PNP 2014-054, Response to NRC Request for Additional Information - 10 CFR 50 Appendix G Equivalent Margin Analysis - Mf 2962: Difference between revisions

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=Text=
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{{#Wiki_filter:.-    J?.- #rijca
{{#Wiki_filter:Entergy Nuclear Operations, Inc.
~Entergy 1_il 1Lt7
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                  ,                                                  Palisades Nuclear Operations, Entergy Nuclear Palisades Nuclear Operations, Inc.
Palisades Nuclear Plant 1_il 1Lt7 27780 Blue Star Memorial Highway Covert, MI 49043-9530 Tel 269 764 2000 Anthony J. Vitale Site Vice President PNP 2014-054 June 12, 2014 U.S. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001
Nuclear Plant Plant Inc.
 
27780 Blue Star Memorial Highway MI 49043*9530 Covert, MI  49043-9530 Tel 269 764 2000 Anthony J. Vitale President Site Vice President PNP 2014-054 12, 2014 June 12,2014 u.s.
==SUBJECT:==
U.S. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001
Response to NRC Request for Additional Information
- Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis
 
ME 2962 Palisades Nuclear Plant Docket No. 50-255 License No. DPR-20
 
==REFERENCES:==
: 1. Palisades Nuclear Plant, Application for Renewed Operating License, dated March 22, 2005 (ADAMS Accession No. ML050940446).
2.
Entergy Nuclear Operations, Inc. letter PNP 2013-028, Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margins Analysis, dated October 21, 2013 (ADAMS Accession No. ML13295A448).
3.
NRC email to Entergy Nuclear Operations, Inc., Request for Additional Information
- Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis
- MF2962, dated May 13, 2014 (ADAMS Accession No. ML14133A684).
 
==Dear Sir or Madam:==
In the Palisades Nuclear Plant (PNP) license renewal application (Reference 1),
Nuclear Management Company (NMC), the former license holder for PNP, committed to submit an equivalent margins analysis (EMA) for Nuclear Regulatory Commission (NRC) approval at least three years before any reactor vessel beltline material Charpy upper-shelf energy (USE) decreases to less than 50 ft-lb, in accordance with 10 CFR 50 Appendix G, Section IV, Fracture Toughness Requirements.
Entergy Nuclear Operations, Inc. submitted the required EMA in Reference 2.
~Entergy Entergy Nuclear Operations, Inc.
Palisades Nuclear Plant 27780 Blue Star Memorial Highway Covert, MI 49043*9530 PNP 2014-054 June 12,2014 Tel 269 764 2000 Anthony J. Vitale Site Vice President u.s. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001  


==SUBJECT:==
==SUBJECT:==
Response to NRC Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis -
Response to NRC Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis -
ME 2962 MF Palisades Nuclear Plant Docket No. 50-255 License No. DPR-20
MF 2962 Palisades Nuclear Plant Docket No. 50-255 License No. DPR-20  


==REFERENCES:==
==REFERENCES:==
: 1. Palisades Nuclear Plant, Application for Renewed Operating License, dated March 22, 2005 (ADAMS Accession No. ML050940446).
: 1. Palisades Nuclear Plant, Application for Renewed Operating License, dated March 22, 2005 (ADAMS Accession No. ML050940446).
: 2. Entergy Nuclear Operations, Inc. letter PNP 2013-028, Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margins Analysis, dated October 21, 2013 (ADAMS Accession No. ML        ML113295A448).
: 2. Entergy Nuclear Operations, Inc. letter PNP 2013-028, Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margins Analysis, dated October 21, 2013 (ADAMS Accession No. ML13295A448).
3295A448).
: 3. NRC email to Entergy Nuclear Operations, Inc., Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis - MF 2962, dated May 13, 2014 (ADAMS Accession No. ML14133A684).  
: 3. NRC email to Entergy Nuclear Operations, Inc., Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis - MF2962,
                                                                  - MF 2962, dated May 13,  13, 2014 (ADAMS Accession No. ML14133A684).


==Dear Sir or Madam:==
==Dear Sir or Madam:==
In the Palisades Nuclear Plant (PNP) license renewal application (Reference 1),
Nuclear Management Company (NMC), the former license holder for PNP, committed to submit an equivalent margins analysis (EMA) for Nuclear Regulatory Commission (NRC) approval at least three years before any reactor vessel beltline material Charpy upper-shelf energy (USE) decreases to less than 50 ft-Ib, in accordance with 10 CFR 50 Appendix G, Section IV, "Fracture Toughness Requirements."
Entergy Nuclear Operations, Inc. submitted the required EMA in Reference 2.


In the Palisades Nuclear Plant (PNP) license renewal application (Reference 1),     1),
PLP 2014-054 Page 2 of 2 In Reference 3, ENO received a request for additional information (RAI) concerning the EMA submittal.
Nuclear Management Company (N      MC), the former license holder for PNP, committed (NMC),
The ENO response to RAI questions 1, 3, 4, 5, and 6 is provided in the attachment.
to submit an equivalent margins analysis (EMA) for Nuclear Regulatory Commission (NRC) approval at least three years before any reactor vessel beltline material Charpy upper-shelf energy (USE) decreases to less than 50 ft-lb, ft-Ib, in accordance with 10 10  CFR  50 Appendix G, Section IV, Fracture "Fracture Toughness Requirements.
The response to RAI question 2 will be provided at a later date, as agreed upon during a RAI clarification phone call between ENO and the NRC on June 6, 2014.
Requirements."
This letter contains no new commitments and no revised commitments.
Entergy Nuclear Nuclear Operations, Inc. submitted the required EMA in Reference 2.
I declare under penalty of perjury that the foregoing is true and correct; executed on June 12, 2014.
Sincerely, ajv/jse


PLP 2014-054 Page 2 of 2 concerning the In Reference 3, ENO received a request for additional information (RAI) conceming EMA submittal.
==Attachment:==
Response to NRC Request for Additional Information
- Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis
- ME 2962 cc:
Administrator, Region Ill, USNRC Project Manager, Palisades, USN RC Resident Inspector, Palisades, USN RC PLP 2014-054 Page 2 of 2 In Reference 3, ENO received a request for additional information (RAI) conceming the EMA submittal.
The ENO response to RAI questions 1, 3, 4, 5, and 6 is provided in the attachment.
The ENO response to RAI questions 1, 3, 4, 5, and 6 is provided in the attachment.
The response to RAI question 2 will be provided at a later date, as agreed upon during a RAI clarification phone call between ENO and the NRC on June 6, 2014.
The response to RAI question 2 will be provided at a later date, as agreed upon during a RAI clarification phone call between ENO and the NRC on June 6, 2014.
This letter contains no new commitments and no revised commitments.
This letter contains no new commitments and no revised commitments.
II declare under penalty of perjury that the foregoing is true and correct; executed on June 12, 2014.
I declare under penalty of perjury that the foregoing is true and correct; executed on June 12, 2014.
Sincerely, ajv/jse
Sincerely, ajv/jse  


==Attachment:==
==Attachment:==
Response to NRC Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis - MF
Response to NRC Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis - MF 2962 cc:
                                                                          - ME 2962 cc:     Administrator, Region III, Ill, USNRC USN RC Project Manager, Palisades, USNRC USN RC Resident Inspector, Palisades, USNRC
Administrator, Region III, USNRC Project Manager, Palisades, USNRC Resident Inspector, Palisades, USNRC  


ATTACHMENT ATTACHMENT RESPONSE TO RESPONSE       TO NRC NRC REQUEST REQUEST FOR   FOR ADDITIONAL ADDITIONAL INFORMATION INFORMATION -  -
ATTACHMENT RESPONSE TO NRC REQUEST FOR ADDITIONAL INFORMATION -
PALISADES NUCLEAR PALISADES      NUCLEAR PLANT PLANT 10    CFR 50 10 CFR       APPENDIX G 50 APPENDIX     G EQUIVALENT MARGIN EQUIVALENT        MARGIN ANAL ANALYSIS VSIS - MF
PALISADES NUCLEAR PLANT 10 CFR 50 APPENDIX G EQUIVALENT MARGIN ANALYSIS - MF 2962 A follow-up request for additional information (RAI) was received from the Nuclear Regulatory Commission (NRC), by electronic mail on May 13, 2014. The RAI requested that the response to the RAI be docketed within 30 days of receipt of the request.
                                                                      - MF 2962 2962 request for additional A follow-up request         additional information information (RAI)
The Entergy Nuclear Operations, Inc. (ENO) Palisades Nuclear Plant (PNP) response to the RAI is provided below.
(RAI) was received received from the Nuclear Nuclear Regulatory Regulatory   Commission     (NRC), by electronic (NRC),       electronic mail on May 13, 13, 2014.
NRC Request (May 13, 2014) 1.
2014. The The RAI RAI requested requested that the response that      response to the RAI be  be docketed within 30 days of receipt of the request.
The EMA is based on American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code (Code) Section Xl, Appendix K as supplemented by Regulatory Guide (AG) 1.161 Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 Ft-Lb ASME Code Section Xl, Appendix K, Article K-4210 and RG 1.161 both include equations for calculating the stress intensity factor due to radial thermal gradients. In Section 5.1 of the EMA submittal, the licensee discusses through-wall thermal stress and states that typical through-wall stress and stress distribution during a heatup transient are shown in Figures 5-1 and 5-2. But Figures 5-1 and 5-2 of the EMA submittal do not show these stresses as discussed. Provide figures showing typical through-wall stress and stress distributions during a heatup transient to support the discussion in paragraph 5.1 of the EMA submittal.
request.
ENO Response to RAI-1 Figures detailing typical heatup thermal axial stress and typical through-wall axial stress for the PNP reactor vessel used in the equivalent margins analysis (EMA) submittal are provided below.
The Entergy Nuclear Operations, Inc. (ENO) Palisades Nuclear Plant (PNP) response to the The RAI is provided below.
1 of 12 ATTACHMENT RESPONSE TO NRC REQUEST FOR ADDITIONAL INFORMATION -
PALISADES NUCLEAR PLANT 10 CFR 50 APPENDIX G EQUIVALENT MARGIN ANAL VSIS - MF 2962 A follow-up request for additional information (RAI) was received from the Nuclear Regulatory Commission (NRC), by electronic mail on May 13, 2014. The RAI requested that the response to the RAI be docketed within 30 days of receipt of the request.
The Entergy Nuclear Operations, Inc. (ENO) Palisades Nuclear Plant (PNP) response to the RAI is provided below.
NRC Request (May 13, 2014)
NRC Request (May 13, 2014)
: 1. The EMA is based on American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code (Code) Section XI,        Xl, Appendix KK as supplemented supplemented by Regulatory Guide (RG)
: 1.
(AG) 1.1.161  Evaluation 161 "Evaluation   of Reactor   Pressure Vessels with Charpy Upper-Shelf Ft-Lb ASME Code Section XI, Energy Less Than 50 Ft-Lb".                                 Xl, Appendix K, Article K-4210 and RG 1.161 both include equations for calculating the stress intensity factor due to radial thermal gradients. In Section 5. 5.11 of the EMA submittal, the licensee discusses through-wall thermal stress and states that typical through-wall stress and stress distribution during a heatup transient are shown in Figures 5-1 and 5-2. But Figures 5-1 and 5-2 5..2 of the EMA submittal do not show these stresses as discussed. Provide figures showing typical through-wall stress and stress distributions during a heatup transient to support the discussion in paragraph 5.1    5. 1 of the EMA submittal.
The EMA is based on American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code (Code) Section XI, Appendix K as supplemented by Regulatory Guide (RG) 1. 161 "Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 Ft-Lb". ASME Code Section XI, Appendix K, Article K-4210 and RG 1.161 both include equations for calculating the stress intensity factor due to radial thermal gradients. In Section 5. 1 of the EMA submittal, the licensee discusses through-wall thermal stress and states that typical through-wall stress and stress distribution during a heatup transient are shown in Figures 5-1 and 5-2. But Figures 5-1 and 5.. 2 of the EMA submittal do not show these stresses as discussed. Provide figures showing typical through-wall stress and stress distributions during a heatup transient to support the discussion in paragraph 5. 1 of the EMA submittal.
ENO ENO Response Response to  to RAI-1 Figures detailing detailing typical heatup thermal axial stress and typical through-wall axial stress stress for the PNP reactor vessel used  used in the equivalent equivalent margins margins analysis analysis (EMA) submittal submittal are are provided provided below.
ENO Response to RAI-1 Figures detailing typical heatup thermal axial stress and typical through-wall axial stress for the PNP reactor vessel used in the equivalent margins analysis (EMA) submittal are provided below.
below.
1 of 12  
11 of of 12 12


