1. Airframe, flight controller, motors, propellers, ESCs, onboard RTK navigation and positioning system;
2. Hybrid gas-electric quad-rotor VTOL fixed-wing aircraft;
3. Fuselage length: 3000 ± 5 mm;
4. Wingspan: 5500 ± 5 mm;
5. Maximum takeoff weight: 100 kg;
6. Maximum payload: 25 kg;
7. Fuel tank capacity: ≥ 24 L;
8. Rear pusher engine: DLE170;
9. Cruising speed: 28 m/s;
10. Maximum flight speed: 160 km/h;
11. Onboard 2.4G video and data link module;
12. Endurance: 240 minutes (with 25 kg payload);