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