SAE AMS5702
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 41.5Ni 16Cr 37Fe 2.9Cb 1.8Ti, Consumable Electrode or Vacuum Induction Melted, 1750°F (954°C) Solution Heat Treated.
Standard:
AKA:
- AMS5702
- 1971-11-01
- Historical. Access the latest revision: AMS5702D
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring a combination of resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C), oxidation resistance up to 1800 degrees F (982 degrees C), and good machinability, particularly parts which are welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5702D | 2007-01-09 | Latest | |
| AMS5702C | 1993-04-01 | Historical | |
| AMS5702B | 1988-01-01 | Historical | |
| AMS5702A | 1981-07-01 | Historical | |
| AMS5702 | 1971-11-01 | Historical |
- SAE AMS 5702
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties