SAE AMS5598D
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate, 72ni 15.5cr 0.95(Cb+Ta) 2.5ti 0.70al 7.0fe, Consumable Electrode Or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable.
Standard:
AKA:
- AMS5598
- Revision: D
- 2000-05-01
- Historical. Access the latest revision: AMS5598E
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in inch/pound units.
MAM 5598 is the metric version of this AMS.
These products have been used typically for parts requiring high strength up to 1500 degrees F and oxidation resistance up to 1800 degrees F and for bellows and flat springs requiring optimum resistance to relaxation up to 1000 degrees F with moderate or relatively low stresses, particularly where welding is involved, but usage is not limited to such applications. Parts may be formed, welded if required, and then heat treated to improve strength at elevated temperatures.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5598E | 2007-07-05 | Latest | |
| AMS5598D | 2000-05-01 | Historical | |
| AMS5598C | 1993-07-01 | Historical | |
| AMS5598B | 1991-10-01 | Historical | |
| AMS5598A | 1981-10-01 | Historical | |
| AMS5598 | 1965-09-01 | Historical |
- SAE AMS 5598
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties