Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Sheet and strip. 2 mm = a = 6 mm. 1080 MPa = Rm =1280 MPa
€172.00
Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Plate. 6 mm « a = 20 mm. 1080 MPa = Rm = 1280 MPa
Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Sheet and strip. 0,5 mm = a = 6 mm. 980 MPa = Rm = 1180 MPa
Aerospace series. Steel FE-CM3801 (X5CrNiCuNb16-4). Homogenized, solution treated and precipitation hardened. Investment casting. De = 50 mm. Rm = 1030 MPa
Aerospace series. Steel FE-PL1507 (40CrMoV12). Consumable electrode remelted. Hardened and tempered. Bar for machining. De = 50 mm. 1250 MPa = Rm = 1400 MPa
Aerospace series. Steel FE-PL1507 (40CrMoV12). Consumable electrode remelted. Annealed. Forging stock. a or D = 350 mm
Aerospace series. Steel FE-PL1507 (40CrMoV12). Air melted. Annealed. Forging stock. a or D = 350 mm
Aerospace series. Steel FE-PA3601 (X6CrNiTi18-10). Air melted. Softened and cold rolled. Sheet and strip. a = 3 mm. Rm = 800 MPa
Aerospace series. Steel FE-PA3004 (X10CrNi18-09). Air melted. Non heat treated. Cold drawn wire. a or D = 2,3 mm
Aerospace series. Test methods. Titanium and titanium alloys Determination of surface contamination
Aerospace series. Titanium and titanium alloys. Test methods Sampling for determination of hydrogen content
Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Solution treated. Seamless tubes. For hydraulic application. D = 50 mm, a = 3 mm
Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stock
Aerospace series. Titanium and titanium alloys. Test method. Chemical analysis for the determination of hydrogen content
€201.00
Aerospace series. Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9). Non heat treated. Forging stock. a or D = 250 mm
