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The Cryogenic Tensile Properties of an Extruded Aluminum-Beryllium AlloyBasic mechanical properties; i.e., ultimate tensile strength, yield strength, percent elongation, and elastic modulus, were obtained for the aluminum-beryllium alloy, AlBeMet162, at cryogenic (-195.5 C (-320 F) and -252.8 C (-423 F)) temperatures. The material evaluated was purchased to the requirements of SAE-AMS7912, "Aluminum-Beryllium Alloy, Extrusions."
Document ID
20020085381
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Gamwell, W. R. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2002
Subject Category
Metals And Metallic Materials
Report/Patent Number
M-1059
NAS 1.15:212049
NASA/TM-2002-212049
Report Number: M-1059
Report Number: NAS 1.15:212049
Report Number: NASA/TM-2002-212049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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