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ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT 52.5Ni - 19Cr - 3.0Mo - 5.1 (Cb + Ta) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1950° F (1065° C) Solution Heat Treated

  • Aerospace Material Specification
  • AMS5597B
  • Revised
Published July 01, 1981 by SAE International in United States
 
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Language: English