ML18134A205

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Enclosurequest for Supplemental Information (Letter to R. Ngwayah Request for Supplemental Information for the Review of the Model No. HI-STAR 100MB Package)
ML18134A205
Person / Time
Site: 07109378
Issue date: 05/11/2018
From: Pierre Saverot
Spent Fuel Licensing Branch
To: Ngwayah R
Holtec
Saverot P
Shared Package
ML18134A204 List:
References
EPID L-2018-NEW-0000
Download: ML18134A205 (6)


Text

Request for Supplemental Information Holtec International Docket No. 71-9378 Model No. HI-STAR 100MB Package By letter dated February 16, 2018, Holtec International (Holtec) submitted an application for Certificate of Compliance No. 9378, Revision No. 0, for the Model No. HI-STAR 100MB package.

This request for supplemental information (RSI) identifies information needed by the U.S.

Nuclear Regulatory Commission staff (the staff) in connection with its acceptance review of the Model No. HI-STAR 100MB package application to confirm whether the applicant has submitted a complete application in compliance with regulatory requirements.

The requested information is listed by chapter number and title in the package application.

NUREG-1617, Standard Review Plan for Transportation Packages for Spent Nuclear Fuel was used for this review.

Chapter 1 - General Description Observations 1-1 Revise the application to clearly state that plutonium, except in the form of depleted UO2 fuel, is not authorized for transport in the Model No. HI-STAR 100MB package.

Section 1.2.3 of the application, Special Requirements for Plutonium, states: The contents of the package provided in Section 1.2.2 and to be transported in the HI-STAR 100MB Package contain plutonium in solid form and in varying quantities. This statement is incorrect as plutonium in any other form than in the spent UO2 fuel is not authorized for transport since the application does not include safety analyses for plutonium contents in solid form for any quantity.

This information is required to determine compliance with 10 CFR 71.33(b)(2), 71.55, and 71.63.

Chapter 2 - Materials Evaluation Observations 2-1 Clarify apparently conflicting information on the nature of the surface preservatives of the HI-STAR 100MB package.

Note 12 on the HI-STAR 100MB drawing states that all non-stainless steel interior containment boundary surfaces and external surfaces of the package are to be coated with a surface preservative such as stainless steel clad or weld overlay. Section 2.2.1.3

of the application also states that the use of stainless clad or overlay removes the concern of surface degradation.

However, Section 2.2.1.2.4 states that outer shells made of carbon steel will employ Carboguard or equivalent surface preservative. Also, Section 2.2.1.2.5 states that the package interior steel surfaces may be coated with Thermaline or equivalent surface preservative.

The applicant should provide a consistent description of the materials used in the HI-STAR 100MB package.

This information is required to determine compliance with 10 CFR 71.33(a)(5) and 71.43(d).

2-2 Revise Section 2.2.1.3 to provide an evaluation of the chemical, galvanic, or other reactions that could occur due to the welding of the MPC.

Section 2.2.1.3 states that no operations were identified that could produce adverse reactions because no closure welding is performed. However, Section 7.1.6 of the application describes a load and go option that includes MPC loading and closure welding.

This information is required to determine compliance with 10 CFR 71.43(d).

Chapter 3 - Thermal Evaluation 3.1 Provide the axial decay heat profile of the fuel assembly.

The applicant states, in Section 3.1.2, that the heat generation in each fuel assembly is non-uniformly distributed over the active fuel length to account for design basis fuel burnup distribution.

The axial decay heat profile of the fuel assembly (Table or Figure) is needed to verify the correct simulation of the heat generation distribution in the thermal evaluation model.

This information is required to determine compliance with 10 CFR 71.71 and 71.73.

3-2 Provide figures of the regionalized storage arrangements (per cell allowable heat loads) of the MPC-32M, and the bare basket configurations F-24M and F-32M, to verify the heat load profiles selected in the thermal analysis.

The applicant states, in Section 3.1.4, that the uniform heat load case bounds all regionalized storage arrangements that meet the requirements of (i), (ii) and (iii) as shown in pages 3.1-2 and 3.1-3.

Figures of the regionalized storage arrangements (per cell allowable heat loads) for the MPC-32M, and the bare basket configurations F-24M and F-32M, are needed to verify the per-cell heat load distribution and the bounding correlation between regionalized and uniform loadings.

This information is required to determine compliance with 10 CFR 71.33(b)(7) and 71.35(a).

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3-3 Provide thermal models and input files for the short-term operations.

Such models for package operations such as vacuum drying are missing from the application.

