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Stress corrosion evaluation of HP 9Ni-4Co-0.20C steelA stress corrosion cracking (SCC) evaluation was undertaken on HP 9Ni-4Co-0.20C steel in support of the Advanced Solid Rocket Motor (ASRM) program. This alloy was tested in plate, bar, and ring forging forms. Several heat treating procedures yielded ultimate tensile strengths ranging from 1,407 to 1,489 MPa (204 to 216 ksi). The test environments were high humidity, alternate immersion in 3.5-percent NaCl, and 5-percent salt spray. Stress levels ranged from 25 to 90 percent of the yield strengths. The majority of the tests were conducted for 90 days. Even though the specimens rusted significantly in salt spray and alternate immersion, no failures occurred. Therefore, it can be concluded that this alloy, in the forms and at the strength levels tested, is highly resistant to SCC in salt and high humidity environments.
Document ID
19930018882
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Torres, Pablo D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Metallic Materials
Report/Patent Number
M-722
NAS 1.60:3384
NASA-TP-3384
Report Number: M-722
Report Number: NAS 1.60:3384
Report Number: NASA-TP-3384
Accession Number
93N28071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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