Product Description：

Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, automatic altitude compensation, wet sump pressure lubrication

Product Feature：

1.with liquid cooled cylinderheads, electronic fuel injection and dual ignition system.
2,The ratio of power weight is higher.
3.Extremely low failure rate.
4.Turbo charger,full take off power at 3500 meters.

Technical Data:

Maximum Power 96 kW / 130 HP at 3000 rpm
Displacement 2424 cm3 / 147.91 cub. in.
Compression ratio 8 : 1
Ignition Electronic engine management
Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL
Dry weight 86 kg, plus accessories
Fuel consumption 255 g/kWh at WOT
240 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.