Titanium Alloy Extrusions and Flash Welded Rings 6Al - 4V Annealed Beta Processed
- Aerospace Material Specification
- AMS4935L
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy Extrusions and Flash Welded Rings 6Al - 4V Annealed Beta Processed |
| Aerospace Material Specification | Titanium Alloy, Extrusions and Flash Welded Rings 6Al - 6V - 2Sn Beta Extruded Plus Annealed, Heat Treatable |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2 | Minimum tensile 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.