TITANIUM ALLOY, BARS, WIRE, AND RINGS 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength
- Aerospace Material Specification
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|TABLE 2A||Minimum Tensile Properties, Inch/Pound Units|
|TABLE 2B||Minimum Tensile Properties, SI Units|
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.