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BS EN 4387:2022
Aerospace series. Non-metallic materials. Rules for drafting and presentation of technical specifications
Aerospace series. Non-metallic materials. Rules for drafting and presentation of technical specifications
Released: 2022-05-17
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154.10 EUR
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BS 2HR 40:2010
Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy billets, bars and forgings (cobalt base Cr 20, W 15, Ni 10, Mn 1.5)
Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy billets, bars and forgings (cobalt base Cr 20, W 15, Ni 10, Mn 1.5)
Released: 2010-01-31
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BS EN 4382:2006
Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Solution treated. Seamless tubes. For hydraulic application. D ≤ 50 mm, a ≤ 3 mm
Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Solution treated. Seamless tubes. For hydraulic application. D ≤ 50 mm, a ≤ 3 mm
Released: 2007-01-31
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BS EN 3102:2013
Aerospace series. Sealants. Test methods. Determination of low-temperature flexibility
Aerospace series. Sealants. Test methods. Determination of low-temperature flexibility
Released: 2013-03-31
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BS EN 4383:2006
Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stock
Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stock
Released: 2007-01-31
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BS 2HR 5:2010
Specification for nickel-chromium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 0.4)
Specification for nickel-chromium-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 19.5, Ti 0.4)
Released: 2010-01-31
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BS 2HC 203:1989
Specification for nickel-chromium-aluminium-molybdenum-niobium alloy castings (Nickel base Cr 13.0, Al 6.0, Mo 4.5, Nb 2.3)
Specification for nickel-chromium-aluminium-molybdenum-niobium alloy castings (Nickel base Cr 13.0, Al 6.0, Mo 4.5, Nb 2.3)
Released: 1989-10-31
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BS 2HR 209:2011
Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)
Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)
Released: 2011-01-31
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19/30395271 DC
BS EN 4628. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
BS EN 4628. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
Released: 2019-04-24
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19/30395270 DC
BS EN 4627. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
BS EN 4627. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
Released: 2019-04-24
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BS EN 2959:2019
Aerospace series. Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al). Solution treated and cold worked. Bar for forged fasteners. 3 mm ≤ D ≤ 30 mm
Aerospace series. Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al). Solution treated and cold worked. Bar for forged fasteners. 3 mm ≤ D ≤ 30 mm
Released: 2019-06-13
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