Titanium Alloy, Round Bar and Wire 3AI - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Cold Drawn
- Aerospace Material Specification
- AMS4957F
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Round Bar and Wire 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Cold Drawn |
| Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated and Aged |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2A | Diameter vs arbor diameter, inch/pound units | |
| Table 2B | Diameter vs arbor diameter, SI units | |
| Table 3A | Tensile properties, inch/pound units | |
| Table 3B | Tensile properties, 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.