Titanium Alloy, Forgings 5.8Al - 4.0Sn - 3.5Zr - 2.8Mo - 0.7Nb - 0.35Si - 0.06C Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS6952
- Issued
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy Forgings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized |
| Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Bars, and Forgings 10Cr - 5.5Ni - 14Co - 2Mo - 1W (0.19-0.23C) Vacuum Induction Melted, Vacuum Arc Remelted, Normalized, Annealed |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2 | Minimum room temperature tensile properties | |
| Table 3 | Minimum elevated temperature tensile properties |
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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