Titanium and Titanium Alloy, Sheet, Strip, and Plate
- Aerospace Material Specification
- AMST9046B
- Cancelled
Scope
Recommended Content
Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed 40.0 ksi (276 MPa) Yield Strength |
Aerospace Material Specification | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Extra Low Interstitial Annealed |
Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
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.