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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.99 Other materials>BS 2HR 207:2009 Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)
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immediate downloadReleased: 2009-11-30
BS 2HR 207:2009 Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)

BS 2HR 207:2009

Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)

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Standard number:BS 2HR 207:2009
Pages:10
Released:2009-11-30
ISBN:978 0 580 67311 5
Status:Standard
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BS 2HR 207:2009


This standard BS 2HR 207:2009 Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder) is classified in these ICS categories:
  • 49.025.99 Other materials

This British Standard specifies requirements for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip.