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49.025.10 Steels
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BS 2S 515:1969+A2:2015
Specification for carbon-manganese steel sheet and strip (softened) (for use in the softened condition: 460/600MPa) (suitable for welding)
Specification for carbon-manganese steel sheet and strip (softened) (for use in the softened condition: 460/600MPa) (suitable for welding)
Released: 2015-04-30
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BS 2S 135:1977
Specification for 1% carbon-chromium steel billets, bars, forgings and parts (limiting ruling section 25 mm)
Specification for 1% carbon-chromium steel billets, bars, forgings and parts (limiting ruling section 25 mm)
Released: 2003-05-30
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BS EN 2206:2008
Aerospace series. Steel FE-PL1502 (25CrMo4). 650 MPa ≤ Rm ≤ 850 MPa. Bars. De ≤ 150 mm
Aerospace series. Steel FE-PL1502 (25CrMo4). 650 MPa ≤ Rm ≤ 850 MPa. Bars. De ≤ 150 mm
Released: 2009-09-30
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BS 2S 131:1977
Specification for high thermal expansion steel billets, bars, forgings and parts (620 MPa: limiting ruling section 150 mm)
Specification for high thermal expansion steel billets, bars, forgings and parts (620 MPa: limiting ruling section 150 mm)
Released: 1977-04-29
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BS EN 4700-003:2010
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Tube
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Tube
Released: 2010-10-31
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BS EN 3816:2006
Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened and cold rolled. Sheet and strip. a ≤ 3 mm. Rm ≥ 800 MPa
Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened and cold rolled. Sheet and strip. a ≤ 3 mm. Rm ≥ 800 MPa
Released: 2007-01-31
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BS HR 251:1974
Specification for heat-resisting alloy plate, sheet and strip (Ni 25.5, Cr 14.7, Ti 1.8, Mn 1.5, Mo 1.2, V 0.3, Fe remainder)
Specification for heat-resisting alloy plate, sheet and strip (Ni 25.5, Cr 14.7, Ti 1.8, Mn 1.5, Mo 1.2, V 0.3, Fe remainder)
Released: 1974-06-28
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BS 2S 92:1964
Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
Released: 1964-01-31
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