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Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1950 °F (1066 °C) Solution Heat Treated, Precipitation Hardenable

  • Aerospace Material Specification
  • AMS5664F
  • Revised
Published January 03, 2017 by SAE International in United States
 
Digital Standard available
Downloadable datasets available
Annotation ability available
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Language: English