NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS AND WIRE 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50AI - 19Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Treated and Cold Worked Precipitation Hardenable
- Aerospace Material Specification
Data Sets - Support Documents
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|TABLE 2||Minimum Tensile Properties|
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.