C20 Drone 100 kg electric vertical take-off and landing fixed-wing UAV
The C20 UAV is a 100 kg electric vertical take-off and landing fixed-wing UAV. It adopts a unique overall configuration design. It is composed of wings and four power modules. Each power module consists of 4 vertical lifts. The rotor is composed of a front pull rotor. The power modules of the same aircraft can be interchanged, and the power modules between different aircrafts can also be interchanged to improve attendance; it has no fuselage, and can be adapted to different sizes of mounts. For logistics and transportation needs, it is also designed with throwing and dropping functions; altitude 5000 meters plateau, can carry 20 kg load for 100 kilometers, the maximum load capacity in plain area is 40 kg; each aircraft has 16 hanging rotors and 4 forward pull rotors , With good safety redundancy and wind resistance.
Item | parameters |
Wingspan | 6 meters |
Length | 3.3 meters |
Maximum take-off weight | 100 kg (plain), 80 kg (5000 meters above sea level) |
Maximum load capacity | 40 kg (at sea level), 20 kg (5000 meters above sea level) |
Endurance time/range | (20 kg load) 1 hour/100 kilometers |
Packing size | 2.6m*0.67m*0.67m, 2.73m*0.62m*0.32m |
Economic cruising speed | 70~100km/h |
Practical vertical take-off altitude of 5000 meters | |
Practical ceiling | >7000m |
Data link range | 30 kilometers data transmission is standard, and the maximum distance can reach 120 kilometers according to demand. |
Wind resistance ability for take-off and landing | >12m/s |
Homework unfolding/folding time | 5 minutes for two persons, 10 minutes for one person |
Takeoff and landing positioning accuracy | 0.5 meters |
Rain | resistance |
Working environment temperature | -20~55℃ |
Battery configuration | Each power module is powered by two 25000mAh batteries in series |