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{{#Wiki_filter:'e, L 2l 1I ELECTRIC POWER RESEARCH INSTITUTE 2015-025 BWR Vessel & Internals Project (BWRVIP)March 09, 2015 Document Control Desk U.S. Nuclear Regulatory Commission 11555 Rockville PikeRockville, MD 20852 Attention: Joseph Holonich
{{#Wiki_filter:United States Nuclear Regulatory Commission Official Hearing Exhibit In the Matter of:                    Entergy Nuclear Operations, Inc.                                                                        ENT000663 (Indian Point Nuclear Generating Units 2 and 3)
ASLBP #: 07-858-03-LR-BD01 Submitted: August 10, 2015 Docket #: 05000247 l 05000286 Exhibit #: ENT000663-00-BD01                  Identified: 11/5/2015 Admitted: 11/5/2015                          Withdrawn:
Rejected:                                      Stricken:
Other:
2l1I ELECTRIC POWER L          RESEARCH INSTITUTE
                                                                                                                                    'e, 2015-025                                                         BWR Vessel & Internals Project (BWRVIP)
March 09, 2015 Document Control Desk U.S. Nuclear Regulatory Commission 11555 Rockville Pike Rockville, MD 20852 Attention:         Joseph Holonich


==Subject:==
==Subject:==
Project No. 704 -Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR Reactor Internals Fabricated of Cast Austenitic Stainless Steel  
Project No. 704 - Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR Reactor Internals Fabricated of Cast Austenitic Stainless Steel


==References:==
==References:==
: 1. Letter from D. Madison (BWRVIP Chairman) and A. McGehee (BWRVIP Program Manager) to J. Holonich (NRC), Project No. 704 -BWRVIP Response to NRC Request for Additional Information on BWRVIP-234, dated May 23, 2014. ADAMS -ML14174A841.
: 1. Letter from D. Madison (BWRVIP Chairman) and A. McGehee (BWRVIP Program Manager) to J. Holonich (NRC), Project No. 704 - BWRVIP Response to NRC Request for Additional Information on BWRVIP-234, dated May 23, 2014. ADAMS - ML14174A841.
: 2. Letter from J. Holonich (NRC) to A. Mendiola (NRC), Summary of the July 15,2014, Meeting with the Electric Power Research Institute on Items Related to Cast Austenitic Stainless Steel and the Materials Reliability Program-227-A,"Pressurized Water Reactor Internals Inspection And Evaluation Guidelines," September 9, 2014. ADAMS -ML14127A077.
: 2. Letter from J. Holonich (NRC) to A. Mendiola (NRC), Summary of the July 15, 2014, Meeting with the Electric Power Research Institute on Items Related to Cast Austenitic Stainless Steel and the Materials Reliability Program-227-A, "Pressurized Water Reactor Internals Inspection And Evaluation Guidelines,"
: 3. "NRC Position on Aging Management of CASS Reactor Vessel Internal Components," June 23, 2014, ADAMS -ML 14174A719.
September 9, 2014. ADAMS - ML14127A077.
: 4. Email from C. Wirtz (EPRI) to J. Holonich (NRC), October 7, 2014.5. NUREG/CR-4513, ANL-93/22, Revision 1, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," Argonne National Laboratory, May 1994.The purpose of this letter is to provide the status of the Industry (PWR and BWR) activities associated with developing and proposing a generic screening criteria to address thermal and irradiation embrittlement of RPV internals fabricated of cast austenitic stainless steel (CASS).Reference I was provided to the NRC in response to a Request for Additional Information (RAI) regarding BWRVIP-234.
: 3. "NRC Position on Aging Management of CASS Reactor Vessel Internal Components," June 23, 2014, ADAMS - ML14174A719.
The RAI response contained supplemental information that provided the technical bases for an Industry screening criteria for CASS internals.
: 4. Email from C. Wirtz (EPRI) to J. Holonich (NRC), October 7, 2014.
Together ...Shaping the Future of Electricity Qýý U*PALO ALTO OFFICE 3420 Fillview Avenue, Palo Alto, CA 94304-1395 USA
: 5. NUREG/CR-4513, ANL-93/22, Revision 1, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," Argonne National Laboratory, May 1994.
* 650.855.2000  
The purpose of this letter is to provide the status of the Industry (PWR and BWR) activities associated with developing and proposing a generic screening criteria to address thermal and irradiation embrittlement of RPV internals fabricated of cast austenitic stainless steel (CASS).
# Customer Service 800.313.3774 9 www.epri.com BWRVIP 2015-025 A meeting was later held on July 15, 2014 at NRC offices in Washington, DC to discuss the Industry and NRC positions (References 2, 3). Based on that meeting, the Industry committed to investigate additional information where there was disagreement with the NRC regarding the screening criteria and provide said information to the NRC at a later date. That information was informally submitted for NRC's consideration (Reference
Reference I was provided to the NRC in response to a Request for Additional Information (RAI) regarding BWRVIP-234. The RAI response contained supplemental information that provided the technical bases for an Industry screening criteria for CASS internals.
: 4) and is contained in Attachments A through D of this letter. A conference call was then held on November 20, 2014 with the NRC to discuss this information.
Together .     . . Shaping the Future of Electricity PALO ALTO OFFICE 3420 Fillview Avenue, Palo Alto, CA 94304-1395 USA
Following this conference call the NRC indicated that they were not willing to deviate from their position documented in Reference 3.Despite the NRC's current stance on the matter, the following comments regarding a generic TE and IE criteria for evaluation of reactor internals are important in forming the basis for the industry position: " The industry recognizes that the NRC is intending to revise its original IE position in the Grimes letter from lxl10 7 n/cm 2 (0.00014 dpa) to a position in the region of 0.5 to 1.5 dpa. Industry agrees that this position is more appropriate and has proposed a conservative value of 1 dpa.* It is not appropriate (for the staff) to penalize all non-Mo containing CASS (such as CF3 and CF8) because of the lower properties associated with the Mo-containing CF8M materials that are included in the ANL/NRC database, i.e., impose a lower bound.* There is no substantive data that demonstrates a synergistic effect for CASS materials that are typical of reactor internals (such as CF3 and CF8). As such the industry has proposed criteria that do not combine TE and IE. Each mechanism is considered distinct and separate." The introduction of a new criteria set for the category of materials with ferrite content between 15% to 20% having a lower proposed screening value for IE of 0.45 dpa is unnecessary and technically unfounded.
* 650.855.2000 # Customer Service 800.313.3774 9 www.epri.com QýýU*
The introduction of this category of ferrite content is significantly burdensome to licensees since it will require more complex and potentially more error-prone assessments of CASS material components by virtue of having more categories.
 
Industry maintains that the categories of materials and associated ferrite levels contained in the Grimes letter are appropriate." The criteria proposed by the industry (20% Ferrite and 1 dpa) have been shown to project significant margin on toughness reduction and therefore safety when compared to measured embrittlement behavior for CF3 and CF8 materials.
BWRVIP 2015-025 A meeting was later held on July 15, 2014 at NRC offices in Washington, DC to discuss the Industry and NRC positions (References 2, 3). Based on that meeting, the Industry committed to investigate additional information where there was disagreement with the NRC regarding the screening criteria and provide said information to the NRC at a later date. That information was informally submitted for NRC's consideration (Reference 4) and is contained in Attachments A through D of this letter. A conference call was then held on November 20, 2014 with the NRC to discuss this information.
Regardless, this letter serves to formally submit this additional information to the NRC for review and consideration in developing a regulatory position for the screening criteria associated with TE and IE for CASS internals and to inform revisions to NUREG-4513, Rev. 1 (Reference 5). The PWR and BWR Industry position for TE and IE screening criteria is shown in Attachment D.2 BWRVIP 2015-025 Irrespective of the staff's decision and future promulgation of a regulatory position on TE and IE for CASS internals, the BWRVIP formally requests the NRC to evaluate and resolve the RAI responses associated with BWRVIP-234 and issue a Safety Evaluation.
Following this conference call the NRC indicated that they were not willing to deviate from their position documented in Reference 3.
Despite the NRC's current stance on the matter, the following comments regarding a generic TE and IE criteria for evaluation of reactor internals are important in forming the basis for the industry position:
    " The industry recognizes that the NRC is intending to revise its original IE position in the Grimes letter from lxl10 7 n/cm 2 (0.00014 dpa) to a position in the region of 0.5 to 1.5 dpa. Industry agrees that this position is more appropriate and has proposed a conservative value of 1 dpa.
* It is not appropriate (for the staff) to penalize all non-Mo containing CASS (such as CF3 and CF8) because of the lower properties associated with the Mo-containing CF8M materials that are included in the ANL/NRC database, i.e., impose a lower bound.
* There is no substantive data that demonstrates a synergistic effect for CASS materials that are typical of reactor internals (such as CF3 and CF8). As such the industry has proposed criteria that do not combine TE and IE. Each mechanism is considered distinct and separate.
    " The introduction of a new criteria set for the category of materials with ferrite content between 15% to 20% having a lower proposed screening value for IE of 0.45 dpa is unnecessary and technically unfounded. The introduction of this category of ferrite content is significantly burdensome to licensees since it will require more complex and potentially more error-prone assessments of CASS material components by virtue of having more categories. Industry maintains that the categories of materials and associated ferrite levels contained in the Grimes letter are appropriate.
    " The criteria proposed by the industry (20% Ferrite and 1 dpa) have been shown to project significant margin on toughness reduction and therefore safety when compared to measured embrittlement behavior for CF3 and CF8 materials.
Regardless, this letter serves to formally submit this additional information to the NRC for review and consideration in developing a regulatory position for the screening criteria associated with TE and IE for CASS internals and to inform revisions to NUREG-4513, Rev. 1 (Reference 5). The PWR and BWR Industry position for TE and IE screening criteria is shown in Attachment D.
2
 
BWRVIP 2015-025 Irrespective of the staff's decision and future promulgation of a regulatory position on TE and IE for CASS internals, the BWRVIP formally requests the NRC to evaluate and resolve the RAI responses associated with BWRVIP-234 and issue a Safety Evaluation.
If you have any questions on this subject please call Ron DiSabatino (Exelon, BWRVIP Assessment Committee Technical Chairman) at 717.456.3685.
If you have any questions on this subject please call Ron DiSabatino (Exelon, BWRVIP Assessment Committee Technical Chairman) at 717.456.3685.
Sincerely, 24 Andrew McGehee, EPRI, BWRVIP Program Manager Tim Hanley, Exelon Corp., BWRVIP Chairman 3 BWRVIP 2015-025 Industry Response to July 15, 2014 Meeting with NRC on CASS On July 15, 2014, representatives from the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS) met with the NRC staff to discuss the thermal and irradiation embrittlement screening criteria for cast austenitic stainless steel. While the working group and NRC staff were in general agreement on the thermal embrittlement (TE) screening criteria, there was a marked difference of opinion on the irradiation embrittlement (IE) screening criteria, particularly for materials with delta ferrite contents of 15-20% (the NRC proposed 0.45 dpa, while the industry proposed 1 dpa).Agreement was reached on the TE screening criteria in part because the data on low-molybdenum and high-molybdenum material are considered separately, resulting in separate TE screening criteria for these materials.
Sincerely, 24 Andrew McGehee, EPRI, BWRVIP Program Manager Tim Hanley, Exelon Corp., BWRVIP Chairman 3
This distinction is made because high-molybdenum materials show a distinctly greater loss of fracture toughness from TE and IE effects than low-molybdenum materials.
 
This is reviewed and discussed further in Attachment A The separate consideration of low- and high-molybdenum materials test data was not carried over into the IE domain. The data set used to determine the NRC's position on IE was obtained from NUREG-7027, which considered irradiated high- and low-molybdenum materials together, along with data on irradiated welds. Because these materials were considered together, the resulting lower bound curve is judged to be overly conservative relative to the low-molybdenum material.
BWRVIP 2015-025 Industry Response to July 15, 2014 Meeting with NRC on CASS On July 15, 2014, representatives from the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS) met with the NRC staff to discuss the thermal and irradiation embrittlement screening criteria for cast austenitic stainless steel. While the working group and NRC staff were in general agreement on the thermal embrittlement (TE) screening criteria, there was a marked difference of opinion on the irradiation embrittlement (IE) screening criteria, particularly for materials with delta ferrite contents of 15-20% (the NRC proposed 0.45 dpa, while the industry proposed 1 dpa).
A reexamination of this data (see Attachment B), shows that by considering the low-molybdenum materials test data independently of the other materials it can be concluded that there is a substantial safety margin in the industry's proposed I dpa screening criteria.These screening criteria are being implemented to ensure that CASS components in reactor vessel internals maintain adequate fracture toughness during the period of extended operation.
Agreement was reached on the TE screening criteria in part because the data on low-molybdenum and high-molybdenum material are considered separately, resulting in separate TE screening criteria for these materials. This distinction is made because high-molybdenum materials show a distinctly greater loss of fracture toughness from TE and IE effects than low-molybdenum materials. This is reviewed and discussed further in Attachment A The separate consideration of low- and high-molybdenum materials test data was not carried over into the IE domain. The data set used to determine the NRC's position on IE was obtained from NUREG-7027, which considered irradiated high- and low-molybdenum materials together, along with data on irradiated welds. Because these materials were considered together, the resulting lower bound curve is judged to be overly conservative relative to the low-molybdenum material. A reexamination of this data (see Attachment B), shows that by considering the low-molybdenum materials test data independently of the other materials it can be concluded that there is a substantial safety margin in the industry's proposed I dpa screening criteria.
The screening level to determine whether this requirement was met was a J value of 255 KJ/m 2 at a crack extension of 2.5 mm. This value was originally determined for pressure boundary components (i.e., large diameter piping, etc.) and was expected to be highly conservative for application to reactor vessel internals.
These screening criteria are being implemented to ensure that CASS components in reactor vessel internals maintain adequate fracture toughness during the period of extended operation.
Additional calculations (see Attachment C) demonstrate the level of this conservatism and show that reactor vessel internal components can safely operate with fracture toughness values much lower than the 255 KJ/m 2 value specified in the Grimes letter.In summary, the actions taken by the CASS industry working group and summarized in Attachments A, B and C support the proposed screening criteria contained in Attachment D.These criteria provide a significant amount of margin for screening of TE and IE. It is concluded that that the use of the proposed screening criteria will allow for continued safe and reliable operation of the LWR fleet.4 BWRVIP 2015-025 Attachment A Discussion on Low Molybdenum vs High Molybdenum CASS Grades Introduction A meeting was held on July 15, 2014 at the NRC Office in Washington, DC between the staff of the U.S. Nuclear Regulatory Commission (NRC) and the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS). The topic of discussion focused on the thermal aging and neutron irradiation embrittlement screening criteria (separately) proposed by the industry and the NRC staff. The proposals included criteria for low-molybdenum CASS grades, such as CF-3 and CF-8, and high-molybdenum CASS grades, such as CF-8M. There was agreement between industry and the NRC staff regarding the differences in such measures of embrittlement as elastic-plastic crack growth resistance (J-R curve) for the low-Mo materials versus the high-Mo materials, at least where thermal aging embrittlement effects are dominant.
The screening level to determine whether this requirement was met was a J value of 255 KJ/m2 at a crack extension of 2.5 mm. This value was originally determined for pressure boundary components (i.e., large diameter piping, etc.) and was expected to be highly conservative for application to reactor vessel internals. Additional calculations (see Attachment C) demonstrate the level of this conservatism and show that reactor vessel internal components can safely operate with fracture toughness values much lower than the 255 KJ/m 2 value specified in the Grimes letter.
In fact, screening criteria proposed by the staff are identical to the industry-proposed screening criteria for the case of thermal aging embrittlement.
In summary, the actions taken by the CASS industry working group and summarized in Attachments A, B and C support the proposed screening criteria contained in Attachment D.
However, the areas of agreement between the industry and the staff did not carry over to combined environments where the effects of neutron irradiation embrittlement begin to approach the same level as those from thermal aging embrittlement.
These criteria provide a significant amount of margin for screening of TE and IE. It is concluded that that the use of the proposed screening criteria will allow for continued safe and reliable operation of the LWR fleet.
In order to address these differences in criteria, the available data for CF-3, CF-8, and CF-8M materials in the literature are reviewed and assessed, with a recommendation to the NRC staff for a change to their proposed criteria to more closely agree with the criteria proposed by the industry.Review and Summary of Thermal Aging Embrittlement Data The significant differences in thermal aging embrittlement behavior of the low-molybdenum grades of cast austenitic stainless steel, such as CF-3 and CF-8, versus the thermal aging embrittlement behavior of the high-molybdenum grades, such as CF-8M, have been known for at least two decades, with extensive data and associated interpretations of said data documented in NUREG/CR-4513, Revision 1 [1]. The lower-bound thermal aging embrittlement estimates shown in Figures 3 (statically-cast steels) and 4 (centrifugally-cast steels) from Reference 1 with varying amounts of delta ferrite provide an excellent illustration of those significant differences, in this case with the measure of significance being the crack-growth resistance J-R curve. In particular, the lower-bound formulas cited in Section 3.1.1 of Reference 1 (and plotted in Figures 3 and 4) can be used to compare the estimated crack growth resistance values at 2.5 mm of crack extension for the CF-3, CF-8, and CF-8M steels with > 15% delta ferrite. Note that Figure 3 provides lower-bound thermal aging estimates for static-cast steels, while Figure 4 provides lower-bound thermal aging estimates for centrifugally-cast steels.5 BWRVIP 2015-025 Crack Extension ha (in.)Crack Extension As (in.)0.06 0.10 0.15 0.00 5.-3 I S a I if 5.-3 I I a 2 3 4 S Lower-Bound J-R Curve Static-Camt Stes>15% Fentbe-290"C J =2510Aa)0-2 03-J=M4a -17&O CF-4u 0 1 2 3 4 0 0.00 0.06 0.10 0.15* I I I ji , ' , : : : , ' , : Lower-Bound J-IR Static-Cast StaWsi 10-16% Fegrkt J -274"0.3 CF035 j- 2740sa)03 2001&a)o 3 6  cF-4 ..-:j -.: '. I: 3 2 CF-Ui-4000-3000 -o-2000f.1000k 0..4000-3000 I 10.0 0.00 0.06 0.10 0.15 lOOO Lower-Bound J-R Curve Static-Cat Steels 80o. l-15% Fenml Room Temp.800- 1 -31(1P40 400 j =3074Uo-38 CF-C 400 J 130-~036-CF-SM 200-CFS 0 1 2 3 4 5 0 1 2 3 4 5 0.00 0.06 0.10 0.1(0.00 0.06 0.10 0.15 5000" 4000~3000 2000j 1 0 0 0 i 0 1 2 3 4 Crack Extension, Aa (mm)Figure 3. Predicted lower-bound J-R curves at RT and 290&deg;C for static-cast SSs with ferrite contents >15, 10-15. or<10%6 BWRVIP 2015-025 Crack Extension As (in.)0.o00. O. .O 0.1s Crack Extension ha (in.)0.00 O.06 0.10 0.15 j400-~2007 Lower-Bound J-R Curve Centrifugally Cast Steels>15% Fmist Room Tnp. J -304SO)0.3 7 JF3348 39C-CF-MM F Lower-Bound J-R Curve Centrifugally Cast Steels>15%FaFnite M-0C J.- 3301AP,340" 3 5  CF-s CF-S CF-Sm.. ......H i I 1 2 3 4 0 1 2 3 4 1 0.00 0.06 010 0.15~20)0-X0-i J.30sWKa 0 4 CF-3 r-Bound J-R Curve C " a olyCast Steels-. 357&#xfd;,,)&deg;0.00 0.0S 0.10 0.15 Lower-Bound J-R Curve Centrifugally Cast Steels 10-15% Forte0 2fOC J -300ma)&deg;35 0-36 CF-S CJ -38M&).3 CF-3-4000 7 C!-2000 'E-1000 0 i 4SO0O I-4000.I 3000-2000 I-1000 0.5000-4O O" I:-3000 20001.1000 Cf-M C0SM 0 1 2 3 S4 1 2 3 4 5 0.00 0.0 0.10 0.15 0O 30 0.06 0.10 0.15 1000 Lower-Bound J-R Curve 4001 200 -Lower-ilound' J-'R C'urv'e' .Centrifugaly Cast SteDes 410% Fernite Room TSm 0 7 P41 CF--3 CF-SM Lower-Bound J-R Curve Centrifugally Cast Steels<10% F-f-n&#xb6; J -435(Aa~5 CF-8 CF-Sm 0 1 2 3 4 5 0 2 3 4 Crack Extension., A (mm) Crack Extension, A (mm)a Figure 4. Predicted lower-bound J-R curves at RT and 290'C for centrifugally cast SSs with ferrite contents > 15. 10- 15. or < 10%7 BWRVIP 2015-025 For CF-3, the lower bound crack growth resistance, for statically-and centrifugally-cast materials, varies between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 Id/m 2.On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2.When the data are examined very closely, there is no significant difference between the static-cast lower-bound estimates for CF-3 and CF-8 in Figure 3 and the centrifugally-cast lower-bound estimates for CF-3 and CF-8 in Figure 4. The data also show that these insignificant differences are roughly identical to the differences between CF-3 and CF-8 estimates within the static-cast and centrifugally-cast populations.
4
Therefore, based on this examination of lower-bound estimates, the CF-8M data exhibit substantially lower fracture toughnesses and are therefore unsuitable as a lower-bound estimate for the low-molybdenum grades. Lower bound estimates must be conservative, but they must also remain representative of the data. Table 1, shown below, succinctly summarizes the data comparisons extracted from Figures 3 and 4 from Reference 1.Table 1. Lower Bound Fracture Toughness Estimates CASS Steels J-values at 2.5 cm of Crack Comments Growth (kJ/m 2)Lower bound above the threshold CF-3 Steels 364 to 478 value of 255 kJ/M 2 Lower bound above the threshold CF-8 Steels 343 to 451 value of 255 kj/m 2 CF-8M Steels 161 to 259 Lower bound might be less than threshold values of 255 kJ/m 2 Table 1 clearly shows that lower bound fracture toughness values of CF-3 and CF-8 steels are much higher than CF-8M steels, and that only the fracture toughness of CF-8M steels fall below the threshold value of 255 kJ/m 2.Therefore, the screening criteria for CF-8M (high molybdenum) steels should be considered separately from CF-3 and CF-8 (low molybdenum) steels.Thus far, the data evaluation has been based on lower-bound fracture toughness estimates derived from Charpy impact correlations.
 
However, these lower-bound thermal aging embrittlement estimates can be confirmed by examining actual crack extension resistance curve measurements for various heats of CF-3, CF-8, and CF-8M with delta ferrite content in the range of 20%. For example, Figure 14 from Reference 1 shows J-R curve measurements, along with thermal aging saturation estimates for two heats of CF-3 material (Heat 69 and Heat I) and one heat of CF-8 material (Heat 68), while Figure 15 from Reference 1 shows similar results for three heats of CF-8M material (Heats 74, 75, and 758).In this case, it should be noted that the actual fracture toughness data are based on thermal aging saturation conditions and are therefore somewhat higher than the lower-bound fracture toughness 8 BWRVIP 2015-025 estimates.
BWRVIP 2015-025 Attachment A Discussion on Low Molybdenum vs High Molybdenum CASS Grades Introduction A meeting was held on July 15, 2014 at the NRC Office in Washington, DC between the staff of the U.S. Nuclear Regulatory Commission (NRC) and the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS). The topic of discussion focused on the thermal aging and neutron irradiation embrittlement screening criteria (separately) proposed by the industry and the NRC staff. The proposals included criteria for low-molybdenum CASS grades, such as CF-3 and CF-8, and high-molybdenum CASS grades, such as CF-8M. There was agreement between industry and the NRC staff regarding the differences in such measures of embrittlement as elastic-plastic crack growth resistance (J-R curve) for the low-Mo materials versus the high-Mo materials, at least where thermal aging embrittlement effects are dominant. In fact, screening criteria proposed by the staff are identical to the industry-proposed screening criteria for the case of thermal aging embrittlement.
Also note that the thermal aging saturation fracture toughness data are based entirely on static-cast data for materials with delta ferrite in the range of 15% to 25%.The crack extension resistance value at 2.5 mm of crack extension for the thermal aging saturation conditions for CF-3 and CF-8 materials ranges between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material are less than half of the low-molybdenum material values.Therefore, the findings from the examination of the data in Figures 14 and 15, and the derived J values at 2.5 mm of crack extension, are completely consistent with the lower-bound thermal aging embrittlement estimates cited previously for both static-cast and centrifugally-cast material.
However, the areas of agreement between the industry and the staff did not carry over to combined environments where the effects of neutron irradiation embrittlement begin to approach the same level as those from thermal aging embrittlement. In order to address these differences in criteria, the available data for CF-3, CF-8, and CF-8M materials in the literature are reviewed and assessed, with a recommendation to the NRC staff for a change to their proposed criteria to more closely agree with the criteria proposed by the industry.
In other words, the development of screening criteria for the low-molybdenum grades should be treated separately from the development of screening criteria for the high-molybdenum grades.9 BWRVIP 2015-025 Crack Extension, An (in.)0.0 0.1 0.2 0.3 Crack Extension, An (in.)0.1 0.2 0.3 0.0 I .Heat 69 ~CF-3 2WC~2000-~1000.8,-21%290"C -SOAN 32 a 4XOy4 0 0' 0.0 -e J.366(AW).4 at320C 2 4 6 a I]0.1 0.2 0.3 I 2 0 a a-~1 I I 200 100 Heat I CF-3 o mw4g(Aa)V bwow 0 A A 0  &#xfd;L 0~ 0~2* 0.5 m~oC47 Roomm Temp. A 0 0 UABW C'.10000 "-600 I0 0-10000 0 10o~I=0-10000-6000 2 4 6 ............
Review and Summary of Thermal Aging Embrittlement Data The significant differences in thermal aging embrittlement behavior of the low-molybdenum grades of cast austenitic stainless steel, such as CF-3 and CF-8, versus the thermal aging embrittlement behavior of the high-molybdenum grades, such as CF-8M, have been known for at least two decades, with extensive data and associated interpretations of said data documented in NUREG/CR-4513, Revision 1 [1]. The lower-bound thermal aging embrittlement estimates shown in Figures 3 (statically-cast steels) and 4 (centrifugally-cast steels) from Reference 1 with varying amounts of delta ferrite provide an excellent illustration of those significant differences, in this case with the measure of significance being the crack-growth resistance J-R curve. In particular, the lower-bound formulas cited in Section 3.1.1 of Reference 1 (and plotted in Figures 3 and 4) can be used to compare the estimated crack growth resistance values at 2.5 mm of crack extension for the CF-3, CF-8, and CF-8M steels with > 15% delta ferrite. Note that Figure 3 provides lower-bound thermal aging estimates for static-cast steels, while Figure 4 provides lower-bound thermal aging estimates for centrifugally-cast steels.
1 0 0.D 0.1 0.2 0.3......1 i 4 .1 1 1. 1- 1 l 1 1 Heat 68'C"- 290C.0 =Sanm.7,40.4 S,, 32 J.46(M d2B0-0 0000 0 0&#xfd;0 00 --0 .2g0Ag 0 iIi I
5
* I U 2 4 6 8 Crack Extension, A& (Mm)10 Crack Extension, As (mm)Figure 14. Saturation fracture toughness J-R curves at RT and 290Co, estimated from the chemical composition of static-cast CF-3 and CF-8 steels, and determined experimentally 10 BWRVIP 2015-025 Crack Extension, ha (in.)Crack Extension, ha (in.)0.0 0.1 0.2 0.3 1 , .I , I I .I .I I .I .i .0.0 0.1 0.2 0.3~1000 Oj 0 0 3000-492000-.[Oo Hiai is 'C", 'Heal 75 CF-SM Ro ep Stall-Caa Slab Sc -25%.Walled 5-WA Room Temp.Unapd j .42")0.42-0 OAO~N4WrC tUegod-~J -461(A&P.3 7 -32 " 0a adI 20'8NtPA~'Co- .o32 *y oo 0 O00000OOOOC5 j .l44(AS)03
 
