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Environmental crack-growth behavior of high strength pressure vessel alloysResults of sustained-load environmental crack growth threshold tests performed on six spacecraft pressure vessel alloys are presented. The alloys were Inconel 718, 6Al-4V titanium, A-286 steel, AM-350 stainless steel, cryoformed AISI 301 stainless steel; and cryoformed AISI 304L steel. The test environments for the program were air, pressurized gases of hydrogen, oxygen, nitrogen, and carbon dioxide, and liquid environments of distilled water, sea water, nitrogen tetroxide, hydrazine, aerozine 50, monomethyl hydrazine, and hydrogen peroxide. Surface flaw type specimens were used with flaws located in both base metal and weld metal.
Document ID
19750013361
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Forman, R. G.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Subject Category
Metallic Materials
Report/Patent Number
NASA-TN-D-7952
JSC-S-423
Report Number: NASA-TN-D-7952
Report Number: JSC-S-423
Accession Number
75N21433
Funding Number(s)
PROJECT: RTOP 786-15-31-01-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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