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{{#Wiki_filter:Y1003J01A03 Class I August 1980 SUPPLEMENTAL RELOAD LICENSING SUBMITTAL FOR BROWNS FERRY NUCLEAR POWER       STATION UNIT 3 RELOAD NO. 3 Prepared:
{{#Wiki_filter:Y1003J01A03 Class I August 1980 SUPPLEMENTAL RELOAD LICENSING SUBMITTAL FOR BROWNS FERRY NUCLEAR POWER STATION UNIT 3 RELOAD NO.
3 Prepared:
C. L. Hilf Approved:
C. L. Hilf Approved:
R. E. Engel, Manager Reload Fuel Licensing NUCLEAR POWER SYSTEMS DIVISION ~ GENERAL ELECTRIC COMPANY SAN JOSE, CALIFORNIA95125 GENERAL                 ELECTRIC DOQOZ, c) QC3$
R.
E. Engel, Manager Reload Fuel Licensing NUCLEAR POWER SYSTEMS DIVISION~ GENERAL ELECTRIC COMPANY SAN JOSE, CALIFORNIA95125 GENERAL ELECTRIC DOQOZ, c) QC3$


Y1003JOlA03 IMPORTANT NOTICE REGARDING CONTENTS OF THIS REPORT PLEASE READ CAREFULLY This report was prepared by General Electric solely for The Tennessee Valley Authority (TVA) for TVA's use with the 'U.S. Nuclear Regulatory Commission (USNRC) for amending TVA's operating license of the Browns Ferry Nuclear Unit 3. The information contained in this report is believed by General Electric to be an accurate and true representation of the facts known, obtained or provided to General Electric at the time this report was prepared.
Y1003JOlA03 IMPORTANT NOTICE REGARDING CONTENTS OF THIS REPORT PLEASE READ CAREFULLY This report was prepared by General Electric solely for The Tennessee Valley Authority (TVA) for TVA's use with the 'U.S. Nuclear Regulatory Commission (USNRC) for amending TVA's operating license of the Browns Ferry Nuclear Unit 3.
The   only undertakings of the General Electric Company respecting information in this document are contained in the contract between The Tennessee Valley Authority and General Electric Company for nuclear fuel and related services for the nuclear system for Browns Ferry Nuclear Plant Unit 3, dated June 17, 1966, and nothing contained in this document shall be constructed as changing said contract. The use of this information except as defined by said contract,,
The information contained in this report is believed by General Electric to be an accurate and true representation of the facts known, obtained or provided to General Electric at the time this report was prepared.
or for any purposes, other than that for which it is intended, is not authorized; and with respect to any such unauthorized use, neither General Electric Company nor any of the contributors to this document makes any representation or warranty (express or implied) as to the completeness, accuracy or usefulness of the information contained in this document or that such use of such infor-mation may not infringe privately owned rights; nor do they assume any respon-sibility for liability or damage of any kind which may result from such use of such information.
The only undertakings of the General Electric Company respecting information in this document are contained in the contract between The Tennessee Valley Authority and General Electric Company for nuclear fuel and related services for the nuclear system for Browns Ferry Nuclear Plant Unit 3, dated June 17,
: 1966, and nothing contained in this document shall be constructed as changing said contract.
The use of this information except as defined by said contract,,
or for any purposes, other than that for which it is intended, is not authorized; and with respect to any such unauthorized use, neither General Electric Company nor any of the contributors to this document makes any representation or warranty (express or implied) as to the completeness, accuracy or usefulness of the information contained in this document or that such use of such infor-mation may not infringe privately owned rights; nor do they assume any respon-sibility for liability or damage of any kind which may result from such use of such information.


Y1003JOlA03
Y1003JOlA03 1.
: 1. PLANT-UNI UE .ITEMS 1.0
PLANT-UNI UE.ITEMS 1.0
* Items   different from or not included in       Reference 1:
* Items different from or not included in Reference 1:
7'ata for Section     4 provided by Tennessee   Valley Authority (TVA}:                               Appendix A Fuel Loading Error LHGR:                                           Appendix B Safety/Relief Valve Capacity:                                     Appendix B Spring Safety Valve Capacity:                                     Appendix B Rated Steam Flow:                                                 Appendix B GETAB Analysis Initial Conditions:                               Appendix B New Bundle Loading, Error Event Analysis Procedures:                                               Reference  3 Margin to Spring Safety Valves:                                   Appendix C
7'ata for Section 4 provided by Tennessee Valley Authority (TVA}:
: 2.     RELOAD FUEL BUNDLES   1.0   3.3.1     and 4.0 F~uel T     e                           Number                  Number    Drilled Initial Core     8DB219                                 288                            288 Reload 1         8DRB265L                               208                            208 Reload   2       P8DRB265L                             144                           144 New             P8DRB265L                             124                           124 TOTAL                        764                            764 3 ~   REFERENCE CORE LOADING PATTERN         3.3.1 Nominal previous cycle core average exposure at end of cycle:                                                               14,297 MWd/t
Fuel Loading Error LHGR:
, Assumed reload cycle core average exposure at end of cycle:                                                                   15,105 MWd/t Core loading pattern:                                                            Figure   1
Safety/Relief Valve Capacity:
  *( ) Refers to areas       of discussion in Reference   l.
Spring Safety Valve Capacity:
Rated Steam Flow:
GETAB Analysis Initial Conditions:
New Bundle Loading, Error Event Analysis Procedures:
Margin to Spring Safety Valves:
Appendix A Appendix B Appendix B
Appendix B Appendix B
Appendix B Reference 3
Appendix C
2.
RELOAD FUEL BUNDLES 1.0 3.3.1 and 4.0 F~uel T e
Initial Core 8DB219 Reload 1
8DRB265L Reload 2
P8DRB265L Number 288 208 144 Number Drilled 288 208 144 New P8DRB265L TOTAL 124 764 124 764 3 ~
REFERENCE CORE LOADING PATTERN 3.3.1 Nominal previous cycle core average exposure at end of cycle:
, Assumed reload cycle core average exposure at end of cycle:
Core loading pattern:
14,297 MWd/t 15,105 MWd/t Figure 1
*( ) Refers to areas of discussion in Reference l.


Y1003 J01A03
Y1003J01A03 4.
: 4. CALCULATED CORE EFFECTIVE MULTIPLICATION AND CORE SYSTEM WORTH NO VOIDS   20'C 3.'3.2.1.1 AND 3.3.2.1.2 See Appendix A     for this data provided   by. The Tennessee   Valley Authority.
CALCULATED CORE EFFECTIVE MULTIPLICATIONAND CORE SYSTEM WORTH NO VOIDS 20'C 3.'3.2.1.1 AND 3.3.2.1.2 See Appendix A for this data provided by. The Tennessee Valley Authority.
: 5. STANDBY LI UID CONTROL SYSTEM   SHUTDOWN CAPABILITY   (3.3.2.1.3)
5.
Shutdown Margin (Ak)
STANDBY LI UID CONTROL SYSTEM SHUTDOWN CAPABILITY (3.3.2.1.3) 600 Shutdown Margin (Ak)
(20'C, Xenon Free) 600                                0.04
(20'C, Xenon Free) 0.04 6.
: 6. RELOAD-UNIQUE TRANSIENT ANALYSIS INPUTS     (3.3.2.1.5   AND 5.2)
RELOAD-UNIQUE TRANSIENT ANALYSIS INPUTS (3.3.2.1.5 AND 5.2)
Void Coefficient N/A* (C/% Rg)                         -6.97/-8.71 Void Fraction'(%)                                       40. 29 Doppler Coefficient N/A (C/'F)                         -0.228/-0.217 Average Fuel Temperature ('F)                           1343 Scram Worth N/A ($ )                                   -37.67/-30.13 Scram Reactivity vs Time                                Figure 2
Void Coefficient N/A* (C/% Rg)
: 7. RELOAD-UNI UE GETAB TRANSIENT ANALYSIS     INITIAL CONDITION PARAMETERS   (5 ')
Void Fraction'(%)
8x8              8x8R            P8x8R Exposure                         EOC 4            EOC 4            EOC 4 Peaking factors (local,radial                 1.22             1.20              1.20 and axial)                                      1.42              1.55              1.55 1.40             1.40              1.40
Doppler Coefficient N/A (C/'F)
'R-Factor                                        1.098            1.051              1.051 Bundle Power (MWt)                              5.987            6.550            '.526 Bundle Flow (10 lb/hr)                      108.2              108.5            109.2 Initial MCPR                                    1.24              1.25              1.25
Average Fuel Temperature
*N = Nuclear     Input Data A   Used in   Transient Analysis
('F)
Scram Worth N/A ($ )
Scram Reactivity vs Time
-6.97/-8.71
: 40. 29
-0.228/-0.217 1343
-37.67/-30.13 Figure 2
7.
RELOAD-UNI UE GETAB TRANSIENT ANALYSIS INITIALCONDITION PARAMETERS (5')
Exposure Peaking factors (local,radial and axial)
'R-Factor Bundle Power (MWt)
Bundle Flow (10 lb/hr)
Initial MCPR 8x8 EOC 4
1.22 1.42 1.40 1.098 5.987 108.2 1.24 8x8R EOC 4
1.20 1.55 1.40 1.051 6.550 108.5 1.25 P8x8R EOC 4
1.20 1.55 1.40 1.051
'.526 109.2 1.25
*N = Nuclear Input Data A
Used in Transient Analysis


