Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved
- Aerospace Material Specification
- AMS4944H
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Titanium Alloy, Hydraulic, Seamless Tubing 3.0Al - 2.5V Annealed |
Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved |
Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
TABLE 2B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
TABLE 3 | FLATTENING PARAMETERS | |
TABLE 4A | OD TOLERANCES, INCH/POUND UNITS | |
TABLE 4B | OD TOLERANCES, SI UNITS |
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.