projectperformance indexprojectperformance indexAircraft categoryVertical takeoff and landing composite wing unmanned aerial vehicledynamical systemV605KV210+AT7215KV220Empty weight<6kgCruise batteryCustomized 12S batteryAircraft materialFull composite material formed by hot pressing canFlight spee
project | performance index | project | performance index |
Aircraft category | Vertical takeoff and landing composite wing unmanned aerial vehicle | dynamical system | V605KV210+AT7215KV220 |
Empty weight | <6kg | Cruise battery | Customized 12S battery |
Aircraft material | Full composite material formed by hot pressing can | Flight speed | 80-120km/h |
Landing and takeoff methods | VTOL | cruising speed | 85-95km/h |
Maximum takeoff weight | 30kg | Wind resistance | Level 6 (facing wind) |
load | <10kg | endurance | >260min(2.5kg counterweight) |
External dimensions | Wingspan 3.6m, Captain 1.82m (with airspeed tube 1.89m), belly clearance>160mm Body: carbon fiber composite PVC foam sandwich Wing: Kevlar composite PVC foam sandwich Vertical takeoff and landing arm: 3K carbon fiber | ||
Flight data | Takeoff weight: 26kg, mounting: 2.5kg Cruise speed: 90km/h, cruise time>260min, range 366km The above data was tested at an altitude of 10m, a flight altitude of 150m, and a wind speed of 3.4-7.0m/s | ||
Takeoff weight: 26.5kg, payload: 5kg Cruise speed: 90km/h, cruise time>200min, range 283km The above data was tested at an altitude of 10m, a flight altitude of 150m, and a wind speed of 3.4-7.0m/s | |||
Takeoff weight: 32kg, payload: 10kg Cruise speed: 90km/h, cruise time>120min, range 196km The above data was tested at an altitude of 10m, a flight altitude of 150m, and a wind speed of 3.4-7.0m/s | |||
Dimensions | 1870*520*560mm;0.55m3(≤65kg) |