TITANIUM ALLOY BARS 11.5Mo - 6.0Zr - 4.5Sn 1375°F (745°C) Solution Heat Treated
- Aerospace Material Specification
- AMS4980B
- Reaffirmed
Recommended Content
Aerospace Material Specification | Washers, Spring Lock, Corrosion Resistant Steel, 18Cr - 9Ni |
Aerospace Material Specification | Steel, Corrosion- and Heat-Resistant, Welding Wire 15Cr - 30Ni - 1.2Mo - 2.2Ti - 0.25Al - 0.001B - 0.030V (0.01 - 0.03C) Vacuum Induction Melted, Environment Controlled Packaging |
Aerospace Material Specification | Titanium Alloy Bars, Wire, Forgings, and Rings 4.5Al - 3V - 2Fe - 2Mo Annealed |
Data Sets - Support Documents
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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.
Reference
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