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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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56.88 EUR
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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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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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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 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)
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)
Released: 1989-10-31
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BS EN 3931:1998
Nickel base alloy NI-B31001 (NiCr19Si10). Filler metal for brazing. Tape
Nickel base alloy NI-B31001 (NiCr19Si10). Filler metal for brazing. Tape
Released: 1998-07-15
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BS 2HC 204:1989
Specification for nickel-cobalt-chromium-aluminium-titanium-molybdenum alloy castings (Nickel base Co 15.0, Cr 10.0, Al 5.5, Ti 4.8, Mo 3.0)
Specification for nickel-cobalt-chromium-aluminium-titanium-molybdenum alloy castings (Nickel base Co 15.0, Cr 10.0, Al 5.5, Ti 4.8, Mo 3.0)
Released: 1989-10-31
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BS EN 4840-102:2019
Aerospace series. Heat shrinkable moulded shapes Elastomeric, semi-rigid, temperature range -75 to 150 °C. Product Standard
Aerospace series. Heat shrinkable moulded shapes Elastomeric, semi-rigid, temperature range -75 to 150 °C. Product Standard
Released: 2020-03-27
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