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Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products
- Aerospace Standard
- ARP982
- Issued
Sector:
Issuing Committee:
Language:
English
Scope
Primarily to provide recommendations concerning minimizing stress corrosion cracking in wrought titanium alloy products.
Recommended Content
| Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Wire 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Spring Temper, Precipitation Hardenable |
| Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Wire 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe No. 1 Temper, Precipitation Hardenable |
| Aerospace Standard | TUBE END, WELD DESIGN STANDARD |
Data Sets - Support Documents
No Datasets Available
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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