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