Y1003J01'A03
Y1003J01'A03 8.
: 8. SELECTED MARGIN IMPROVEMENT OPTIONS                     (5. 2. 2)
SELECTED MARGIN IMPROVEMENT OPTIONS (5. 2. 2)
Recirculation.           Pump   Trip
Recirculation. Pump Trip 9.
: 9. CORE-WIDE TRANSIENT ANALYSIS RESULTS                     (5.2.2)
CORE-WIDE TRANSIENT ANALYSIS RESULTS (5.2.2)
Core P
Transient e
                                'Power Flow     4           Q/A         el       V                  4CPR          Plant Transient      e p    e          (2)   (2 NBR)   ( . NBR)   (psig)   (psig)   Sx8           8xSR PgxBR  Response e
Load Refection Without Bypass e Loss oE 100 F
Load Refection    BOC4-EOC4     104.5 100     239           111       1226     1250   0.17         0.18 0.18   Figure   3 Without Bypass  e Loss oE 100 F                  104.5 100      124          123      1013    1069    0.15          0.15  0.15. Pigure 4 Feedwater Heating Feedwster         BOC4-EOC4   .,104 ' 100     164           112   "
Feedwater Heating
1155     1189   0.12         0.12 0.12   Figure 5 Controller Failure
'Power e p e
: 10. LOCAL ROD .WITHDRAWAL ERROR (WITH                   LIMITING INSTRUMENT FAILURE)
Core Flow 4
Q/A el (2)
(2 NBR)
(. NBR)
(psig)
PV 4CPR (psig)
Sx8 8xSR 104.5 100 124 123 1013 1069 0.15 0.15 BOC4-EOC4 104.5 100 239 111 1226 1250 0.17 0.18 Plant PgxBR
 
===Response===
0.18 Figure 3
0.15.
Pigure 4
Feedwster Controller Failure BOC4-EOC4
.,104 '
100 164 112 1155 1189 0.12 0.12 0.12 Figure 5
10.
LOCAL ROD.WITHDRAWAL ERROR (WITH LIMITING INSTRUMENT FAILURE)
TRANSIENT  
TRANSIENT  


==SUMMARY==
==SUMMARY==
(5.2.1) b CPR~~                        XLRGR Rod   Block           Rod  Position                            8x8R/                    8x8R/            Limiting
(5.2.1)
~Readia             (Feet Withdrawn)             8x8 P8x8R       8x8   '8xRR               Rod   Pattern 104                       3.5                                 0.10        14.8                          Figure    6 105                      4.0                 0.12            0.11         15.2        16.5 16.2'5.2
Rod Block
                                                                                                            'igure      6 106*                      4.5                0.14         ,  0.12                     16.6              Figure    6 r
~Readia Rod Position (Feet Withdrawn) b CPR~~
107 108 7.5'.10 4.5 5.5 0.14 0.18 0.12 0.14      ,
8x8R/
15,2 15.2 16.6 16.7'5.2 Figure Figure 6
8x8 P8x8R XLRGR
6 109                      6.5                0.20            0.16                    16.7             Figure    6 110                                          0.20            0.17        15.2       16.7              Figure     6
* 8x8R/
  *Indicates setpoint selected.
8x8 '8xRR Limiting Rod Pattern 104 105 106*
**The     initial MCPR       (1.24) for the 8x8R and P8x8R fuel was 0.01 less than the operating     limit MCPR (1.25}.         This is discussed on pp. B-114 and B-115 of Reference     l.
r 107 108 109 110 3.5 4.0 4.5 4.5 5.5 6.57.5'.10 0.12 0.10 0.11 0.14
+*+A 2.2X peaking penalty for               densification is included.
, 0.12 0.14 0.12 0.18 0.14 0.20 0.16 0.20 0.17 14.8 16.2'5.2 16.6 15,2 16.6
  +Less than 25 psi margin to               spring safety valves. One safety/relief valve is   assumed     out of service.         See Appendices             B and C.
, 15.2 16.7'5.2 16.7 15.2 16.7 15.2 16.5 Figure 6
'igure 6
Figure 6
Figure 6
Figure 6
Figure 6
Figure 6
*Indicates setpoint selected.
**The initial MCPR (1.24) for the 8x8R and P8x8R fuel was 0.01 less than the operating limit MCPR (1.25}.
This is discussed on pp. B-114 and B-115 of Reference l.
+*+A 2.2X peaking penalty for densification is included.
+Less than 25 psi margin to spring safety valves.
One safety/relief valve is assumed out of service.
See Appendices B and C.


Y1003J01A03
Y1003J01A03 11.
: 11. OPERATING MCPR LIMIT (5.2),
OPERATING MCPR LIMIT (5.2),
BOC4 to EOC4 1.24                                         8x8 Fuel
BOC4 to EOC4 1.24
: 1. 25                                       8x8R Fuel
: 1. 25
: l. 25                                       P8x8R Fuel
: l. 25 8x8 Fuel 8x8R Fuel P8x8R Fuel 12.
: 12. OVERPRESSURIZATION ANALYSIS  
OVERPRESSURIZATION ANALYSIS  


==SUMMARY==
==SUMMARY==
(5. 3)
(5. 3)
Power         Core Flow        'sl            P V  Plant Transient            (%)           (%)           (psig)         (psig) Response MSIV  Closure        104.5            100            1265          1299  Figure   7 (Flux Scram)
Transient MSIV Closure (Flux Scram)
: 13. STABILITY ANALYSIS RESULTS     (5.4)
Power
Decay Ratio:   Figure   8 Reactor Core   Stability:
(%)
Decay Ratio, *x /x                     0.85 (105% Rod Line   - Natural Circulation Power)
104.5 Core Flow
Channel Hydrodynamic Performance Decay   Ratio, x /x (105%   Rod Line Natural Circulation   Power) 8x8R/P8x8R                                          0.29 8x8                                                0.36
(%)
: 14. LOSS-OF-COOLANT ACCIDENT RESULTS       (5.5.2)
100
'sl (psig) 1265 PV (psig) 1299 Plant
 
===Response===
Figure 7
13.
STABILITY ANALYSIS RESULTS (5.4)
Decay Ratio:
Figure 8
Reactor Core Stability:
Decay Ratio, *x /x (105% Rod Line - Natural Circulation Power)
Channel Hydrodynamic Performance 8x8R/P8x8R 8x8 0.85 Decay Ratio, x /x (105% Rod Line Natural Circulation Power) 0.29 0.36 14.
LOSS-OF-COOLANT ACCIDENT RESULTS (5.5.2)
Reference 2.
Reference 2.


Y1003J01A03
Y1003J01A03 15.
: 15. LOADING ERROR RESULTS (5.5.4)
LOADING ERROR RESULTS (5.5.4)
Limiting Event:   Rotated Bundle PSDRB265L MCPR:   1.08"
Limiting Event:
: 16. CONTROL'ROD'DROP ANALYSIS RESULTS   (5.5.1)
Rotated Bundle PSDRB265L MCPR:
Doppler Reactivity Coefficient:   Figure 9 Accident Reactivity Shape Functions: Figures 10 and   ll Scram Reactivity Functions:   Figures 12 and 13 Plant specific analysis results Parameter not bounded: None
1.08" 16.
CONTROL'ROD'DROP ANALYSIS RESULTS (5.5.1)
Doppler Reactivity Coefficient:
Figure 9
Accident Reactivity Shape Functions:
Figures 10 and ll Scram Reactivity Functions:
Figures 12 and 13 Plant specific analysis results Parameter not bounded:
None


Y1003J01A03 REFERENCES
Y1003J01A03 REFERENCES 1.
: 1. General Electric Boiling Water Generic Reload Fuel   Application, NEDE-24011-P-A, August 1979.
General Electric Boiling Water Generic Reload Fuel Application, NEDE-24011-P-A, August 1979.
: 2. Loss-Of-Coolant Accident Analysis Report for Browns Ferry Nuclear Plant Unit 3, NED0-24194A, July 1979.
2.
: 3. Supplemental Reload Licensing Submittal for Browns Ferry Nuclear Plant Unit 3 Reload 1, NEDO-24128 (Appendix A), June 1978.
Loss-Of-Coolant Accident Analysis Report for Browns Ferry Nuclear Plant Unit 3, NED0-24194A, July 1979.
3.
Supplemental Reload Licensing Submittal for Browns Ferry Nuclear Plant Unit 3 Reload 1, NEDO-24128 (Appendix A), June 1978.


