Molybdenum Alloy Bars 0.48Ti - 0.09Zr - 0.02C Arc Cast, Stress Relieved
- Aerospace Material Specification
- AMS7819C
- Revised
Scope
Recommended Content
Aerospace Material Specification | Leaded Phosphor Bronze Strip 88.5Cu - 4.0Sn - 4.0Pb - 3.0Zn - 0.26P Cold Rolled, Half Hard (H02) |
Aerospace Material Specification | Aluminum Bronze Bars, Rods, and Forgings 87Cu - 9Al - 3Fe Stress Relieved |
Aerospace Material Specification | Molybdenum Alloy Bars 0.48Ti - 0.09Zr - 0.02C Arc Cast, Stress Relieved |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | Composition | |
TABLE 2A | Tolerances, Hot-Cold Worked, Inch/Pound Units | |
TABLE 2B | Tolerances, Hot-Cold Worked, SI Units | |
TABLE 3 | Maximum Hardness | |
TABLE 4A | Tolerances, Hot Worked, Inch/Pound Units | |
TABLE 4B | Tolerances, Hot Worked, SI Units | |
TABLE 5 |
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 |
---|---|
ANSI/B46.1 | This document is not part of the subscrption. |
ASTME350 | This document is not part of the subscrption. |
ASTME8 | This document is not part of the subscrption. |
ASTME92 | This document is not part of the subscrption. |