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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 58Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al Consumable Electrode or Vacuum Induction Melted 1975 °F (1079 °C) Solution Heat Treated

  • Aerospace Material Specification
  • AMS5708H
  • Revised
Published November 21, 2002 by SAE International in United States
 
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Language: English