - SECONDARY SOURCE I____ I____ I____ I PS - PRIMARY SOURCE ATTACHED TO 12 BURNABLE POISON ROD CLUSTER 8
FIGURE 1.5 SURRY UNIT l - CYCLE 6 CONTROL ROD LOCATICNS R 1' N M L K J H G F E D C B A 180° I LOOP C I I I I LOOP B 1 OUTLET I__ I _ I__ I INLET
~I IAI IDI IAI 1/ 2
_1_1_1_1_1_1_1_1_ N-41 I I I I SA I I SA I I I I N-43 3* _1_1_1_1_1_1_1_1_1_1_ I I c I I B I I I I B I I c I I 4 _1_1_1_1_1_1_1_1_1_1_1_1_ I I I sa I I SP I I SP I I SB I I I I 5 1_1_1_1_1_1_1_1_1_1_1_1_1_1 IAI IBI IDI ICI IDI IBI IAI 6 LOOP C _ _ I _ _ I _ _ I __ I _ I _ _ I _ _ I _ I _ _ I _ _ I _ _ I _ _ I _ _ I _ _ I__ LOOP B INLET I I I SA I I SP I I SB I I SB I I SP I I SA I I I OUTLET 7 9~ 1-l-D-l-l-l-lTl-l-l-.-l-c-l-l-l-l-D-l-l /[7o
. 1_1_1_1_1_1_1_1_1_1_1_1_1_1_1_1 0
8 I I I SA I I SP I I SB I I SB I I SP I I SA I I I 9 1_1_1_1_1_1_1_1_1_1_1_1_1_1_1_1 IAI IBI IDI ICI !DI IBI IAI 10 1_1_1_1_1_1_1_1_1_1_,_,_1_1 I I I I SB I I SP I I SP I I SB I I I I 11 1_1_1_1_1_1_1_1_1_1_1_1_1_1 I I c I I B I I I I B I I c I I 12 1_1_1_1_1_1_1_1_1_1_1_1 I I I I SA I I SA I I I I 13 N-44 I_I_I_I_I_I_I_I_I_I N-42 I I A I I o I I A I I 14
,_1_1_,_,_1_1_1 Jr"' I I I I ~ 15 LOOP A I_ _ I _ I _ _ I LOOP A ABSORBER MATERIAL OUTLET INLET AG-IN-CO 10 0
FUNCTION NUMBER OF CLUSTERS Ulfffffflllflfl fllllllllllffllfllllllllllflllllllfl CONTROL BANK D 8 CONTROL BANK C 8 CONTROL BANK B 8 CONTROL BANK A 8 SHUTDOWN BANK SB 8 SHUTDO~'N BANK SA 8 SP (SPARE ROD LOCATIONS) 8 9
Section 2 CONTROL ROD DROP TIME MEASUREMENTS The drop time of each control rod was measured at cold and at hot RCS conditions in ordex to confirm satisfactory operation and to verify that the ~od drop times were less than the maximum allowed by the Technical Specifications. The hot control rod drop time measurements were run with the RCS at hot, full flow conditions C 597 °F, 2235 psig) and are described below. The rod qrop time measurements were performed by first withdrawing a rod bank to its fully withdrawn position, and then removing the movable gripper coil fuse and stationary gripper coil fuse for the test rod. This allows the rod to drop into the core as it would in a normal plant trip. The data recorded during this test are, the stationary g~ipper coil voltage, the LVDT (Linear Variable Differential Transformer) primary coil voltage and a 60Hz timing trace which are recorded via a visicorder. The rod drop time to the dashpot entry and to the bottom of the dashpot are determined from this data. Figure 2.1 provides an example of the data that is recorded during a rod drop time measurement. As shown in Figure 2_.1, the initiation of the rod drop is indicated by the decay of the stationary gripper coil voltage when the stationary coil fuse is removed. A voltage is then induced in the LVDT primary A coil as the rod drops. The magnitude of this voltage is a function of. the rod velocity. When the rod enters the dashpot section of its guide 10
tube, the velocity slows causing a voltage decrease in the LVDT coil. The LVDT voltage the11 reaches a minimum as the rod reaches the bottom of the dashpot. Subsequent variations in the trace are caused by the rod bouncing. This procedure was repeated for each control rod. The measured drop times for each control rod are recorded on Figure 2.2. The slowest, fastest, and average drop times are summarized in Table 2.1. Technical Specification 3.12.C. 1 specifies a maximum rod drop time from loss of stationary gripper coil voltage to dashpot entry of 1.8 seconds with the RCS at hot, full flow conditions. All test results met this limit. ll
Table 2.1 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST HOT ROD DROP TIME
SUMMARY
ROD DROP TIME TO DASHPOT ENTRY SLOWEST ROD FASTEST ROD AVERAGE TIME C-9, 1.42 sec. M-12, 1.24 sec. 1.29 sec.
"ROD DROP TIME TO BOTTOM OF DASHPOT SLOt.?EST ROD FASTEST ROD AVERAGE TIME G-13, 2.16 sec. P-8, 1.76 sec. 1.91 sec.
12
( Figure 2.1 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST TYPICAL ROD DROP TRACE
FIGURE 2.2 SURRY UNIT l - CYCLE 6 BOL PHYSICS TEST ROD DROP TIME - HOT FULL FLOW CONDITIONS R p N M L K J H G F E D C B A I I I I I l
-__,,-_1 _ _ 1_ _ 1_ _ 1_ __,,__
I 1. 30 I I 1. 25 I I 1. 28 I I I 1.93 I I 1.81 I I 1.91 I I 2 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 _ I I I I l. 28 I I 1. 30 I I I I I I I I 2. 05 I I 1. 90 I I I I 3 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ I I 1. 29 I I 1. 25 I I I I 1. 28 I I 1. 29 I I I I 1.82 I I 1. 77 I I I I 1.85 I I l.89 I I 4 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ I I I I 1. 28 I I I I I I 1. 32 I I I I I I I I 1. 93 I I I I I I 1. 95 I I I I s 1_ _ 1_ _ 1_ _ 1_._1 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I 1. 30 I I 1. 2s I I 1. 29 I I 1. 28 I I 1. 28 I I 1. 28 I I 1. 33 l I 1. 93 I I 1. 78 I I 1. 86 I I 1. 83 I I 1. 82 I I 1. 83 I I 1. 98 I 6 _ _ 1_ _ 1_*_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ I I I 1. 28 I I I I 1. 30 I I 1. 28 I I I I 1. 28 I I I I I I 1. 95 I I I I 1. 98 I I 1. 95 I I I I 2 .13 I I I 7 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I I 1.26 I I I I 1.28 I I I I 1.29 I I I I 1.28 I I I I 1.76 I I I I 1.80 I I I I 1.84 I I I I 1.82 I I. 8 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I I I 1. 32 I I I I 1. 30 I I L 32 I I I I 1. 42 I I I I I I 2. os I *I I I 2. 02 I I 1. 90 I I I I 1. 95 I I I 9 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _*_1 _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I 1.30 I I 1.27. I I 1.29 I I 1.25 I I 1.31 I I 1.26 I I 1.32 I I 1.98 I I 1.80 I I 1.82 I I 1.84 I I 1.87 I I 1.83 I I 1.97 I 10 1_ _ , _ _ 1_ _ 1_ _ , _ _ 1_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I I I I l. 28 I I I I I I 1. 27 I I I I I, _ _ I1_
- _ I1_ _ I1_ 2. oo I I I I I I 2. 07 I
_ 1_ _ , _ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I I I 11 I I 1. 24 I I 1. 28 I I I I 1. 28 I I 1. 35 I I I I 1.77 I I 1.85 I I I I 1.81. I I .1.87 I I 12 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1_ _ , _ _ 1_ _ , _ _ 1_ _ 1 I I I I l. 32 I I 1. 28 I I I I I I I I l. 92 I I 2 .16 I I I I 13 1_ _ 1_ _ 1_ _ 1_ _ , _ _ 1_ _ 1_ _ 1_ _ 1_ _ 1 I I 1. 32 I I 1. 2s I I 1. 35 I I I I 2
- os I I l
- 79 I I 2
- os I I 14 I !--ROD DROP TIME TO 1_ _ , _ _ 1_._1 _ _ 1_ _ 1_ _ 1_ _ 1 I I DASHPOT ENTRYCSEC. l I I I I I _ _ I--ROD DROP TIME TO I I I I 15 BOTTOM OF DASHPOTCSEC.l 1_ _ 1_ _ 1_ _ 1 14
Section 3 REACTOR COOLANT SYSTEM FLOW MEASUREMENT The reactor coolant flow rate is measured in order to verify that the minimum flow rate ~equirement is sa~isfied. The RCS flow rate is determined using the calorimetric measurement technique. Precision calorimetric data (i.e., feedwater temperature, feedwater flow, and steam pressure) are obtained in order to accurately determine the secondary-side heat rate._ The primary-side enthalpy rise is determined from the RCS pressure and. the temperature: ii:icrease associated with each RCS loop. The flow for each RCS loop is determined by establishing a primary-side to secondary-sid~ heat balance. Steam generator blowdown heat loss, system heat losses, . and the power produced by the reactor coolant pumps are taken into account in the heat balance. A reactor coolant flow measurement was performed at 100% power.
,I This data was analyzed .using the RXFLows computer code. A summary of the results for this test is given in Table 3.1. As shown by this table, the results demonstrated that the RCS flow limit was met.
15 _j
Table 3.1 SURRY 1 - CYCLE 6 BOL PHYSICS TEST REACTOR COOLANT SYSTEM FLOW MEASUREMENT
SUMMARY
I Percent Loop A Loop B I Loop C !Total Flow Minimum Flowl I Power
- IFlow Cgpm)IFlow (gpm)IFlow Cgpm) I (gpm) Limit* Cgpm)I I I I I I I I I I I I I I 10 0 ?. I 97,526 I 97,502 I 96,710 I 291,738 265,500 I I I I I I I
- FSAR Section 4.1.3; Letter from J. H. Ferguson CVepco) to H. R. Denton CNRC) dated April 28, 1981 (Se*rial No. 232);
Letter from C. M. Stallings (Vepco) to E. G. Case CNRC) dated November 16, 1977 (Serial No. 516). lb
Section 4 CONTROL ROD BANK WORTH MEASUREMENTS Control rod bank worth measurements were obtained for all control and shutdown banks using the rod swap technique. The first step in the rod swap procedure was to dilute the most reactive control rod bank (hereafter referred to as the reference bank) into the core and measure its reactivity worth using conventional test techniques. The reactivity changes resulting from the reference bank movements. were recorded continuously by the reactivity computer 6 and were used to determine the differential and integral worth of the reference bank (Control Bank B). At the completion ._of the reference bank reactivity worth measurement, the reactor coolant system temperature and boron concentration were stabilized such that the reactor was critical with the reference bank near iull insertion. Initial statepoint data £or the rod swap maneuver were obtained by moving the reference bank to its fully inserted position and recording the co%e reactivity and moderator temperature. At this point, a rod swap maneuver was performed by withdrawing the reference hank while one of the other control rod banks Ci~e., a test bank) was inserted. The core was kept nominally critical throughout this rod swap and the maneuver was continued until the test bank was fully inserted and the reference bank was at the position at which the core was just critical. This measured critical position CMCP) of the reference bank with the test bank fully inserted is the major parameter of interest and was used to determine the integral reactivity worth of the test bank. Statepoint data (core reactivity, moderator temperature, 17
and the differential worth of the reference bank) were recorded with the reference bank at the MCP. The rod swap maneuver was then performed in reverse order such that the reference bank once again was near full insertion and the test bank was once again fully withdrawn from the core. The rod swap process was then repeated for all of the other control rod banks (control and shutdown). A summary of the results for these tests is given in Table 4.1. As shown by this table and the Startup Physics Tests Results and Evaluation Sheets given in the Appendix, the individual measured bank worths for all of the control and shutdown banks were within the design tolerance (+/-10% for the reference bank and +/-15% for the t~st banks). The sum of the individual rod bank worths was measured to be within 1.6% of the design prediction. This is well within the design tolerance of +/-10% for the sum of the individual control rod bank worths. The integral and differential reactivity worths of the reference bank * (Control Bank B) are shown in Figures 4.1 and 4.2, respectively. The design predictions and the measured data are plotted together in order to illustrate their agreement. In suMrnary, all measured rod worth values were satisfactory. 18
Table 4.1 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST CONTROL ROD BANK WORTH
SUMMARY
MEASURED PREDICTED PERCENT DIFFERENCE WORTH WORTH BANK (PCM) (PCM) (M-P)/P X 100 B-Refe1:ence Bank 1440 1406 + 2.4 D 1234 1226 + 0.7 C 815 833 - 2.2 A 551 546 + 0.9 SB 1013 1005 + 0.8 SA 1137 1078 + 5.5 Total Wo1:th 6190 6094 + 1. 6 19
FJ GURE 4. i SURRY UNIT l - CYCLE 6 BOL PHYSICS TEST BRNK. B INTEGRAL ROD WORTH B BRNK WITH ALL OTHER ROOS OUT PREDJCTEO
)I( MEASURED 0
D
"" I N
I 0 D D I N - I '.L 0 u 0 lD I Q_ .- I
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l>I I I ' ,..... .,. ' I I
"' ! I-
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D ' 0 40 80 12Cl 160 200 226 BANK POSITION (STEPS) 20
FlG-URE 4.2 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST BANK B DIFFERENTIAL ROD WORTH B BANK WITH ALL OTHER RODS OUT PREDICTED llE MEASURED 0 0
""d" N I I I I ! I ! I I I I :
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0 .,,"' I I I I I I I I I 40 80 120 160 200 228 BANK POSITION (STEPS) 21
Section 5 BORON ENDPOINT AND WORTH MEASUREMENTS Boron Endpoint With the reactor critical at hot zero power, reactor coolant system boron concentrations were measured at selected rod bank configurations to enable a direct comparison of measured boron endpoints with design predictions. For each measurement, the RCS conditions were stabilized with the control banks at or very near a selected endpoint position. The critical boron concentration was then measured. If necessary, an adjustment to the. measured critical boron concentration was made to account for o£f-nominal core conditions, i.e., for rod position and moderator temperature. The results of these measurements are given in Table 5.1. As shown in this table and in the Startup Physics Test Results and Evaluation Sheets given in the Appendix, all measured critical boron endpoint values were within their respective design tolerances. All measured values met the accident anal~sis acceptance criterion. In summary, all results were satisfactory. Boron Worth Coefficient The measured boron endpoint values provide stable statepoint data from which the boron worth coefficient was determined. A plot of the boron concentration as a function of integrated reactivity can be constructed by relating each endpoint concentration to the integrated 22
rod worth present in the core at the time of the endpoint measurement. The value of the boron coefficient, over the range of boron endpoint concentrations, is obtained directly from this plot. The boron worth plot is shown in Figure 5.1. As indicated in this figure and in the Appendix, the boron worth coefficient of reactivity was measured to be -8.78 pcm/ppm. The measured boron worth coefficient is within 4.3% of the predicted value of -8.42 pcm/ppm and is well within the design tolerance of +/-10%. The measurement result also met the accident analysis acceptance criterion. In summary, this result was satisfactory. 23
Table 5.1 SURRY UHIT 1 - CYCLE 6 BOL PHYSICS TEST BORON ENDPOINTS
SUMMARY
Measured P:redicted I Difference Cont:rol Rod Endpoint Endpoint I M-P Configuration (ppm) (ppm) I (ppm) I I ARO 1484 1480 I 4 I B Bank In 1320 1320 :t: I 0 I
- t:The predicted endpoint fo:r the B Bank in configuration has been adjusted for the difference between the measured and predi~ted values of the endpoint taken at the ARO configuration as shown in the boron endpoint Startup Physics Test Results and Evaluation Sheets in the Appendix.
24
FIGURE 5 .1. SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST BORON WORTH COEFFICIENT l!l ENDPOINT MEASUREMENTS 2400 2000
~~ = -8. 78 pcm/ppn .--1---
~ I 10 v:
r-..
~
u 1600
"" "' r,,.
(L
"'I t(
"" ["..
I-1--i 1200
"'""' ~
1--i I- ~ u 0: w 0:::: 800
""' " ~
"~
400
"' I~
0
- "" ""rs..
~
C--- 1280 1320 1360 1400 1440 1480 1520 1560 1600 BORON CONCENTRATION (*PPMl
Section 6 TEMPERATURE COEFFICIENT MEASUREMENTS The isothermal temperature coefficient measurements. were accomplished by controlling the RCS heat gains/losses with the steam dump valves to the condenser, and/or steam generator blowdown establishing a constant and uniform heatup/cooldown rate, and then monitoring the resulting reactivity changes on the reactivity computer. These measurements were performed at very low power levels in order to minimize the effects of non-uniform nuclear heating, thus, the moderator and fuel were approximately at the same temperature (between 543-549 °F) during these measurements. To eliminate the boron reactivity effect of
- outflow from the pressurizer, the pressurizer level was maintained constant or slightly increasing during these measurements.
