Titanium Alloy, 5.4al 1.4cr 1.3fe 1.25mo Annealed 135,000 Psi Yield
- Aerospace Material Specification
- AMS4929
- Cancelled
Recommended Content
Aerospace Material Specification | Aluminum Alloy, Foil 4.4cu 1.5mg 0.60mn |
Aerospace Material Specification | Titanium Alloy Sheet and Strip 8mn Annealed, 110 Ksi (760 Mpa) Yield Strength |
Aerospace Material Specification | Titanium Alloy, Bars and Forgings 4al 4mn Annealed, 130,000 Psi Yield |
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.
Reference
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