Columbium (Niobium) Alloy Sheet, Strip, and Plate, 10Hf - 1.0Ti
- Aerospace Material Specification
- AMS7852C
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Columbium (Niobium) Alloy Bars, Rods, and Extrusions 10Hf - 1.0Ti, Recrystallization Annealed |
Aerospace Material Specification | Columbium (Niobium) Sheet, Strip, and Foil |
Aerospace Material Specification | Titanium Alloy, Sheet, Strip, and Plate 4Al - 2.5V - 1.5Fe Annealed |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
TABLE 2B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
TABLE 3 | BEND FACTOR | |
TABLE 4 | MINIMUM RECRYSTALLIZATION |
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.