10 10 Heatup Ir~nJ~J~!'t
10 Heatup Transient Thermal Stress - Sxx vs Time ID Midwall 5E 0
___~I_ H~aJ~p                  Thermal $t!_~SS Transient l11~r.!ltal Stress- S~
1 2
                                                                  - Sxx ~~~
3 4
vs 11m~
5 6
Time
7 8
                                    ---ir
U, U,
                                                                                      -ID
I U,-5
                                                                                        ' 10 I        I            I
[-
                                                                                      -Midwall
-10
                                                                                        . Midwall
-15 Time (hr)
                                                                                      - j OD 55E o0                                                                                      -
Figure 5-1 (a)
1        2          3          4          5         6          7        8 U,
PNP Typical Thermal Transient Axial Stress Profile Stress versus Time 2 of 12 10  
U,      I U,
~I _H~aJ~p Ir~nJ~J~!'t l11~r.!ltal $t!_~SS - S~ ~~~ 11m~
    -5      [-
I I
1
I
      -10
' 10  
    -10                                  -- - -
. Midwall j
      -15
OD 5  
    -15 Time (hr)
---ir o
Time  (hr)
1  
Figure 5-1 Figure   5-1(a)(a) - PNP PNP Typical Typical Thermal Thermal Transient Transient Axial Axial Stress Stress Profile Profile - Stress versus Time Stress versus  Time 22 of 12 of 12
-10 1--- --
-15 Time (hr)
Figure 5-1 (a) - PNP Typical Thermal Transient Axial Stress Profile - Stress versus Time 2 of 12  


r                -,
Heatup Transient Thermal Stress - Sxx vs. x/t 10 5
Heatup Transient Thermal Stress - Sxx vs. x/t 10 10 I
0 U,.
r
Ll
                                                                          . ----r-l I
-5
5
-10
                                                        -~
-15 Figure 5-2(a) - PNP Typical Thermal Transient Axial Through-Wall Stress Distribution NRC Request (May 13, 2014) 2.
U, o
Section 5.1 states, Only circumferential base metal flaws are considered in this analysis, because only the weak orientation USE is projected to drop below 50 ft-lbs as described below. Please demonstrate that assuming a circumferential flaw in the base metal with the weak Charpy V-Notch (CVN) value in the EMA is more limiting than assuming an axial flaw in the base metal with the strong CVN value. Please note that the significantly greater applied J integral associated with the axial flaw may challenge the fundamental assumption in the EMA submittal.
0 0      0.1     0.2     0,3
ENO Response to RAI-2 Based on discussions between ENO and the NRC during a June 6, 2014 RAI conference call, the response to this RAI question will be provided at a later date, as agreed upon during the call.
                                                      ---------- ----r ------ --- -
0 0.1 0.2 0,3 06 0.7 08 09
0!5       0.6 06
------------H I Transient Time (sec)I 6300 12600 15700 30300 Distance Ratio x/t 3 of 12 Heatup Transient Thermal Stress - Sxx vs. x/t 10 r
                                                                          ~
5 o
0.7 Or7     0.8 08        0.9 09        1 Ll
-10
        -5                                                                      I
-15 r
                                                                          ----,:-----+-
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                                                                      ~-
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                                                                                    ------------H
---------- ~ ----r ------ ----
      -10
0!5 0.6 Or7 0.8 0.9 1
__________0-.1I Trarisient                   (sec)I Transient Time (sec)1
I  
                                                                                    - - 6300
~- ----,:-----+-
                                                                                    - - 12600
__________ 0-.1 Trarisient Time (sec)1  
:          -    15700 I
-- 6300  
                                                                  , _ _ --1-__
-- 12600 15700 I  
                                                                                    -30300
- - - 30300
                                                                                        - - 30300
--1-__
      -15 Distance Ratio x/t Figure 5-2(a) - PNP Typical Thermal Transient Axial Through-Wall Stress Distribution NRC Request (May 13, 2014)
Distance Ratio x/t Figure 5-2(a) - PNP Typical Thermal Transient Axial Through-Wall Stress Distribution NRC Request (May 13, 2014)
: 2.     Section 5.
: 2.
5.11 states, "0nly Only circumferential base metal flaws are considered in this analysis, because only the "weak"weak orientation USE is projected to drop below 50      50 ft-lbs ft-Ibs below. Please demonstrate that assuming a circumferential flaw in the as described below."
Section 5. 1 states, "0nly circumferential base metal flaws are considered in this analysis, because only the "weak" orientation USE is projected to drop below 50 ft-Ibs as described below." Please demonstrate that assuming a circumferential flaw in the base metal with the weak Charpy V-Notch (CVN) value in the EMA is more limiting than assuming an axial flaw in the base metal with the strong CVN value. Please note that the significantly greater applied J integral associated with the axial flaw may challenge the fundamental assumption in the EMA submittal.
base metal with the weak Charpy V-Notch (CVN) value in the EMA is more limiting than assuming an axial flaw in the base metal with the strong CVN value. Please note that the significantly greater applied J integral associated with the axial flaw may challenge the fundamental assumption in the EMA submittal.
ENO Response to RAI-2 Based on discussions between ENO and the NRC during a June 6, 2014 RAI conference call, the response to this RAI question will be provided at a later date, as agreed upon during the call.
ENO Response to RAI-2 Based on discussions between ENO and the NRC        NRC during a June 6, 2014 RAI conference call, the response to this RAI question will be provided at a later date, as agreed upon during the call.
3 of 12  
33 of 12 12


NRC Request NRC    Request (May (May 13, 13, 2014) 2014) 3.
NRC Request (May 13, 2014) 3.
: 3. The applied The   applied J-integral J-integral values values for for the   circumferential flaws the circumferential      flaws forfor all  Level AA and all Level       and BB service service level conditions level  conditions are     shown in are shown       in Figure Figure 5-1, 5-1, and and the the applied applied J-integral J-integral values values forfor the the circumferential flaws circumferential    flaws for for Level Level C     and D C and    D service service level level conditions conditions are   are shown shown in in Figure Figure 5-2. Since Section 5-2. Since    Section 5. provides very 5.11 provides     very limited limited information information regarding regarding the  the applied applied J-integral calculations, J-integral    calculations, please please confirm confirm thatthat the the calculations calculations underlying           Figures 5-1 underlying Figures          5-7 and and 5-2   are based 5-2 are  based onon the the formulas formulas in  in RG RG 1.161, 1.761, uEvaluation REvaluation of of Reactor Reactor Pressure Pressure Vessels Vessels with Charpy with  Charpy Upper-Shelf Upper-Shelf Energy Less Than          Than 50    FT-LB. If 50 FT-LB."     If not, not, please please describe, describe, in addition to your response addition            response to  to RAI-1, RAt- 1, your plant-specific plant-specific calculations calculations to   to support support their their acceptance in this application.
The applied J-integral values for the circumferential flaws for all Level A and B service level conditions are shown in Figure 5-1, and the applied J-integral values for the circumferential flaws for Level C and D service level conditions are shown in Figure 5-2. Since Section 5.1 provides very limited information regarding the applied J-integral calculations, please confirm that the calculations underlying Figures 5-7 and 5-2 are based on the formulas in RG 1.761, REvaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 FT-LB. If not, please describe, in addition to your response to RAt-1, your plant-specific calculations to support their acceptance in this application.
ENO Response to RAI-3 Yes, the applied J-integral calculations underlying Figures 5-1 and 5-2 are based on formulas in RG 1.161.1.161.
ENO Response to RAI-3 Yes, the applied J-integral calculations underlying Figures 5-1 and 5-2 are based on formulas in RG 1.161.
NRC Request (May 13, 2014) 4.
Table 4-4 was presented but without being mentioned in Section 4 regarding how it was used in the EMA analysis. Therefore, please confirm that the calculated available margins presented in Table 5-3 for various time during coo/down are results, using the relevant J-R curves adjusted by the material margin factors of Table 4-4.
ENO Response to RAI-4 As discussed in Section 2.2 of WCAP-17651-NP, Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis, Revision 0, RG 1.161 material margin factors (ME) in Table 4-4 were used for the J-R curves.
NRC Request (May 13, 2014)
: 5. Section 5.2 provides justification for using the high-toughness/low-sulfur model from RG 1.161 in the proposed EMA for the high-sulfur plates, and Section 5.3 provides the corresponding EMA results. When the high-sulfur model (e.g., for the 6T specimen) of NUREG/CR-5265, Size Effects on J-R Curves for A 302-B Plate, is used, please demonstrate that The updated safety factors (see Table 5-3), after adjusting for temperature, will still be greater than 1.15.
The updated applied J/J-R curves (see figures 5-8, 5-9, and 5-12), after adjusting for temperature, will still show that dJappjjeci/da <dJmaterja/da at Japplied = Jmateriai 4 of 12 NRC Request (May 13, 2014)
: 3.
The applied J-integral values for the circumferential flaws for all Level A and B service level conditions are shown in Figure 5-1, and the applied J-integral values for the circumferential flaws for Level C and D service level conditions are shown in Figure 5-2. Since Section 5. 1 provides very limited information regarding the applied J-integral calculations, please confirm that the calculations underlying Figures 5-1 and 5-2 are based on the formulas in RG 1.161, uEvaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 FT-LB." If not, please describe, in addition to your response to RAI-1, your plant-specific calculations to support their acceptance in this application.
ENO Response to RAI-3 Yes, the applied J-integral calculations underlying Figures 5-1 and 5-2 are based on formulas in RG 1.161.
NRC Request (May 13, 2014)
: 4. Table 4-4 was presented but without being mentioned in Section 4 regarding how it was used in the EMA analysis. Therefore, please confirm that the calculated available margins presented in Table 5-3 for various time during cooldown are results, using the relevant J-R curves adjusted by the material margin factors of Table 4-4.
ENO Response to RAI-4 As discussed in Section 2.2 of WCAP-17651-NP, "Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis," Revision 0, RG 1.161 material margin factors (MF) in Table 4-4 were used for the J-R curves.
NRC Request (May 13, 2014)
NRC Request (May 13, 2014)
: 4. Table 4-4 was presented but without being mentioned in Section 4 regarding how it was 4.
: 5. Section 5.2 provides justification for using the high-toughness/low-sulfur model from RG 1.161 in the proposed EMA for the high-sulfur plates, and Section 5.3 provides the corresponding EMA results. When the high-sulfur model (e.g., for the 6Tspecimen) of NUREG/CR-5265, uSize Effects on J-R Curves for A 302-8 Plate," is used, please demonstrate that The updated safety factors (see Table 5-3), after adjusting for temperature, will still be greater than 1. 15.
used in the EMA analysis. Therefore, please confirm that the calculated available margins presented in Table 5-3 for various time during coo/down            cooldown are results, using the relevant J-R curves adjusted by the material margin factors of Table 4-4.
The updated applied J/J-R curves (see figures 5-8, 5-9, and 5-12), after adjusting for temperature, will still show that dJappliecida < dJmaterialda at Japplied = Jmaterial.
ENO Response to RAI-4 As discussed discussed in Section 2.2 of WCAP-1765WCAP-17651-NP,    1-NP, Palisades "Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis,    Analysis," Revision 0, RG 1.161      1.161 material margin factors (ME)
4 of 12  
(MF) in Table 4-4 4-4 were used for the J-R curves.
NRC Request (May 13,      13, 2014) 2014)
: 5. Section
: 5. Section 5.2 5.2 provides provides justification justification for using using thethe high-toughne      ss/low-sulfur model high-toughness/low-sulfur             model from RG  RG 1.161 1.161 in the proposed proposed EMA EMA for the high-sulfur high-sulfur plates, plates, and and Section Section 5.3  5.3 provides the the correspondin corresponding     g EMA EMA results.
results. WhenWhen the the high-sulfur high-sulfur model model (e.g.,
(e.g., for for the the 6T6Tspecimen) specimen) of   of NUREG/CR NUREG/CR-5265, -5265, Size uSize Effects Effects on on J-R Curves for A       A 302-B 302-8 Plate, Plate," is used, used, please please demonstrate demonstrate that  that
            **  The The updated updated safety safety factors factors (see (see Table     5-3), after Table 5-3),    after adjusting adjusting for for temperature, temperature, will will still still be be greater greater than than 1.15.
: 1. 15.
            **  The The updated updated applied applied J/J-R J/J-R curves curves (see (see figures   5-8, 5-9, figures 5-8,    5-9, and     5-12), after and 5-12),      after adjusting adjusting for  temperature, for temperature, will will still still show show thatthat dJappjjeci/da dJappliecida <dJmaterja/d
                                                                              < dJmaterialda a atat Japplied Japplied == Jmateriai Jmaterial.
of 12 44 of  12


