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ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al Solution, Stabilization, and Precipitation Heat Treated 1825 - 1900 F (996.1 - 1037.8 C) Treatment Consumable Electrode or Vacuum Induction Melted

  • Aerospace Material Specification
  • AMS5707B
  • Revised
Published March 01, 1966 by SAE International in United States
 
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Language: English