
Key Differentials
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Ready to fly in 15 minutes.
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Only a 2-person crew is needed.
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Easy to be transported in the back of a SUV.
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Easy sensor integration.
Specifications
Rotary system: Flettner double rotor system (4 blades)
Rotor diameter:2 x 2,82 m
Engine:High performance turbine
Fuel:JET A1
Fuel consumption:Approx. 15 L/hour
Dimension l/w/h:2,32 m x 0,7 m x 0,92 m
Empty weight: 42 kg
Max payload:45 kg
MTOW:87 kg
Max fuel capacity:Main tank 13 L; additional tanks available for longer flying time (2 x 4 L; 2 x 7 L; 2 x 13 L)
Max flight time:Up to 2,5 hours
Max service ceiling:Up to 3000 m AMSL
Max airspeed:20 m/s (72 km/h)
Note: All performance data about the SDO 50 V2 and the GCS are subject to change, depending on final payload configuration.