Isothermal temperature coefficient measurements were performed at various control rod configurations. For each rod configuration, reactivity measurements were taken during both RCS heatup and*cooldown ramps during which the RCS t~mperature varied approximately 6°F. Reactivity was determined using the reactivity computer and was plotted against the RCS temperature on an x-y recorder. The temperature coefficient was then determined from the slope of the plotted lines. The x-y recorder plots of reactivity changes versus RCS temperature for each measurement are shown in Figures 6.1 and 6.2. The predicted and measured isothermal temperature coefficient - values are compared in Table 6.1. As can be seen from this summary and from the Startup Physics Test Results and Evaluation Sheets given in the 26
Appendix, all measured isothermal temperature coefficient values were within the design tolerance of +/-3 pcm/°F and met the accident analysis acceptance criterion.. In summary, all measured results were satisfactory. 27
Table 6.1 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT
SUMMARY
I BANK !ISOTHERMAL TEMPERATURE COEFFICIENT! IPOSITIOH I (PCI1/°F) I I Csteps) ITEMPERATUREI BOROM I__________________ I I RANGE I CONCENTRATION I I COOL I I I DIFFER. I I B I D I C0 Fl I (PPM) IHEATUPI DOWN IAVER. IPRED. I CI1-P) I I _ _ I _ _ I ______ I_ _ _ _ _ _ _ I_ _ _ I _ _ _ I I I_ _ _ _ I I I I I I I I I I I 1228 1202 I 543 - 549 I 1463 1-2.17 1-2.rn 1-2.321-4.00I +1.68 I I I I I I I I I I I I o 1223 I 543 - 549 I 1331 1-5.52 1-5.57 1-5.551-6.361 +0.81 I t _ _ l _ _ l ______ l _______ l _ _ _ l _ _ _ l I I____ I 28
Figu:r:e 6. 1 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, ARO TEMPERATURE (Op) 29
Figure 6.2 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, B-BANK IM TEMPEPmURE (°F). 10
Section 7 POWER DISTRIBUTION MEASUREMENTS The core power distributions were measured using the incore movable detector flux mapping system. This system consists of five fission detectors which traverse fuel assembly instrumentation thimbles in 50 core locations (see Figure 1.3). For each traverse, the detector output is continuously monitored on a strip chart recorder. The output is also scanned £or 61 discrete axial points by the PRODAC P-250 process computer. Full core, three-dimensional power distributions are then determined by analyzing this data using the Westinghouse computer program, INCORE7. INCORE couples the measured fluK map data with predetermined analytic power-to-flux ratios in order to determine the power distribution £or the whole core. A list of all the flux maps taken during the test program together with a list of the measured values of the important power distribution parameters is given in Table 7.1. The measured power distribution parameter values are compared with their Technical Specifications limits in Table 7.2. Flux Maps 1 and 2 were taken at zero power. These flux maps serve as the base case design checks. Figures 7.1 and 7.2 show the resulting radial power d~stributions associated with these flux maps. These maps indicated the presence of a slight quadrant power tilt (2.8%) and some assemblywise relative power values in excess of the design tolerance, but all measured hot channel £actor values were within the Technical Specifications limits. Flux Maps 3 through 8 were taken over a wide range of power levels and control rod configurations. These flux 31
maps were taken to check the at-power design predictions and to measure core power distributions at various operating conditions. These maps also provide incore/excore calibration data for the nuclear instrumentation system. The radial power distributions for these maps are given in Figures 7.3 through 7.8. These figures show that the measured relative assembly power values are generally within 5% of the predicted values, and that the quadrant power tilt ratio decreased significantly during power ascension. In conclusion, all power distribution measurement results were considered to be acceptable with respect to the design tolerances, the accident analysis acceptance criteria, and the Technical Specification limits. It is therefore anticipated that the core will continue to operate safely throughout Cycle 6. 32
TABLE 7.1 SURRY UNIT 1 - CYCLE6 BOL PHYSICS TESTS INCORE FLUX MAP
SUMMARY
I I I 1 2 I I I I I I I BURNI F-Q(T> HOT F-DHINJ HOT I CORE f(ZJ I 4 I I I I I I UP I IBANK CHANNEL FACTOR CHNL.FACTOR I MAX I 31 QPTR AXIAL I NO.I I MAP IMAPI DATE I MWD/IPWRI D I I IF<XYJI OFF I OF I I DESCRIPTION INO. I I MTU l<Y.JISTEPSI I IAXIAL I IAXIAL I I I SET ITHIMI I I I I I I IASSYIPINIPOINTI F-Q<TJIASSYIPINIF-DH(NJIPOINTI FIZll I MAX ILOCI 00 IBLESI I I_I 1_ _ 1_1 _ _ 1_1_1 _ _ 1 I_I_I 1_ _ , _ _ , _ _ 1_ _ 1_1 _ _ 1_1 I I I I I I I I I I I I I I I IARO 11 7- 7-81 01 01 201 J12I GHI 22 2.442 J12I GHI 1.584 22 ll.50111.48211.0261 SWI 21.411 40 I I I I I I I I I I I I I I IB AT 21/22 21 7- 8-81 01 01 228 H09 HGI 21 2. 776 H091 HGI 1.796 21 ll.43Sll.780ll.028I SWI 21.511 40 I I I I I I I I I I I I I II/E CAL. 31 7- 8-81 DI 321 160 Fll HG! 32 2.184 D071 HII 1.473 33 ll.43911.41411.0131 SWI -7.191 41 I I I I I I I I I I I I I l,..l l,..l II/E CAL. 41 7- 9-81 101 471 180 L06 GHI 25 1*.930 J121 GHI 1.451 32 11.29411.37411.0111 swl -1.181 40 I I I I *I I I I I I I I I II/E CAL. SI 7-13-81 301 571 175 Fll HGI 33 1.986 D071 HII 1.451 34 ll.32711.39511.0lOI SWI -7.651 41 I I I I I I I I I I I I I II/E CAL. 61 7-14-81 351 651 200 L06 GHI 23 1.918 0071 HII 1.435 23 ll.28211.38911.0121 SWI 5.901 42 I I I I I I I I I I I I I II/E CAL. 71 7-14-81 401 851 204 Fll HGI 31 1.828 Jl2I GHI 1.421 33 l1.232ll.383ll.012I SWI -1.221 41 I I I I I I I I I I I I I IHFP, EQ.XENON 81 7-21-811 11011001 228 Fll HGI 34 1.810 Flll HGI 1.413 34 ll.22311.37711.0lOI SWI -2.471 42 NOTES: HOT SPOT LOCATIONS ARE SPECIFIED BY GIVING ASSEMBLY LOCATIONS (E.G. H-8 IS THE CENTER-OF-CORE ASSEMBLY!, FOLLOWED BY THE PIN LOCATION lDENOTED BY THE "Y" COORDINATE WITH THE FIFTEEN ROWS OF FUEL RODS LETTERED A THROUGH RAND THE "X" COORDINATE DESIGNATED IN A SIMILAR MANNER). IN THE "Z" DIRECTION THE CORE IS DIVIDED INTO 61 AXIAL POINTS STARTING FROM THE TOP OF THE CORE.
- 1. F-Q(Tl INCLUDES A TOTAL UNCERTAINTY OF 1.08.
- 2. F-DHINJ IHCLUDES A MEASUREMENT UNCERTAINTY OF 1.04.
- 3. F(XYI IS EVALUATED AT THE MIDPLAtlE OF THE CORE.
- 4. QPTR - QUADRANT POWER TILT RATIO.
Table 7.2 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TESTS COMPARISION OF MEASURED POWER DISTRIBUTION PARAMETERS WITH THEIR TECHNICAL SPECIFICATION LIMITS I F-2(T) HOT I F-DH(N) HOT CHANNEL FACTOR 1 I CHANNEL FACTORZ MAP I HO. MEASI LIMITIMARGIHI MEASI LIMIT I 1'IARGIH I I (%) I I I 0!) I I I l I 3 2. 18 I 4.36 I 49.9 I 1. 471 1. 76 I 16. S 4 1. 9 o I 4.30 I 55.0 I 1.451 1. 71 I 15.2 5 1.991 3.82 I 48. 1 I 1. 45 I 1. 68 I 13.7 6 1.921 3.29 I 41. 6 I 1.441 1 . 6 6 I 13.3 7 1.831 2.56 I 28.5 I 1 . 42 I 1. 60 I 11. 2 8 1 . 81 I 2. 18 I 17.0 I 1. 41I 1. 55 I 9. 0 I I I I I 1 The technical specification limit for the heat £lux hot channel
£actor, F-2CT) is a £unction of core height. The value £or F-2(T) listed above is the maximum value of F-2CT) in the core. The technical specification limit list~d above is evaluated at the plane of maximum F-2CT). The minimum margin values listed above are the minimum percent difference between the measured values of F-2CT) and the technical specifications limit for each map. All measured F-QCT) hot channel factors include 8% total uncertainty.
2 The measured values for the enthalpy rise hot channel £actor, F-dHCH) include 4% measurement uncertainty. 34
Figure 7.1 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST A.SSEMBLYWISE PG-JER DISTRIBUTION HZP, ARO p H L H A R
" K J G D C II g t
PREDICTED , 11E~SllllED 0,311 0,37 0.67 0.67 0.311 0.37 PIICD ICTtD
- 11£ASVl'ED r
1~
, PCT DIFHREIIC!,
o.u 0,90
-0.1 1.oz
-0.2 1.n
-1.11 1.oz o.9o o.36
.PCT DIFPEREHC!,
~fi o.36 0.111 1.00 1.01 o.n o.e6 o.34 z'*
*O.:S -:S.4, *1,7, *l,1 * *Z,9, *4,11 *lt,11 o.39
- o."
- 1.1"
- 1.zz
- 1.zs
- 1.zz
- 1.1"
- o." o.39 *
- a. 39
- o. 91
- 1. o9
- 1.111
- 1. 21
- 1.11
- 1. n . o. 90 o. 311
- 3
, -0.11 , -2.11 , *4, 7 , .-3.lt * -J.5 , -3.9 * -4. 7 , *lt,5 o.39
- a.ee 1.1s 1.26
- 1.z"
- 1.z"
- 1.z, 1.211 1.is
- a.ea 0,39*. o.~6
- 1.10
- 1.zo
- 1.19
- 1.n
- 1.20
- 1.z1
- 1.1s
- o.e11
- o.~o *
-o.ti , -z.1. -4,l * -4.t * -4.o. -3,11. -3.4. 1.1 * -0.1 * -0.1. z.ti
- 0,311 , 0,9lt , 1,15 1,ZG 1.24, 1.Z:S, 1,16 , 1.Zl , l,Z4 1.ZII, 1,15 , O."
o.39
- 0,36,
. {{
~
0,39 , 0,91 , 1,lZ , 1.25
- 1.21 , 1.17 , 1,11 , 1,111 , 1.:Z
- 1,Z9 , 1,17 , 0,99 , 0,40 , 5 11,9, *3,1 , -z.z , *2,7, *l,9, *<>,4, *°'1,2 * -4,l , *l.5, 0,7, 1,7, 5,11, 9,7,
, 0,90 , 1,14 1,Z6 1,24 1,19 , 1,17 l,OZ , 1.17 1.19 1.Zlt 1,26 1,1'1 0,90 ,
, 0,'16 , 1.ZZ , 1.ZII, 1.25 , 1.17, 1.IZ ; 0,911 , 1.U, J,U , 1.23 , l.Z7, 1.111, 0.96 , 6.,
, 6,9 , 11., , 1,11 , 0.9 , *l.5 , -4.J , -1., , *3,11 , *3,5 , *0.11 , 0.11 , J,11 , 6.5 ,
0,311 , l,OZ , 1,ZZ , 1,Z4 , 1.Z3 , 1,17 , 0.91 , 1.10 , 0.91 , 1,17 , 1,Z3 , l,Z4 , 1,ZZ , 1.0Z , 0,311 , (<:
- 0.11
- 1.olt
- 1,z9
- 1.21
- 1.z4
- 1.111
- o.es
- 1.01
- 0.119
- 1.n
- 1.:0
- 1.n
- 1.23
- 1.0<1
- o.39 *
* *0,6
- Z,11 , 5,9 , Z, 7 , O,G , 0,11 , -4,l , *2,9 , *Z,J , -J,O , *Z,2 , *0,11 , 0,11 , Z,6 , 2, 7 ,
*********************************************************************************************************** 71 0,67 , 1,03 , 1,25 1,24 1*.16 1.oz 1.10 0.911 , 1.10 1,02 , 1.111 l,Z°'I 1,Z5 , 1.0J , 0.67 ,
- o.66
- 1.05
- 1.21. 1.z11
- 1.16 1.oz
- 1.10
- 0.,1. 1.011 o.99 1.1". 1.u. 1.25 1,05. 0.11 a~
, *0,7, 1,Z, 1,1, 1,7, O,l, 0,6, *0,1, *1,9, *2,6, *Z,9, *t,J, *1,0, -0,6, 1,9. 6,1,
, 0,311 1,0£ l,ZZ , l,Z4 , l.Z3 1,17 , 0,91
,;,,, ..................................................... .
1,10 , 0,91 1,17 1,ZJ l,Z4 1,ZZ 1,0Z , 0,311 I/!' o,37
* -o., o *., . o.,. o.,. 1.:,
1.02 1.n
- 1.zs
- 1.zs 1.111
- o.n o.9. 1.,
1.12
- o.eo 1,5. -:,.1 1.n 1.:0
-1.2 * -z.11 1.zz
-1.5. -0.1 1.21 , 1.os
- 0,41 J,J. 10., '
, 0,90 , 1.14 , l,ZII , l,ZC'i, 1,19, 1,17, 1.oz , 1.17, 1.19, 1.Zil , l.Z6 , l,IC'i , 0,90 ,
- o.91
- 1.16
- 1.26
- 1.z<i
- 1.111
- 1.19
- 1.01
- 1.16
- 1.111
- 1.zz
- 1.Zlt
- 1.u
- o.119
- 10 f
- 1.1. 1.1. o.5. -o.,. -o.s. 1,5
- 1.s. -o.,. -z.1 * -1.3. -1,3. -1.1. -o.ti.
0,36 , O." , 1,15 , 1,ZII , 1,29 , l,Zl , 1,16
- l,ZJ , l,Z9 , 1,ZII , 1,15 , 0,9'o , 0,3" , t~
0.3& , 0,99 , 1,17 , 1,Z5 , 1.211 , 1.3Z , 1,19 , 1,25 , 1,Z'o , 1,ZII , 1,15 , 0.93 , 0,35 , 11
- 5,6 ., 5,11 , *Z.O , *Z,5 , 3,5 , 7,0 , 2,6
- 1,5 , *O,Z , *0,2 , *O,J , *0,9 , *Z,O ,
, O,J9
- 0,1111 , 1,15 , l,Z6 , 1,24 , 1,Z4 , 1,24 , l,ZII
- 1,15 , 0,1111 , 0,39 *
, 0,43 , 0,93 , 1,12 , 1.34 , 1,36 , 1,211
- 1,Z._ , 1.26 , 1.is , 0.89 , 0,40 , 11 **
, 9,5 , 4,11. *t,5 , 6,7 , 10,l , 3,7 * *O,J , O,J , 0,4
- 0,7, 0,11 ,
, 0,59 , 0,94 , 1,14 , l,ZZ , l,ZS , 1,ZZ , 1,14 , 0,94 , 0,39 *
- o.43
- o.91
- 1.:9
- 1.za
- 1.z~
- 1.zz
- 1.is
- o.95
- o.4o
- n
* . 9,5 , *2,11
- lZ,11 , ti.II * *1,0
- 0,4 , 0,9 , 0.7 , 0,11 *
, 0,36 , 0,90 , 1,0Z
- l,OJ
- l,OZ , 0,90 , O,Jfl ,
0,37 , 0,91 , 1,01 , 1.04 , 1,04 , 0,9Z O,Jfl
- 14i,
- 1.J , 1,J , *0,5 , 0,5
- Z,7 , 1,0 , o.* . ~c"!
STAIIOARD 0.311 , 0,67 , 0,311 , AV[IIAG! DEVIATION 0.311 , 0.611 , 0.39 , ,PCT DlfFEREHC!, 15 j
*Z ,311 1,1 , Z,0 ., J,S ,
- Z,6 HAP NO: Sl 1 DATE: 7/ 7/81 POWER: ox COHTROL ROD .POSITIONS: F-QCTJ = 2.442 QPTR:
D BANK AT 201 STEPS F-DHCN) = 1.584 NW 0.995 I NE 0.986 FCZl = 1.501
----------1----------
SW 1. 026 I SE 0.993 'l FCXYl = 1.482 BURNUP = 0 HWD/HTU A.O = 21.41( X) 35
Figure 7.2 SURRY.UNIT 1...; CYCLE 6 'BOL PHYSICS 'IEST ASSEMBLYWISE PCWER DISTRIBUTION HZP, B-BANK IN p H II
" l K J H G D C A PREDICTED
- 0.46 0.114
- 0,46 PPEDICTED
- 11EASURED
- o.41
- o.eo
- o . .r,1
- 11CASURCD
- PCT D1FFEREIIC!. , *5.0 * *5,0 , *4.9 * .PCT D1FF[IIEIIC!.
0.35 O.U 1.16
- 1.26
- 1.16 0.93
- 0.35 *
- o.35
- o.u
- 1.n. 1.:z. 1.12
- o.e6
- o.n. 2
, 1.4 , o.o , -2.5 * -z.s , *3.5 , *4.11 , .... 6 ,
0.34 0.110 0.99
- 1.Z6 1.40 1.:6 0.99 0.110 0.34
- 0.34
- 0.79
- 0.97
- 1.Z6
- 1.40. 1.23. 0,9ft
- 0.76
- 0.33
- J
- 1.0 * -o.3 * -1.9 , o.o * -o.o * -1., . -4.9 * -4,,. ** -..1 .
o.34. o.74 0.1111 o.6!1
- 1.16 1.n. 1.i. o.u 0.1111 o.74 o.34
- 0.35. 0.74
- 0.87
- 0.63
- 1.12
- 1.30
- 1.16
- 0.66
- 0.611
- 0.74
- 0.35.