-., I ., .I I , ..I I ' ' '2 4 6 8 0 0.1 0.2 0.3 0 0 2 4' 6 S 14 0.0 0.1 0.2 0.3-15000 C-10000-3OO-000-15000 &#xa3;:1m.1 Heat 74 CF-SM Room T SARc--CaM Slab 6Sc= 16% Uae 040o Und J. 57" )o 0 42 0 000ht 0C =A 324 Olp 0 0. !aOC a *? * .o0 ,-- J -03*7 emp.al 320*C Heat 74 CF-SM 9*taw-cau SWa 6C16%32 efpy J 30(sa)0 3 7 32 OOY N 290'Cj~at320*C C)00N~0 O~0!!!-7 KSaknil F- J .WM~)U. 3 N s 0 0 0. 4 6 0 10 0.0 0.1 0.2 0.3 0.0 0.1 0.2 0.3 I 2000-1000.Hieat 7'581 6F4 R'' Temp.SONO-C*M Etow SC-21%Unap 32 apy 3 2 4P&I 290C at 30*C WA OA&#xa3; kj MA AL J/ 2(a03 Heat 758 CF-SM 290'C SUMc-CaN Elbow J .487(aa)0.38~ 32 Id290t Id 3py';'>eso 4 -?>(V 3,3[ 16000-10000-5000 C O*P 0 2 4 6 8 Crack Extension, Aa (mm)10 0 Crack Extension, Aa (mm)10 Figure 15. Saturation fracture toughness J-R curves at RT and 290*C. estimated from die chemical composition of static-cast CF-SM steels, and determined experimentally 11 BWRVIP 2015-025 Review and Summary of Combined TE and IE Data The available data for purely thermally-embrittled CASS materials is quite extensive.
BWRVIP 2015-025 Crack Extension ha (in.)                           Crack Extension As (in.)
However, that is not the case for a combination of thermal aging and neutron irradiation embrittlement.
0.00            0.06         0.10         0.15 Lower-Bound J-R Curve Static-Camt Stes I
In spite of the limited data, the evaluation of available crack growth resistance data for CF-3, CF-8, and CF-8M material is not altered by including information on material subjected to both thermal aging and neutron irradiation embrittlement, as shown in Figures 23, 41, 49, and 58 from ANL-12/56 [2]. The results for Specimen B-1 (static-cast CF-3 material taken from Heat 69, with approximately 24% delta ferrite, thermally aged for 10,000 hours at 400'C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 23 -taken from Reference
5.
: 2. The extrapolated J value at 2.5 mm of crack extension is 789 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 for Heat 69 from Reference 1.640 480 1-1-74 320 160 0.5 1.0 1.Crack Extension (mm)2.0 Figure 23. The J-R curve for specimen B-1.Similarly, the results for Specimen F-1 (static-cast CF-8 material taken from Heat 68, with approximately 23% delta ferrite, thermally aged for 10,000 hours at 400'C and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 41 -also taken from Reference 2.The extrapolated J value at 2.5 mm of crack extension is 657 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 from Reference 1 for Heat 68.12 BWRVIP 2015-025 640 ....Specimen F-1 CF-8, aged, 0.08 dpa 480 Low-DO high-purity water, 3200C I A J= 372"Aao.6 2 E 320 1 V, I 160 AI max 0 0.0 0.5 1.0 1.5 2.0 Crack Extension (mm)Figure 41. The J-R curve of specimen F-i.Finally, the results for Specimens I-1 (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, unaged but subjected to a neutron irradiation dose of 0.08 dpa) and J-1I (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, thermally aged for 10,000 hours at 4001C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figures 49 and 58 -also taken from Reference
                                                                  >15% Fentbe
: 2. In this case the extrapolated J value at 2.5 mm of crack extension for Specimen J-1 is 466 k/m , which can be compared to the results shown in Figure 15 from Reference I for Heat 75 that appear to be of the order of 300 to 400 kJ/m 2 at room temperature and operating temperature.
                                                                -290"C                                                 -4000
13 BWR VIP 2015-025 640 480.. ......I .I Specimen I-1 CF-8M, unaged, 0.0 Low-DO high-purity dna-~5~~cm I I I I water, 320PC .J7 mJ= 336-Aa max I'320 160 n IAamax=145 kJ/m 2 I I 0 0.5 1.0 1.5 Crack Extension (mm)Figure 49. The JR curve of specimen I-1.2.0 640 480 (N-320 160 2.0 Crack Extension (mm)Figure 58. The JR curve of specimen J-1.14 BWRVIP 2015-025 Conclusions and Recommendation This review and summary of available data on CF-3, CF-8, and CF-8M CASS materials subjected to both individual and combined effects of thermal aging and neutron irradiation embrittlement demonstrated that: Thermal aging embrittlement effects on high-Mo grades are significantly more pronounced than the effects on the low-Mo grades, by roughly a factor of two or more based upon lower-bound crack growth resistance estimates.
  -3                                                                                                        0 J =2510Aa)
For CF-3, the lower-bound crack growth resistance values at 2.5 mm of crack extension for > 15% delta ferrite vary between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 kJ/m 2.On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2 which are significantly lower compared to CF-3/8. These results are consistent with the results obtained by examining actual crack growth resistance value measurements at 2.5 mm of crack extension for the thermal aging to saturation for CF-3 and CF-8 materials (low-Mo) that range between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material (high-Mo) are less than half of the low-molybdenum material values.* There is no significant difference between the static-cast lower-bound estimates and the centrifugally-cast lower-bound estimate for CF-3 and CF-8 materials, and those relatively small differences are roughly identical to differences between CF-3 and CF-8 lower-bound estimates.
                                                                          -   2     03-                               -3000  -
Using lower-bound crack growth resistance values at 2.5 mm of crack extension as the comparative measure, the CF-3 static-cast values of 364 and 410 kJ/m 2 compare very well to the 477 and 478 kJ/m 2 values for centrifugally-cast material, while the CF-8 static-cast values of 343 and 366 kJ/m 2 compare favorably with the 427 and 451 kJ/m 2 values for centrifugally-cast material.
17&O
The differences between static-cast and centrifugally-cast values, and between CF-3 and CF-8 values are both inconsequential in comparison to the differences between low-Mo and high-Mo materials.
                                                                                          - J=M4a                      -2000f o
Therefore these two grades may be considered as a combined category for screening purposes.* The added effect of neutron irradiation embrittlement does not change the conclusions drawn with respect to low-Mo versus high-Mo fracture toughness.
                                                                                                                        .1000k CF-4u 0.
Finally, since the conclusions are drawn primarily from static-cast fracture toughness data, a recommendation to the NRC staff to maintain the screening threshold for low-Mo static-cast grades at 20% is supported by the data.Therefore, this review shows that the CF-8M data provide an extremely conservative and thus unrepresentative lower bound to the data for the low-molybdenum grades. As such, the CF-8M lower bound is separable and distinct from the low-molybdenum grade lower bounds, which therefore require their own screening category and fracture toughness estimates.
0            1          2        3            4      0 2        3         4     S 0.00          0.06    0.10        0.15        0.00             0.06         0.10         0.15
Thus, the delta ferrite levels stated in the BWRVIP-234 RAI response (from the Grimes letter) is further supported by this evaluation.
                                                                        *I I         , 'I , : : :           ji , ' , :
lOOO Lower-Bound J-R Curve                            Lower-Bound J-IR Static-Cat Steels                                Static-Cast StaWsi aS    80o. l-15%Fenml                                      10-16% Fegrkt Room Temp.                                                                      J - 274"0.3           .4000 36        j- 2740sa)03 2001&a)o         cF-4             ..
800-     1 - 31(1P40 I
CF035                              -3000
* 400                                  j =3074Uo-38                                                                      I CF-C 400                      J 130-~036 200-                      -          CF-SM                                                    32                  10
                                                                  -  :j        -         .: '. I:
CF-Ui CFS                                                                        .0 0          1      2        3          4    5  0            1          2        3            4      5 0.00          0.06    0.10        0.1(        0.00             0.06         0.10         0.15 5000" 5.
if 4000~
  -3 3000 I
Ia                                                                                                                    2000j 1000i 0
1       2       3         4 Crack Extension, Aa (mm)
Figure3.           Predictedlower-bound J-R curves at RT and 290&deg;C for static-castSSs with ferrite contents >15, 10-15. or<10%
6
 
BWRVIP 2015-025 Crack Extension As (in.)                                   Crack Extension ha (in.)
0.o00.               O.     .O           0.1s             0.00           O.06       0.10         0.15 Lower-Bound J-R Curve                                    Lower-Bound J-R Curve Centrifugally Cast Steels                                 Centrifugally Cast Steels
            >15% Fmist                               0 37            >15%FaFnite Room Tnp.                   J - 304SO) .                 M-0C                    J.-3301AP,34      -4000  7 0 35 J.934r*a)    "         CF-s JF3348 39C-                                                                      CF-S C!
j400-CF-MM                                                                      -2000 '
E
~2007                                                                                                              -1000 CF-Sm
                          .. .. . . . . H                   i F                                                      0 I         1       2           3           4           0           1         2         3         4 1 0.00           0.06       010           0.15             0.00          0.0S        0.10          0.15 i
r-Bound J-R Curve                                 Lower-Bound J-R Curve C a " olyCast Steels                              Centrifugally Cast Steels 4SO0OI 10-15% Forte0                               -4000.
    )0-                                                                2fOC                 J - 300ma)&deg;35                 I 04                                                        0-36     CF-S J.30sWKa i                                                          CJ- 38M&).3 X0-    CF-3                                                       CF-3                                          3000
                                -. *    '* *. 357&#xfd;,,)&deg;
                                                                                                                    -2000 I
~20                                                                                                                -1000 Cf-M                                             C0SM 0
0          1       2         3                     S4             1         2         3         4 5 0O30            0.06        0.10          0.15            0.00          0.0         0.10         0.15 1000       Lower-Bound J-R Curve Lower-ilound' J-'R C'urv'e'                 .             Lower-Bound J-R Curve Centrifugaly Cast SteDes                                 Centrifugally Cast Steels                    .5000 410% Fernite                                                                                           - 4OO"
                                                                        <10% F-f-n&#xb6; Room TSm              07                                  2*0T P41 J -435(Aa~5                                         I:
                                                                                                                    -3000  -2 CF--3                                                                      CF-8 4001
                                                                                                                    -20001 200 -                            CF-SM                                                      CF-Sm               .1000 a
0           1       2         3             4       5   0                     2         3         4 Crack Extension., A (mm)                                   Crack Extension, A (mm)
Figure 4.         Predictedlower-bound J-R curves at RT and 290'C for centrifugally cast SSs with ferrite contents > 15. 10-15. or < 10%
7
 
BWRVIP 2015-025 For CF-3, the lower bound crack growth resistance, for statically- and centrifugally-cast materials, varies between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 Id/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2. When the data are examined very closely, there is no significant difference between the static-cast lower-bound estimates for CF-3 and CF-8 in Figure 3 and the centrifugally-cast lower-bound estimates for CF-3 and CF-8 in Figure 4. The data also show that these insignificant differences are roughly identical to the differences between CF-3 and CF-8 estimates within the static-cast and centrifugally-cast populations. Therefore, based on this examination of lower-bound estimates, the CF-8M data exhibit substantially lower fracture toughnesses and are therefore unsuitable as a lower-bound estimate for the low-molybdenum grades. Lower bound estimates must be conservative, but they must also remain representative of the data. Table 1, shown below, succinctly summarizes the data comparisons extracted from Figures 3 and 4 from Reference 1.
Table 1. Lower Bound Fracture Toughness Estimates CASS Steels           J-values at 2.5 cm of2 Crack                 Comments Growth (kJ/m )
Lower bound above the threshold 2
CF-3 Steels                 364 to 478                       value of 255 kJ/M Lower bound above the threshold 2
CF-8 Steels                 343 to 451                       value of 255 kj/m CF-8M Steels                   161 to 259                 Lower bound might be less than2 threshold values of 255 kJ/m Table 1 clearly shows that lower bound fracture toughness values of CF-3 and CF-8 steels are much higher than CF-8M steels, and that only the fracture toughness of CF-8M steels fall below the threshold value of 255 kJ/m 2. Therefore, the screening criteria for CF-8M (high molybdenum) steels should be considered separately from CF-3 and CF-8 (low molybdenum) steels.
Thus far, the data evaluation has been based on lower-bound fracture toughness estimates derived from Charpy impact correlations. However, these lower-bound thermal aging embrittlement estimates can be confirmed by examining actual crack extension resistance curve measurements for various heats of CF-3, CF-8, and CF-8M with delta ferrite content in the range of 20%. For example, Figure 14 from Reference 1 shows J-R curve measurements, along with thermal aging saturation estimates for two heats of CF-3 material (Heat 69 and Heat I) and one heat of CF-8 material (Heat 68), while Figure 15 from Reference 1 shows similar results for three heats of CF-8M material (Heats 74, 75, and 758).
In this case, it should be noted that the actual fracture toughness data are based on thermal aging saturation conditions and are therefore somewhat higher than the lower-bound fracture toughness 8
 
BWRVIP 2015-025 estimates. Also note that the thermal aging saturation fracture toughness data are based entirely on static-cast data for materials with delta ferrite in the range of 15% to 25%.
The crack extension resistance value at 2.5 mm of crack extension for the thermal aging saturation conditions for CF-3 and CF-8 materials ranges between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material are less than half of the low-molybdenum material values.
Therefore, the findings from the examination of the data in Figures 14 and 15, and the derived J values at 2.5 mm of crack extension, are completely consistent with the lower-bound thermal aging embrittlement estimates cited previously for both static-cast and centrifugally-cast material. In other words, the development of screening criteria for the low-molybdenum grades should be treated separately from the development of screening criteria for the high-molybdenum grades.
9
 
BWRVIP 2015-025 Crack Extension, An (in.)                           Crack Extension, An (in.)
0.0         0.1     0.2           0.3           0.0 I .           0.1           0.2           0.3 2WC Heat 69 ~CF-3                               290"C -
C' 8,-21%
  ~2000-                                                                                                              .10000 "
SOAN32 a           4XOy4 0           0'
                                                                                                                          -600 0.
  ~1000.                                                                                  0                   -e 0
J.366(AW).4         at320C I0 2         4         6         a           I0
          ]         0.1     0.2         0.3 Heat I CF-3 0
o mw4g(Aa)V bwow         A 0         A   &#xfd;L 200                                                                                                              0 2                                                                                  -10000 I
0~
* 0~ 0 10o~
100 20 a              Roomm Temp.
                            .5 m~oC47 A00        UABW 2     4       6 . ........... 10                                                            0 I=
0.D             0.1           0.2           0.3
                                                                  .. . .   . .       1 i 4 .1 1 1. 1- 1 l       1 1 Heat 68'C"-                                 290C a-
                                                            .0       =Sanm.7,40.4
~1                                                                          S,,   32           J.46(M             -10000 I                                                                                  d2B0 I                                                              -
00 0     0000 0
                                                                              --                0 0&#xfd;0
                                                                                                                    -6000 0                     .2g0Ag iIi I
* I     U 2         4         6         8           10 Crack Extension, As (mm)                           Crack Extension, A& (Mm)
Figure 14. Saturationfracture toughness J-R curves at RT and 290Co, estimatedfrom the chemical composition of static-cast CF-3 and CF-8 steels, and determined experimentally 10
 
BWRVIP 2015-025 Crack Extension, ha (in.)                                                 Crack Extension, ha (in.)
0.0               0.1             0.2             0.3                   0.01 , . I , I 0.1I . I .
0.2 I I . I . 0.3 i.
Heal Hiai is75 'C",
CF-SM       '              Ro Room Temp.      ep Stall-Caa Slab                                                                                                                     -15000 C Sc
                    - 25%
Unapd
                    .       Walled j . 42")0.42                           -     0OAO~N4WrC                   tUegod 5-WA                                                                -         ~J                   -461(A&P.
37
                                                                                                                                                -  -10000 32 "                             0a                         -3OO
                            'Co- .o32 *y         oo0      O00000OOOOC5
  ~1000                                                                                        adI20' 8NtPA~
Oj                                                        j .l44(AS)03                                                                           -000
              -   .   , 2 I .   , . 4I      I,     6 . .     I 8I '       ' '   0  0            2           4'        6             S      14 00
          .10            0.1             0.2               0.3                   0.0             0.1           0.2             0.3 3000-Heat 74 CF-SM                            Room T emp.                     Heat 74 CF-SM                                     9*
SARc--CaM Slab                                                             taw-cau SWa 6Sc=16%                           Uae
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[Oo          040o       Und                   J. 57" 0
                                                                )o 42                                                                             -15000  &#xa3; 492000-              0     =A000ht 0C 03 7 324Olp                                                                                          32 efpy      J 30(sa)
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0                                                    at320*C               C)00N aOCa              *?    *    .o0        0.!                                                      ~0 O~0
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s             0   0             0.       4   0      6                     10 0.0             0.1           0.2             0.3 0.0               0.1             0.2               0.3 Hieat 7'581 6F4                         R''         Temp.               Heat 758 CF-SM                                  290'C SONO-C*M Etow                                                             SUMc-CaN Elbow                                          [  16000 SC-21%Unap 2000-
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J .487(aa) . 38~Id290t        32 Id  3py C
1000.                                              &I290C          at 30*C
                                                                                                                                                    -5000 WAOA&#xa3; kj               MA AL                                           ';'>eso J/   2(a03 4-?>(V      3,3 O*P 0             2           4             6               8           10  0                                                            10 Crack Extension, Aa (mm)                                                 Crack Extension, Aa (mm)
Figure 15.         Saturationfracture toughness J-R curves at RT and 290*C. estimated from die chemical composition of static-castCF-SM steels, and determined experimentally 11
 
BWRVIP 2015-025 Review and Summary of Combined TE and IE Data The available data for purely thermally-embrittled CASS materials is quite extensive. However, that is not the case for a combination of thermal aging and neutron irradiation embrittlement. In spite of the limited data, the evaluation of available crack growth resistance data for CF-3, CF-8, and CF-8M material is not altered by including information on material subjected to both thermal aging and neutron irradiation embrittlement, as shown in Figures 23, 41, 49, and 58 from ANL-12/56 [2]. The results for Specimen B-1 (static-cast CF-3 material taken from Heat 69, with approximately 24% delta ferrite, thermally aged for 10,000 hours at 400'C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 23 - taken from Reference 2. The extrapolated J value at 2.5 mm of crack extension is 789 kJ/m 2, very similar to the saturated, thermally-aged result, as shown in Figure 14 for Heat 69 from Reference 1.
640 480 1-1 320
        -74 160 0.5             1.0           1.             2.0 Crack Extension (mm)
Figure 23. The J-R curve for specimen B-1.
Similarly, the results for Specimen F-1 (static-cast CF-8 material taken from Heat 68, with approximately 23% delta ferrite, thermally aged for 10,000 hours at 400'C and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 41 - also taken from Reference 2.
The extrapolated J value at 2.5 mm of crack extension is 657 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 from Reference 1 for Heat 68.
12
 
BWRVIP 2015-025 640                       . .   . .
Specimen F-1 CF-8, aged, 0.08 dpa 480       Low-DO high-purity water, 3200CI            A 62 J=1 372"Aao.
E 320 V,       I 160                                               AI max 0
0.0           0.5           1.0             1.5           2.0 Crack Extension (mm)
Figure 41. The J-R curve of specimen F-i.
Finally, the results for Specimens I-1 (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, unaged but subjected to a neutron irradiation dose of 0.08 dpa) and J-1I (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, thermally aged for 10,000 hours at 4001C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figures 49 and 58 - also taken from Reference 2. In this case the extrapolated J value at 2.5 mm of crack extension for Specimen J-1 is 466 k/m , which can be compared to the results shown in Figure 15 from Reference forI Heat 75 that appear to be of the order of 300 to 400 kJ/m 2 at room temperature and operating temperature.
13
 
BWR VIP 2015-025 640   ..     .       I  .I .     .       .   .     .
Specimen I-1 CF-8M, unaged, 0.0       -
dna
                                          ~5~~
Low-DO high-purity       water,       320PC           .
480 I
I mJ= J7 I
cm                                                            336-Aa I
320 max     I' 160 IAamax 2
                              =145 kJ/m I
n                  I 0               0.5             1.0             1.5         2.0 Crack Extension (mm)
Figure 49. The JR curve of specimen I-1.
640 480 (N-320 160 2.0 Crack Extension (mm)
Figure 58. The JR curve of specimen J-1.
14
 
BWRVIP 2015-025 Conclusions and Recommendation This review and summary of available data on CF-3, CF-8, and CF-8M CASS materials subjected to both individual and combined effects of thermal aging and neutron irradiation embrittlement demonstrated that:
Thermal aging embrittlement effects on high-Mo grades are significantly more pronounced than the effects on the low-Mo grades, by roughly a factor of two or more based upon lower-bound crack growth resistance estimates. For CF-3, the lower-bound crack growth resistance values at 2.5 mm of crack extension for > 15% delta ferrite vary between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 kJ/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2 which are significantly lower compared to CF-3/8. These results are consistent with the results obtained by examining actual crack growth resistance value measurements at 2.5 mm of crack extension for the thermal aging to saturation for CF-3 and CF-8 materials (low-Mo) that range between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material (high-Mo) are less than half of the low-molybdenum material values.
* There is no significant difference between the static-cast lower-bound estimates and the centrifugally-cast lower-bound estimate for CF-3 and CF-8 materials, and those relatively small differences are roughly identical to differences between CF-3 and CF-8 lower-bound estimates. Using lower-bound crack growth resistance values at 2.5 mm of crack 2
extension as the comparative measure, the CF-3 static-cast values of 364 and 410 kJ/m compare very well to the 477 and 478 kJ/m 2 values for centrifugally-cast material, while the CF-8 static-cast values of 343 and 366 kJ/m 2 compare favorably with the 427 and 451 kJ/m 2 values for centrifugally-cast material. The differences between static-cast and centrifugally-cast values, and between CF-3 and CF-8 values are both inconsequential in comparison to the differences between low-Mo and high-Mo materials. Therefore these two grades may be considered as a combined category for screening purposes.
* The added effect of neutron irradiation embrittlement does not change the conclusions drawn with respect to low-Mo versus high-Mo fracture toughness. Finally, since the conclusions are drawn primarily from static-cast fracture toughness data, a recommendation to the NRC staff to maintain the screening threshold for low-Mo static-cast grades at 20% is supported by the data.
Therefore, this review shows that the CF-8M data provide an extremely conservative and thus unrepresentative lower bound to the data for the low-molybdenum grades. As such, the CF-8M lower bound is separable and distinct from the low-molybdenum grade lower bounds, which therefore require their own screening category and fracture toughness estimates. Thus, the delta ferrite levels stated in the BWRVIP-234 RAI response (from the Grimes letter) is further supported by this evaluation.
Finally, this review and the associated quantitative comparisons utilize the data sets as delineated in extensive documentation in NUREG/CR-4513, Revision 1 [1] and other relevant publically available references.
Finally, this review and the associated quantitative comparisons utilize the data sets as delineated in extensive documentation in NUREG/CR-4513, Revision 1 [1] and other relevant publically available references.
15 BWRVIP 2015-025 References
15
[1]. 0. K. Chopra, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," NUREG/CR-4513 (ANL-93/22), Revision 1, Argonne National Laboratory, Argonne, Illinois (August 1994).[2]. Y. Chen, B. Alexandreanu, and K. Natesan, "Crack Growth Rate and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Report No. ANL-12/56, Argonne National Laboartory, Argonne, Illinois (November 2012).16 BWRVIP 2015-025 Attachment B Conclusions Regarding Screening Criteria for Irradiation Embrittlement of CASS Materials The screening criteria for TE and IE in CASS components proposed and discussed with the NRC[1] appears to be based on materials testing data that includes a high-molybdenum material, grade CF-8M, presented in Figure 64 in NUREG 7027 [2], with the following conclusions on page 79: 1. CF-8M materials represent a 'worst case' for thermal embrittlement
 
: 2. Thermal aging does not seem to lower the toughness below that expected for irradiation alone at the dose levels examined.In regards to the use of this data, it is important to note that:* CF-8M materials are not present in LWR core internal components.
BWRVIP 2015-025 References
* Moreover, the embrittlement identified in NUREG-7027 is conservative because many of the heats examined had delta ferrite contents greater than 20% and as high as 42% [3].It is also important to emphasize that in LWR reactor internals, delta ferrite content does not typically exceed 20% as compared to the materials assessed in the NUREG database[2, 3].* Loss of fracture toughness due to thermal embrittlement is driven by the amount of delta ferrite in a given material, thus the use of high delta ferrite material data is also conservative.
[1]. 0. K. Chopra, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," NUREG/CR-4513 (ANL-93/22), Revision 1, Argonne National Laboratory, Argonne, Illinois (August 1994).
* ANL results comparing loss of fracture toughness measurements on unaged, thermally aged only, irradiation aged only and sequentially thermally aged and irradiation aged CF-3 and CF-8 materials show significant loss of toughness on all forms of aging.Measured toughnesses of thermally aged, irradiation aged and sequentially thermal plus irradiation aged materials are similar. Given the variances that are inherent in estimating J values as material characteristics, the differences in loss of toughness cited in Reference 4 cannot be taken to unequivocally demonstrate that irradiation and thermal aging are significantly additive effects to the loss of toughness in CF-3 and CF-8 cast austenitic stainless steels.* The data summarized in Figure 64 of NUREG-7027 includes many high ferrite content and Mo-containing chemical compositions.
[2]. Y. Chen, B. Alexandreanu, and K. Natesan, "Crack Growth Rate and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Report No. ANL-12/56, Argonne National Laboartory, Argonne, Illinois (November 2012).
The correlations developed in analyses based on this database are therefore expected to be very conservative with regard to the irradiation and thermal response of low ferrite content and low Mo containing chemical compositions.
16
17 BWRVIP 2015-025 The NRC is concerned that interaction between thermal and irradiation embrittlement mechanisms may lower the fracture toughness of CASS material below levels expected from the effect of either mechanism alone. Based on the potential for a synergistic effect and taking into account the NUREG-7027 data, the NRC has concluded that a very low level of irradiation would reduce the fracture toughness of a CASS component below the 255 KJ/m 2 criteria.This led to the NRC proposing a neutron irradiation screening criteria of 0.45 dpa for low molybdenum static CASS components with 15-20% delta ferrite. By reexamination of the data in NUREG-7027 a considerable amount of conservatism can be removed from the analysis while still providing reasonable assurance that CASS components in the LWR environment will retain adequate fracture toughness through the period of extended operations.
 
