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Unmanned Aerial System

Unmanned Airs system It consists of an aerial vehicle and ground segment. The control is performed by Pilot Control Software. It is powered by an internal combustion engine. Takeoff is performed via pneumatic catapult.
Unmanned Aerial System is a state of the art system. It is suitable for most complex missions including:

• Border control
• Reconnaissance/observation
• Aerial photography
• Geophysical prospecting
• Disaster monitoring
• Coastguard service
• Radiation probing or sampling
• Day/night reconnaissance
• Battlefield monitoring
• Target positioning
• Signals intelligence
• Battlefield damage and casualty assessment

UAV is intended for medium ranged active tactical reconnaissance unmanned class, it is equipped with reconnaissance systems and its direct aim is the online monitoring of the battlefield, to ascertain exact coordinates of warlike equipment and the opponent’s troops. The aircraft can also be used for civilian purposes. During landing the aircraft on the ground, parachute and air bag is opening for easing the excessive damage.
After aircraft landing automatically opens parachute, system can be used in any climate conditions and during temperature gradation.
UAV body is designed with composite materials. Aircraft has two flight regime: with radio control in online regime and automatically in complete radio silence.
After its suppression flight continuous in free-running mode. Reconnaissance optical machinery are installed in front part of the aircraft.
On special gyro stabilization platform, in two flatness of day/night vision there is installed a movable camera.
For photography the aircraft is equipped with photographic camera. Power plant of the aircraft is an inter burning engine with the power of 3,5 hr/p.
In unmanned air system complete set includes radio control antenna, pneumatic launcher mechanism and computer management system.

CC BY 4.0 This work is licensed under a Creative Commons Attribution 4.0 International License.

Length
1960 mm
Wingspan
3075 mm
Weight
12 kg
Fuel weight
3 Litre
Minimum speed
60 km/h
Maximum speed
160 km/h
Combat range
150 km
Flight altitude
100-3000 m
Flight time
8 h
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System
Unmanned Aerial System