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
€172.00
Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed Sheet and strip. 0,3 mm = a = 2 mm. For prevailing torque nuts
Aerospace series. Steel FE-PM1505 (X1CrNiMoAlTi12-9-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D = 150 mm. Rm = 1400 MPa
Aerospace series. Titanium and titanium alloys. Technical specification Plate, sheet strip
€281.00
Aerospace series. Macrostructure of titanium and alloy wrought products bar, section, forging stock forgings
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 cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (Cobalt base, Cr 20, W 15, Ni 10, Mn 1.5)
Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy wire for thread inserts (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) (0.45 mm to 2 mm diameter)
Specification for nickel-chromium-titanium heat-resisting alloy bar and wire for rivets and rivets (Maximum diameter or minor sectional dimension 20 mm) (Nickel base, Cr 19.5, Ti 0.4)
Procedure for inspection, testing and acceptance of aluminium-base and magnesium-base ingots and castings
€329.00
Specification for nickel-chromium-iron-titanium-niobium-aluminium heat-resisting alloy round wire with a maximum diameter of 2 mm for thread inserts (nickel base Cr 15.5, Fe 7.0, Ti 2.5, Nb/Ta 0.95, Al 0.70)
Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire: softened (nickel base, Cr 19.5, Co 1.8, Ti 2.5, Al 1.5)
Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4)
