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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 2HC 211:1989 Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6)
immediate downloadReleased: 1989-10-31
BS 2HC 211:1989 Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6)

BS 2HC 211:1989

Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6)

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Standard number:BS 2HC 211:1989
Pages:8
Released:1989-10-31
ISBN:0 580 17577 4
Status:Standard
DESCRIPTION

BS 2HC 211:1989


This standard BS 2HC 211:1989 Specification for nickel-chromium-cobalt-molybdenum-aluminium-titanium alloy castings (Nickel base Cr 15.5, Co 10.0, Mo 8,3, Al 4.2, Ti 3.6) is classified in these ICS categories:
  • 49.025.99 Other materials

This British Standard specifies the chemical composition, mechanical properties and inspection and test requirements for a heat resisting nickel alloy (Nickel base, Cr 15.5, Co 10.0, Mo 8.3, Al 4.2, Ti 3.6) in the form of castings and remelting stock.


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