This information is required to determine compliance with 10 CFR 71.35, 71.71 and 71.73(a)(4).

Observations 3-4 Clarify the maximum normal operating pressures (MNOPs) for the MPC-32M and the bare basket F-32.

The applicant states in Note 2 of Table 3.1.2 that the MNOP of the MPC cavity is calculated based on an initial MPC cavity with helium backfill pressure limits as specified in Tables 7.1.2, 7.1.4, and 7.1.8 of the application. Table 3.1.2 shows higher MNOPs in the MPC-32M than in the F-32M, with a 0% rod rupture under normal conditions of transport (NCT) and a 3% rod rupture, even though the design heat load for the bare basket F-32M is greater than the design heat load for the MPC-32M (32 kW compared to 29 kW).

It is not clear to the staff how the MNOPs for the MPC-32M can be greater than those for the bare basket F-32M. The applicant should provide calculations for those MNOPs under NCT and 0% rod rupture, as well as a 3% rod rupture.

This information is required to determine compliance with 10 CFR 71.71.

3-5 Perform the NCT thermal analysis with the personnel barrier included in the thermal model The applicant states, in Section 3.1.7, that (i) under 38°C (100°F) and in the shade, the maximum computed package surface temperature (Table 3.1.5) is above the allowable surface temperature limit of 85°C (185°F) and (ii) a personnel barrier will be required to meet the accessible surface temperature limit.

Given the fact that the personnel barrier may block the air from cooling down the package during NCT, the applicant should provide a thermal analysis with the personal barrier included in the model to demonstrate that its use does not impact the rate of heat rejection from the package to the ambient by convection and radiation.

This information is required to determine compliance with 10 CFR 71.43(g) and 71.71.

3-6 Demonstrate that the mesh/grid size used in the thermal model is appropriate for both the NCT and HAC thermal evaluations.

The applicant states, in Section 3.3.2, that (i) the mesh defined for the thermal analysis is guided by grid sensitivity studies carried out in for the Model No. HI-STAR 190 package, and (ii) therefore, the grid independent calculation of the peak cladding temperature is reasonably assured.

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Given the fact that the configurations of the Model Nos. HI-STAR 100MB and HI-STAR 190 packages are not completely identical, the applicant should either demonstrate that the grid independent calculation from the HI-STAR 190 is applicable to the HI-STAR 100MB, or perform stand-alone grid sensitivity studies for the HI-STAR 100MB.

This information is required to determine compliance with 10 CFR 71.71 and 71.73.

3-7 Explain how the backfill pressures for the MPC-32M, F-32M, and F-24M are determined.

The applicant provided helium backfill requirements of 6-15 psig for the MPC-32M annulus, 2.9 -31.8 psig for the MPC-32M cavity (as shown in Tables 7.1.2 and 7.1.4, respectively) and of 2.9-21.8 psig for the F-32M/F-24M cavity and 0-2.5 psig for the F-32M/F-24M inter-lid space (as shown in Table 7.1.8), but did not explain or provide any calculation on how these backfill pressures for either the MPC-32M, F-32M, and the F-24M are determined.

This information is required to determine compliance with 10 CFR 71.35 and 71.71.

3-8 Provide the references for the thermal properties of Holtite-A and Holtite-B used for the neutron shield.

The applicant provided the thermal properties of Holtite-A and Holtite-B, such as thermal conductivity, density, and specific heat, in Tables 3.2.1, 3.2.2 and 3.2.7, but did not provide the corresponding references (e.g., pages in Sourcebook) for staffs review.

This information is required to determine compliance with 10 CFR 71.71 and 71.73.

Chapter 4 - Containment Evaluation 4-1 Provide the layout of a single closure lid - MPC containment boundary and containment system components in SAR Chapter 4.

The HI-STAR 100MB design includes options for a single closure lid when used with an MPC and a dual closure lid when used with a bare basket. The applicant provided the layout of a dual closure lid cask containment boundary and containment system components in Figure 4.1.1 but did not provide the corresponding layout for a single closure lid - MPC containment boundary and containment system.

This information is required to determine compliance with 10 CFR 71.33(a)(4).

Observations 4-2 Clarify whether there are seals in the inner closure lid for the bare basket configuration.

The applicant provided Table 4.9.1 for a concise evaluation of the ability of the two containment boundaries in the HI-STAR 100MB system to individually maintain leak-tightness under the various loading conditions. The Inner Containment Column of Table 4.9.1 states, There are no seals or gaskets in the inner containment, and the inner containment boundary has no seals or gasket. However, Section 4.1.5.1 states that, In the inner closure lid, the inner seal is the containment seal.