If the If  the above above cannot cannot be     demonstrated, perform be demonstrated,        perform aa sensitivity sensitivity study, study, showing showing at      what at what percentage of    of the the proposed J-R       cuive (e.g.,
If the above cannot be demonstrated, perform a sensitivity study, showing at what percentage of the proposed J-R cuive (e.g., 90%), your EMA calculation results will meet the criteria on both crack extension and stability.
J-R curve    (e.g., 90%),
: 6. Section 6 presents conclusions of this submittal. For Service Level C condition with 400&deg;F/hr cooldown, it is concluded that, The equivalent margins analyses for the plate materials are acceptable and bounded by the conservative test data reported in NUREG/CR-5265 in all cases for the Level C transient. This conclusion was repeated later for Service Level D condition with 600&deg;F/hr cooldown, with C in the quote replaced by D. Plot the relevant NUREG/CR 5265 6T data in Figure 5-12 and provide sufficientjustification to support your conclusions.
90%), your EMA EMA calculation calculation results results will will meet the criteria on both both crack crack extension extension and stability.
stability.
Section 6 presents conclusions
: 6. Section                    conclusions of this this submittal. For Service Service Level C condition condition with 400&deg;F/hr 400&deg;Flhr    cooldown,     it is concluded   that,   The "The equivalent margins analyses for          for the plate materials are acceptable and bounded by              by the conservative test data reported in NUREG/CR-5265 in all cases for the Level C transient."
NUREGICR-5265                                                transient. This This conclusion was  was repeated later for Service Level D condition with     with 600&deg;Flhr 600&deg;F/hr cooldown, with IIC"      C in the quote replaced by liD."D. Plot the relevant NUREGICR NUREG/CR 5265 6T data in Figure 5-12 and provide sufficient justification to support your conclusions.
ENO Responses to RAI-5 and RAI-6 Updated Figures 5-9 and 5-12 with the V-50 plate data are provided below, along with added Tables 5-4 and 5-5 showing the Level C and D safety factors, respectively.
ENO Responses to RAI-5 and RAI-6 Updated Figures 5-9 and 5-12 with the V-50 plate data are provided below, along with added Tables 5-4 and 5-5 showing the Level C and D safety factors, respectively.
Table 5-6 was added, which demonstrates the available margins on pressure loading with the V-50 plate data, adjusted for temperature, with consideration of all service loadings, Level A, B, C and D. The minimum safety factor (SF) with consideration of V-SO plate data and the PNP-specific J-applied values is 1.5, which is above the the V-50 minimum required SF of 1.15 per RG 1.161.
Table 5-6 was added, which demonstrates the available margins on pressure loading with the V-50 plate data, adjusted for temperature, with consideration of all service loadings, Level A, B, C and D. The minimum safety factor (SF) with consideration of the V-SO plate data and the PNP-specific J-applied values is 1.5, which is above the minimum required SF of 1.15 per RG 1.161.
Figure 5-8 from WCAP-1           7651-NP, Revision 0, along with the updated Figures 5-9 and WCAP-17651-NP, 5-1 2 below, all demonstrate that at Japplied 5-12                                            Japplied == Jmaterial, Jmaterial, dJapplieJd      dJmateriai/da, is satisfied dJapplied/daa < dJmateria~da, for all three cases (i.e., the slope of the Japplied  Japplied is smaller than the Jmaterial Jmaterial at the point of intersection).
Figure 5-8 from WCAP-1 7651-NP, Revision 0, along with the updated Figures 5-9 and 5-1 2 below, all demonstrate that at Japplied = Jmaterial, dJapplied/da < dJmateriai/da, is satisfied for all three cases (i.e., the slope of the Japplied is smaller than the Jmaterial at the point of intersection).
intersection) .
Therefore, as demonstrated below and in WCAP-1 7651-NP, the equivalent margins of safety per ASME Code Section Xl (References 4 and 5) are found to be acceptable for the PNP reactor vessel beltline and extended beltline regions with predicted Charpy upper-shelf energy levels falling below the 50 ft-lb 10 CFR 50, Appendix G requirements at end-of-license-extension.
Therefore, as demonstrated below and in WCAP-1                       7651-NP, the equivalent margins of WCAP-17651-NP, safety per ASME Code Section Xl           XI (References 4 and 5) are found to be acceptable for the PNP reactor vessel beltline and extended beltline regions with predicted Charpy upper-shelf energy levels falling below the 50 ft-lb         ft-Ib 10 10 CFR 50, Appendix G        G requirements at end-of-license-extension.
Westinghouse discovered during the development of this RAI response that the Level C and D loading J-applied curves plotted in WCAP-1 7651-NP, Figure 5-12, were not the most limiting case. This error also propagated onto Figures 5-2 and 5-13 in the WCAP.
end-of-license-extension.
This has been updated in the attached figures as part of this RAI response. Note that the conclusions to the report, including the safety factor determination, are unchanged; only the figures were in error. This has been documented in the Westinghouse corrective action system, and will be corrected when the WCAP is revised to incorporate these RAI changes.
Westinghouse discovered during the development of this RAI response that the Level C and D loading J-applied curves plotted in        in WCAP-1       7651-NP, Figure 5-12, were not WCAP-17651-NP,                                    not the most limiting      case. This limiting case. This error also propagated onto Figures        Figures 5-2 5-2 and 5-13 in    in the WCAP.
Lastly, note that the Level C and D margin tables (Tables 5-4 and 5-5 below) were originally omitted from WCAP-1 7651-NP because Service Level A and B, as discussed in Section 5.3 of WCAP-1 7651-NP, are the governing transients.
This has been updated in the attached figures as part of                  of this RAI response. Note    Note that the conclusions to the report, including including the safety factor determination, are unchanged;    unchanged; only the figures were were in in error.
5 of 12 If the above cannot be demonstrated, perform a sensitivity study, showing at what percentage of the proposed J-R curve (e.g., 90%), your EMA calculation results will meet the criteria on both crack extension and stability.
error. This This has has been documented documented in    in the the Westinghouse corrective action action system, system, and and will be be corrected corrected whenwhen the WCAP is      is revised revised to to incorporate incorporate these these RAIRAI changes.
: 6. Section 6 presents conclusions of this submittal. For Service Level C condition with 400&deg;Flhr cooldown, it is concluded that, "The equivalent margins analyses for the plate materials are acceptable and bounded by the conservative test data reported in NUREGICR-5265 in all cases for the Level C transient." This conclusion was repeated later for Service Level D condition with 600&deg;Flhr cooldown, with IIC" in the quote replaced by liD." Plot the relevant NUREGICR 5265 6T data in Figure 5-12 and provide sufficient justification to support your conclusions.
Lastly, Lastly, note note that that the the Level Level C    and D C and   D margin margin tables tables (Tables (Tables 5-4 5-4 and     5-5 below) and 5-5  below) werewere originally originally omitted omitted from from WCAP-1       7651-NP because WCAP-17651-NP                       Service Level because Service       Level A A and and B,B, as as discussed discussed in in Section     5.3 of Section 5.3    of WCAP-1      7651-NP, are WCAP-17651-NP,                 the governing are the   governing transients.
ENO Responses to RAI-5 and RAI-6 Updated Figures 5-9 and 5-12 with the V-50 plate data are provided below, along with added Tables 5-4 and 5-5 showing the Level C and D safety factors, respectively.
transients.
Table 5-6 was added, which demonstrates the available margins on pressure loading with the V-50 plate data, adjusted for temperature, with consideration of all service loadings, Level A, B, C and D. The minimum safety factor (SF) with consideration of the V-50 plate data and the PNP-specific J-applied values is 1.5, which is above the minimum required SF of 1.15 per RG 1.161.
55 of of 12 12
Figure 5-8 from WCAP-17651-NP, Revision 0, along with the updated Figures 5-9 and 5-12 below, all demonstrate that at Japplied = Jmaterial, dJapplieJda < dJmateria~da, is satisfied for all three cases (i.e., the slope of the Japplied is smaller than the Jmaterial at the point of intersection).
Therefore, as demonstrated below and in WCAP-17651-NP, the equivalent margins of safety per ASME Code Section XI (References 4 and 5) are found to be acceptable for the PNP reactor vessel beltline and extended beltline regions with predicted Charpy upper-shelf energy levels falling below the 50 ft-Ib 10 CFR 50, Appendix G requirements at end-of-license-extension.
Westinghouse discovered during the development of this RAI response that the Level C and D loading J-applied curves plotted in WCAP-17651-NP, Figure 5-12, were not the most limiting case. This error also propagated onto Figures 5-2 and 5-13 in the WCAP.
This has been updated in the attached figures as part of this RAI response. Note that the conclusions to the report, including the safety factor determination, are unchanged; only the figures were in error. This has been documented in the Westinghouse corrective action system, and will be corrected when the WCAP is revised to incorporate these RAI changes.
Lastly, note that the Level C and D margin tables (Tables 5-4 and 5-5 below) were originally omitted from WCAP-17651-NP because Service Level A and B, as discussed in Section 5.3 of WCAP-17651-NP, are the governing transients.
5 of 12  


