a power plant based on a 40 cm3 internal combustion engine with a capacity of 3.7 hp, with a unique vibration-damping motor and a starter generator;
launcher with rubber shock absorbers;
ground control station (NSO).
With a full supply of fuel for flight, it can be equipped with a payload weighing up to 5 kg. The design of the UAV hull provides two compartments for accommodating payloads, which makes it possible to apply several loads simultaneously. Payload options: high-resolution camera;
video surveillance system;
multispectral camera;
thermal imaging camera;
magnetometric equipment.
Maximum take-off weight up to 29 kg Wingspan 4000 mm Length 2000 mm Payload weight up to 5 kg Speed characteristics The maximum flight speed is 45 m/s (160 km/h) Cruising flight speed 22-26 m/s (80-90 km/h) Tactical characteristics The maximum flight duration with a payload of 1.5 kg is at least 14 hours. The maximum duration of a flight with a payload of 3 kg is at least 10 hours. The maximum duration of a flight with a payload of 5 kg is at least 8 hours. The maximum flight range is 1000 km. The maximum flight altitude is 4000 m Launcher take-off mode Parachute landing mode Wind speed limit, no more than 15 m/s Ambient temperature range from -30 to +40 °C
Unmanned aircraft systems of the airplane type have high performance due to the long duration, speed and altitude of flight. All these characteristics make them indispensable for collecting as much information as possible in one flight. They are ideal for flying over large areas and monitoring extended linear objects. A camera, a multispectral camera, a laser scanner, a UV direction finder, a thermal imager, and a radar can be used as a payload.
Classic fixed–wing aircraft-type UAVs usually require a catapult to launch, and a parachute to land; a site that is sufficiently unprepared in engineering terms for takeoff and landing.
However, in case of problems with the availability of the necessary infrastructure, our company is ready to offer its customers modified versions of this type of UAS. In particular, to offset the above difficulties, we also offer an aircraft-type UAS with the possibility of vertical takeoff and landing (VTOL). The aircraft-type UAS is a hybrid of a fixed-wing aircraft and a multicopter."/>
D-20 With the ability to fly at a distance of up to 1,000 km and an autonomy of up to 14 hours
The D-20 unmanned aircraft system with an internal combustion engine is designed to perform work on remote, extended facilities and large-area facilities. In 14 hours of flight, the D-20 is capable of covering more than 1,000 km. The D-20 UAS includes: an unmanned aerial vehicle (UAV). Made according to the aerodynamic scheme "duck";
a power plant based on a 40 cm3 internal combustion engine with a capacity of 3.7 hp, with a unique vibration-damping motor and a starter generator;
launcher with rubber shock absorbers;
ground control station (NSO).
With a full supply of fuel for flight, it can be equipped with a payload weighing up to 5 kg. The design of the UAV hull provides two compartments for accommodating payloads, which makes it possible to apply several loads simultaneously. Payload options: high-resolution camera;
video surveillance system;
multispectral camera;
thermal imaging camera;
magnetometric equipment.
Maximum take-off weight up to 29 kg Wingspan 4000 mm Length 2000 mm Payload weight up to 5 kg Speed characteristics The maximum flight speed is 45 m/s (160 km/h) Cruising flight speed 22-26 m/s (80-90 km/h) Tactical characteristics The maximum flight duration with a payload of 1.5 kg is at least 14 hours. The maximum duration of a flight with a payload of 3 kg is at least 10 hours. The maximum duration of a flight with a payload of 5 kg is at least 8 hours. The maximum flight range is 1000 km. The maximum flight altitude is 4000 m Launcher take-off mode Parachute landing mode Wind speed limit, no more than 15 m/s Ambient temperature range from -30 to +40 °C
Unmanned aircraft systems of the airplane type have high performance due to the long duration, speed and altitude of flight. All these characteristics make them indispensable for collecting as much information as possible in one flight. They are ideal for flying over large areas and monitoring extended linear objects. A camera, a multispectral camera, a laser scanner, a UV direction finder, a thermal imager, and a radar can be used as a payload.
Classic fixed–wing aircraft-type UAVs usually require a catapult to launch, and a parachute to land; a site that is sufficiently unprepared in engineering terms for takeoff and landing.
However, in case of problems with the availability of the necessary infrastructure, our company is ready to offer its customers modified versions of this type of UAS. In particular, to offset the above difficulties, we also offer an aircraft-type UAS with the possibility of vertical takeoff and landing (VTOL). The aircraft-type UAS is a hybrid of a fixed-wing aircraft and a multicopter.
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