, 1.:s * *0.5 * *1.6 * -:s.:s , -:S.6 , -z ... , 0.1 , 1.1 , *0,1 * -0.4
- 1.6
- o.:ss 0.110
- 0.1111 1.011
- 1.11 , 1.:so
- 1.:sz
- 1.,0
- 1.11 , 1.06 o.ae o.eo o.n *
- 0.35
- 0.79. 0.119
- 1.06
- 1.10
- 1.ZZ
- 1.26
- 1.ZZ
- 1.07. 1.07. 0.90
- 0,113
- 0.37 *
- z.11. -o.9. o.4 * -o.3. -1.5. -5.7. -4.6. -5.e. -3,6
- o.5
- z.1 * "*". 6.s *
- o.n. o.99. o.65 1.11 1.n
- 1,.r,z 1.n. 1.u
- 1.1z 1.11
- o.65 o.n o.n *
- o.95
- 1.oz
- o.66
- 1.16
- 1.12
- 1.1s
- 1.z4. 1.1s
- 1.n. 1.09 . 0,66
- 1,0,
- o.99 *
- Z,4. z.11
- z.1 * <1.1
- o.:s, -4.6 * -3.4. -4,6 * -1.1 * -1.1. o.e. 1.11. 6.,.
- 0.46
- 1.16
- 1.26
- 1,16
- 1.10 , 1,42
- 1.22
- 1.52
- 1.ZZ
- 1.42
- 1.30
- 1.16
- 1,26
- 1,16
- 0.46
- 0.47 , 1.19 , 1.29
- 1.19
- 1.32
- 1.45
- 1,111
- 1.411
- 1.111
- 1.35
- 1.26
- 1.16
- 1.27
- 1.21
- 0,47
- 3,1
- z.s. Z.4, z.z
- 2,0
- Z.O. *3.3, *Z.7, *Z.9, *4.7, *3,3, *O.Z , 0.7. 4.5. 3.5.
o.84
- 1.26
- 1 *.r,o
- 1.n
- 1.n
- 1.2,
- 1.sz
- 1.40
- 1.5z
- 1.29
- 1.12
- 1.n
- 1.40
- 1.26
- o.e<t
- i 0.87. 1.29 . 1.41. 1.35 . 1.Jl . 1.30
- 1.50 . 1.37. 1,46
- 1.:3 . 1.27. 1.30 . 1.37. 1,Z6
- 0.88.
3.1
- Z.6 , z.z
- 1.6 * *O,:S
- 0.9 * *1.1 * *Z,1 , o<\.O , *4,0 * *3.6 , *1. 7 , *Z.Z , 0,3 , lt,2 ,
0.46
- 1.16 , 1.26
- 1.16
- 1.30
- 1,42
- 1,ZZ , 1.52 , 1.22 , 1.4Z , 1,30 , 1,16 , 1,2' 1.16 , 0.46 ,
0.47
- 1.Zl
- 1.lZ
- 1.%0
- 1.34
- 1.45
- 1.Z6
- 1.53
- 1.14
- 1.lZ
- 1.ZZ
- 1.lZ
- 1.23 , 1.17
- 0.49
- 9*
J,l
- 4.6
- 5.3
- 3.,.
- J,Z
- 1.9
- 3.9 *. 0.7 * *l.9 * *6.1 , *!I.II , *:S.S , *2.0
- 1.0 , 6,J ,
- o.n. o.99. o.n 1.11
- 1.12
- 1.4Z
- 1.z9. 1.4z
- 1.12
- 1.11
- o.65 o.99. o.n.
- 1.01
- 1.011
- 0.61
- 1.13
- 1.34 , 1.43
- 1.30
- l.ll
- 1,211
- 1.09
- 0.66
- 0,98
- 0,93
- 10 .
- 8.,.
- 8,Z * -..z
- 1.8
- 1.8
- o.e . 0.1 * -Z.9 * -1.1 * -1.0
- 1.11 * -1.0 * -o.o *
- ii:is *: *ii:aii *: *ii:ii; *: *i:a6 *: *i:ii *: *i:iii **: *i:ii': *i:iii *: *i:ii *: *i :;,6 *:*ii:;,;,*:* ii:aii *: *ii:;s*:
- 0.11
- o.a6
- 0.,2
- 1.0,
- 1.12
- 1.,2
- 1.n
- 1,z9
- 1.10
- 1.011
- o.,o
- a.so
- o.34
- 11
. 1,4. 11.3 *. -..4 * *0,5
- 0.0 * ~*? ;_ 0.9. *0.7 * -1.7
- 1.4
- z.z , O.O. *l,O ,
, 0.34 , O. 711 , 0.88 , 0.65 , l,'16 , 1.33
- 1.16 , 0.65 , 0.811 , O. 74 , O.Vt ,
, 0,37, 0,70. 0.86. 0.611
- 1,19 .* l.JZ, 1.15, 0.65. 0.69, 0.76
- 0.3S. 1Z
, 8.3
- 4.0 , *0.6
- 1.3 , 1.9 * *0.3 , *1.1 , *O.l
- 1.Z
- Z.5 , Z,6 ,
*******:*ii:;;*:* ii:aii *:*ii:;;::* i:i,:: *i:;ii *: *i:26 *:*ii:;,*:* ;,:,ii*:* ii:i4 *: *** ****
- 0.11
- o.79
- 1.oz
- 1,z& : 1.1s
- 1.u
- 1.01
- 0.111
- 0.1s
- 1J
- 8.J * -o.s
- z. 7 * -o.,:. -1.-. * -o.8
- 1.5
- z.11
- z., .*
* * * * * * * -* * * * * * * * .; * * * * * * * * * ***.-.-.;-*.-;* * * ,i ~ ** * * * -.; . . . . . . . . . . . . . . . . . . . . . . . . . . . .
, 0.35 , 0.9:S , 1,16 , 1.26 , 1,16 , 0.9J , 0.35 ,
- 0.1s
- 0.111
- 1.14
- 1.z*
- 1.16
- o.94
- 0.1s , 14 .
- o.*
- o.* . *-1.5 * -1.s * -o.o
- 1.0
- 1.6
- STANDARD
- o.46
- o.e~
- o.*, * , AVERAGE ,
DEVIATION *
- o.*6
- o.o*
- o.46 * .PCT DIFFEIIEHCE, 15 ..
2z.os1
- O,J
- O.J , O.J ,
- z.,
HAP NO: Sl 2 DATE: 7/ 8/81 POWER: or. CONTROL ROD POSITIONS: F-QCTJ = 2,776 QPTR: D BANK AT 228 STEPS F-DHCNJ = l.796 NW l.003 I NE 0.983
----------1----------
SW l.028 I SE 0.986 B BANK AT 21/22 STEPS FCZJ = l.435 FCXYJ = l.780 . BURNUP = 0 MWD/MTU A.O = 2l.S1Cr.J 36
Figure 7.:3 SURRY UNIT *1 ...;. CYCLE 6 "BOL PHYSICS TEST ASSEMBLYWISE PCWER"DISTRIBUTION I/E CALIBRATION *...;. FLUX MAP
. N n L K J* H G , r D C D PREDICTED
- 11EASUl!ED
- PCT DIFFEREIICE.
- 0.311
- 0.66
- 0.311 *
- 0.15. 0.62. 0.15.
* ***" * *6.6 * ***"
- PREDICTED
- 11USUPED
,PCT DlfFEREIICE
- J 0.311
- 0.92 1.01 0.97
- 1.01
- 0.92
- 0.311 *
- o.37
- 0.1111
- o.9S
- o.n
- 0.11s. 0.1111. o.n
- Zf r
* -2.2 * *"*1. -s.J. -6.0. -s.J. *"*1 * -z.e. I 0,62 . 0.97
- 1,16 , 1,22 , 1,24
- 1,22 , 1,16 , 0,97
- 0."2 *
- 0.41 , 0.96
- 1.16
- 1.17, 1.18. 1.17, 1.11 , 0,94
- 0.40 *
* -1.9 * -0.9
- O.J * -4.Z * "",J * *4,Z * -4,0 * *2,9 ** *2,9
- 0,42 0.91 , 1,16
- 1.26
- 1.24
- 1,24
- 1.24
- 1,26 , 1.u.
- 0,91 , o.u *
- 0,41
- 0,90. 1.16 , 1.a , 1.zo
- 1.ZO. 1,19, l.ZS
- 1.u. , 0.91
- 0.42 *
* *2,Z * *1,3. *0,3, *1.0. *2.7. *J,Z * *"*1 * *0,6 * *O.J. *0.1
- 0,4 * "'*
- 0,311 0.97 1.16
- 1.27
- 1,ZZ ** 1,U
- 1,16
- l.:Z
- 1,ZZ
- 1.27
- 1.16
- 0.97
- 0.311 *
, 0.38
- 0.94
- 1,16 , 1.25. 1.Zl , 1.zo
- 1.14. l.ZO , 1.Zl
- 1.27. 1.19. 0.9'1. 0.311. s
* *0,6 * *Z,". *O,J. *l.4. *0,7. *l.7, *1,4, *l,Z, *1,0 , *O.Z
- 2.4 , 2.1
- 1.J *
- 0.'12
- 1.16 , 1,26
- 1.22. 1.10 , 1.15. 1.0Z , 1.1!1, 1.10. 1.22
- 1.26
- 1.16 , 0.92 *
- 0,'11 , 1.15
- 1.:6 , 1,24
- 1.10
- 1.14
- 1.01
- 1.14
- 1.09
- 1.23
- 1.29
- 1.19
- 0.94 * ,:
* *0.7 * *0,7
- O.Z
- 1,11 * *0,0 * *1.4 * *l.Z * -1.J * *l,6
- 0,6 , Z.l
- Z.6
- Z.J *
, 0.38
- 1.01
- 1.zz
- 1,24
- 1.22
- 1,15
- 0.92
- 1.12
- 0.92
- 1.15
- 1.22 , 1.24
- 1.22
- 1.01 , 0.311 ,
. , 0,38
- 1.00
- 1.Zl
- 1,24 . 1,24
- l.111
- 0.91
- 1.11
- 0.'11 , 1.14
- 1,23
- 1.27
- 1.ZJ
- 1.03
- 0.39
- 7 .
* -o.6 * -0.1. -0.1. o.6. z.1. z.1 * -1.1 * -1.2. -1.J. -1.2. o.6
- z.,. 1.5. 2.s. z.1 *
**a:"*** a*:;;*** i:z.;* **i:24*: *i:i, *: *i:at: *i:ii *: *i:oo *: *i:ii ***i:az *: *i:i, *: *i:z. *: *i:z~ *: *;:,; *: *;:,;,; *:
- o.66
- o.96
- 1.21
- 1.24
- 1.111
- 1..04
- 1.14
- 0,99 .* 1.11
- 1.01
- 1.16
- 1.zs
- 1.n
- o.911
- o.67 *
* -o.a * -1.0 * -o.6
- o.5
- 1.6
- 1.s
- 1.6 * -1." * -1.1 * -1.0
- o.z
- o.9 * -o.s
- o.4
- z.o *
, 0,38
- 1,01 l.ZZ
- 1,2"1 , 1,22
- 1,15
- 0.92
- 1.lZ
- 0,92 , 1.15 , 1.22 , 1.24
- 1.22
- 1.01 0,311 ,
- 0.311
- 1.01
- 1.23
- 1,25 , 1.24
- 1.17 , 0,'11
- 1,14
- 0.91 , 1.14
- l.Zl
- 1.24
- 1.22 , 1,02
- 0.39 *
* *0,1 . O.S. 0.9, l,J, 1 .... 1,5. 1,4, 1,1. *0,9, *0.9. *O.J. O,Z. O.Z. l,l
- 1.7,
- 0.92
- 1.16
- l,ZI,
- 1.22
- l,10
- 1.15
- l,OZ
- 1,15
- 1.10
- l.ZZ
- 1.26
- 1.16
- 0.92 *
- o.94
- 1.111
- 1.21
- 1.zz
- 1.11
- 1.11
- 1.0"
- 1.11
- 1.12
- 1.2:s
- 1.21
- 1.11
- o.n *
- z.4
- 2.<,
- 1.1
- o.z
- o."
- 1.9
- 1.a
- 1.6
- 1.0 *. 0.9
- 1.0
- 1.0
- 1.z *
- o.Ja
- 0.97
- 1.16
- 1.21
- 1.22
- 1.zz
- 1.16
- 1.zz
- 1.zz
- 1.21
- 1.16
- o.97
- o.38 *
- 0.111
- o.911
- 1.11
- 1.26
- 1.:z
- 1.zs
- 1.111
- 1.zs
- 1.zs
- 1.28
- 1.16
- o.97
- 0.111 *
- 1.6
- 1.6
- o.z * -1.2
- o...
- z.J
- 1.9
- z.s
- 2.11
- o.4 * -o.s * -0.1
- 0.11 *
- o.4Z
- o.91
- 1.16
- 1.26
- 1.z*
- 1.z"
- 1.2"
- 1.26
- 1.16
- o.91
- o.*2 *
- 0,42
- 0.91
- 1,1S
- 1,27
- 1.26
- 1.25
- l.ZS
- 1,29
- 1.17
- 0.119
- 0.42 *
- o.5 * -o.s * -1.1
- 1.z
- z.2
- 0.1
- 1.1
- z.z
- 0.1 * *Z,6
- 0.1 *
- o.42
- o.97
- 1.1,
- 1.u
- 1.z*
- 1.zz
- 1.16
- 0.,1
- o.u *
- o.42
- o.95
- 1.n
- 1.22
- 1.21
- 1.21
- 1.111
- o.97
- o.*1
- 1J .
- 0,5 * *l,J
- Z.7
- O,l * -Z.l * *0.7. z.o
- 0.1 * -1.1 *
- 0.31
- 0,92
- 1,01
- 0.97
- 1.01
- 0,92
- 0.38 *
- 0,39
- o.94 ** 1,01
- 0.96
- 0.99
- 0,'12
- O.J9 *
- J.O
- Z.9
- O.S * -1.J * *1,5
- l,J
- Z,4
- STAlllARD
- 0.38 , D.66
- 0.38 * , AVER.AGE DEVIATION , , 0,39. D,67. 0.37. .PCT DIFFERENCE. 15J
- 1.,
21,325
- Z.4
- D. 7 * -1.a
- I MAP NO: Sl 3 DATE: 7/ 8/81 POWER: 32?.
CONTROL ROD' POSITIONS: F-QCTl = 2.184 QPTR: D BANK AT 160 STEPS F-DHCN) = 1.473 NW 0.986 I NE 0.989 FCZ) = 1.439
----------1----------
SW 1.013 I SE 1.012 " FCXYl = 1.414 BURNUP = 0 MW0/11TU A.O = -7.19(?.l 37
Figure 7.4 SURRY UNIT 1*~ CYCLE'6 BOL PHYSICS TEST ASSEMBLYWISE'PrnER*DISTRIBUTION I/E CALIBRATICN - FLUX MAP p t: K J H G , [ -o "?" D" -I R i 0.39 0.611 , 0.]9 PREDICTED 1it-1' PREDICTED tl 11EASUl!ED 0,311 0.66. 0.38 11EA5l'R[D
*].l *],3 , *l, 7 ,PCT DIFFEREIIC!, ;,
, PCT DIFFERENCE.
0,37 0.91 l.OZ l,OJ l,OZ 0.91 0,37 i:~* o.39 o.e6 o,QII o.'111 1.ao 0.,1 o.]11 ti
-5.t . .... t . * ,.,5 . -t.z
- o." .
1.z 1.z h 0,41 o.95 1.1"
- 1.zz 1.u
- 1.zz 1.14 o.95
- o.u o.<o: o.97 1.14. 1.15 1.111. 1.111 1.15 o.n. o.42 3 2,9 1.5 *O,Z *, *5,J *5,3 , *J.O o., 1,6 , 2,4 <
0,41 0.90, 1,15 1,25, l,ZJ. l,ZJ, l,ZJ, 1.Z5 1.15 0,90 0.41, o.4Z
- o.9o
- 1.1s
- 1.z1
- 1.19
- 1.111
- 1.16
- 1.zz
- 1.15
- o.90
- o.tiz
, 3,Z , 0,6 , *O,Z , *1,1 , *2,9 * *J,7 , *5,t , *Z,J , *O,l , 0,6 , Z,5 "'.~
0.37, 0."5, 1,15, 1.26 , 1,ZZ , l,ZZ , 1,16 , 1.Z2 , 1.zz , 1,Z6 1,15 0.95 0,37, f 0,311, 0,'13, 1.l<t , 1.Z<t, 1.21 , 1,20 , 1,14, 1.1'1, 1.111 , 1.24, 1.15 , 0,911 , 0,39 , 5~ 1,2 , *2.3 , *1,0 , *1,6 , *l,O , *l,J , *0,9 , *Z,3 , *1,2 , *Z,O , O,J , 2,6 , ,.,6 , 0,91 1.1 .. , 1,2!1 1.ZZ 1,16 , 1,16 , 1.oz 1,16 1,16 1.ZZ 1,25 1,14 0,91
, 0,9Z , 1,16 , 1.24, l,ZZ , l;l!I, 1.15, 1.0Z , 1.1", 1,11 , 1,21 , 1.25 , 1,17, 0,94 , 6
- 1:z
- 1.2 * -o.z * -o.o * -0.11 * -o., * -o.,. * -1,5 * -1.11 * -1.5
- o.,
- 2.1
- 1.1
- o.39 1.oz 1.zz 1.21 1.zz 1.16 0.9Z 1.1t o.9z 1.16 1.22
- 1.n 1.zz 1.az 0.19 0.39 1.03 l.n 1.24 l,ZJ 1.17 0.92 l.lZ 0.92 1.14 1.Zl , 1,24 1.22 1,03 0.39 7
, 1.s o.5 0.11 o.6 1.0 1.0 -o., -0.1 -o., -1.1 -0.11
- 1.z o.6 1.z 1.s
[i
- 0.611
- 1.n
- 1.z5
- 1.n
- 1.16
- 1.02
- 1.u
- 1.00
- 1.12
- 1.oz
- 1.16
- 1.n
- 1.25
- 1.01
- 0.611 *
, 0,69 , l,DJ. 1.23. 1,24. 1,111. 1.04. 1.14, 1.00. 1.11
- 1.01
- 1.15
- 1.23
- l.Zlt
- 1.04 , 0,71
- e(
, 1.5. o.o * -1.1
- 0.1. 1.11. 1.11. 1.1. o.r. -o.*. -o.,. -0.1
- 0.1 * -0.11. 1.3. 3,'I. ~
o.39. 1.02. 1.zz. 1.23. 1.zz. 1.16. o.,z. 1.12. o.9z. 1.16. 1.zz. 1.21. 1.zz. 1.02. o.39.
