Project Description
2 seats (including the pilot)
maximum takeoff weight: 622 kg / empty weight: 387 kg
maximum range: 463 Km
maximum speed: 189 km/h / cruising speed: 176 km/h
maximum altitude: 4662 m
engine: Lycoming O-360-J2A
average fuel consumption: 30 l/h
main rotor diameter: 8 m
height: 3 m / length: 10 m
