Cryogenic Tensile Properties of Selected Aerospace Materials

  • W. Weleff
  • H. S. McQueen
  • W. F. Emmons
Conference paper
Part of the Advances in Cryogenic Engineering book series (ACRE, volume 10)


The information presented in this paper represents the results of screening tests conducted in conjunction with the NERVA program. The following families of materials were investigated :
  • Titanium: A-110-AT-ELI (5A1-2.5Sn), C-120-AV-ELI (6A1–4V)

  • Iron-base alloys: 321, 347-C, AM-350, A-286, 18 %Ni (250) maraging steel

  • Nickel-base alloys: Hastelloy C, Inconel X-750, and 713-C

  • Aluminum alloys: A-356-T6, 2219-T81, 5456-O, 6061-T6, and 7079-T6


Tensile Property Maraging Steel Area Reduction Martensitic Stainless Steel Tensile Machine 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.


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Copyright information

© Plenum Press, New York 1965

Authors and Affiliations

  • W. Weleff
    • 1
  • H. S. McQueen
    • 1
  • W. F. Emmons
    • 1
  1. 1.Aerojet-General CorporationAzusaUSA

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