Titanium Alloy, Bars, Wire, Forgings, and Rings, 6.0AI - 4.0V, Solution Heat Treated and Aged
- Aerospace Material Specification
|Aerospace Material Specification||Titanium Alloy, Sheet 6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si Annealed|
|Aerospace Material Specification||Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated|
|Aerospace Material Specification||Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated and Aged|
Data Sets - Support Documents
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.