Titanium and Titanium Alloy, Sheet, Strip, and Plate
- Aerospace Material Specification
- AMST9046A
- Revised
Scope
Recommended Content
Aerospace Material Specification | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
Aerospace Material Specification | Titanium Alloy, Sheet, Strip, and Plate 4.5Al - 3V - 2Fe - 2Mo Annealed |
Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated and Aged |
Topic
Data Sets - Support Documents
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TABLE I | Chemical composition, percent by weight | |
TABLE II | Commercially pure and alpha titanium alloy sheet, strip and plate annealed tensile properties. | |
TABLE III | Alpha-beta titanium alloys sheet, strip and plate minimum tensile properties | |
TABLE IV | Beta titanium alloys sheet, strip and plate minimum tensile properties | |
TABLE V | Bend factors for annealed or solution treated sheet and strip products | |
TABLE VI | Sheet flatness tolerances | |
TABLE VII | Flatness tolerance for annealed and duplex annealed plate. | |
TABLE VIII | Quality conformance sampling (see , , , and ) | |
TABLE IX | Cross-reference composition classification |
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.