One task can fly
for 4 hours, the area
of operation is 30-60
square kilometers, voyage
Speed is 100 kilometers per hour,
wind resistance ability is 6-7 level.
obtained by KC2000
is verified by Wuhan
University professor team,
can fly in all kinds of
with an independent
system, it can effectively reduce
the field control point
workload at least 80%.
simple to operate only by 3
steps- catapult-assisted takeoff,
intelligent flight control,
spot parachute landing
With the powerful rear 30cc engine,
2.8L fuel tank to fill a cruise 450Km.
The carbon fiber armor design of fuselage reduce the weight
while increase of the main structure strength.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.
The unique aerodynamic configuration gives
aircraft with the maximum lift-drag ratio .
It greatly improve the aircraft's load capacity and endurance.
The aircraft nose using of special sponge
can effectively absorb the kinetic energy
of landing and increase the buffer.
Using the parachute’s own weight
to ensure the success rate of opening and can
also protect the aircraft equipment will not be
damage by the impact of landing wave.
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.
|ceiling height||3000m（High altitude aircraft need OEM）|
|size of load cabin||0.16m*0.20m*0.16m|
|duration of flight||4小时|
|maximum wind resistance ability||6级|
|camera capable to carry||Full-frame digital SLR
resolution 36 million pixe
|typical operation efficiency||1:500 a sorties 10 square kilometers
1:1000 a sorties 40 square kilometers