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QGjpe DCI IQo IQc IQE I Kl K El E El Z E El K E EI IXI EI Kl lm Al IOE              OE~
I
IAI QEIQO pC KIDD pc KIQO  QejQH I
'1 3
[g IJ g) E EI Im QG                                        QG  QG          QG QG 22            QH                    DE      pe      pc Qo  IJ fg          [g Kl Kl IJ                Q IJ          Im 20  Qo+K + PE+ Pc+ Pc+K        QG              QG Pc+ +Pc Qo          DG            QG  Qo
5 7
                                                                                                                      +
S11 131517 1921 2325272S313335373941 4345474S5153555759 A R SDB219,IC' SDB219,IC C w SDRB265L,R1 D ~ PSDRB265L,R2 a IC ~ INITIALCORE, R I ~ RELOAD 1, R2 ~ RELOAD 2, etc.
OH Qo 18 QA+Qo                                        Dc+Pc                  DE+Pc    +Pc    Do+DE        PE+Do  Po+
FUEL TYPE.'
PAPAEIEIKEIKIKKKKIKIEIDAKJKlEIOD                                                                      CCIKZ 16        pA QA      Qo OE pe  Qs K  Qo  Qe  Qs  K      Qs  Qe    QE  Qe, Qe Qo, QE    pe    QEQO pcIKA 14            Z EJ KIQo      DG  ps QD  CEI OG  pe po OEQG      OGK DD    QG  OG  KQD    DG Csl Qo 12            08  Z KK      po  OE Dc      Col  OE        Col Qo pc      K    Oo      pc  DE Oo  QE K      08 10                    pa+pA pA+pa  p+pc    pa+pa    pA+pc pa+pa    pc+p~ pa+pa pc+p~ pa+pA        E+pa 8                      EIEIEIEIKOe            Oe Col KIOG lE K EIE Oe EIEI                  El Q8 6                      0808CAIDCQO880AOOQHOHOO880oCCIK0808 4                              ggKIEJ EJ IJEJOOODEJ IIEJ II,EIKIBJ 2                                p+pA pa+CA]      p+Z pA+Z pA+pA        pA+pa pA+pF I  I  I    I  I  I  I  I  I  I    I  I  I  I
~ PSDRB265L,R3 F w SDB219 IC G ~ BDB219,IC H ~ SDRB265L,R1 Figure 1.
                        '1   3 5 7     S11 131517 1921         2325272S313335373941                   4345474S5153555759 FUEL TYPE.'
Reference Core Loading Pattern
AR  SDB219,IC'                                                               ~ PSDRB265L,R3 SDB219,IC                                                              F w SDB219        IC C w SDRB265L,R1                                                             G ~ BDB219,IC D ~ PSDRB265L,R2                                                           H ~ SDRB265L,R1 a IC ~ INITIALCORE, RI ~ RELOAD 1, R2 ~ RELOAD 2, etc.
Figure 1.         Reference Core Loading Pattern


Y1003J01A03
Y1003J01A03
  .100 C-679 CRD IN PERCENT I-NOHINRL SCRRH CURVE IN (-0) 90        2-SCRRN CURVE USEO IN RNRLl'SIS 40 80 35
.100 90 C-679 CRD IN PERCENT I-NOHINRL SCRRH CURVE IN (-0) 2-SCRRN CURVE USEO IN RNRLl'SIS 40 80 35
                                                                              '0 30 60 Q
'0 30 60 Q
25 50 (A
50 (A
o                                                                         20 40 15 30 10 20 10 0                                                                   0 0                                 2;             3 TIME (SECQNDS)
o 40 25 20 30 15 20 10 10 0
Figure 2. Scram Reactivity   and   Control Rod Drive Specifications
0 2;
3 TIME (SECQNDS) 0 Figure 2.
Scram Reactivity and Control Rod Drive Specifications


1 NEUTRON   LUX                                        1 VESSEL    ES RISE IPSI) 2 AVE SURF CE HEAT FLUX                                 2 SAFETT V LVE FLOW 150.                      3 CORE INL T F OH                                        3 RE EF V LVE FLOW 8 BTPRSS V LV   LOH 5
150.
6 o  100.
1 NEUTRON 2 AVE SURF 3 CORE INL LUX CE HEAT FLUX T F OH 1
VESSEL 2 SAFETT V 3 RE EF V 8 BTPRSS V
5 6
ES RISE IPSI)
LVE FLOW LVE FLOW LV LOH o
100.
I I
I I
100.
100.
: 0.                                                 0.
0.0.
: 0. 8.           12.         16.               0.           8.           12.         16; TINE (SEC)                                               TINE (SEC)
8.
I LEVEL(1 H-REF-SEP-SKIRT                               I VOIO AE TIVITT 2 VESSEL 5 EAHFLOH 3 ~TUR8INE  TEANFLOH                                    3 SCRAN RE CTIVITT 100.
12.
TINE (SEC) 16.
0.0.
8.
12.
TINE (SEC) 16; I LEVEL(1 2 VESSEL 5 3 ~TUR8INE H-REF-SEP-SKIRT EAHFLOH TEANFLOH I VOIO AE 3 SCRAN RE TIVITT CTIVITT 100.
0.
0.
  -100.
-100.
0     8.           12.         16.               0. O.Q     0.8         1.2           1.6.
0 8.
TINE (SEC)                                            TINE ISEC)
12.
Figure 3.     Plant Response to Generator Load Rejection Mithout Bypass
TINE (SEC) 16.
0.
O.Q 0.8 TINE ISEC) 1.2 1.6.
Figure 3.
Plant Response to Generator Load Rejection Mithout Bypass


I VESSEL P ES RISE (PSI)
150.
                                "I HEUTROH VC~hr LUX GE-HEAT-R.UX                                         2 RELIEF V LVE FLOH 3 CORE IMl I FLOH              125.
I HEUTROH
3 BTPASS Vl V F 150.                        'l CURE IHL I SUB 5
" VC~hr 3 CORE IMl
o 4J 100.
'l CURE IHL 5
I h
LUX GE-HEAT-R.UX I FLOH I SUB 125.
I Ps 50.
I VESSEL P 2 RELIEF V 3 BTPASS Vl ES RISE (PSI)
: 0.                                                         -25.
LVE FLOH V
: 0. QO. 80.         120.         160.                     0     QO.       80.       120.        160.
F o
TIME (SEC)                                                         TIME (SEC)
100.
I LEVEL(I H-REF"SEP-SKIRT                                         I VOID REA T I VITY 2 VESSEL S EAMFLOH                                               2 OOPPLER EACT I V ITT 3 TURBINE   TEAHFLOH                                             3 SCRAH AE CTIVITT 150.                                                                                                       CTIVITV th Vl 100.                                                      I   0.
4J I
h I
Ps 50.
0.0.
QO.
80.
120.
TIME (SEC) 160.
-25.0 QO.
80.
120.
TIME (SEC) 160.
150.
I LEVEL(I H-REF"SEP-SKIRT 2 VESSEL S EAMFLOH 3 TURBINE TEAHFLOH I VOID REA 2 OOPPLER 3 SCRAH AE TIVITY EACTIVITT CTIVITT CTIVITV 100.
th Vl I
W 0
W 0
LJ
LJ 0.
                                                                -1.
-1.
I 0.
I 0.0.
: 0.         80.         120.         160.                     0     )(0.     80.         120.        160.
80.
TIME (SEC)                                                      TINE (SEC)
120.
Figure 4. Plant     -Response   to Loss of 100 Deg F Feedwater   Heating
TIME (SEC) 160.
0
)(0.
80.
120.
TINE (SEC) 160.
Figure 4.
Plant -Response to Loss of 100 Deg F Feedwater Heating


