1、Performance
2.5HP/9000rpm (2.5HP/9000rpm)
Idle Speed: 1750 rpm/min
Static Thrust 6Kg / 100 meters Altitude
Static Thrust 5.3Kg / 1800 meters Altitude
The specification of the aircraft propeller:14 X10;15 X 8;16 X 6;16 X 8;17 X 6
the type of the sparking plug ：NGK CM6
2、Parameter
Exhaust Amount : 20cm3
diameter × stroke : 32mm×25mm
Ratio of compression: 10.5：1
Ratio of lubricating capacity : 30:1
Weight: Main engine - 650g Exhaust pipe - 50g
Ignition equipment - 120g
