Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 57Ni - 20Cr - 10Co - 8.5Mo - 2.1Ti - 1.5Al - 0.005B Vacuum Induction and Consumable Electrode Melted, Solution Heat Treated Precipitation Heat Treatable
- Aerospace Material Specification
- AMS5951
- Issued
Scope
Rationale
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2A | TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 2B | TENSILE PROPERTIES, SI UNITS | |
| TABLE 3 | BENDING PARAMETERS | |
| TABLE 4 | BENDING PARAMETERS | |
| TABLE 6A | STRESS RUPTURE PARAMETERS AND LIMITS, INCH/POUND UNITS | |
| TABLE 6B | STRESS RUPTURE PARAMETERS AND LIMITS, 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.