METALS AND ALLOYS FOR CRYOGENIC APPLICATIONS - A REVIEW
Abstract
An up-to-data review of metals and alloys suitable for cryogenic aerospace structural applications has been made. The mechanical properties of austenitic stainless steels, other steels, aluminum alloys, titanium alloys, nickel alloys and cobalt alloys from +78 to -423 F are presented, including tensile and yield strengths, elongation and notch/tensile ratios. Mechanical properties of weldments are also presented. The question of notch toughness and the notch acuity factor is discussed with respect to low temperature tensile testing. Compatibility with the liquid gases is discussed and alloys most suitable for containing liquid oxygen and hydrogen in aerospace vehicles are recommended.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 20, 1964
- Accession Number
- AD0429244
Entities
People
- E. G. Kendall
Organizations
- The Aerospace Corporation