projectperformance indexprojectperformance indexAircraft categoryFixed wing UAVdynamical system120cc-170cc engineEmpty weight<20Kg(Oil free, battery free)Practical ceiling6000mAircraft materialFull composite material formed by hot pressing canFlight speed90-150km/hLanding and takeoff methodsROLLcru
project | performance index | project | performance index |
Aircraft category | Fixed wing UAV | dynamical system | 120cc-170cc engine |
Empty weight | <20Kg(Oil free, battery free) | Practical ceiling | 6000m |
Aircraft material | Full composite material formed by hot pressing can | Flight speed | 90-150km/h |
Landing and takeoff methods | ROLL | cruising speed | 100-120km/h |
Maximum takeoff weight | 60kg | Maximum takeoff weight | Level 6 |
load | ≥30kg(Oil containing) | endurance | 1-20h(depending on the fuel load) |
External dimensions | The fuselage is 2.5m long, with a wingspan of 3.8m and a height of 0.8m Body: carbon fiber, glass fiber composite PVC foam sandwich Wing: carbon fiber, Kevlar composite PVC foam sandwich Landing gear: aluminum alloy&carbon fiber Fuel tank: Kevlar fuel tank |