BS 2HR 3:2010
BS 2HR 3:2010
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BS 2HR 3:2010

Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)

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BS 2HR 3:2010

Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)

Purchase Options: Immediate PDF Download

Printed publication for Next Day or Standard Delivery
Price:  £122 (50% discount for members - click here for more information)

BS 2HR 3:2010

Specification for nickel-cobalt-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 14.8, Mo 5, Al 4.8, Ti 1.2)

Purchase Options: Immediate PDF Download

Printed publication for Next Day or Standard Delivery
Price:  £122 (50% discount for members - click here for more information)
Product details for BS 2HR 3:2010
Category: AIRCRAFT AND SPACE VEHICLE ENGINEERING

Publication date:

Product detail: 16 pages

ISBN reference: 978 0 580 67041 1

Cross references to standards relating to BS 2HR 3:2010:

Keywords: Air transport engineering, Nickel alloys, Cobalt-containing alloys, Chromium-containing alloys, Molybdenum-containing alloys, Aluminium-containing alloys, Titanium-containing alloys, Heat-resistant materials, Billets, Bars (materials), Forgings, Metal sections, Semi-finished products, Chemical composition, Heat treatment, Mechanical properties of materials

Variations and abbreviations: BS2HR3:2010,BS2HR3,BS 2HR 3

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