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- W1994615087 abstract "This paper describes the development of a high-strength alloy (1241 MPa ultimate and 1103 MPa yield, with little or no degradation in hydrogen) for application in advanced hydrogen-fueled rocket engines. Various compositions of the Fe-Ni-Co-Cr system with elemental additions of Cb, Ti and Al are discussed. After processing, notched tensile specimens were tested in 34.5-MPa hydrogen at room temperature, as the main screening test. The H2/air notch tensile ratio was used as the selection/rejection criterion. The most promising alloys are discussed." @default.
- W1994615087 created "2016-06-24" @default.
- W1994615087 creator A5074501222 @default.
- W1994615087 date "1986-06-16" @default.
- W1994615087 modified "2023-09-27" @default.
- W1994615087 title "A new high strength alloy for hydrogen fueled propulsion systems" @default.
- W1994615087 cites W2329089017 @default.
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- W1994615087 doi "https://doi.org/10.2514/6.1986-1478" @default.
- W1994615087 hasPublicationYear "1986" @default.
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