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NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.006B - 0.05Zr Consumable Electrode or Vacuum Induction Melted 995 to 1040 °C Solution Heat Treated

  • Aerospace Material Specification
  • MAM5706B
  • Revised
Published July 01, 1998 by SAE International in United States
 
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Language: English