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Heat-resistant alloys are arbitrarily defined as iron alloys richer in alloy content than the 18 percent chromium, 8 percent nickel types, or as alloys with a base element other than iron and which are intended for elevated-temperature service.

This chapter contains strength properties and related characteristics of wrought heat-resistant alloy products used in aerospace vehicles. The strength properties are those commonly used in structural design, such as tension, compression, bearing and shear.
 

Document History

  1. MMPDS MMPDS-13 Chapter 6


    Metallic Materials Properties Development and Standardization (MMPDS) Handbook - Chapter 6 - Heat Resistant Alloys

    • Most Recent
  2. MMPDS MMPDS-12 Chapter 6


    Metallic Materials Properties Development and Standardization (MMPDS) Handbook - Chapter 6 - Heat Resistant Alloys

    • Historical Version
  3. MMPDS MMPDS-11 Chapter 6


    Metallic Materials Properties Development and Standardization (MMPDS) Handbook - Chapter 6 - Heat Resistant Alloys

    • Historical Version
  4. MMPDS MMPDS-10 Chapter 6


    Metallic Materials Properties Development and Standardization (MMPDS) Handbook - Chapter 6 - Heat Resistant Alloys

    • Historical Version
  5. MMPDS MMPDS-09 Chapter 6


    Metallic Materials Properties Development and Standardization (MMPDS) Handbook - Chapter 6 - Heat Resistant Alloys

    • Historical Version
  6. MMPDS MMPDS-08 Chapter 6

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    Metallic Materials Properties Development and Standardization (MMPDS) Handbook - Chapter 6 - Heat Resistant Alloys

    • Historical Version