projectperformance indexprojectperformance indexAircraft categoryVertical takeoff and landing composite wing UAVdynamical system110cc-180cc gasoline engineEmpty weight<14KgPractical ceiling5000mAircraft materialFull composite material formed by hot pressing canFlight speed90-190km/hLanding and take
project | performance index | project | performance index |
Aircraft category | Vertical takeoff and landing composite wing UAV | dynamical system | 110cc-180cc gasoline engine |
Empty weight | <14Kg | Practical ceiling | 5000m |
Aircraft material | Full composite material formed by hot pressing can | Flight speed | 90-190km/h |
Landing and takeoff methods | VTOL | cruising speed | 100-160km/h |
Maximum takeoff weight | 55kg | Wind resistance capability (facing wind) | Level 6 |
load | 2-10kg | endurance | 1-10h(depending on the fuel load) |
External dimensions | The aircraft has a length of 3.45m, a wingspan of 5m, a height of 0.72m, a transverse wheelbase of 1.56m, and a longitudinal wheelbase of 1.3m Body: carbon fiber composite PVC foam sandwich Wing: carbon fiber composite PVC foam sandwich Vertical takeoff and landing arm: 3K carbon fiber Landing gear: carbon fiber Fuel tank: Soft fuel tank |