The irradiated materials data from NUREG-7027 were digitized from the plots of NUREG-7027 and reanalyzed to produce a trend curve for irradiated CF-3 and CF-8 materials only as shown in Figure 1 below. Note that the exposures of these materials not only represent irradiation effects but also some degree of thermal embrittlement.
BWRVIP 2015-025 Attachment B Conclusions Regarding Screening Criteria for Irradiation Embrittlement of CASS Materials The screening criteria for TE and IE in CASS components proposed and discussed with the NRC
These data for CF-3 and CF-8 materials are most relevant to the behavior of CASS in LWR internals, as these are the materials that are principally known to be present in LWR reactor internals.
[1] appears to be based on materials testing data that includes a high-molybdenum material, grade CF-8M, presented in Figure 64 in NUREG 7027 [2], with the following conclusions on page 79:
Thus the correlation and proposed screening criteria are appropriately developed for these materials.
: 1. CF-8M materials represent a 'worst case' for thermal embrittlement
As an outcome of this analysis a plot of fracture toughness against neutron exposure was created, and a 'best fit' line was developed and the resulting curve was calculated to have a strong correlation with the data (R 2=0.94). The best fit line was then modified using conservative engineering judgment and standard curve offsetting techniques to bound all of the irradiated CF-3 and CF-8 material measured toughness values. (i.e., the pre-exponential constant multiplier was reduced by approximately 25% and the exponential factor was increased by 35% in order to bound every data point above the red-line exponential curve fit.) A constant of 30 kJ/m 2 was also included as a saturated fracture toughness value.This saturated fracture toughness value is proposed by Chopra in NUREG-7027, and the overall form of the equation is consistent with irradiation hardening models [6]. This results in a curve fit where all data points are above the curve, with resulting curve fit of: KJ e_.25xdpa J2.Smm = 30 + 520 -- x e x This bounding line is shown as a red line in Figure 1.By using the red (lower bound) line as a gauge for how CF-3 and CF-8 materials will age in the LWR environment, it can be shown that these materials will not encroach upon the 255 KJ/m 2 fracture toughness limit until the fluence level experienced by these components approaches 3.3 dpa. The industry proposed use of I dpa for neutron exposure screening criteria, provides more than a 2 dpa margin on neutron exposure between a CASS component at 1 dpa and the 255 18 BWRVIP 2015-025 KJ/m 2 fracture toughness limit. At 1 dpa, the fracture toughness predicted by the bounding curve in Figure 1 is 435 KJ/m 2 , which results in a fracture toughness margin of 180 KJ/m 2.Therefore, the industry's proposed criterion of 1 dpa has substantial margin in both the fluence and fracture toughness domains. This analysis and argument supports the use of the irradiation screening criteria of I dpa proposed by the industry for low molybdenum CASS components with ferrite content less than 20 percent.Additionally, a study designed to investigate the potential interaction between thermal and irradiation embrittlement mechanisms concluded that irradiation can reduce the extent of thermal aging effects [5], suggesting an antergistic effect between the two mechanisms rather than a synergistic one.This information indicates that the NRC's position is highly conservative, and that the industry's position on the screening criteria of CASS components, while also conservative, is justified.
: 2. Thermal aging does not seem to lower the toughness below that expected for irradiation alone at the dose levels examined.
In regards to the use of this data, it is important to note that:
* CF-8M materials are not present in LWR core internal components.
* Moreover, the embrittlement identified in NUREG-7027 is conservative because many of the heats examined had delta ferrite contents greater than 20% and as high as 42% [3].
It is also important to emphasize that in LWR reactor internals, delta ferrite content does not typically exceed 20% as compared to the materials assessed in the NUREG database
[2, 3].
* Loss of fracture toughness due to thermal embrittlement is driven by the amount of delta ferrite in a given material, thus the use of high delta ferrite material data is also conservative.
* ANL results comparing loss of fracture toughness measurements on unaged, thermally aged only, irradiation aged only and sequentially thermally aged and irradiation aged CF-3 and CF-8 materials show significant loss of toughness on all forms of aging.
Measured toughnesses of thermally aged, irradiation aged and sequentially thermal plus irradiation aged materials are similar. Given the variances that are inherent in estimating J values as material characteristics, the differences in loss of toughness cited in Reference 4 cannot be taken to unequivocally demonstrate that irradiation and thermal aging are significantly additive effects to the loss of toughness in CF-3 and CF-8 cast austenitic stainless steels.
* The data summarized in Figure 64 of NUREG-7027 includes many high ferrite content and Mo-containing chemical compositions. The correlations developed in analyses based on this database are therefore expected to be very conservative with regard to the irradiation and thermal response of low ferrite content and low Mo containing chemical compositions.
17
 
BWRVIP 2015-025 The NRC is concerned that interaction between thermal and irradiation embrittlement mechanisms may lower the fracture toughness of CASS material below levels expected from the effect of either mechanism alone. Based on the potential for a synergistic effect and taking into account the NUREG-7027 data, the NRC has concluded that a very low level of irradiation would reduce the fracture toughness of a CASS component below the 255 KJ/m 2 criteria.
This led to the NRC proposing a neutron irradiation screening criteria of 0.45 dpa for low molybdenum static CASS components with 15-20% delta ferrite. By reexamination of the data in NUREG-7027 a considerable amount of conservatism can be removed from the analysis while still providing reasonable assurance that CASS components in the LWR environment will retain adequate fracture toughness through the period of extended operations.
The irradiated materials data from NUREG-7027 were digitized from the plots of NUREG-7027 and reanalyzed to produce a trend curve for irradiated CF-3 and CF-8 materials only as shown in Figure 1 below. Note that the exposures of these materials not only represent irradiation effects but also some degree of thermal embrittlement. These data for CF-3 and CF-8 materials are most relevant to the behavior of CASS in LWR internals, as these are the materials that are principally known to be present in LWR reactor internals. Thus the correlation and proposed screening criteria are appropriately developed for these materials.
As an outcome of this analysis a plot of fracture toughness against neutron exposure was created, and a 'best fit' line was developed and the resulting curve was calculated to have a strong correlation with the data (R2=0.94). The best fit line was then modified using conservative engineering judgment and standard curve offsetting techniques to bound all of the irradiated CF-3 and CF-8 material measured toughness values. (i.e., the pre-exponential constant multiplier was reduced by approximately 25% and the exponential factor was increased by 35% in order to bound every data point above the red-line exponential curve fit.) A constant of 30 kJ/m 2 was also included as a saturated fracture toughness value.
This saturated fracture toughness value is proposed by Chopra in NUREG-7027, and the overall form of the equation is consistent with irradiation hardening models [6]. This results in a curve fit where all data points are above the curve, with resulting curve fit of:
KJ     e_.25xdpa J2.Smm =       30 + 520 -- x e             x This bounding line is shown as a red line in Figure 1.
By using the red (lower bound) line as a gauge for how CF-3 and CF-8 materials will age in the 2
LWR environment, it can be shown that these materials will not encroach upon the 255 KJ/m fracture toughness limit until the fluence level experienced by these components approaches 3.3 dpa. The industry proposed use of I dpa for neutron exposure screening criteria, provides more than a 2 dpa margin on neutron exposure between a CASS component at 1 dpa and the 255 18
 
BWRVIP 2015-025 KJ/m 2 fracture toughness limit. At 1 dpa, the fracture toughness predicted by the bounding curve in Figure 1 is 435 KJ/m 2 , which results in a fracture toughness margin of 180 KJ/m 2 .
Therefore, the industry's proposed criterion of 1 dpa has substantial margin in both the fluence and fracture toughness domains. This analysis and argument supports the use of the irradiation screening criteria of I dpa proposed by the industry for low molybdenum CASS components with ferrite content less than 20 percent.
Additionally, a study designed to investigate the potential interaction between thermal and irradiation embrittlement mechanisms concluded that irradiation can reduce the extent of thermal aging effects [5], suggesting an antergistic effect between the two mechanisms rather than a synergistic one.
This information indicates that the NRC's position is highly conservative, and that the industry's position on the screening criteria of CASS components, while also conservative, is justified.


==References:==
==References:==
: 1. U.S. NRC, "NRC Staff Compiled Comments on Industry CASS Screening Position," July 18, 2014 (NRC ADAMS Accession Number ML14198A282.
: 1. U.S. NRC, "NRC Staff Compiled Comments on Industry CASS Screening Position,"
: 2. NUREG/CR-7027, "Degradation of LWR Core Internal Materials due to Neutron Irradiation," December, 2010 (NRC ADAMS Accession Number ML 102790482.
July 18, 2014 (NRC ADAMS Accession Number ML14198A282.
: 2. NUREG/CR-7027, "Degradation of LWR Core Internal Materials due to Neutron Irradiation," December, 2010 (NRC ADAMS Accession Number ML102790482.
: 3. NUREG/CR-4513, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," U.S. Nuclear Regulatory Commission, August 1994 (NRC ADAMS Accession No. ML052360554).
: 3. NUREG/CR-4513, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," U.S. Nuclear Regulatory Commission, August 1994 (NRC ADAMS Accession No. ML052360554).
: 4. ANL-12/56, "Crack Growth and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Argonne National Lab., November 2012.5. K Fuji, K. Fukuya, "Effects of Radiation on Spinodal Decomposition of Ferrite in Duplex Stainless Steel," Journal of Nuclear Materials, May 2012. Presented at the NuMat 2012 Conference, pages 613 to 616, October 22-25, 2012, Osaka, Japan.6. Was, Gary S., "Fundamentals of Radiation Materials Science: Metals and Alloys," Springer-Verlag, 2007.7. Kim, C., R. Lott, S. Byrne, M. Burke, and G. Gerzen, "Embrittlement of Cast Austenitic Stainless Steel Reactor Internals Components," Proc. 6th Intl. Symp. On Contribution of Materials Investigations to Improve the Safety and Performance of LWRs, Fontevraud 6, French Nuclear Energy Society, SFEN, Fontevraud Roayal Abbey, France, September 18-22, 2006.19 BWRVIP 2015-025 Figure 1 -Irradiated CF-3 and CF-8 Fracture Toughness Data from Literature (Refs. 2, 4 and 7)Fracture Toughness of Irradiated CF3 and CF8 (0.02 dpa and greater)1000 900 800 700 E 500~400 300 200 100 0 0 1 2 3 4 5 6 7 8 9 10 Neutron Exposure (dpa)11 12 13 14 15 16 17 18 20 Attachment C Reactor Internals CASS Flaw Tolerance In the draft Interim Staff Guidance (ISG) on Aging Management of CASS Reactor Vessel Internal Components, issued in June 2014, the NRC technical position observed that "The fracture toughness screening.
: 4. ANL-12/56, "Crack Growth and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Argonne National Lab., November 2012.
value of 255 kJ/m 2 specified in the Grimes Letter is based on a generic flaw tolerance evaluation for piping, and may be overly conservative for RVI CASS components that are subject to mainly compressive stresses during operation, and are part of a population of redundant components where failure of individual components can be tolerated." The technical position went on to add that "therefore, the staff applies the 255 kJ/m 2 value for screening purposes with the knowledge that there likely is additional conservatism present in this screening for non-pressure boundary RVI components." In an effort to provide further evidence with respect to the NRC staff technical position, some industry efforts since the July 15, 2014 meeting with the NRC staff have been directed toward this issue. The results are summarized in the following paragraphs.
: 5. K Fuji, K. Fukuya, "Effects of Radiation on Spinodal Decomposition of Ferrite in Duplex Stainless Steel," Journal of Nuclear Materials, May 2012. Presented at the NuMat 2012 Conference, pages 613 to 616, October 22-25, 2012, Osaka, Japan.
The industry selected three different geometries that can be related to typical BWR and PWR CASS reactor internals in order to estimate flaw tolerance capability:
: 6. Was, Gary S., "Fundamentals of Radiation Materials Science: Metals and Alloys,"
(1) a large-diameter cylinder with a through-wall vertical flaw located in a longitudinal seam weld, subjected to combined membrane and bending stress; (2) an edge-cracked beam-column subjected to combined membrane and bending stress; and (3) a six-inch-diameter, Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure.
Springer-Verlag, 2007.
The internal pressure for the third geometry was selected such that the circumferential tensile stress in the pipe was identical to the membrane tensile stress level chosen for the first two geometries.
: 7. Kim, C., R. Lott, S. Byrne, M. Burke, and G. Gerzen, "Embrittlement of Cast Austenitic Stainless Steel Reactor Internals Components," Proc. 6th Intl. Symp. On Contribution of Materials Investigations to Improve the Safety and Performance of LWRs, Fontevraud 6, French Nuclear Energy Society, SFEN, Fontevraud Roayal Abbey, France, September 18-22, 2006.
In all three case studies, the initial flaw size (length for the first and third geometries, and depth for the second geometry) was selected to be consistent with reactor vessel internals fabrication workmanship standards.
19
No flaw growth criteria were applied to the initial flaw sizes, although the initial flaw sizes were increased to some extent in order to determine the rate at which the crack driving force increased as a function of the increase in flaw size.For the first geometry (large-diameter cylinder with through-wall vertical flaw), the diameter was selected to be 452 inches with a wall thickness of either one or two inches, the membrane tensile stress was selected to be 5 ksi, and the bending stress was selected to be 7.5 ksi. The total initial flaw length was selected to be 0.226 inches (about 1/4-inch in length), but was increased in increments up to 4.294 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. For the largest initial flaw lengths examined, the typical LEFM stress intensity is of the order of 25 ksiin, which converts to an elastic-plastic crack driving force of about 4 kJ/m 2.This implies a very large margin relative to the screening value of 255 kJ/m 2.For the second geometry (edge-cracked beam column), the solid column diameter was selected to be three inches, and the membrane and bending stresses were selected to be identical to those selected for the first geometry.
 
The smallest initial flaw depth was selected as 0.1 inches, and was incremented by 0.1 inch up to a maximum depth of 1.7 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 lillview Avenue, Palo Alto, CA 94304-1395 USA
BWRVIP 2015-025 Figure 1 - Irradiated CF-3 and CF-8 Fracture Toughness Data from Literature (Refs. 2, 4 and 7)
Fracture Toughness of Irradiated CF3 and CF8 (0.02 dpa and greater) 1000 900 800 700 E   500
  ~400 300 200 100 0
0 1     2     3     4       5     6       7       8     9     10     11     12     13 14 15 16 17 18 Neutron Exposure (dpa) 20
 
Attachment C Reactor Internals CASS Flaw Tolerance In the draft Interim Staff Guidance (ISG) on Aging Management of CASS Reactor Vessel Internal Components, issued in June 2014, the NRC technical position observed that "The fracture toughness screening. value of 255 kJ/m 2 specified in the Grimes Letter is based on a generic flaw tolerance evaluation for piping, and may be overly conservative for RVI CASS components that are subject to mainly compressive stresses during operation, and are part of a population of redundant components where failure of individual components can be tolerated."
The technical position went on to add that "therefore, the staff applies the 255 kJ/m 2 value for screening purposes with the knowledge that there likely is additional conservatism present in this screening for non-pressure boundary RVI components." In an effort to provide further evidence with respect to the NRC staff technical position, some industry efforts since the July 15, 2014 meeting with the NRC staff have been directed toward this issue. The results are summarized in the following paragraphs.
The industry selected three different geometries that can be related to typical BWR and PWR CASS reactor internals in order to estimate flaw tolerance capability: (1) a large-diameter cylinder with a through-wall vertical flaw located in a longitudinal seam weld, subjected to combined membrane and bending stress; (2) an edge-cracked beam-column subjected to combined membrane and bending stress; and (3) a six-inch-diameter, Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure. The internal pressure for the third geometry was selected such that the circumferential tensile stress in the pipe was identical to the membrane tensile stress level chosen for the first two geometries. In all three case studies, the initial flaw size (length for the first and third geometries, and depth for the second geometry) was selected to be consistent with reactor vessel internals fabrication workmanship standards. No flaw growth criteria were applied to the initial flaw sizes, although the initial flaw sizes were increased to some extent in order to determine the rate at which the crack driving force increased as a function of the increase in flaw size.
For the first geometry (large-diameter cylinder with through-wall vertical flaw), the diameter was selected to be 452 inches with a wall thickness of either one or two inches, the membrane tensile stress was selected to be 5 ksi, and the bending stress was selected to be 7.5 ksi. The total initial flaw length was selected to be 0.226 inches (about 1/4-inch in length), but was increased in increments up to 4.294 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. For the largest initial flaw lengths examined, the typical LEFM stress intensity is of the order of 25 ksiin, which converts to an elastic-plastic crack driving force of about 4 kJ/m 2 . This implies a very large margin relative to the screening value of 255 kJ/m2 .
For the second geometry (edge-cracked beam column), the solid column diameter was selected to be three inches, and the membrane and bending stresses were selected to be identical to those selected for the first geometry. The smallest initial flaw depth was selected as 0.1 inches, and was incremented by 0.1 inch up to a maximum depth of 1.7 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 lillview Avenue, Palo Alto, CA 94304-1395 USA
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* www.epri.com BWRVIP 2015-025 J-crack driving forces. For the largest initial flaw depth examined (1.7 inches), the LEFM stress intensity was 42 ksiIin, which converts to an elastic-plastic crack driving force of about 10 kJ/m 2.Again, this calculation implies a very large margin relative to the screening value of 255 kJ/m 2.For the third geometry (six-inch diameter Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure), the internal pressure was selected such that the circumferential stress was approximately 5 ksi, matching the membrane tensile stress used for the first and second geometries.
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Because of the thin pipe wall, this case was found to be the most critical of the three geometries.
 
The initial flaw length was selected to be 0.1 inches, and was then incremented in 0.1-inch increments up to a maximum flaw length of 2.0 inches. For this case, the applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. In addition, this case was also analyzed using elastic-plastic fracture mechanics, in order to compare derived crack-driving forces with directly calculated elastic-plastic crack-driving forces. For an initial flaw length of 2.0 inches, the LEFM stress intensity factor was about 54 ksi/in, which converts to a crack driving force of about 96 in-lb/in 2 or about 16 kJ/m 2.The directly-calculated elastic-plastic crack driving force is almost exactly the same, but very slightly lower. When the initial flaw length was doubled -to about 4.0 inches, the applied LEFM stress intensity was found to be 120 ksi/in, which converts to a crack driving force of about 476 in-lb/in 2 or about 83 kJ/m 2.Even for this very severe example, the calculations show a sizable margin relative to the screening value of 255 kJ/m 2.From this exercise, CASS reactor internals components subjected to nominal stress levels, even in the presence of initial flaws that are well beyond fabrication workmanship acceptance criteria, are extremely flaw tolerant, with margins against flaw instability of the order of a factor of five to 10 relative to the fracture toughness screening criterion of 255 kJ/m 2 specified in the Grimes letter. When this flaw tolerance is coupled with the additional margin inherent in the separation of CF-3/CF-8 screening data from CF-8M screening data, the conservatism of the industry technical position is further confirmed.
BWRVIP 2015-025 J-crack driving forces. For the largest initial flaw depth examined (1.7 inches), the LEFM stress intensity was 42 ksiIin, which converts to an elastic-plastic crack driving force of about 10 kJ/m 2 . Again, this calculation implies a very large margin relative to the screening value of 255 kJ/m 2 .
22 BWRVIP 2015-025 Attachment D Tahlo I virarlld o/- larrto RPnonpe (Indivetru PnaifinnI 23  
For the third geometry (six-inch diameter Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure), the internal pressure was selected such that the circumferential stress was approximately 5 ksi, matching the membrane tensile stress used for the first and second geometries. Because of the thin pipe wall, this case was found to be the most critical of the three geometries. The initial flaw length was selected to be 0.1 inches, and was then incremented in 0.1-inch increments up to a maximum flaw length of 2.0 inches. For this case, the applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM),
'e, L 2l 1I ELECTRIC POWER RESEARCH INSTITUTE 2015-025 BWR Vessel & Internals Project (BWRVIP)March 09, 2015 Document Control Desk U.S. Nuclear Regulatory Commission 11555 Rockville PikeRockville, MD 20852 Attention: Joseph Holonich
and were then converted to J-crack driving forces. In addition, this case was also analyzed using elastic-plastic fracture mechanics, in order to compare derived crack-driving forces with directly calculated elastic-plastic crack-driving forces. For an initial flaw length of 2.0 inches, the LEFM stress intensity factor was about 54 ksi/in, which converts to a crack driving force of about 96 in-lb/in 2 or about 16 kJ/m 2. The directly-calculated elastic-plastic crack driving force is almost exactly the same, but very slightly lower. When the initial flaw length was doubled - to about 4.0 inches, the applied LEFM stress intensity was found to be 120 ksi/in, which converts to a crack driving force of about 476 in-lb/in 2 or about 83 kJ/m 2 . Even for this very severe example, the calculations show a sizable margin relative to the screening value of 255 kJ/m 2 .
From this exercise, CASS reactor internals components subjected to nominal stress levels, even in the presence of initial flaws that are well beyond fabrication workmanship acceptance criteria, are extremely flaw tolerant, with margins against flaw instability of the order of a factor of five to 10 relative to the fracture toughness screening criterion of 255 kJ/m 2 specified in the Grimes letter. When this flaw tolerance is coupled with the additional margin inherent in the separation of CF-3/CF-8 screening data from CF-8M screening data, the conservatism of the industry technical position is further confirmed.
22
 
BWRVIP 2015-025 Attachment D Tahlo I   virarlld o/- larrto RPnonpe (Indivetru PnaifinnI 23
 
United States Nuclear Regulatory Commission Official Hearing Exhibit In the Matter of:                    Entergy Nuclear Operations, Inc.                                                                        ENT000663 (Indian Point Nuclear Generating Units 2 and 3)
ASLBP #: 07-858-03-LR-BD01 Submitted: August 10, 2015 Docket #: 05000247 l 05000286 Exhibit #: ENT000663-00-BD01                  Identified: 11/5/2015 Admitted: 11/5/2015                          Withdrawn:
Rejected:                                      Stricken:
Other:
2l1I ELECTRIC POWER L          RESEARCH INSTITUTE
                                                                                                                                    'e, 2015-025                                                         BWR Vessel & Internals Project (BWRVIP)
March 09, 2015 Document Control Desk U.S. Nuclear Regulatory Commission 11555 Rockville Pike Rockville, MD 20852 Attention:         Joseph Holonich


==Subject:==
==Subject:==
Project No. 704 -Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR Reactor Internals Fabricated of Cast Austenitic Stainless Steel  
Project No. 704 - Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR Reactor Internals Fabricated of Cast Austenitic Stainless Steel


==References:==
==References:==
: 1. Letter from D. Madison (BWRVIP Chairman) and A. McGehee (BWRVIP Program Manager) to J. Holonich (NRC), Project No. 704 -BWRVIP Response to NRC Request for Additional Information on BWRVIP-234, dated May 23, 2014. ADAMS -ML14174A841.
: 1. Letter from D. Madison (BWRVIP Chairman) and A. McGehee (BWRVIP Program Manager) to J. Holonich (NRC), Project No. 704 - BWRVIP Response to NRC Request for Additional Information on BWRVIP-234, dated May 23, 2014. ADAMS - ML14174A841.
: 2. Letter from J. Holonich (NRC) to A. Mendiola (NRC), Summary of the July 15,2014, Meeting with the Electric Power Research Institute on Items Related to Cast Austenitic Stainless Steel and the Materials Reliability Program-227-A,"Pressurized Water Reactor Internals Inspection And Evaluation Guidelines," September 9, 2014. ADAMS -ML14127A077.
: 2. Letter from J. Holonich (NRC) to A. Mendiola (NRC), Summary of the July 15, 2014, Meeting with the Electric Power Research Institute on Items Related to Cast Austenitic Stainless Steel and the Materials Reliability Program-227-A, "Pressurized Water Reactor Internals Inspection And Evaluation Guidelines,"
: 3. "NRC Position on Aging Management of CASS Reactor Vessel Internal Components," June 23, 2014, ADAMS -ML 14174A719.
September 9, 2014. ADAMS - ML14127A077.
: 4. Email from C. Wirtz (EPRI) to J. Holonich (NRC), October 7, 2014.5. NUREG/CR-4513, ANL-93/22, Revision 1, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," Argonne National Laboratory, May 1994.The purpose of this letter is to provide the status of the Industry (PWR and BWR) activities associated with developing and proposing a generic screening criteria to address thermal and irradiation embrittlement of RPV internals fabricated of cast austenitic stainless steel (CASS).Reference I was provided to the NRC in response to a Request for Additional Information (RAI) regarding BWRVIP-234.
: 3. "NRC Position on Aging Management of CASS Reactor Vessel Internal Components," June 23, 2014, ADAMS - ML14174A719.
The RAI response contained supplemental information that provided the technical bases for an Industry screening criteria for CASS internals.
: 4. Email from C. Wirtz (EPRI) to J. Holonich (NRC), October 7, 2014.
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: 5. NUREG/CR-4513, ANL-93/22, Revision 1, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," Argonne National Laboratory, May 1994.
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The purpose of this letter is to provide the status of the Industry (PWR and BWR) activities associated with developing and proposing a generic screening criteria to address thermal and irradiation embrittlement of RPV internals fabricated of cast austenitic stainless steel (CASS).
# Customer Service 800.313.3774 9 www.epri.com BWRVIP 2015-025 A meeting was later held on July 15, 2014 at NRC offices in Washington, DC to discuss the Industry and NRC positions (References 2, 3). Based on that meeting, the Industry committed to investigate additional information where there was disagreement with the NRC regarding the screening criteria and provide said information to the NRC at a later date. That information was informally submitted for NRC's consideration (Reference
Reference I was provided to the NRC in response to a Request for Additional Information (RAI) regarding BWRVIP-234. The RAI response contained supplemental information that provided the technical bases for an Industry screening criteria for CASS internals.
: 4) and is contained in Attachments A through D of this letter. A conference call was then held on November 20, 2014 with the NRC to discuss this information.
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Following this conference call the NRC indicated that they were not willing to deviate from their position documented in Reference 3.Despite the NRC's current stance on the matter, the following comments regarding a generic TE and IE criteria for evaluation of reactor internals are important in forming the basis for the industry position: " The industry recognizes that the NRC is intending to revise its original IE position in the Grimes letter from lxl10 7 n/cm 2 (0.00014 dpa) to a position in the region of 0.5 to 1.5 dpa. Industry agrees that this position is more appropriate and has proposed a conservative value of 1 dpa.* It is not appropriate (for the staff) to penalize all non-Mo containing CASS (such as CF3 and CF8) because of the lower properties associated with the Mo-containing CF8M materials that are included in the ANL/NRC database, i.e., impose a lower bound.* There is no substantive data that demonstrates a synergistic effect for CASS materials that are typical of reactor internals (such as CF3 and CF8). As such the industry has proposed criteria that do not combine TE and IE. Each mechanism is considered distinct and separate." The introduction of a new criteria set for the category of materials with ferrite content between 15% to 20% having a lower proposed screening value for IE of 0.45 dpa is unnecessary and technically unfounded.
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The introduction of this category of ferrite content is significantly burdensome to licensees since it will require more complex and potentially more error-prone assessments of CASS material components by virtue of having more categories.
 
Industry maintains that the categories of materials and associated ferrite levels contained in the Grimes letter are appropriate." The criteria proposed by the industry (20% Ferrite and 1 dpa) have been shown to project significant margin on toughness reduction and therefore safety when compared to measured embrittlement behavior for CF3 and CF8 materials.
BWRVIP 2015-025 A meeting was later held on July 15, 2014 at NRC offices in Washington, DC to discuss the Industry and NRC positions (References 2, 3). Based on that meeting, the Industry committed to investigate additional information where there was disagreement with the NRC regarding the screening criteria and provide said information to the NRC at a later date. That information was informally submitted for NRC's consideration (Reference 4) and is contained in Attachments A through D of this letter. A conference call was then held on November 20, 2014 with the NRC to discuss this information.
Regardless, this letter serves to formally submit this additional information to the NRC for review and consideration in developing a regulatory position for the screening criteria associated with TE and IE for CASS internals and to inform revisions to NUREG-4513, Rev. 1 (Reference 5). The PWR and BWR Industry position for TE and IE screening criteria is shown in Attachment D.2 BWRVIP 2015-025 Irrespective of the staff's decision and future promulgation of a regulatory position on TE and IE for CASS internals, the BWRVIP formally requests the NRC to evaluate and resolve the RAI responses associated with BWRVIP-234 and issue a Safety Evaluation.
Following this conference call the NRC indicated that they were not willing to deviate from their position documented in Reference 3.
Despite the NRC's current stance on the matter, the following comments regarding a generic TE and IE criteria for evaluation of reactor internals are important in forming the basis for the industry position:
    " The industry recognizes that the NRC is intending to revise its original IE position in the Grimes letter from lxl10 7 n/cm 2 (0.00014 dpa) to a position in the region of 0.5 to 1.5 dpa. Industry agrees that this position is more appropriate and has proposed a conservative value of 1 dpa.
* It is not appropriate (for the staff) to penalize all non-Mo containing CASS (such as CF3 and CF8) because of the lower properties associated with the Mo-containing CF8M materials that are included in the ANL/NRC database, i.e., impose a lower bound.
* There is no substantive data that demonstrates a synergistic effect for CASS materials that are typical of reactor internals (such as CF3 and CF8). As such the industry has proposed criteria that do not combine TE and IE. Each mechanism is considered distinct and separate.
    " The introduction of a new criteria set for the category of materials with ferrite content between 15% to 20% having a lower proposed screening value for IE of 0.45 dpa is unnecessary and technically unfounded. The introduction of this category of ferrite content is significantly burdensome to licensees since it will require more complex and potentially more error-prone assessments of CASS material components by virtue of having more categories. Industry maintains that the categories of materials and associated ferrite levels contained in the Grimes letter are appropriate.
    " The criteria proposed by the industry (20% Ferrite and 1 dpa) have been shown to project significant margin on toughness reduction and therefore safety when compared to measured embrittlement behavior for CF3 and CF8 materials.
Regardless, this letter serves to formally submit this additional information to the NRC for review and consideration in developing a regulatory position for the screening criteria associated with TE and IE for CASS internals and to inform revisions to NUREG-4513, Rev. 1 (Reference 5). The PWR and BWR Industry position for TE and IE screening criteria is shown in Attachment D.
2
 
BWRVIP 2015-025 Irrespective of the staff's decision and future promulgation of a regulatory position on TE and IE for CASS internals, the BWRVIP formally requests the NRC to evaluate and resolve the RAI responses associated with BWRVIP-234 and issue a Safety Evaluation.
If you have any questions on this subject please call Ron DiSabatino (Exelon, BWRVIP Assessment Committee Technical Chairman) at 717.456.3685.
If you have any questions on this subject please call Ron DiSabatino (Exelon, BWRVIP Assessment Committee Technical Chairman) at 717.456.3685.
Sincerely, 24 Andrew McGehee, EPRI, BWRVIP Program Manager Tim Hanley, Exelon Corp., BWRVIP Chairman 3 BWRVIP 2015-025 Industry Response to July 15, 2014 Meeting with NRC on CASS On July 15, 2014, representatives from the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS) met with the NRC staff to discuss the thermal and irradiation embrittlement screening criteria for cast austenitic stainless steel. While the working group and NRC staff were in general agreement on the thermal embrittlement (TE) screening criteria, there was a marked difference of opinion on the irradiation embrittlement (IE) screening criteria, particularly for materials with delta ferrite contents of 15-20% (the NRC proposed 0.45 dpa, while the industry proposed 1 dpa).Agreement was reached on the TE screening criteria in part because the data on low-molybdenum and high-molybdenum material are considered separately, resulting in separate TE screening criteria for these materials.
Sincerely, 24 Andrew McGehee, EPRI, BWRVIP Program Manager Tim Hanley, Exelon Corp., BWRVIP Chairman 3
This distinction is made because high-molybdenum materials show a distinctly greater loss of fracture toughness from TE and IE effects than low-molybdenum materials.
 
