KUR-400 Technical data
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TECHNICAL DATA Unmanned Aerial Vehicle Rotary wing, 4 rotors Maximum TakeOff Mass (MTOM) 4 Battery type Lithium polymer 6 cells Maximum payload mass 1 Frame mass (no batteries) 1.8 Radio Control, telemetry and Ground Control Station Empty takeoff mass (no payload) 3 Screen 15.46 in 1080p capacitive touch screen Transport case mass 3 Telemetry and GCS protocol MAVLink Material Polished carbon fiber Maximum dimensions (no propellers) 470 x 470 x 275 Connectivity micro USB, Bluetooth / WIFI / GPS / 2.4G Maximum dimensions (with propellers) 800 x 800 x 275 Battery Built-in 4950 mAh LiPo Transport case dimensions 350 x 250 x 490

TECHNICAL DATA On-board sensors FCU Pixhawk 2.1 The Cube Orange Maximum horizontal speed 20 m/s Minimal ratio: (Max Thrust)/(Max Weight) 2.23 IMU Redundant triple IMU unit, temperature controlled and vibration isolated Type • Optical sensors • Thermal sensors • Multispectral sensors • Active/Passive payloads • Other kinds Maximum ratio: (Max Thrust)/(Min Weight) 2.97 Flight Time 34 min. (no payload) 27 min. (0.5 kg payload) 24 min. (1 kg payload) Video Downlink Double video stream 1080p 30/60 fps Ground measurement Soon available Video transmission range CE 12 km, FCC 20 km Maximum vertical...