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The Mistral Engines are available in two and three rotor versions

For both aircrafts and helicopters, and is adaptable to all light aircraft. The naturally aspirated engines with take-off power ratings of 200hp for the two rotor engine and 300hp for the three rotor engine are now available.

G-200 G-300
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G-200 Two Rotors

200 hp two rotors gasoline engine, completed with Full Authority Digital Engine Control (FADEC).
Runs on avgas 100LL as well as on leaded or unleaded mogas, 87 octane (US), 92 octane (Europe) or higher .

Engine Type Naturally aspirated rotary
Number of Rotors 2
Displacement 3x654cc (3x39.9 cu.in.) per rotor
Cooling Coolant: water / ethylene glycol
Coolant heat load: 58kW / 198kBTU/hr
Oil heat load: 26kW / 90kBTU/hr
Engine Management Fully redundant dual-ECU digital control
Fuel System Dual electronic injection
Dual fuel pumps
Recommended Fuel 100LL avgas
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 200 hp @ 2,250 propeller rpm
Max. Continuous Power As above
Weight 1 132 kgs / 291 lbs
Dual alternators 14V 70 Amp or 28V 40A
¹ Dry engine, PSRU weight including starter, main alternator included

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G-300 Three Rotors

300 hp three rotors gasoline engine, completed with Full Authority Digital Engine Control (FADEC)
Runs on avgas 100LL as well as on leaded or unleaded mogas, 87 octane (US), 92 octane (Europe) or higher.

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 fuel pumps
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
Weight 1 177kg / 390 lbs
Dual alternators 14V 70 Amp or 28V 40A
¹ Dry engine, PSRU weight including starter, main alternator included

unique rotary engine