This is reviewed and discussed further in Attachment A The separate consideration of low- and high-molybdenum materials test data was not carried over into the IE domain. The data set used to determine the NRC's position on IE was obtained from NUREG-7027, which considered irradiated high- and low-molybdenum materials together, along with data on irradiated welds. Because these materials were considered together, the resulting lower bound curve is judged to be overly conservative relative to the low-molybdenum material.
BWRVIP 2015-025 Industry Response to July 15, 2014 Meeting with NRC on CASS On July 15, 2014, representatives from the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS) met with the NRC staff to discuss the thermal and irradiation embrittlement screening criteria for cast austenitic stainless steel. While the working group and NRC staff were in general agreement on the thermal embrittlement (TE) screening criteria, there was a marked difference of opinion on the irradiation embrittlement (IE) screening criteria, particularly for materials with delta ferrite contents of 15-20% (the NRC proposed 0.45 dpa, while the industry proposed 1 dpa).
A reexamination of this data (see Attachment B), shows that by considering the low-molybdenum materials test data independently of the other materials it can be concluded that there is a substantial safety margin in the industry's proposed I dpa screening criteria.These screening criteria are being implemented to ensure that CASS components in reactor vessel internals maintain adequate fracture toughness during the period of extended operation.
Agreement was reached on the TE screening criteria in part because the data on low-molybdenum and high-molybdenum material are considered separately, resulting in separate TE screening criteria for these materials. This distinction is made because high-molybdenum materials show a distinctly greater loss of fracture toughness from TE and IE effects than low-molybdenum materials. This is reviewed and discussed further in Attachment A The separate consideration of low- and high-molybdenum materials test data was not carried over into the IE domain. The data set used to determine the NRC's position on IE was obtained from NUREG-7027, which considered irradiated high- and low-molybdenum materials together, along with data on irradiated welds. Because these materials were considered together, the resulting lower bound curve is judged to be overly conservative relative to the low-molybdenum material. A reexamination of this data (see Attachment B), shows that by considering the low-molybdenum materials test data independently of the other materials it can be concluded that there is a substantial safety margin in the industry's proposed I dpa screening criteria.
The screening level to determine whether this requirement was met was a J value of 255 KJ/m 2 at a crack extension of 2.5 mm. This value was originally determined for pressure boundary components (i.e., large diameter piping, etc.) and was expected to be highly conservative for application to reactor vessel internals.
These screening criteria are being implemented to ensure that CASS components in reactor vessel internals maintain adequate fracture toughness during the period of extended operation.
Additional calculations (see Attachment C) demonstrate the level of this conservatism and show that reactor vessel internal components can safely operate with fracture toughness values much lower than the 255 KJ/m 2 value specified in the Grimes letter.In summary, the actions taken by the CASS industry working group and summarized in Attachments A, B and C support the proposed screening criteria contained in Attachment D.These criteria provide a significant amount of margin for screening of TE and IE. It is concluded that that the use of the proposed screening criteria will allow for continued safe and reliable operation of the LWR fleet.4 BWRVIP 2015-025 Attachment A Discussion on Low Molybdenum vs High Molybdenum CASS Grades Introduction A meeting was held on July 15, 2014 at the NRC Office in Washington, DC between the staff of the U.S. Nuclear Regulatory Commission (NRC) and the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS). The topic of discussion focused on the thermal aging and neutron irradiation embrittlement screening criteria (separately) proposed by the industry and the NRC staff. The proposals included criteria for low-molybdenum CASS grades, such as CF-3 and CF-8, and high-molybdenum CASS grades, such as CF-8M. There was agreement between industry and the NRC staff regarding the differences in such measures of embrittlement as elastic-plastic crack growth resistance (J-R curve) for the low-Mo materials versus the high-Mo materials, at least where thermal aging embrittlement effects are dominant.
The screening level to determine whether this requirement was met was a J value of 255 KJ/m2 at a crack extension of 2.5 mm. This value was originally determined for pressure boundary components (i.e., large diameter piping, etc.) and was expected to be highly conservative for application to reactor vessel internals. Additional calculations (see Attachment C) demonstrate the level of this conservatism and show that reactor vessel internal components can safely operate with fracture toughness values much lower than the 255 KJ/m 2 value specified in the Grimes letter.
In fact, screening criteria proposed by the staff are identical to the industry-proposed screening criteria for the case of thermal aging embrittlement.
In summary, the actions taken by the CASS industry working group and summarized in Attachments A, B and C support the proposed screening criteria contained in Attachment D.
However, the areas of agreement between the industry and the staff did not carry over to combined environments where the effects of neutron irradiation embrittlement begin to approach the same level as those from thermal aging embrittlement.
These criteria provide a significant amount of margin for screening of TE and IE. It is concluded that that the use of the proposed screening criteria will allow for continued safe and reliable operation of the LWR fleet.
In order to address these differences in criteria, the available data for CF-3, CF-8, and CF-8M materials in the literature are reviewed and assessed, with a recommendation to the NRC staff for a change to their proposed criteria to more closely agree with the criteria proposed by the industry.Review and Summary of Thermal Aging Embrittlement Data The significant differences in thermal aging embrittlement behavior of the low-molybdenum grades of cast austenitic stainless steel, such as CF-3 and CF-8, versus the thermal aging embrittlement behavior of the high-molybdenum grades, such as CF-8M, have been known for at least two decades, with extensive data and associated interpretations of said data documented in NUREG/CR-4513, Revision 1 [1]. The lower-bound thermal aging embrittlement estimates shown in Figures 3 (statically-cast steels) and 4 (centrifugally-cast steels) from Reference 1 with varying amounts of delta ferrite provide an excellent illustration of those significant differences, in this case with the measure of significance being the crack-growth resistance J-R curve. In particular, the lower-bound formulas cited in Section 3.1.1 of Reference 1 (and plotted in Figures 3 and 4) can be used to compare the estimated crack growth resistance values at 2.5 mm of crack extension for the CF-3, CF-8, and CF-8M steels with > 15% delta ferrite. Note that Figure 3 provides lower-bound thermal aging estimates for static-cast steels, while Figure 4 provides lower-bound thermal aging estimates for centrifugally-cast steels.5 BWRVIP 2015-025 Crack Extension ha (in.)Crack Extension As (in.)0.06 0.10 0.15 0.00 5.-3 I S a I if 5.-3 I I a 2 3 4 S Lower-Bound J-R Curve Static-Camt Stes>15% Fentbe-290"C J =2510Aa)0-2 03-J=M4a -17&O CF-4u 0 1 2 3 4 0 0.00 0.06 0.10 0.15* I I I ji , ' , : : : , ' , : Lower-Bound J-IR Static-Cast StaWsi 10-16% Fegrkt J -274"0.3 CF035 j- 2740sa)03 2001&a)o 3 6  cF-4 ..-:j -.: '. I: 3 2 CF-Ui-4000-3000 -o-2000f.1000k 0..4000-3000 I 10.0 0.00 0.06 0.10 0.15 lOOO Lower-Bound J-R Curve Static-Cat Steels 80o. l-15% Fenml Room Temp.800- 1 -31(1P40 400 j =3074Uo-38 CF-C 400 J 130-~036-CF-SM 200-CFS 0 1 2 3 4 5 0 1 2 3 4 5 0.00 0.06 0.10 0.1(0.00 0.06 0.10 0.15 5000" 4000~3000 2000j 1 0 0 0 i 0 1 2 3 4 Crack Extension, Aa (mm)Figure 3. Predicted lower-bound J-R curves at RT and 290&deg;C for static-cast SSs with ferrite contents >15, 10-15. or<10%6 BWRVIP 2015-025 Crack Extension As (in.)0.o00. O. .O 0.1s Crack Extension ha (in.)0.00 O.06 0.10 0.15 j400-~2007 Lower-Bound J-R Curve Centrifugally Cast Steels>15% Fmist Room Tnp. J -304SO)0.3 7 JF3348 39C-CF-MM F Lower-Bound J-R Curve Centrifugally Cast Steels>15%FaFnite M-0C J.- 3301AP,340" 3 5  CF-s CF-S CF-Sm.. ......H i I 1 2 3 4 0 1 2 3 4 1 0.00 0.06 010 0.15~20)0-X0-i J.30sWKa 0 4 CF-3 r-Bound J-R Curve C " a olyCast Steels-. 357&#xfd;,,)&deg;0.00 0.0S 0.10 0.15 Lower-Bound J-R Curve Centrifugally Cast Steels 10-15% Forte0 2fOC J -300ma)&deg;35 0-36 CF-S CJ -38M&).3 CF-3-4000 7 C!-2000 'E-1000 0 i 4SO0O I-4000.I 3000-2000 I-1000 0.5000-4O O" I:-3000 20001.1000 Cf-M C0SM 0 1 2 3 S4 1 2 3 4 5 0.00 0.0 0.10 0.15 0O 30 0.06 0.10 0.15 1000 Lower-Bound J-R Curve 4001 200 -Lower-ilound' J-'R C'urv'e' .Centrifugaly Cast SteDes 410% Fernite Room TSm 0 7 P41 CF--3 CF-SM Lower-Bound J-R Curve Centrifugally Cast Steels<10% F-f-n&#xb6; J -435(Aa~5 CF-8 CF-Sm 0 1 2 3 4 5 0 2 3 4 Crack Extension., A (mm) Crack Extension, A (mm)a Figure 4. Predicted lower-bound J-R curves at RT and 290'C for centrifugally cast SSs with ferrite contents > 15. 10- 15. or < 10%7 BWRVIP 2015-025 For CF-3, the lower bound crack growth resistance, for statically-and centrifugally-cast materials, varies between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 Id/m 2.On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2.When the data are examined very closely, there is no significant difference between the static-cast lower-bound estimates for CF-3 and CF-8 in Figure 3 and the centrifugally-cast lower-bound estimates for CF-3 and CF-8 in Figure 4. The data also show that these insignificant differences are roughly identical to the differences between CF-3 and CF-8 estimates within the static-cast and centrifugally-cast populations.
4
Therefore, based on this examination of lower-bound estimates, the CF-8M data exhibit substantially lower fracture toughnesses and are therefore unsuitable as a lower-bound estimate for the low-molybdenum grades. Lower bound estimates must be conservative, but they must also remain representative of the data. Table 1, shown below, succinctly summarizes the data comparisons extracted from Figures 3 and 4 from Reference 1.Table 1. Lower Bound Fracture Toughness Estimates CASS Steels J-values at 2.5 cm of Crack Comments Growth (kJ/m 2)Lower bound above the threshold CF-3 Steels 364 to 478 value of 255 kJ/M 2 Lower bound above the threshold CF-8 Steels 343 to 451 value of 255 kj/m 2 CF-8M Steels 161 to 259 Lower bound might be less than threshold values of 255 kJ/m 2 Table 1 clearly shows that lower bound fracture toughness values of CF-3 and CF-8 steels are much higher than CF-8M steels, and that only the fracture toughness of CF-8M steels fall below the threshold value of 255 kJ/m 2.Therefore, the screening criteria for CF-8M (high molybdenum) steels should be considered separately from CF-3 and CF-8 (low molybdenum) steels.Thus far, the data evaluation has been based on lower-bound fracture toughness estimates derived from Charpy impact correlations.
 
However, these lower-bound thermal aging embrittlement estimates can be confirmed by examining actual crack extension resistance curve measurements for various heats of CF-3, CF-8, and CF-8M with delta ferrite content in the range of 20%. For example, Figure 14 from Reference 1 shows J-R curve measurements, along with thermal aging saturation estimates for two heats of CF-3 material (Heat 69 and Heat I) and one heat of CF-8 material (Heat 68), while Figure 15 from Reference 1 shows similar results for three heats of CF-8M material (Heats 74, 75, and 758).In this case, it should be noted that the actual fracture toughness data are based on thermal aging saturation conditions and are therefore somewhat higher than the lower-bound fracture toughness 8 BWRVIP 2015-025 estimates.
BWRVIP 2015-025 Attachment A Discussion on Low Molybdenum vs High Molybdenum CASS Grades Introduction A meeting was held on July 15, 2014 at the NRC Office in Washington, DC between the staff of the U.S. Nuclear Regulatory Commission (NRC) and the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS). The topic of discussion focused on the thermal aging and neutron irradiation embrittlement screening criteria (separately) proposed by the industry and the NRC staff. The proposals included criteria for low-molybdenum CASS grades, such as CF-3 and CF-8, and high-molybdenum CASS grades, such as CF-8M. There was agreement between industry and the NRC staff regarding the differences in such measures of embrittlement as elastic-plastic crack growth resistance (J-R curve) for the low-Mo materials versus the high-Mo materials, at least where thermal aging embrittlement effects are dominant. In fact, screening criteria proposed by the staff are identical to the industry-proposed screening criteria for the case of thermal aging embrittlement.
Also note that the thermal aging saturation fracture toughness data are based entirely on static-cast data for materials with delta ferrite in the range of 15% to 25%.The crack extension resistance value at 2.5 mm of crack extension for the thermal aging saturation conditions for CF-3 and CF-8 materials ranges between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material are less than half of the low-molybdenum material values.Therefore, the findings from the examination of the data in Figures 14 and 15, and the derived J values at 2.5 mm of crack extension, are completely consistent with the lower-bound thermal aging embrittlement estimates cited previously for both static-cast and centrifugally-cast material.
However, the areas of agreement between the industry and the staff did not carry over to combined environments where the effects of neutron irradiation embrittlement begin to approach the same level as those from thermal aging embrittlement. In order to address these differences in criteria, the available data for CF-3, CF-8, and CF-8M materials in the literature are reviewed and assessed, with a recommendation to the NRC staff for a change to their proposed criteria to more closely agree with the criteria proposed by the industry.
In other words, the development of screening criteria for the low-molybdenum grades should be treated separately from the development of screening criteria for the high-molybdenum grades.9 BWRVIP 2015-025 Crack Extension, An (in.)0.0 0.1 0.2 0.3 Crack Extension, An (in.)0.1 0.2 0.3 0.0 I .Heat 69 ~CF-3 2WC~2000-~1000.8,-21%290"C -SOAN 32 a 4XOy4 0 0' 0.0 -e J.366(AW).4 at320C 2 4 6 a I]0.1 0.2 0.3 I 2 0 a a-~1 I I 200 100 Heat I CF-3 o mw4g(Aa)V bwow 0 A A 0  &#xfd;L 0~ 0~2* 0.5 m~oC47 Roomm Temp. A 0 0 UABW C'.10000 "-600 I0 0-10000 0 10o~I=0-10000-6000 2 4 6 ............
Review and Summary of Thermal Aging Embrittlement Data The significant differences in thermal aging embrittlement behavior of the low-molybdenum grades of cast austenitic stainless steel, such as CF-3 and CF-8, versus the thermal aging embrittlement behavior of the high-molybdenum grades, such as CF-8M, have been known for at least two decades, with extensive data and associated interpretations of said data documented in NUREG/CR-4513, Revision 1 [1]. The lower-bound thermal aging embrittlement estimates shown in Figures 3 (statically-cast steels) and 4 (centrifugally-cast steels) from Reference 1 with varying amounts of delta ferrite provide an excellent illustration of those significant differences, in this case with the measure of significance being the crack-growth resistance J-R curve. In particular, the lower-bound formulas cited in Section 3.1.1 of Reference 1 (and plotted in Figures 3 and 4) can be used to compare the estimated crack growth resistance values at 2.5 mm of crack extension for the CF-3, CF-8, and CF-8M steels with > 15% delta ferrite. Note that Figure 3 provides lower-bound thermal aging estimates for static-cast steels, while Figure 4 provides lower-bound thermal aging estimates for centrifugally-cast steels.
1 0 0.D 0.1 0.2 0.3......1 i 4 .1 1 1. 1- 1 l 1 1 Heat 68'C"- 290C.0 =Sanm.7,40.4 S,, 32 J.46(M d2B0-0 0000 0 0&#xfd;0 00 --0 .2g0Ag 0 iIi I
5
* I U 2 4 6 8 Crack Extension, A& (Mm)10 Crack Extension, As (mm)Figure 14. Saturation fracture toughness J-R curves at RT and 290Co, estimated from the chemical composition of static-cast CF-3 and CF-8 steels, and determined experimentally 10 BWRVIP 2015-025 Crack Extension, ha (in.)Crack Extension, ha (in.)0.0 0.1 0.2 0.3 1 , .I , I I .I .I I .I .i .0.0 0.1 0.2 0.3~1000 Oj 0 0 3000-492000-.[Oo Hiai is 'C", 'Heal 75 CF-SM Ro ep Stall-Caa Slab Sc -25%.Walled 5-WA Room Temp.Unapd j .42")0.42-0 OAO~N4WrC tUegod-~J -461(A&P.3 7 -32 " 0a adI 20'8NtPA~'Co- .o32 *y oo 0 O00000OOOOC5 j .l44(AS)03
 
-., I ., .I I , ..I I ' ' '2 4 6 8 0 0.1 0.2 0.3 0 0 2 4' 6 S 14 0.0 0.1 0.2 0.3-15000 C-10000-3OO-000-15000 &#xa3;:1m.1 Heat 74 CF-SM Room T SARc--CaM Slab 6Sc= 16% Uae 040o Und J. 57" )o 0 42 0 000ht 0C =A 324 Olp 0 0. !aOC a *? * .o0 ,-- J -03*7 emp.al 320*C Heat 74 CF-SM 9*taw-cau SWa 6C16%32 efpy J 30(sa)0 3 7 32 OOY N 290'Cj~at320*C C)00N~0 O~0!!!-7 KSaknil F- J .WM~)U. 3 N s 0 0 0. 4 6 0 10 0.0 0.1 0.2 0.3 0.0 0.1 0.2 0.3 I 2000-1000.Hieat 7'581 6F4 R'' Temp.SONO-C*M Etow SC-21%Unap 32 apy 3 2 4P&I 290C at 30*C WA OA&#xa3; kj MA AL J/ 2(a03 Heat 758 CF-SM 290'C SUMc-CaN Elbow J .487(aa)0.38~ 32 Id290t Id 3py';'>eso 4 -?>(V 3,3[ 16000-10000-5000 C O*P 0 2 4 6 8 Crack Extension, Aa (mm)10 0 Crack Extension, Aa (mm)10 Figure 15. Saturation fracture toughness J-R curves at RT and 290*C. estimated from die chemical composition of static-cast CF-SM steels, and determined experimentally 11 BWRVIP 2015-025 Review and Summary of Combined TE and IE Data The available data for purely thermally-embrittled CASS materials is quite extensive.
BWRVIP 2015-025 Crack Extension ha (in.)                           Crack Extension As (in.)
However, that is not the case for a combination of thermal aging and neutron irradiation embrittlement.
0.00            0.06         0.10         0.15 Lower-Bound J-R Curve Static-Camt Stes I
In spite of the limited data, the evaluation of available crack growth resistance data for CF-3, CF-8, and CF-8M material is not altered by including information on material subjected to both thermal aging and neutron irradiation embrittlement, as shown in Figures 23, 41, 49, and 58 from ANL-12/56 [2]. The results for Specimen B-1 (static-cast CF-3 material taken from Heat 69, with approximately 24% delta ferrite, thermally aged for 10,000 hours at 400'C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 23 -taken from Reference
5.
: 2. The extrapolated J value at 2.5 mm of crack extension is 789 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 for Heat 69 from Reference 1.640 480 1-1-74 320 160 0.5 1.0 1.Crack Extension (mm)2.0 Figure 23. The J-R curve for specimen B-1.Similarly, the results for Specimen F-1 (static-cast CF-8 material taken from Heat 68, with approximately 23% delta ferrite, thermally aged for 10,000 hours at 400'C and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 41 -also taken from Reference 2.The extrapolated J value at 2.5 mm of crack extension is 657 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 from Reference 1 for Heat 68.12 BWRVIP 2015-025 640 ....Specimen F-1 CF-8, aged, 0.08 dpa 480 Low-DO high-purity water, 3200C I A J= 372"Aao.6 2 E 320 1 V, I 160 AI max 0 0.0 0.5 1.0 1.5 2.0 Crack Extension (mm)Figure 41. The J-R curve of specimen F-i.Finally, the results for Specimens I-1 (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, unaged but subjected to a neutron irradiation dose of 0.08 dpa) and J-1I (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, thermally aged for 10,000 hours at 4001C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figures 49 and 58 -also taken from Reference
                                                                  >15% Fentbe
: 2. In this case the extrapolated J value at 2.5 mm of crack extension for Specimen J-1 is 466 k/m , which can be compared to the results shown in Figure 15 from Reference I for Heat 75 that appear to be of the order of 300 to 400 kJ/m 2 at room temperature and operating temperature.
                                                                -290"C                                                 -4000
13 BWR VIP 2015-025 640 480.. ......I .I Specimen I-1 CF-8M, unaged, 0.0 Low-DO high-purity dna-~5~~cm I I I I water, 320PC .J7 mJ= 336-Aa max I'320 160 n IAamax=145 kJ/m 2 I I 0 0.5 1.0 1.5 Crack Extension (mm)Figure 49. The JR curve of specimen I-1.2.0 640 480 (N-320 160 2.0 Crack Extension (mm)Figure 58. The JR curve of specimen J-1.14 BWRVIP 2015-025 Conclusions and Recommendation This review and summary of available data on CF-3, CF-8, and CF-8M CASS materials subjected to both individual and combined effects of thermal aging and neutron irradiation embrittlement demonstrated that: Thermal aging embrittlement effects on high-Mo grades are significantly more pronounced than the effects on the low-Mo grades, by roughly a factor of two or more based upon lower-bound crack growth resistance estimates.
  -3                                                                                                        0 J =2510Aa)
For CF-3, the lower-bound crack growth resistance values at 2.5 mm of crack extension for > 15% delta ferrite vary between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 kJ/m 2.On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2 which are significantly lower compared to CF-3/8. These results are consistent with the results obtained by examining actual crack growth resistance value measurements at 2.5 mm of crack extension for the thermal aging to saturation for CF-3 and CF-8 materials (low-Mo) that range between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material (high-Mo) are less than half of the low-molybdenum material values.* There is no significant difference between the static-cast lower-bound estimates and the centrifugally-cast lower-bound estimate for CF-3 and CF-8 materials, and those relatively small differences are roughly identical to differences between CF-3 and CF-8 lower-bound estimates.
                                                                          -   2     03-                               -3000  -
Using lower-bound crack growth resistance values at 2.5 mm of crack extension as the comparative measure, the CF-3 static-cast values of 364 and 410 kJ/m 2 compare very well to the 477 and 478 kJ/m 2 values for centrifugally-cast material, while the CF-8 static-cast values of 343 and 366 kJ/m 2 compare favorably with the 427 and 451 kJ/m 2 values for centrifugally-cast material.
17&O
The differences between static-cast and centrifugally-cast values, and between CF-3 and CF-8 values are both inconsequential in comparison to the differences between low-Mo and high-Mo materials.
                                                                                          - J=M4a                      -2000f o
Therefore these two grades may be considered as a combined category for screening purposes.* The added effect of neutron irradiation embrittlement does not change the conclusions drawn with respect to low-Mo versus high-Mo fracture toughness.
                                                                                                                        .1000k CF-4u 0.
Finally, since the conclusions are drawn primarily from static-cast fracture toughness data, a recommendation to the NRC staff to maintain the screening threshold for low-Mo static-cast grades at 20% is supported by the data.Therefore, this review shows that the CF-8M data provide an extremely conservative and thus unrepresentative lower bound to the data for the low-molybdenum grades. As such, the CF-8M lower bound is separable and distinct from the low-molybdenum grade lower bounds, which therefore require their own screening category and fracture toughness estimates.
0            1          2        3            4      0 2        3         4     S 0.00          0.06    0.10        0.15        0.00             0.06         0.10         0.15
Thus, the delta ferrite levels stated in the BWRVIP-234 RAI response (from the Grimes letter) is further supported by this evaluation.
                                                                        *I I         , 'I , : : :           ji , ' , :
lOOO Lower-Bound J-R Curve                            Lower-Bound J-IR Static-Cat Steels                                Static-Cast StaWsi aS    80o. l-15%Fenml                                      10-16% Fegrkt Room Temp.                                                                      J - 274"0.3           .4000 36        j- 2740sa)03 2001&a)o         cF-4             ..
800-     1 - 31(1P40 I
CF035                              -3000
* 400                                  j =3074Uo-38                                                                      I CF-C 400                      J 130-~036 200-                      -          CF-SM                                                    32                  10
                                                                  -  :j        -         .: '. I:
CF-Ui CFS                                                                        .0 0          1      2        3          4    5  0            1          2        3            4      5 0.00          0.06    0.10        0.1(        0.00             0.06         0.10         0.15 5000" 5.
if 4000~
  -3 3000 I
Ia                                                                                                                    2000j 1000i 0
1       2       3         4 Crack Extension, Aa (mm)
Figure3.           Predictedlower-bound J-R curves at RT and 290&deg;C for static-castSSs with ferrite contents >15, 10-15. or<10%
6
 
BWRVIP 2015-025 Crack Extension As (in.)                                   Crack Extension ha (in.)
0.o00.               O.     .O           0.1s             0.00           O.06       0.10         0.15 Lower-Bound J-R Curve                                    Lower-Bound J-R Curve Centrifugally Cast Steels                                 Centrifugally Cast Steels
            >15% Fmist                               0 37            >15%FaFnite Room Tnp.                   J - 304SO) .                 M-0C                    J.-3301AP,34      -4000  7 0 35 J.934r*a)    "         CF-s JF3348 39C-                                                                      CF-S C!
j400-CF-MM                                                                      -2000 '
E
~2007                                                                                                              -1000 CF-Sm
                          .. .. . . . . H                   i F                                                      0 I         1       2           3           4           0           1         2         3         4 1 0.00           0.06       010           0.15             0.00          0.0S        0.10          0.15 i
r-Bound J-R Curve                                 Lower-Bound J-R Curve C a " olyCast Steels                              Centrifugally Cast Steels 4SO0OI 10-15% Forte0                               -4000.
    )0-                                                                2fOC                 J - 300ma)&deg;35                 I 04                                                        0-36     CF-S J.30sWKa i                                                          CJ- 38M&).3 X0-    CF-3                                                       CF-3                                          3000
                                -. *    '* *. 357&#xfd;,,)&deg;
                                                                                                                    -2000 I
~20                                                                                                                -1000 Cf-M                                             C0SM 0
0          1       2         3                     S4             1         2         3         4 5 0O30            0.06        0.10          0.15            0.00          0.0         0.10         0.15 1000       Lower-Bound J-R Curve Lower-ilound' J-'R C'urv'e'                 .             Lower-Bound J-R Curve Centrifugaly Cast SteDes                                 Centrifugally Cast Steels                    .5000 410% Fernite                                                                                           - 4OO"
                                                                        <10% F-f-n&#xb6; Room TSm              07                                  2*0T P41 J -435(Aa~5                                         I:
                                                                                                                    -3000  -2 CF--3                                                                      CF-8 4001
                                                                                                                    -20001 200 -                            CF-SM                                                      CF-Sm               .1000 a
0           1       2         3             4       5   0                     2         3         4 Crack Extension., A (mm)                                   Crack Extension, A (mm)
Figure 4.         Predictedlower-bound J-R curves at RT and 290'C for centrifugally cast SSs with ferrite contents > 15. 10-15. or < 10%
7
 
