title: Mistral G-300
text: # Mistral G-300
  
  The Mistral G-300 is a Swiss aircraft engine designed and produced by Mistral Engines of Geneva for use in light aircraft.
  
  ## Design and development
  
  The engine is a three-rotor, 3X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with a mechanical gearbox reduction drive. It employs dual electronic ignition systems and produces 300 hp (224 kW) at 2250 rpm.
  
  ## Applications
  
  * Seaflight Shearwater
  
  ## Specifications (G-300)
  
  Data from Tacke
  
  ### General characteristics
  
  * Type: Three rotor Wankel aircraft engine
  * Displacement: 3X3X654 cc (39.9 cu in)
  * Dry weight: 177 kg (390.2 lb)
  
  ### Components
  
  * Fuel type: gasoline
  * Cooling system: liquid
  * Reduction gear: mechanical gearbox
  
  ### Performance
  
  * Power output: 300 hp (224 kW)
  