Table 5-4   Available Margins 5-4 Available  Margins on  on Pressure Pressure Load   Load for for Level Level C, C, 400&deg;F/hr 400&deg;F/hr Cooldown Cooldown Base Material Base    Material                                        Material Weld Material Weld Circumferential Flaw Flaw                      Circumferential Flaw Circumferential     Flaw JJo.
Table 5-4 Available Margins on Pressure Load for Level C, 400&deg;F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw Jo.
1O*1                                             JJo.
1 Jo.
1 O*1 Time Time          SF SF    J-applied xx SF J-applied             material material        SF SF     J-applied xx SF J-applied     SF         material material (sec)
1 Time SF J-applied x SF material SF J-applied x SF material (sec)
(sec)                )
(in-lb/in 2
2 (in-lb/in (in-lb/in2)      )
)
2 (in-lb/in (in-lb/in2)                 )
(in-lb/in 2
2 (in-lb/in (in-lb/in2)           (in-lb/in2)
)
                                                                                            )
(in-lb/in 2
2 (in-lb/in 0         5.8     682                 682           5.2       511                 510 1,197       8.6     885                 839           7.1       613                 613 4,122       8.9     1,535 1,535               1,534         7.1       1,050               1,050 Minimum SF     5.8                                         5.2 Table 5-5 Available Margins on Pressure Load for Level D, 600&deg;F/hr Cooldown Base Material                                 Weld Material Circumferential Flaw                           Circumferential Flaw JJo.
)
1O*1                                       JJo.
(in-lb/in 2
1 O*1 Time         SF     J-applied x SF         material       SF     J-applied x SF       material (sec)                    )
)
2 (in-lb/in (in-lb/in2)      )
0 5.8 682 682 5.2 511 510 1,197 8.6 885 839 7.1 613 613 4,122 8.9 1,535 1,534 7.1 1,050 1,050 Minimum SF 5.8 5.2 Table 5-5 Available Margins on Pressure Load for Level D, 600&deg;F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw Jo.
2 (in-lb/in (in-lb/in2)                  )
1 Jo.
2 (in-lb/in (in-lb/in2)       (in-lb/in2)
1 Time SF J-applied x SF material SF J-applied x SF material (sec)
                                                                                              )
(in-lb/in 2
2 (in-lb/in 0         5.8           682               682         5.2       510                 510 798         8.1           830               830         6.9       607                 607 2,748         7.0           1,491             1,491         5.2       1,023               1,023 Minimum SF       5.8                                           5.2 66 of of 1212
)
(in-lb/in 2
)
(in-lb/in 2
)
(in-lb/in 2
)
0 5.8 682 682 5.2 510 510 798 8.1 830 830 6.9 607 607 2,748 7.0 1,491 1,491 5.2 1,023 1,023 Minimum SF 5.8 5.2 6 of 12 Table 5-4 Available Margins on Pressure Load for Level C, 400&deg;F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw JO*1 JO*1 Time SF J-applied x SF material SF J-applied x SF material (sec)
(in-lb/in2)
(in-lb/in2)
(in-lb/in2)
(in-lb/in2) 0 5.8 682 682 5.2 511 510 1,197 8.6 885 839 7.1 613 613 4,122 8.9 1,535 1,534 7.1 1,050 1,050 Minimum SF 5.8 5.2 Table 5-5 Available Margins on Pressure Load for Level D, 600&deg;F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw JO*1 JO*1 Time SF J-applied x SF material SF J-applied x SF material (sec)
(in-lb/in2)
(in-lb/in2)
(in-lb/in2)
(in-lb/in2) 0 5.8 682 682 5.2 510 510 798 8.1 830 830 6.9 607 607 2,748 7.0 1,491 1,491 5.2 1,023 1,023 Minimum SF 5.8 5.2 6 of 12


Table 5-6: Available Margins Table                Margins on Pressure Pressure Load Load for All Transients, Transients, Levels Levels A, B, B, C C andand 0, D, with Consideration Consideration of V-50 V-50 Plate Plate Data Data Plate V-50 Plate                                              Plate V-50 Plate                                       V-50 Plate Plate Level A Circumferential                 Level C LevelC        Circumferential                         Level 0D Level        Circumferential and B                                 JJ 0O1*1                                            JJ 0O1.1 Flaw                                             Flaw                                               Flaw                 JO*1 material                                         material J-applied                                       J-applied                                         J-applied         material Time                                 (in-       Time                                   (in-         Time                                       2 SF           SF xSF                                SF          xSF                                    SF        xSF x SF         (in-lblin
Table 5-6: Available Margins on Pressure Load for All Transients, Levels A, B, C and D, with Consideration of V-50 Plate Data V-50 Plate V-50 Plate V-50 Plate Level A Circumferential Level C Circumferential Level D Circumferential and B J
                                                                                                                                          ))
01 J
2 (in-lb/in (sec)                        2     Iblin 2)
01 Flaw Flaw Flaw material material J-applied J-applied J-applied material Time SF SF (in-Time (in-Time SF x SF (in-lb/in 2
                                      )
)
2 lb/in       (sec)                         2       Iblin
SF xSF (sec)
                                                                                          )}
(in-lb/in 2
2 lb/in 2
)
(sec)                     2
lb/in 2
                      )
)
2 (in-lb/in (in-lblin  )                                   )
(sec)
2 (in-lb/in (in-lblin  )                                     (in-lblin
(in-lb/in 2
                                                                                                                          ))
)
2 (in-lb/in 0       1.8         397           397         0       3.4         397             397             0       3.4       397              397 397 2800     1.6         441         441       1,197     4.7         488             488           798     4.7       483              483 483 3600       1.6         459         459       4,122     1.9         893             893           2,748     1.5       868             868 5400     1.7         503           503 7200       1.8         554           554 9000     1.9         611           611 10800 10800      18.0         675           675 I Minimum SF 1.6 1.6                               [ Minimum SF 1.9 1.9 Minimum 1.5 SF                                                   SF 77 of  12 of 12
lb/in 2
)
(sec)
(in-lb/in 2
)
0 1.8 397 397 0
3.4 397 397 0
3.4 397 397 2800 1.6 441 441 1,197 4.7 488 488 798 4.7 483 483 3600 1.6 459 459 4,122 1.9 893 893 2,748 1.5 868 868 5400 1.7 503 503 7200 1.8 554 554 9000 1.9 611 611 10800 18.0 675 675 I
Minimum
[ Minimum Minimum SF 1.6 SF 1.9 SF 1.5 7 of 12 Table 5-6: Available Margins on Pressure Load for All Transients, Levels A, B, C and 0, with Consideration of V-50 Plate Data Level A V-50 Plate V-50 Plate V-50 Plate and B Circumferential JO*1 LevelC Circumferential JO.1 Level 0 Circumferential Flaw material Flaw material Flaw JO*1 Time J-applied (in-Time J-applied (in-Time J-applied material (sec)
SF xSF Iblin2)
(sec)
SF xSF Iblin2}
(sec)
SF xSF (in-lblin2)
(in-lblin2)
(in-lblin2)
(in-lblin2) 0 1.8 397 397 0
3.4 397 397 0
3.4 397 397 2800 1.6 441 441 1,197 4.7 488 488 798 4.7 483 483 3600 1.6 459 459 4,122 1.9 893 893 2,748 1.5 868 868 5400 1.7 503 503 7200 1.8 554 554 9000 1.9 611 611 10800 18.0 675 675 Minimum 1.6 Minimum 1.9 Minimum 1.5 SF SF SF 7 of 12  


Applied J-Integral Applied    J-lntegral Curve Curve - Circumferential
Applied J-lntegral Curve - Circumferential Flaw, Level C & D, a = lIlOt, SF=1 400 Load LeveIC
                                                        - Circumferential Flaw, Flaw, Level Level C         D, aa =
 
C && D,      lIlOt, SF=1
Load LevelD 300 C\\4 100 0
                                                                                                            = 1/10t, SF=1 400 400    -
0.8 0.9 1
                    -Load     LeveIC
1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)
                        - Load Level  C
WCAP-1 7651-NP, Revision 0, Updated Figure 5-2 with Corrected, Limiting, Level C and 0 Transients 8 of 12 f::j  
                    - - -Load LevelD Load level 0                                                                     -_ .. ----------
< c:  
300 f::j C\4 c:
.Q  
.Q
~
~
e Ie) 200                                                                                                                  ,--~
e Ie)  
~
~
:J; 100 100  ~ ---------------------------------------------------------------
:J; Applied J-Integral Curve - Circumferential Flaw, Level C & D, a = 1/10t, SF=1 400
0o                                                              -
-- Load Level C
0.8 0.8               0.9 0.9                1                  1.1 1.1                        1.2 1.2                 1.3 1.3              1.4 1.4 Flaw Flaw Depth Depth inin Base Base Metal Metal aa (in)
- - - Load level 0 300 200
(in)
,--~
WCAP-1  7651-NP, Revision WCAP-17651-NP,       Revision 0,   0, Updated Updated Figure Figure 5-2 5-2 with with Corrected, Corrected, Limiting, Limiting, LevelLevel C C and and 0D Transients Transients of 12 88 of 12
100  
~ ---------------------------------------------------------------
o 0.8 0.9 1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)
WCAP-17651-NP, Revision 0, Updated Figure 5-2 with Corrected, Limiting, Level C and D Transients 8 of 12  


