TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC, 3Al - 2.5V, Texture Controlled, 105,000 psi (724 MPa) Yield Strength
- Aerospace Material Specification
- AMS4945
- Issued
Scope
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Hydraulic, Seamless Tubing 3.0Al - 2.5V Annealed |
| Aerospace Material Specification | Aluminum Alloy, Extrusions 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T6511 or T6510) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated |
| Aerospace Standard | Studs, Steel, Low Alloy Heat Treated, Roll Threaded |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Unnamed Dataset 4 | ||
| Unnamed Dataset 5 | ||
| TABLE I | ||
| Table II | ||
| TABLE III | ||
| TABLE III | (SI) |
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 |
|---|