Steel, Corrosion and Heat-Resistant, Welding Wire 11.8Cr - 2.8Ni - 1.6Co - 1.8Mo - 0.32V Vacuum Induction Melted
- Aerospace Material Specification
- AMS5822E
- Stabilized
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel-Iron Alloy, Magnetic, Sheet and Strip 50Ni - 50Fe Stamping Quality, Half-Hard Temper |
Aerospace Material Specification | Nickel-Iron Alloy, Corrosion and Heat-Resistant, Welding Wire 12.5Cr - 42.5Ni - 6.0Mo - 2.7Ti - 0.015B - 35Fe |
Aerospace Material Specification | Steel, Corrosion- and Heat-Resistant, Welding Wire 11.8Cr - 2.8Ni - 1.6Co - 1.8Mo - 0.32V |
Data Sets - Support Documents
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.