title: Mistral G-200
text: # Mistral G-200
  
  The Mistral G-200 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 twin-rotor, 2X3X654 cc (39.9 cu in) displacement, liquid-cooled, gasoline Wankel engine design, with an integral mechanical gearbox reduction drive with a reduction ratio of 2.82:1. It employs dual electronic ignition systems and produces 150 hp (112 kW).
  
  ## Specifications (G-200)
  
  Data from Tacke
  
  ### General characteristics
  
  * Type: Twin rotor Wankel aircraft engine
  * Displacement: 2X3X654 cc (39.9 cu in)
  * Dry weight: 132 kg (291.0 lb)
  
  ### Components
  
  * Fuel type: gasoline
  * Cooling system: liquid
  * Reduction gear: integral mechanical gearbox
  
  ### Performance
  
  * Power output: 150 hp (112 kW)
  