Circumferential Flaw Circumferential              Stability -- Base Flaw Stability      Base Metal, Metal, P=2.75ksi P2.T5ksi 100F/hr  Cooldown, a/t=1/4t, IOOF/hr Cooldown, alt=114t, SF=1.25 SFI .25 1800 1800
Circumferential Flaw Stability - Base Metal, P2.T5ksi IOOF/hr Cooldown, alt=114t, SFI.25 N
                    -      Japplied T=533F
(=
                        - Japplied   T=533F
I:1 C
                    -      Japplied T=480F
0) t Japplied T=533F Japplied T=480F Japplied T46OF Japplied Th31 3F JR Base T=533F JR Base T=480F JR Base T=460F JR Base T=31 3F da=O.1 Line 6T V-50 plate data at I SOF A
                        - Japplied  T=480F 1600 I- I __ Japplied T=460F 1600          Japplied T46OF Japplied T=313F Th31 3F r
6T V-50 plate data 1800 1600 1400 1200 1000 800 600 400 200 0
                    - - Japplied 1400 1400      I JR.Base
+
                    <===
AAA A
JR Base T:;S33F T=533F
A 2.1 2.2 I
                    - - JR  JR Base Base T=480F T=480F
2.3 A
                    - JR  JR Base Base T=460F T=460F 1200 ~
A A
1200      I -=====- JR Base T=313F T=31 3F N                I~ .= da =0.1" Line da=O.1   Line I
2.4 2.5 2.7 Flaw Depth a (in) 2.6 WCAP-17651-NP, Revision 0, Updated Figure 5-9 with V-50 Plate Data Included 9 of 12 N
N
.E :a  
(
'"i c::  
    =
~
* 6T V-50 plate data at I SOF
  .E     1000
:a'"i I:1                    A    6T V-50 plate data c::
C 800 800
  ~ 0)
C)
C)
CD
CD..
                                                                              *                *                  +,
C  
                                                                                                                    +
'"i..,
* tr*
Circumferential Flaw Stability - Base Metal, P=2.75ksi 100F/hr Cooldown, a/t=1/4t, SF=1.25 1800
* t C
-- Japplied T=533F
  '"i
-- Japplied T=480F 1600 I-I __ Japplied T=460F
  -;     600 400   l                           AAA
-- Japplied T=313F 1400 r I <=== JR.Base T:;S33F
                                                            !A 0
-- JR Base T=480F JR Base T=460F 1200 ~ I -=====- JR Base T=313F 1000 I 800 600 400 l 200 o
                                                              ~
2.1 I ~.= da = 0.1" Line tr 2.2
A
+,
                                                              ~                                A A                 A
0  
                                                                                                                    ~     A 200 I
~  
0o 2.1 2.1                    2.2 2.2                  2.3 2.3               2.4 2.4               2.5               2.6   2.7 2.7 Flaw Depth Flaw   Depth aa (in)
~
(in)
A A  
WCAP-1765 WCAP-17651-NP,   1-NP, Revision Revision 0, 0, Updated Updated Figure Figure 5-9 5-9 with with V-50 V-50 Plate Plate Data Data Included Included 99 of 12 of 12
~
2.3 2.4 2.5 2.6 Flaw Depth a (in)
WCAP-17651-NP, Revision 0, Updated Figure 5-9 with V-50 Plate Data Included 9 of 12 2.7


Circumferential Flaw Circumferential      Flaw Stability Stability - Base
Circumferential Flaw Stability - Base Metal, Level C & D, a = lIlOt, SFI
                                                                        - Base Metal, Metal, Level Level C && 0,D, aa == 1/10t, SFI lIlOt, SF=1 1800 1800
=
                  - - Level C
                                ) Lom LOJ T =  = 121F
                  - - -Leve{DLoadT=135F Level DLoooT= 135F 1600 ~ I 1600
                  ~=JR        Baset/1O4IDF JR Base  tl10 400F
                  -      JR Base JR  Base t/10 tIlO 500F 5XF 1400 ~ I 1400 JR
                  ==-        BasetIlO6lOF JR Baset/10610F
                  <=    =da=0.1
                        <= da= 0.1D 1200 ~ I 1200 N"
                      **  6TV-50pIatec1ata 6T V-50 pille data Ii 180F 100F
,<c=                  ~    6TV-50  pIe data 6TV-5O plme
.0    1000  1-1        adusted to rolF
~
E 1:7)
C)
C)
~=     800
=
::i;
 
                                                          ~                                               *
) LOJ
* I
=
* 600 600                                              ~
 
Leve{DLoadT=135F
=JR Baset/1O4IDF JR Base tIlO 5XF JR BasetIlO6lOF
=da=0.1 6TV-50pIatec1ata 180F 6TV-50 pIe data 1800 1600 1400 1200 1000 800 600 400 200 0
0.8
-A-J A
A A
0.9 1
1.1 1.2 1.3 A
Flaw Depth in Base Metal a (in) 1.4 WCAP-1 7651-NP, Revision 0, Updated Figure 5-12 with V-50 Plate Data Included and Corrected, Limiting, Level C and D Transients 10 of 12 N"
< c,
.0
~
E 1:7) 1800 1600
~ I 1400
~ I 1200
~ I 1000 1-1 Circumferential Flaw Stability - Base Metal, Level C & 0, a = 1/10t, SF=1
-- Level C Lom T = 121F
- - - Level DLoooT= 135F
~
JR Base tl10 400F JR Base t/10 500F
 
==-JR Baset/10610F
<= <= da= 0.1D
* 6T V-50 pille data Ii 100F
~ 6TV-5O plme data adusted to rolF
~
800
::i;  
~
I 600
~
o o
o o
400 400
j
                                          ~ A_ ~ -A-J    j - - - - - - - - i - - - - - - - - -~
~ A_ ~  
                                                  - A - ~-                                                 - - - - - - -----------_.
- A - ~- - - - - - - - - i - - - - - - - - -~ - - - - - -
A               A A                          A                    A              A 200 0o 0.8 0.8                         0.9 0.9              1                    1.1 1.1                        1.2 1.2                1.3 1.3             1.4 1.4 Flaw Flaw Depth Depth inin Base Base Metal Metal aa (in)
A A
(in)
400 200 o
WCAP-1      7651-NP, Revision WCAP-17651-NP,                 Revision 0,  0, Updated Updated Figure Figure 5-12 5-12 with with V-50V-50 Plate Plate DataData Included Included andand Corrected, Corrected, Limiting, Limiting, Level Level C and and D    0 Transients Transients 10 of 10   of 12 12
0.8 0.9 1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)
WCAP-17651-NP, Revision 0, Updated Figure 5-12 with V-50 Plate Data Included and Corrected, Limiting, Level C and 0 Transients 10 of 12
 
C4
-,)
Circumferential Flaw Stability Weld Metal, Level C & D, a = lIlOt, SF=1 LeveIC Load 121F
 
Level D Load 135F
 
===JRWeld t/10 400F JRWeldfJ105O0F 0


Circumferential Flaw Circumferential      Flaw Stability.
===JRWeldfJ1O61OF 0
Stability Weld Weld Metal, Metal, Level Level C C&     D, aa == 1/10t,
da0.1 1800 1600 1400 1200 1000 800 800 400 200 0
                                                                                                    & 0,        lIlOt, SF=1 SF=1 1800 1800 1600 1600          -LeveIC          Load 121F
II 0.8 0.9 1
                            - Level C Load     121F Level D
1.1 1.2 1.3 1.4 fl___.
                    - - - Level D Load Load 135F 135F 1400 1400          -===JRWeld
WCAP-1 7651-NP, Revision 0, Updated Figure 5-13 with Corrected, Limiting, Level C and D Transients 11 of 12 Circumferential Flaw Stability. Weld Metal, Level C & 0, a = 1/10t, SF=1 1800 1600  
                            -JRWeld tl10t/10 400F 400F
--Level C Load 121F  
                    -JRWeldfJ1          05O0F JR Weld tl10   500F       0 1200         ====JRWeldf      J1O61OF JRWeldtl10610F             0 1200 c:::> =- da = O.1n da0.1 N'
- - - Level D Load 135F 1400  
C4 c
--JRWeld tl10 400F JR Weld tl10 500F 1200  
..:::: 1000 B      1000
=
JRWeldtl10610F c:::> =- da = O.1n N'  
< c 1000 B
~
1!
~
800 s
oJ, 600 400
-- ------- ~ --------------------------------------.
200 0
~
~
1!
________ ~
~       800 s
___ L_ _________ i 0.8 0.9 1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)
oJ,
WCAP-17651-NP, Revision 0, Updated Figure 5-13 with Corrected, Limiting, Level C and 0 Transients 11 of 12  
-,)
800 800 600 400                                              II
                                  -- ------- ~ -------------------------------------- .
200 00  ~_ _ _ _ _ _ _ _~_ _ _L __ _ _ _ _ _ _ _ _ i 0.8 0.8                      0.9 0.9                 1                  1.1 1.1                      1.2 1.2                1.3 1.3             1.4 1.4 Flaw Depth in Base Metal a (in) _.
fl__
WCAP-1      7651-NP, Revision WCAP-17651-NP,               Revision 0,     0, Updated Updated Figure Figure 5-13 5-13 with with Corrected, Corrected, Limiting, Limiting, LevelLevel C C and   0 Transients and D Transients 11 of 11     12 of 12


References References 1.
References 1.
: 1. Regulatory Guide Regulatory  Guide 1.161, 1.161, "Evaluation Evaluation of of Reactor Reactor Pressure Pressure Vessels Vessels with with Charpy Charpy Upper-Shelf Energy Upper-Shelf   Energy Less Less than than 50  Ft-Lb, U.
Regulatory Guide 1.161, Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less than 50 Ft-Lb, U. S. Nuclear Regulatory Commission, June 1995.
50 Ft-Lb,U. S. Nuclear Regulatory S. Nuclear Regulatory Commission, Commission, June June 1995.
1995.
2.
2.
: 2. Westinghouse Report Westinghouse    Report WCAP-17651-NP, WCAP-1 7651-NP, Revision Revision 0, 0, "Palisades Palisades Nuclear Nuclear Power Power Plant Plant Reactor Vessel Reactor  Vessel Equivalent Equivalent Margins Margins Analysis,"
Westinghouse Report WCAP-1 7651-NP, Revision 0, Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis, February 2013 (ADAMS Accession No. ML13295A448).
Analysis, February February 2013 2013 (ADAMS (ADAMS Accession Accession No.
3.
No.
Code of Federal Regulations, 10 CFR Part 50, Appendix G, Fracture Toughness Requirements, U.S. Nuclear Regulatory Commission, Washington, D.C., Federal Register, Volume 60, No. 243, dated December 19, 1995.
ML13295A448).
4.
ML13295A448).
ASME Boiler and Pressure Vessel (B&PV) Code, Section Xl, Division 1, Appendix K, Assessment of Reactor Vessels with Low Upper Shelf Charpy Impact Energy Levels, 2007 Edition up to and including 2008 Addenda.
: 3. Code of Federal Federal Regulations, Regulations, 1010 CFR Part Part 50, Appendix G, "Fracture Fracture Toughness Toughness Requirements, U.S. Nuclear Regulatory Requirements,"                Regulatory Commission, Commission, Washington, D.C., Federal Register, Volume 60, No. 243, dated December 19, 1995.
5.
: 4. ASME Boiler and Pressure Vessel (B&PV) Code, Section XI,        Xl, Division 1, Appendix K, Assessment of Reactor Vessels with Low Upper Shelf Charpy Impact Energy Levels,"
ASME B&PV Code, Section Xl, Division 1, Appendix G, Fracture Toughness Criteria for Protection Against Failure, 1998 Edition up to and including 2000 Addenda.
    "Assessment                                                                          Levels, 2007 Edition up to and including 2008 Addenda.
12 of 12 References
: 5. ASME B&PV Code, Section XI,  Xl, Division 1, Appendix G, "Fracture Fracture Toughness Criteria for Protection Against Failure,"
: 1.
Failure, 1998 Edition up to and including 2000 Addenda.
Regulatory Guide 1.161, "Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less than 50 Ft-Lb," U. S. Nuclear Regulatory Commission, June 1995.
12  of 12 12 of 12}}
: 2.
Westinghouse Report WCAP-17651-NP, Revision 0, "Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis," February 2013 (ADAMS Accession No. ML13295A448).
: 3.
Code of Federal Regulations, 10 CFR Part 50, Appendix G, "Fracture Toughness Requirements," U.S. Nuclear Regulatory Commission, Washington, D.C., Federal Register, Volume 60, No. 243, dated December 19, 1995.
: 4.
ASME Boiler and Pressure Vessel (B&PV) Code, Section XI, Division 1, Appendix K, "Assessment of Reactor Vessels with Low Upper Shelf Charpy Impact Energy Levels,"
2007 Edition up to and including 2008 Addenda.
: 5.
ASME B&PV Code, Section XI, Division 1, Appendix G, "Fracture Toughness Criteria for Protection Against Failure," 1998 Edition up to and including 2000 Addenda.
12 of 12}}

