INDELA-I.N.SKY

Результат пошуку зображень за запитом "I.N. Sky (Indela UAV)"

INDELA-I.N.SKY is a rotary wing unmanned aerial vehicle, medium-range with the weight up to 140 kg. It is developed and produced by KB INDELA Ltd. Serial production has been set up since 2014.

INDELA-I.N.SKY is designed for monitoring of remote and extensive objects at long distances, intelligence and surveillance, search and detection of objects with the determination of exact geographic coordinates, recognition and auto tracking of moving objects, cargo delivery and payload release.

UAV INDELA-I.N.SKY is a part of multifunctional unmanned aircraft system INDELA-SKY. The helicopter is controlled via ground control station INDELA-GCS.

UAV INDELA-I.N.SKY fulfills vertical automatic takeoff and landing, automatic flight and return to the start point in case of communication loss.

Unmanned helicopter operates without a prepared runway, system deployment time is up to 15 min.

UAV flight has 4 modes: – Autonomous. UAV follows a specified route. At any moment during flight mission coordinates can be changed, added or deleted. – Mode “To the point”. UAV follows in automatic mode to the specified point. After the flight to the point the RPA mode is turned on. – Remotely piloted (RPA). This mode is used to study the territory/terrain; it is more flexible in comparison with waypoint navigation. – Mode “Home”. UAV automatic piloting mode to the takeoff point regardless of the previous mode.

Flight mission can have a route of various configuration and consist of more than 2000 intermediate points. It can be rapidly edited during the execution, including the change of the height and flight speed form point to point. INDELA-I.N.SKY is equipped with gyro-stabilized electro-optical system INDELA OGD-20HIR for monitoring, surveillance and intelligence. This system includes thermal imager, color camera, Laser rangefinder, video processor and inertial module. INDELA OGD-20HIR allows conducting of aerial photography, determining of range to target and receiving on monitors of the ground control station color, black and white and in infrared range video images in real time.

Electro-optical system allows detecting of moving target and its automatic tracking. Target “auto tracking” is performed at day and night hours. Construction of the UAV INDELA-I.N.SKY allows increasing of aircraft navigation equipment and installing different types of payloads (radiometer, gas analyzer, direction finding systems, detachable containers with cargo, rescue equipment, special-purpose equipment, etc.).

UAV INDELA-I.N.SKY can deliver cargo at exactly specified coordinates. Dosed release of the payload is possible.

Performance characteristics

Technical characteristics:

Length/height 3052/1346 mm
Main rotor diameter 3400 mm
Wheelbase 1180 mm
Takeoff weight 140 kg
Payload weight 25 kg
Standard fuel margin 29 kg
Takeoff capacity 26 kW
Fuel consumption 5-8 kg/h
Engine four cycle, rotary piston
Cooling system liquid

Flight characteristics:

Flight duration 5 h
Practical flight range 350 km
Cruise speed near the ground 75 km/h
Static ceiling 1500 m
Max. allowable wind speed during takeoff 37 km/h
Operating temperature -40…+55 °С

 

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