SAE AMS5755E
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 64ni 5.0cr 24.5mo 5.5fe, Solution Heat Treated.
Standard:
AKA:
- AMS5755
- Revision: E
- 2000-09-01
- 1993-04-01
- Historical. Access the latest revision: AMS5755F
- 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 oxidation resistance up to 1600 degrees F (871 degrees C), good strength up to 1200 degrees F (649 degrees C), and low coefficient of expansion, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5755F | 2002-08-21 | Latest | |
| AMS5755E | 1993-04-01 | Historical | |
| AMS5755D | 1988-01-01 | Historical | |
| AMS5755C | 1981-04-01 | Historical | |
| AMS5755B | 1973-12-01 | Historical | |
| AMS5755A | 1966-03-01 | Historical | |
| AMS5755 | 1957-01-01 | Historical |
- SAE AMS 5755
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties