Fixed-wing UAV KWT-F360-E/H

instrumentaerial photographymonitoring

KWT-F360-E/H vertical take-off and landing fixed wing, adopting hybrid power with quadrotor + propeller. This model combines the characteristics of long-endurance, high-speed and long-distance of fixed-wing UAVs and the vertical take-off and landing of rotor-wing drones. It does not require runway but only small space for take-off and landing, and can be operated smoothly on ship deck, narrow airspace, mountain, complex terrain and densely populated areas such as hills, jungles. This type of UAV has a wingspan of 3.6 meters and is divided into a pure electric version and a hybrid version. The electric version has a battery endurance time of 2 hours, and the hybrid version’s endurance up to 8 hours. The whole process of autonomous flight can be completed without operator intervention for cruise, flight state transition and vertical take-off and landing. No need for runway and flight assistance equipment, vertical take-off and landing, can be used anywhere One drone with multiple functions, suitable for various mission pods The fuselage is designed for quick release, adopts reliable electrical connection, plug and play, and the deployment and withdrawal time is less than 5 minutes. • Maximum level flying speed : 130km/h • Cruising speed : 70~100km/h • Lift limit : 5000m • Maximum endurance time : 2.5h (load 1kg, altitude below 1000m, 25 ℃) • Takeoff weight : 27kg • Maximum mission load : 5kg • Power system : Efficient brushless motor • Control method : Fully autonomous control • Wind resistance : 10.8~13.8 m/s • Takeoff and landing altitude : Maximum 4500m