~
0.39. 1.03. 1.zz
- 1.24
- l,Z'I
- 1.111. 0,9ft. 1.12
- 0.9Z , 1.16
- 1.:1
- 1.23, l.Zl , 1.04
- 0.41 ,t~
1,5 * *o.6
- 0.1
- 1.1
- 1.11
- 1.11
- 1.11
- o.5 * -0.1 * -o.5 * -o.J * -o.3 * -o.z
- z.z
- 5.1 ,
- o.91
- 1.14
- 1.z5 1.zz 1.16
- 1.16
- 1.oz
- 1.16 1.u 1.zz 1.25 1.14
- o.n *
- o.93
- 1.16
- 1.26
- 1.21 1.16
- 1.11
- 1.n
- 1.11,
- 1.1,
- 1.zz
- 1.zs
- 1.15
- o.n
- 10,
, 1,7 , 1,7 , 0.11
- O.Z
- O.:S , o ... , 0.5
- 0.0 , *l,l * *0.6
- O.l , 0.7
- 1.5 ,
- o.37
- o.9!1
- 1.15
- 1.26
- 1.zz
- 1.zz
- 1.16
- 1.zz
- 1.zz
- 1.26
- 1.l!J
- o.9!1
- o.37 * !'i
- 0.39
- 0,911
- 1,16
- 1,24
- 1.22
- l.Zlt
- 1.16
- l,ZZ , 1.zo
- 1.25
- 1.15
- 0.97
- 0,311 ,
.. ....*.,r*.-o.41
* :s.1 ; 3.1
- 1.1 * -1.6
- 0:1
- 1.s
- 0.1.* o.s * -1.1 * -1.z
- o.6
- 1.1
- 2.1 *
- 0.90
- 1.15
- 1.25 .* 1.n
- 1.n
- 1.21
- 1.25
- 1.15
- o.9o
- 0 ... 1 *
.* :o.43. 0.91
- 1.n .1.z&. 1.zs. 1.z:s. 1.z:s. 1.25. r.1s. o.90
- 0,4Z
- 11 lZ
}~* 4,5 , Z,1 * *1,6 , 0,9 , 1.11 , *0,1 * *O.Z
- 0.6
- o.z
- 1,1 , l,Z ,
, 0,,.1
- 0.9!1 , 1,1,.
- l,t2
- 1.25 , l,ZZ , 1.1* , 0.95
- 0.41 ,
O,lt3
- 0.94
- 1,17 , l,Zl , l,Zl
- l,Zl
- 1.16
- 0.97
- 0."2 13
, 4.5 * *1,6
- Z,5 , *O ... , *Z, 7 , *0.11 , 1.11 , 1,6 , Z,O
- o.l7
- o.91
- 1.oz
- 1.01
- 1.02
- o.91
- 0.11 *
- o.40
- o.96 , 1.o<o
- 1.oz
- 1.01
- 0.,2
- o.311
- H
- 5.11
- 5.7
- z.o * -o.6 * -1.0
- a.s
- z.a
- STAll!IARD 0,39
- 0.611 , 0,39 , , AVERAGE ,
DEVIAT10H o.u
- 0.10
- 0.311 *
- PCT DIFFEREHCE. 15
=l.3119
- 5,5
- z.11 * -1.1 *
- 1,6
SUMMARY
MAP NO: Sl 4 DATE: 7/ 9/81 POWER: 4TI. CONTROL ROD POSITIONS: F-QCT> = 1.930 QPTR: D BANK AT 180 STEPS F-DH!Nl = l.451 NW 0.994 I NE 0.994 'I FCZl = l.294
----------1----------
sw 1.011 I SE l.001
. FCXYl = l. 374 BURNUP = 10 HWD/MTU A.O = -l.18Ci0 38
Figure 7.5 SURRY UNIT *1 """ CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE'PCWER.'DISTRIBUTION I/E CALIBRATION - FLUX MAP p I( J p II R N
" L H G t: C II A PPED!CTED , 0.40 0.70 0.40 l'!!EDICTED ,
HEASURED 0,37 0.65 0,37 HUS\/RED l {
~
.PCT DIFFEREIICE, 0.39 0,9]
-7.11 l.Ol
-11.1 1.02
-7.11 1,0l 0.91 0.39
,PCT DHFEREIIC!.
I O.J9 0,07 0.96 0.9S 0,96 0,117 0,35 ei ~ 0,7 -6,0 , -6.11 , -7.4, -6.11, *6,0 -z.o r 0.43 0,96 1.14 , 1.ZZ 1.ZS 1,Z2 l,14 0.96 O.U 0,"3 0.97 1,15 , 1,14 1.17 1.14 1,07 0.94
- 0.4Z :sl 0.6 0.5 0.4 *. -6.0 -6.0 *6.0 -6.0 -z.o -z.o r
f 0.4] 0,91 1.14 l.Z4 1,2: l.ZZ l.ZZ 1.Z4 o.43. o.91
- 1.14
- 1.n
- 1.111. 1.111. 1.14
- 1.a
- 1.u
- o.n
- 0,41 1.14 0,6 , -0.4 , *0,0 * -0.11 , -Z,6 , -J,11 * *6,0 , -2.1 , -1.0 , -0.7 , 0.0 0,91 0,4l 4 !,:
i, 0,39 0.% 1.14 l.ZS l,ZO l.ZO 1,14 1.ZO l,ZO l,ZS l,lc; 0.96 0.31 0,39 0.91 1.14 1.23 1.ZO 1.20 1,13 1,20 1.19 1.23 1,16 0,97 0,39 sf,,
-1.0 * -1.: . -0.1 * -1.1. -o.z . -o.c;. -o.s. 0.2 * -o.6 * -1.1
- 1.1
- 1.0
- o.c; 11 0,93 1.14 1.Z4 1.20 1,12 1.15 1.03 1.15 1.lZ 1.:0 1.24 1,14 0,93 ~
t 0,92 1.13 1.25 l.Z3 1.13 l,lc;
- 1.0Z 1,15 1.12 1.Zl 1.26 1,16 0,94 6 t;
-1.0 -1,0 0.6 Z,9 0.9 -0.5 *0.6 0.0 O.Z
- 0.40 , 1.01 , 1,Z2 , 1.22 , l.ZO , 1.15 , 0,93 , 1.13 , 0.93 , 1.15 , 1.ZO , 1.Z2 , l,ZZ 0.7 1.5 1.6 1.0 1.0l , 0,40
!;
, 0.1;0
- 1.01
- 1.:0
- 1.:2
- 1.zs
- 1.19
- o.Ql
- 1.11
- o.9J
- 1.15
- 1.22
- 1.:5
- 1.22
- 1.04
- 0,40
- 7/:
* -1.1 * -1.4 * -1.z
- 0.1. 3.6
- 1.1 * -o.6 * -o.4 * -0.1
- o.o
- 1.1
- 1.1
- o.6
- 0.11. o.o *
- 0.70 , 1,0:! , 1,25 1.22 1,14 , 1.03 , 1.13 , 1.0:S 1.13 I.OJ , 1.14 l.ZZ 1,25 1,02 0.70 r
' , 0.70 , 1.00 , 1.:2 , 1.:3 , 1,17, 1,05 , 1,17. 1.0:S, 1.13 , 1.02 , 1,15 , 1.:1. l.ZJ, 1.00 , 0.70 , at
, -1,3, -z.o , -Z.5, O.Z , 2.9, Z.4
- 3,l, -0.l , 0,2 , *0,2 , 1.J , 0.9, -1.Z , -2.1 , -0.l *
*~ ~ .........................................................................................................
0,40 1,03 l.:z l.Z2 l.ZO 1,15 0,9J 1.13 0.9J 1.15 l.ZO 1,22 1.22 1.01 0,40
~ 9¢ 11 0.40 1.02 l.U 1.Z3 1.22 1.17 0.'14 1,16 0,?4 1,16 l.U l.Z2 1,20 l.OZ 0,41 * ~ -1.1 -o.,s -0.1 o,9 1.J 1.9 o.9 z.1 0.11 1.1 o.9 -0.1 -1.0 -a.a 1.0 t t
0.93 0.95 1,14 1.17 l.Z'* l,ZS l.ZO 1.ZO 1.12 1,12 1.15 1,111 l,Ol 1,05 1.15 1,17 1.12 1.14 l.ZO l.Zl 1.24 1.25 1,14 1.14 0,93 0,92 * ~I 2,1 Z,l 1,0 0,3 0.4 2,6 . 2,6 Z,S 1,8 1,3 0.9 -0,1 -0.9 l 0.39 , 0.96 , 1,14
- l.ZS , 1.20 1.20 , 1.14
- 1.:0 , 1.20 1.25 1,14 0.96 0,39
~
~
- 0.19
- o,97
- 1.1s
- 1.:5
- 1.:1
- 1.n
- 1.11
- 1.:4
- 1.:1
- 1.z5
- 1.14
- o.96
- o.J9 ll~
- 0.1.
...0,41
.. .. ., .0,91 0.1. *
......* .1.14 0.2 * -o.4
- o.6
- z.4. Z,6
- 1.0
- z.11. o.z * -0.1 * -0.1. -0.11 *
, l,Z4
- 1,22 , 1,22 , l.ZZ
- l.Z4 , 1,14 , 0,91 0,U
- 0,91 , l,H , l,ZS
- l,Z4 , l.ZJ , 1.2]
- l,Z7
- 1,.15 , 0,91
- 0.4]
0.4:S ll(*
, -0,11, -0.7, -0,5
- 1,1 , 1.6. O.Z , l,Z , Z,4 , 0.8. -1.0 , -0.:S.
o.43. o.96
- 1.14
- 1.zz
- 1.25. 1.zz
- 1.14. o.%
- o.41 o.42
- o.96
- 1.11
- 1.zo
- 1.:0
- 1.:0
- 1.11
- o.9s
- 0.42 13.,
..-o.a *
-o.s
- 2.2 * -1.1 * -1.11 * -1.1
- 2.s
- 1.4 * -o.a 0.19 0,93 1,03 1.02 1.01 0.91 0.39
- o.39
- o.M 1.02 o.99 1.01 o.n
- l,J
- l,Z , -1.Z * -2,6 * -1,9 , 0.5
- l.O ,
o.40 14f STAIIDARD 0,40 o. 70 0,40 , AVERAGE , DEVIATION
- 0.41
- 0,70 0,39 * .PCT DIFFERElltE.
=1, 777 o. 7 -0.6 -z.z
- 1,7 15" ,,
\'
HAP NO! Sl 5 DATE: 7/13/81 POWER: 57/. CONTROL ROD POSITIONS: F-QCTJ = 1.986 QPTR: D BANK AT 175 STEPS F-DHCNl = 1.451 NW 0.991 I NE 0.992 FCZl = 1.327 SW 1.010 I SE 1. 007 ~. FCXYJ = 1.395 BURNUP = 30 MWD/MTU A.O = -7 .65(Y.) 39
Figure 7.6 SURRY UNIT l *...:. CYCLE .6 'EOL PHYSICS TEST ASSEMBLYWISE PO'JER'DISTRIBtJrION I/E CALIBRATION'""" FLUX MAP R p L ; , f N
" K J D C 8 A t !* PREDICTED *
- o.1o1
- o.tJ
- o.u
- PIIEDICTED ,
;
- 11EASU1lED *
- 0.3&
- 0.67
- O.J9. , 11EASU1!ED , 1~
.PCT DlFFEl!EIICE.
0.39. 0.92
* -7.0 * -7.Z * -5.5
- 1.04 1.06 0.1a
- o.e8
- o.98
- 1.00
- o.99
- o.e,
- o.:sa 1.04. 0.92
- O.J9
,PCT DlffUEIIC!
- r fl t i:},*
-1.0 * -4.1 * -s.6 * -6.o * -ti.s * -J.z * -2.8 I
- 0.42
- 0.95 , 1.13 , 1.21 , 1.25 , 1.21 , 1.13
- 0,95 , 0."2 ,
- 0,42 , 0,95
- 1,14 , 1,16 , 1,ZO
- 1,17
- 1,10 , 0.9J
- O.U , 3f I
* -o.9 * -o.J
- o.4 * -4.2 * -4.J * -l.8 * -1.2 * -2.6 * -2.2 *
, 0,42 0.90 , 1.ll , 1.23
- 1.21 , 1.22 , 1.21 , 1.23 , 1.ll
- 0.90 , 0.42 *
, 0.42 , 0.90 , 1.13
- 1.22
- 1.18 , 1.18 , 1.16
- 1,22 , 1,lZ , 0.90 , 0.42 , .r
..0.1,
.......o.95 .......1.n
* -1.0
.......1.zti
.......1.20
-o.,
- o.o * -o.6 * -Z.4 * -1.0 * -4.1 * -o.9 * -o., . -o.6
- 0.2
- 1.20 1.1* 1.20 1.20
- 1.2* 1.u o.95 o.n
- 0.38 0,94 , 1,13 1,24 1,20 1.19, 1,U, 1,19 1,19 1.24, 1,1", 0,96 , 0,39, I
* -0.1. -1,4
- o.4 * -o.6 * -0.1 * -1.z * -0.1. -o.6. -o.,. -o.,. 1.0
- 1.4. 1.* *
- 0,92
- 1.13
- 1.:J
- 1,20 , 1.16 , 1.15
- 1,0l
- 1.15 , 1.16
- 1,20
- I.ZJ
- 1.ll , 0.92 *
, 0.92 , 1.12, 1.24, l.2J. 1,16, 1.15. I.OS. 1.15, 1.15, 1.21, 1.25, 1.15, 0,93, I I e
, 0.41 I I*
* -0.1. -0.1. o.e. 2.5 , 0.1. -o.8. -o.J. -o.J. -1.0
- o.*. 1.s. 1.8. 1.J.
e e * * * * * * * * * * * *
- e 1.04 1.21
****I I I* e *I******* I** a*
1.21 1.ZO 1.15 , 0.94 I e e * *
- e *
- e e e *
- e * * ** ee * * *
- e 1.U
- 0.94
- 1.15
******I** I* e 1.20 1.21 I e e * *
- e ** * * * * * * * * * * * ** e 1.21 1.04
- 0.41 o.41
- 1.01 1.zo 1.22 1.:1 1,19
- o.94 1.u
- o.94
- 1.15 1.21 1.24 1.:z 1.04
- o,41 7
-1.4 -1.0 -0.1 0.1 2.8 2.8. -o.z o.o
- o.o * -o.s o.9 2.1 o.4 o.4 * -0.2
..*, *o:0,71;j*:,
- i:1.05o& *:, *1.Z4 i:zs**, *1,Z2 i:22 *:, *1.16 i:i.i **, *i:oi *: *i:ii *: *i:oi *: *i:ii *: *i :oi***i:i; *: *i:zz ***i:is***i:o, ** *o: ;;**
1.05 , 1.16 , l.Ol , 1.ll , 1.0Z , 1.1, , 1.2]
- 1.24 , 1,04 , 0.7Z , er
~
* -1.5. -1.4. -1.2. o.5. 2.2. 2~0. 2.1. o.J*, o.o. -o.4. o.8. o.8. -1.1. -z.1. -0.1.
**I** I****** I**** I I I***** I I I* I** I** I** I* I* I***** I* I** I** I****** I****** I***** I I I I* I** I* I I* I I I I I*** I* I I* I* I I
, 0,41 , 1.04
- l.Zl , l.Zl , 1.20
- 1.15 , 0,94
- 1.ll , 0.94
- 1.15
- 1.20 , 1.21
- 1,21 , 1.04 , 0.41 ,
- ct.41
- 1.04
- 1.22
- 1.22
- 1.22
- 1.19
- o.95
- 1.16
- o.94
- 1.16
- 1.20
- 1.20
- 1.20
- 1.01
- o.41 * , *..
, -1 *** -0.J. O.Z
- 1.1
- 1.6
- 1.9, 1.5. 2.Z
- 0.2
- 0.5. O.l. -0.5. -0.9. -0.6 , 0.7 *
- o.92
- 1.n. 1.2J. 1.zo
- 1.16
- 1.15. 1.n. 1.1s. 1.1,
- 1.:0
- 1.21. 1.u. o.92 *
, 0.94
- 1.15 , 1.24 , 1.21 , 1,16 , 1.10
- 1.05 , 1,18 , 1.17
- l,U , 1.23
- 1.U , 0.92
- 10,
.. 0.39. .. .....1.11. .......1,24.
...... ..1.20,...... ....... ...... ....... ........ ..... .......... ....... .....
