Alloy, Sheet and Strip 42Fe - 37.5Ni - 14Co - 4.8(Cb + Ta) - 1.6Ti Solution Heat Treated, Precipitation Hardenable Multiple Melted, High Temperature, Low Expansion
- Aerospace Material Specification
- AMS5892A
- Reaffirmed
Scope
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Tensile Properties | |
| TABLE 3 | Bending Factor | |
| TABLE 4 | Minimum Tensile Properties | |
| TABLE 5A | Minimum Tensile Properties at 1200 °F, Inch/Pound Units | |
| TABLE 5B | Minimum Tensile Properties at 649 °C, SI Units | |
| TABLE 6A | Minimum Stress-Rupture Properties, Inch/Pound Units | |
| TABLE 6B | Minimum Stress-Rupture Properties, SI Units |
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.