Idle Speed: 1500 rpm/min.
14.5Kg Static Thrust/100 meters Altitude
12.8Kg Static Thrust/1800 meters Altitude
The specification of the aircraft propeller: 22*8, 22*10, 23*8, 23*10
the type of the sparking plug: NGK CM6
Exhaust Amount: 55.6cm3
Diameter x stroke: 45mm*35mm
Ratio of compression: 7.6:1
Ratio of lubricating capacity: 30:1
Weight: Main engine -1330g, Exhaust pipe -130g , ignition equipment - 130g
Ignition Volt: 4.8V-8.4V
Note: the enginee include completed ignition equipment one set, exhaust pipe, and carbureter.