Titanium Alloy, Bars, Wire, and Rings, 5al 2.5sn, Annealed, 110 Ksi (758 Mpa) Yield Strength
- Aerospace Material Specification
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings.
These products have been used typically for parts requiring strength up to 800 degrees F (427 degrees C) and which may be welded during fabrication, but usage is not limited to such applications.
|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.