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Steel, Bars and Forgings 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C) Vacuum Melted, Annealed Heat Treatable to 290 ksi (1999 MPa) Tensile Strength

  • Aerospace Material Specification
  • AMS6478A
  • Revised
Published October 01, 2001 by SAE International in United States
Downloadable datasets available
Annotation ability available
Language: English