I NEUTRON LUX                                            1 VESSEL P ES RISE IPSI) 2 AVE SURF CE HEAT fLUX                                 2 SAFETT V LVE FL%
150.
150.                            3 CO        I FLOW 125.                       3REI FV     V  FOH 9 CORE INL  I  SUB                                      0 BTPRSS V LV    LON 5                                                        5 6
I NEUTRON 2 AVE SURF 3 CO 9 CORE INL 5
oUJ 100.
LUX CE HEAT fLUX I FLOW I SUB 125.
I I
1 VESSEL P 2 SAFETT V 3REI FV 0 BTPRSS V
Pu  50.
5 6
g 0.
ES RISE IPSI)
: 0. 10.      20 0        30.          40.                    10. 20.        30.        QO.
LVE FL%
TINE (SEC)                                              TINE (SEC)
V FOH LV LON o
I LEVEL (I    -REF-SEP-SKIRT                            1 VOIO RE  T IVIT 2 VESSEL S EAHFLOK                                      2  OPPLER  ERG    ITT 3 TURBINE TEAHFLOW                                          CRAH RE CT  ITT 150.
100.
100.
0.
UJ I
: 0. 10.       20.       30.           40.                   0         12.         18.
I Pu 50.
TINE ISEC)                                           TIRE (SEC)
g 0.0.
Figure 5. Plant Response to Feedwater Controller Failure, Maximum Demand
10.
20 0 30.
TINE (SEC) 40.
10.
20.
30.
TINE (SEC)
QO.
150.
I LEVEL(I
-REF-SEP-SKIRT 2 VESSEL S EAHFLOK 3 TURBINE TEAHFLOW 1 VOIO RE 2
OPPLER CRAH RE TIVIT ERG ITT CT ITT 100.
0.0.
10.
20.
30.
TINE ISEC) 40.
0 12.
TIRE (SEC) 18.
Figure 5.
Plant Response to Feedwater Controller Failure, Maximum Demand


Y1003J01A03 1
Y1003J01A03 1
NOTES: lo ROD PATTERN IS 1/4 CORE MIRROR SYMMETRIC (FULL CORE SHOWN)
NOTES: lo ROD PATTERN IS 1/4 CORE MIRROR SYMMETRIC (FULL CORE SHOWN) 2.
: 2. NO. INDICATES NUMBER OF NOTCHES WITHDRAWN OUT OF. 48.
NO.
BLANK IS A WITHDRAWN ROD
INDICATES NUMBER OF NOTCHES WITHDRAWN OUT OF. 48.
: 3. ERROR ROD IS (26 ~ 35) 2    6  10  14  18    22    26    30  34  38    42  46  50 54 58 59                       6           4         4           6 55                36         36         36       36    .,  36 51            6        6          2         2        ~ 6       6 47        36        36        36          36      36        36      36 43 39 35 31 27 6
BLANK IS A WITHDRAWN ROD 3.
4 4
ERROR ROD IS (26 ~ 35) 59 55 51 47 43 6
36 36 2,
39 35 4
31 27 4
23 19 6
15ll v
7 3
10 36 0
36 10 36 2
6 10 14 18 22 26 6
4 36 36 6
6 2
6 2
36 36 10 14 14 36 40 14 0
36 36 36 6
0 40 36 14 0
14 36 36 36 2,
36 40 10 14 14 36 36 6
14 0
2 2
36 40 2
14 36 36 6
36 36 6
36 36 6
4 4
6 2
23      36       36         36         40       36       36     36 19  6          6        10                   14        10        6     6 15      36       36         36         36       36       36     36 v
36 36 40 36 0
ll 7
40 14 36 2.
36 14 36 10 36 36 4
36 36 36 36 30 34 38 42 46 4
6 36 36 36 2
~ 6 36 36 36 14 10 40 36 36 14 50 54 58 6
36 6
6 36 2
4 36 2
4 36 6
6 36 6
6 36 6
36 2
Figure 6.
36 2.
Limiting RWE Rod Pattern 12
36        36 6
3                                            4 Figure 6. Limiting RWE Rod Pattern 12


1 NEUTRON   LUX                                                    1 VESSEL P ES RISE  (PSI) 2 AVE SURF CE HEAT FLUX                                             2 SAFETT V LVE FLON 150.                  3 CORE INL T F OW                                                    3 RELIEF V LVE FLON 0 BTPASS V LV     ON 5
150.
6 r)   100.
1 NEUTRON 2 AVE SURF 3 CORE INL LUX CE HEAT FLUX T F OW 1
I Pu   50.                                                 100.
VESSEL P 2 SAFETT V 3 RELIEF V
: 0.                                                   0.
0 BTPASS V
0 8.            12.         16.                     0.               8.           12.        16.
5 6
TIHE (SEC)                                                           TIHE (SEC)
ES RISE (PSI)
I LEVEL(I H-REF-SEP-SKIRT                                           1 VOIO RER TIVIT 2 VESSEL S ERHFLON                                                   2 OGPPLER        V ITT 3 TURBINE     TEAHFLON                                               3 SCR       CTIVITY 100.
LVE FLON LVE FLON LV ON r) 100.
I Pu 50.
100.
0.0 8.
12.
TIHE (SEC) 16.
0.0.
8.
12.
TIHE (SEC) 16.
I LEVEL(I H-REF-SEP-SKIRT 2 VESSEL S ERHFLON 3 TURBINE TEAHFLON 1 VOIO RER TIVIT 2 OGPPLER VITT 3 SCR CTIVITY 100.
0.
-100.
0 8.
12.
TINE (SEC) 16.
0.
0.
  -100.
0.6 1.2 1.8 TIHE (SEC)
0  8.          12.          16.                    0.      0.6       1.2       1.8         2. (I TINE (SEC)                                                        TIHE (SEC)
: 2. (I Figure 7.
Figure 7.     Plant Response to   MSIV Closure
Plant Response to MSIV Closure
 
Y1003J01A03 1.2 1.0 ULTIMATESTABILITYLIMIT O
0,8 X
OI-K 0.6 NATURAL CIRCULATION 105% ROD LINE 0,4 0.2 0
0 40 60 PERCENT POWER 80 Figure 8.
Decay Ratio 14


Y1003J01A03 1.2 ULTIMATESTABILITYLIMIT 1.0 O
Y1003J01A03 A CALCULATEDVALUE@OLD B
0,8 X        NATURAL O         CIRCULATION I-K 0.6 105% ROD LINE 0,4 0.2 0
CALCULATEDVALUEWSB C
0          40            60              80 PERCENT POWER Figure 8. Decay  Ratio 14
BOUNDINGVALUEFOR 280 eel/g, COLD D BOUNDINGVALUEFOR 280 eel/g, HSB xI-z0 e
zIII O
IL IL UI00L III 00
-10
-16
-20
-26
-30 0
1000


Y1003J01A03 A CALCULATEDVALUE@OLD B CALCULATEDVALUEWSB C BOUNDING VALUE FOR 280 eel/g, COLD D BOUNDING VALUE FOR 280 eel/g, HSB
1600 2000
        -10 xI-z 0
, FUEL TEMPERATURE tdeg C)
        -16 e
Figure 9.
z III O
Doppler Reactivity Coefficient Comparison for RDA
IL    -20 IL UI 00 L
III 0    -26 0
        -30 0              1000        1600       2000
                              , FUEL TEMPERATURE tdeg C)
Figure 9. Doppler Reactivity Coefficient Comparison         for   RDA


Y1003J01A03 A ACCIDENT FUNCTION B BOUNDING VALUE FOR 280 eel/II 15 10 0
Y1003J01A03 A ACCIDENT FUNCTION B
0                         10                 15                  20 ROD POSITION, feet OUT Figure 10. Accident Reactivity Shape Function at 20         C
BOUNDINGVALUEFOR 280 eel/II 15 10 0
0 10 ROD POSITION, feet OUT 15 20 Figure 10.
Accident Reactivity Shape Function at 20 C


Y1003JOlA03 20 A ACCIDENT FUNCTION B BOUNDING VALUE FOR &0 csl/g, Z
Y1003JOlA03 20 A ACCIDENT FUNCTION B
I 0
BOUNDINGVALUEFOR &0csl/g, Z
Z 0
I0Z 0XI-Y 10 0
X I-Y 10 0
b K
b K
0 0                           10                 15 ROD POSITION, fest OUT Figure 11.. Accident Reactivity   Shape   Function at 286'C 17
0 0
10 ROD POSITION, fest OUT 15 Figure 11.. Accident Reactivity Shape Function at 286'C 17


Y1003J01A03 60 A SCRAM FUNCTION B BOUNDING VALUE FOR 280 ceI/O 40 x
Y1003J01A03 60 A SCRAM FUNCTION B
O D
BOUNDINGVALUE FOR 280 ceI/O 40 x
0 x
O D0 Ix 30 5C 0
I 30 5C 0
E3 z
E3 z
20 I-I-
20 I-I-
O K
O K
10 0
10 0
0 ELAPSED TIME, seconds Figurerl2. Scram   Reactivity Function at 20'C
0 ELAPSED TIME,seconds Figurerl2.
Scram Reactivity Function at 20'C


Y1003J01A03 A SCRAM FUNCTION 75                                B BOUNDING VALUE FOR 280 eel/g 50 25 0
Y1003J01A03 75 A SCRAM FUNCTION B
0                         3             4 ELAPSED TIME, seconds Figure 13. Scram Reactivity Function at 286'C 19/20
BOUNDING VALUEFOR 280 eel/g 50 25 0
0 3
4 ELAPSED TIME,seconds Figure 13.
Scram Reactivity Function at 286'C 19/20


