Maximum takeoff weight, kg | 7.0+(-)10% |
Payload weight, kg | 1 |
Wing span, m | 1.84+(-)10% |
Flight speed range, km/h | 65–100 |
Flight time, h | not more than 2 |
Radio-link communication range, km | 40 |
Above sea-level flight altitude, m | 4000 |
Ground surface operating temperature range, °C | between −30°C to +40°C |
Assigned life time, h | not less than 100 |
Engine type | electric |
Takeoff / landing technique | catapult / parachute |
System composition | 2 UAVs, GCS, GSE, SPTA |
Combat crew, persons | 2 |