Performance 17.5HP/7500rpm Idle Speed:1100 rpm/min Static Thrust 35Kg / 100 meters Altitude Static Thrust 31.5Kg / 1800 meters Altitude The specification of the aircraft propeller:30 X 12;32×10
Parameter
Exhaust Amount:170cm3 Diameter × stroke:52mm × 40mm Ratio of compression:9.5:1 Ratio of lubricating capacity:30:1 Weight:Main Engine - 3550g;Exhaust pipe – 200g × 2;Ignition equipment - 160g
|