Latest revision as of 20:23, 10 January 2025

Response to NRC Request for Additional Information - 10 CFR 50 Appendix G Equivalent Margin Analysis - Mf 2962
ML14163A662
Person / Time
Site: Palisades Entergy icon.png
Issue date: 06/12/2014
From: Vitale A
Entergy Nuclear Operations
To:
Document Control Desk, Office of Nuclear Reactor Regulation
References
PNP 2014-054
Download: ML14163A662 (14)


Text

Entergy Nuclear Operations, Inc.

J?.- #rijca,

Palisades Nuclear Plant 1_il 1Lt7 27780 Blue Star Memorial Highway Covert, MI 49043-9530 Tel 269 764 2000 Anthony J. Vitale Site Vice President PNP 2014-054 June 12, 2014 U.S. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001

SUBJECT:

Response to NRC Request for Additional Information

- Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis

ME 2962 Palisades Nuclear Plant Docket No. 50-255 License No. DPR-20

REFERENCES:

1. Palisades Nuclear Plant, Application for Renewed Operating License, dated March 22, 2005 (ADAMS Accession No. ML050940446).

2.

Entergy Nuclear Operations, Inc. letter PNP 2013-028, Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margins Analysis, dated October 21, 2013 (ADAMS Accession No. ML13295A448).

3.

NRC email to Entergy Nuclear Operations, Inc., Request for Additional Information

- Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis

- MF2962, dated May 13, 2014 (ADAMS Accession No. ML14133A684).

Dear Sir or Madam:

In the Palisades Nuclear Plant (PNP) license renewal application (Reference 1),

Nuclear Management Company (NMC), the former license holder for PNP, committed to submit an equivalent margins analysis (EMA) for Nuclear Regulatory Commission (NRC) approval at least three years before any reactor vessel beltline material Charpy upper-shelf energy (USE) decreases to less than 50 ft-lb, in accordance with 10 CFR 50 Appendix G, Section IV, Fracture Toughness Requirements.

Entergy Nuclear Operations, Inc. submitted the required EMA in Reference 2.

~Entergy Entergy Nuclear Operations, Inc.

Palisades Nuclear Plant 27780 Blue Star Memorial Highway Covert, MI 49043*9530 PNP 2014-054 June 12,2014 Tel 269 764 2000 Anthony J. Vitale Site Vice President u.s. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001

SUBJECT:

Response to NRC Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis -

MF 2962 Palisades Nuclear Plant Docket No. 50-255 License No. DPR-20

REFERENCES:

1. Palisades Nuclear Plant, Application for Renewed Operating License, dated March 22, 2005 (ADAMS Accession No. ML050940446).
2. Entergy Nuclear Operations, Inc. letter PNP 2013-028, Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margins Analysis, dated October 21, 2013 (ADAMS Accession No. ML13295A448).
3. NRC email to Entergy Nuclear Operations, Inc., Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis - MF 2962, dated May 13, 2014 (ADAMS Accession No. ML14133A684).

Dear Sir or Madam:

In the Palisades Nuclear Plant (PNP) license renewal application (Reference 1),

Nuclear Management Company (NMC), the former license holder for PNP, committed to submit an equivalent margins analysis (EMA) for Nuclear Regulatory Commission (NRC) approval at least three years before any reactor vessel beltline material Charpy upper-shelf energy (USE) decreases to less than 50 ft-Ib, in accordance with 10 CFR 50 Appendix G, Section IV, "Fracture Toughness Requirements."

Entergy Nuclear Operations, Inc. submitted the required EMA in Reference 2.

PLP 2014-054 Page 2 of 2 In Reference 3, ENO received a request for additional information (RAI) concerning the EMA submittal.

The ENO response to RAI questions 1, 3, 4, 5, and 6 is provided in the attachment.

The response to RAI question 2 will be provided at a later date, as agreed upon during a RAI clarification phone call between ENO and the NRC on June 6, 2014.

This letter contains no new commitments and no revised commitments.

I declare under penalty of perjury that the foregoing is true and correct; executed on June 12, 2014.

Sincerely, ajv/jse

Attachment:

Response to NRC Request for Additional Information

- Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis

- ME 2962 cc:

Administrator, Region Ill, USNRC Project Manager, Palisades, USN RC Resident Inspector, Palisades, USN RC PLP 2014-054 Page 2 of 2 In Reference 3, ENO received a request for additional information (RAI) conceming the EMA submittal.

The ENO response to RAI questions 1, 3, 4, 5, and 6 is provided in the attachment.

The response to RAI question 2 will be provided at a later date, as agreed upon during a RAI clarification phone call between ENO and the NRC on June 6, 2014.

This letter contains no new commitments and no revised commitments.

I declare under penalty of perjury that the foregoing is true and correct; executed on June 12, 2014.

Sincerely, ajv/jse

Attachment:

Response to NRC Request for Additional Information - Palisades Nuclear Plant 10 CFR 50 Appendix G Equivalent Margin Analysis - MF 2962 cc:

Administrator, Region III, USNRC Project Manager, Palisades, USNRC Resident Inspector, Palisades, USNRC

ATTACHMENT RESPONSE TO NRC REQUEST FOR ADDITIONAL INFORMATION -

PALISADES NUCLEAR PLANT 10 CFR 50 APPENDIX G EQUIVALENT MARGIN ANALYSIS - MF 2962 A follow-up request for additional information (RAI) was received from the Nuclear Regulatory Commission (NRC), by electronic mail on May 13, 2014. The RAI requested that the response to the RAI be docketed within 30 days of receipt of the request.

The Entergy Nuclear Operations, Inc. (ENO) Palisades Nuclear Plant (PNP) response to the RAI is provided below.

NRC Request (May 13, 2014) 1.

The EMA is based on American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code (Code) Section Xl, Appendix K as supplemented by Regulatory Guide (AG) 1.161 Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 Ft-Lb ASME Code Section Xl, Appendix K, Article K-4210 and RG 1.161 both include equations for calculating the stress intensity factor due to radial thermal gradients. In Section 5.1 of the EMA submittal, the licensee discusses through-wall thermal stress and states that typical through-wall stress and stress distribution during a heatup transient are shown in Figures 5-1 and 5-2. But Figures 5-1 and 5-2 of the EMA submittal do not show these stresses as discussed. Provide figures showing typical through-wall stress and stress distributions during a heatup transient to support the discussion in paragraph 5.1 of the EMA submittal.

ENO Response to RAI-1 Figures detailing typical heatup thermal axial stress and typical through-wall axial stress for the PNP reactor vessel used in the equivalent margins analysis (EMA) submittal are provided below.

1 of 12 ATTACHMENT RESPONSE TO NRC REQUEST FOR ADDITIONAL INFORMATION -

PALISADES NUCLEAR PLANT 10 CFR 50 APPENDIX G EQUIVALENT MARGIN ANAL VSIS - MF 2962 A follow-up request for additional information (RAI) was received from the Nuclear Regulatory Commission (NRC), by electronic mail on May 13, 2014. The RAI requested that the response to the RAI be docketed within 30 days of receipt of the request.

The Entergy Nuclear Operations, Inc. (ENO) Palisades Nuclear Plant (PNP) response to the RAI is provided below.

NRC Request (May 13, 2014)

1.

The EMA is based on American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code (Code)Section XI, Appendix K as supplemented by Regulatory Guide (RG) 1. 161 "Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 Ft-Lb". ASME Code Section XI, Appendix K, Article K-4210 and RG 1.161 both include equations for calculating the stress intensity factor due to radial thermal gradients. In Section 5. 1 of the EMA submittal, the licensee discusses through-wall thermal stress and states that typical through-wall stress and stress distribution during a heatup transient are shown in Figures 5-1 and 5-2. But Figures 5-1 and 5.. 2 of the EMA submittal do not show these stresses as discussed. Provide figures showing typical through-wall stress and stress distributions during a heatup transient to support the discussion in paragraph 5. 1 of the EMA submittal.

ENO Response to RAI-1 Figures detailing typical heatup thermal axial stress and typical through-wall axial stress for the PNP reactor vessel used in the equivalent margins analysis (EMA) submittal are provided below.

1 of 12

10 Heatup Transient Thermal Stress - Sxx vs Time ID Midwall 5E 0

1 2

3 4

5 6

7 8

U, U,

I U,-5

[-

-10

-15 Time (hr)

Figure 5-1 (a)

PNP Typical Thermal Transient Axial Stress Profile Stress versus Time 2 of 12 10

~I _H~aJ~p Ir~nJ~J~!'t l11~r.!ltal $t!_~SS - S~ ~~~ 11m~

I I

I

' 10

. Midwall j

OD 5

---ir o

1

-10 1--- --

-15 Time (hr)

Figure 5-1 (a) - PNP Typical Thermal Transient Axial Stress Profile - Stress versus Time 2 of 12

Heatup Transient Thermal Stress - Sxx vs. x/t 10 5

0 U,.

Ll

-5

-10

-15 Figure 5-2(a) - PNP Typical Thermal Transient Axial Through-Wall Stress Distribution NRC Request (May 13, 2014) 2.

Section 5.1 states, Only circumferential base metal flaws are considered in this analysis, because only the weak orientation USE is projected to drop below 50 ft-lbs as described below. Please demonstrate that assuming a circumferential flaw in the base metal with the weak Charpy V-Notch (CVN) value in the EMA is more limiting than assuming an axial flaw in the base metal with the strong CVN value. Please note that the significantly greater applied J integral associated with the axial flaw may challenge the fundamental assumption in the EMA submittal.

