SAE AMS5950
Nickel Alloy, Corrosion and Heat Resistant, Sheet and Strip 52.5ni 19cr 3.0mo 5.0cb 0.90ti 0.50al 18fe Vacuum Induction and Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable.
Standard:
AKA:
- AMS5950
- 1996-01-01
- Historical. Access the latest revision: AMS5950B
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet and strip 0.080 inch (2.03 mm) and under in nominal thickness.
These products have been used typically for parts requiring resistance to low-cycle fatigue, creep and stress-rupture up to 1300 degrees F (704 degrees C), and oxidation resistance up to 1800 degrees F (982 degrees C), particularly those parts which are superplastically or otherwise formed or welded and then heat treated to develop desired properties, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5950B | 2008-02-15 | Latest | |
| AMS5950A | 2002-11-21 | Historical | |
| AMS5950 | 1996-01-01 | Historical |
- SAE AMS 5950
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties