Titanium Tubing, Welded Annealed, 40,000 psi (275 MPa) Yield Strength
- Aerospace Material Specification
- AMS4941C
- Reaffirmed
Scope
Recommended Content
Aerospace Material Specification | Titanium Tubing, Seamless Annealed, 40.0 ksi (275 MPa) Yield Strength |
Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved |
Aerospace Material Specification | Steel, Welding Wire 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (SAE 4340 Mod) Vacuum Melted, Environment-Controlled Packaging |
Topic
Data Sets - Support Documents
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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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AMS2244 | TOLERANCES Titanium and Titanium-Base Alloy Tubing |
AMS2249 | CHEMICAL CHECK ANALYSIS LIMITS Titanium and Titanium Alloys |
AMS2350 | STANDARD TEST METHODS |
ASTME120 | This document is not part of the subscrption. |
ASTME8 | This document is not part of the subscrption. |
FED-151 | This document is not part of the subscrption. |
MAM2244 | This document is not part of the subscrption. |
MIL-H-81200 | This document is not part of the subscrption. |
MIL-STD-163 | This document is not part of the subscrption. |