Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70.0 ksi (483 MPa) Yield Strength
- Aerospace Material Specification
|Aerospace Material Specification||Titanium Welding Wire Commercially Pure Environment Controlled Packaging|
|Aerospace Material Specification||Sheet and Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-O) Annealed and Recrystallized|
|Aerospace Material Specification||Magnesium Alloy, Sheet and Plate 3.0Al - 1.0Zn – 0.20Mn (AZ31B-H24) Cold Rolled, Partially Annealed|
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.