NASA/TM-2002-212049, Gamwell, W.R., The Cryogenic Tensile Properties of an Extruded Aluminum-Beryllium Alloy, George C. Marshall Space Flight Center , Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546-0001, October 2002, pp. 24, Format(s): PDF 1752k |
Basic 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.”
| Keywords: | albemet162, tensile properties, extrusions, cryogenic |
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| Subjects: | Chemistry and Materials: Metals and Metallic Materials: Beryllium Chemistry and Materials: Metals and Metallic Materials: Aluminum |
| ID Code: | 606 |
| Deposited On: | 12 January 2004 |