- 1.6 , 1.6
- 0.9
- 0.4
- 0.5
- Z.2
- 2.z , 2.0
- l.l , 0.8
- 0.2
- 0.1
- 0.1 *
.......0.95. 1.20. 1.14. 1.20. 1.20. 1.24, 1.11. 0.95, 0.39,
*0.1,
- 0.,1
- 1.11o
- 1.21
- 1.21
- 1.zs
- 1.16
- 1.n
- 1.u
- 1.24
- 1.n
- o.9s
- o.n
- 11/i
- 1.6
- 1.5
- o.5 * -o.8
- o.6
- 2.4
- 2.2
- z.1
- z.1 * -o.o * -0.1 * -0.2 * -o.o
- e I I I e
- I e I I* I** I I I* I* e. I e *I*** e *I* e e II I*** Ill I I I I e I I e I I I ae I II I I I* I* II** I II I I I I e
, 0.4Z
- 0.90 , 1.1]
- 1.21 , 1.21 , 1.zz , 1.21 , l,Zl , 1.ll
- 0.90 , 0.4Z ,
- o.41
- 0.,1
- 1.12
- 1.24
- 1.n
- 1.22
- 1.22
- 1.25
- 1.1,
- o.89
- o.*z
- 11
- 1.5
- o.6 * -o.,
- 1.z
- 2.0
- o.5
- 1.0
- 1.a
- o., * -o.9 * -o.z *
- 0.4Z
- 0,95
- 1.13 , 1.21
- 1.25
- 1.21
- 1.13 , 0.95
- O.ltZ *
- o.o
- o.94
- 1.16
- 1.21
- 1.zz
- 1.20
- 1.1s
- o.96
- o.4Z
- 1J
.. ...... ... .. ......z.6.....* ..... ... .. ..... .. .. ... .. .... ..o.e.. .......
- 1.s * -o.,
- 0.39
-o.3 * -z.6 * -o.9
- 1.6*
- 0.92 , 1.04 , 1.06
- 1.04 , 0.92 0.39
. -0.1 *
- 0,39 0.94 , l.Ol 1.05 1.03 D.9S
- D,39
- H(f 1.7 , 1.6 , -0.5 * -1.7 * -1.l
- O.l
- Z.O *
[i STANDARD 0.<11 , o. 73 , 0.41 , , AV[IIAGIE , ~ DEVIATION
- 0,42
- o. 73
- 0.41 * ,PCT D1ff£REIIC!, 15U
=l.330 l.l
- 0.1 , -1., *
- 1., ~
~
SUMMARY
MAP NO: Sl 6 DATE: 7/14/81 POWER: 65?. CONTROL ROD POSITIONS: F-QCT) = 1.918 QPTR: D BANK AT 200 STEPS F-OHCN> = l.43S NW 0.991 I NE 0.992 '1 FCZ> = 1.282
----------1----------
SW 1.012 I SE 1.oos FCXY> = 1.389 BIJRNUP = 35 MWO/MTU A.O = 5.90(,-) 40
Figure 7.7 SURRY UNIT 1 ....; CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE'PCWER'DISTRIBurION I/E CALIBRATION*- FLUX MAP I
- p H
" L I( J H G [ D C II A PREDICTED ,
- a.42
- o.n. o.tiz
- PREDICTED *
, M£ASUR£0 ,
- 0.19
- o.~a
- o.40 *
- HtASL'11£D ,
r ,PCT DIHERCNCE. , -6,7, -6.11, -4.7, ,PCT DIFFERENCE.
- 0.1,
- o.9:
- 1.04. 1.01. 1.a,
- o.92
- o.39.
zl l
- o.n
- o.87. o.95. 1.01
- 1.00
- o.91
- o.38.
, 0.1 , -5.5 , *6,l. *6.J * -4,l * -1., . *1,6 * \
- 0,'12
- 0,95 , l.U, 1.21 , 1.zs, 1.21
- l,U. 0.95
- o.-.z
- t
, 0.42
- 0.95 , l,U
- 1.1'
- 1.111 , 1,16
- 1,11
- 0,9J , 0.42 , JI
- 0,1 , O,Z , D,S * *5,5 * *5,5 * * -..o , *1,6 * *l,6 , ~1.6 *
, 0.42 , 0,90 , 1,12 , l,ZZ , l,ZO , 1.21 , 1.ZD
- l,ZZ
- l,lZ , 0.90
- O,U ,
- 0.1 * -o.*.
- 0,42
- 0.90 , 1,12
- l,Zl
- 1,17. 1.17. 1.14. 1,21
- 1,12 , O,H. 0.42 *
-0.1 * -0.1 ** z.s. -J.6 **,., * -o., * -0.1 * -o., . 0.1 *
. o.n . o.n
- 1.12
- 1.24
- 1.20
- 1.zo
- 1.n
- 1.20
- 1.zo
- 1.z,
- 1.12
- o.95
- 0,39 *
, 0,39. 0,93 , l,lZ , 1,22 , 1.19. 1,19. l.lJ, 1.19, 1,19, l,U. l.lJ, 0,96, 0.39,
, *0,7 , -z.z * *O,J , *l,3 * *0,4 * *0,6 * *0,6 * *0.7 * *0,1 * *0,7
- D,'I
- 1,0
- 1,3 *
- o.92
- 1,13
- 1.22
- 1.zo. 1.11. 1.u.. 1.n. 1.16
- 1.11. 1.20
- 1.zz
- 1.u
- o.9Z *
- o.n
- 1.12
- 1.zz
- 1.n
- 1.11. 1.15. 1.n. 1.15
- 1.u, . 1.20 , 1.21. 1.1, , o.93, 6'
, *0.7 , *0,7 , 0,0 , l,S
- D,O , *0,6 , *0,5 , *O,'I * *0.9 , 0,1 , 0,9 , l,! , l,O ,
, o.'IZ
- 1.a,
- 1.21
- 1.zo. 1.20
- 1.16
- o.95. 1.1,. 0,95. 1.16. 1.2a. 1.20
- 1.21
- 1.04
- o.42.
, 0.41
- 1.03 , 1.za , l,Zl , 1,22 , 1,111 , 0,94 , 1.14 , 0.95 , 1,15 , 1.n , l,Z] , l,Zl , 1.04 , 0.41 , 7
, *1,9 , *1,4 , *0,9 , O,S , Z,l , 2,1 , *0,5 , *0,2 , -O.l * -0.4
- 0,7 , 1,9 * *0,1
- 0.0 , *0.7 ,
- o.n
- 1.01
- 1.25
- 1.21
- 1.n
- 1.0:s
- 1.14
- 1.H
- 1.14
- 1.n
- 1.n
- 1.21
- 1.zs
- 1.01
- o.73 *
- o.n. 1.05. 1.21. 1.zz. 1.u.
- 1.as
- 1.11. 1.0,*. 1.14. 1.01
- 1.1,. 1.zz
- 1.21
- 1.05
- o.n *
* -r.1 * -1.9 , -1.1
- 0.1
- z.1
- 1.6
- z.:s
- 0.1
- o.z * -0.1
- o.,
- o.z * -1.s ** z.s * -o., .
- 0.4Z
- 1.04
- 1.21
- 1.20
- 1.::0
- 1,16
- 0.95
- 1,1'
- 0.95
- 1.1'
- 1.20
- 1.zo
- l,Zl
- 1,04*, O.ltZ ,
- o.41
- 1.01
- 1.21
- 1.21
- 1.21
- 1.11 , o.9s
- 1.19
- o.9s
- 1.11
- 1.n
- 1.20
- 1.20
- 1.n
- o.tiz *
, *1,9 , *0,8 * *0,3 , 0,6 , 0,S , 1,3
- 0.6 , '1.0
- 0,6 , 1,0 , 0,7 * *O.Z , *l,Z , *0,1 , 1,1 ,
- o.9z
- 1.n
- 1.zz
- 1.:0
- 1.11
- 1.16
- 1.n
- 1.16
- 1.11
- 1.20
- 1.zz
- 1.n
- a.9Z *
- o.n
- 1.14
- 1.:1
- 1.20
- 1.11
- 1.21 , 1.os
- 1.19
- 1.18
- 1.:1
- 1.z1
- 1.u
- o.n
- 10
- 1.J
- 1.z
- o.4 * -0.1 * -0.1 * ,.1 * -..1
- z.1
- 1.J
- o.e
- o.e * -0.1 * -0.1 *
- o.39
- o.95
- 1.12
- 1.z4
- 1.zo
- 1.20
- 1.n
- 1.zo
- 1.zo
- 1.211
- 1.12
- o.95
- o.J9 *
, 0,39, 0.96
- 1.12 .*1.z3, l.Zl. 1.z*. 1,18, 1,24. 1,ZZ , 1.Z4
- 1.12
- 0,95. o.J9, 11
. o.e . 0.1
- 0.1 * -o.9
- o.,
- s.<1 * ,.,
- 3,J
- z.1 * -o.z * -0.1
- o.o * -o.J *
- o.u
- 0,90
- 1.12
- 1.22
- 1.20
- 1.n
- 1.zo
- 1.zz
- 1.12
- 0,90
- o.u *
- a.o
- 0,90
- 1.11
- 1.z4
- 1.zs
- 1.zz
- 1.zz
- 1.z4
- 1.n
- o.s9
- o.u .
, O,'I , *0,1 , *0.9
- 1.3 , Z,Z , 0,7 , 1.1 , 1.7 , O,* , *0,9
- 0.6
- e e * * * * * *
- e s e s *
- s s s
- s es s s s s s e *
- e ***I**** I**************** I I I**** I* I********* P.**
. o.u . o.95
- 1.n
- 1.21
- 1.zs
- 1.u
- 1.n
- o.95
- o."z *
, o.u
- 0.9*
- 1.16 , 1.20 , 1.zo , 1,ZO , 1.15 , 0.16 , 0.4Z ,
- 0,'I * *0.9 , Z.I * *0.9 * -'1,0 , *1,Z
- z.z , 0.9 , *O,'I ,
- 0.39 , 0,9Z , 1.04 , 1.07
- 1.04 , 0.9Z
- I.H ,
, 0,40
- O.~ , l,OJ
- 1.05
- 1.03
- 0.9'
- O.toO *
, Z,J , Z.3 , *0,5 , *Z.Z , *l,Z
- Z,Z , z.z ,
!ITAIIOAIID * , o.,z . 0.73
- o.u , , AYEIIAGE
- DEVIAT10M , , 0.43
- 0.75
- O.ioJ *
- PCT DJFFERENCIZ, s1.to86 , Z,Z , Z.1 , Z,Z ,
- 1.*
MAP NO: Sl 7 DATE: 7/14/81 POWER: 85Z CONTROL ROD POSITIONS: F-QC Tl = 1.828 QPTR: D BANK AT 204 STEPS F-DHCNl = 1.421 NW 0.988 I NE 0.988 FCZ) = l.232
----------1----------
SW 1.012 I SE l.012 FCXYl = 1.383 BURNUP = 40 MWD/MTU A.O = -l.22CZl 41
Figure 7.8 SURRY UNIT 1 - CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION HFP, EQ. XENON R p C B A PRED!CTEO 0.42 0.74 0.42 PRC:OICTED 11EASUREO . 0.40. 0.70 . 0.40. MEASU;;!ED
.PCT DIFFERENCE. . -5.7. -5.7. -4.5. .PCT DIFFEREHCE.
0.39 0.91 l.04 l.09 1.04 0.91 0.39
. 0.39. 0.88. 0.99. 1.04. l.00 . 0.89. 0.38.
0.7. -3.9. -4.8. -4.8. -3.9. -2.7. -1.3. 0.42 0.94 1.12 1.20 l.25 1.20 1.12 0.94 0.42
. 0.43
- 0.94
- l.ll . l.16 . 1.20 . 1.16 . l.09
- 0.?4 . 0.43 .
0.6 . 0.2 * -0.3. -3.9. -3.9. -3.4. -2.7. -0.5. 0.9 .
- 0.42 0.90 1.12
- l.21. l.20 . l.21 1.20. 1.21 l.12
- 0.90 0.42
- 0.43. 0.89. l . l l . 1.21. l.18. l.18. l.15. 1.21 . 1.12. 0.90 . 0.43.
0.1 * -0.1 . -o.3 . -0.1 * -2.0 :* -2.6 . -3.9 . -o.3 . o.3
- o.6 . 2.0 .
0.39 0.94 1.12 l.23 l.20 1.20 ~ l.14 1.20 l.20 1.23 1.12 0.94. 0.39
. 0.39. 0.93. 1.11. 1.22. 1.20 . 1.19. 1.14. 1.19. l.18. l.23. l.12 . 0.96
- 0.40
- 0.5. -l.2. -0.2*. -0.7. -0.3. -0.6. 0.0 * -0.9. -l.4. -0.4. 0.6 . 2.5. 4.2.
0.91 1.12 1.21 l.20 l.~9 1.17 l.04 1.17 l.19 1.20 l.21 1.12 0.91
- 0.92 . 1.12. 1.22. 1.22. 1.19. 1.17 ~ l.05. 1.17. 1.17. 1.20 . 1.22 . 1.13. 0.93. 6 0.5. 0.5. 0.5. 1.2
- 0.2 . 0.0 . 0.7. -0.l. -2.0 . -c.s . 0.6
- l.3. 1.7.
0.42 l.04 1.20 1.20 l.20 l.17 0.96 l.15 0.96 1.17 1.20 1.20 1.20 1.04 0.42 ~. 0.41. l.D3. 1.21. 1.21. 1.22. 1.19. 0.97 .. 1.16
- 0.97. 1.17. 1.20 . 1.21 . 1.19. l.03 . 0.42 *
, * -1.8 * -Q.7
- 0.2
- o.5 . 1.5 . l.5
- o.a . 1.1 . 1.0 . -0.2 * -0.1 . o.8 * -o.9 . -i.o . -1.2
- 0.74 1.09 1.25 1.21 l.14 1.04 1.15 1.05 1.15 l.04 1.14 1.21 1.25 1.09 0.74
- 0.73. l.OS. 1.23. 1.21 . 1.15. 1.06
- l.!7. l.06 . l.lf. . 1.05. 1.14. l.20 . 1.22
- 1.07. 0.7~ .
* -1.a. -1.1 * -1.1. o.5. 1.5. 1.6 . 1.4. 1.4, o.8. o., . o.6 . -o.6 *. -1.9. -1.5. o.6
- 0.42 1.04. l.20 1.20 1.20 1.17 0.96 1.15 0.96 l.17 1.20 1.20 1.20 l.04 0.42
- 0.41. l.03. 1.20. 1.21. 1.22
- 1.19. 0.98. 1.18. 0.96 . 1.17. 1.20 . 1.19. 1.19. 1.04. 0.44. 9
* -1.8. -0.9. -0.5. 0.7. 1.8. 1.7. l.9. 2.3. 0.4. 0.3. 0.2. -1.0 . -1.4. 0.1 . 3.2.
- 0.91
- 1.12. 1.21
- 1.20 . 1.19. 1.17. 1.04. 1.17. 1.19. 1.20 . 1.21 . 1.12
- 0.91 .
t
- 0.92. 1.12. l.?.2. l.Zl. l.19. 1.20
- 1.06. 1.19. 1.20
- 1.21. 1.21
- l . l l . 0.92.
0.4 . 0.4 . 0.3 . 0.3
- 0.3
- 2.3 . 2*.3 . l.6 . 1.0
- 0.4 . -0.l . -0.2
- O.l .
10 ' 0.39. 0.94 l.l2 l.23 l.ZO 1.20 l.14 1.20 1.20 l.23 1.12 0.94 0.39
- 0.40 . 0.96. 1.12. 1.22. 1.21 . l.23. 1.16
- 1.23. 1.23. 1.23. 1.12 . 0.95
- 0.39. 11 r 2.2. 2.2. 0.7. -1.3. 0.4. 2.7. 2.4. 2.3 . 2.0 . 0.2 . 0.4. 0.9. 0.9 *
- 0.42 0.90 1.12 1.21 1.20 1.21 1.20 1.21. 1.12 0.90 0.42
** 0.44. 0.91
- 1.10
- 1.23. l.Z3. 1.21. l.ZO
- l.Zi. 1.12
- 0.90
- 0.43. 12 4.0. 1.9. -1.3. l.3. 2.3. 0.4. O.l. 0.9 .* 0.4. 0.3. 2.5 *
- 0.42. 0.94. 1.12 . 1.20
- l.25. 1.20. 1.12
- 0.94. 0.42.
. 0.44. 0.93. 1.15. 1.20. 1.21. l.!8. 1.12. O.S4. 0.43
- l3
- 4.o. -1.3. 3.1. -o.5. -3.2. -1.8. -0.1. -a.1. 1.1 *
~; ; ;
0.39 0.91 1.04 l.09 l.O~ 0.91 0.39
- 0.40 . 0.95. 1.05. l.08. l.03. 0.91. 0.39. 14
- 3.6. 3.6 . 0.6 . -l.l. -1.4. -0.6 * -o.o
- i STANOARO 0.42 0.74 0.42 AVERAGE DEVIATION . 0.44 0.75 0.42 .PCT DIFFERENCE
- 15
=l.251 3.6 l.7 * -l.3 * = l.4
SUMMARY
MAP NO: Sl 8 DATE: 7/21/81 POWER: 100?. CONTROL ROD POSITIONS: F-Q(T) = 1.810 QPTR: D BANK AT 228 STEPS F-DHCNJ = l.413 NW 0.992 I NE 0.997
----------1----------
sw 1.010 I SE 1.001 F(Zl = 1.223 FCXYJ = l.377 BURNUP = 170 MWO/MTU A.O = -2.47(?.l 42
Se"c:tion 8 REFERENCES
- 1. S. A. Ahmed, T. W. Schleicher, "Surry Unit 1, Cycle 6, Design Report," N'.FE Technical Report No. 183, Vepco, May, 1981.
