Cobalt Alloy, Corrosion and Heat Resistant, Bars 62Co-28Cr-6Mo Warm-Worked
- Aerospace Material Specification
- AMS5918
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe Solution Heat Treated |
Aerospace Material Specification | Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 46Fe – 20.5Cr – 32Ni – 1.1Ti Annealed |
Aerospace Material Specification | Steel, Corrosion Resistant Bars, Forgings, Tubing, and Rings 15Cr - 6.5Ni - 0.75Mo - 0.50Cb (Nb) - 1.5Cu Solution Heat Treated |
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2 | MINIMUM LONGITUDINAL TENSILE PROPERTIES |
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
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.