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ALLOY BARS AND FORGINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al Solution Heat Treated, 1975 F (1079.4 C) Treatment Consumable Electrode or Vacuum Induction Melted

  • Aerospace Material Specification
  • AMS5708
  • Issued
Published July 15, 1963 by SAE International in United States
Downloadable datasets available
Annotation ability available
Language: English