- 2. Surry Power Station Technical Specifications.
- 3. Surry Power Station Final Safety Analysis Report.
- 4. T. K. Ross, W. C. ~eek, "Control Rod Reactivity Worth Determination By The Rod Swap Technique," VEP-FRD-36A, December, 1980.
- 5. T. J. Kunsitis, "RXFLOW, A Computer Program to Calculate Reactor Flow and Thermal Output," NFO-CCR-8, Vepco, Decemb~r, 1979.
- 6. "Technical Manual for Westinghouse Solid State Reactivity Computer,"
Westinghouse Electric Corporation.
- 7. W. Leggett and L. Eisenhart, "The INCORE Code," WCAP-7149, December, 1967.
43
APPENDIX STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEETS
JUL 3 1981 SURRY POWER STATIC~ UHIT 1 CYCLE 6
- I STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test
Description:
Reactivity Compute:r Checkout Re:fe:rence P:roc Ho /Section: PT28.11/APP. B Sequence Step Ho= ~ II Bank- Positions (Steps) RCS Ternpe:ratu:re C°F): 547 Test Powe:r Level C?. F.P.): 0 Conditions I SDA: 228 SDB: 228 CA: 228 Othe:c (specify): (Design) I CB: 228 cc: 228 CD: X Below Huciea:r Heating I *At the just c:rit. position III Bank Positions (Steps) RCS Ternperatu::e C°F): S1S: 0 'F Test Powe:r Level C7. F. P. ) : -o fo Conditions SDA: 228 SDE: 228 CA: 228 Othe:c (Speci:fy): (Actual) CB: 228 cc: 228 en: 1513 Date/Time Test Per£o:rmed: Measu:red Parameter ~ = Measured Reactivty using ~ -corn?
- IV . CDes-cz:iption) ~ = Inferred React f:rom :react period Heasu:red Va1ue
~est Resul.ts Design Value (Actual Conditions) 7.D = I C~c.. - ~-t ) / ~;t- X 1007. S 4.0?.
Design Value (Design Conditions) 7.D =IC~~---~)/~ I x 1007. S. 4.07. Re:ference WCAP 7905, Rev. 1, Table 3. 6 V FSAR/Tech Spec Hot Applicable Acceptance Crite:ria Re:fe:rence Mot Applicable Design Tolerance is met /YES _NO V:I Acceptance Criteria is met .. 7YES _ _ HO Comments Allowable Range = :!: S 'f pe,m Evaluated By: Recommended £0:r App:roval B.y : NFO Enginee:r A. l
JUL 3 1931 SURRY POWER STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Test Desc:r:iption: C::c:itical Bo:r:on Concent::c:ation - ARO Re£e:r:ence P::c:oc Ho /Section: PT28.11/APP. C Sequence Step No: 7 II Bank Positions (Steps) RCS Tempe::c:atu::c:e (°F): 547 Test Powe~ Level. C?. F.P.): 0 Conditions SDJI.: 228 SDB: 228 CA: 22.8 Othe:r: Cspeci£y): (Design) CB: 228 cc: 228 CD: 228 Below Huclea:r: Heating III Bank Positions (Steps) RCS Tempe:r:atu:r:e (°F): S4S.Z °F Test Powe:r: Level. C:'. F.P.): 0% Conditions SDA: 228 SDB: 2.2..S CA: Z.2..8 Othe:r: CSpeci:y): (Actual) CB: Z..28 cc: Z.2-8 CD: .;t2.8 Date/Time Test Pe:r::fo:r:med: 1-1:;1a1 Meas Pa:r:amete:r:
- I I os 11 IV CDesc::c:iption) I 'C ""
C5 )MO; C::c:i t Boz:on Cone - ARO 1 Test I1easu:.::ed Value CCB ):P.D = I 1-8_ +.-;;;;m.. Resul.ts Design Value
'*( Actual Cond l Design-Value (Design Cond) Cs= 1480 ! 50 ppm Re:fe:r:ence- VEP-FRD-HFE-183 V FSAR/Tech Spec Acceptance
\Cz:ite:r:ia Ref~::c:ence FSAR Section 14.2.5 Design Tole:r:ance is met 7°YES _HO Acceptance C::c:itez:ia is met :Z:YES _NO v:c o< -Comments .C.& = -8.42 pcm/ppm :fo::c: p:r:elimima:ry anal.ysis o<: C B --=- -8.1B re-/pr~ f.w. +\...J """"-'~ys*,s
/
Compl.eted Eval.uated By: J. 4 -1~ Recommended :fo:r: _;,f,.....,..~,) App:coval By C_. A7 __
}ff~ Eng inee:r A.2
JUL 3 1981 SURRY POWER STATION UH!T 1 CYCLE 6 STARTUP PHYSICS -TEST RESULTS AND EVALUATION SHEET I Test Desc:tiption: Isothezmal Tempe:tatu:te Coei:ficient-ARO Re:fe:tence P:toc No /Section: PT28.11/APP. D Sequence* Step Ho= ~ II Bank Positions (Steps) I RCS Tempe?:ature C°F)L 547 Test I Powe?: Level (% F.P.): 0 Conditions SDA: 228 SDB: 228 C".,. . 228 I OtheI: Cspeci:fy): (Design) CB: 228 cc: 228 en= 228 I Below NucleaI: Heating I III Bank Positions (Steps) I RCS TemPeratuI:e C°F): t:."'4L/,1 °f Test I Poue:r L~vel C?. F.P.): -oio Conditions SDA: :Z..Z ~ SDB: :U..l?° CA : "l.2.. 3'" I Othe:r (Specify): CAc t'!._al ) CB: 2.2.%- cc: 22.3- CD: ~C'l.. I Below Nuclea:t Heating I Date/Time Test Pe:i::i:01:med: I 7/1/8! /1../0 "'2.. I I Meas Pa:i:::amete:i::: IV (Desci:iption) ,4so )AAD Iso Temp Coe:£:£ - AP.O Test Measui:ed Value (~o )AAO = - 1~32. pur,/ r 0 CC5 =1r./f::.3 ) pp.-.-- Results nesign Value (Actual Cond) c.qso )AAo -= ~--4.00 +/-?,o r,vnj°f(ce, = 1'-lb3. >pf,.._ Design Value = - 3.79 ! 3.0 pcm/°F (Design Cond) (Cs = 1480 ppm) Re:fe:rence VEP-FRD-HFE 183 V FSAR/Tech Spec ~ 0.45 pcm/°F * ~ p = -2. 05 pcm/°F Acceptance C:z:i te?:'ia Re:fezence TS 3.1, VEP-FRD-HFE 183 Design Tole:i:::ance is met /YES _NO VI Acceptance Crite:i:::ia is met* LYES _NO Comments
- Uncer.tainty on aT MOD
"' 0.5 pcm/Op (
Reference:
memorandum from ~~~~~-L C.T. Snow to E. J. Lo~ito dated June 27, 1980) Completed By~-~.LJ~~~
. Test °tlgit)"
.Evaluated By, Recommended -£or ti ft. ,CP,,Ad,
// /? * /
<< ~
App:roval ~Y ;---z?-?- ~ /C........ ./ XFO Enginee:i:: A. 3
JUL 3 rsar SUP.RY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I I Test Desc:t:iption : H/D Flux Map - HZP, ARO Re:fe:t:ence I P:r:oc No / Section: PT28. 2, OP-57 Sequence* Step Ho: C\ II Bank Positions (Steps) I RCS Ternperatu:r:e C°F):TRE~ !1 Test _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ ! PotJe:t: I.evel o: F.P.): .... o Conditions I SDA= 228 SDB: 228 CA: 228 I Othe:z:: (specify) T (Design) I CB III I I 22s cc : 22s en: 22s I Must have~ 40 thimbles Bank Positions (Steps) 1 RCS TempeI:a tux:e ( ° F) : 5'45" 0 F' Test I Conditions I SDA: :Z2Z SDB: 223" CA: 22.B Powe:r: Level (7. F.P.): ,.....0 I Othe:r: (Specify): (Actual) I CB : z:z.?: CC : ZZli CD: 20 I I I I Date/Time Test :1-,; I I Pe:r::fo:z::rned: 7/7; // /030 I I I MAX. REL I NUC ENTHALITOTAL HEATI 2UADRANT
- rv I Meas Pa:r:amete:r:I ASSY PWR I P.ISE HOT I FLUX HOT !POWER TIL~
I (Description) I ~ DIFF I CHAN FACT ICHAN FACT RATIO I I CM-P)/P I F-dHCH) I F-2CT) 2PTR I I ----------'112. (/'(.._ C f'l(.13=i.;z1I' '--------------- I ;;k Test I Measu:r:ed Valuel/c.4~£-p :o411 /.584 I 2.430 /. 0257. Results I- - - - - - - - ' A~
- I '------ -------
~ Design Value f :io: for Pi .:o.
- 9 I .
- l I cDesign Conds) I ~1s: for Pi< .9 I -!a..s1.ssc1+.2c1-P)) I r~cz:)~4.36 :z: x~z) $ 1.02
*I -------- I (Pi
- Asay. Pvr.) I * - ** J I I WCAP-7905 I I WCAP-7905 I Re:fe:r:ence" I REV; 1 I NONE I HONE REV. 1 I
I - - - - - - - - - '! II 'I - - - - - - - - - - - - - V I FSAR/Tech Spec! MONE I HA I HA MA Acceptance C:r:ite:z:ia - - - - - - - - - - '! II 'I - - - - - - - - - - - - - R.e:£e1:ence I NONE I T.S. 3.12 I T.S. 3.121 T.S. 3.12 I I I I
-------------------' I '------'-------
Design ToleI:ance is met Acceptance CI:ite:z::ia is met VI Comments K °""'SAT"" .-tcl<2.v-~-s no+~, ~ ~ ~s:+.:. .c,.,r'4. A.ce>r--b..bk. j"""' R"k~: L Sv,.<< . f'o~ s+,d~\°" l'.).w'1cet\~ ~e,,y-t:; No: Sl-~l-1,s-. 1 Completed Evaluated By: Recommended £0:z:: Appi::oval By HFO Engineer A.4
JUL 3 7987 SURRY POWE?. STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Test
Description:
Cntl Bank B Worth Meas.-Rod swap Re:£ Bank Re:fe:r:ence Px:oc Ho /Section: PT28.11/APP. E Sequence Step No: \0 II Bank Posi*tions (Steps) I RCS Tempe:r:atu:r:e C ° F) : 547 Test I Powe:c Level C1. F.P.): 0 Conditions SDA: 228 .SDB: 228 CA: 228 I Othe:r: (specify): (Design) CB:t1oving cc: 228 en: 228 I Belot.1 Huc1.ea:c Heating I III Bank Positions (Steps) I RCS Tempe:r:atuxe (OF): S45.Z "F Test I Powe:c Level ( 7. F.P.): 0% Conditions SDA: '-'-8 SDB: z:z.B CA: 'Z..'Z..S I Othe:r: (Speci:Ey): (Actual) CB: l'1o"i"j cc: Z2.8 cn:z'Z.8 I Below Nuclear Heating I Date/Time Test Pe:r:fox:med: I I 1-/7/8! /Zl30 I Measured Parameter ;Integral Wo:r:th o:f Cntl Bank B, CDesc:r:iption) All Othe::c Rods Out IV Test Measu::ced Value I P.$.F = ei Results Design Value IRE.F = jActual Conditions) e, /_4ot +/-:' 14 / f°Cl'Yt. Design .Value (Design Conditions) 1406 +/- 141 pcm R.e:fe::cence VEP-FRD-HFE-183 I£ Design Tolex:ance is exceeded, SHSOC shall evaluate impact 0£ test ::cesult FSAR/Tech Spec on safety analysis. SHSOC may specify
- v. that additional testing be pe:cfo::cmed.
Acceptance C::cite::cia Re:fe::cence VEP-FRD-36A Design ~ole:cance is met VJ: Acceptance C::citeria is met Comments Completed By* Evaluated By: J S. !f;;tdi~ Recommended £0::c App:coval By C. :J. .c-t:-J HFO EngineeJ: A.5
JUL 3 1931 SURRY POWER STAtIOH* UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET. I Test
Description:
Critical Boron Concentration - B In Re:fe:i::ence P:r:oc Ho /Section: PT28.11/APP. C Sequence *Step Ho: \ \ II Bank Positions (Steps) Res- Tempe:i::ature C°F): 547 Test Power Level. C?. F .P.): 0 Conditions I SDA: 228" SDB: 228 CA: 228 Othe:i:: Cspeci:fy): (Design> I CB: .O cc: 228 CD: 228 Below Hucl.ear Heating III Test
!I __________________
Bank Positions (Steps) _ RCS Temperature C°F): 546.l"f" Powe:r:: Level. (?. F.P.): 0 % Conditions SDA: Z..2. 8 SDB: z.z.. g CA: Z'Z-8 othe:i:: CSpeci:fy): (Actual.) CB: o cc: u . s CD=Z.U':l Date/Time Test Perfo:i::med: t-(8/81 I 03-z.o Meas Paramete::c I M IV (Desc:i::iption) I CC5)s ; C:i::it Boron Cone - B Bank In 1 Test Maasu:r::ed Val.ue I I I 3_2.., p f rm Re13ults Design Value*
.(Actual Cond) 'I ca= / 31.. 0 I 2-t -~l°m Design Value 1 (Design Cond) I C B = 1 3 1 6 + ~ C.~RE'I :!: C10 Re:ference 1 VEP-FP.D-HFE-183*
----------'-------------------------1
. V FSAR/Tech Spec
_ _ _ _ _ _ _ _ _ II_________________________ o<.c..5xCe,S15,115pcm _ Acceptance . C1:ite:r::ia Re:fe:r::ence I FSAR Section 14.2.5 - - - - - - __________ l _________~ - - - - - - - - - - - - - - - Design Tole::cance is met 7YES __ HO Acceptance C:r::iteria is met VYES _HO VI . Comments -8.42 pcm/ppm *:for p:r:elimimary analysis
= Cc6 )AAo - 1480 ppm
- 8.TS t""lf'r"' .f-. f.-~- I ~lys;*s Completed By: Evaluated By: J.d. rfM:-
Recommended £01: App:r::oval By c..:J. ~ HFO Enginee:t: A, 6
JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATIOH SHEET I Test Desc:z:iption: Isothermal Temperatu:z:e Coe:f:ficient-B In Re:fe:z:ence P:z:oc Ho /Section: PT28.11/APP. D Sequence Step Ho: l 7: II Bank Positions (Steps) RCS Temperature C°F): 547 Test Powe:z: Level CY. F.P.): 0 Conditions I SDA: 228 SDB: 228 er..: 22s Othe::t Cspecify): (Design) I CB: ______ I ___________________ 0 cc: 228 CD: 228 Below Huclea::t Heating III I Bank Positions (Steps) RCS Ternpe:z:atu:z:e C0 f): Power Level (7. F.P.): Test Conditions ' - -SDA: I
---- - - - -SDB:
Z.."Z..8 - - - -2.-'t.8
- - - -CA:- - -z.:z..8
---- Other CSpecify):
(Actual) I CB: 0 cc: Z..Z..8 CD: 2.'2.3 Below Huclea::t Heating 1 Date/Time Test Pe:x:£0:z:med: 1 1!a/Bt / o4-Jo
, _ _...z.:___________________ - - - - - - - - - - - - - - - - - - - - -
1 Meas Pa::tamete::t IV I CDesc:z:iption) c4So )i; Iso Temp Coe:fi - B Bank In 1 Test Results I Measu:z:ed Value I ___________ (~ )5 = ..:.*i. s~ i'~m/o'F-ca =133/ >rt"'- I Design Value I (Actual Cond) cciqso = - '- . 3fo ~ ( C B = l 33 [
- 3 . 0 f'cf1{.c~
)5 ) ff""-
Design Value (~ )~ =- 6.55 : 3.0 pcm/°F (Design Cond) CC13 = 1316 ppr:i.) Re:fe::tence VEP-FR.D-NFE 183 V FSAR/Tech Spec Acceptance Cl:ite:z:ia Re:fe:z:ence TS 3.1. VEP-FRD-NFE 183 1 I Design Tole:z:ance is met : .,/YES _HO VJ: I Acceptance C:z:ite:z:ia is met ~YES _HO Comments 1 * '---------------------------------------- I Uncertainty on aT a 0.5 pcm/OF (
Reference:
memorandum from I
- MOD C. T. Snow to E. J. Lozito dated June 27, 1980)
I Completed By Evaluated By: R.ecommended :fo:z: App?:oval By NFC Enginee:r: A. 7
JUL 3 1931 SURRY POWER STATION UNIT 1 .CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test Desc:r:iption: HZP Bo:r:on Wo:r:th Coefficient Refe:r:ence P:roc Ho /Section: PT28.11/APP. E Sequence Step Ho: ff/A II I* Bank Positions (Steps) RCS Tempe:r:atu:r:e (°F): 547 Test l~~~~~~~~~~~~~~~~~- Powe:r: Level (?. F.P.): 0 Conditionsl SDA: 228 SDB: 228 CA: 228 Othez: (specify):
'(Design) I CB=noving cc: 228 CD: 228 Below Huclea:r: Heating III Bank Positions (Steps) RCS Tempe:r:atu:r:e C°F): S-46,/Dp-'
Test Powe:r: Level (7. F.P.): 0% Conditions SDA: 2.'Z. 8 SDB: 2:2..s CA: Z.z..8 Othe:r: (Specify): (Actual) CB: no.ti~ cc: z. Z.8 CD: 'Z. Z..B Date/Time Test Pe:r:fo:rmed:
~/8/BI I 03s-o Measu:r:ed Pa:r:amete:r:
IV CDesc:r:iption) ()( C.e,, Bo::r:on Wo::r:th Coe:f:ficient Measu::r:ed Value
, Design Value
{Actual Conditions) Design Value (Design Conditions) Re:fe:r:ence VEP-FRD-HFE 183 FSAR/Tech Spec °'C5 x Ce, S 15,115 pcm V Acceptance Cz:ite::r:ia Re:fe:r:ence FSAR Section 14.2.S Design Tole::r:ance is met VI Acceptance C:r:ite:ria is met
- Comments Completed By: Evaluated By: ~xf.11'd-Recommended fo:r:
App:r:oval ~y: c~ :J'. J~ MFO Enginee:r: A. 8
JUL 3 i3B1 SURRY POWER STATIOij UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATIOH SHEET I Test
Description:
M/D Flux Map *~HZP, B-Bank In Reference Proc No / Section: PT28. 2, OP-57 Sequence Step No: \ 3
- -*~
II Bank Posi~ions (Steps) I RCS Temperature C°F):TREF !1 Test ----------------------------------' Power Level (7. F.P.):-o Conditions SDA: 22S SDB: 228 CA: 228 I Other {specify) (Design) CB 0 cc : 228 CD: 228 I Must have*~ 40 thimbles III
---------------------------1---------------------
Bank Positions (Steps) I RCS Temperature ( ° F): .,47-Test -----------------------I SDA: l'Z 6 SDB: -z.zs CA: 7.z.B P 01Je r Leve 1 C?. F
- P * ) : -o Conditions I Other CSpeci:::y):
(Actual) CB :u/z.~ cc : Z.-Z.8 CD: "l..Ze. I 10 pl/,,..,,6L.£'"$ Date/Time Test: ;r'~BJ I Performed: 07:J.J I MAX. REL I HUC EHTHALITOTAL HEAT QUADRANT IV Meas Parameter! ASSY PWR I RISE HOT I FLUX HOT POWER TILT (Description) I ~ DIFF I CHAH FACT ICHAH FACT RATIO I CM-P)/P I F-dHCN) I F-2CT) QPTR
---------'I +sAj;,~di:>"11'1..--------'------ I Test Measured Value 1.,6-4,;FoJt fl,;0.3'r I*] '1~ I z. 11~ 1.oz 7rs,
- Rirsults
---------~--=-,,-----=-'
Design Value .:10: for Pi ~
- 9
.:15% for pi< .9 I
I HA I'-------------- 1*
=cnesign Conds) HA !':: 1. 02 I I (Pi
- Auy. Pvr.)
