Aerospace series. Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3). Non heat treated. Remelting stock
€165.00
Aerospace series. Titanium and titanium alloys. Test method. Chemical analysis for the determination of hydrogen content
€193.00
Aerospace series. Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9). Non heat treated. Forging stock. a or D = 250 mm
Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products sheet for superplastic forming
Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products plate
€269.00
Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products bars, sections, forging stock and forgings
Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products General requirements
Aerospace series. Aluminium alloy AL-P7010-T76. Die Forgings. a = 200 mm
Aerospace series. Steel FE-PL1501 (30CrMo12). Air melted. Softened. Forging stock. a or D = 300 mm
Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Plate - 6 mm < a = 20 mm - 1070 MPa = Rm = 1220 MPa
Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted. Hardened and tempered. Forgings. De = 100 mm. 900 MPa = Rm = 1100 MPa
Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Non heat treated. Forging stock. a or D = 250 mm
Aerospace series. Test methods. Titanium alloy wrought products. Determination of primary a content. Point count method and line intercept method
Aerospace series. Test methods. Titanium alloy wrought products. Determination of ß transus temperature. Metallographic method
Aerospace series. Steel FE-PA3901 (X1CrNi18-10). Air melted. Softened. Wires. 0,4 mm = D = 12,5 mm. 450 MPa = Rm = 650 MPa