Climb ratio: 2000 ft/min | 10 m/s Glide ratio: 15:1
Max. take off weight: 472 kg | 1041 lbs Empty weight: 295 kg | 650 lbs
Engine: 2 x Hirth F23ES 40 hp Fuel consumption: 14 lit/h
Other aircraft information: Text and photo from: http://www.aeronix.fr/
Three-axis ULM, two-seater side by side, with median wing, twin-engine
push-pull, canard formula, tricycle landing gear, composites construction
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