Product overview
The C-200 is a heavy-lift multirotor for mountain engineering and transport, built with four axes and eight propellers. It measures 205 × 195 × 90 cm deployed and 150 × 135 × 90 cm stowed, with an aircraft weight of 105 kg excluding batteries. Maximum payload is 200 kg, standard payload is 160 kg, and maximum takeoff weight is 440 kg. A weighing system is supplied as standard equipment. Cruising speed is 10 m/s, with a maximum horizontal speed of 20 m/s and maximum ascent/descent speed of 8 m/s.
The four-battery configuration has an energy capacity of at least 14 kWh. Flight endurance is 25 minutes unloaded and 9 minutes with a 150 kg load. Charging takes 10 minutes per set with four fast chargers, within a charging ambient temperature range of -10°C to 45°C. The C-200 operates at temperatures from -20°C to 55°C and has a Level 7 wind resistance rating. Communication distance is 30 km with line of sight and no interference, while the flight ceiling is ≤3000 m.
