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This quad with "Cosmos 300" engine. This is a good solution for heavy pilots, or flying with a passenger. On this quad we install a propeller with a diameter of 150 centimeters. This model can be equipped with an automatic wing start assistant, which makes start easier and more stable. Cosmos 300 Cycle 2 strokes Stroke 60 mms Displacement 293,9 cc Bore Ø 79 mms Power 36 HP at 7.500 RPM Reed valve intake Cooling system Liquid cooling Starter Manual: 3S (Soft Starter System) Dual: Electric Starter + 3S (Soft Starter System) Transmission Oil lubricated spur gear system Centrifugal clutch Reduction 1/3,04 Balancing system Spark plug NGK BR9ES Max. EGT (Exhaust Gas Temperature) EGT 650 °C (measured at 21 cms from the piston) Max. coolant temperature 90 °C Maximum RPM 7.300-7.650 RPM* Engine idle 1.800-2.000 RPM Static thrust 124 kgs prop. 160 cms at 7.500 RPM (3 blades Vittorazi Approved Prop) 116 kgs prop. 150 cms at 7.450 RPM (2 blades Vittorazi Approved Prop) 110 kgs prop. 140 cms at 7.450 RPM (3 blades Vittorazi Approved Prop) Fuel Unleaded gasoline with 2,0 % synthetic oil (Motul710) Unleaded gasoline with 1,5 % synthetic oil (Motul800) Fuel consumption : 3,2 litres/hour, at 40 kgs of static thrust, prop. 160 cms at 4.500 RPM (2 blades Vittorazi Approved Prop) 8,5 litres/hour, at 75 kgs of static thrust, prop. 160 cms at 6.000 RPM (2 blades Vittorazi Approved Prop) Weight: Single Spark, Manual: 25,0 kgs Single Spark, Dual: 26,5 kgs Twin Spark, Dual: 27,0 kgs (full weight, radiator included, liquid excluded) |