I C
I C


Y1003J01A03 APPENDIX A SHUTDOWN MARGIN DETERMINATION A.l   BASES The reference loading pattern, documented in item 3 of this supplemental reload submittal, is the basis for, all reload licensing and operational planning and is comprised of the fuel bundles designated in item 2 of this supplemental submittal. It in'urn is based on the best possible prediction of the core condition at the end of the present cycle and on the desired c'ore energy capability for the reload cycle. It is designed with the intent k
Y1003J01A03 APPENDIX A SHUTDOWN MARGIN DETERMINATION A.l BASES The reference loading pattern, documented in item 3 of this supplemental reload submittal, is the basis for, all reload licensing and operational planning and is comprised of the fuel bundles designated in item 2 of this supplemental submittal.
that it will represent, as clos'ely as possible, the actual core loading pattern.
It in'urn is based on the best possible prediction of the core condition at the end of the present cycle and on the desired c'ore energy capability for the reload cycle.
A.2   CORE CHARACTERISTICS The reference. core is analyzed in detail to ensure that adequate cold shutdown margin exists. This section discusses the results of core calculations for shutdown margin.
It is designed with the intent k
A.2.1 Core Effective Multiplication and'Control     Rod Worth Core effective multiplication and.control rod worths   were calculated using the TVA BWR simulator. code (References A-l, A-3) in conjunction with the TVA lattice physics data generation code (References A-2, A-3) to determine the core reactivity with all rods withdrawn and with all rods inserted. A tabulation of the results is provided in Table A.l. These three eigenvalues (effective multi-plication of the core; uncontrolled, fully controlled, and with the strongest rod out) were calculated at the beginning-of-cycle 4 core average exposure corresponding to the minimum expected end-of-cycle 3 core average exposure.
that it will represent, as clos'ely as possible, the actual core loading pattern.
A.2 CORE CHARACTERISTICS The reference. core is analyzed in detail to ensure that adequate cold shutdown margin exists.
This section discusses the results of core calculations for shutdown margin.
A.2.1 Core Effective Multiplication and'Control Rod Worth Core effective multiplication and.control rod worths were calculated using the TVA BWR simulator. code (References A-l, A-3) in conjunction with the TVA lattice physics data generation code (References A-2, A-3) to determine the core reactivity with all rods withdrawn and with all rods inserted.
A tabulation of the results is provided in Table A.l.
These three eigenvalues (effective multi-plication of the core; uncontrolled, fully controlled, and with the strongest rod out) were calculated at the beginning-of-cycle 4 core average exposure corresponding to the minimum expected end-of-cycle 3 core average exposure.
The core was assumed to be in a xenon-free condition.
The core was assumed to be in a xenon-free condition.


Y1003J01A03 Cold keff was calculated ff                with the strongest control rod out at various exposures through the cycle. The value R is the difference between the strongest rod out keffff at BOC and the maximum calculated strongest rod out ff at any exposure point. The strongest rod out keff keff                                                    ff at any exposure point is equal to or less than:
Y1003J01A03 Cold k ff was calculated with the strongest control rod out at various eff exposures through the cycle.
k SRO = (Fully controlled keff ) BOC + (Strongest Rod Worth) BOC + R eff A.2.2 Reactor Shutdown Margin Technical Specifications require that the refueled core must be capable of being made subcritical with 0.38 percent Ak margin in the most reactive condition throughout the subsequent operating cycle with the most reactive control rod in its full out position and all other rods fully inserted.
The value R is the difference between the strongest rod out k ff at BOC and the maximum calculated strongest rod out eff k ff at any exposure point.
The shutdown margin   is determined by using the BWR simulator code to calcu-late the core multiplication at selected'exposure points with the strongest rod fully withdrawn. The shutdown margin for the reloaded core is obtained SRO by subtracting the keff given in Table A.l from the critical keff of 1.0, resulting in a calculated cold shutdown margin of 1.1 percent Ak.
The strongest rod out k ff at any exposure eff eff point is equal to or less than:
k
= (Fully controlled k
)
BOC + (Strongest Rod Worth)
BOC + R SRO eff eff A.2.2 Reactor Shutdown Margin Technical Specifications require that the refueled core must be capable of being made subcritical with 0.38 percent Ak margin in the most reactive condition throughout the subsequent operating cycle with the most reactive control rod in its full out position and all other rods fully inserted.
The shutdown margin is determined by using the BWR simulator code to calcu-late the core multiplication at selected'exposure points with the strongest rod fully withdrawn.
The shutdown margin for the reloaded core is obtained by subtracting the k given in Table A.l from the critical k of 1.0, SRO eff eff resulting in a calculated cold shutdown margin of 1.1 percent Ak.
A-2
A-2


Y1003JOlA03 Table A.'1 CALCULATED CORE EFFECTIVE MULTIPLICATION AND CONTROL ROD WORTHS NO VOIDS, NO XENON, 20 C UNC Uncontrolled, K ff eff                         1.120 CON Fully Controlled, K eff                     0.955-SRO Strongest Control     Out, Rod      K ff eff           0.989 R, Maximum Increase in Cold Core Reactivity       0.000 With Exposure Into Cycle, Ak A-3
Y1003JOlA03 Table A.'1 CALCULATED CORE EFFECTIVE MULTIPLICATIONAND CONTROL ROD WORTHS NO VOIDS, NO XENON, 20 C
Uncontrolled, K ff UNC eff Fully Controlled, KCON eff Strongest Control Rod Out, K ff SRO eff 1.120 0.955-0.989 R,
Maximum Increase in Cold Core Reactivity With Exposure Into Cycle, Ak 0.000 A-3


Y1003J01A03 REFERENCES A-l. S. L. Forkner, G. H; Meriwether, and T. D. Beu, "Three-Dimensional LWR Core Simulation Methods," TVA-TR78-03A, 1978 A-2. B. L. Darnell, T. D. Beu, and G. W. Perry, "Methods   for the Lattice Physics Analysis of LWR's," TVA-TR78-02A, 1978 A-3. "Verification of TVA Steady-State BWR Physics Methods," TVA-TR79-01A, 1979 A-4
Y1003J01A03 REFERENCES A-l.
A-2.
A-3.
S. L. Forkner, G. H; Meriwether, and T. D. Beu, "Three-Dimensional LWR Core Simulation Methods," TVA-TR78-03A, 1978 B. L. Darnell, T. D. Beu, and G.
W. Perry, "Methods for the Lattice Physics Analysis of LWR's," TVA-TR78-02A, 1978 "Verification of TVA Steady-State BWR Physics Methods," TVA-TR79-01A, 1979 A-4


Y1003J01A03 APPENDIX B Fuel Loading Error   LHGR :   Rotated Bundle, 16.9 kW/ft; Misplaced Bundle, 18.1 kW/ft Safety/Relief Valve Capacity at Setpoint (No./%): 10/63.6**
Y1003J01A03 APPENDIX B Fuel Loading Error LHGR :
Spring Safety Valve Capacity at Setpoint (No./%): 2/14.2 Rated Steam Flow: 14.09 x 10 6 lb/hr GETAB Analysis Initial Conditions Reactor Pressure:   1035 psia Inlet Enthalpy:     521.5 Btu/lb king penalty for densification is included.
Rotated Bundle, 16.9 kW/ft; Misplaced Bundle, 18.1 kW/ft Safety/Relief Valve Capacity at Setpoint (No./%):
10/63.6**
Spring Safety Valve Capacity at Setpoint (No./%):
2/14.2 Rated Steam Flow:
14.09 x 10 lb/hr 6
GETAB Analysis Initial Conditions Reactor Pressure:
1035 psia Inlet Enthalpy:
521.5 Btu/lb king penalty for densification is included.
one safety/relief vlave out of service.
one safety/relief vlave out of service.
B-1/B-2
B-1/B-2


N I
N I
          'E I
'E I
C 4 ~   I r   l
C 4 ~
I r
l


Y1003JOlA03 APPENDIX C MARGIN TO SPRING SAFETY VALVES The rationale for changing the basis for providing pressure margin to the safety valves is presented in Reference C-1. This change has been h
Y1003JOlA03 APPENDIX C MARGIN TO SPRING SAFETY VALVES The rationale for changing the basis for providing pressure margin to the
                                                                          'pring accepted by the   NRC (Reference C-2).
'pring safety valves is presented in Reference C-1.
On this basis the plant can operate at full power throughout the cycle.
This change has been h
accepted by the NRC (Reference C-2).
On this basis the plant can operate at full power throughout the cycle.


