DESCRIPTION：
Four
cylinder, horizontally opposed engine, with liquid cooled cylinderheads,
electronic fuel injection and dual ignition system, automatic altitude
compensation, wet sump pressure lubrication
FEATURERS：
1.Liquid
cooled cylinderheads, electronic fuel injection and dual ignition system.
2,The ratio of power weight is higher.
3.Extremely low failure rate.
TECHNICAL DATA:
Maximum
Power 74 kW / 100 HP at 3000 rpm
Displacement 2424 cm3 / 147.91 cub. in.
Compression ratio 9.5 : 1
Ignition Electronic engine management
Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL
Dry weight 76 kg, plus accessories
Fuel consumption 265 g/kWh at WOT,245 g/kWh at part throttle.
APPLICATION:
Used
for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
OTHER INFORMATION:
We can provide propellers, generators(for UAV),
start-generators and other accessories.
