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

  • Aerospace Material Specification
  • AMS5664B
  • Revised
Published October 1, 1980 by SAE International in United States
 
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Language: English