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The stress corrosion resistance and the cryogenic temperature mechanical properties of annealed Nitronic 60 bar materialAmbient and cryogenic temperature mechanical properties and the ambient temperature stress corrosion properties of annealed, straightened, and centerless ground Nitronic 60 stainless steel alloy bar material are presented. The mechanical properties of longitudinal specimens were evaluated at test temperatures from ambient to liquid hydrogen. The tensile test data indicated increasing strength with decreasing temperature to -196 C. Below liquid nitrogen temperature the smooth tensile and notched tensile strengths decreased slightly while the elongation and reduction of area decreased drastically. The Charpy V-notched impact energy decreased steadily with decreasing test temperature. Stress corrosion tests were performed on longitudinal tensile specimens and transverse C-ring specimens exposed to: alternate immersion in a 3.5% NaCl bath; humidity cabinet; and a 5% salt spray atmosphere. The longitudinal tensile specimens experienced no corrosive attack. Approximately 3/4 of the transverse C-rings exposed to alternate immersion and to salt spray experienced a pitting attack on the top and bottom ends. Additional stress corrosion tests were performed on transverse tensile specimens. No failures occurred in the 90% stressed specimens exposed for 90 days in the alternate immersion and salt spray environments
Document ID
19770009206
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Montano, J. W. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-X-73359
Report Number: NASA-TM-X-73359
Accession Number
77N16149
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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