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NASA - MSFC-SPEC-522

DESIGN CRITERIA FOR CONTROLLING STRESS CORROSION CRACKING

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Organization: NASA
Publication Date: 1 March 1988
Status: active
Page Count: 30
scope:

The requirements established herein apply to all metallic components proposed for use in space vehicles and other flight hardware, ground support equipment, and facilities for testing. These requirements are applicable not only to items designed and fabricated by MSFC and its prime contractors, but also to items supplied to the prime contractor by subcontractors and vendors.

PURPOSE: This document sets forth the criteria to be used in the selection of materials for space vehicles and associated equipment and facilities so that failure resulting from stress corrosion will the prevented.

Document History

MSFC-SPEC-522
March 1, 1988
DESIGN CRITERIA FOR CONTROLLING STRESS CORROSION CRACKING
The requirements established herein apply to all metallic components proposed for use in space vehicles and other flight hardware, ground support equipment, and facilities for testing. These...
November 18, 1977
DESIGN CRITERIA FOR CONTROLLING STRESS CORROSION CRACKING
A description is not available for this item.

References

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