Titanium Alloy Extrusions and Flash Welded Rings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized
- Aerospace Material Specification
- AMS4933C
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength |
| Aerospace Material Specification | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable, Modified Strength |
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 for Notched Rupture Test, Inch/Pound Units | |
| TABLE 4B | Stress for Notched Rupture Test, 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.