Depleted Uranium Castings
- Aerospace Material Specification
- AMS7730F
- Cancelled
Rationale
Recommended Content
| Technical Paper | A New High Fluidity Zinc Die Cast Alloy |
| Aerospace Material Specification | Alloy Castings, Investment, Corrosion and Heat Resistant 65.5Co - 25Cr - 1.8Ni - 5.0W As Cast |
| Aerospace Material Specification | Alloy Castings, Investment, Corrosion and Heat Resistant , 65Co - 25Cr - 1.8Ni - 5.0W, as Cast |
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
| Number | Title |
|---|---|
| AMS2350 | STANDARD TEST METHODS |
| AMS2350B | Standards and Test Methods |
| AMS2360 | ROOM TEMPERATURE TENSILE PROPERTIES OF CASTINGS |
| AMS2645 | Fluorescent Penetrant Inspection |
| AMS2645K | FLUORESCENT PENETRANT INSPECTION |
| AMS2646 | Contrast Dye Penetrant Inspection |
| ASTME8 | This document is not part of the subscrption. |
| MIL-STD-794 | This document is not part of the subscrption. |