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Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products
- Aerospace Standard
- ARP982D
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products.
Rationale
ARP982D has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
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Topic
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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