Columbium (Niobium) Alloy Bars, Rods, and Extrusions 10Hf - 1.0Ti, Recrystallization Annealed
- Aerospace Material Specification
- AMS7857C
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Columbium (Niobium) Alloy Sheet, Strip, and Plate, 10Hf - 1.0Ti |
Aerospace Material Specification | Cobalt Alloy, Corrosion and Heat Resistant, Bars 62Co-28Cr-6Mo Warm-Worked |
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | COMPOSITION | |
TABLE 2 | GRAIN SIZE | |
TABLE 3 | MINIMUM TENSILE PROPERTIES | |
TABLE 4A | DIAMETER TOLERANCES, ROUND BARS AND RODS, INCH/POUND UNITS | |
TABLE 4B | DIAMETER TOLERANCES, ROUND BARS AND RODS, SI UNITS | |
TABLE 5 | THICKNESS TOLERANCES, SQUARE AND RECTANGULAR BARS |
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.