Chemical Check Analysis Limits Titanium and Titanium Alloys
- Aerospace Material Specification
- AMS2249G
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Chemical Check Analysis Limits Titanium and Titanium Alloys |
Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated |
Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 25.0 ksi (172 MPa) Yield Strength |
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 |
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ASTME1409 | This document is not part of the subscrption. |
ASTME1447 | 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. |
ASTME539 | This document is not part of the subscrption. |