BWRVIP 2015-025 For CF-3, the lower bound crack growth resistance, for statically- and centrifugally-cast materials, varies between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 Id/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2. When the data are examined very closely, there is no significant difference between the static-cast lower-bound estimates for CF-3 and CF-8 in Figure 3 and the centrifugally-cast lower-bound estimates for CF-3 and CF-8 in Figure 4. The data also show that these insignificant differences are roughly identical to the differences between CF-3 and CF-8 estimates within the static-cast and centrifugally-cast populations. Therefore, based on this examination of lower-bound estimates, the CF-8M data exhibit substantially lower fracture toughnesses and are therefore unsuitable as a lower-bound estimate for the low-molybdenum grades. Lower bound estimates must be conservative, but they must also remain representative of the data. Table 1, shown below, succinctly summarizes the data comparisons extracted from Figures 3 and 4 from Reference 1.
Table 1. Lower Bound Fracture Toughness Estimates CASS Steels           J-values at 2.5 cm of2 Crack                 Comments Growth (kJ/m )
Lower bound above the threshold 2
CF-3 Steels                 364 to 478                       value of 255 kJ/M Lower bound above the threshold 2
CF-8 Steels                 343 to 451                       value of 255 kj/m CF-8M Steels                   161 to 259                 Lower bound might be less than2 threshold values of 255 kJ/m Table 1 clearly shows that lower bound fracture toughness values of CF-3 and CF-8 steels are much higher than CF-8M steels, and that only the fracture toughness of CF-8M steels fall below the threshold value of 255 kJ/m 2. Therefore, the screening criteria for CF-8M (high molybdenum) steels should be considered separately from CF-3 and CF-8 (low molybdenum) steels.
Thus far, the data evaluation has been based on lower-bound fracture toughness estimates derived from Charpy impact correlations. However, these lower-bound thermal aging embrittlement estimates can be confirmed by examining actual crack extension resistance curve measurements for various heats of CF-3, CF-8, and CF-8M with delta ferrite content in the range of 20%. For example, Figure 14 from Reference 1 shows J-R curve measurements, along with thermal aging saturation estimates for two heats of CF-3 material (Heat 69 and Heat I) and one heat of CF-8 material (Heat 68), while Figure 15 from Reference 1 shows similar results for three heats of CF-8M material (Heats 74, 75, and 758).
In this case, it should be noted that the actual fracture toughness data are based on thermal aging saturation conditions and are therefore somewhat higher than the lower-bound fracture toughness 8
 
BWRVIP 2015-025 estimates. Also note that the thermal aging saturation fracture toughness data are based entirely on static-cast data for materials with delta ferrite in the range of 15% to 25%.
The crack extension resistance value at 2.5 mm of crack extension for the thermal aging saturation conditions for CF-3 and CF-8 materials ranges between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material are less than half of the low-molybdenum material values.
Therefore, the findings from the examination of the data in Figures 14 and 15, and the derived J values at 2.5 mm of crack extension, are completely consistent with the lower-bound thermal aging embrittlement estimates cited previously for both static-cast and centrifugally-cast material. In other words, the development of screening criteria for the low-molybdenum grades should be treated separately from the development of screening criteria for the high-molybdenum grades.
9
 
BWRVIP 2015-025 Crack Extension, An (in.)                           Crack Extension, An (in.)
0.0         0.1     0.2           0.3           0.0 I .           0.1           0.2           0.3 2WC Heat 69 ~CF-3                               290"C -
C' 8,-21%
  ~2000-                                                                                                              .10000 "
SOAN32 a           4XOy4 0           0'
                                                                                                                          -600 0.
  ~1000.                                                                                  0                   -e 0
J.366(AW).4         at320C I0 2         4         6         a           I0
          ]         0.1     0.2         0.3 Heat I CF-3 0
o mw4g(Aa)V bwow         A 0         A   &#xfd;L 200                                                                                                              0 2                                                                                  -10000 I
0~
* 0~ 0 10o~
100 20 a              Roomm Temp.
                            .5 m~oC47 A00        UABW 2     4       6 . ........... 10                                                            0 I=
0.D             0.1           0.2           0.3
                                                                  .. . .   . .       1 i 4 .1 1 1. 1- 1 l       1 1 Heat 68'C"-                                 290C a-
                                                            .0       =Sanm.7,40.4
~1                                                                          S,,   32           J.46(M             -10000 I                                                                                  d2B0 I                                                              -
00 0     0000 0
                                                                              --                0 0&#xfd;0
                                                                                                                    -6000 0                     .2g0Ag iIi I
* I     U 2         4         6         8           10 Crack Extension, As (mm)                           Crack Extension, A& (Mm)
Figure 14. Saturationfracture toughness J-R curves at RT and 290Co, estimatedfrom the chemical composition of static-cast CF-3 and CF-8 steels, and determined experimentally 10
 
BWRVIP 2015-025 Crack Extension, ha (in.)                                                 Crack Extension, ha (in.)
0.0               0.1             0.2             0.3                   0.01 , . I , I 0.1I . I .
0.2 I I . I . 0.3 i.
Heal Hiai is75 'C",
CF-SM       '              Ro Room Temp.      ep Stall-Caa Slab                                                                                                                     -15000 C Sc
                    - 25%
Unapd
                    .       Walled j . 42")0.42                           -     0OAO~N4WrC                   tUegod 5-WA                                                                -         ~J                   -461(A&P.
37
                                                                                                                                                -  -10000 32 "                             0a                         -3OO
                            'Co- .o32 *y         oo0      O00000OOOOC5
  ~1000                                                                                        adI20' 8NtPA~
Oj                                                        j .l44(AS)03                                                                           -000
              -   .   , 2 I .   , . 4I      I,     6 . .     I 8I '       ' '   0  0            2           4'        6             S      14 00
          .10            0.1             0.2               0.3                   0.0             0.1           0.2             0.3 3000-Heat 74 CF-SM                            Room T emp.                     Heat 74 CF-SM                                     9*
SARc--CaM Slab                                                             taw-cau SWa 6Sc=16%                           Uae
:1m 6C16%
[Oo          040o       Und                   J. 57" 0
                                                                )o 42                                                                             -15000  &#xa3; 492000-              0     =A000ht 0C 03 7 324Olp                                                                                          32 efpy      J 30(sa)
        .                                                                                              32 OOY   N 290'Cj~
0                                                    at320*C               C)00N aOCa              *?    *    .o0        0.!                                                      ~0 O~0
                                    ,*--       J-          03*7 al 320*C                  F- !!!-7                      KSaknil J .WM~)U. 3 N
s             0   0             0.       4   0      6                     10 0.0             0.1           0.2             0.3 0.0               0.1             0.2               0.3 Hieat 7'581 6F4                         R''         Temp.               Heat 758 CF-SM                                  290'C SONO-C*M Etow                                                             SUMc-CaN Elbow                                          [  16000 SC-21%Unap 2000-
                                                                                                                                                    -10000 I                                                    32 apy 32 4P 0
J .487(aa) . 38~Id290t        32 Id  3py C
1000.                                              &I290C          at 30*C
                                                                                                                                                    -5000 WAOA&#xa3; kj               MA AL                                           ';'>eso J/   2(a03 4-?>(V      3,3 O*P 0             2           4             6               8           10  0                                                            10 Crack Extension, Aa (mm)                                                 Crack Extension, Aa (mm)
Figure 15.         Saturationfracture toughness J-R curves at RT and 290*C. estimated from die chemical composition of static-castCF-SM steels, and determined experimentally 11
 
BWRVIP 2015-025 Review and Summary of Combined TE and IE Data The available data for purely thermally-embrittled CASS materials is quite extensive. However, that is not the case for a combination of thermal aging and neutron irradiation embrittlement. In spite of the limited data, the evaluation of available crack growth resistance data for CF-3, CF-8, and CF-8M material is not altered by including information on material subjected to both thermal aging and neutron irradiation embrittlement, as shown in Figures 23, 41, 49, and 58 from ANL-12/56 [2]. The results for Specimen B-1 (static-cast CF-3 material taken from Heat 69, with approximately 24% delta ferrite, thermally aged for 10,000 hours at 400'C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 23 - taken from Reference 2. The extrapolated J value at 2.5 mm of crack extension is 789 kJ/m 2, very similar to the saturated, thermally-aged result, as shown in Figure 14 for Heat 69 from Reference 1.
640 480 1-1 320
        -74 160 0.5             1.0           1.             2.0 Crack Extension (mm)
Figure 23. The J-R curve for specimen B-1.
Similarly, the results for Specimen F-1 (static-cast CF-8 material taken from Heat 68, with approximately 23% delta ferrite, thermally aged for 10,000 hours at 400'C and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 41 - also taken from Reference 2.
The extrapolated J value at 2.5 mm of crack extension is 657 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 from Reference 1 for Heat 68.
12
 
BWRVIP 2015-025 640                       . .   . .
Specimen F-1 CF-8, aged, 0.08 dpa 480       Low-DO high-purity water, 3200CI            A 62 J=1 372"Aao.
E 320 V,       I 160                                               AI max 0
0.0           0.5           1.0             1.5           2.0 Crack Extension (mm)
Figure 41. The J-R curve of specimen F-i.
Finally, the results for Specimens I-1 (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, unaged but subjected to a neutron irradiation dose of 0.08 dpa) and J-1I (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, thermally aged for 10,000 hours at 4001C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figures 49 and 58 - also taken from Reference 2. In this case the extrapolated J value at 2.5 mm of crack extension for Specimen J-1 is 466 k/m , which can be compared to the results shown in Figure 15 from Reference forI Heat 75 that appear to be of the order of 300 to 400 kJ/m 2 at room temperature and operating temperature.
13
 
BWR VIP 2015-025 640   ..     .       I  .I .     .       .   .     .
Specimen I-1 CF-8M, unaged, 0.0       -
dna
                                          ~5~~
Low-DO high-purity       water,       320PC           .
480 I
I mJ= J7 I
cm                                                            336-Aa I
320 max     I' 160 IAamax 2
                              =145 kJ/m I
n                  I 0               0.5             1.0             1.5         2.0 Crack Extension (mm)
Figure 49. The JR curve of specimen I-1.
640 480 (N-320 160 2.0 Crack Extension (mm)
Figure 58. The JR curve of specimen J-1.
14
 
BWRVIP 2015-025 Conclusions and Recommendation This review and summary of available data on CF-3, CF-8, and CF-8M CASS materials subjected to both individual and combined effects of thermal aging and neutron irradiation embrittlement demonstrated that:
Thermal aging embrittlement effects on high-Mo grades are significantly more pronounced than the effects on the low-Mo grades, by roughly a factor of two or more based upon lower-bound crack growth resistance estimates. For CF-3, the lower-bound crack growth resistance values at 2.5 mm of crack extension for > 15% delta ferrite vary between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 kJ/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2 which are significantly lower compared to CF-3/8. These results are consistent with the results obtained by examining actual crack growth resistance value measurements at 2.5 mm of crack extension for the thermal aging to saturation for CF-3 and CF-8 materials (low-Mo) that range between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material (high-Mo) are less than half of the low-molybdenum material values.
* There is no significant difference between the static-cast lower-bound estimates and the centrifugally-cast lower-bound estimate for CF-3 and CF-8 materials, and those relatively small differences are roughly identical to differences between CF-3 and CF-8 lower-bound estimates. Using lower-bound crack growth resistance values at 2.5 mm of crack 2
extension as the comparative measure, the CF-3 static-cast values of 364 and 410 kJ/m compare very well to the 477 and 478 kJ/m 2 values for centrifugally-cast material, while the CF-8 static-cast values of 343 and 366 kJ/m 2 compare favorably with the 427 and 451 kJ/m 2 values for centrifugally-cast material. The differences between static-cast and centrifugally-cast values, and between CF-3 and CF-8 values are both inconsequential in comparison to the differences between low-Mo and high-Mo materials. Therefore these two grades may be considered as a combined category for screening purposes.
* The added effect of neutron irradiation embrittlement does not change the conclusions drawn with respect to low-Mo versus high-Mo fracture toughness. Finally, since the conclusions are drawn primarily from static-cast fracture toughness data, a recommendation to the NRC staff to maintain the screening threshold for low-Mo static-cast grades at 20% is supported by the data.
Therefore, this review shows that the CF-8M data provide an extremely conservative and thus unrepresentative lower bound to the data for the low-molybdenum grades. As such, the CF-8M lower bound is separable and distinct from the low-molybdenum grade lower bounds, which therefore require their own screening category and fracture toughness estimates. Thus, the delta ferrite levels stated in the BWRVIP-234 RAI response (from the Grimes letter) is further supported by this evaluation.
Finally, this review and the associated quantitative comparisons utilize the data sets as delineated in extensive documentation in NUREG/CR-4513, Revision 1 [1] and other relevant publically available references.
Finally, this review and the associated quantitative comparisons utilize the data sets as delineated in extensive documentation in NUREG/CR-4513, Revision 1 [1] and other relevant publically available references.
15 BWRVIP 2015-025 References
15
[1]. 0. K. Chopra, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," NUREG/CR-4513 (ANL-93/22), Revision 1, Argonne National Laboratory, Argonne, Illinois (August 1994).[2]. Y. Chen, B. Alexandreanu, and K. Natesan, "Crack Growth Rate and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Report No. ANL-12/56, Argonne National Laboartory, Argonne, Illinois (November 2012).16 BWRVIP 2015-025 Attachment B Conclusions Regarding Screening Criteria for Irradiation Embrittlement of CASS Materials The screening criteria for TE and IE in CASS components proposed and discussed with the NRC[1] appears to be based on materials testing data that includes a high-molybdenum material, grade CF-8M, presented in Figure 64 in NUREG 7027 [2], with the following conclusions on page 79: 1. CF-8M materials represent a 'worst case' for thermal embrittlement
 
: 2. Thermal aging does not seem to lower the toughness below that expected for irradiation alone at the dose levels examined.In regards to the use of this data, it is important to note that:* CF-8M materials are not present in LWR core internal components.
BWRVIP 2015-025 References
* Moreover, the embrittlement identified in NUREG-7027 is conservative because many of the heats examined had delta ferrite contents greater than 20% and as high as 42% [3].It is also important to emphasize that in LWR reactor internals, delta ferrite content does not typically exceed 20% as compared to the materials assessed in the NUREG database[2, 3].* Loss of fracture toughness due to thermal embrittlement is driven by the amount of delta ferrite in a given material, thus the use of high delta ferrite material data is also conservative.
[1]. 0. K. Chopra, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," NUREG/CR-4513 (ANL-93/22), Revision 1, Argonne National Laboratory, Argonne, Illinois (August 1994).
* ANL results comparing loss of fracture toughness measurements on unaged, thermally aged only, irradiation aged only and sequentially thermally aged and irradiation aged CF-3 and CF-8 materials show significant loss of toughness on all forms of aging.Measured toughnesses of thermally aged, irradiation aged and sequentially thermal plus irradiation aged materials are similar. Given the variances that are inherent in estimating J values as material characteristics, the differences in loss of toughness cited in Reference 4 cannot be taken to unequivocally demonstrate that irradiation and thermal aging are significantly additive effects to the loss of toughness in CF-3 and CF-8 cast austenitic stainless steels.* The data summarized in Figure 64 of NUREG-7027 includes many high ferrite content and Mo-containing chemical compositions.
[2]. Y. Chen, B. Alexandreanu, and K. Natesan, "Crack Growth Rate and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Report No. ANL-12/56, Argonne National Laboartory, Argonne, Illinois (November 2012).
The correlations developed in analyses based on this database are therefore expected to be very conservative with regard to the irradiation and thermal response of low ferrite content and low Mo containing chemical compositions.
16
17 BWRVIP 2015-025 The NRC is concerned that interaction between thermal and irradiation embrittlement mechanisms may lower the fracture toughness of CASS material below levels expected from the effect of either mechanism alone. Based on the potential for a synergistic effect and taking into account the NUREG-7027 data, the NRC has concluded that a very low level of irradiation would reduce the fracture toughness of a CASS component below the 255 KJ/m 2 criteria.This led to the NRC proposing a neutron irradiation screening criteria of 0.45 dpa for low molybdenum static CASS components with 15-20% delta ferrite. By reexamination of the data in NUREG-7027 a considerable amount of conservatism can be removed from the analysis while still providing reasonable assurance that CASS components in the LWR environment will retain adequate fracture toughness through the period of extended operations.
 
The irradiated materials data from NUREG-7027 were digitized from the plots of NUREG-7027 and reanalyzed to produce a trend curve for irradiated CF-3 and CF-8 materials only as shown in Figure 1 below. Note that the exposures of these materials not only represent irradiation effects but also some degree of thermal embrittlement.
BWRVIP 2015-025 Attachment B Conclusions Regarding Screening Criteria for Irradiation Embrittlement of CASS Materials The screening criteria for TE and IE in CASS components proposed and discussed with the NRC
These data for CF-3 and CF-8 materials are most relevant to the behavior of CASS in LWR internals, as these are the materials that are principally known to be present in LWR reactor internals.
[1] appears to be based on materials testing data that includes a high-molybdenum material, grade CF-8M, presented in Figure 64 in NUREG 7027 [2], with the following conclusions on page 79:
Thus the correlation and proposed screening criteria are appropriately developed for these materials.
: 1. CF-8M materials represent a 'worst case' for thermal embrittlement
As an outcome of this analysis a plot of fracture toughness against neutron exposure was created, and a 'best fit' line was developed and the resulting curve was calculated to have a strong correlation with the data (R 2=0.94). The best fit line was then modified using conservative engineering judgment and standard curve offsetting techniques to bound all of the irradiated CF-3 and CF-8 material measured toughness values. (i.e., the pre-exponential constant multiplier was reduced by approximately 25% and the exponential factor was increased by 35% in order to bound every data point above the red-line exponential curve fit.) A constant of 30 kJ/m 2 was also included as a saturated fracture toughness value.This saturated fracture toughness value is proposed by Chopra in NUREG-7027, and the overall form of the equation is consistent with irradiation hardening models [6]. This results in a curve fit where all data points are above the curve, with resulting curve fit of: KJ e_.25xdpa J2.Smm = 30 + 520 -- x e x This bounding line is shown as a red line in Figure 1.By using the red (lower bound) line as a gauge for how CF-3 and CF-8 materials will age in the LWR environment, it can be shown that these materials will not encroach upon the 255 KJ/m 2 fracture toughness limit until the fluence level experienced by these components approaches 3.3 dpa. The industry proposed use of I dpa for neutron exposure screening criteria, provides more than a 2 dpa margin on neutron exposure between a CASS component at 1 dpa and the 255 18 BWRVIP 2015-025 KJ/m 2 fracture toughness limit. At 1 dpa, the fracture toughness predicted by the bounding curve in Figure 1 is 435 KJ/m 2 , which results in a fracture toughness margin of 180 KJ/m 2.Therefore, the industry's proposed criterion of 1 dpa has substantial margin in both the fluence and fracture toughness domains. This analysis and argument supports the use of the irradiation screening criteria of I dpa proposed by the industry for low molybdenum CASS components with ferrite content less than 20 percent.Additionally, a study designed to investigate the potential interaction between thermal and irradiation embrittlement mechanisms concluded that irradiation can reduce the extent of thermal aging effects [5], suggesting an antergistic effect between the two mechanisms rather than a synergistic one.This information indicates that the NRC's position is highly conservative, and that the industry's position on the screening criteria of CASS components, while also conservative, is justified.
: 2. Thermal aging does not seem to lower the toughness below that expected for irradiation alone at the dose levels examined.
In regards to the use of this data, it is important to note that:
* CF-8M materials are not present in LWR core internal components.
* Moreover, the embrittlement identified in NUREG-7027 is conservative because many of the heats examined had delta ferrite contents greater than 20% and as high as 42% [3].
It is also important to emphasize that in LWR reactor internals, delta ferrite content does not typically exceed 20% as compared to the materials assessed in the NUREG database
[2, 3].
* Loss of fracture toughness due to thermal embrittlement is driven by the amount of delta ferrite in a given material, thus the use of high delta ferrite material data is also conservative.
* ANL results comparing loss of fracture toughness measurements on unaged, thermally aged only, irradiation aged only and sequentially thermally aged and irradiation aged CF-3 and CF-8 materials show significant loss of toughness on all forms of aging.
Measured toughnesses of thermally aged, irradiation aged and sequentially thermal plus irradiation aged materials are similar. Given the variances that are inherent in estimating J values as material characteristics, the differences in loss of toughness cited in Reference 4 cannot be taken to unequivocally demonstrate that irradiation and thermal aging are significantly additive effects to the loss of toughness in CF-3 and CF-8 cast austenitic stainless steels.
* The data summarized in Figure 64 of NUREG-7027 includes many high ferrite content and Mo-containing chemical compositions. The correlations developed in analyses based on this database are therefore expected to be very conservative with regard to the irradiation and thermal response of low ferrite content and low Mo containing chemical compositions.
17
 
BWRVIP 2015-025 The NRC is concerned that interaction between thermal and irradiation embrittlement mechanisms may lower the fracture toughness of CASS material below levels expected from the effect of either mechanism alone. Based on the potential for a synergistic effect and taking into account the NUREG-7027 data, the NRC has concluded that a very low level of irradiation would reduce the fracture toughness of a CASS component below the 255 KJ/m 2 criteria.
This led to the NRC proposing a neutron irradiation screening criteria of 0.45 dpa for low molybdenum static CASS components with 15-20% delta ferrite. By reexamination of the data in NUREG-7027 a considerable amount of conservatism can be removed from the analysis while still providing reasonable assurance that CASS components in the LWR environment will retain adequate fracture toughness through the period of extended operations.
The irradiated materials data from NUREG-7027 were digitized from the plots of NUREG-7027 and reanalyzed to produce a trend curve for irradiated CF-3 and CF-8 materials only as shown in Figure 1 below. Note that the exposures of these materials not only represent irradiation effects but also some degree of thermal embrittlement. These data for CF-3 and CF-8 materials are most relevant to the behavior of CASS in LWR internals, as these are the materials that are principally known to be present in LWR reactor internals. Thus the correlation and proposed screening criteria are appropriately developed for these materials.
As an outcome of this analysis a plot of fracture toughness against neutron exposure was created, and a 'best fit' line was developed and the resulting curve was calculated to have a strong correlation with the data (R2=0.94). The best fit line was then modified using conservative engineering judgment and standard curve offsetting techniques to bound all of the irradiated CF-3 and CF-8 material measured toughness values. (i.e., the pre-exponential constant multiplier was reduced by approximately 25% and the exponential factor was increased by 35% in order to bound every data point above the red-line exponential curve fit.) A constant of 30 kJ/m 2 was also included as a saturated fracture toughness value.
This saturated fracture toughness value is proposed by Chopra in NUREG-7027, and the overall form of the equation is consistent with irradiation hardening models [6]. This results in a curve fit where all data points are above the curve, with resulting curve fit of:
KJ     e_.25xdpa J2.Smm =       30 + 520 -- x e             x This bounding line is shown as a red line in Figure 1.
By using the red (lower bound) line as a gauge for how CF-3 and CF-8 materials will age in the 2
LWR environment, it can be shown that these materials will not encroach upon the 255 KJ/m fracture toughness limit until the fluence level experienced by these components approaches 3.3 dpa. The industry proposed use of I dpa for neutron exposure screening criteria, provides more than a 2 dpa margin on neutron exposure between a CASS component at 1 dpa and the 255 18
 
BWRVIP 2015-025 KJ/m 2 fracture toughness limit. At 1 dpa, the fracture toughness predicted by the bounding curve in Figure 1 is 435 KJ/m 2 , which results in a fracture toughness margin of 180 KJ/m 2 .
Therefore, the industry's proposed criterion of 1 dpa has substantial margin in both the fluence and fracture toughness domains. This analysis and argument supports the use of the irradiation screening criteria of I dpa proposed by the industry for low molybdenum CASS components with ferrite content less than 20 percent.
Additionally, a study designed to investigate the potential interaction between thermal and irradiation embrittlement mechanisms concluded that irradiation can reduce the extent of thermal aging effects [5], suggesting an antergistic effect between the two mechanisms rather than a synergistic one.
This information indicates that the NRC's position is highly conservative, and that the industry's position on the screening criteria of CASS components, while also conservative, is justified.


==References:==
==References:==
: 1. U.S. NRC, "NRC Staff Compiled Comments on Industry CASS Screening Position," July 18, 2014 (NRC ADAMS Accession Number ML14198A282.
: 1. U.S. NRC, "NRC Staff Compiled Comments on Industry CASS Screening Position,"
: 2. NUREG/CR-7027, "Degradation of LWR Core Internal Materials due to Neutron Irradiation," December, 2010 (NRC ADAMS Accession Number ML 102790482.
July 18, 2014 (NRC ADAMS Accession Number ML14198A282.
: 2. NUREG/CR-7027, "Degradation of LWR Core Internal Materials due to Neutron Irradiation," December, 2010 (NRC ADAMS Accession Number ML102790482.
: 3. NUREG/CR-4513, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," U.S. Nuclear Regulatory Commission, August 1994 (NRC ADAMS Accession No. ML052360554).
: 3. NUREG/CR-4513, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," U.S. Nuclear Regulatory Commission, August 1994 (NRC ADAMS Accession No. ML052360554).
: 4. ANL-12/56, "Crack Growth and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Argonne National Lab., November 2012.5. K Fuji, K. Fukuya, "Effects of Radiation on Spinodal Decomposition of Ferrite in Duplex Stainless Steel," Journal of Nuclear Materials, May 2012. Presented at the NuMat 2012 Conference, pages 613 to 616, October 22-25, 2012, Osaka, Japan.6. Was, Gary S., "Fundamentals of Radiation Materials Science: Metals and Alloys," Springer-Verlag, 2007.7. Kim, C., R. Lott, S. Byrne, M. Burke, and G. Gerzen, "Embrittlement of Cast Austenitic Stainless Steel Reactor Internals Components," Proc. 6th Intl. Symp. On Contribution of Materials Investigations to Improve the Safety and Performance of LWRs, Fontevraud 6, French Nuclear Energy Society, SFEN, Fontevraud Roayal Abbey, France, September 18-22, 2006.19 BWRVIP 2015-025 Figure 1 -Irradiated CF-3 and CF-8 Fracture Toughness Data from Literature (Refs. 2, 4 and 7)Fracture Toughness of Irradiated CF3 and CF8 (0.02 dpa and greater)1000 900 800 700 E 500~400 300 200 100 0 0 1 2 3 4 5 6 7 8 9 10 Neutron Exposure (dpa)11 12 13 14 15 16 17 18 20 Attachment C Reactor Internals CASS Flaw Tolerance In the draft Interim Staff Guidance (ISG) on Aging Management of CASS Reactor Vessel Internal Components, issued in June 2014, the NRC technical position observed that "The fracture toughness screening.
: 4. ANL-12/56, "Crack Growth and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Argonne National Lab., November 2012.
value of 255 kJ/m 2 specified in the Grimes Letter is based on a generic flaw tolerance evaluation for piping, and may be overly conservative for RVI CASS components that are subject to mainly compressive stresses during operation, and are part of a population of redundant components where failure of individual components can be tolerated." The technical position went on to add that "therefore, the staff applies the 255 kJ/m 2 value for screening purposes with the knowledge that there likely is additional conservatism present in this screening for non-pressure boundary RVI components." In an effort to provide further evidence with respect to the NRC staff technical position, some industry efforts since the July 15, 2014 meeting with the NRC staff have been directed toward this issue. The results are summarized in the following paragraphs.
: 5. K Fuji, K. Fukuya, "Effects of Radiation on Spinodal Decomposition of Ferrite in Duplex Stainless Steel," Journal of Nuclear Materials, May 2012. Presented at the NuMat 2012 Conference, pages 613 to 616, October 22-25, 2012, Osaka, Japan.
The industry selected three different geometries that can be related to typical BWR and PWR CASS reactor internals in order to estimate flaw tolerance capability:
: 6. Was, Gary S., "Fundamentals of Radiation Materials Science: Metals and Alloys,"
(1) a large-diameter cylinder with a through-wall vertical flaw located in a longitudinal seam weld, subjected to combined membrane and bending stress; (2) an edge-cracked beam-column subjected to combined membrane and bending stress; and (3) a six-inch-diameter, Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure.
Springer-Verlag, 2007.
The internal pressure for the third geometry was selected such that the circumferential tensile stress in the pipe was identical to the membrane tensile stress level chosen for the first two geometries.
: 7. Kim, C., R. Lott, S. Byrne, M. Burke, and G. Gerzen, "Embrittlement of Cast Austenitic Stainless Steel Reactor Internals Components," Proc. 6th Intl. Symp. On Contribution of Materials Investigations to Improve the Safety and Performance of LWRs, Fontevraud 6, French Nuclear Energy Society, SFEN, Fontevraud Roayal Abbey, France, September 18-22, 2006.
In all three case studies, the initial flaw size (length for the first and third geometries, and depth for the second geometry) was selected to be consistent with reactor vessel internals fabrication workmanship standards.
19
No flaw growth criteria were applied to the initial flaw sizes, although the initial flaw sizes were increased to some extent in order to determine the rate at which the crack driving force increased as a function of the increase in flaw size.For the first geometry (large-diameter cylinder with through-wall vertical flaw), the diameter was selected to be 452 inches with a wall thickness of either one or two inches, the membrane tensile stress was selected to be 5 ksi, and the bending stress was selected to be 7.5 ksi. The total initial flaw length was selected to be 0.226 inches (about 1/4-inch in length), but was increased in increments up to 4.294 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. For the largest initial flaw lengths examined, the typical LEFM stress intensity is of the order of 25 ksiin, which converts to an elastic-plastic crack driving force of about 4 kJ/m 2.This implies a very large margin relative to the screening value of 255 kJ/m 2.For the second geometry (edge-cracked beam column), the solid column diameter was selected to be three inches, and the membrane and bending stresses were selected to be identical to those selected for the first geometry.
 
