IRON ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N Solution Heat Treated
- Aerospace Material Specification
- AMS5532F
- Revised
Scope
Recommended Content
Aerospace Material Specification | Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7 Cb (Nb) Annealed |
Aerospace Material Specification | Iron-Nickel Alloy, Strip 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al Solution Heat Treated, Cold Rolled, 50% Reduction |
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 |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Composition | |
TABLE 2 | Room Temperature Tensile Properties | |
TABLE 3 | Bending Parameters |
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.