The unique design features of the SDO 50V2 provide a superior payload capacity, prolonged endurance, stable flight patterns and a high degree of safety features.
An integrated autopilot system allows autonomous take-off and landing procedures as well as autonomous flight patterns following pre-set trajectories.
|Rotor system||Flettner Double Rotor System|
|Rotor diameter||2 x 2,80m|
|Engine||Turbine Jet Engine|
|Fuel||Diesel / Jet A1|
|Dimensions L x W x H||2.32m x 0.70m x 0.98m|
|Empty weight||36 Kg|
|Payload||Max 50 Kg|
|Max. fuel capacity||Main tank 13 lt. + add. tanks (2 x 4 lt.) (2 x 7 lt.) (2 x 13 lt.)|
|Service ceiling||up to 10'000 feet MSL/400m AGL (ISA conditions)|
|Max. Airspeed||15 m/s|
All performance specifications about the SDO 50V2 and for the GCS depend
on payload configuration!
E.g. with Leica RCD30 payload you have other specs for altitude and airspeed!