49.025 : Materials for aerospace construction

49.025.01

Materials for aerospace construction in general

49.025.05

Ferrous alloys in general

49.025.10

Steels

49.025.15

Non-ferrous alloys in general

49.025.20

Aluminium

49.025.30

Titanium

49.025.40

Rubber and plastics

49.025.50

Adhesives

49.025.60

Textiles

49.025.99

Other materials
BS HR 10:1972

BS HR 10:1972

Superseded Historical

Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)

€165.00

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BS HR 40:1972

BS HR 40:1972

Superseded Historical

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)

€165.00

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BS HR 240:1972

BS HR 240:1972

Superseded Historical

Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (cobalt base Cr 20, W 15, Ni 10, Mn 1.5)

€165.00

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BS HC 100:1972

BS HC 100:1972

Superseded Historical

Inspection and testing procedure for iron, nickel, copper, cobalt and refractory metal base alloy castings

€193.00

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BS TA 43:1972

BS TA 43:1972

Withdrawn Most Recent

Specification for forging stock of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm2) (limiting ruling section 65 mm)

€77.00

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BS TA 44:1972

BS TA 44:1972

Withdrawn Most Recent

Specification for forgings of titanium-aluminium-zirconium-molybdenum-silicon alloy (tensile strength 990-1140 N/mm2) (limiting ruling section 65 mm)

€77.00

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BS HR 4:1972

BS HR 4:1972

Superseded Historical

Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)

€165.00

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BS HR 3:1972

BS HR 3:1972

Superseded Historical

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 4.7, Ti 1.2)

€165.00

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BS HR 650:1972

BS HR 650:1972

Superseded Historical

Specification for high expansion heat-resisting steel bar and wire for the manufacture of bolts, studs, set screws and nuts (Ni 25.5, Cr 15, Ti 2, Mn 1.5, Mo 1.25, Si 0.7, V 0.3) (limiting ruling section 20 mm)

€81.00

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BS HR 203:1972

BS HR 203:1972

Superseded Historical

Specification for nickel-chromium-titanium heat-resisting alloy plate, sheet and strip (nickel base, Cr 19.5, Ti 0.4)

€165.00

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BS HR 204:1972

BS HR 204:1972

Superseded Historical

Specification for nickel-chromium-iron-molybdenum-cobalt-tungsten heat-resisting alloy plate, sheet and strip (nickel base Cr 22, Fe 18.5, Mo 9, Co 1.5, W 0.6)

€81.00

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BS L 113:1971 (R2003)

BS L 113:1971 (R2003)

Superseded Historical

Specification for sheet and strip of aluminium-magnesium-silicon-manganese alloy (solution treated and precipitation treated) (suitable for welding) (Mg 0.8, Si 1, Mn 0.7)

€165.00

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BS TA 38:1971

BS TA 38:1971

Superseded Historical

Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm2) (limiting ruling section 25 mm)

€165.00

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BS TA 39:1971

BS TA 39:1971

Superseded Historical

Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 N/mm2) (limiting ruling section 25 mm)

€165.00

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BS TA 40:1971

BS TA 40:1971

Superseded Historical

Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 N/mm2) (limiting ruling section over 25 mm up to and including 75 mm)

€165.00

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