Titanium Alloy Sheet 6Al - 4V Driver Sheet
- Aerospace Material Specification
- AMS4932C
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Titanium Alloy Sheet 6Al - 4V Driver Sheet |
Aerospace Material Specification | Titanium Tubing, Seamless Annealed, 40.0 ksi (275 MPa) Yield Strength |
Aerospace Material Specification | Tantalum Alloy Sheet, Strip, and Plate 90Ta - 10W |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | COMPOSITION | |
TABLE 2 | MINIMUM 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
Number | Title |
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AMS2249 | CHEMICAL CHECK ANALYSIS LIMITS Titanium and Titanium Alloys |
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. |
ASTME8/E8M | This document is not part of the subscrption. |