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Nickel-Iron Alloy, Corrosion and Heat-Resistant, Bars and Forgings, 12.5Cr - 42.5Ni - 6.0Mo - 2.7Ti - 0.015B - 34Fe, Consumable Electrode Remelted or Vacuum Induction Melted, Solution, Stabilization, and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS5660A
  • Revised
Published January 01, 1960 by SAE International in United States
Language: English