TITANIUM ALLOY BARS AND WIRE 11.5Mo - 6.0Zr - 4.5Sn Solution Heat Treated
- Aerospace Material Specification
- AMS4977
- Issued
Recommended Content
Aerospace Material Specification | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable |
Aerospace Material Specification | Nickel Alloy, Brazing Filler Metal 94Ni - 3.5Si - 1.8B 1800 °F (982 °C) Solidus, 1950 °F (1066 °C) Liquidus |
Aerospace Material Specification | Tantalum Alloy, Bars and Rods 90Ta - 10W |
Topic
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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