Aerokon INSPECTOR-301 Multipurpose UAV
UAVs "Inspector-301" developed in Zhukovsky CJSC "Aerokon" chief designer Alexander Kornushenko. Purpose apparatus is the implementation of the clock monitoring of the Earth's surface in a wide range of weather conditions. UAVs can be used for the benefit of various departments to collect and transmit information about the monitored object in real time. The distinctive features of the complex include a longer duration and range, meteonezavisimost, buoyancy and maintainability UAVs.
"Inspector 301" - the heaviest of drone, part of a series of three mikroBLA that have been developed now "Aerokon." The device weighs six kilograms. Running is made of rubber-mechanical catapult. UAVs can conduct a flight duration of up to 2 hours and staffed with a payload of up to 1 kg.
The complex consists of two UAVs "Inspector-301", a ground control station, means of transportation and management. On the deployment of complex leaves 10 minutes. The flight time, depending on the mode selected to range from 45 120 min. Height practical ceiling - 4000 m. Airspeed - 55-150 km / h, operating altitude - 50-500 m.
Payload is presented in the form of a fixed low-level camera forward-looking, stable in pitch and roll, cameras with different focal lengths and a digital camera with a resolution of 10 megapixels. Additionally, the machine can be equipped with infrared cameras and sensors the presence of gas.
Takeoff UAV performed mechanical catapult, landing on an aircraft can type "on its belly" or by parachute in semiautomatic or automatic mode. For takeoff and landing pad sizes required 75h75 m (along the perimeter allowed the location shelterbelts consisting of medium-trees).
The complex unmanned aerial surveillance "Inspector 301" in 2009 year expressed interest interregional grid companies. Besides them, the purchase represented complexes interested Emergencies Ministry and many other organizations and agencies.
Aerokon INSPECTOR-301 multipurpose UAV. Characteristics:
|engine's type||1 ED|
|Power, hp||1 x|
|Cruising speed, km / h||55-150|
|Practical range, km||200|
|Radius of action, km|
|The flight duration, min||45-120|
|Operating altitude, m||50-500|
|Practical ceiling, m||4000|
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