ENO Response to RAI-2 Based on discussions between ENO and the NRC during a June 6, 2014 RAI conference call, the response to this RAI question will be provided at a later date, as agreed upon during the call.

0 0.1 0.2 0,3 06 0.7 08 09


H I Transient Time (sec)I 6300 12600 15700 30300 Distance Ratio x/t 3 of 12 Heatup Transient Thermal Stress - Sxx vs. x/t 10 r

5 o

-10

-15 r

I I

-~. ----r-l


~ ----r ------ ----

0!5 0.6 Or7 0.8 0.9 1

I

~- ----,:-----+-

__________ 0-.1 Trarisient Time (sec)1

-- 6300

-- 12600 15700 I

- - - 30300

--1-__

Distance Ratio x/t Figure 5-2(a) - PNP Typical Thermal Transient Axial Through-Wall Stress Distribution NRC Request (May 13, 2014)

2.

Section 5. 1 states, "0nly circumferential base metal flaws are considered in this analysis, because only the "weak" orientation USE is projected to drop below 50 ft-Ibs as described below." Please demonstrate that assuming a circumferential flaw in the base metal with the weak Charpy V-Notch (CVN) value in the EMA is more limiting than assuming an axial flaw in the base metal with the strong CVN value. Please note that the significantly greater applied J integral associated with the axial flaw may challenge the fundamental assumption in the EMA submittal.

ENO Response to RAI-2 Based on discussions between ENO and the NRC during a June 6, 2014 RAI conference call, the response to this RAI question will be provided at a later date, as agreed upon during the call.

3 of 12

NRC Request (May 13, 2014) 3.

The applied J-integral values for the circumferential flaws for all Level A and B service level conditions are shown in Figure 5-1, and the applied J-integral values for the circumferential flaws for Level C and D service level conditions are shown in Figure 5-2. Since Section 5.1 provides very limited information regarding the applied J-integral calculations, please confirm that the calculations underlying Figures 5-7 and 5-2 are based on the formulas in RG 1.761, REvaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 FT-LB. If not, please describe, in addition to your response to RAt-1, your plant-specific calculations to support their acceptance in this application.

ENO Response to RAI-3 Yes, the applied J-integral calculations underlying Figures 5-1 and 5-2 are based on formulas in RG 1.161.

NRC Request (May 13, 2014) 4.

Table 4-4 was presented but without being mentioned in Section 4 regarding how it was used in the EMA analysis. Therefore, please confirm that the calculated available margins presented in Table 5-3 for various time during coo/down are results, using the relevant J-R curves adjusted by the material margin factors of Table 4-4.

ENO Response to RAI-4 As discussed in Section 2.2 of WCAP-17651-NP, Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis, Revision 0, RG 1.161 material margin factors (ME) in Table 4-4 were used for the J-R curves.

NRC Request (May 13, 2014)

5. Section 5.2 provides justification for using the high-toughness/low-sulfur model from RG 1.161 in the proposed EMA for the high-sulfur plates, and Section 5.3 provides the corresponding EMA results. When the high-sulfur model (e.g., for the 6T specimen) of NUREG/CR-5265, Size Effects on J-R Curves for A 302-B Plate, is used, please demonstrate that The updated safety factors (see Table 5-3), after adjusting for temperature, will still be greater than 1.15.

The updated applied J/J-R curves (see figures 5-8, 5-9, and 5-12), after adjusting for temperature, will still show that dJappjjeci/da <dJmaterja/da at Japplied = Jmateriai 4 of 12 NRC Request (May 13, 2014)

3.

The applied J-integral values for the circumferential flaws for all Level A and B service level conditions are shown in Figure 5-1, and the applied J-integral values for the circumferential flaws for Level C and D service level conditions are shown in Figure 5-2. Since Section 5. 1 provides very limited information regarding the applied J-integral calculations, please confirm that the calculations underlying Figures 5-1 and 5-2 are based on the formulas in RG 1.161, uEvaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less Than 50 FT-LB." If not, please describe, in addition to your response to RAI-1, your plant-specific calculations to support their acceptance in this application.

ENO Response to RAI-3 Yes, the applied J-integral calculations underlying Figures 5-1 and 5-2 are based on formulas in RG 1.161.

NRC Request (May 13, 2014)

4. Table 4-4 was presented but without being mentioned in Section 4 regarding how it was used in the EMA analysis. Therefore, please confirm that the calculated available margins presented in Table 5-3 for various time during cooldown are results, using the relevant J-R curves adjusted by the material margin factors of Table 4-4.

ENO Response to RAI-4 As discussed in Section 2.2 of WCAP-17651-NP, "Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis," Revision 0, RG 1.161 material margin factors (MF) in Table 4-4 were used for the J-R curves.

NRC Request (May 13, 2014)

5. Section 5.2 provides justification for using the high-toughness/low-sulfur model from RG 1.161 in the proposed EMA for the high-sulfur plates, and Section 5.3 provides the corresponding EMA results. When the high-sulfur model (e.g., for the 6Tspecimen) of NUREG/CR-5265, uSize Effects on J-R Curves for A 302-8 Plate," is used, please demonstrate that The updated safety factors (see Table 5-3), after adjusting for temperature, will still be greater than 1. 15.

The updated applied J/J-R curves (see figures 5-8, 5-9, and 5-12), after adjusting for temperature, will still show that dJappliecida < dJmaterialda at Japplied = Jmaterial.

4 of 12

If the above cannot be demonstrated, perform a sensitivity study, showing at what percentage of the proposed J-R cuive (e.g., 90%), your EMA calculation results will meet the criteria on both crack extension and stability.

6. Section 6 presents conclusions of this submittal. For Service Level C condition with 400°F/hr cooldown, it is concluded that, The equivalent margins analyses for the plate materials are acceptable and bounded by the conservative test data reported in NUREG/CR-5265 in all cases for the Level C transient. This conclusion was repeated later for Service Level D condition with 600°F/hr cooldown, with C in the quote replaced by D. Plot the relevant NUREG/CR 5265 6T data in Figure 5-12 and provide sufficientjustification to support your conclusions.

ENO Responses to RAI-5 and RAI-6 Updated Figures 5-9 and 5-12 with the V-50 plate data are provided below, along with added Tables 5-4 and 5-5 showing the Level C and D safety factors, respectively.

Table 5-6 was added, which demonstrates the available margins on pressure loading with the V-50 plate data, adjusted for temperature, with consideration of all service loadings, Level A, B, C and D. The minimum safety factor (SF) with consideration of the V-SO plate data and the PNP-specific J-applied values is 1.5, which is above the minimum required SF of 1.15 per RG 1.161.

Figure 5-8 from WCAP-1 7651-NP, Revision 0, along with the updated Figures 5-9 and 5-1 2 below, all demonstrate that at Japplied = Jmaterial, dJapplied/da < dJmateriai/da, is satisfied for all three cases (i.e., the slope of the Japplied is smaller than the Jmaterial at the point of intersection).

Therefore, as demonstrated below and in WCAP-1 7651-NP, the equivalent margins of safety per ASME Code Section Xl (References 4 and 5) are found to be acceptable for the PNP reactor vessel beltline and extended beltline regions with predicted Charpy upper-shelf energy levels falling below the 50 ft-lb 10 CFR 50, Appendix G requirements at end-of-license-extension.

Westinghouse discovered during the development of this RAI response that the Level C and D loading J-applied curves plotted in WCAP-1 7651-NP, Figure 5-12, were not the most limiting case. This error also propagated onto Figures 5-2 and 5-13 in the WCAP.

This has been updated in the attached figures as part of this RAI response. Note that the conclusions to the report, including the safety factor determination, are unchanged; only the figures were in error. This has been documented in the Westinghouse corrective action system, and will be corrected when the WCAP is revised to incorporate these RAI changes.

Lastly, note that the Level C and D margin tables (Tables 5-4 and 5-5 below) were originally omitted from WCAP-1 7651-NP because Service Level A and B, as discussed in Section 5.3 of WCAP-1 7651-NP, are the governing transients.

5 of 12 If the above cannot be demonstrated, perform a sensitivity study, showing at what percentage of the proposed J-R curve (e.g., 90%), your EMA calculation results will meet the criteria on both crack extension and stability.

6. Section 6 presents conclusions of this submittal. For Service Level C condition with 400°Flhr cooldown, it is concluded that, "The equivalent margins analyses for the plate materials are acceptable and bounded by the conservative test data reported in NUREGICR-5265 in all cases for the Level C transient." This conclusion was repeated later for Service Level D condition with 600°Flhr cooldown, with IIC" in the quote replaced by liD." Plot the relevant NUREGICR 5265 6T data in Figure 5-12 and provide sufficient justification to support your conclusions.

ENO Responses to RAI-5 and RAI-6 Updated Figures 5-9 and 5-12 with the V-50 plate data are provided below, along with added Tables 5-4 and 5-5 showing the Level C and D safety factors, respectively.

Table 5-6 was added, which demonstrates the available margins on pressure loading with the V-50 plate data, adjusted for temperature, with consideration of all service loadings, Level A, B, C and D. The minimum safety factor (SF) with consideration of the V-50 plate data and the PNP-specific J-applied values is 1.5, which is above the minimum required SF of 1.15 per RG 1.161.

Figure 5-8 from WCAP-17651-NP, Revision 0, along with the updated Figures 5-9 and 5-12 below, all demonstrate that at Japplied = Jmaterial, dJapplieJda < dJmateria~da, is satisfied for all three cases (i.e., the slope of the Japplied is smaller than the Jmaterial at the point of intersection).

Therefore, as demonstrated below and in WCAP-17651-NP, the equivalent margins of safety per ASME Code Section XI (References 4 and 5) are found to be acceptable for the PNP reactor vessel beltline and extended beltline regions with predicted Charpy upper-shelf energy levels falling below the 50 ft-Ib 10 CFR 50, Appendix G requirements at end-of-license-extension.

Westinghouse discovered during the development of this RAI response that the Level C and D loading J-applied curves plotted in WCAP-17651-NP, Figure 5-12, were not the most limiting case. This error also propagated onto Figures 5-2 and 5-13 in the WCAP.

This has been updated in the attached figures as part of this RAI response. Note that the conclusions to the report, including the safety factor determination, are unchanged; only the figures were in error. This has been documented in the Westinghouse corrective action system, and will be corrected when the WCAP is revised to incorporate these RAI changes.

Lastly, note that the Level C and D margin tables (Tables 5-4 and 5-5 below) were originally omitted from WCAP-17651-NP because Service Level A and B, as discussed in Section 5.3 of WCAP-17651-NP, are the governing transients.

5 of 12

Table 5-4 Available Margins on Pressure Load for Level C, 400°F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw Jo.

1 Jo.

1 Time SF J-applied x SF material SF J-applied x SF material (sec)

(in-lb/in 2

)

(in-lb/in 2

)

(in-lb/in 2

)

(in-lb/in 2

)

0 5.8 682 682 5.2 511 510 1,197 8.6 885 839 7.1 613 613 4,122 8.9 1,535 1,534 7.1 1,050 1,050 Minimum SF 5.8 5.2 Table 5-5 Available Margins on Pressure Load for Level D, 600°F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw Jo.

