Aerospace series. Steel FE-PL1502 (25CrMo4). 900 MPa = Rm = 1100 MPa. Bars. De = 40 mm
€165.00
Aerospace series. Steel FE-PL1502 (25CrMo4). 650 MPa = Rm = 850 MPa. Bars. De = 150 mm
Aerospace series. Steel FE-PL2102 (35NiCr6). 900 MPa = Rm = 1100 MPa. Bars. De = 40 mm
Aerospace series. Steel FE-PL2102 (34NiCr6). 900 MPa = Rm = 1100 MPa. Forgings. De = 40 mm
Aerospace series. Steel FE-PL1503 (35CrMo4). 1100 MPa = Rm = 1300 MPa. Bars. De = 25 mm
Aerospace series. Steel FE-PL1503 (35CrMo4). 900 MPa = Rm = 1100 MPa. Bars. De = 40 mm
Aerospace series. Steel FE-PM1901 (X12CrNi13). 600 MPa = Rm = 800 MPa. Bars. De = 70 mm
Aerospace series. Steel FE-PM1901 (X12CrNi13). 600 MPa = Rm = 800 MPa. Forgings. De = 70 mm
Aerospace series. Steel FE-PA3901 (X2CrNi19-11). Softened. Forgings. De = 100 mm
Aerospace series. Steel FE-PL1502 (25CrMo4). 900 MPa = Rm = 1100 MPa. Sheets, strips and plates. 0,5 mm = a = 20 mm
Aerospace series. Steel FE-PL1502 (25CrMo4). Annealed. Sheet and strip. 0,3 mm = a = 2 mm. For prevailing torque nuts
Aerospace series. Steel FE-PL1503 (35CrMo4). Annealed. Bar and wire. De = 40 mm. For prevailing torque nuts
Aerospace series. Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn). Solution treated and aged. Plate. 6 mm < a = 50 mm
Specification for bar for machining of titanium-aluminium-molybdenum-tin-silicon- carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)
Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)