Y1003 J01A03 REFERENCES C-l. J. F. Quirk (GE) letter to Olan D. Parr (NRC), "General Electric Licensing Topical Report NEDE-24011-P-A, 'Generic Reload Fuel Submittal," dated February 28, 1979.
Y1003J01A03 REFERENCES C-l.
Application,'ppendix D, Second C-2. Letter, T. A. Ippolito (NRC) to D. L. Peoples (Commonwealth Edison Co.)
C-2.
enclosing a Safety Evaluation supporting Amendment No. 42 to Facility Operating License No. DPR-25.Dresden Nuclear Power Station Unit 3, dated April 16, 1980.
J. F. Quirk (GE) letter to Olan D. Parr (NRC), "General Electric Licensing Topical Report NEDE-24011-P-A,
'Generic Reload Fuel Application,'ppendix D, Second Submittal," dated February 28, 1979.
Letter, T. A. Ippolito (NRC) to D. L. Peoples (Commonwealth Edison Co.)
enclosing a Safety Evaluation supporting Amendment No. 42 to Facility Operating License No. DPR-25.Dresden Nuclear Power Station Unit 3, dated April 16, 1980.
C-2}}
C-2}}

Latest revision as of 04:07, 7 January 2025

Application for Amend of License DPR-68,changing Tech Specs to Accomodate Reload 3,Cycle 4 Operation of Unit 3.Shutdown Planned for 801020 to Begin Refueling Outage W/Restart on 801201.Class III Fee Encl
ML18025B054
Person / Time
Site: Browns Ferry 
Issue date: 08/27/1980
From: Mills L
TENNESSEE VALLEY AUTHORITY
To:
Shared Package
ML18025B055 List:
References
TVA-BFNP-TS-148, NUDOCS 8009020406
Download: ML18025B054 (30)


Text

Y1003J01A03 Class I August 1980 SUPPLEMENTAL RELOAD LICENSING SUBMITTAL FOR BROWNS FERRY NUCLEAR POWER STATION UNIT 3 RELOAD NO.

3 Prepared:

C. L. Hilf Approved:

R.

E. Engel, Manager Reload Fuel Licensing NUCLEAR POWER SYSTEMS DIVISION~ GENERAL ELECTRIC COMPANY SAN JOSE, CALIFORNIA95125 GENERAL ELECTRIC DOQOZ, c) QC3$

Y1003JOlA03 IMPORTANT NOTICE REGARDING CONTENTS OF THIS REPORT PLEASE READ CAREFULLY This report was prepared by General Electric solely for The Tennessee Valley Authority (TVA) for TVA's use with the 'U.S. Nuclear Regulatory Commission (USNRC) for amending TVA's operating license of the Browns Ferry Nuclear Unit 3.

The information contained in this report is believed by General Electric to be an accurate and true representation of the facts known, obtained or provided to General Electric at the time this report was prepared.

The only undertakings of the General Electric Company respecting information in this document are contained in the contract between The Tennessee Valley Authority and General Electric Company for nuclear fuel and related services for the nuclear system for Browns Ferry Nuclear Plant Unit 3, dated June 17,

1966, and nothing contained in this document shall be constructed as changing said contract.

The use of this information except as defined by said contract,,

or for any purposes, other than that for which it is intended, is not authorized; and with respect to any such unauthorized use, neither General Electric Company nor any of the contributors to this document makes any representation or warranty (express or implied) as to the completeness, accuracy or usefulness of the information contained in this document or that such use of such infor-mation may not infringe privately owned rights; nor do they assume any respon-sibility for liability or damage of any kind which may result from such use of such information.

Y1003JOlA03 1.

PLANT-UNI UE.ITEMS 1.0

  • Items different from or not included in Reference 1:

7'ata for Section 4 provided by Tennessee Valley Authority (TVA}:

Fuel Loading Error LHGR:

Safety/Relief Valve Capacity:

Spring Safety Valve Capacity:

Rated Steam Flow:

GETAB Analysis Initial Conditions:

New Bundle Loading, Error Event Analysis Procedures:

Margin to Spring Safety Valves:

Appendix A Appendix B Appendix B

Appendix B Appendix B

Appendix B Reference 3

Appendix C

2.

RELOAD FUEL BUNDLES 1.0 3.3.1 and 4.0 F~uel T e

Initial Core 8DB219 Reload 1

8DRB265L Reload 2

P8DRB265L Number 288 208 144 Number Drilled 288 208 144 New P8DRB265L TOTAL 124 764 124 764 3 ~

REFERENCE CORE LOADING PATTERN 3.3.1 Nominal previous cycle core average exposure at end of cycle:

, Assumed reload cycle core average exposure at end of cycle:

Core loading pattern:

14,297 MWd/t 15,105 MWd/t Figure 1

  • ( ) Refers to areas of discussion in Reference l.

Y1003J01A03 4.

CALCULATED CORE EFFECTIVE MULTIPLICATIONAND CORE SYSTEM WORTH NO VOIDS 20'C 3.'3.2.1.1 AND 3.3.2.1.2 See Appendix A for this data provided by. The Tennessee Valley Authority.

5.

STANDBY LI UID CONTROL SYSTEM SHUTDOWN CAPABILITY (3.3.2.1.3) 600 Shutdown Margin (Ak)

(20'C, Xenon Free) 0.04 6.

RELOAD-UNIQUE TRANSIENT ANALYSIS INPUTS (3.3.2.1.5 AND 5.2)

Void Coefficient N/A* (C/% Rg)

Void Fraction'(%)

Doppler Coefficient N/A (C/'F)

Average Fuel Temperature

('F)

Scram Worth N/A ($ )

Scram Reactivity vs Time

-6.97/-8.71

40. 29

-0.228/-0.217 1343

-37.67/-30.13 Figure 2

7.

RELOAD-UNI UE GETAB TRANSIENT ANALYSIS INITIALCONDITION PARAMETERS (5')

Exposure Peaking factors (local,radial and axial)

'R-Factor Bundle Power (MWt)

Bundle Flow (10 lb/hr)

Initial MCPR 8x8 EOC 4

1.22 1.42 1.40 1.098 5.987 108.2 1.24 8x8R EOC 4

1.20 1.55 1.40 1.051 6.550 108.5 1.25 P8x8R EOC 4

1.20 1.55 1.40 1.051

'.526 109.2 1.25

  • N = Nuclear Input Data A

Used in Transient Analysis

Y1003J01'A03 8.

SELECTED MARGIN IMPROVEMENT OPTIONS (5. 2. 2)

Recirculation. Pump Trip 9.

CORE-WIDE TRANSIENT ANALYSIS RESULTS (5.2.2)

Transient e

Load Refection Without Bypass e Loss oE 100 F

Feedwater Heating

'Power e p e

Core Flow 4

Q/A el (2)

(2 NBR)

(. NBR)

(psig)

PV 4CPR (psig)

Sx8 8xSR 104.5 100 124 123 1013 1069 0.15 0.15 BOC4-EOC4 104.5 100 239 111 1226 1250 0.17 0.18 Plant PgxBR

Response

0.18 Figure 3

0.15.

Pigure 4

Feedwster Controller Failure BOC4-EOC4

.,104 '

100 164 112 1155 1189 0.12 0.12 0.12 Figure 5

10.

LOCAL ROD.WITHDRAWAL ERROR (WITH LIMITING INSTRUMENT FAILURE)

TRANSIENT

SUMMARY

(5.2.1)

Rod Block

~Readia Rod Position (Feet Withdrawn) b CPR~~

8x8R/

8x8 P8x8R XLRGR

  • 8x8R/

8x8 '8xRR Limiting Rod Pattern 104 105 106*

r 107 108 109 110 3.5 4.0 4.5 4.5 5.5 6.57.5'.10 0.12 0.10 0.11 0.14

, 0.12 0.14 0.12 0.18 0.14 0.20 0.16 0.20 0.17 14.8 16.2'5.2 16.6 15,2 16.6

, 15.2 16.7'5.2 16.7 15.2 16.7 15.2 16.5 Figure 6

'igure 6

Figure 6

Figure 6

Figure 6

Figure 6

Figure 6

  • Indicates setpoint selected.
    • The initial MCPR (1.24) for the 8x8R and P8x8R fuel was 0.01 less than the operating limit MCPR (1.25}.

This is discussed on pp. B-114 and B-115 of Reference l.

+*+A 2.2X peaking penalty for densification is included.

+Less than 25 psi margin to spring safety valves.

One safety/relief valve is assumed out of service.

See Appendices B and C.

Y1003J01A03 11.

OPERATING MCPR LIMIT (5.2),

BOC4 to EOC4 1.24

1. 25
l. 25 8x8 Fuel 8x8R Fuel P8x8R Fuel 12.

OVERPRESSURIZATION ANALYSIS

SUMMARY

(5. 3)

Transient MSIV Closure (Flux Scram)

Power

(%)

104.5 Core Flow

(%)

100

'sl (psig) 1265 PV (psig) 1299 Plant

Response

Figure 7

13.

