Product overview
The C-180 heavy-lift multirotor is designed for mountain engineering and transport. Its four-axis, eight-propeller structure measures 175 × 175 × 87 cm when deployed and 130 × 120 × 87 cm when stowed. Aircraft weight excluding batteries is 80 kg, with a standard payload of 150 kg, a maximum payload of 180 kg and a maximum takeoff weight of 320 kg. The aircraft uses four batteries with an energy capacity of ≥8 kWh. Landing-assistance radar and front and rear obstacle-avoidance radar are optional.
Fast-charge batteries provide 25 minutes of unloaded endurance or 9 minutes with a 150 kg payload; slow-charge batteries provide 45 minutes unloaded or 20 minutes with the same payload. Charging takes 10 minutes per set with four fast chargers, or 1.5 hours per set with four slow chargers. Charging ambient temperature is -10°C to 45°C, and aircraft operating temperature is -20°C to 55°C. Cruising speed is 10 m/s, maximum horizontal speed is 20 m/s and maximum ascent and descent speed is 8 m/s. Wind resistance is Level 7, service ceiling is ≤3000 m, and communication distance is 30 km with interference-free line of sight.
