Aerospace series. O-rings, in fluorosilicone rubber (FVMQ). Technical specification
€172.00
Space systems. Safety and compatibility of materials Determination reactivity system/component with aerospace propellants
€201.00
Space systems. Safety and compatibility of materials Determination reactivity processing with aerospace fluids
Space systems. Safety and compatibility of materials Determination permeability penetration to aerospace fluids
Space systems. Safety and compatibility of materials Determination offgassed products from assembled articles
Specification for 18% nickel-cobalt-molybdenum maraging steel forging stock, forgings, bars and parts (1800 MPa: double vaccuum melted)
Specification for 1% carbon-chromium steel (vacuum arc remelted) billets, bars, forgings and parts (limiting ruling section 25 mm)
Specification for chromium-nickel-molybdenum-vanadium heat-resisting steel sheet and strip (930-1130 MPa: maximum thickness 6 mm) (Cr 12, Ni 2.5, Mo 1.7, V 0.3)
Space systems. Safety and compatibility of materials Determination upward flammability in pressurized gaseous oxygen or oxygen-enriched environments
Space systems. Safety and compatibility of materials Determination flammability electrical-wire insulation accessory
€281.00
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)
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
