ZK600-M Military Unmanned Helicopter System

Обзор

ZK600-M drone is a coaxial twin-rotor unmanned helicopter with vertical lift, stable hover, ultra -low ground-skimming and other dynamic characteristics. It can also accomplish fixed-point ultra long time stable flight, large attitude, large Angle dynamic flight and exploration flight of threatening targets. While effectively saving manpower costs and reducing combatant casualties, it can also reduce political risk. ZK600-M adopts terrain tracking technology, wireless control technology and swarm network adaptive to match technology, providing effective support for the whole process of operations and combat forces under certain geographical and relative airspace conditions. It also can carry out fire strike, communication relay, electronic interference, intelligence reconnaissance and other missions under all-weather complex weather conditions. ZK600-M is characterized by long endurance, heavy load, high speed and high comprehensive efficiency, and can be used for a variety of military missions by carrying photoelectric reconnaissance equipment and airborne weapon equipment. ZK600-M can provide communication connection for different army cooperative operations with the equipment of communication relay device and to expand the coverage of communications and the mission radius of unmanned helicopters. Intelligence Reconnaissance ZK600-M has all-weather integrated reconnaissance capability and efficient and diverse reconnaissance methods. Using intelligence collection equipment, can penetrate enemy hinterland, can also be slow or hovering flight stare, the enemy on the battlefield of various kinds of information (e.g., data communications, high-definition pictures, television image, infrared night vision image, etc.) are collected, and through the reliable and confidential communications channel distribution and transmission, provide real-time intelligence support for the troops, to satisfy the tactical battlefield surveillance, target reconnaissance mission requirements.

Технические характеристики

Основные характеристики: Autonomy fully autonomous take-off, waypoint navigation and landing, Navigation redundant INS and GPS (BD optional), Engine piston engine, No. 95 gasoline . The power of 125 HP, Data/video link fully digitized, compressed video, Mission radius 350 km, Cruising speed 150 km/h, Air weight 330 kg, Max take-off weight 600 kg, Mission payload > 200 kg, Endurance 5 hours, Dimensions 7.2 m long 1.65 meters wide 2.77 meters high, Rotor diameter 6.5 m, Number of blades 2 2, Use limit 8000 m.

Технические характеристики

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