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Given that the inner seal is located in the inner closure lid and therefore is a part of the inner containment boundary for the bare basket configuration, it would appear then that there are seals in the inner containment.

The applicant should clarify such inconsistencies between Table 4.9.1 and Section 4.1.5.1.

This information is needed to determine compliance with 10 CFR 71.33(a)(4) and 71.7.

Chapter 6 - Criticality Evaluation Observations 6-1 Provide the sources of the material composition data used in the criticality safety analyses.

Table 6.3.5 of the application provides the material composition data of the major components of the HI-STAR 100MB packaging but does not provide the sources of such data. Because the material composition data is critical to the accuracy of the criticality safety analyses, the applicant needs to provide the sources of the data and demonstrate that the data is reliable and accurate.

This information is required to demonstrate compliance with 10 CFR 71.55(b), 71.55(d),

and 71.55(e).

6-2 Provide justification for the material compositions assumed for the BWR control rods in Table 6.B.6 and demonstrate that it is conservative to use this data to determine the material compositions of the fuel for burnup credit analyses.

Page 6.B-33 of the application shows material compositions assumed for the BWR control rods. However, such material composition data appears more likely to be used in PWR control rods: as an example, B4C is more commonly used in the BWR control rods. The applicant needs to provide justification for this assumption and demonstrate that this assumption is conservative for burnup credit analyses because B4C has a fairly large difference in absorption cross sections in comparison with the control rod material composition.

This information is required to determine compliance with 10 CFR 71.55(b), 71.55(d),

and 71.55(e).

Chapter 8 - Acceptance tests and maintenance Program 8-1 Revise Section 8.1.6 to demonstrate that the proposed approach for defining the allowable MPC flaw depth adequately considers flaw propagation.

Section 8.1.6 states that the integrity of MPCs containing high burnup fuel will be demonstrated by inspecting for flaws that exceed an allowable depth. The allowable flaw depth is established by considering the flaws effect of reducing the net wall thickness, which increases the local membrane stress.

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It is not clear to the staff whether flaws approaching the net wall thickness limit could propagate in a hypothetical accident. The applicant should demonstrate that defining the allowable flaw depth, based on net wall thickness, is conservative, and that a flaw propagation failure mode could not occur.

This information is required to demonstrate compliance with 10 CFR 71.73 and 71.85(a).

8-2 Revise Section 8.1.6 to clarify the extent of surface coverage of the eddy current testing for MPCs containing high burnup fuel.

Section 8.1.6 states that that eddy current testing will be used to identify defects in the MPC shell; however, the applicant is not clear regarding the extent of the inspection on a given MPC (i.e., entire MPC shell vs. a fraction of the shell surface). The staff requires this understanding of the proposed inspection in order to evaluate the efficacy of the approach to demonstrate the integrity of MPCs that contain high burnup fuel.

This information is required to demonstrate compliance with 10 CFR 71.85(a).

8-3 Clarify why the leakage testing of an MPC is required only when the package contains high burnup fuel (HBF).

The applicant stated in Note 4 of SAR Table 8.1.2 that for a single lid - MPC containment system, the leakage testing of an MPC is required if it contains HBF.

However, being a part of containment boundary for a single lid - MPC containment system, MPC should be leakage rate tested for any types of spent fuel (e.g., MBF and LBF) loaded in HI-STAR 100MB.

This information is needed to determine compliance with 10 CFR 71.51(a)(1) and (a)(2).

Observations 8-4 Add Note 2 to Fabrication Leakage Rate Test and Pre-shipment Leakage Rate Test under the column Leakage Test in SAR Table 8.1.2.

Instead of Note 4, the applicant should also add Note 2 to Fabrication Leakage Rate Test and Pre-shipment Leakage Rate Test under the column Leakage Test in SAR Table 8.1.2. This add is based on the items (a) and (b) under Note 2 in SAR Table 8.1.2.

This information is needed to determine compliance with 10 CFR 71.51(a)(1).

8-5 Correct a typographical error HI-STAR 1100MB Cask under the column of System Tested in SAR Table 8.1.2.

The applicant should correct HI-STAR 1100MB Cask to HI-STAR 100MB Cask under the column of System Tested in Table 8.1.2.

This information is needed to determine compliance with 10 CFR 71.7.

8-6 Section 8.1.6 paragraph on the proposed approach for defining the allowable MPC flaw depth contains an incomplete sentence.

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