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ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 3.1Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al Consumable Electrode or Vacuum Induction Melted 1750 F (954.4 C) Solution Heat Treated

  • Aerospace Material Specification
  • AMS5596B
  • Revised
Published November 01, 1967 by SAE International in United States
 
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Language: English