WCAP-7905 I I
------ WCAP-7905 Re:Eerence REV. 1 I NOHE I HONE I REV. 1
-------'1 '------'------
I I V FSAR/Tech Spec NOHE I NA I HA I HA Acceptance -----------------1 I I______ C:z:iteria I I I Re:Eerence HONE I T.S. 3.12 I T.S. 3.121 T.S. 3.12 I I I ~ - - - - - - - - - - - - - - - - - - - - ______ I I I _______ Design Tolerance is met _ YES /xo Acceptance Criteria is met vYES _ _ HO VI
- .comments ,;,:: 0"S:,V\ -b lca.,,-~c..cz. t'\O+ ~ I bv::*f ~ ('".;a.su.1+ ,~ o...cf,,j,k_. ~ ~-t~-:.
. 1. 5,~*--vYl ~'u1.......r St~IC'Y'- ~.o:*,iey,.. ~c:-r-t- No. S\-8\-t,s.
Completed Evaluated Recommended Approval A. 9
JUL SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Test
Description:
Cntl Bank D Worth Measurement-Rod Swap Reference Proc Ho /Section: PT28.~1/APP. F Sequence Step No= \4 Bank Positions (Steps) RCS Temperature ( 0 : ) : 547 Test Power Level C?. F.P.): 0 Conditions! SDA: 228 SDB: 228 CA: 228 Other (specify): (Design) I CB=Moving cc: 228 CD:Moving Below Nuclear Heating III Bank Positions (Steps) RCS Terape::c:atu:i:e ( 0 f):£"+7."/ Test Power Level(% F.P.):0 Conditions SDA: 2.'2. g SDB: 2.2 g CA: 2.2.8 Other CSpeci:::y): (Actual) e. CB =N\oviY\~ cc: 2.8 cn: Mw*~ Below Nuclear Heating Date/Time Test Performed: 7 /?/81 - /02S-Meas Parameter (Description) I:;5 ;Int Wo:z::th o:f Cntl Bank D-P.od Swap IV (Adj. Meas. Crit. Re:: Bank Test I Measured Value I~ . =. / 2. 31- fC-M Position*= /7S-.steps) Results I I Design Value (Adj. Meas. Crit. Re:: Bank IC Actual Cond) I:,S =/2.2~ +/- /S'rpcrnPosition = J 7.S- steps) I I I Design Value I~= 1221 +/- 183 pcm (Critical Re! Bank D ICDesign Cond) . P6sition = 185 steps) I I I Re:ference VEP-FRD-NFE-183, VEP-FRD-36A, HFO-TI-2.2A I I I:f Design Tolerance is exceeded, SKSOC shall evaluate impact o:f test result on V FSAR/Tech Spec safety analysis. SHSOC may specify that Acceptance additional testing be performed. C:z::iteria Reference VEP-FRD-36A Design* Tolerance is met ~YES _NO VI Acceptance Crite~ia is met ...X.,YES _HO Comments Evaluated By: 7K& Recommended :for Approval By c.:J~ NFO Engineer: A.10
JUL 3 1981 SURRY POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test
Description:
Cntl Bank C Worth Measurement-Rod Swap Re:ference Proc No /Section: PT28.11/APP. F Sequence Step Ho: l6 II Bank Positions (Steps) RCS Temperature C°F): 547 Test Power Level (2 F.P.): 0 Conditions I SDA~ 228 SDB: 228 CA: 228 Other (specify): (Design) I CB=Moving cc:Moving en: 228 Below Huclear Heating III Bank Positions (Steps) RCS Temperatu:z:e C°F): S~7.S" Test Powe:x: Level C~ F.P.):O Conditions SDA: 2.2.8 SDB: 2.2.8 CA: 22.8 Othe:z: (Speci:fy): (Actual) CB :/J\ovi~~ CC: Movi~~ CD: Z:28 Below Nuclear Heating Date/Time Test Performed: 7/a/s, /(0~ Meas Pa:z:ameter I CDesc:z:iption) I I~ ; Int Wo:z:th o:f Cntl Bank C-Rod Swap I IV I (Adj. Meas. Crit. Ref Bank Test Measured Value I I~ = g /5" pe,'tf\ Position= /10 steps) Results I Design Value I (Adj. Meas. Crit. Ref Bank ,;:- (Actual Cond) I I~ = 833:t lcS-pe.'ft\ Position = //0 steps)
~- ~f . I I
Design Value I I~= c.. 827: 124 pcm (Critical Re:f Bank
- (Design Cond) I Position= 130 steps)
I I Re:fe:x:ence I VEP-FRD-HFE-183, VEP-FRD-36A, HFO-TI-2.2A I I If Design Tolerance is exceeded, SHSOC I shall evaluate impact o: test result on V FSAR/Tech Spec I safety analysis. SHSOC may specify that Acceptance I additional testing he performed. C:z:ite:x:ia I Re:fe1:ence I VEP-FRD-36A I Design Tolerance is met ~YES _HO VI: Acceptance Criteria is met ~YES __ NO Comments
.Evaluated By:
Recommended fox: App::i::oval. By c.~2~ XFO Enginee::c A.11
JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test Desc:z:iption: Cntl. Bank A Wo:z:th Measu:z:ernent-Rod Swap Re£e:z:ence Pz:oc Ho /Section:. PT28.11/APP. F Sequence *step }{o: I (p II Bank Positions (Steps) RCS Tempe:z:atu:z:e C0 f): 547 Test Powe:z: Level C?. F.P.): 0 Conditions I SDA: 228 SDB: 228 CA=Moving Othe:i: Cspeci:fy): (Design) I CB=Moving cc: 228 en: 228 BeJ.ow Nuclea:z: Heating III Bank Positions (Steps) RCS Tempe:z: atu:z:e C°F): Sl/--7. 3 Test !I ________________ ,___ Powe:z: Level(~ F.P.):O Conditions! SDA:22~ SDB:22.8 CA:Mbvi°"-' othe:z: CSpeci:fy): CActuaJ.) CB:Mov1\I\~ cc: 2.2.8 CD: 228 Be1ow Nuclea:z: Heating Date/Time Test Pe:z::fo:z:med= 7/3/91 //37 Meas Pa::camete:r CDesc:z:iption) I~ ;Int Wo:z:th o:f* CntJ. Bank A-Rod Swap IV (Adj. Meas. C:z:it. Ref Bank Test Measu:z::ed Valu'e I~ = S-S"/ pc'('()
- Position = 83 steps)
-Results Design Value RS (Adj. Meas. C:z:it. Ref Bank (Actual Cond) IA =S-1-,"!:. /OO~fl)Position = g:; steps) Design Value I~S = 555 ~ 100 pcm CC:ritical Ref Bank (Design Cond) Position= 100 steps) Re:fe:rence VEP-FRD-HFE-183, VEP-FRD-36A, HFO-TI-2.2A I:f Design Tole:i:ance is exceeded, SNSOC shall evaluate impact of test ~esult on V FSAR/Tech Spec safety knalysis. SHSOC ~ay specify that Acceptance! additional testing be pe:z::o:i:med. C:rite:i:ia ' - -R.e:fe:z:ence
- - - - - - - - -VEP-FRD-36A 1
1 Design Tole:z:ance--------------------------- is met ~YES __NO VI I Acceptance C:z:ite:i:ia is met ~YES __NO Comments 1 '------------------------------------------- I Completed B Evaluated By: .7K..~ Recommended £0:i: App:coval. By c.:J.~ NFO Enginee:z:: A. 12
JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP'PHYSICS TEST RESULTS AHD EVALUATIOH SHEET I Test Desc:z:iption=Shutdown Bank B Wo:z:th Measurement-Rod Swap Re:fe:z:ence P:z:oc Ho /Section: PT28. 11/ APP. F Sequence *step Ho: \ ~ II Bank Positions (Steps) RCS Tempe:z:atu:z:e (°F): 547 Test Power Level (7. r.P.): 0 Conditions! SDA: 228 SDB:Moving CA: 228 Othe:z: (specify):. (Design) I CB=Moving cc: 228 en: 22s* Below Nuclea:z: Heating II:I I Bank Positions (Steps) RCS Tempe?:atu:z:e C° F): S".l/-7.1-Powe:z: Level (7. F.P.): 0 Test '-----~---..-~------- Othe:z: (Specify): Conditions I SDA=2.2.~ SDBdVlovlY\"CA= 2.2.8 (Actual) i CB=.Mo\/1"j cc:2.28 cn:228 Below Huclea:z: Heating 1 Date/Time Test Pe:z::fo:z:med: I 7/a/ 8/ /2 Lf-J 1 Meas Pa:z:amete:z: I CDesc?:iption) I~ ;Int Wo::rth o:f Shutdo.wn Bank B-Rod Swap IV I
------------------------- (Adj. Meas. C:z:it. Ref Bank Test I Heasu:z:ed Val'l.te I~ =. /0/3 f>C..Yf>
- Position = /38 steps)
Results '- 1 ---- Design - - - - - - - - - - - - - - - -(Adj. Value ---- ---- Meas. - - -Ref exit. - - -Bank IC.Actual Cond) :I~ =/()()St/S-lpe'ff\Position = /38 ste:i:;s> (D/0 *IS2 Design Value ~ :t .J-6< pcm CC::ritical Re:f Bank (Design Cond) ';'7 /<.f.?.. '1Kie. Position = J.,&6"' steps) 7/9/a, 7/~/81 ,s~ 11</l il1/i1 Re:fe:z:ence VEP-FRD-HFE-183, VEP-FRD-36A, HFO-TI-2.2A I£ Design Tole:z:ance is exceeded, SNSOC shall evaluate impact of test ~esult on V FSAR/Tech Spec safety analysis. SNSOC may specify that Acceptance additional testing be pe:z:fo:z:med. C:z:ite:z:ia Re£e:z:ence VEP-FRD-36A Design Tole:z:ance is. met ~YES __ HO VI Acceptance Ci:ite:z:ia is met -2(.YES __NO Comments Completed Evaluated By: Recommended £0:z:
. Appi:oval. B,Y c.:J.~
NFC Enginee:r
.ll. 11
JUL 3 1987 SURRY POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Test Descz:iption:Shutdown Bank A Woz::th Measuz::ement-Rod Swap Re:fez:ence Pz:oc H.o /Section: PT28. 11 /APP. F Sequence Step Ho:
- l B II Bank Positions (Steps) RCS Tempez:atuz:e C°F): 547 Test Power Level (7. F.P.): 0
- Conditions SDA:Moving SDB: 228 CA: 228 Othez: (specify):
(Design) CB:Moving cc: 228 CD: 2 28 Below Hucleaz: Heating III Bank Position~ (Steps) RCS Tempez::atuz:e ( ° F): .S-'f-7.S-Test Powe:r Level C?. F.P.):0 Conditions SDA: MoiJIYi9 SDB: c.2.8 CA: 2.~ Othez: (Specify): (Actual) CB: /AO'li~~ CC: '2.28 CD: 2.2.8 Below Nucleaz: Heating Date/Time Test Pez::oz:med: 7/8/~1 le.OS-Meas Parametez: (Descz:iption> PS ;Int Wo:z:th o:f Shutdown Bank A-Rod Swap IsA IV (Adj. Meas. C:z:it. Ref Bank Test l1easu:red Value I~ =//37fC!.rf\. Position = /5'1 steps) R~sults Design Value (Adj. Meas. Crit. Re:f Bank (Actual Cond) I~ = /078 :t 1,; p¢W\ Position = / S7 steps) Design Val.ue
,,2.
~pcm tCz::itical. Ref Bank (Design Cond) iK.f.
7/'l/91 ,~s-Position= )...S-S"'"steps) 71<./c. 1/9/81 Re:Ee:rence VEP-FRD-HFE-183p VEP-FRD-36A, NFO-TI-2.2A If Design Tolerance is exceeded, SHSOC shall evaluate impact of test*z::esult on V FSAR/Tech Spec safety analysis. SHSOC may specify that Acceptance additional testing be peI::formed. C:z:ite:z:ia Re:fe:rence VEP-FRD-36A Design Tolexance is met ..2S:..YES _NO VI I Acceptance CI:iteI:ia is met : ..XYES _NO Comments ' - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 1 I . Ev~luated By: Recommended £oI:
...AppI:oval By : C.,1.~
NFC EngineeI: A.14
JUL 3 1981 SURRY POWER STATION UNIT 1 *CYCLE 6 STARTUP PH~SICS TEST RESULTS AHD EVALUATION SHEET I Test Desc:z:iption: Total Rod Wo:z:th-Rod Swap Re:fe:z:ence P:z:oc Ko /Section: PT28.11/AP~. F Sequence Step Ko: lq
- II Bank Positions (Steps) RCS Tempe:z:atuie C°F): 547 Test Powe:z: Level C~ F.P.): 0 ConditionslSDA:Moving SDB:Moving CA:Movingl Othe:z: (specify):
(Design) I CB=Moving CC=Moving CD=Movingl Below Kuclea:z: Heating III Bank Positions (Steps) ( RCS Tempe:z:atu:z:e C°F):5'f7.J Test Conditions
--------------- ......-'I SDA :/y\o..,in, SDB: /v'to'liV\~ CA: ,V\ovi.,.,
Powe:c Level C?. F.P.): 0 Othe:c (Specify): (Actual) CB: Mo"i""' CC: M O'liv"I-' CD: Mb\JiV\j I Below Huclea% Heating - - - - - - __________________ i Date/Time Test Pe:c~o:z:med: I 7/7/a1 e.130 7!9/~I
/
1 lc.~J I Heasu:z:ed Pa:camete:c I rTo~\;rnteg:cal Worth oz All Rod Banks-CDesc~iption) I Rod Swap J:V Test Measu:ced.Value '
- :!.roib.1 = <o. I CJ O f~m Results ------------
Design Value I
-(Actual Conditions) : ITc,;c..J= 0.0 91- t ~ DCf pe,vn Design Value I (Design Conditions) I I"G'h>J= 6098 ! 610 pcm R.e:fe:cence ' VEP-FRD~HFE-183, VEP-FRD-36A, NFO-TI-2.2.A
------------'--------------------- ! I:f Design ~ole:cance is exceeded, SHSOC I shall evall.fate impact o:f test :cesult FSJl.lVTech Spec I on sa:fety analysis. SNSOC may specify V I that additional testing be pe%fo:cmed.