1 Jo.

1 Time SF J-applied x SF material SF J-applied x SF material (sec)

(in-lb/in 2

)

(in-lb/in 2

)

(in-lb/in 2

)

(in-lb/in 2

)

0 5.8 682 682 5.2 510 510 798 8.1 830 830 6.9 607 607 2,748 7.0 1,491 1,491 5.2 1,023 1,023 Minimum SF 5.8 5.2 6 of 12 Table 5-4 Available Margins on Pressure Load for Level C, 400°F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw JO*1 JO*1 Time SF J-applied x SF material SF J-applied x SF material (sec)

(in-lb/in2)

(in-lb/in2)

(in-lb/in2)

(in-lb/in2) 0 5.8 682 682 5.2 511 510 1,197 8.6 885 839 7.1 613 613 4,122 8.9 1,535 1,534 7.1 1,050 1,050 Minimum SF 5.8 5.2 Table 5-5 Available Margins on Pressure Load for Level D, 600°F/hr Cooldown Base Material Weld Material Circumferential Flaw Circumferential Flaw JO*1 JO*1 Time SF J-applied x SF material SF J-applied x SF material (sec)

(in-lb/in2)

(in-lb/in2)

(in-lb/in2)

(in-lb/in2) 0 5.8 682 682 5.2 510 510 798 8.1 830 830 6.9 607 607 2,748 7.0 1,491 1,491 5.2 1,023 1,023 Minimum SF 5.8 5.2 6 of 12

Table 5-6: Available Margins on Pressure Load for All Transients, Levels A, B, C and D, with Consideration of V-50 Plate Data V-50 Plate V-50 Plate V-50 Plate Level A Circumferential Level C Circumferential Level D Circumferential and B J

01 J

01 Flaw Flaw Flaw material material J-applied J-applied J-applied material Time SF SF (in-Time (in-Time SF x SF (in-lb/in 2

)

SF xSF (sec)

(in-lb/in 2

)

lb/in 2

)

(sec)

(in-lb/in 2

)

lb/in 2

)

(sec)

(in-lb/in 2

)

0 1.8 397 397 0

3.4 397 397 0

3.4 397 397 2800 1.6 441 441 1,197 4.7 488 488 798 4.7 483 483 3600 1.6 459 459 4,122 1.9 893 893 2,748 1.5 868 868 5400 1.7 503 503 7200 1.8 554 554 9000 1.9 611 611 10800 18.0 675 675 I

Minimum

[ Minimum Minimum SF 1.6 SF 1.9 SF 1.5 7 of 12 Table 5-6: Available Margins on Pressure Load for All Transients, Levels A, B, C and 0, with Consideration of V-50 Plate Data Level A V-50 Plate V-50 Plate V-50 Plate and B Circumferential JO*1 LevelC Circumferential JO.1 Level 0 Circumferential Flaw material Flaw material Flaw JO*1 Time J-applied (in-Time J-applied (in-Time J-applied material (sec)

SF xSF Iblin2)

(sec)

SF xSF Iblin2}

(sec)

SF xSF (in-lblin2)

(in-lblin2)

(in-lblin2)

(in-lblin2) 0 1.8 397 397 0

3.4 397 397 0

3.4 397 397 2800 1.6 441 441 1,197 4.7 488 488 798 4.7 483 483 3600 1.6 459 459 4,122 1.9 893 893 2,748 1.5 868 868 5400 1.7 503 503 7200 1.8 554 554 9000 1.9 611 611 10800 18.0 675 675 Minimum 1.6 Minimum 1.9 Minimum 1.5 SF SF SF 7 of 12

Applied J-lntegral Curve - Circumferential Flaw, Level C & D, a = lIlOt, SF=1 400 Load LeveIC

Load LevelD 300 C\\4 100 0

0.8 0.9 1

1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)

WCAP-1 7651-NP, Revision 0, Updated Figure 5-2 with Corrected, Limiting, Level C and 0 Transients 8 of 12 f::j

< c:

.Q

~

e Ie)

~

J; Applied J-Integral Curve - Circumferential Flaw, Level C & D, a = 1/10t, SF=1 400

-- Load Level C

- - - Load level 0 300 200

,--~

100

~ ---------------------------------------------------------------

o 0.8 0.9 1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)

WCAP-17651-NP, Revision 0, Updated Figure 5-2 with Corrected, Limiting, Level C and D Transients 8 of 12

Circumferential Flaw Stability - Base Metal, P2.T5ksi IOOF/hr Cooldown, alt=114t, SFI.25 N

(=

I:1 C

0) t Japplied T=533F Japplied T=480F Japplied T46OF Japplied Th31 3F JR Base T=533F JR Base T=480F JR Base T=460F JR Base T=31 3F da=O.1 Line 6T V-50 plate data at I SOF A

6T V-50 plate data 1800 1600 1400 1200 1000 800 600 400 200 0

+

AAA A

A 2.1 2.2 I

2.3 A

A A

2.4 2.5 2.7 Flaw Depth a (in) 2.6 WCAP-17651-NP, Revision 0, Updated Figure 5-9 with V-50 Plate Data Included 9 of 12 N

.E :a

'"i c::

~

C)

CD..

C

'"i..,

Circumferential Flaw Stability - Base Metal, P=2.75ksi 100F/hr Cooldown, a/t=1/4t, SF=1.25 1800

-- Japplied T=533F

-- Japplied T=480F 1600 I-I __ Japplied T=460F

-- Japplied T=313F 1400 r I <=== JR.Base T:;S33F

-- JR Base T=480F JR Base T=460F 1200 ~ I -=====- JR Base T=313F 1000 I 800 600 400 l 200 o

2.1 I ~.= da = 0.1" Line tr 2.2

+,

0

~

~

A A

~

2.3 2.4 2.5 2.6 Flaw Depth a (in)

WCAP-17651-NP, Revision 0, Updated Figure 5-9 with V-50 Plate Data Included 9 of 12 2.7

Circumferential Flaw Stability - Base Metal, Level C & D, a = lIlOt, SFI

=

C)

=

) LOJ

=

Leve{DLoadT=135F

=JR Baset/1O4IDF JR Base tIlO 5XF JR BasetIlO6lOF

=da=0.1 6TV-50pIatec1ata 180F 6TV-50 pIe data 1800 1600 1400 1200 1000 800 600 400 200 0

0.8

-A-J A

A A

0.9 1

1.1 1.2 1.3 A

Flaw Depth in Base Metal a (in) 1.4 WCAP-1 7651-NP, Revision 0, Updated Figure 5-12 with V-50 Plate Data Included and Corrected, Limiting, Level C and D Transients 10 of 12 N"

< c,

.0

~

E 1:7) 1800 1600

~ I 1400

~ I 1200

~ I 1000 1-1 Circumferential Flaw Stability - Base Metal, Level C & 0, a = 1/10t, SF=1

-- Level C Lom T = 121F

- - - Level DLoooT= 135F

~

JR Base tl10 400F JR Base t/10 500F

==-JR Baset/10610F

<= <= da= 0.1D

  • 6T V-50 pille data Ii 100F

~ 6TV-5O plme data adusted to rolF

~

800

i;

~

I 600

~

o o

j

~ A_ ~

- A - ~- - - - - - - - - i - - - - - - - - -~ - - - - - -

A A

400 200 o

0.8 0.9 1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)

WCAP-17651-NP, Revision 0, Updated Figure 5-12 with V-50 Plate Data Included and Corrected, Limiting, Level C and 0 Transients 10 of 12

C4

-,)

Circumferential Flaw Stability Weld Metal, Level C & D, a = lIlOt, SF=1 LeveIC Load 121F

Level D Load 135F

===JRWeld t/10 400F JRWeldfJ105O0F 0

===JRWeldfJ1O61OF 0

da0.1 1800 1600 1400 1200 1000 800 800 400 200 0

II 0.8 0.9 1

1.1 1.2 1.3 1.4 fl___.

WCAP-1 7651-NP, Revision 0, Updated Figure 5-13 with Corrected, Limiting, Level C and D Transients 11 of 12 Circumferential Flaw Stability. Weld Metal, Level C & 0, a = 1/10t, SF=1 1800 1600

--Level C Load 121F

- - - Level D Load 135F 1400

--JRWeld tl10 400F JR Weld tl10 500F 1200

=

JRWeldtl10610F c:::> =- da = O.1n N'

< c 1000 B

~

1!

~

800 s

oJ, 600 400

-- ------- ~ --------------------------------------.

200 0

~

________ ~

___ L_ _________ i 0.8 0.9 1.1 1.2 1.3 1.4 Flaw Depth in Base Metal a (in)

WCAP-17651-NP, Revision 0, Updated Figure 5-13 with Corrected, Limiting, Level C and 0 Transients 11 of 12

References 1.

Regulatory Guide 1.161, Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less than 50 Ft-Lb, U. S. Nuclear Regulatory Commission, June 1995.

2.

Westinghouse Report WCAP-1 7651-NP, Revision 0, Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis, February 2013 (ADAMS Accession No. ML13295A448).

3.

Code of Federal Regulations, 10 CFR Part 50, Appendix G, Fracture Toughness Requirements, U.S. Nuclear Regulatory Commission, Washington, D.C., Federal Register, Volume 60, No. 243, dated December 19, 1995.

4.

ASME Boiler and Pressure Vessel (B&PV) Code, Section Xl, Division 1, Appendix K, Assessment of Reactor Vessels with Low Upper Shelf Charpy Impact Energy Levels, 2007 Edition up to and including 2008 Addenda.

5.

ASME B&PV Code, Section Xl, Division 1, Appendix G, Fracture Toughness Criteria for Protection Against Failure, 1998 Edition up to and including 2000 Addenda.

12 of 12 References

1.

Regulatory Guide 1.161, "Evaluation of Reactor Pressure Vessels with Charpy Upper-Shelf Energy Less than 50 Ft-Lb," U. S. Nuclear Regulatory Commission, June 1995.

2.

Westinghouse Report WCAP-17651-NP, Revision 0, "Palisades Nuclear Power Plant Reactor Vessel Equivalent Margins Analysis," February 2013 (ADAMS Accession No. ML13295A448).

3.

Code of Federal Regulations, 10 CFR Part 50, Appendix G, "Fracture Toughness Requirements," U.S. Nuclear Regulatory Commission, Washington, D.C., Federal Register, Volume 60, No. 243, dated December 19, 1995.

4.

ASME Boiler and Pressure Vessel (B&PV) Code,Section XI, Division 1, Appendix K, "Assessment of Reactor Vessels with Low Upper Shelf Charpy Impact Energy Levels,"

2007 Edition up to and including 2008 Addenda.

5.

ASME B&PV Code,Section XI, Division 1, Appendix G, "Fracture Toughness Criteria for Protection Against Failure," 1998 Edition up to and including 2000 Addenda.

12 of 12