SAE AMS5598E
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb (Nb) + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode, Remelted or Vacuum Induction Melted, Solution Heat Treated, Precipitation-Hardenable
Historical
Standard by SAE International, 2012-10-12
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About This Item
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate procured in inch/pound units.
AMS5598E has been reaffirmed to comply with the SAE five-year review policy.
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Standard Details
- Publication Date: 2012-10-12
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Coatings, colorants, and finishes, Heat treatment, Nickel alloys, Cobalt alloys, Tensile strength, Heat resistant materials, Corrosion, Chemicals, Magnetic materials
- Official SAE: Doi link
Document History
- New Version Available: AMS5598G (2024-07-15)
- Previous Version: AMS5598F (2019-04-11)
- This Version: AMS5598E (2012-10-12)
- Previous Version: AMS5598B (2011-08-12)
- Previous Version: AMS5598D (2000-05-01)
- Previous Version: AMS5598C (1993-07-01)
- Previous Version: AMS5598A (1981-10-01)
- Previous Version: AMS5598 (1965-09-01)
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