Unmanned Aircraft Systems


The V-3M-C is standard conventional take-off and landing (CTOL) configuration of the UAV in the form of a flying wing, 2.2 m wing span and maximum take-off mass of (MTOW) 5.5 kg of which 1.5 kg is the maximum payload. The battery system is designed to give the aircraft the autonomy of 3 hours at 60 km / h cruising speed, with a top speed of 140 km / h and 100 km range, or 200 km without return to launch point. It is suitable for long range missions (Type A). The take-off of the aircraft itself can be manual with a bungy cord or autonomous with a catapult with predefined instructions in the system. The advantage of autonomous take-offs is that the pilot or person in charge of operating the aircraft and catapult may not be in close proximity to the system. Even with bungy cord launch the aircraft will start the motor and take off automatically once it has been pulled by a cord. The landing can be done automatically by parachute system or landing in the net.


  • ‘Real-Time’ HD Video Stream up to 50 km
  • Telemetry, controls and FPV Stream up to 100 km
  • 40 km^2 coverage
  • Endurance up to 3h
  • Max. speed – 130 km/h (70 kt)
  • Stall speed – 35 km/h (19 kt)
  • Empty weight – 1.6 kg (3.5 lbs)

Long range  with predefined flight mission flight.

  • Up to 3 hours of flight time with cruise speed of 70 km/h
  • Geo-mapping and video surveillance, package drop off…..
  • Fully autonomous and remotely controlled
  • Real-time video feed to the ground station
  • Newly issued regulatory framework on BVLoS, such as USA FAA Part 107 and EU EASA rules, as well as local laws
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The V-3M-V is the configuration of the flying with two additional modules with two rotors each to be plugged in between the hull and the wings which enable the aircraft to have vertical takeoff and landing. Once the aircraft is in the air safely above ground the rear propeller will start and the aircraft will transition to regular straight flight with lift and the vertical rotors will stop and they will be positioned in an direction of the flight so that they do not cause more drag. The wing span is 2.45 m, maximum take-off mass is 6.5 kg of which 1 kg is payload. The battery system is designed to have maximum flight duration of 1.5 h. The cruise speed is 70 km/h and maximum flight speed of the V-3M-V is 90 km / h. It is suitable for taking off and landing in inaccessible terrains, delivering packages to the point delivery and for other medium-range missions 20-30 km (mission type B). Due to the modularity of the complete system, payload itself is variable depending on the need.


  • ‘Real-Time’ HD Video Stream up to 50 km
  • Telemetry, controls and FPV Stream up to 100 km
  • 20 km^2 coverage
  • Endurance up to 1.5h
  • Max. speed – 100 km/h (54 kt)
  • Stall speed – N/A
  • Empty weight – 3 kg (4.5 lbs)
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Short or vertical take off.

Up to hour flight time with possible transitions to hovering

Predefined flight path and automatic video search and rescue, emergency air delivery to exact point, or geo mapping


The V-3M-X8 is the configuration of the aircraft with two additional modules plugged in instead of wings with four rotors on each side in coaxial configuration of double X. This in fact turns the aircraft into a multirotor drone capable of heavy maneuvering and steady vertical flights. V-3M-X8 is a fully autonomous drone with 2m diameter and with a MTOW take-off mass of 6kg, of which 1,5 kg is a useful payload. The battery system gives the aircraft the autonomy of 30 min in flight but with greater maneuverability than VTOL version. This configuration is suitable for short-range missions up to 5 km and the application of inspection of a high-rise building, bridge or a slow moving or stationary object (mission type C).


  • ‘Real-Time’ HD Video Stream up to 50 km
  • Telemetry, controls and FPV Stream up to 100 km
  • 5 km^2 coverage
  • Endurance up to 30 min
  • Max. speed – 80 km/h (43 kt)
  • Empty weight – 3kg (6 lbs)

Inspection of a bridge or a high-rise building

Up to 30 minutes of  flight time, but with greater maneuverability and payload

Image recognition software to detect the anomalies.

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The system includes ground control station (GCS) for ground communication with the aircraft, broadcast real-time HD video signals (EO / IR) at a distances of 50 km in LOS and telemetry data and control up to 100 km. Antenna tracker for more accurate and better connection to the aircraft and launch system or catapult, which can also be autonomous and can be controlled from a distance.

UAV with MTOWs up to 5,5 (7) kg
Ground Control Station
Communication station with Tracking antenna
Launcher System
Transport equipment and battery charging equipment

VECTOR V3M can broadcast real-time transmission at distances of HD video signals (EO/IR) over distances greater than 50 km in LOS and telemetry data and control up to 100 km and BvLOS with connection to 4G networks

The mission can be completely autonomous with no need for a pilot BVLOS. Maximum flight time is 3 hours at a speed of 60 kmh.

The whole system fits disassembled in two suitcases (828 x 467 x 280 mm) and it is easily transportable.

Ready for all weather conditions (waterproof and wind resistant up to 15 m/s).

VECTOR V3M can be launched with the help of a slingshot or catapult. Lands by parachute or net.