Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength
- Aerospace Material Specification
- AMS4921R
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| Aerospace Material Specification | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Annealed |
| Aerospace Material Specification | Titanium Alloy, Bars, Wire, and Rings 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo - 0.08Si Solution and Precipitation Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Unnamed Dataset 4 | ||
| Table 1 | Composition | |
| Table 2 | Minimum tensile properties (see ) |
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.