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Structural Materials for High Altitude/High Temperature Vehicles
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1966 by SAE International in United States
Annotation ability available
This paper discusses those materials that appear to offer the most promise for structural usage in high altitude/high temperature vehicles. Various aluminum-, titanium-, beryllium-, iron-, and nickel-base alloys are compared with respect to density, short time tensile, creep, fatigue, and fracture toughness properties. Their corrosion and stress corrosion characteristics as well as long time stability are discussed.
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CitationRoush, M., "Structural Materials for High Altitude/High Temperature Vehicles," SAE Technical Paper 660665, 1966, https://doi.org/10.4271/660665.
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