Space systems. Safety and compatibility of materials Determination upward flammability in pressurized gaseous oxygen or oxygen-enriched environments
€193.00
Space systems. Safety and compatibility of materials Determination flammability electrical-wire insulation accessory
€269.00
Specification for chromium-molybdenum-vanadium-niobium heat-resisting steel billets, bars, forgings and parts (930-1080 MPa) (Cr 10.5, Mo 0.6, V 0.2, Nb 0.3)
€165.00
Specification for 2 1/2% nickel-chromium-molybdenum steel billets, bars, forgings and parts (1080-1280 MPa: limiting ruling section 150 mm)
High chromium-nickel corrosion resisting steel forging stock, bars, forgings and parts (880 to 1080 MPa: limiting ruling section 100 mm)
Aerospace series. Aluminium alloy AL-P2618A-T6. Hand and die forgings. a = 150 mm
Aerospace series. Aluminium alloy AL-P2618A-T851. Hand and die forgings. a = 150 mm
Aerospace series. Aluminium alloy AL-P7010-T74. Hand and die forgings. a = 150 mm
Aerospace series. Aluminium alloy AL-P7010-T7651. Plate. 6 mm < a = 140 mm
Aerospace series. Aluminium alloy AL-P7010-T7451. Plate. 6 mm < a = 160 mm
Aerospace series. Aluminium alloy AL-P2618A-T6511. Extruded bar and section. a or D = 160 mm
Aerospace series. Aluminium AL-P1050A. H14. Sheet and strip. 0,4 mm = a = 6 mm
Specification for chromium-cobalt-molybdenum-vanadium-niobium heat-resisting steel billets, bars, forgings and parts (consumable electrode remelted) (1000-1140 MPa) (Cr 10.5, Co 6, Mo 0.8, V 0.2, Nb 0.3)
Aerospace series. Aluminium alloy AL-P2618A. Forging stock
Aerospace series - Metallic materials - Test methods - Part 002 : tensile testing at elevated temperature - Série aérospatiale
€25.33
