Operated by 1 or 2 persons depending on mission complexity. 15 min deployment from the stowed position. Automatic takeoff and landing. Flying the route with the possibility of changing the route during the mission. Radio silence mode flight. GPS, GLONASS, Galileo, BeiDou, QZSS and SBAS support.
Autonomous optical navigation system (optical flow). Autonomous flight and return to the home point without using satellite navigation systems. AES256 encrypted command line, reserved digital command line. Automatic targeting and automatic static and moving target tracking. Camera guided flight mode.
Advanced antenna complex with stepping motor antenna tracker. Ability to carry out the mission while driving. Improved analyst software workplace with augmented reality based on ArcGIS software. Integration with artillery fire control system.
|Materials||fiberglass, carbon fiber, kevlar;|
|Power unit||electric motor|
|Power supply||Li-Po/Li-ion batteries up to 42000 mAh|
|Range||up to 50 km|
|Flight time||more then 3 hours *|
|Cruise speed||65 km/h|
|Maximum speed||130 km/h|
|Flight distance||up to 200 km|
|Flight modes||semiautomatic guided, autonomous, camera guided mode|
|Practical ceiling||2500 m|
|Wind speed during mission||up to 15 m/s|
|Takeoff weight||5,5 kg|
|Two way launch||elastic or mechanical catapult|
|Two way landing||parachute (normal) or on landing skid|