Flight Model

1. Body material: carbon fiber, glass fiber, Kevlar, PVC, etc

2. Landing gear mounting position: below the rotor rod

3. Mission bay position: directly below the center of gravity of the aircraft

4. Weight of structure: about 3450g (including all structural parts and mounting parts)

5. Maximum take-off weight: 13.5kg

6. Maximum load: 3kg(standard load :1.2kg)

7. Wing area: about 52dm2

8. Wing load: about 240g/dm2@12.5kg

9. Endurance: 3.67h (220min) @1kg load (measured near sea level in calm wind)

10. Maximum control distance: manual control by remote control/about 0.5km-1km, ground station /5km-30km

11. Standard cruising speed: 20m/s@12.5kg (recommended mountain operation speed 21m/s@12.5kg)

12. Maximum cruising speed: 93.6km/h (26m/s)

13. Standard battery configuration: 22.8V /25Ah*2 (45.6V)

14. Never exceed speed: 122km/h (about 34m/s)

15. Stall speed: 15.5m/s@12.5kg (16m/ s@roll 25°/pitch 15°)

16. Minimum hovering radius: 120m@19m/s (roll 18°) (safe turning radius at plateau is not less than 200m)

17. Maximum flat flight limit: altitude 4800m

18. Wind resistance of fixed wing mode: no less than force 6 wind (gust force 7)

19. Maximum wind resistance of rotorcraft takeoff and landing mode: no less than force 4 wind (gust force 6)

20. Uav operating environment: -20℃~45℃; Can fly in light rain (safe running time is more than 10min)

21. Rotor emergency operation time: not less than 6.5min (rotor battery independent power supply (non-standard power configuration))

Takeoff and landing mode: vertical takeoff and landing

23. Vertical power blade size: 16/17 inches (recommended)

24. Fixed wing tail push blade: 15~18 inches (recommended)

25. Maximum thrust to weight ratio of fixed wing: 0.6 (standard configuration)

26. Plateau performance: Passed the plateau test (please contact the manufacturer for plateau standard power configuration)

27. Standard no-load takeoff weight: approx. 11.5kg

28. Safety voltage when entering landing course: not less than 44V(Grignard high voltage battery)

Mounting Angle of wing: 2°

30. Number of pitot tube installation: 2 (single pitot tube opening is standard)

31. Does the system support continuous power replacement of power battery pack? Yes (non-standard)

32. Flight control support type: flight control supporting composite wing control can be used in this uav system