|Key geometric characteristics|
|Span of wings||mm||2800|
|Standard fuel margin||ml||8200|
|Basic flight characteristics|
|Range of horizontal flight speed||km/h||100-400|
|Flight attitude range||m||50-3500|
|Practical flight length||km||110|
|Communication range (within line of sight)||km||100|
|Control system||Autonomous navigation, automatic performance of the flight task|
Ground control facilities are designed to ensure efficient change of target flight task as well as receipt, display and documenting of telemetric and external trajectory information. Means of ground servicing include ground automated control system and technological equipment complex. These means are intended to carry out checkouts of the target’s on-board systems as well as its preparation to launch and reutilization. Major flight modes of «BERKUT» airborne target are: takeoff, climb, horizontal flight, descent, turn, swooping, pitching, low-flying, emergency parachute landing, landing.
The target is designed for multipurpose utilization and can be used up to 50 times. Autonomous and radio-adjusted methods of performing the flight task can be used.
The complex consists of:
airborne target vehicle «BERKUT», including radar imitator of reflected «RIZ» signal
ground control station INDELA-GCS
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