300 hp 3-rotor gasoline engine, complete with Digital Engine Management system. Runs on avgas 100LL as well as leaded or unleaded mogas 87 octane or higher.

Engine model G300 C2B is presently undergoing FAA type certification under FAA project number TC9823 AT-E. Certification expected end 2008.

Specifications G-300

 

Engine Type Naturally Aspirated Rotary
Number of Rotors 3
Displacement 3x654cc (3x39.9 cu.in.) per rotor
Cooling Coolant: water / ethylene glycol
Coolant heat load: 87kW / 297kBTU/hr
Oil heat load: 39kW / 135kBTU/hr
Engine Management Fully redundant dual-ECU digital control
Fuel System Dual electronic injection
Dual electric pump
Recommended Fuel 100LL avgas
Leaded or unleaded mogas (US: 87, Europe: 92)
PSRU 6-pinion planetary, ratio 2.8235:1
Hydraulic CS propeller governor drive
Propeller Rotation Tractor configuration: clockwise
Pusher configuration: anti-clockwise
Max. Take-off power 300 hp @ 2,250 propeller rpm
Max. Continuous Power As above
75% Cruise Power 225 hp @ 2,000 propeller rpm
Weight¹ 177kg / 390 lbs
Dual Alternators 14V 70 Amp or 28V 40A

¹ Dry engine, PSRU weight including starter, main alternator included

Fact sheet :

Fiche_G300.pdf 3.50 MB
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