Aerospace series - Heat resisting nickel base alloy NI-P96-HT - Cold drawn and precipitation treated - Wire - D = 10 mm
€58.00
Aerospace series - Metallic materials - Test methods - Part 16: Non-destructive testing - Penetrant testing
Aerospace series - Steel X8CrNiTi18-10 (1.4878/1.4544) - Annealed - Reference heat treatment: softened - Forging stock - De = 100 mm
Aerospace series - Steel X8CrNiTi18-10 (1.4878/1.4544) - Annealed - Reference heat treatment: softened - Hollow bars - 5 mm = a = 12 mm
Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Softened. 500 = Rm = 750 MPa. Tubes for structures. 0,5 = a = 5 mm
€165.00
Aerospace series. Steel X3CrNiMoAl13-8-2 (1.4534). Solution annealed and precipitation hardened. 1 400 = Rm = 1 550 MPa. Forgings. De = 100 mm
Aerospace series. Steel X5CrNiCuNb16-4 (1.4549 type 1.4542). As cast. Reference heat treatment: homogenised, solution treated, precipitation hardened and sub zero. Remelting stock
Aerospace series. Steel X5CrNoMoCuNb14-5 (1.4594). 930 MPa = Rm = 1 080 MPa. Bars
Aerospace series. Steel X5CrNoMoCuNb14-5 (1.4594). 930 MPa = Rm = 1 080 MPa. Forgings. De = 150 mm
Aerospace series. Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1). Consumable electrode remelted. Cold drawn wire for the manufacture of thread inserts. D = 3 mm
Aerospace series. Steel 30CrNiMo8 (1.6580). 1 100 MPa = Rm = 1 300 MPa. Forgings. De = 100 mm
Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Annealed. Reference heat treatment: softened. Hollow bars. 5 mm = a = 12 mm
Aerospace series. Heat resisting nickel base alloy NI-P96-HT. Cold drawn and precipitation treated. Wire. D = 10 mm
Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Softened. 500 MPa = Rm = 700 MPa. Forgings. De = 100 mm
Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Annealed. Reference heat treatment: softened. Forging stock. De = 100 mm