The CH-200A high speed target drone was successfully developed and tested by a Chinese technology company in May 2019. The power system adopts YZS-D80 small turbojet engine independently developed by the company. The flight control system adopts digital flight control system, which can be pre-programmed and fully autonomous flight or manually controlled flight.
Flight control system
Used in a digital flight control system, including the flight control computer, inertial sensors (IMU), barometric altitude sensor, speed sensor, heading sensor, radio transponder, engine controller (ECU, TCU), GPS receiver, detonator action, control steering gear and other equipment, which can be preprogrammed fully autonomous flight, can also be manned flight.
Ground station control system
The computer of the ground station displays the flight track, heading, azimuth, speed, altitude, distance, attitude, power supply voltage and working state of the engine of the target aircraft in real time through the electronic map for the control of the ground operator.
Take-off launch system
Ground (or ship) zero-length launcher rocket is used to boost takeoff, and the booster rocket accelerates the target to 60m/s and then automatically falls off.
Recovery system
The target aircraft is equipped with parachute recovery system, including parachute recovery, parachute opening device, shock absorption airbag, etc., to ensure that the target aircraft can be recycled for multiple times.
Main features
The aerodynamic shape adopts the conventional layout of the single wing V tail and controls the target aircraft by oblique turning.
The fuselage is mainly made of composite materials and aluminum alloy materials, with a semi-hard shell structure.
Detailed technical specifications
1. Flight performance
Flight altitude：50-8200m
The maximum horizontal velocity at sea level：210m/s
Endurance： >30min
Maximum range：300km
The control radius：100km
Wind resistance： level 5
Maneuvering overload： 5G
Maximum takeoff weight (including booster)：85kg
Payload：5-10kg
Radar reflection area ：< 0.01㎡
Operating temperature： -50 -- +50°C
2. Main parameters
Length: 3020 mm
Fuselage diameter: 260mm
Wingspan: 1615 mm
Wing area:0.53m²
