Titanium Alloy, Forgings 6Al - 4V Alpha-Beta or Beta Processed, Annealed
- Aerospace Material Specification
- AMS4920C
- Revised
Scope
Recommended Content
Aerospace Material Specification | Titanium Alloy, Forgings 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo - 08Si Solution and Precipitation Heat Treated |
Aerospace Material Specification | Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Overaged 140 ksi (965 MPa) Tensile Strength |
Aerospace Material Specification | Titanium Tubing, Seamless Annealed, 40.0 ksi (275 MPa) Yield Strength |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
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 |
---|---|
AMS2249 | CHEMICAL CHECK ANALYSIS LIMITS Titanium and Titanium Alloys |
AMS2750 | PYROMETRY |
AMS2808 | Identification Forgings |
ARP982 | Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products |
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. |
ASTME8 | This document is not part of the subscrption. |