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ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0 (Cb+Ta) - 0.15N

  • Aerospace Material Specification
  • AMS5532C
  • Revised
Published July 01, 1977 by SAE International in United States
 
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Language: English