Tungsten Alloy Shapes, Sintered, High Density
- Aerospace Material Specification
- AMS7725C
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Copper-Beryllium Alloy, Bars, Rods, Shapes, and Forgings 98Cu - 1.9Be Solution Heat Treated TB00 (A) |
| Aerospace Material Specification | Forgings, Magnesium Alloy 5.5Zn - 0.45Zr (ZK60A-T5) Precipitation Heat Treated |
| Aerospace Material Specification | Silicon Bronze Bars, Rods, Forgings, and Tubing 92Cu - 3.2Si - 2.8Zn - 1.5Fe Stress Relieved |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | Minimum, Mechanical Properties |
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.
Reference
| Number | Title |
|---|---|
| ASTMB311 | This document is not part of the subscrption. |
| ASTME18 | This document is not part of the subscrption. |
| ASTME8 | This document is not part of the subscrption. |