CH-5 UAV Engine

Length x widthx height??712??706??643mm (Integrated intake manifold status) 712??706??588mm??Split inlet manifold status)
Main uses??Apply to heavy load long endurance UAV, light helicopter, navigation fixed-wing aircraft, light leisure sport aircraft etc and range extenders.

The engine has been used in the CH-5 UAV and AR-500B carrier-based unmanned helicopter

CHI-5 drone

AR-500B Shipborne Unmanned Helicopter

600kW military drone heavy fuel engine Main product features：
Boxer 8 cylinders ,4-stroke
Suitable for heavy fuel: diesel, RP- 3/RP-5
Light-weight design, high power-to-weight ratio
No attenuation altitude 4000m, the limit altitude is 10000m
Low fuel consumption, long-endurance
TBO time > 2000h

Fuel：Diesel, Jetfuel(RP- 3/RP- 5);
Boxer 8 cylinders,Liquid-cooled, 4-stroke, High pressure common rail, TCI
Maximum continuous power/Speed：805hp/4000rpm
Minimum fuel consumption：213g/kW·h
Weight(dry)：Air version 515kg, face version 650kg

Length x widthx height：712×706×643mm (Integrated intake manifold status) 712×706×588mm（Split inlet manifold status)
Main uses：Apply to heavy load long endurance UAV, light helicopter, navigation fixed-wing aircraft, light leisure sport aircraft etc and range extenders.

600kW military drone heavy fuel engine characteristic curve