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Homepage>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.10 Steels

49.025.10 Steels

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488 results
First page123...343537394041Last page
BS 5S 82:1976
Specification. 4% nickel-chromium-molybdenum case-hardening steel billets, bars, forgings and parts (1320-1520 MPa)
Released: 2003-05-30
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BS EN 3527:2007
Aerospace series. Steel FE-PL1504 (33CrMoV12). Air melted. Softened. Forging stock. a or D ≤ 300 mm
Released: 2007-04-30
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BS S 161:1990
Specification for chromium-nickel-molybdenum corrosion-resisting steel. Bright bars and parts (540 MPa, limiting ruling section 160 mm) (Cr 17.5, Ni 12.5, Mo 2.25, controlled nitrogen content)
Released: 1990-09-28
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BS 2S 147:1976
Specification for 0.5% nickel-chromium-molybdenum steel bars for the manufacture of forged bolts and forged nuts
Released: 1976-11-30
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BS EN 3163:2007
Aerospace series. Steel FE-PM3801 (X5CrNiCu17-4). Air melted, softened, forging stock a or D ≤ 300 mm
Released: 2008-07-31
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BS EN 3529:2010
Aerospace series. Steel FE-PM2701 (X2NiCoMo18-8-5). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Forgings. a or D ≤ 150 mm. 1750 MPa ≤ Rm ≤ 2000 MPa
Released: 2010-04-30
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BS 2S 136:1977
Specification for 1% carbon-chromium steel (vacuum arc remelted) billets, bars, forgings and parts (limiting ruling section 25 mm)
Released: 2005-03-09
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BS S 206:1999
Chromium-nickel-aluminium corrosion resisting steel (precipitation hardening) rod, cold drawn wire and springs
Released: 1999-11-15
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BS EN 4632-003:2010
Aerospace series. Weldability and brazeability of materials in aerospace constructions Welding and brazing of homogeneous assemblies of unalloyed and low alloy steels
Released: 2010-05-31
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BS HC 106:1974
Specification for precipitaton hardening chromium-nickel-copper corrosion-resisting steel castings (1250-1500 MPa) (Cr 16, Ni 4, Cu 3)
Released: 1974-11-29
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BS HC 103:1974
Specification for 23% chromium-nickel-tungsten corrosion-resisting steel castings (Cr 23, Ni 11, W 3)
Released: 1974-05-10
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BS EN 3532:2007
Aerospace series. Steel FE-PM2701 (X2NiCoMo18-8-5).Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated.Plate. 6 mm < a ≤ 40 mm. 1750 MPa ≤ Rm ≤ 2000 MPa
Released: 2007-04-30
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488 results
First page123...343537394041Last page