Chemical Check Analysis Limits Titanium and Titanium Alloys
- Aerospace Material Specification
- AMS2249F
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Tantalum Alloy Sheet, Strip, and Plate 90Ta - 10W |
| Aerospace Material Specification | Precipitation Hardenable Steel Alloy, Corrosion and Heat-Resistant Powder for Additive Manufacturing 16.0Cr - 4.0Ni - 4.0Cu - 0.30Nb |
| Aerospace Material Specification | Tantalum Alloy Bars and Rods, 90Ta - 10W, Annealed |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | Check Analysis Limits |
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
| Number | Title |
|---|---|
| ASTME120 | This document is not part of the subscrption. |
| ASTME1409 | This document is not part of the subscrption. |
| ASTME1447 | This document is not part of the subscrption. |
| ASTME1937 | This document is not part of the subscrption. |
| ASTME1941 | This document is not part of the subscrption. |
| ASTME2371 | This document is not part of the subscrption. |
| ASTME59 | This document is not part of the subscrption. |