Single-flight upto 70
60km range,a flight
range of 5-8 square
section box to adjust
the route fixed-point
landing,survey data will
be safely returned.
upgrade based on the flight
experience in different types of
terrain.The final aerial survey data
was field verified by Wuhan Unive-
rsity professor and the
horizontal accuracy was
Fuselage with carbon fiber skeleton,the main structure is high strength,
light weightand not easy deformation.Fuselage surface with high temperature.
resistance ,toughness advantages by using honeycomb structure,Kevlar fiber
composite and aramid fiber which is equivalent to 5 times steel.
According to the civil aviation’s dual power back up standard to use dual motor.
Even though one of the motor broken, it can safely return.
Powerful and the maximum climb angle is more than 15 °
Ensure the normal operation in the six scale of wind force condition.
Special sponge protect the landing force point ,airborne equipment and data safety
and avoid wearing of the fuselage’s key parts.
Enhance the aerodynamic performance of the fuselage,energy saving and environmental
protection.This can greatlyprotect the safety of the transmission
device and ensure the steering servo control accuracy.
The whole machine is assembled with two screws ,simple structure ,convenient for
disassembly and assembly, easy to transport.
Using patent-guided ejection device take-off, no need remote control.
No need professional operators,automate operational processes. Simply complete the setup on the computer, automatically complete the route design, free to fly.
Opening parachute from bottom-cabin and backside landing design,high success rate of releasing parachute effectively protect the airborne equipment safety.
|driving mode||dual motor drive|
|size of load cabin||0.14m*0.12m*0.09m|
|maximum wind resistance ability||6级|
|duration of flight||70min|
|typical operation efficiency||1:500 a sorties 1.5 square kilometers
1:1000 a sorties 6 square kilometer