The engine has been used in the CH-5 UAV and AR-500B carrier-based unmanned helicopter
- MOQ
- 1
CH-5 UAV Engine
SKU: MD-P00483·Spare Parts & Components·Made to Order
Overview
The engine has been used in the CH-5 UAV and AR-500B carrier-based unmanned helicopter 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 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
Technical specification
Specifications. Key specifications: Suitable for heavy fuel diesel, RP- 3/RP-5, Fuel Diesel, Jetfuel(RP- 3/RP- 5);, 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).
Technical specification — 1 groups
Key specifications: Suitable for heavy fuel diesel, RP- 3/RP-5, Fuel Diesel, Jetfuel(RP- 3/RP- 5);, 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).
Technical specifications
Specifications
- Suitable for heavy fuel
- diesel, RP- 3/RP-5
- Fuel
- Diesel, Jetfuel(RP- 3/RP- 5);
- 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)
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.
Documents
Compatible spare parts
The engine has been used in the CH-5 UAV and AR-500B carrier-based unmanned helicopter
- MOQ
- 1