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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 1825 to 1900°F Solution Heat Treated

  • Aerospace Material Specification
  • AMS5706A
  • Revised
Published September 01, 1965 by SAE International in United States
 
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Language: English