STABILITY ANALYSIS RESULTS (5.4)

Decay Ratio:

Figure 8

Reactor Core Stability:

Decay Ratio, *x /x (105% Rod Line - Natural Circulation Power)

Channel Hydrodynamic Performance 8x8R/P8x8R 8x8 0.85 Decay Ratio, x /x (105% Rod Line Natural Circulation Power) 0.29 0.36 14.

LOSS-OF-COOLANT ACCIDENT RESULTS (5.5.2)

Reference 2.

Y1003J01A03 15.

LOADING ERROR RESULTS (5.5.4)

Limiting Event:

Rotated Bundle PSDRB265L MCPR:

1.08" 16.

CONTROL'ROD'DROP ANALYSIS RESULTS (5.5.1)

Doppler Reactivity Coefficient:

Figure 9

Accident Reactivity Shape Functions:

Figures 10 and ll Scram Reactivity Functions:

Figures 12 and 13 Plant specific analysis results Parameter not bounded:

None

Y1003J01A03 REFERENCES 1.

General Electric Boiling Water Generic Reload Fuel Application, NEDE-24011-P-A, August 1979.

2.

Loss-Of-Coolant Accident Analysis Report for Browns Ferry Nuclear Plant Unit 3, NED0-24194A, July 1979.

3.

Supplemental Reload Licensing Submittal for Browns Ferry Nuclear Plant Unit 3 Reload 1, NEDO-24128 (Appendix A), June 1978.

Y1003J01A03 60 PFQA P8 QA QAI I Ipe PAIQF 58 g KEI Do EJ Do EJ EJ lm Oo OB 56 Qe De pcIQO DH OH ph Qo DH,QHQQ QH QH po,pc OA,OG 08 54 ps OD pcpopE pe Qe Oo OEQG CGlOE Qo OG QG pE Qo Qc Qo OB 52 Qe OA OA Qo DAI K Oo DA QEIK IDA COIIQE DCIQA OoIOA DIOG 5o 08 K K po K pc po I Do po OE po CCI OE Qo K K 08

~

48 KEl KEl OG Os IJ K El QG DD KlRIIJKEl DGIDG KIDD DGIQG Qo Im QA 46 KK CCI Qo OE Pe Os K Po pe Qe PE CCI ps DG PE Os Pe Do DE Oe Qs 0+CI Pc+Oh K 44 Ph Dc EJ Q EI KI Ph OE DA EIKIEJIK EJIK DA [P EJ I Do [Q PAI 42 Po Col QE OE Oo Pc Pc K K Pc +Pc Do+DE CCI K+DO Po Z 40 Q8 Qo OH DG KJ EJ DG OG KI De Q Dc Oo Ds DG EJ g] [g DG Dc K QG QG Qo KI QG DH Im El 38PA'Pc 8 Csl Oo'OE ps De Pc QE Pe Cel OE Ps gs PE Oe Cel K CCI Os Os K Col Qe 8 Pc Kl 36DAIIQDDAIIKK KIDAEJEKIEIKKJEIDCEODOAEJtmZ 34Ipc Qo QE ~

QE pc Qo pc Qc po pc K

Qc QE Qo pc 32Z Po OH Oe OE Qo CGJ Ps DE Pe 06 OE PszOG OE OGIOG IK QGIOG OOIQE Cel 8 Do K 30 Oo QH Os KIIJ ps Os DE Qe Qe QE ps C<IEJ KI Qs Qs ElKIOe Qs Qo QE Oe OH po ph 28 ph pc QOIQE QE Dc Qo pc I

DCI IQo IQc IQE I QEIQO pC 26Z[I El KlEl OH E KEl EI KlKElIE El Z E El K IA I E EI IXIEI Kllm IAl 24 pC pH Qe Qo OE pG QG pC OE lm Qs K QGjpe IOE QG QG OE~

QG QG KIQO QejQH pc 22[g IJ QH g) E EI Im QG DE pe QG pc Qo IJ fg Qo

[g DG KlKlIJ QG Qo Q IJ OH Qo Im 20 QA+Qo Qo+K +

PE+

Pc+

Pc+K Dc+Pc Pc+

+Pc DE+Pc +Pc Do+DE +

PE+Do Po+

18PAPAEIEIKEIKIKKKKIKIEIDAKJKlEIOD CCIKZ 16 14 12 10 8

6 4

2 pA QA Qo OE pe Qs K Qo Qe Qs K Qs Qe QE Qe, Qe Qo, QE pe QEQO pcIKA Z EJ KIQo DG ps QD CEI OG pe po OEQG OGK DD QG OG KQD DG Csl Qo KIDD

08 Z KK po OE Dc Col OE Col Qo pc K Oo pc DE Oo QE K 08 pa+pA pA+pa p+pc pa+pa pA+pc pa+pa pc+p~

pa+pa pc+p~

pa+pA E+pa EIEIEIEIKOe Oe Col KIOG lEKEIE Oe EIEI El Q8 0808CAIDCQO880AOOQHOHOO880oCCIK0808 ggKIEJ EJ IJEJOOODEJ IIEJ II,EIKIBJ p+pA pa+CA] p+Z pA+Z pA+pA pA+pa pA+pF I

I I

I I

I I

I I

I I

I I

I

'1 3

5 7

S11 131517 1921 2325272S313335373941 4345474S5153555759 A R SDB219,IC' SDB219,IC C w SDRB265L,R1 D ~ PSDRB265L,R2 a IC ~ INITIALCORE, R I ~ RELOAD 1, R2 ~ RELOAD 2, etc.

FUEL TYPE.'

~ PSDRB265L,R3 F w SDB219 IC G ~ BDB219,IC H ~ SDRB265L,R1 Figure 1.

Reference Core Loading Pattern

Y1003J01A03

.100 90 C-679 CRD IN PERCENT I-NOHINRL SCRRH CURVE IN (-0) 2-SCRRN CURVE USEO IN RNRLl'SIS 40 80 35

'0 30 60 Q

50 (A

o 40 25 20 30 15 20 10 10 0

0 2;

3 TIME (SECQNDS) 0 Figure 2.

Scram Reactivity and Control Rod Drive Specifications

150.

1 NEUTRON 2 AVE SURF 3 CORE INL LUX CE HEAT FLUX T F OH 1

VESSEL 2 SAFETT V 3 RE EF V 8 BTPRSS V

5 6

ES RISE IPSI)

LVE FLOW LVE FLOW LV LOH o

100.

I I

100.

0.0.

8.

12.

TINE (SEC) 16.

0.0.

8.

12.

TINE (SEC) 16; I LEVEL(1 2 VESSEL 5 3 ~TUR8INE H-REF-SEP-SKIRT EAHFLOH TEANFLOH I VOIO AE 3 SCRAN RE TIVITT CTIVITT 100.

0.

-100.

0 8.

12.

TINE (SEC) 16.

0.

O.Q 0.8 TINE ISEC) 1.2 1.6.

Figure 3.

Plant Response to Generator Load Rejection Mithout Bypass

150.

I HEUTROH

" VC~hr 3 CORE IMl

'l CURE IHL 5

LUX GE-HEAT-R.UX I FLOH I SUB 125.

I VESSEL P 2 RELIEF V 3 BTPASS Vl ES RISE (PSI)

LVE FLOH V

F o

100.

4J I

h I

Ps 50.

0.0.

QO.

80.

120.

TIME (SEC) 160.

-25.0 QO.

80.

120.

TIME (SEC) 160.

150.

I LEVEL(I H-REF"SEP-SKIRT 2 VESSEL S EAMFLOH 3 TURBINE TEAHFLOH I VOID REA 2 OOPPLER 3 SCRAH AE TIVITY EACTIVITT CTIVITT CTIVITV 100.

th Vl I

W 0

LJ 0.

-1.

I 0.0.

80.

120.

TIME (SEC) 160.

0

)(0.

80.

120.

TINE (SEC) 160.

Figure 4.

Plant -Response to Loss of 100 Deg F Feedwater Heating

150.

I NEUTRON 2 AVE SURF 3 CO 9 CORE INL 5

LUX CE HEAT fLUX I FLOW I SUB 125.

1 VESSEL P 2 SAFETT V 3REI FV 0 BTPRSS V

5 6

ES RISE IPSI)

LVE FL%

V FOH LV LON o

100.

UJ I

I Pu 50.

g 0.0.

10.

20 0 30.

TINE (SEC) 40.

10.

20.

30.

TINE (SEC)

QO.

150.

I LEVEL(I

-REF-SEP-SKIRT 2 VESSEL S EAHFLOK 3 TURBINE TEAHFLOW 1 VOIO RE 2

OPPLER CRAH RE TIVIT ERG ITT CT ITT 100.

0.0.

10.

20.

30.

