PURPOSE AND MAIN TASKS
The system is designed for reconnaissance with changeable payloads at any day time and information support of the units of armed forces, inclusive of: -
imagery intelligence;
-
radar intelligence;
-
electromagnetic intelligence.
The system is based upon the modular-design with the open architecture and the UAV equipment and target instrumentation composition, the ground component composition may vary with due account for usage conditions.
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MAIN PERFORMANCE SPECIFICATIONS
UAV system deployment time, h |
4 |
Runway length, m |
900 |
Combat crew size, inclusive of:
information control and processing station, persons
takeoff and landing control module, persons
ground technical support station, persons
operating personnel, persons |
25
8 (2 shifts x 4 persons)
2 (2 shifts x 1 person)
10
5 |
Wing span, m |
16 |
Height, m |
3 |
Length, m |
8 |
Maximum takeoff weight, kg |
1 000 |
Fuel weight, kg |
350 |
Standard payload weight, kg
maximum, kg |
60
200 |
Horizontal flight speed, km/h |
120–200 |
Takeoff speed, km/h |
120 |
Landing speed, km/h |
110 |
Flight time (maximum under standard payload), h |
24 |
Maximum flight altitude, m |
7 500 |
Line of sight radius, km |
250 |
UAV-relay radius, km |
300 |
Power unit (reciprocating internal combustion engine), HP |
115 |
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