High Speed Target Drone CH-200A

概要

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. 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. 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. 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. 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 The maximum horizontal velocity at sea level：210m/s Maximum takeoff weight (including booster)：85kg Radar reflection area ： 2. Main parameters

技術仕様

主な仕様： 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 2. Main parameters、Length 3020 mm、Fuselage diameter 260mm、Wingspan 1615 mm、Wing area 0.53m²。

技術仕様

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