TINE ISEC) 40.

0 12.

TIRE (SEC) 18.

Figure 5.

Plant Response to Feedwater Controller Failure, Maximum Demand

Y1003J01A03 1

NOTES: lo ROD PATTERN IS 1/4 CORE MIRROR SYMMETRIC (FULL CORE SHOWN) 2.

NO.

INDICATES NUMBER OF NOTCHES WITHDRAWN OUT OF. 48.

BLANK IS A WITHDRAWN ROD 3.

ERROR ROD IS (26 ~ 35) 59 55 51 47 43 6

39 35 4

31 27 4

23 19 6

15ll v

7 3

10 36 0

36 10 36 2

6 10 14 18 22 26 6

4 36 36 6

6 2

36 36 36 6

14 36 36 36 2,

14 0

36 40 2

14 36 36 6

36 36 6

6 2

36 36 40 36 0

40 14 36 2.

36 14 36 10 36 36 4

36 36 36 36 30 34 38 42 46 4

6 36 36 36 2

~ 6 36 36 36 14 10 40 36 36 14 50 54 58 6

36 6

6 36 2

4 36 2

4 36 6

6 36 6

Figure 6.

Limiting RWE Rod Pattern 12

150.

1 NEUTRON 2 AVE SURF 3 CORE INL LUX CE HEAT FLUX T F OW 1

VESSEL P 2 SAFETT V 3 RELIEF V

0 BTPASS V

5 6

ES RISE (PSI)

LVE FLON LVE FLON LV ON r) 100.

I Pu 50.

100.

0.0 8.

12.

TIHE (SEC) 16.

0.0.

8.

12.

TIHE (SEC) 16.

I LEVEL(I H-REF-SEP-SKIRT 2 VESSEL S ERHFLON 3 TURBINE TEAHFLON 1 VOIO RER TIVIT 2 OGPPLER VITT 3 SCR CTIVITY 100.

0.

-100.

0 8.

12.

TINE (SEC) 16.

0.

0.6 1.2 1.8 TIHE (SEC)

2. (I Figure 7.

Plant Response to MSIV Closure

Y1003J01A03 1.2 1.0 ULTIMATESTABILITYLIMIT O

0,8 X

OI-K 0.6 NATURAL CIRCULATION 105% ROD LINE 0,4 0.2 0

0 40 60 PERCENT POWER 80 Figure 8.

Decay Ratio 14

Y1003J01A03 A CALCULATEDVALUE@OLD B

CALCULATEDVALUEWSB C

BOUNDINGVALUEFOR 280 eel/g, COLD D BOUNDINGVALUEFOR 280 eel/g, HSB xI-z0 e

zIII O

IL IL UI00L III 00

-10

-16

-20

-26

-30 0

1000

1600 2000

, FUEL TEMPERATURE tdeg C)

Figure 9.

Doppler Reactivity Coefficient Comparison for RDA

Y1003J01A03 A ACCIDENT FUNCTION B

BOUNDINGVALUEFOR 280 eel/II 15 10 0

0 10 ROD POSITION, feet OUT 15 20 Figure 10.

Accident Reactivity Shape Function at 20 C

Y1003JOlA03 20 A ACCIDENT FUNCTION B

BOUNDINGVALUEFOR &0csl/g, Z

I0Z 0XI-Y 10 0

b K

0 0

10 ROD POSITION, fest OUT 15 Figure 11.. Accident Reactivity Shape Function at 286'C 17

Y1003J01A03 60 A SCRAM FUNCTION B

BOUNDINGVALUE FOR 280 ceI/O 40 x

O D0 Ix 30 5C 0

E3 z

20 I-I-

O K

10 0

0 ELAPSED TIME,seconds Figurerl2.

Scram Reactivity Function at 20'C

Y1003J01A03 75 A SCRAM FUNCTION B

BOUNDING VALUEFOR 280 eel/g 50 25 0

0 3

4 ELAPSED TIME,seconds Figure 13.

Scram Reactivity Function at 286'C 19/20

I C

Y1003J01A03 APPENDIX A SHUTDOWN MARGIN DETERMINATION A.l BASES The reference loading pattern, documented in item 3 of this supplemental reload submittal, is the basis for, all reload licensing and operational planning and is comprised of the fuel bundles designated in item 2 of this supplemental submittal.

It in'urn is based on the best possible prediction of the core condition at the end of the present cycle and on the desired c'ore energy capability for the reload cycle.

It is designed with the intent k

that it will represent, as clos'ely as possible, the actual core loading pattern.

A.2 CORE CHARACTERISTICS The reference. core is analyzed in detail to ensure that adequate cold shutdown margin exists.

This section discusses the results of core calculations for shutdown margin.

A.2.1 Core Effective Multiplication and'Control Rod Worth Core effective multiplication and.control rod worths were calculated using the TVA BWR simulator. code (References A-l, A-3) in conjunction with the TVA lattice physics data generation code (References A-2, A-3) to determine the core reactivity with all rods withdrawn and with all rods inserted.

A tabulation of the results is provided in Table A.l.

These three eigenvalues (effective multi-plication of the core; uncontrolled, fully controlled, and with the strongest rod out) were calculated at the beginning-of-cycle 4 core average exposure corresponding to the minimum expected end-of-cycle 3 core average exposure.

The core was assumed to be in a xenon-free condition.

Y1003J01A03 Cold k ff was calculated with the strongest control rod out at various eff exposures through the cycle.

The value R is the difference between the strongest rod out k ff at BOC and the maximum calculated strongest rod out eff k ff at any exposure point.

The strongest rod out k ff at any exposure eff eff point is equal to or less than:

k

= (Fully controlled k

)

BOC + (Strongest Rod Worth)

BOC + R SRO eff eff A.2.2 Reactor Shutdown Margin Technical Specifications require that the refueled core must be capable of being made subcritical with 0.38 percent Ak margin in the most reactive condition throughout the subsequent operating cycle with the most reactive control rod in its full out position and all other rods fully inserted.

The shutdown margin is determined by using the BWR simulator code to calcu-late the core multiplication at selected'exposure points with the strongest rod fully withdrawn.

The shutdown margin for the reloaded core is obtained by subtracting the k given in Table A.l from the critical k of 1.0, SRO eff eff resulting in a calculated cold shutdown margin of 1.1 percent Ak.

A-2

Y1003JOlA03 Table A.'1 CALCULATED CORE EFFECTIVE MULTIPLICATIONAND CONTROL ROD WORTHS NO VOIDS, NO XENON, 20 C

Uncontrolled, K ff UNC eff Fully Controlled, KCON eff Strongest Control Rod Out, K ff SRO eff 1.120 0.955-0.989 R,

Maximum Increase in Cold Core Reactivity With Exposure Into Cycle, Ak 0.000 A-3

Y1003J01A03 REFERENCES A-l.

A-2.

A-3.

S. L. Forkner, G. H; Meriwether, and T. D. Beu, "Three-Dimensional LWR Core Simulation Methods," TVA-TR78-03A, 1978 B. L. Darnell, T. D. Beu, and G.

W. Perry, "Methods for the Lattice Physics Analysis of LWR's," TVA-TR78-02A, 1978 "Verification of TVA Steady-State BWR Physics Methods," TVA-TR79-01A, 1979 A-4

Y1003J01A03 APPENDIX B Fuel Loading Error LHGR :

Rotated Bundle, 16.9 kW/ft; Misplaced Bundle, 18.1 kW/ft Safety/Relief Valve Capacity at Setpoint (No./%):

10/63.6**

Spring Safety Valve Capacity at Setpoint (No./%):

2/14.2 Rated Steam Flow:

14.09 x 10 lb/hr 6

GETAB Analysis Initial Conditions Reactor Pressure:

1035 psia Inlet Enthalpy:

521.5 Btu/lb king penalty for densification is included.

one safety/relief vlave out of service.

B-1/B-2

N I

'E I

C 4 ~

I r

l

Y1003JOlA03 APPENDIX C MARGIN TO SPRING SAFETY VALVES The rationale for changing the basis for providing pressure margin to the

'pring safety valves is presented in Reference C-1.

This change has been h

accepted by the NRC (Reference C-2).

On this basis the plant can operate at full power throughout the cycle.

Y1003J01A03 REFERENCES C-l.

C-2.

J. F. Quirk (GE) letter to Olan D. Parr (NRC), "General Electric Licensing Topical Report NEDE-24011-P-A,

'Generic Reload Fuel Application,'ppendix D, Second Submittal," dated February 28, 1979.

Letter, T. A. Ippolito (NRC) to D. L. Peoples (Commonwealth Edison Co.)

enclosing a Safety Evaluation supporting Amendment No. 42 to Facility Operating License No. DPR-25.Dresden Nuclear Power Station Unit 3, dated April 16, 1980.

C-2