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Evaluation of the stress corrosion cracking resistance of several high strength low alloy steelsThe stress corrosion cracking resistance was studied for high strength alloy steels 4130, 4340, for H-11 at selected strength levels, and for D6AC and HY140 at a single strength. Round tensile and C-ring type specimens were stressed up to 100 percent of their yield strengths and exposed to alternate immersion in salt water, salt spray, the atmosphere at Marshall Space Flight Center, and the seacoast at Kennedy Space Center. Under the test conditions, 4130 and 4340 steels heat treated to a tensile strength of 1240 MPa (180 ksi), H-11 and D6AC heat treated to a tensile strength of 1450 MPa (210 ksi), and HY140 (1020 MPa, 148 ksi) are resistant to stress corrosion cracking because failures were not encountered at stress levels up to 75 percent of their yield strengths. A maximum exposure period of one month for alternate immersion in salt water or salt spray and three months for seacoast is indicated for alloy steel to avoid false indications of stress corrosion cracking because of failure resulting from severe pitting.
Document ID
19800016917
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Humphries, T. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nelson, E. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-78276
Report Number: NASA-TM-78276
Accession Number
80N25413
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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