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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.10 Steels>BS 2HR 53:2010 Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder)
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immediate downloadReleased: 2010-01-31
BS 2HR 53:2010 Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder)

BS 2HR 53:2010

Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder)

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Standard number:BS 2HR 53:2010
Pages:16
Released:2010-01-31
ISBN:978 0 580 67438 9
Status:Standard
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BS 2HR 53:2010


This standard BS 2HR 53:2010 Specification for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 42.5, Cr 12.5, Mo 5.8, Ti 3.0, Fe remainder) is classified in these ICS categories:
  • 49.025.10 Steels

This British Standard specifies requirements for nickel-iron-chromium-molybdenum-titanium heat-resisting alloy supplied in the following forms, and as parts.

  1. Bars for machining: solution treated, designation HR 53A.

  2. Extruded section for subsequent forming: solution treated, designation HR 53B.

  3. Billets and bars for forging: hot or cold worked and subsequently machined or ground, designation HR 53C.

  4. Forgings: solution treated and precipitation treated, designation HR 53D.