Aircraft. De-icing/anti-icing fluids. ISO type II, III and IV
€165.00
Aerospace series. O-rings, in fluorosilicone rubber (FVMQ). Hardness 80 IRHD
Aerospace series. O-rings, in fluorosilicone rubber (FVMQ). Technical specification
Aerospace series. Nuts, hexagon, self-locking, in heat resisting steel, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature)/315°C
Space environment (natural and artificial). Process for determining solar irradiances
€193.00
Aerospace series. Insert, thin wall, self-locking, short, in heat resisting nickel base alloy NI-PH2601 (Ni-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
Aerospace series. Bolts, pan head, six lobe recess, relieved shank, long thread, in heat resisting steel FE-PA2601 (FE-PA92HT, A286), silver plated. Classification: 1100 MPa (at ambient temperature) / 650°C
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. Test method. Microstructure of (a + ß) titanium alloy wrought products bars, sections, forging stock and forgings
€269.00
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
