Titanium and Titanium Alloys, Extruded Bars and Shapes, Aircraft Quality
- Aerospace Material Specification
- AMST81556A
- Cancelled
Scope
Recommended Content
Aerospace Material Specification | Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Overaged 160 ksi (1103 MPa) Tensile Strength |
Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 8Al - 1Mo - 1V Duplex Annealed |
Aerospace Material Specification | Titanium Alloy, Bars, Wire, Forgings, and Rings 6Al - 6V - 2Sn Solution and Precipitation Heat Treated |
Data Sets - Support Documents
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.