Description
1. Body material: carbon fiber, glass fiber, Kevlar, PVC, aviation aluminum alloy, 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 9kg (including all structural parts and mounting parts)
5. Maximum takeoff weight: ≥33.5kg
6. Maximum load: ≥12kg(standard load :5kg)
7. Wing area: about 113dm2
8. Wing load: about 240g/dm2@28kg
9. Battery life: 160min@5kg; P 140 min @ 7 kg; P 70 min @ 10 kg; P 60 min @ 12 kg
10. Maximum control distance: manual control by remote control/about 0.5km-1km, ground station /5km-30km
11. Standard cruising speed: 22m/s (standard mounting) (recommended operating speed in mountainous areas: 23m/s)
12. Maximum cruising speed: 26m/s
13. Battery configuration: 22.8V /25Ah*4 (45.6V) @1kg-7kg; 22.8V /25Ah*2 (45.6V) @8kg-12kg
14. Never exceed speed: 122km/h (about 34m/s)
15. Stall speed: 19m/s@25.5kg (19m/ s@roll 25°/pitch 13°)
16. Minimum hovering radius: 180m@22m/s (safe turning radius of plateau is not less than 250m)
17. Maximum flat flight limit: to be updated
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 30min@ dual multifaceted system)
21. Rotor emergency operation time: not less than 4.5min (rotor battery independent power supply (non-standard power configuration))
Takeoff and landing mode: vertical takeoff and landing
23. Vertical power blade size: 26 inches (suggested)
24. Fixed wing tail push blade: 24 inches (recommended)
25. Maximum thrust-to-weight ratio of fixed wing: 0.56 (standard configuration)
26. Plateau performance: to be updated (plateau standard power configuration please contact the manufacturer to obtain)
Standard no-load takeoff weight: ≥20kg
28. Safety voltage when entering the 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
Payment & Security
