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Controlling stress corrosion cracking in mechanism components of ground support equipmentThe selection of materials for mechanism components used in ground support equipment so that failures resulting from stress corrosion cracking will be prevented is described. A general criteria to be used in designing for resistance to stress corrosion cracking is also provided. Stress corrosion can be defined as combined action of sustained tensile stress and corrosion to cause premature failure of materials. Various aluminum, steels, nickel, titanium and copper alloys, and tempers and corrosive environment are evaluated for stress corrosion cracking.
Document ID
19880012096
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Majid, W. A.
(Lockheed Space Operations Co. Cocoa Beach, FL, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: NASA. Langley Research Center, The 22nd Aerospace Mechanisms Symposium
Subject Category
Metallic Materials
Accession Number
88N21480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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