SR100-B UAV
Product Details
Product Appearance
Product Description
The SR100-B composite-wing unmanned aerial vehicle has a maximum takeoff weight of 145 kg and adopts a reliability design with power redundancy of coaxial eight propellers. In the case of a single rotor failure, the unmanned aerial vehicle can still land safely, which improves the flight safety of the unmanned aerial vehicle. At the same time, it can be integrated with our company's lightweight and high-throughput airborne broadband satellite communication equipment, effectively breaking the geographical and distance limitations of traditional communication, enabling the unmanned aerial vehicle to easily carry out ultra-long-distance cross-regional operations.
Product Specifications
L/T method | VTOL |
Power | Oil-electric hybrid power |
Size | wingspan:6.12m Aircraft length:3.57m |
Max Payload Weight | 40kg |
Flight Endurance | 12h |
Endurance | 4~5h@30kg Payload |
7~9h@20kg Payload | |
Cruising speed | 100-110km/h |
Wind resistance ability | Level 6 |
Takeoff altitude | 4000m |
Max ceiling | 5500m |
Link type | Broadband satcom communication,30km/50km/100km Radio optional |
Features
l Be equipped with a high-throughput airborne satellite communication antenna, enabling the control radius of the UAV to be extended infinitely.
l The maximum payload can reach 40 kilograms, and the maximum flight endurance can reach 12 hours.
l It has a redundant design with eight coaxial propellers. In the situation where a single rotor fails, the UAV can still land safely.