The smallest initial flaw depth was selected as 0.1 inches, and was incremented by 0.1 inch up to a maximum depth of 1.7 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 lillview Avenue, Palo Alto, CA 94304-1395 USA
BWRVIP 2015-025 Figure 1 - Irradiated CF-3 and CF-8 Fracture Toughness Data from Literature (Refs. 2, 4 and 7)
Fracture Toughness of Irradiated CF3 and CF8 (0.02 dpa and greater) 1000 900 800 700 E   500
  ~400 300 200 100 0
0 1     2     3     4       5     6       7       8     9     10     11     12     13 14 15 16 17 18 Neutron Exposure (dpa) 20
 
Attachment C Reactor Internals CASS Flaw Tolerance In the draft Interim Staff Guidance (ISG) on Aging Management of CASS Reactor Vessel Internal Components, issued in June 2014, the NRC technical position observed that "The fracture toughness screening. value of 255 kJ/m 2 specified in the Grimes Letter is based on a generic flaw tolerance evaluation for piping, and may be overly conservative for RVI CASS components that are subject to mainly compressive stresses during operation, and are part of a population of redundant components where failure of individual components can be tolerated."
The technical position went on to add that "therefore, the staff applies the 255 kJ/m 2 value for screening purposes with the knowledge that there likely is additional conservatism present in this screening for non-pressure boundary RVI components." In an effort to provide further evidence with respect to the NRC staff technical position, some industry efforts since the July 15, 2014 meeting with the NRC staff have been directed toward this issue. The results are summarized in the following paragraphs.
The industry selected three different geometries that can be related to typical BWR and PWR CASS reactor internals in order to estimate flaw tolerance capability: (1) a large-diameter cylinder with a through-wall vertical flaw located in a longitudinal seam weld, subjected to combined membrane and bending stress; (2) an edge-cracked beam-column subjected to combined membrane and bending stress; and (3) a six-inch-diameter, Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure. The internal pressure for the third geometry was selected such that the circumferential tensile stress in the pipe was identical to the membrane tensile stress level chosen for the first two geometries. In all three case studies, the initial flaw size (length for the first and third geometries, and depth for the second geometry) was selected to be consistent with reactor vessel internals fabrication workmanship standards. No flaw growth criteria were applied to the initial flaw sizes, although the initial flaw sizes were increased to some extent in order to determine the rate at which the crack driving force increased as a function of the increase in flaw size.
For the first geometry (large-diameter cylinder with through-wall vertical flaw), the diameter was selected to be 452 inches with a wall thickness of either one or two inches, the membrane tensile stress was selected to be 5 ksi, and the bending stress was selected to be 7.5 ksi. The total initial flaw length was selected to be 0.226 inches (about 1/4-inch in length), but was increased in increments up to 4.294 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. For the largest initial flaw lengths examined, the typical LEFM stress intensity is of the order of 25 ksiin, which converts to an elastic-plastic crack driving force of about 4 kJ/m 2 . This implies a very large margin relative to the screening value of 255 kJ/m2 .
For the second geometry (edge-cracked beam column), the solid column diameter was selected to be three inches, and the membrane and bending stresses were selected to be identical to those selected for the first geometry. The smallest initial flaw depth was selected as 0.1 inches, and was incremented by 0.1 inch up to a maximum depth of 1.7 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 lillview Avenue, Palo Alto, CA 94304-1395 USA
* 650.855.2000
* 650.855.2000
* Customer Service 800.313.3774
* Customer Service 800.313.3774
* www.epri.com BWRVIP 2015-025 J-crack driving forces. For the largest initial flaw depth examined (1.7 inches), the LEFM stress intensity was 42 ksiIin, which converts to an elastic-plastic crack driving force of about 10 kJ/m 2.Again, this calculation implies a very large margin relative to the screening value of 255 kJ/m 2.For the third geometry (six-inch diameter Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure), the internal pressure was selected such that the circumferential stress was approximately 5 ksi, matching the membrane tensile stress used for the first and second geometries.
* www.epri.com
Because of the thin pipe wall, this case was found to be the most critical of the three geometries.
 
The initial flaw length was selected to be 0.1 inches, and was then incremented in 0.1-inch increments up to a maximum flaw length of 2.0 inches. For this case, the applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. In addition, this case was also analyzed using elastic-plastic fracture mechanics, in order to compare derived crack-driving forces with directly calculated elastic-plastic crack-driving forces. For an initial flaw length of 2.0 inches, the LEFM stress intensity factor was about 54 ksi/in, which converts to a crack driving force of about 96 in-lb/in 2 or about 16 kJ/m 2.The directly-calculated elastic-plastic crack driving force is almost exactly the same, but very slightly lower. When the initial flaw length was doubled -to about 4.0 inches, the applied LEFM stress intensity was found to be 120 ksi/in, which converts to a crack driving force of about 476 in-lb/in 2 or about 83 kJ/m 2.Even for this very severe example, the calculations show a sizable margin relative to the screening value of 255 kJ/m 2.From this exercise, CASS reactor internals components subjected to nominal stress levels, even in the presence of initial flaws that are well beyond fabrication workmanship acceptance criteria, are extremely flaw tolerant, with margins against flaw instability of the order of a factor of five to 10 relative to the fracture toughness screening criterion of 255 kJ/m 2 specified in the Grimes letter. When this flaw tolerance is coupled with the additional margin inherent in the separation of CF-3/CF-8 screening data from CF-8M screening data, the conservatism of the industry technical position is further confirmed.
BWRVIP 2015-025 J-crack driving forces. For the largest initial flaw depth examined (1.7 inches), the LEFM stress intensity was 42 ksiIin, which converts to an elastic-plastic crack driving force of about 10 kJ/m 2 . Again, this calculation implies a very large margin relative to the screening value of 255 kJ/m 2 .
22 BWRVIP 2015-025 Attachment D Tahlo I virarlld o/- larrto RPnonpe (Indivetru PnaifinnI 23}}
For the third geometry (six-inch diameter Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure), the internal pressure was selected such that the circumferential stress was approximately 5 ksi, matching the membrane tensile stress used for the first and second geometries. Because of the thin pipe wall, this case was found to be the most critical of the three geometries. The initial flaw length was selected to be 0.1 inches, and was then incremented in 0.1-inch increments up to a maximum flaw length of 2.0 inches. For this case, the applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM),
and were then converted to J-crack driving forces. In addition, this case was also analyzed using elastic-plastic fracture mechanics, in order to compare derived crack-driving forces with directly calculated elastic-plastic crack-driving forces. For an initial flaw length of 2.0 inches, the LEFM stress intensity factor was about 54 ksi/in, which converts to a crack driving force of about 96 in-lb/in 2 or about 16 kJ/m 2. The directly-calculated elastic-plastic crack driving force is almost exactly the same, but very slightly lower. When the initial flaw length was doubled - to about 4.0 inches, the applied LEFM stress intensity was found to be 120 ksi/in, which converts to a crack driving force of about 476 in-lb/in 2 or about 83 kJ/m 2 . Even for this very severe example, the calculations show a sizable margin relative to the screening value of 255 kJ/m 2 .
From this exercise, CASS reactor internals components subjected to nominal stress levels, even in the presence of initial flaws that are well beyond fabrication workmanship acceptance criteria, are extremely flaw tolerant, with margins against flaw instability of the order of a factor of five to 10 relative to the fracture toughness screening criterion of 255 kJ/m 2 specified in the Grimes letter. When this flaw tolerance is coupled with the additional margin inherent in the separation of CF-3/CF-8 screening data from CF-8M screening data, the conservatism of the industry technical position is further confirmed.
22
 
BWRVIP 2015-025 Attachment D Tahlo I   virarlld o/- larrto RPnonpe (Indivetru PnaifinnI 23}}

Latest revision as of 03:57, 31 October 2019

Official Exhibit - ENT000663-00-BD01 - Letter from A. Mcgehee & T. Hanley, EPRI, to NRC DCD, BWRVIP 2015-025, Project No. 704-Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR React
ML15334A267
Person / Time
Site: Indian Point  Entergy icon.png
Issue date: 03/09/2015
From:
Entergy Nuclear Operations
To:
Atomic Safety and Licensing Board Panel
SECY RAS
References
RAS 28136, ASLBP 07-858-03-LR-BD01, 50-247-LR, 50-286-LR
Download: ML15334A267 (23)


Text

United States Nuclear Regulatory Commission Official Hearing Exhibit In the Matter of: Entergy Nuclear Operations, Inc. ENT000663 (Indian Point Nuclear Generating Units 2 and 3)

ASLBP #: 07-858-03-LR-BD01 Submitted: August 10, 2015 Docket #: 05000247 l 05000286 Exhibit #: ENT000663-00-BD01 Identified: 11/5/2015 Admitted: 11/5/2015 Withdrawn:

Rejected: Stricken:

Other:

2l1I ELECTRIC POWER L RESEARCH INSTITUTE

'e, 2015-025 BWR Vessel & Internals Project (BWRVIP)

March 09, 2015 Document Control Desk U.S. Nuclear Regulatory Commission 11555 Rockville Pike Rockville, MD 20852 Attention: Joseph Holonich

Subject:

Project No. 704 - Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR Reactor Internals Fabricated of Cast Austenitic Stainless Steel

References:

1. Letter from D. Madison (BWRVIP Chairman) and A. McGehee (BWRVIP Program Manager) to J. Holonich (NRC), Project No. 704 - BWRVIP Response to NRC Request for Additional Information on BWRVIP-234, dated May 23, 2014. ADAMS - ML14174A841.
2. Letter from J. Holonich (NRC) to A. Mendiola (NRC), Summary of the July 15, 2014, Meeting with the Electric Power Research Institute on Items Related to Cast Austenitic Stainless Steel and the Materials Reliability Program-227-A, "Pressurized Water Reactor Internals Inspection And Evaluation Guidelines,"

September 9, 2014. ADAMS - ML14127A077.

3. "NRC Position on Aging Management of CASS Reactor Vessel Internal Components," June 23, 2014, ADAMS - ML14174A719.
4. Email from C. Wirtz (EPRI) to J. Holonich (NRC), October 7, 2014.
5. NUREG/CR-4513, ANL-93/22, Revision 1, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," Argonne National Laboratory, May 1994.

The purpose of this letter is to provide the status of the Industry (PWR and BWR) activities associated with developing and proposing a generic screening criteria to address thermal and irradiation embrittlement of RPV internals fabricated of cast austenitic stainless steel (CASS).

Reference I was provided to the NRC in response to a Request for Additional Information (RAI) regarding BWRVIP-234. The RAI response contained supplemental information that provided the technical bases for an Industry screening criteria for CASS internals.

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BWRVIP 2015-025 A meeting was later held on July 15, 2014 at NRC offices in Washington, DC to discuss the Industry and NRC positions (References 2, 3). Based on that meeting, the Industry committed to investigate additional information where there was disagreement with the NRC regarding the screening criteria and provide said information to the NRC at a later date. That information was informally submitted for NRC's consideration (Reference 4) and is contained in Attachments A through D of this letter. A conference call was then held on November 20, 2014 with the NRC to discuss this information.

Following this conference call the NRC indicated that they were not willing to deviate from their position documented in Reference 3.

Despite the NRC's current stance on the matter, the following comments regarding a generic TE and IE criteria for evaluation of reactor internals are important in forming the basis for the industry position:

" The industry recognizes that the NRC is intending to revise its original IE position in the Grimes letter from lxl10 7 n/cm 2 (0.00014 dpa) to a position in the region of 0.5 to 1.5 dpa. Industry agrees that this position is more appropriate and has proposed a conservative value of 1 dpa.

  • It is not appropriate (for the staff) to penalize all non-Mo containing CASS (such as CF3 and CF8) because of the lower properties associated with the Mo-containing CF8M materials that are included in the ANL/NRC database, i.e., impose a lower bound.
  • There is no substantive data that demonstrates a synergistic effect for CASS materials that are typical of reactor internals (such as CF3 and CF8). As such the industry has proposed criteria that do not combine TE and IE. Each mechanism is considered distinct and separate.

" The introduction of a new criteria set for the category of materials with ferrite content between 15% to 20% having a lower proposed screening value for IE of 0.45 dpa is unnecessary and technically unfounded. The introduction of this category of ferrite content is significantly burdensome to licensees since it will require more complex and potentially more error-prone assessments of CASS material components by virtue of having more categories. Industry maintains that the categories of materials and associated ferrite levels contained in the Grimes letter are appropriate.

" The criteria proposed by the industry (20% Ferrite and 1 dpa) have been shown to project significant margin on toughness reduction and therefore safety when compared to measured embrittlement behavior for CF3 and CF8 materials.

Regardless, this letter serves to formally submit this additional information to the NRC for review and consideration in developing a regulatory position for the screening criteria associated with TE and IE for CASS internals and to inform revisions to NUREG-4513, Rev. 1 (Reference 5). The PWR and BWR Industry position for TE and IE screening criteria is shown in Attachment D.

2

BWRVIP 2015-025 Irrespective of the staff's decision and future promulgation of a regulatory position on TE and IE for CASS internals, the BWRVIP formally requests the NRC to evaluate and resolve the RAI responses associated with BWRVIP-234 and issue a Safety Evaluation.

If you have any questions on this subject please call Ron DiSabatino (Exelon, BWRVIP Assessment Committee Technical Chairman) at 717.456.3685.

Sincerely, 24 Andrew McGehee, EPRI, BWRVIP Program Manager Tim Hanley, Exelon Corp., BWRVIP Chairman 3

BWRVIP 2015-025 Industry Response to July 15, 2014 Meeting with NRC on CASS On July 15, 2014, representatives from the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS) met with the NRC staff to discuss the thermal and irradiation embrittlement screening criteria for cast austenitic stainless steel. While the working group and NRC staff were in general agreement on the thermal embrittlement (TE) screening criteria, there was a marked difference of opinion on the irradiation embrittlement (IE) screening criteria, particularly for materials with delta ferrite contents of 15-20% (the NRC proposed 0.45 dpa, while the industry proposed 1 dpa).

Agreement was reached on the TE screening criteria in part because the data on low-molybdenum and high-molybdenum material are considered separately, resulting in separate TE screening criteria for these materials. This distinction is made because high-molybdenum materials show a distinctly greater loss of fracture toughness from TE and IE effects than low-molybdenum materials. This is reviewed and discussed further in Attachment A The separate consideration of low- and high-molybdenum materials test data was not carried over into the IE domain. The data set used to determine the NRC's position on IE was obtained from NUREG-7027, which considered irradiated high- and low-molybdenum materials together, along with data on irradiated welds. Because these materials were considered together, the resulting lower bound curve is judged to be overly conservative relative to the low-molybdenum material. A reexamination of this data (see Attachment B), shows that by considering the low-molybdenum materials test data independently of the other materials it can be concluded that there is a substantial safety margin in the industry's proposed I dpa screening criteria.

These screening criteria are being implemented to ensure that CASS components in reactor vessel internals maintain adequate fracture toughness during the period of extended operation.

The screening level to determine whether this requirement was met was a J value of 255 KJ/m2 at a crack extension of 2.5 mm. This value was originally determined for pressure boundary components (i.e., large diameter piping, etc.) and was expected to be highly conservative for application to reactor vessel internals. Additional calculations (see Attachment C) demonstrate the level of this conservatism and show that reactor vessel internal components can safely operate with fracture toughness values much lower than the 255 KJ/m 2 value specified in the Grimes letter.

In summary, the actions taken by the CASS industry working group and summarized in Attachments A, B and C support the proposed screening criteria contained in Attachment D.

These criteria provide a significant amount of margin for screening of TE and IE. It is concluded that that the use of the proposed screening criteria will allow for continued safe and reliable operation of the LWR fleet.

4

BWRVIP 2015-025 Attachment A Discussion on Low Molybdenum vs High Molybdenum CASS Grades Introduction A meeting was held on July 15, 2014 at the NRC Office in Washington, DC between the staff of the U.S. Nuclear Regulatory Commission (NRC) and the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS). The topic of discussion focused on the thermal aging and neutron irradiation embrittlement screening criteria (separately) proposed by the industry and the NRC staff. The proposals included criteria for low-molybdenum CASS grades, such as CF-3 and CF-8, and high-molybdenum CASS grades, such as CF-8M. There was agreement between industry and the NRC staff regarding the differences in such measures of embrittlement as elastic-plastic crack growth resistance (J-R curve) for the low-Mo materials versus the high-Mo materials, at least where thermal aging embrittlement effects are dominant. In fact, screening criteria proposed by the staff are identical to the industry-proposed screening criteria for the case of thermal aging embrittlement.

However, the areas of agreement between the industry and the staff did not carry over to combined environments where the effects of neutron irradiation embrittlement begin to approach the same level as those from thermal aging embrittlement. In order to address these differences in criteria, the available data for CF-3, CF-8, and CF-8M materials in the literature are reviewed and assessed, with a recommendation to the NRC staff for a change to their proposed criteria to more closely agree with the criteria proposed by the industry.

Review and Summary of Thermal Aging Embrittlement Data The significant differences in thermal aging embrittlement behavior of the low-molybdenum grades of cast austenitic stainless steel, such as CF-3 and CF-8, versus the thermal aging embrittlement behavior of the high-molybdenum grades, such as CF-8M, have been known for at least two decades, with extensive data and associated interpretations of said data documented in NUREG/CR-4513, Revision 1 [1]. The lower-bound thermal aging embrittlement estimates shown in Figures 3 (statically-cast steels) and 4 (centrifugally-cast steels) from Reference 1 with varying amounts of delta ferrite provide an excellent illustration of those significant differences, in this case with the measure of significance being the crack-growth resistance J-R curve. In particular, the lower-bound formulas cited in Section 3.1.1 of Reference 1 (and plotted in Figures 3 and 4) can be used to compare the estimated crack growth resistance values at 2.5 mm of crack extension for the CF-3, CF-8, and CF-8M steels with > 15% delta ferrite. Note that Figure 3 provides lower-bound thermal aging estimates for static-cast steels, while Figure 4 provides lower-bound thermal aging estimates for centrifugally-cast steels.

5

BWRVIP 2015-025 Crack Extension ha (in.) Crack Extension As (in.)

0.00 0.06 0.10 0.15 Lower-Bound J-R Curve Static-Camt Stes I

5.

>15% Fentbe

-290"C -4000

-3 0 J =2510Aa)

- 2 03- -3000 -

17&O

- J=M4a -2000f o

.1000k CF-4u 0.

0 1 2 3 4 0 2 3 4 S 0.00 0.06 0.10 0.15 0.00 0.06 0.10 0.15

  • I I , 'I , : : : ji , ' , :

lOOO Lower-Bound J-R Curve Lower-Bound J-IR Static-Cat Steels Static-Cast StaWsi aS 80o. l-15%Fenml 10-16% Fegrkt Room Temp. J - 274"0.3 .4000 36 j- 2740sa)03 2001&a)o cF-4 ..

800- 1 - 31(1P40 I

CF035 -3000

  • 400 j =3074Uo-38 I CF-C 400 J 130-~036 200- - CF-SM 32 10

- :j - .: '. I:

CF-Ui CFS .0 0 1 2 3 4 5 0 1 2 3 4 5 0.00 0.06 0.10 0.1( 0.00 0.06 0.10 0.15 5000" 5.

if 4000~

-3 3000 I

Ia 2000j 1000i 0

1 2 3 4 Crack Extension, Aa (mm)

Figure3. Predictedlower-bound J-R curves at RT and 290°C for static-castSSs with ferrite contents >15, 10-15. or<10%

6

BWRVIP 2015-025 Crack Extension As (in.) Crack Extension ha (in.)

0.o00. O. .O 0.1s 0.00 O.06 0.10 0.15 Lower-Bound J-R Curve Lower-Bound J-R Curve Centrifugally Cast Steels Centrifugally Cast Steels

>15% Fmist 0 37 >15%FaFnite Room Tnp. J - 304SO) . M-0C J.-3301AP,34 -4000 7 0 35 J.934r*a) " CF-s JF3348 39C- CF-S C!

j400-CF-MM -2000 '

E

~2007 -1000 CF-Sm

.. .. . . . . H i F 0 I 1 2 3 4 0 1 2 3 4 1 0.00 0.06 010 0.15 0.00 0.0S 0.10 0.15 i

r-Bound J-R Curve Lower-Bound J-R Curve C a " olyCast Steels Centrifugally Cast Steels 4SO0OI 10-15% Forte0 -4000.

)0- 2fOC J - 300ma)°35 I 04 0-36 CF-S J.30sWKa i CJ- 38M&).3 X0- CF-3 CF-3 3000

-. * '* *. 357ý,,)°

-2000 I

~20 -1000 Cf-M C0SM 0

0 1 2 3 S4 1 2 3 4 5 0O30 0.06 0.10 0.15 0.00 0.0 0.10 0.15 1000 Lower-Bound J-R Curve Lower-ilound' J-'R C'urv'e' . Lower-Bound J-R Curve Centrifugaly Cast SteDes Centrifugally Cast Steels .5000 410% Fernite - 4OO"

<10% F-f-n¶ Room TSm 07 2*0T P41 J -435(Aa~5 I:

-3000 -2 CF--3 CF-8 4001

-20001 200 - CF-SM CF-Sm .1000 a

0 1 2 3 4 5 0 2 3 4 Crack Extension., A (mm) Crack Extension, A (mm)

Figure 4. Predictedlower-bound J-R curves at RT and 290'C for centrifugally cast SSs with ferrite contents > 15. 10-15. or < 10%

7

BWRVIP 2015-025 For CF-3, the lower bound crack growth resistance, for statically- and centrifugally-cast materials, varies between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 Id/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2. When the data are examined very closely, there is no significant difference between the static-cast lower-bound estimates for CF-3 and CF-8 in Figure 3 and the centrifugally-cast lower-bound estimates for CF-3 and CF-8 in Figure 4. The data also show that these insignificant differences are roughly identical to the differences between CF-3 and CF-8 estimates within the static-cast and centrifugally-cast populations. Therefore, based on this examination of lower-bound estimates, the CF-8M data exhibit substantially lower fracture toughnesses and are therefore unsuitable as a lower-bound estimate for the low-molybdenum grades. Lower bound estimates must be conservative, but they must also remain representative of the data. Table 1, shown below, succinctly summarizes the data comparisons extracted from Figures 3 and 4 from Reference 1.

Table 1. Lower Bound Fracture Toughness Estimates CASS Steels J-values at 2.5 cm of2 Crack Comments Growth (kJ/m )

Lower bound above the threshold 2

CF-3 Steels 364 to 478 value of 255 kJ/M Lower bound above the threshold 2

CF-8 Steels 343 to 451 value of 255 kj/m CF-8M Steels 161 to 259 Lower bound might be less than2 threshold values of 255 kJ/m Table 1 clearly shows that lower bound fracture toughness values of CF-3 and CF-8 steels are much higher than CF-8M steels, and that only the fracture toughness of CF-8M steels fall below the threshold value of 255 kJ/m 2. Therefore, the screening criteria for CF-8M (high molybdenum) steels should be considered separately from CF-3 and CF-8 (low molybdenum) steels.

Thus far, the data evaluation has been based on lower-bound fracture toughness estimates derived from Charpy impact correlations. However, these lower-bound thermal aging embrittlement estimates can be confirmed by examining actual crack extension resistance curve measurements for various heats of CF-3, CF-8, and CF-8M with delta ferrite content in the range of 20%. For example, Figure 14 from Reference 1 shows J-R curve measurements, along with thermal aging saturation estimates for two heats of CF-3 material (Heat 69 and Heat I) and one heat of CF-8 material (Heat 68), while Figure 15 from Reference 1 shows similar results for three heats of CF-8M material (Heats 74, 75, and 758).

In this case, it should be noted that the actual fracture toughness data are based on thermal aging saturation conditions and are therefore somewhat higher than the lower-bound fracture toughness 8

BWRVIP 2015-025 estimates. Also note that the thermal aging saturation fracture toughness data are based entirely on static-cast data for materials with delta ferrite in the range of 15% to 25%.

The crack extension resistance value at 2.5 mm of crack extension for the thermal aging saturation conditions for CF-3 and CF-8 materials ranges between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material are less than half of the low-molybdenum material values.

Therefore, the findings from the examination of the data in Figures 14 and 15, and the derived J values at 2.5 mm of crack extension, are completely consistent with the lower-bound thermal aging embrittlement estimates cited previously for both static-cast and centrifugally-cast material. In other words, the development of screening criteria for the low-molybdenum grades should be treated separately from the development of screening criteria for the high-molybdenum grades.

9

BWRVIP 2015-025 Crack Extension, An (in.) Crack Extension, An (in.)

0.0 0.1 0.2 0.3 0.0 I . 0.1 0.2 0.3 2WC Heat 69 ~CF-3 290"C -

C' 8,-21%

~2000- .10000 "

SOAN32 a 4XOy4 0 0'

-600 0.

~1000. 0 -e 0

J.366(AW).4 at320C I0 2 4 6 a I0

] 0.1 0.2 0.3 Heat I CF-3 0

o mw4g(Aa)V bwow A 0 A ýL 200 0 2 -10000 I

0~

  • 0~ 0 10o~

100 20 a Roomm Temp.

