Materials | Carbon fiber, glass fiber, kevlar, PVC |
Landing gear position | Below the rotor arm |
Location of the task room | Directly below the center of gravity |
Structural weight | Approximately 3450g (including structure and installment payment) |
Maximum takeoff weight | 13.5kg |
Maximum payload | 3 kilograms (standard: 1.2 kilograms) |
Wing area | Approximately 52dm2 |
Wing loading | Approximately 240g/dm 2@12.5kg |
Endurance | 3.67H(220min)@1kg load(measured near sea level, no wind.) |
Maximum control distance | Manual remote control/0.5-1km left and right ground station km-30km / 5 |
Standard speed | 20m/s@12.5kg(suggested speed in areas.21m / s@12.5kg) |
Maximum endurance speed | 93.6 km/h (26 m/s) |
Standard battery | 22.8v/25Ah*2(45.6V) |
Maximum speed | 122 kilometers/hour (about 34 meters/second) |
Stall speed | 15.5m/s@12.5kg (16m/s@roll 25°/ pitch 15°) |
Minimum turning radius | 120m@19m/s (bank angle 18°) (safe turn the radius should not be smaller than 200 meters on the plateau) |
Maximum flight altitude | Altitude 4800 meters |
Fixed wing wind resistance | Not less than a level 6 wind (level 7 gusts) |
Maximum drag rotor aircraft takeoff capability and landing mode | A wind speed of not less than force 4 (force 6 gusts) |
Drone operating environment | -20℃~45℃; flying in light rain; safe operation time greater than 10min) |
Emergency operation time of the rotor | Rotor independent power battery (non-standard power configuration) greater than 6.5 minutes |
Takeoff/Landing | Vertical direction |
Hanging propeller blades | 16/17 inches |
Fixed wing tail propeller blade | 15 to 18 inches |
Fixed wing***thrust-to-weight ratio | 0.6 (standard) |
High-altitude performance | Yes |
Standard load weight | About 11.5 kilograms |
Safe voltage method during descent | Greater than 44V (Ge high pressure battery) |
Wing installation angle | 2° |
Number of pitot tubes installed | 2 (Standard: single hole in the pitot tube) |
Can this system be heated? Replace the power battery pack? | 22.8v/25Ah*2(45.6V) |
Maximum speed | Yes |
Ground control | The flight control system supports the use of composite wings to control this type of unmanned aerial vehicle system. |
"Solid-state" battery duration | 4.35 hours (261 minutes) @ no load (measured nearby) sea level, no wind. |