The 312CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 312CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 140kg~ 200kg. FOR PROTOCOL INTEGRATION, CONTACT TEAM AUSTARS TO GET 24/7 TECHNICAL SUPPORT

THIS IS HEAVY FUEL VERSION

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND! THIS ENGINE IS UNDER EXPORT CONTROL

Technical Parameter

Configuration	2Cyl. Horizontally Opposed	Displacement	312ml
Bore × Stroke	65mm×47mm	Speed Range	1600rpm~7000rpm
Compression Ratio		10.6:1
Lubrication	Oil Gas Lubrication	Fuel Delivery	Electronic Fuel Injection
Fuel Type	3# JET Fuel (or 92# Gasoline and Above, Aviation Gasoline)
Starting Method	External Starter Starting, Integrated Starter Starting
Starting Conditions	Cylinder Temperature ≥ 85 Celsius (JET Fuel),Throttle Position ≥ 25%
Weight	10.8kg	Fuel Consumption	410g/kW·h
Rated Power	18.4kW@8000rpm	Generator	Customized