.5 m~oC47 A00 UABW 2 4 6 . ........... 10 0 I=

0.D 0.1 0.2 0.3

.. . . . . 1 i 4 .1 1 1. 1- 1 l 1 1 Heat 68'C"- 290C a-

.0 =Sanm.7,40.4

~1 S,, 32 J.46(M -10000 I d2B0 I -

00 0 0000 0

-- 0 0ý0

-6000 0 .2g0Ag iIi I

  • I U 2 4 6 8 10 Crack Extension, As (mm) Crack Extension, A& (Mm)

Figure 14. Saturationfracture toughness J-R curves at RT and 290Co, estimatedfrom the chemical composition of static-cast CF-3 and CF-8 steels, and determined experimentally 10

BWRVIP 2015-025 Crack Extension, ha (in.) Crack Extension, ha (in.)

0.0 0.1 0.2 0.3 0.01 , . I , I 0.1I . I .

0.2 I I . I . 0.3 i.

Heal Hiai is75 'C",

CF-SM ' Ro Room Temp. ep Stall-Caa Slab -15000 C Sc

- 25%

Unapd

. Walled j . 42")0.42 - 0OAO~N4WrC tUegod 5-WA - ~J -461(A&P.

37

- -10000 32 " 0a -3OO

'Co- .o32 *y oo0 O00000OOOOC5

~1000 adI20' 8NtPA~

Oj j .l44(AS)03 -000

- . , 2 I . , . 4I I, 6 . . I 8I ' ' ' 0 0 2 4' 6 S 14 00

.10 0.1 0.2 0.3 0.0 0.1 0.2 0.3 3000-Heat 74 CF-SM Room T emp. Heat 74 CF-SM 9*

SARc--CaM Slab taw-cau SWa 6Sc=16% Uae

1m 6C16%

[Oo 040o Und J. 57" 0

)o 42 -15000 £ 492000- 0 =A000ht 0C 03 7 324Olp 32 efpy J 30(sa)

. 32 OOY N 290'Cj~

0 at320*C C)00N aOCa *? * .o0 0.! ~0 O~0

,*-- J- 03*7 al 320*C F- !!!-7 KSaknil J .WM~)U. 3 N

s 0 0 0. 4 0 6 10 0.0 0.1 0.2 0.3 0.0 0.1 0.2 0.3 Hieat 7'581 6F4 R Temp. Heat 758 CF-SM 290'C SONO-C*M Etow SUMc-CaN Elbow [ 16000 SC-21%Unap 2000-

-10000 I 32 apy 32 4P 0

J .487(aa) . 38~Id290t 32 Id 3py C

1000. &I290C at 30*C

-5000 WAOA£ kj MA AL ';'>eso J/ 2(a03 4-?>(V 3,3 O*P 0 2 4 6 8 10 0 10 Crack Extension, Aa (mm) Crack Extension, Aa (mm)

Figure 15. Saturationfracture toughness J-R curves at RT and 290*C. estimated from die chemical composition of static-castCF-SM steels, and determined experimentally 11

BWRVIP 2015-025 Review and Summary of Combined TE and IE Data The available data for purely thermally-embrittled CASS materials is quite extensive. However, that is not the case for a combination of thermal aging and neutron irradiation embrittlement. In spite of the limited data, the evaluation of available crack growth resistance data for CF-3, CF-8, and CF-8M material is not altered by including information on material subjected to both thermal aging and neutron irradiation embrittlement, as shown in Figures 23, 41, 49, and 58 from ANL-12/56 [2]. The results for Specimen B-1 (static-cast CF-3 material taken from Heat 69, with approximately 24% delta ferrite, thermally aged for 10,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> at 400'C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 23 - taken from Reference 2. The extrapolated J value at 2.5 mm of crack extension is 789 kJ/m 2, very similar to the saturated, thermally-aged result, as shown in Figure 14 for Heat 69 from Reference 1.

640 480 1-1 320

-74 160 0.5 1.0 1. 2.0 Crack Extension (mm)

Figure 23. The J-R curve for specimen B-1.

Similarly, the results for Specimen F-1 (static-cast CF-8 material taken from Heat 68, with approximately 23% delta ferrite, thermally aged for 10,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> at 400'C and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 41 - also taken from Reference 2.

The extrapolated J value at 2.5 mm of crack extension is 657 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 from Reference 1 for Heat 68.

12

BWRVIP 2015-025 640 . . . .

Specimen F-1 CF-8, aged, 0.08 dpa 480 Low-DO high-purity water, 3200CI A 62 J=1 372"Aao.

E 320 V, I 160 AI max 0

0.0 0.5 1.0 1.5 2.0 Crack Extension (mm)

Figure 41. The J-R curve of specimen F-i.

Finally, the results for Specimens I-1 (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, unaged but subjected to a neutron irradiation dose of 0.08 dpa) and J-1I (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, thermally aged for 10,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> at 4001C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figures 49 and 58 - also taken from Reference 2. In this case the extrapolated J value at 2.5 mm of crack extension for Specimen J-1 is 466 k/m , which can be compared to the results shown in Figure 15 from Reference forI Heat 75 that appear to be of the order of 300 to 400 kJ/m 2 at room temperature and operating temperature.

13

BWR VIP 2015-025 640 .. . I .I . . . . .

Specimen I-1 CF-8M, unaged, 0.0 -

dna

~5~~

Low-DO high-purity water, 320PC .

480 I

I mJ= J7 I

cm 336-Aa I

320 max I' 160 IAamax 2

=145 kJ/m I

n I 0 0.5 1.0 1.5 2.0 Crack Extension (mm)

Figure 49. The JR curve of specimen I-1.

640 480 (N-320 160 2.0 Crack Extension (mm)

Figure 58. The JR curve of specimen J-1.

14

BWRVIP 2015-025 Conclusions and Recommendation This review and summary of available data on CF-3, CF-8, and CF-8M CASS materials subjected to both individual and combined effects of thermal aging and neutron irradiation embrittlement demonstrated that:

Thermal aging embrittlement effects on high-Mo grades are significantly more pronounced than the effects on the low-Mo grades, by roughly a factor of two or more based upon lower-bound crack growth resistance estimates. For CF-3, the lower-bound crack growth resistance values at 2.5 mm of crack extension for > 15% delta ferrite vary between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 kJ/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2 which are significantly lower compared to CF-3/8. These results are consistent with the results obtained by examining actual crack growth resistance value measurements at 2.5 mm of crack extension for the thermal aging to saturation for CF-3 and CF-8 materials (low-Mo) that range between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material (high-Mo) are less than half of the low-molybdenum material values.

  • There is no significant difference between the static-cast lower-bound estimates and the centrifugally-cast lower-bound estimate for CF-3 and CF-8 materials, and those relatively small differences are roughly identical to differences between CF-3 and CF-8 lower-bound estimates. Using lower-bound crack growth resistance values at 2.5 mm of crack 2

extension as the comparative measure, the CF-3 static-cast values of 364 and 410 kJ/m compare very well to the 477 and 478 kJ/m 2 values for centrifugally-cast material, while the CF-8 static-cast values of 343 and 366 kJ/m 2 compare favorably with the 427 and 451 kJ/m 2 values for centrifugally-cast material. The differences between static-cast and centrifugally-cast values, and between CF-3 and CF-8 values are both inconsequential in comparison to the differences between low-Mo and high-Mo materials. Therefore these two grades may be considered as a combined category for screening purposes.

  • The added effect of neutron irradiation embrittlement does not change the conclusions drawn with respect to low-Mo versus high-Mo fracture toughness. Finally, since the conclusions are drawn primarily from static-cast fracture toughness data, a recommendation to the NRC staff to maintain the screening threshold for low-Mo static-cast grades at 20% is supported by the data.

Therefore, this review shows that the CF-8M data provide an extremely conservative and thus unrepresentative lower bound to the data for the low-molybdenum grades. As such, the CF-8M lower bound is separable and distinct from the low-molybdenum grade lower bounds, which therefore require their own screening category and fracture toughness estimates. Thus, the delta ferrite levels stated in the BWRVIP-234 RAI response (from the Grimes letter) is further supported by this evaluation.

Finally, this review and the associated quantitative comparisons utilize the data sets as delineated in extensive documentation in NUREG/CR-4513, Revision 1 [1] and other relevant publically available references.

15

BWRVIP 2015-025 References

[1]. 0. K. Chopra, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," NUREG/CR-4513 (ANL-93/22), Revision 1, Argonne National Laboratory, Argonne, Illinois (August 1994).

[2]. Y. Chen, B. Alexandreanu, and K. Natesan, "Crack Growth Rate and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Report No. ANL-12/56, Argonne National Laboartory, Argonne, Illinois (November 2012).

16

BWRVIP 2015-025 Attachment B Conclusions Regarding Screening Criteria for Irradiation Embrittlement of CASS Materials The screening criteria for TE and IE in CASS components proposed and discussed with the NRC

[1] appears to be based on materials testing data that includes a high-molybdenum material, grade CF-8M, presented in Figure 64 in NUREG 7027 [2], with the following conclusions on page 79:

1. CF-8M materials represent a 'worst case' for thermal embrittlement
2. Thermal aging does not seem to lower the toughness below that expected for irradiation alone at the dose levels examined.

In regards to the use of this data, it is important to note that:

  • CF-8M materials are not present in LWR core internal components.
  • Moreover, the embrittlement identified in NUREG-7027 is conservative because many of the heats examined had delta ferrite contents greater than 20% and as high as 42% [3].

It is also important to emphasize that in LWR reactor internals, delta ferrite content does not typically exceed 20% as compared to the materials assessed in the NUREG database

[2, 3].

  • Loss of fracture toughness due to thermal embrittlement is driven by the amount of delta ferrite in a given material, thus the use of high delta ferrite material data is also conservative.
  • ANL results comparing loss of fracture toughness measurements on unaged, thermally aged only, irradiation aged only and sequentially thermally aged and irradiation aged CF-3 and CF-8 materials show significant loss of toughness on all forms of aging.

Measured toughnesses of thermally aged, irradiation aged and sequentially thermal plus irradiation aged materials are similar. Given the variances that are inherent in estimating J values as material characteristics, the differences in loss of toughness cited in Reference 4 cannot be taken to unequivocally demonstrate that irradiation and thermal aging are significantly additive effects to the loss of toughness in CF-3 and CF-8 cast austenitic stainless steels.

  • The data summarized in Figure 64 of NUREG-7027 includes many high ferrite content and Mo-containing chemical compositions. The correlations developed in analyses based on this database are therefore expected to be very conservative with regard to the irradiation and thermal response of low ferrite content and low Mo containing chemical compositions.

17

BWRVIP 2015-025 The NRC is concerned that interaction between thermal and irradiation embrittlement mechanisms may lower the fracture toughness of CASS material below levels expected from the effect of either mechanism alone. Based on the potential for a synergistic effect and taking into account the NUREG-7027 data, the NRC has concluded that a very low level of irradiation would reduce the fracture toughness of a CASS component below the 255 KJ/m 2 criteria.

This led to the NRC proposing a neutron irradiation screening criteria of 0.45 dpa for low molybdenum static CASS components with 15-20% delta ferrite. By reexamination of the data in NUREG-7027 a considerable amount of conservatism can be removed from the analysis while still providing reasonable assurance that CASS components in the LWR environment will retain adequate fracture toughness through the period of extended operations.

The irradiated materials data from NUREG-7027 were digitized from the plots of NUREG-7027 and reanalyzed to produce a trend curve for irradiated CF-3 and CF-8 materials only as shown in Figure 1 below. Note that the exposures of these materials not only represent irradiation effects but also some degree of thermal embrittlement. These data for CF-3 and CF-8 materials are most relevant to the behavior of CASS in LWR internals, as these are the materials that are principally known to be present in LWR reactor internals. Thus the correlation and proposed screening criteria are appropriately developed for these materials.

As an outcome of this analysis a plot of fracture toughness against neutron exposure was created, and a 'best fit' line was developed and the resulting curve was calculated to have a strong correlation with the data (R2=0.94). The best fit line was then modified using conservative engineering judgment and standard curve offsetting techniques to bound all of the irradiated CF-3 and CF-8 material measured toughness values. (i.e., the pre-exponential constant multiplier was reduced by approximately 25% and the exponential factor was increased by 35% in order to bound every data point above the red-line exponential curve fit.) A constant of 30 kJ/m 2 was also included as a saturated fracture toughness value.

This saturated fracture toughness value is proposed by Chopra in NUREG-7027, and the overall form of the equation is consistent with irradiation hardening models [6]. This results in a curve fit where all data points are above the curve, with resulting curve fit of:

KJ e_.25xdpa J2.Smm = 30 + 520 -- x e x This bounding line is shown as a red line in Figure 1.

By using the red (lower bound) line as a gauge for how CF-3 and CF-8 materials will age in the 2

LWR environment, it can be shown that these materials will not encroach upon the 255 KJ/m fracture toughness limit until the fluence level experienced by these components approaches 3.3 dpa. The industry proposed use of I dpa for neutron exposure screening criteria, provides more than a 2 dpa margin on neutron exposure between a CASS component at 1 dpa and the 255 18

BWRVIP 2015-025 KJ/m 2 fracture toughness limit. At 1 dpa, the fracture toughness predicted by the bounding curve in Figure 1 is 435 KJ/m 2 , which results in a fracture toughness margin of 180 KJ/m 2 .

Therefore, the industry's proposed criterion of 1 dpa has substantial margin in both the fluence and fracture toughness domains. This analysis and argument supports the use of the irradiation screening criteria of I dpa proposed by the industry for low molybdenum CASS components with ferrite content less than 20 percent.

Additionally, a study designed to investigate the potential interaction between thermal and irradiation embrittlement mechanisms concluded that irradiation can reduce the extent of thermal aging effects [5], suggesting an antergistic effect between the two mechanisms rather than a synergistic one.

This information indicates that the NRC's position is highly conservative, and that the industry's position on the screening criteria of CASS components, while also conservative, is justified.

References:

1. U.S. NRC, "NRC Staff Compiled Comments on Industry CASS Screening Position,"

July 18, 2014 (NRC ADAMS Accession Number ML14198A282.

2. NUREG/CR-7027, "Degradation of LWR Core Internal Materials due to Neutron Irradiation," December, 2010 (NRC ADAMS Accession Number ML102790482.
3. NUREG/CR-4513, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," U.S. Nuclear Regulatory Commission, August 1994 (NRC ADAMS Accession No. ML052360554).
4. ANL-12/56, "Crack Growth and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Argonne National Lab., November 2012.
5. K Fuji, K. Fukuya, "Effects of Radiation on Spinodal Decomposition of Ferrite in Duplex Stainless Steel," Journal of Nuclear Materials, May 2012. Presented at the NuMat 2012 Conference, pages 613 to 616, October 22-25, 2012, Osaka, Japan.
6. Was, Gary S., "Fundamentals of Radiation Materials Science: Metals and Alloys,"

Springer-Verlag, 2007.

7. Kim, C., R. Lott, S. Byrne, M. Burke, and G. Gerzen, "Embrittlement of Cast Austenitic Stainless Steel Reactor Internals Components," Proc. 6th Intl. Symp. On Contribution of Materials Investigations to Improve the Safety and Performance of LWRs, Fontevraud 6, French Nuclear Energy Society, SFEN, Fontevraud Roayal Abbey, France, September 18-22, 2006.

19

BWRVIP 2015-025 Figure 1 - Irradiated CF-3 and CF-8 Fracture Toughness Data from Literature (Refs. 2, 4 and 7)

Fracture Toughness of Irradiated CF3 and CF8 (0.02 dpa and greater) 1000 900 800 700 E 500

~400 300 200 100 0

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Neutron Exposure (dpa) 20

Attachment C Reactor Internals CASS Flaw Tolerance In the draft Interim Staff Guidance (ISG) on Aging Management of CASS Reactor Vessel Internal Components, issued in June 2014, the NRC technical position observed that "The fracture toughness screening. value of 255 kJ/m 2 specified in the Grimes Letter is based on a generic flaw tolerance evaluation for piping, and may be overly conservative for RVI CASS components that are subject to mainly compressive stresses during operation, and are part of a population of redundant components where failure of individual components can be tolerated."

The technical position went on to add that "therefore, the staff applies the 255 kJ/m 2 value for screening purposes with the knowledge that there likely is additional conservatism present in this screening for non-pressure boundary RVI components." In an effort to provide further evidence with respect to the NRC staff technical position, some industry efforts since the July 15, 2014 meeting with the NRC staff have been directed toward this issue. The results are summarized in the following paragraphs.

The industry selected three different geometries that can be related to typical BWR and PWR CASS reactor internals in order to estimate flaw tolerance capability: (1) a large-diameter cylinder with a through-wall vertical flaw located in a longitudinal seam weld, subjected to combined membrane and bending stress; (2) an edge-cracked beam-column subjected to combined membrane and bending stress; and (3) a six-inch-diameter, Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure. The internal pressure for the third geometry was selected such that the circumferential tensile stress in the pipe was identical to the membrane tensile stress level chosen for the first two geometries. In all three case studies, the initial flaw size (length for the first and third geometries, and depth for the second geometry) was selected to be consistent with reactor vessel internals fabrication workmanship standards. No flaw growth criteria were applied to the initial flaw sizes, although the initial flaw sizes were increased to some extent in order to determine the rate at which the crack driving force increased as a function of the increase in flaw size.

For the first geometry (large-diameter cylinder with through-wall vertical flaw), the diameter was selected to be 452 inches with a wall thickness of either one or two inches, the membrane tensile stress was selected to be 5 ksi, and the bending stress was selected to be 7.5 ksi. The total initial flaw length was selected to be 0.226 inches (about 1/4-inch in length), but was increased in increments up to 4.294 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. For the largest initial flaw lengths examined, the typical LEFM stress intensity is of the order of 25 ksiin, which converts to an elastic-plastic crack driving force of about 4 kJ/m 2 . This implies a very large margin relative to the screening value of 255 kJ/m2 .

For the second geometry (edge-cracked beam column), the solid column diameter was selected to be three inches, and the membrane and bending stresses were selected to be identical to those selected for the first geometry. The smallest initial flaw depth was selected as 0.1 inches, and was incremented by 0.1 inch up to a maximum depth of 1.7 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 lillview Avenue, Palo Alto, CA 94304-1395 USA

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BWRVIP 2015-025 J-crack driving forces. For the largest initial flaw depth examined (1.7 inches), the LEFM stress intensity was 42 ksiIin, which converts to an elastic-plastic crack driving force of about 10 kJ/m 2 . Again, this calculation implies a very large margin relative to the screening value of 255 kJ/m 2 .

For the third geometry (six-inch diameter Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure), the internal pressure was selected such that the circumferential stress was approximately 5 ksi, matching the membrane tensile stress used for the first and second geometries. Because of the thin pipe wall, this case was found to be the most critical of the three geometries. The initial flaw length was selected to be 0.1 inches, and was then incremented in 0.1-inch increments up to a maximum flaw length of 2.0 inches. For this case, the applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM),

and were then converted to J-crack driving forces. In addition, this case was also analyzed using elastic-plastic fracture mechanics, in order to compare derived crack-driving forces with directly calculated elastic-plastic crack-driving forces. For an initial flaw length of 2.0 inches, the LEFM stress intensity factor was about 54 ksi/in, which converts to a crack driving force of about 96 in-lb/in 2 or about 16 kJ/m 2. The directly-calculated elastic-plastic crack driving force is almost exactly the same, but very slightly lower. When the initial flaw length was doubled - to about 4.0 inches, the applied LEFM stress intensity was found to be 120 ksi/in, which converts to a crack driving force of about 476 in-lb/in 2 or about 83 kJ/m 2 . Even for this very severe example, the calculations show a sizable margin relative to the screening value of 255 kJ/m 2 .

From this exercise, CASS reactor internals components subjected to nominal stress levels, even in the presence of initial flaws that are well beyond fabrication workmanship acceptance criteria, are extremely flaw tolerant, with margins against flaw instability of the order of a factor of five to 10 relative to the fracture toughness screening criterion of 255 kJ/m 2 specified in the Grimes letter. When this flaw tolerance is coupled with the additional margin inherent in the separation of CF-3/CF-8 screening data from CF-8M screening data, the conservatism of the industry technical position is further confirmed.

22

BWRVIP 2015-025 Attachment D Tahlo I virarlld o/- larrto RPnonpe (Indivetru PnaifinnI 23

United States Nuclear Regulatory Commission Official Hearing Exhibit In the Matter of: Entergy Nuclear Operations, Inc. ENT000663 (Indian Point Nuclear Generating Units 2 and 3)

ASLBP #: 07-858-03-LR-BD01 Submitted: August 10, 2015 Docket #: 05000247 l 05000286 Exhibit #: ENT000663-00-BD01 Identified: 11/5/2015 Admitted: 11/5/2015 Withdrawn:

Rejected: Stricken:

Other:

2l1I ELECTRIC POWER L RESEARCH INSTITUTE

'e, 2015-025 BWR Vessel & Internals Project (BWRVIP)

March 09, 2015 Document Control Desk U.S. Nuclear Regulatory Commission 11555 Rockville Pike Rockville, MD 20852 Attention: Joseph Holonich

Subject:

Project No. 704 - Summary of Industry Position on Screening Criteria for Thermal and Irradiation Embrittlement for PWR and BWR Reactor Internals Fabricated of Cast Austenitic Stainless Steel

References:

1. Letter from D. Madison (BWRVIP Chairman) and A. McGehee (BWRVIP Program Manager) to J. Holonich (NRC), Project No. 704 - BWRVIP Response to NRC Request for Additional Information on BWRVIP-234, dated May 23, 2014. ADAMS - ML14174A841.
2. Letter from J. Holonich (NRC) to A. Mendiola (NRC), Summary of the July 15, 2014, Meeting with the Electric Power Research Institute on Items Related to Cast Austenitic Stainless Steel and the Materials Reliability Program-227-A, "Pressurized Water Reactor Internals Inspection And Evaluation Guidelines,"

September 9, 2014. ADAMS - ML14127A077.

3. "NRC Position on Aging Management of CASS Reactor Vessel Internal Components," June 23, 2014, ADAMS - ML14174A719.
4. Email from C. Wirtz (EPRI) to J. Holonich (NRC), October 7, 2014.
5. NUREG/CR-4513, ANL-93/22, Revision 1, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," Argonne National Laboratory, May 1994.

The purpose of this letter is to provide the status of the Industry (PWR and BWR) activities associated with developing and proposing a generic screening criteria to address thermal and irradiation embrittlement of RPV internals fabricated of cast austenitic stainless steel (CASS).

Reference I was provided to the NRC in response to a Request for Additional Information (RAI) regarding BWRVIP-234. The RAI response contained supplemental information that provided the technical bases for an Industry screening criteria for CASS internals.

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BWRVIP 2015-025 A meeting was later held on July 15, 2014 at NRC offices in Washington, DC to discuss the Industry and NRC positions (References 2, 3). Based on that meeting, the Industry committed to investigate additional information where there was disagreement with the NRC regarding the screening criteria and provide said information to the NRC at a later date. That information was informally submitted for NRC's consideration (Reference 4) and is contained in Attachments A through D of this letter. A conference call was then held on November 20, 2014 with the NRC to discuss this information.

Following this conference call the NRC indicated that they were not willing to deviate from their position documented in Reference 3.

Despite the NRC's current stance on the matter, the following comments regarding a generic TE and IE criteria for evaluation of reactor internals are important in forming the basis for the industry position:

" The industry recognizes that the NRC is intending to revise its original IE position in the Grimes letter from lxl10 7 n/cm 2 (0.00014 dpa) to a position in the region of 0.5 to 1.5 dpa. Industry agrees that this position is more appropriate and has proposed a conservative value of 1 dpa.

  • It is not appropriate (for the staff) to penalize all non-Mo containing CASS (such as CF3 and CF8) because of the lower properties associated with the Mo-containing CF8M materials that are included in the ANL/NRC database, i.e., impose a lower bound.
  • There is no substantive data that demonstrates a synergistic effect for CASS materials that are typical of reactor internals (such as CF3 and CF8). As such the industry has proposed criteria that do not combine TE and IE. Each mechanism is considered distinct and separate.

" The introduction of a new criteria set for the category of materials with ferrite content between 15% to 20% having a lower proposed screening value for IE of 0.45 dpa is unnecessary and technically unfounded. The introduction of this category of ferrite content is significantly burdensome to licensees since it will require more complex and potentially more error-prone assessments of CASS material components by virtue of having more categories. Industry maintains that the categories of materials and associated ferrite levels contained in the Grimes letter are appropriate.

" The criteria proposed by the industry (20% Ferrite and 1 dpa) have been shown to project significant margin on toughness reduction and therefore safety when compared to measured embrittlement behavior for CF3 and CF8 materials.

Regardless, this letter serves to formally submit this additional information to the NRC for review and consideration in developing a regulatory position for the screening criteria associated with TE and IE for CASS internals and to inform revisions to NUREG-4513, Rev. 1 (Reference 5). The PWR and BWR Industry position for TE and IE screening criteria is shown in Attachment D.

2

BWRVIP 2015-025 Irrespective of the staff's decision and future promulgation of a regulatory position on TE and IE for CASS internals, the BWRVIP formally requests the NRC to evaluate and resolve the RAI responses associated with BWRVIP-234 and issue a Safety Evaluation.

If you have any questions on this subject please call Ron DiSabatino (Exelon, BWRVIP Assessment Committee Technical Chairman) at 717.456.3685.

Sincerely, 24 Andrew McGehee, EPRI, BWRVIP Program Manager Tim Hanley, Exelon Corp., BWRVIP Chairman 3

BWRVIP 2015-025 Industry Response to July 15, 2014 Meeting with NRC on CASS On July 15, 2014, representatives from the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS) met with the NRC staff to discuss the thermal and irradiation embrittlement screening criteria for cast austenitic stainless steel. While the working group and NRC staff were in general agreement on the thermal embrittlement (TE) screening criteria, there was a marked difference of opinion on the irradiation embrittlement (IE) screening criteria, particularly for materials with delta ferrite contents of 15-20% (the NRC proposed 0.45 dpa, while the industry proposed 1 dpa).

Agreement was reached on the TE screening criteria in part because the data on low-molybdenum and high-molybdenum material are considered separately, resulting in separate TE screening criteria for these materials. This distinction is made because high-molybdenum materials show a distinctly greater loss of fracture toughness from TE and IE effects than low-molybdenum materials. This is reviewed and discussed further in Attachment A The separate consideration of low- and high-molybdenum materials test data was not carried over into the IE domain. The data set used to determine the NRC's position on IE was obtained from NUREG-7027, which considered irradiated high- and low-molybdenum materials together, along with data on irradiated welds. Because these materials were considered together, the resulting lower bound curve is judged to be overly conservative relative to the low-molybdenum material. A reexamination of this data (see Attachment B), shows that by considering the low-molybdenum materials test data independently of the other materials it can be concluded that there is a substantial safety margin in the industry's proposed I dpa screening criteria.

These screening criteria are being implemented to ensure that CASS components in reactor vessel internals maintain adequate fracture toughness during the period of extended operation.

The screening level to determine whether this requirement was met was a J value of 255 KJ/m2 at a crack extension of 2.5 mm. This value was originally determined for pressure boundary components (i.e., large diameter piping, etc.) and was expected to be highly conservative for application to reactor vessel internals. Additional calculations (see Attachment C) demonstrate the level of this conservatism and show that reactor vessel internal components can safely operate with fracture toughness values much lower than the 255 KJ/m 2 value specified in the Grimes letter.

In summary, the actions taken by the CASS industry working group and summarized in Attachments A, B and C support the proposed screening criteria contained in Attachment D.

These criteria provide a significant amount of margin for screening of TE and IE. It is concluded that that the use of the proposed screening criteria will allow for continued safe and reliable operation of the LWR fleet.

4

BWRVIP 2015-025 Attachment A Discussion on Low Molybdenum vs High Molybdenum CASS Grades Introduction A meeting was held on July 15, 2014 at the NRC Office in Washington, DC between the staff of the U.S. Nuclear Regulatory Commission (NRC) and the BWRVIP/MRP Working Group on Cast Austenitic Stainless Steels (CASS). The topic of discussion focused on the thermal aging and neutron irradiation embrittlement screening criteria (separately) proposed by the industry and the NRC staff. The proposals included criteria for low-molybdenum CASS grades, such as CF-3 and CF-8, and high-molybdenum CASS grades, such as CF-8M. There was agreement between industry and the NRC staff regarding the differences in such measures of embrittlement as elastic-plastic crack growth resistance (J-R curve) for the low-Mo materials versus the high-Mo materials, at least where thermal aging embrittlement effects are dominant. In fact, screening criteria proposed by the staff are identical to the industry-proposed screening criteria for the case of thermal aging embrittlement.

