Titanium Alloy Wire 13.5V - 11Cr - 3Al Spring Temper
- Aerospace Material Specification
- AMS4959G
- Stabilized
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Wire, Steel Welding 18.5Ni - 8.5Co - 5.2Mo - 0.72Ti - 0.10Al (Marage 300) Vacuum Melted, Environment Controlled Packaging |
| Aerospace Material Specification | Aluminum Alloy, Bar, Rod, and Wire, Rolled, Drawn, or Cold Finished, 6262 |
| Aerospace Material Specification | Steel Bars, Forgings, and Tubing, 1.2Cr - 3.2Ni - 0.12Mo (0.11 - 0.17C) (9315) |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Table 1 | Composition | |
| Table 2A | Coiling parameters, inch/pound units | |
| Table 2B | Coiling parameters, SI units | |
| Table 3A | Minimum tensile properties, inch/pound units | |
| Table 3B | Minimum tensile properties, SI units |
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.