Acceptance C:cite:cia
------------'----------------------1 Re:fe%ence I VEP-FRD-36A I --------------'------,-----------------
I Design Tolerance is met .2S...YES -'-HO VJ: *, Acceptance C:z:ite%ia is met -A.YES _NO Comments I I I I Completed . Evaluated By: Recommended :fo% App:coval By c.f.~_ NFO Enrr~;. A.15
JUL - 3 1931 SUP.RY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Test Description M/D Flux Map - At Power, HI Calib. Re:ference Proc Ho/ Section: PT28.2, OP-57 Sequence Step Ho: 45 - .< II Bank Positions (Steps) I RCS Temperature ( 0 f):TR~F !1 Test I Power Level C?. F.P.):-40 Conditions I SDA: 228 SDB: 228 CA: 228 I Other Cspeci::fy) (Design) I CB 228 cc : 228 en: :s: I. Must have~ 40 thimbles I I III I Bank Positions (Steps) I RCS Temper a ture C ° F) : 5"S"o cp Test I I Power Level (7. F.P.): 3Zio Conditions I SDA: 2'2.8 SDB: .z..z..B CA: iz.s I Other CSpeci:fy): (Actual) I CB : 2.2.8 cc : Z..z.8 en: l~O I I I I Date/Time Test: I 4-i Th -im b Jes I Per:Eormed: I I t-/8/8! / 1ss-3 I I MAX. REL I HUC EHTHALITOTAL HEATI QUADRANT IV I Meas Parameter! ASSY PWR I RISE HOT I FLUX HOT !POWER TILT I (Description) I 7. DIFF I CHAN FACT ICHAH FACT I RATIO I I CH-P)/P I F-dHCH) I F-2CT) I QPTR I I ---------------'
. 1-,% ~ ~z.= o.,t1 '------'I '------
I
.Jl'est I Measured Value I .,, r I ;,423 I z. / 84-. I /. ()/33 Results I ------------ i-'*~ ;,,.- ~-I.: 0.6~ T I I _ _ _ _ __
I~ Design Value I :1io::: for l'i .2.
- 9 I I I I (Design Conds) I :1t5% to-r Fi< *9 I HA NA I S 1. 02 I - I (P *
- Any. Pv?-,) I I
-------------- 1WC AP - 7905 I IWCAP-7905 Re:ference I REV . 1 I HONE HONE I REV. 1 ---------------------! I I
I I ______ I FSAR/Tech Spec I I NOHE II _____ V ~s1.s5C1+.2C1-P>> F~C:n~4.J6 z iccz> HA _______________ I I __ Acceptance C:2:iteria I I I Re:ference I HONE I T. S. 3. 12 T. S
- 3
- 12 I T
- S. 3. 12 I I I
----------------------' I '-------
Design Tolerance is met VYES _xo Acceptance Criteria is met . / YES _:_xo VJ: Comments
- Above Insertion Limits Completed B Evaluated By:
Recommended :fol: Approval. F:Y MFO Enginee.i: A. 16
JUL . 3 1981 SURRY POWER STATION UNIT 1 *CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test
Description:
M/D Flux Map - At Power. NI Calib.
*Re:ference Proc Ho/ Section: PT28.2, OP-57
- Sequence Step Ho= 4G, II Bank Positions (Steps) RCS Temperature C°F):TREF :1 Test Power Level CX F.P.l=-50 Conditions I SDA: 228 SDB: 228 CA: 228 Other Cspeci::i:y)
.(Design) I CB 228 CC : 228 CD: x Must have~ 40 thimbles III I Bank Positions (Steps)
RCS Tempe:z:ature( °F): TR.EF! I Test ! _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ __ Powez: Level C7. F. P. ) : ..,..47°7o Conditions I SDA: 1.:2.& SDB: _1.1~ CA: '1.2.'?° Other CS~eci:fy): (Actual) I CB : 2.2% cc : ").:i.8 cn:nCJ/,~o LI o Th ,*.....bks Da.te/Time Test:* Pei:£01:med: 7/'i/%1 tlAX. REL HUC EHTHALITOT;tL HEAT QUADRANT
- IV Heas Pai:ametei:1 ASSY PWR RISE HOT I FLUX HOT POWER TILT (Description) I X DIFF CHAN FACT ICHAH FACT RATIO I Ctl-P)/P F-dHCH) I F-Q(T) QPTR
________ I !
. I+s:,"lo .f.r P~,q0.9(. I Test Measured Value Il+s:i-, n :o.uu
- i / or-~_rLI'~ ,,
I. YS'I f.9'3>0 1.0lll/ Results
~ Design Value 1::io:forPi.2.. 9 CDesign Conds) I ::t 5::t fol' Pi<
- 9 I CPi. #Jay. Pvr.>
NA . HA s 1. 02
-------- 1'WC AP - 7905 WCAP-7905 "'
Reference l REv.*1 NOHE NONE REV. 1
- - - - - - _________ I_ _ _ __
I V FSAR/Tech Specl NOHE ~Hst.SS(l+.2(1-P)) F~Cz.>i;1 8 X J;(Z.) HA Acceptance--------'------ C~iteria I I I Refe~ence I NONE T.S. 3. 12 T.S. 3.12 T.S. 3. 12 I *1
--------'1 '------ ------- --------------
I Design Tolerance is met _LYES _HO I Acceptance C;ite~ia .is met /YES __ NO VI: Comme~ts 'I -*- - - - - -Insertion Above -------- ------------------------------- Limits I I
------'---~--:---~-----==-------------------:--------:-----
Completed Eva1uate d By* ~Jl. ,C~~
- Recommended for --;-) / / /
Appx:oval By : .-..k_;(..t._v._/_...h,
!7 /
~--~~=---'""--
... NFO Engiieex:
A.17
JUL 3 1sa1 SURRY POWER STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATIOH SHEET
'I Test Descr:iption*: M/D F1uK Map - At Pouer:. KI Calib.
Re£er:ence Pr:oc Ho/ Section: PT28.2. OP-57 Sequence Step Ho= 47 - .. II Bank Positions (Steps) RCS Tempe~atu%e C°F)=T~EF t1 Test Poue:z: Level C?. r.P.):-60 Conditions I SDA: 228 SDB: 228 CA: 228 Othe:z: (speci::::y) (Design) I CB : 22a cc : 22a en: % Must have~ 40 thiDbles III I Bank Positions (Steps) RCS Tern Per: a tu:z:e ( ° F) : ...., -56Z '"'!= Test Conditionsl 1-------------------- SDA: zzS SDB: z.z.S CA: Z.'Z.S Pouer: L~vel C~ F.P.):57%. Othe:z: CSpeci:y): (Actual) I CB _____ r________________ :z~g cc : *u .. s CD: , 1-s I Date/Time Test: I Per::for:med: 1 /1a/ 8/ j Z 00.f:>
+I T/i,*ml,le~
I I I MAX. REL I HUC EHTHALITOTAL H~ATI 2UADRAHT
'IV I Meas Par:ameter:l ASSY PWR I RISE HOT I FLUX HOT !POWER TILT CDescr:iption) I 7. DIFF I CHAH FACT ICHAH FACT I RATIO I CM-P)/P I F-dHCH) .I F-2CT) I 2PTR
-'\ ________ ! I I I _ _ _ _ __
- 1-1-.+t fw. ':-r= o.1s-l I . I Test Measur:ed Value:-s.,i{....fy.fMf: /,4S"/ : /. 'f8(,. : /.OO?~
Results
* *Design Value 1::1o:forPi 2 "9 I I I
*cnesign Conds)l~lS%forPi<. 9 I HA I HA I s*1.02
. (pi
- Auy. ~ . ) I I I
---~-- ~ I I WCAP-7905 I I IWCAP-7905 i P..e:fe:z:ence REV.1 I NOHE l HONE l REV.1 . -
- I I
-------------------- _______ ! l I _______
I I I V FSAR/Tech Spec HONE I ;M:.l!sl.SS(l+.2(1-P)) I F~(z>s\ 18 x xcz> I NA Acceptance - - - - - - - - -
- I I I _ _ _ _ __
C:cite:cia I I I R.e:fe:rence HONE I T.S. 3.12 I T.S. 3.121 T.S. 3.12 I I I
------* I I I '-------
-----I- Design To*le:rance is met - - ~YES HO I Acceptance Cr:ite:z::ia is met VYES =HO VI Comments I'--------------------------------------------------------------
~ Above Inser:tion Limits I
I Completed Byr:
- Evaluated By: J. ,.I. r,Zl(,_
>< I /- , *.* ~ .
Recommended :£01: App:z:oval By : C.,1~ NFO Engineer: A.18
JUL 3 1'81 I SQRRY POWER STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test Desc::ciption : M/D Flux Map - At Powe:z::, NI Calib. P.e:fe:z::ence P:z::oc }{o / Section: PT28. 2, OP-57 Sequence Step Ho: 4B II Bank Positions (Steps) RCS Tempe:z::atu:z::e C°F)=T~Ef :1 Test Powe:z:: Level CX F.P.)=-70 Conditions I SDA: 228 SDB: 228 CA: 228 .othe:z:: Cspeci:fy) (Design) I CB III I 228 CC : 228 Bank Positions (Steps) CD: x Must have~ 40 thimbles RCS Tempe:z::atu:z::e{ °F): ,,.,5(;::, GF Power Level C:'. F.P.): ~5'%
- Test Conditions 'I - - - - -ZZ.8 SDA: ---- - - -Z.Z.8 SDB: - - -CA: --- ---
2U3 Othe:z:: CSpeci:f.y) : (Actual) I CB : 2.2-8 cc= ~~a en= ~oo
' Date/Time Test:
I Pe::c:fo::cmed: , 1 I. /
?!(418'/ . OeJZ.4-1 I
I MAi. REL I HUC EHIHAL TOTAL HEATI QUADRANT IV l Meas Pa:z::amete::cl ASSY PWR I RISE HOT FLUX HOT !POWER TILT (Desc::ciption) I X DIFF l CHAN FACT CHAH FACT I RATIO
-------------' I CM-P)/P 1-~ .f.... ~-z 1.00 I
; ____________ ,_______
I F-dHCH) F-Q(T) I I QPTP. Test Measu::ced Value: .. '1,1.'f.~P.t.,o.,'fl /.435° /.1/8 : /.0//r Resu1ts ------------ Design Value. ( :tlO::: for pi 2 *9
------ ------ I (Design Conds) :!lS:t for Pi<
- 9 HA NA I S 1 ~ 02 (pi
- Auy. Pvr.) I WCAP-7905 IWCAP-7905 Re:fe::cence REV. 1 HOME I HONE I REV. 1
_N * - - 'I T 2.18 I V .FSAR/Tech Spec HONE *i11.s.1.55(1+.2(1-PD FQ(Z):.-l'- x K(Z) HA Acceptance I _________ -------- C::cite:cia . '-------'------ I I Re:fe1:ence HONE T.S. 3.12 IT.S. 3.12 I T.S. 3. 12 I I Design Tole:cance is met ./YES _NO Acceptance C:z::ite:cia is met ;_LYES __HO v:r Comments = Above Inse::ction Limits Completed B Eva1uated By:
' . Recommended :fo?:
App:coval By c.:J~ NFO Engineer A.19
JUL 3 7987 SURRY POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATIOH SHEET I Test Desc:ciption : M/D Flux Map - At Powe:c, HI Calib. Refe:cence P:coc No / Section: P-TZ8. 2, OP-57 Sequence* Step Ho: 4 C\ -
- II Bank Positions (Steps) RCS Tempe:catu:ce C°F):TREF +/-1 Test Powe:z:: Level(~ F.P.)=-90 Conditions SDA: 228 SDB :* 228 CA: 228 Othe:r (specify)
(Design) CB 228 cc : 228 en: :s: Must have~ 40 thimbies III Bank Positions (Steps) RCS Tempe:ratu:ce C°F) :T~ t I Test Powe:r Level (~ F. P.) =-is-% Conditions SDA: 2.2..% SDB:22~ CA: 2.2..8- Othe:c CSpeci:fy): (Actual) CB : 2.2.S- cc : 2.2.~ CD: *u:J'-f 4I Th;,.,..bl e..s Date/Time Test:/.;/ Pe:z:::fo:cmed: 7 14 'if MAX. REL NUC EHTHALITOTAL HEATI QUADRANT IV Meas Pa:camete:c! ASSY PWR RISE HOT I FLUX HOT !POWER TILT CDesc:ciption) I 7. DIFF CHAH FACT !CHAN FACT I RATIO I (?1-P)/P F-dHOO I F-QCT) I 2PTR
-----------'1c..s%~rP1t-~1,01 -------'I '------
J Test I1easu:ced Value I,~"",. P. ~0 ,,~ ___________ l,.,1r,oto<" ~-I "'O l.* -fZ.I 1 I f l.~'2...% I l,Ol7-I _ _ _ _ __ Results
- Design Value I ~io: £or Pi 2
- 9 I* I (Design Conds) I :is: for Pi<
- 9 HA I NA I S 1. 02
- - - - - - - - ' \ ' . P i
- bay. ?wr.) ------' '------
JWCAP-7905 I IWCAP-7905 Re:fe:z::ence I REV. 1 NOHE I HONE I REV. 1
--------'------ 1 -------'I '------
I V FSAR/Tech Spec I HONE ~ 8 ~1.ssc1+.:ZC1-,>> I r~CZ>s-\;1- 8 x KCZ) I HA A c c e p t a n c e - - - - - - - - - ' - - - - - - - _________ I I ________ C:cite:cia I I I I I Re:£e:cence I NOHE T. S. 3. 12 I T. S. 3. 121 T. S. 3. 12 ______ II II II II _ _ _ _ __ I I Design Tole~ance is met : /YES _MO II_________________________________________ Acceptance C:z::ite:cia is met . / YES _ _ HO VI __ Comments I :s: Above Inse:ction Limits I I
'----,,--,.---,,....-----------------~---------
Completed Evaluated By: Recommended £0:c * ./ / ...-;--7 / App:toval ~Y : ,JU;/~/~/ NFO Eng*i.nee.r: A.20
JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Test Desc::ciption: M/D Flux Map - HFP, ARO, Eq: Xe. Map Re:Eerence P::coc No/ Section: PT28.2, OP-57 Sequence Step No: 5D - - . II Bank Positions (Steps) RCS Tempe::cature C°F):TREf =1 Test PotJer Level C?. :r.P.): 100 Conditions SDA: 228 SDB: 228 CA: 228. Other (specify): Eq. Xe. (Design) CB 228 CC: 228 CD: x Must have~ 40 thimbles II! Bank Positions (Steps) RCS Temperature C° F): T,..11¥' +/- l Test Power Level C?. F .P.): Joo t.' Conditions SDA: ~,;). 8 SDB: .l..). 0 CA: ~i,l. 9 Other (Speci~y): ' (Actual) CB : ;)._J-8 CC :~.). 8 CD: ~;J..8 '-/~ Th;ft'ble-s Date/Time Test: Performed: ?'/
~1(8! 01'{1 I MAX. REI. I NUC EHTHALIT~TAL HEAT 2UADRANT IV Meas Parameter! ASSY PWR I RISE HOT I FLUX HOT POWER TILT (Description) I 7. DIFF I CHAN FACT !CHAN FACT RATIO I CM-P)/P I F-dHCN) I F-2CT) 2PTR
--------'1-C{. gZ f'oc- f:D-111'------------
-?est I Measured Value I :r--~ I J~ '-/ I 3 I. 'ii O f .O/ o ~
Resul.ts _ _ _ _ _ _ _-_t*S.71.-t... :, "'0.~------ ------ ------.. .
-- Design Value I ,no: for Pi 2
- 9 (Design Conds) I :is: £or Pi<
- 9 NA HA S 1. 02 I (pi* Asay. Pvr.)
-------- 1WC AP - 7905 WCA.P-7905 Reference I REV. 1 HONE NOHE REV. 1 V
Acceptance FSAR/Tech Spec! ' I NONE r'.6llsl.55(1+.2Cl-P)) r~cz,s?/ 8 s 1'(i) NA Criteria I Reference I HONE T.S. 3.12 T.S. 3.12 T.S. 3.12 I I Design Tolerance is met Acceptance Criteria is met v:r::"
- Comments
- Above Insertion Limits Compl~ted BY, Evaluated By:
Recommended :for Approval By : NFO Engineer A,21
JUt s rsa 1 5u..r~
~ POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I. Test
Description:
RCS Flow Measurement Refe:rence P:roc Ho /Section: ST-52 / eTA-4,ooo.:z. Sequence Step Ho: 5/ II Bank Positions (Steps) RCS Tempe:ratuz:e C°F)=T~ !1 Test Power Level(~ F.P.):95 +5/-0 Conditions I SDA: 228 SDB: 223 CA: 2 2 8 Otli.e:z: (specify): (Design) CB: 228 cc: 228 en: AR III Bank Positions (Steps) RCS Ternperatu:re C° F): 574°F /SIDC/ cp Test PotJe:z: Level C?. F. P.): /Oo%, Conditions SDA: Z,.?..S SDB: 2.2.s CA: '2.2.8 Othe:r (Specify): CA.ctual) CB: cc: Z.2.8 en: A Z.l.. S Date/Time Test Pez:formed: B-G,-8 I 0946- /34-5 Meas Parametez: I IV CDesc:z::iption) I FTam.~ , Total RCS Flou Rate I I Test Results Measu:z::ed Value I I r Tc:1rAL.. = ::z. q \ 1 o
> B '\.~ ""'
Design Value I (Actual Cond) I Hot Appl.icabl.e I Design Value I (Design Cond) I Hot Applicable .,. I Refez:ence I Hot Applicable 1 I FSAR/Tech Spec I FTbTA.L / 1. 02 Cmeas unce::cty) ~ 265,500 gpm V I Acceptance I !SAR Section 4.1.3; Letter from J. H. Ferguson(Vepco) to Criteria Re:fe:z::ence I H. R. Denton(NRC) dated April 28, 1981 (Serial No. 232);
*I Letter from C. M. Stallings(Vepco) to E.G. Case(NRC) dated November 16, 1977 (Serial Na. 516)
1I---------- 1-------------------------
I Design Tolerance is met ;,YES _HO VI: I Acceptance Criteria is met _ _ YES _HO Comme*nts '----------------------------------
'II
______ ,____µl,,i,t___ct_,~------------------------ Completed By: Evaluated By: ti: zztt:.v' f'est Engine~ A.22
~~-------------------~~-,
~ NOTICE - .
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