Titanium Alloy, Round Bar and Wire, 3al 8v 6cr 4mo 4zr, Consumable Electrode Melted, Solution Heat Treated and Cold Drawn
- Aerospace Material Specification
This specification covers a titanium alloy in the form of round bar and wire, 0.625 inch (15.88 mm) and under in nominal diameter or thickness.
These products have been used typically for coil springs requiring high tensile strength, and corrosion resistance, but usage is not limited to such application.
Data Sets - Support Documents
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.