Titanium Alloy Cold Rolled Sheet and Strip 15V - 3Al - 3Cr - 3Sn Solution Heat Treated
- Aerospace Material Specification
- AMS4914D
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Titanium Alloy, Sheet and Strip 15Mo - 3.0AI - 2.8Cb - 0.20Si |
Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 55 ksi (379 MPa) Yield Strength |
Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed 40.0 ksi (276 MPa) Yield Strength |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2 | TENSILE PROPERTIES | |
TABLE 3 | Bending | |
TABLE 4 | MINIMUM TENSILE PROPERTIES AFTER PRECIPITATION HEAT TREATMENT OF HEATING TO 950 °F ± 10 (510 °C ± 6), HOLDING AT HEAT FOR 8 HOURS ± 0.5, AND COOLING IN AIR OR FASTER | |
TABLE 5 | MINIMUM TENSILE PROPERTIES AFTER PRECIPITATION HEAT TREATMENT OF HEATING TO 900 °F ± 10 (482 °C ± 6), HOLDING AT HEAT FOR 16 HOURS ± 0.5, AND COOLING IN AIR |
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.