Structural Materials for High Altitude/High Temperature Vehicles
Date Published: 1966-02-01
Paper Number:660665
DOI: 10.4271/660665
Citation:
Roush, M., "Structural Materials for High Altitude/High Temperature Vehicles," SAE Technical Paper 660665, 1966, doi:10.4271/660665.
Author(s):
Milton S. Roush - AiResearch Manufacturing Co. of Arizona, Div., Garrett Corp.
Abstract:
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.
File Size: 1897K
Product Status: In Stock
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