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Development of hydrogen resistant structural alloy NASA-23Hydrogen-resistant alloy NASA-23 was developed specifically as a structural alloy for application in liquid propulsion systems that use hydrogen fuel. NASA-23 was designed to be similar to Alloy 718 in strength, ductility, and corrosion resistance, but with superior resistance to hydrogen environment embrittlement. The alloy is readily processed; it can be both hot and cold worked and is castable and weldable. A material property data base is being generated for both cast and wrought NASA-23. This paper will present the status of alloy development and discuss potential applications in propulsion systems.
Document ID
19930066322
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bhat, B. N.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mcpherson, W. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kuruvilla, A. K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Chen, P. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Panda, B.
(IIT Research Inst. Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Metallic Materials
Report/Patent Number
AIAA PAPER 93-2612
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASEE, ASME, AIAA, SAE
Accession Number
93A50319
Distribution Limits
Public
Copyright
Other

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