Tolerances, Metric Titanium and Titanium Alloy Extruded Bars, Rods, and Shapes
- Aerospace Material Specification
- MAM2245B
- Noncurrent
Scope
Recommended Content
Aerospace Material Specification | Aluminum Alloy, Extruded Profiles (7449-T79511) 8.1Zn - 1.8Cu - 2.2Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged |
Aerospace Material Specification | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Extrusions, Tubing, and Rings Wear and Galling Resistant 8.0Mn - 4.0Si - 17Cr - 8.5Ni - 0.13N Solution Heat Treated |
Aerospace Material Specification | Titanium Alloy Extrusions and Flash Welded Rings 6Al - 4V Annealed Beta Processed |
Data Sets - Support Documents
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TABLE I | ||
TABLE IV | ||
TABLE VII | ||
TABLE VIII |
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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