MINIMIZING STRESS CORROSION IN WROUGHT HEAT TREATABLE TITANIUM ALLOY PRODUCTS
- Aerospace Standard
- ARP982
- Issued
Recommended Content
Aerospace Material Specification | Titanium Alloy Bars, Forgings and Forging Stock, 6.0Al - 4.0V, Solution Heat Treated and Aged |
Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated |
Aerospace Material Specification | Titanium and Titanium Alloy, Bars (Rolled or Forged) and Reforging Stock, Aircraft Quality |
Topic
Data Sets - Support Documents
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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