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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
  • AMS5708G
  • Revised
Published December 01, 1995 by SAE International in United States
 
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Language: English