TITANIUM ALLOY 6Al - 4V Annealed - 120,000 psi Yield
- Aerospace Material Specification
- AMS4928
- Issued
Recommended Content
Aerospace Material Specification | Molybdenum Alloy Bars 0.48Ti - 0.09Zr - 0.02C Arc Cast, Stress Relieved |
Aerospace Material Specification | Titanium Alloy, Forgings 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo - 08Si Solution and Precipitation Heat Treated |
Aerospace Material Specification | Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Aged 180 ksi (1241 MPa) Tensile Strength |
Topic
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.
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