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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 1750°F (955°C) Solution Heat Treated

  • Aerospace Material Specification
  • AMS5596F
  • Revised
Published January 01, 1987 by SAE International in United States
Downloadable datasets available
Annotation ability available
Language: English