Columbium (Niobium) Alloy Foil, Sheet, Strip, and Plate 10W - 2.5Zr Recrystallized
- Aerospace Material Specification
- AMS7851D
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Columbium (Niobium) Alloy Bars, Rods, and Wire 10W - 2.5Zr Recrystallized |
| Aerospace Material Specification | Steel Bars and Forgings 3.5Cr – 7.5Ni – 16.3Co – 1.75Mo – 0.2W – (0.09 - 0.13C) Double Vacuum Melted, Normalized, Annealed |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | MINIMUM TENSILE PROPERTIES AT ROOM TEMPERATURE | |
| TABLE 3 | MINIMUM TENSILE PROPERTIES AT 2200 °F (1204 °C) | |
| TABLE 4 | MINIMUM BEND ANGLE |
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.