Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products
- Aerospace Standard
|Aerospace Standard||Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products|
|Aerospace Material Specification||Columbium (Niobium) Alloy Sheet, Strip, and Plate, 10Hf - 1.0Ti|
|Aerospace Material Specification||Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn, Extra Low Interstitial Annealed|
Data Sets - Support Documents
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.