However, the areas of agreement between the industry and the staff did not carry over to combined environments where the effects of neutron irradiation embrittlement begin to approach the same level as those from thermal aging embrittlement. In order to address these differences in criteria, the available data for CF-3, CF-8, and CF-8M materials in the literature are reviewed and assessed, with a recommendation to the NRC staff for a change to their proposed criteria to more closely agree with the criteria proposed by the industry.

Review and Summary of Thermal Aging Embrittlement Data The significant differences in thermal aging embrittlement behavior of the low-molybdenum grades of cast austenitic stainless steel, such as CF-3 and CF-8, versus the thermal aging embrittlement behavior of the high-molybdenum grades, such as CF-8M, have been known for at least two decades, with extensive data and associated interpretations of said data documented in NUREG/CR-4513, Revision 1 [1]. The lower-bound thermal aging embrittlement estimates shown in Figures 3 (statically-cast steels) and 4 (centrifugally-cast steels) from Reference 1 with varying amounts of delta ferrite provide an excellent illustration of those significant differences, in this case with the measure of significance being the crack-growth resistance J-R curve. In particular, the lower-bound formulas cited in Section 3.1.1 of Reference 1 (and plotted in Figures 3 and 4) can be used to compare the estimated crack growth resistance values at 2.5 mm of crack extension for the CF-3, CF-8, and CF-8M steels with > 15% delta ferrite. Note that Figure 3 provides lower-bound thermal aging estimates for static-cast steels, while Figure 4 provides lower-bound thermal aging estimates for centrifugally-cast steels.

5

BWRVIP 2015-025 Crack Extension ha (in.) Crack Extension As (in.)

0.00 0.06 0.10 0.15 Lower-Bound J-R Curve Static-Camt Stes I

5.

>15% Fentbe

-290"C -4000

-3 0 J =2510Aa)

- 2 03- -3000 -

17&O

- J=M4a -2000f o

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0 1 2 3 4 0 2 3 4 S 0.00 0.06 0.10 0.15 0.00 0.06 0.10 0.15

  • I I , 'I , : : : ji , ' , :

lOOO Lower-Bound J-R Curve Lower-Bound J-IR Static-Cat Steels Static-Cast StaWsi aS 80o. l-15%Fenml 10-16% Fegrkt Room Temp. J - 274"0.3 .4000 36 j- 2740sa)03 2001&a)o cF-4 ..

800- 1 - 31(1P40 I

CF035 -3000

  • 400 j =3074Uo-38 I CF-C 400 J 130-~036 200- - CF-SM 32 10

- :j - .: '. I:

CF-Ui CFS .0 0 1 2 3 4 5 0 1 2 3 4 5 0.00 0.06 0.10 0.1( 0.00 0.06 0.10 0.15 5000" 5.

if 4000~

-3 3000 I

Ia 2000j 1000i 0

1 2 3 4 Crack Extension, Aa (mm)

Figure3. Predictedlower-bound J-R curves at RT and 290°C for static-castSSs with ferrite contents >15, 10-15. or<10%

6

BWRVIP 2015-025 Crack Extension As (in.) Crack Extension ha (in.)

0.o00. O. .O 0.1s 0.00 O.06 0.10 0.15 Lower-Bound J-R Curve Lower-Bound J-R Curve Centrifugally Cast Steels Centrifugally Cast Steels

>15% Fmist 0 37 >15%FaFnite Room Tnp. J - 304SO) . M-0C J.-3301AP,34 -4000 7 0 35 J.934r*a) " CF-s JF3348 39C- CF-S C!

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~2007 -1000 CF-Sm

.. .. . . . . H i F 0 I 1 2 3 4 0 1 2 3 4 1 0.00 0.06 010 0.15 0.00 0.0S 0.10 0.15 i

r-Bound J-R Curve Lower-Bound J-R Curve C a " olyCast Steels Centrifugally Cast Steels 4SO0OI 10-15% Forte0 -4000.

)0- 2fOC J - 300ma)°35 I 04 0-36 CF-S J.30sWKa i CJ- 38M&).3 X0- CF-3 CF-3 3000

-. * '* *. 357ý,,)°

-2000 I

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0 1 2 3 S4 1 2 3 4 5 0O30 0.06 0.10 0.15 0.00 0.0 0.10 0.15 1000 Lower-Bound J-R Curve Lower-ilound' J-'R C'urv'e' . Lower-Bound J-R Curve Centrifugaly Cast SteDes Centrifugally Cast Steels .5000 410% Fernite - 4OO"

<10% F-f-n¶ Room TSm 07 2*0T P41 J -435(Aa~5 I:

-3000 -2 CF--3 CF-8 4001

-20001 200 - CF-SM CF-Sm .1000 a

0 1 2 3 4 5 0 2 3 4 Crack Extension., A (mm) Crack Extension, A (mm)

Figure 4. Predictedlower-bound J-R curves at RT and 290'C for centrifugally cast SSs with ferrite contents > 15. 10-15. or < 10%

7

BWRVIP 2015-025 For CF-3, the lower bound crack growth resistance, for statically- and centrifugally-cast materials, varies between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 Id/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2. When the data are examined very closely, there is no significant difference between the static-cast lower-bound estimates for CF-3 and CF-8 in Figure 3 and the centrifugally-cast lower-bound estimates for CF-3 and CF-8 in Figure 4. The data also show that these insignificant differences are roughly identical to the differences between CF-3 and CF-8 estimates within the static-cast and centrifugally-cast populations. Therefore, based on this examination of lower-bound estimates, the CF-8M data exhibit substantially lower fracture toughnesses and are therefore unsuitable as a lower-bound estimate for the low-molybdenum grades. Lower bound estimates must be conservative, but they must also remain representative of the data. Table 1, shown below, succinctly summarizes the data comparisons extracted from Figures 3 and 4 from Reference 1.

Table 1. Lower Bound Fracture Toughness Estimates CASS Steels J-values at 2.5 cm of2 Crack Comments Growth (kJ/m )

Lower bound above the threshold 2

CF-3 Steels 364 to 478 value of 255 kJ/M Lower bound above the threshold 2

CF-8 Steels 343 to 451 value of 255 kj/m CF-8M Steels 161 to 259 Lower bound might be less than2 threshold values of 255 kJ/m Table 1 clearly shows that lower bound fracture toughness values of CF-3 and CF-8 steels are much higher than CF-8M steels, and that only the fracture toughness of CF-8M steels fall below the threshold value of 255 kJ/m 2. Therefore, the screening criteria for CF-8M (high molybdenum) steels should be considered separately from CF-3 and CF-8 (low molybdenum) steels.

Thus far, the data evaluation has been based on lower-bound fracture toughness estimates derived from Charpy impact correlations. However, these lower-bound thermal aging embrittlement estimates can be confirmed by examining actual crack extension resistance curve measurements for various heats of CF-3, CF-8, and CF-8M with delta ferrite content in the range of 20%. For example, Figure 14 from Reference 1 shows J-R curve measurements, along with thermal aging saturation estimates for two heats of CF-3 material (Heat 69 and Heat I) and one heat of CF-8 material (Heat 68), while Figure 15 from Reference 1 shows similar results for three heats of CF-8M material (Heats 74, 75, and 758).

In this case, it should be noted that the actual fracture toughness data are based on thermal aging saturation conditions and are therefore somewhat higher than the lower-bound fracture toughness 8

BWRVIP 2015-025 estimates. Also note that the thermal aging saturation fracture toughness data are based entirely on static-cast data for materials with delta ferrite in the range of 15% to 25%.

The crack extension resistance value at 2.5 mm of crack extension for the thermal aging saturation conditions for CF-3 and CF-8 materials ranges between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material are less than half of the low-molybdenum material values.

Therefore, the findings from the examination of the data in Figures 14 and 15, and the derived J values at 2.5 mm of crack extension, are completely consistent with the lower-bound thermal aging embrittlement estimates cited previously for both static-cast and centrifugally-cast material. In other words, the development of screening criteria for the low-molybdenum grades should be treated separately from the development of screening criteria for the high-molybdenum grades.

9

BWRVIP 2015-025 Crack Extension, An (in.) Crack Extension, An (in.)

0.0 0.1 0.2 0.3 0.0 I . 0.1 0.2 0.3 2WC Heat 69 ~CF-3 290"C -

C' 8,-21%

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0~

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00 0 0000 0

-- 0 0ý0

-6000 0 .2g0Ag iIi I

  • I U 2 4 6 8 10 Crack Extension, As (mm) Crack Extension, A& (Mm)

Figure 14. Saturationfracture toughness J-R curves at RT and 290Co, estimatedfrom the chemical composition of static-cast CF-3 and CF-8 steels, and determined experimentally 10

BWRVIP 2015-025 Crack Extension, ha (in.) Crack Extension, ha (in.)

0.0 0.1 0.2 0.3 0.01 , . I , I 0.1I . I .

0.2 I I . I . 0.3 i.

Heal Hiai is75 'C",

CF-SM ' Ro Room Temp. ep Stall-Caa Slab -15000 C Sc

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37

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)o 42 -15000 £ 492000- 0 =A000ht 0C 03 7 324Olp 32 efpy J 30(sa)

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s 0 0 0. 4 0 6 10 0.0 0.1 0.2 0.3 0.0 0.1 0.2 0.3 Hieat 7'581 6F4 R Temp. Heat 758 CF-SM 290'C SONO-C*M Etow SUMc-CaN Elbow [ 16000 SC-21%Unap 2000-

-10000 I 32 apy 32 4P 0

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1000. &I290C at 30*C

-5000 WAOA£ kj MA AL ';'>eso J/ 2(a03 4-?>(V 3,3 O*P 0 2 4 6 8 10 0 10 Crack Extension, Aa (mm) Crack Extension, Aa (mm)

Figure 15. Saturationfracture toughness J-R curves at RT and 290*C. estimated from die chemical composition of static-castCF-SM steels, and determined experimentally 11

BWRVIP 2015-025 Review and Summary of Combined TE and IE Data The available data for purely thermally-embrittled CASS materials is quite extensive. However, that is not the case for a combination of thermal aging and neutron irradiation embrittlement. In spite of the limited data, the evaluation of available crack growth resistance data for CF-3, CF-8, and CF-8M material is not altered by including information on material subjected to both thermal aging and neutron irradiation embrittlement, as shown in Figures 23, 41, 49, and 58 from ANL-12/56 [2]. The results for Specimen B-1 (static-cast CF-3 material taken from Heat 69, with approximately 24% delta ferrite, thermally aged for 10,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> at 400'C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 23 - taken from Reference 2. The extrapolated J value at 2.5 mm of crack extension is 789 kJ/m 2, very similar to the saturated, thermally-aged result, as shown in Figure 14 for Heat 69 from Reference 1.

640 480 1-1 320

-74 160 0.5 1.0 1. 2.0 Crack Extension (mm)

Figure 23. The J-R curve for specimen B-1.

Similarly, the results for Specimen F-1 (static-cast CF-8 material taken from Heat 68, with approximately 23% delta ferrite, thermally aged for 10,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> at 400'C and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figure 41 - also taken from Reference 2.

The extrapolated J value at 2.5 mm of crack extension is 657 kJ/m 2 , very similar to the saturated, thermally-aged result, as shown in Figure 14 from Reference 1 for Heat 68.

12

BWRVIP 2015-025 640 . . . .

Specimen F-1 CF-8, aged, 0.08 dpa 480 Low-DO high-purity water, 3200CI A 62 J=1 372"Aao.

E 320 V, I 160 AI max 0

0.0 0.5 1.0 1.5 2.0 Crack Extension (mm)

Figure 41. The J-R curve of specimen F-i.

Finally, the results for Specimens I-1 (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, unaged but subjected to a neutron irradiation dose of 0.08 dpa) and J-1I (CF-8M material taken from Heat 75, with approximately 28% delta ferrite, thermally aged for 10,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> at 4001C, and then subjected to a neutron irradiation dose of 0.08 dpa) are shown in Figures 49 and 58 - also taken from Reference 2. In this case the extrapolated J value at 2.5 mm of crack extension for Specimen J-1 is 466 k/m , which can be compared to the results shown in Figure 15 from Reference forI Heat 75 that appear to be of the order of 300 to 400 kJ/m 2 at room temperature and operating temperature.

13

BWR VIP 2015-025 640 .. . I .I . . . . .

Specimen I-1 CF-8M, unaged, 0.0 -

dna

~5~~

Low-DO high-purity water, 320PC .

480 I

I mJ= J7 I

cm 336-Aa I

320 max I' 160 IAamax 2

=145 kJ/m I

n I 0 0.5 1.0 1.5 2.0 Crack Extension (mm)

Figure 49. The JR curve of specimen I-1.

640 480 (N-320 160 2.0 Crack Extension (mm)

Figure 58. The JR curve of specimen J-1.

14

BWRVIP 2015-025 Conclusions and Recommendation This review and summary of available data on CF-3, CF-8, and CF-8M CASS materials subjected to both individual and combined effects of thermal aging and neutron irradiation embrittlement demonstrated that:

Thermal aging embrittlement effects on high-Mo grades are significantly more pronounced than the effects on the low-Mo grades, by roughly a factor of two or more based upon lower-bound crack growth resistance estimates. For CF-3, the lower-bound crack growth resistance values at 2.5 mm of crack extension for > 15% delta ferrite vary between 364 and 478 kJ/m 2 , and for CF-8, between 343 and 451 kJ/m 2 . On the other hand, the CF-8M values vary between 161 and 259 kJ/m 2 which are significantly lower compared to CF-3/8. These results are consistent with the results obtained by examining actual crack growth resistance value measurements at 2.5 mm of crack extension for the thermal aging to saturation for CF-3 and CF-8 materials (low-Mo) that range between 681 and 820 kJ/m 2 at room temperature, with values between 516 and 584 kJ/m 2 at operating temperature, while the values for CF-8M material (high-Mo) are less than half of the low-molybdenum material values.

  • There is no significant difference between the static-cast lower-bound estimates and the centrifugally-cast lower-bound estimate for CF-3 and CF-8 materials, and those relatively small differences are roughly identical to differences between CF-3 and CF-8 lower-bound estimates. Using lower-bound crack growth resistance values at 2.5 mm of crack 2

extension as the comparative measure, the CF-3 static-cast values of 364 and 410 kJ/m compare very well to the 477 and 478 kJ/m 2 values for centrifugally-cast material, while the CF-8 static-cast values of 343 and 366 kJ/m 2 compare favorably with the 427 and 451 kJ/m 2 values for centrifugally-cast material. The differences between static-cast and centrifugally-cast values, and between CF-3 and CF-8 values are both inconsequential in comparison to the differences between low-Mo and high-Mo materials. Therefore these two grades may be considered as a combined category for screening purposes.

  • The added effect of neutron irradiation embrittlement does not change the conclusions drawn with respect to low-Mo versus high-Mo fracture toughness. Finally, since the conclusions are drawn primarily from static-cast fracture toughness data, a recommendation to the NRC staff to maintain the screening threshold for low-Mo static-cast grades at 20% is supported by the data.

Therefore, this review shows that the CF-8M data provide an extremely conservative and thus unrepresentative lower bound to the data for the low-molybdenum grades. As such, the CF-8M lower bound is separable and distinct from the low-molybdenum grade lower bounds, which therefore require their own screening category and fracture toughness estimates. Thus, the delta ferrite levels stated in the BWRVIP-234 RAI response (from the Grimes letter) is further supported by this evaluation.

Finally, this review and the associated quantitative comparisons utilize the data sets as delineated in extensive documentation in NUREG/CR-4513, Revision 1 [1] and other relevant publically available references.

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BWRVIP 2015-025 References

[1]. 0. K. Chopra, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," NUREG/CR-4513 (ANL-93/22), Revision 1, Argonne National Laboratory, Argonne, Illinois (August 1994).

[2]. Y. Chen, B. Alexandreanu, and K. Natesan, "Crack Growth Rate and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Report No. ANL-12/56, Argonne National Laboartory, Argonne, Illinois (November 2012).

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BWRVIP 2015-025 Attachment B Conclusions Regarding Screening Criteria for Irradiation Embrittlement of CASS Materials The screening criteria for TE and IE in CASS components proposed and discussed with the NRC

[1] appears to be based on materials testing data that includes a high-molybdenum material, grade CF-8M, presented in Figure 64 in NUREG 7027 [2], with the following conclusions on page 79:

1. CF-8M materials represent a 'worst case' for thermal embrittlement
2. Thermal aging does not seem to lower the toughness below that expected for irradiation alone at the dose levels examined.

In regards to the use of this data, it is important to note that:

  • CF-8M materials are not present in LWR core internal components.
  • Moreover, the embrittlement identified in NUREG-7027 is conservative because many of the heats examined had delta ferrite contents greater than 20% and as high as 42% [3].

It is also important to emphasize that in LWR reactor internals, delta ferrite content does not typically exceed 20% as compared to the materials assessed in the NUREG database

[2, 3].

  • Loss of fracture toughness due to thermal embrittlement is driven by the amount of delta ferrite in a given material, thus the use of high delta ferrite material data is also conservative.
  • ANL results comparing loss of fracture toughness measurements on unaged, thermally aged only, irradiation aged only and sequentially thermally aged and irradiation aged CF-3 and CF-8 materials show significant loss of toughness on all forms of aging.

Measured toughnesses of thermally aged, irradiation aged and sequentially thermal plus irradiation aged materials are similar. Given the variances that are inherent in estimating J values as material characteristics, the differences in loss of toughness cited in Reference 4 cannot be taken to unequivocally demonstrate that irradiation and thermal aging are significantly additive effects to the loss of toughness in CF-3 and CF-8 cast austenitic stainless steels.

  • The data summarized in Figure 64 of NUREG-7027 includes many high ferrite content and Mo-containing chemical compositions. The correlations developed in analyses based on this database are therefore expected to be very conservative with regard to the irradiation and thermal response of low ferrite content and low Mo containing chemical compositions.

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BWRVIP 2015-025 The NRC is concerned that interaction between thermal and irradiation embrittlement mechanisms may lower the fracture toughness of CASS material below levels expected from the effect of either mechanism alone. Based on the potential for a synergistic effect and taking into account the NUREG-7027 data, the NRC has concluded that a very low level of irradiation would reduce the fracture toughness of a CASS component below the 255 KJ/m 2 criteria.

This led to the NRC proposing a neutron irradiation screening criteria of 0.45 dpa for low molybdenum static CASS components with 15-20% delta ferrite. By reexamination of the data in NUREG-7027 a considerable amount of conservatism can be removed from the analysis while still providing reasonable assurance that CASS components in the LWR environment will retain adequate fracture toughness through the period of extended operations.

The irradiated materials data from NUREG-7027 were digitized from the plots of NUREG-7027 and reanalyzed to produce a trend curve for irradiated CF-3 and CF-8 materials only as shown in Figure 1 below. Note that the exposures of these materials not only represent irradiation effects but also some degree of thermal embrittlement. These data for CF-3 and CF-8 materials are most relevant to the behavior of CASS in LWR internals, as these are the materials that are principally known to be present in LWR reactor internals. Thus the correlation and proposed screening criteria are appropriately developed for these materials.

As an outcome of this analysis a plot of fracture toughness against neutron exposure was created, and a 'best fit' line was developed and the resulting curve was calculated to have a strong correlation with the data (R2=0.94). The best fit line was then modified using conservative engineering judgment and standard curve offsetting techniques to bound all of the irradiated CF-3 and CF-8 material measured toughness values. (i.e., the pre-exponential constant multiplier was reduced by approximately 25% and the exponential factor was increased by 35% in order to bound every data point above the red-line exponential curve fit.) A constant of 30 kJ/m 2 was also included as a saturated fracture toughness value.

This saturated fracture toughness value is proposed by Chopra in NUREG-7027, and the overall form of the equation is consistent with irradiation hardening models [6]. This results in a curve fit where all data points are above the curve, with resulting curve fit of:

KJ e_.25xdpa J2.Smm = 30 + 520 -- x e x This bounding line is shown as a red line in Figure 1.

By using the red (lower bound) line as a gauge for how CF-3 and CF-8 materials will age in the 2

LWR environment, it can be shown that these materials will not encroach upon the 255 KJ/m fracture toughness limit until the fluence level experienced by these components approaches 3.3 dpa. The industry proposed use of I dpa for neutron exposure screening criteria, provides more than a 2 dpa margin on neutron exposure between a CASS component at 1 dpa and the 255 18

BWRVIP 2015-025 KJ/m 2 fracture toughness limit. At 1 dpa, the fracture toughness predicted by the bounding curve in Figure 1 is 435 KJ/m 2 , which results in a fracture toughness margin of 180 KJ/m 2 .

Therefore, the industry's proposed criterion of 1 dpa has substantial margin in both the fluence and fracture toughness domains. This analysis and argument supports the use of the irradiation screening criteria of I dpa proposed by the industry for low molybdenum CASS components with ferrite content less than 20 percent.

Additionally, a study designed to investigate the potential interaction between thermal and irradiation embrittlement mechanisms concluded that irradiation can reduce the extent of thermal aging effects [5], suggesting an antergistic effect between the two mechanisms rather than a synergistic one.

This information indicates that the NRC's position is highly conservative, and that the industry's position on the screening criteria of CASS components, while also conservative, is justified.

References:

1. U.S. NRC, "NRC Staff Compiled Comments on Industry CASS Screening Position,"

July 18, 2014 (NRC ADAMS Accession Number ML14198A282.

2. NUREG/CR-7027, "Degradation of LWR Core Internal Materials due to Neutron Irradiation," December, 2010 (NRC ADAMS Accession Number ML102790482.
3. NUREG/CR-4513, "Estimation of Fracture Toughness of Cast Stainless Steels During Thermal Aging in LWR Systems," U.S. Nuclear Regulatory Commission, August 1994 (NRC ADAMS Accession No. ML052360554).
4. ANL-12/56, "Crack Growth and Fracture Toughness Tests on Irradiated Cast Stainless Steels," Argonne National Lab., November 2012.
5. K Fuji, K. Fukuya, "Effects of Radiation on Spinodal Decomposition of Ferrite in Duplex Stainless Steel," Journal of Nuclear Materials, May 2012. Presented at the NuMat 2012 Conference, pages 613 to 616, October 22-25, 2012, Osaka, Japan.
6. Was, Gary S., "Fundamentals of Radiation Materials Science: Metals and Alloys,"

Springer-Verlag, 2007.

7. Kim, C., R. Lott, S. Byrne, M. Burke, and G. Gerzen, "Embrittlement of Cast Austenitic Stainless Steel Reactor Internals Components," Proc. 6th Intl. Symp. On Contribution of Materials Investigations to Improve the Safety and Performance of LWRs, Fontevraud 6, French Nuclear Energy Society, SFEN, Fontevraud Roayal Abbey, France, September 18-22, 2006.

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BWRVIP 2015-025 Figure 1 - Irradiated CF-3 and CF-8 Fracture Toughness Data from Literature (Refs. 2, 4 and 7)

Fracture Toughness of Irradiated CF3 and CF8 (0.02 dpa and greater) 1000 900 800 700 E 500

~400 300 200 100 0

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Neutron Exposure (dpa) 20

Attachment C Reactor Internals CASS Flaw Tolerance In the draft Interim Staff Guidance (ISG) on Aging Management of CASS Reactor Vessel Internal Components, issued in June 2014, the NRC technical position observed that "The fracture toughness screening. value of 255 kJ/m 2 specified in the Grimes Letter is based on a generic flaw tolerance evaluation for piping, and may be overly conservative for RVI CASS components that are subject to mainly compressive stresses during operation, and are part of a population of redundant components where failure of individual components can be tolerated."

The technical position went on to add that "therefore, the staff applies the 255 kJ/m 2 value for screening purposes with the knowledge that there likely is additional conservatism present in this screening for non-pressure boundary RVI components." In an effort to provide further evidence with respect to the NRC staff technical position, some industry efforts since the July 15, 2014 meeting with the NRC staff have been directed toward this issue. The results are summarized in the following paragraphs.

The industry selected three different geometries that can be related to typical BWR and PWR CASS reactor internals in order to estimate flaw tolerance capability: (1) a large-diameter cylinder with a through-wall vertical flaw located in a longitudinal seam weld, subjected to combined membrane and bending stress; (2) an edge-cracked beam-column subjected to combined membrane and bending stress; and (3) a six-inch-diameter, Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure. The internal pressure for the third geometry was selected such that the circumferential tensile stress in the pipe was identical to the membrane tensile stress level chosen for the first two geometries. In all three case studies, the initial flaw size (length for the first and third geometries, and depth for the second geometry) was selected to be consistent with reactor vessel internals fabrication workmanship standards. No flaw growth criteria were applied to the initial flaw sizes, although the initial flaw sizes were increased to some extent in order to determine the rate at which the crack driving force increased as a function of the increase in flaw size.

For the first geometry (large-diameter cylinder with through-wall vertical flaw), the diameter was selected to be 452 inches with a wall thickness of either one or two inches, the membrane tensile stress was selected to be 5 ksi, and the bending stress was selected to be 7.5 ksi. The total initial flaw length was selected to be 0.226 inches (about 1/4-inch in length), but was increased in increments up to 4.294 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to J-crack driving forces. For the largest initial flaw lengths examined, the typical LEFM stress intensity is of the order of 25 ksiin, which converts to an elastic-plastic crack driving force of about 4 kJ/m 2 . This implies a very large margin relative to the screening value of 255 kJ/m2 .

For the second geometry (edge-cracked beam column), the solid column diameter was selected to be three inches, and the membrane and bending stresses were selected to be identical to those selected for the first geometry. The smallest initial flaw depth was selected as 0.1 inches, and was incremented by 0.1 inch up to a maximum depth of 1.7 inches. The applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM), and were then converted to Together ... Shaping the Future of Electricity PALO ALTO OFFICE 3420 lillview Avenue, Palo Alto, CA 94304-1395 USA

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BWRVIP 2015-025 J-crack driving forces. For the largest initial flaw depth examined (1.7 inches), the LEFM stress intensity was 42 ksiIin, which converts to an elastic-plastic crack driving force of about 10 kJ/m 2 . Again, this calculation implies a very large margin relative to the screening value of 255 kJ/m 2 .

For the third geometry (six-inch diameter Schedule 40 pipe with a through-wall longitudinal flaw subjected to internal pressure), the internal pressure was selected such that the circumferential stress was approximately 5 ksi, matching the membrane tensile stress used for the first and second geometries. Because of the thin pipe wall, this case was found to be the most critical of the three geometries. The initial flaw length was selected to be 0.1 inches, and was then incremented in 0.1-inch increments up to a maximum flaw length of 2.0 inches. For this case, the applied stress intensity factors were found using linear-elastic fracture mechanics (LEFM),

and were then converted to J-crack driving forces. In addition, this case was also analyzed using elastic-plastic fracture mechanics, in order to compare derived crack-driving forces with directly calculated elastic-plastic crack-driving forces. For an initial flaw length of 2.0 inches, the LEFM stress intensity factor was about 54 ksi/in, which converts to a crack driving force of about 96 in-lb/in 2 or about 16 kJ/m 2. The directly-calculated elastic-plastic crack driving force is almost exactly the same, but very slightly lower. When the initial flaw length was doubled - to about 4.0 inches, the applied LEFM stress intensity was found to be 120 ksi/in, which converts to a crack driving force of about 476 in-lb/in 2 or about 83 kJ/m 2 . Even for this very severe example, the calculations show a sizable margin relative to the screening value of 255 kJ/m 2 .

From this exercise, CASS reactor internals components subjected to nominal stress levels, even in the presence of initial flaws that are well beyond fabrication workmanship acceptance criteria, are extremely flaw tolerant, with margins against flaw instability of the order of a factor of five to 10 relative to the fracture toughness screening criterion of 255 kJ/m 2 specified in the Grimes letter. When this flaw tolerance is coupled with the additional margin inherent in the separation of CF-3/CF-8 screening data from CF-8M screening data, the conservatism of the industry technical position is further confirmed.

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BWRVIP 2015-025 Attachment D Tahlo I virarlld o/- larrto RPnonpe (Indivetru PnaifinnI 23