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Type NASA-23NASA-23 alloy has been designed to fulfil NASA's unique need for a high strength, oxidation-and corrosion resistant alloy that is compatible with a high-pressure hydrogen environment. This alloy is a precipitation hardened iron-nickel base alloy with excellent strength and ductility art gaseous hydrogen (GH2), comparable to those of other alloys in its class, Inconel 718 and IN-903. NASA-23 has been designed with a sufficient amount of chromium to provide good corrosion/oxidation resistance. For hydrogen resistance, the alloy maintains a (Ni + Co)/Fe ratio close to 1.26, the same as that of Incoloy 903. Hardening constituents, Nb, Ti, and Al, are optimized for strength and ductility both in air and GH2 atmospheres.
Document ID
20020048636
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Binayak, Panda
(Purdue Univ. West Lafayette, IN United States)
Jones, Clyde S.
Date Acquired
August 20, 2013
Publication Date
November 1, 2001
Publication Information
Publication: Aerospace Structural Metals Handbook
Subject Category
Metals And Metallic Materials
Distribution Limits
Public
Copyright
Other

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