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Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved
- Aerospace Material Specification
- AMS4945H
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers a titanium alloy in the form of seamless tubing.
Rationale
AMS4945H results from a Five-Year Review and update of this specification that adds additional controls on produced material (8.6).
Recommended Content
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2 | Minimum tensile properties | |
| Table 3 | Flattening test | |
| Table 4 | Tubing sizes for 1.3 minimum contractile strain ratio | |
| Table 5 | Tubing sizes for 1.5 minimum contractile strain ratio | |
| Table 6A | Tolerances, outer diameter, inch/pound units | |
| Table 6B | Tolerances, outer diameter, SI units | |
| Table 7A | Tolerances, inner diameter, inch/pound units | |
| Table 7B | Tolerances, inner diameter, 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.
Reference
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