The very urbane fighter
Dedicated to personal inter-urban mobility 2-seater tandem STOL airplane Adapted to small airfields For leisure flights, pilot training and other uses (air taxi, surveillance, data collection…)
Technical parameters
Optimised aerodynamics for short take-off & landing (STOL) and high cruise speed Airframe built in natural composite materials Hydrogen propulsion compatible with sustainable aviation fuels (SAF)
Technical parameters
Maximum power | 100 kW | 135 hp | |
| Range | 740 km | 400 NM | |
| Cruise speed | 250 km/h | 135 kt | |
| Take-off & landing distance | < 200 m | < 650 ft | |
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| Maximum take-off weight (MTOW) | 700 kg | 1540 lb | |
| Useful load | 250 kg | 550 lb | |
| Empty weight (SAF) | 450 kg | 990 lb | |
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| Lenght | 7.7 m | 25 ft | |
| Wingspan | 11.5 m | 38 ft |