projectperformance indexprojectperformance indexAircraft categoryVertical takeoff and landing composite wing unmanned aerial vehicledynamical system60cc-80cc gasoline engineEmpty weight≤6KgPractical ceiling﹥5000mAircraft materialFull composite material formed by hot pressing canFlight speed70-160k
project | performance index | project | performance index |
Aircraft category | Vertical takeoff and landing composite wing unmanned aerial vehicle | dynamical system | 60cc-80cc gasoline engine |
Empty weight | ≤6Kg | Practical ceiling | ﹥5000m |
Aircraft material | Full composite material formed by hot pressing can | Flight speed | 70-160km/h |
Landing and takeoff methods | VTOL | cruising speed | 100-150km/h |
Maximum takeoff weight | 25kg | Wind resistance capability (facing wind) | Level 6 |
load | ≤5kg | endurance | 1-5h(depending on the fuel load) |
External dimensions | The aircraft has a length of 2.2m, a wingspan of 3.5m, a height of 0.41m, a transverse wheelbase of 0.98m, and a longitudinal wheelbase of 0.96m 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 |