4.5 hour
Flight time
≥380 km
Range
10 kg
Load capacity（sea level）
140 km/h
Max cruise speed
﹥7000 m
Practical ceiling
≥5000 m
Practical ceiling
Unique patent technology of retractable rotors
E6 uses the unique patent technology of retractable rotor,enable the UAV fold the rotors after vertical take off to decrease the resistance of cruise flight. It could reduce the resistance to 50% compared with the unfold rotors UAV.
Rotor deploy
Rotor folded
Fearless of complex environment.
Anti light rain，operate normally in temperature of -20℃-55℃， anti 13m/s wind in vertical take off and land, 28m/s wind in cruise status.
Multiple loads, flexible configuration
Can carry dual-light pods, tilt cameras, shouters, LIDAR, dropping boxes and other loads to meet the needs of a variety of scenarios
Photoelectric pod
3 axis stabilization, 30x visible zoom/IR, tracking flight, target recognition
Lidar
Large height difference measurement, high point cloud density, more than 150 km in one take-off and landing operation
tilt cameras
210 million pixel five-lens tilt photography, 5 cm accuracy of a landing and takeoff operation area of more than 40 square kilometers
Emergency delivery
Optical pod emergency search and rescue, emergency delivery of food, medicine and life-saving substances to the target
Shouters
Shouting in the air to evacuate stranded people or evacuate nearby people
Reliable and stable VTX
Optional 30km, 50km, 100km VTX, to meet the needs of long-distance operations, built-in 4G/5G transmission module, support real-time video sharing
Planning the route, one click to takeoff
One-click takeoff by planning route to execute the mission without manual intervention. Support real-time mission change and manual takeover in case of emergency
Multiple redundancy, safe and reliable
Dual power system
When the fixed-wing mode is out of control, the aircraft can enter the multi-rotor mode; if the multi-rotor mode is out of control, the aircraft can enter the gliding mode.
Auto return
Support return automatically when low battery, abnormal aircraft attitude or trajectory deviation cannot be recovered.
Emergency Landing
The aircraft can be set up with more than 1,000 emergency landing points, and the aircraft can land vertically with multi-rotor or glide to the emergency landing point or designated landing point with fixed wing when abnormal.
System self-test
The aircraft will not be able to take off if there is any abnormality in the self-test before takeoff or if the air frame components are monitored to reach their design life.
Quick disassembly and easy to operate
Quick disassembly structure design, two people can complete the unpacking to take-off in 2 minutes.
Specifications
| Project | Paramete |
|---|---|
| Wingspan | 3.8m |
| length | 2.3m |
| practical take off weight | 36kg |
| Mac load capacity | 10kg(sea level) |
| Flight time/range (no wind，altitude 300m) |
>4.5h（1kg load and battery configuration）/>380km >1.5h（10kgload and battery configuration）/>150km |
| Box size | 2m*0.6m*0.6m |
| Economy cruise speed | 75-94km/h |
| Max cruise speed | ＞140km/h |
| Max practical ceiling | 5000m |
| 30km、50km、100km（optional） | 30km、50km、100km（optional） |
| Anti-wind capacity | （Take off and land） 15m/s （cruise）25m/s |
| （Take off and land） 15m/s （cruise）25m/s | <2min，2 personnel operate |
| Accuracy of land and take off | 0.5m |
| Anti-rain capacity | Light rain |
| Operate temperature | -20~55℃ |
Product Video
