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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 208:1989 Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5)
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immediate downloadReleased: 1989-10-31
BS 2HC 208:1989 Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5)

BS 2HC 208:1989

Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5)

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Standard number:BS 2HC 208:1989
Pages:8
Released:1989-10-31
ISBN:0 580 17575 8
Status:Standard
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BS 2HC 208:1989


This standard BS 2HC 208:1989 Specification for nickel-cobalt-tungsten-chromium-aluminium-molybdenum-titanium-tantalum alloy castings (nickel base Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5) 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, Co 10.0, W 10.0, Cr 9.0, Al 5.5, Mo 2.5, Ti 1.5, Ta 1.5) in the form of castings and remelting stock.