Titanium Alloy Bars, Wire, and Rings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized
- Aerospace Material Specification
- AMS4972E
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| Aerospace Material Specification | Titanium Alloy, Cold Rolled Sheet and Strip 15V - 3Al - 3Cr - 3Sn Solution Heat Treated |
| Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Minimum Tensile Properties, Inch/Pound Units | |
| TABLE 2B | Minimum Tensile Properties, SI Units | |
| TABLE 3A | Minimum Tensile Properties, Inch/Pound Units | |
| TABLE 3B | Minimum Tensile Properties, SI Units | |
| TABLE 4A | Stress-Rupture Test Stress, Inch/Pound Units | |
| TABLE 4B | Stress-Rupture Test Stress, SI Units |
Issuing Committee
AMS G Titanium and Refractory Metals Committee
The committee of Titanium, Beryllium, and Refractory Materials, AMS Committee G, is responsible for preparation, revision, review and approval of documents related to aerospace application of these materials. Included are titanium, beryllium, and refractory metallic such as molybdenum, tantalum, and columbium. The committee provides a forum for interchange of experience and ideas among industry representatives, both suppliers and users, along with interested government agencies, to ensure the utility, proper technical content, and industry acceptance of published documents.