About UAVHELI
KB Unmanned Helicopters presents to its customers a wide range of services for the development and production of unmanned aerial systems of helicopter and aircraft types:
manufacturing at the company's own capacities
manufacturing at the company's own capacities
design and development
design and development
modernization and adaptation of products
modernization and adaptation of products
testing
testing
service
service
training
training
The team's long-term experience, accumulated knowledge and professionalism make it possible for them to manufacture products that meet world aviation standards and meet the customer's requirements.
In the last 5 years the organization has developed the line of unmanned helicopters with takeoff weight from 150 kg to 2500 kg. The company's team foresees the development of technologies, understands the needs of the market and is ready to offer a product that meets their current and future needs.
  • Слайд 1
    The history of the team of creators begins in 1996, when design engineer Vladimir Chudakov created a design bureau «KB Indela» specializing in the development of unmanned aerial vehicles.
  • Слайд 2
    The design bureau was performing work on the development of a unified modular control system (onboard equipment and ground control station) for advanced robotic unmanned aerial vehicles developed in the interests of orders from various countries.
  • Слайд 3
    The first experiment in this field was the modification project of remote-controlled targets. As part of this project, a navigation and autopilot system with automatic flight task termination was tested and developed.
  • Слайд 4
    The idea of developing its own robotic, small-sized, interspecific UAV with vertical takeoff and landing came from this project. The new possibilities in the development of robotic aircraft were opened up by the technologies obtained, independent of the range and quality of radio communication with the ground station.
  • Слайд 5
    In 2002, specialists of the design bureau proposed to participate in the international tender one of its developments - the robotic aerial vehicle with vertical takeoff and landing “RotaryWing”.
  • Слайд 6
    Subsequently, this project was transformed into a new project, the unmanned aerial vehicle "DEAD CALM".
2003 - 2007
  • Revolution
    helicopter-type flying laboratory weighing 20 kg with the rotor diameter 1.6 m.
  • Legion
    helicopter-type flying laboratory with a gas turbine engine, weighing 60 kg with the rotor diameter 3.0 m.
  • H.U.SKY
    small-sized robotic unmanned helicopter with a gas turbine engine, weighing 100 kg with the rotor diameter 3.1 m.
2007 - 2010
  • Arrow
    robotic aerial target with a wingspan of 2.8 m, weighing 33 kg, turbojet engine, parachute rescue system and a speed of 350 km/h.
  • berkut
    aerial target with a wingspan of 2.8 m, weighing 36 kg, turbojet engine, parachute landing system, maximum air speed 400 km/h.
  • Burevestnik
    robotic aerial target with a wingspan of 3.0 m, two turbojet engines, parachute rescue system and a speed of 600 km/h.
  • INDELA - 6
    is an aerial reconnaissance complex with a wingspan of 6.0 m, weighing 35 kg, electric motor and flight duration up to 1.5 hours.
  • INDELA - 6m
    is an aerial reconnaissance complex with a wingspan of 6.0 m, weighing 35 kg, parachute rescue system, a gyrostabilized optoelectronic system and flight duration up to 10 hours.
2008 - 2009
  • INDELA-COUNTRY
    robotic small-sized unmanned helicopter weighing 120 kg and with the rotor diameter of 3.1 m is recommended for use in experimental agricultural enterprises and research institutes of agriculture as a carrier for performing aerial chemical operations.
  • SKY LAB
    robotic small–sized unmanned helicopter for using as an aviation testbed, weighing 120 kg with the rotor diameter 3,1 m.
2010 - 2011
  • Griff-1
    tactical unmanned aerial vehicle of aircraft type with a wingspan of 5.0 m, weighing 150 kg, parachute rescue system and flight duration up to 8 hours.
  • Griffon-200
    tactical unmanned aerial vehicle of aircraft type with a wingspan of 6.2 m, weighing 200 kg, payload mass 50 kg and flight duration up to 12 hours.
2009 - 2017
  • I.N.SKY
    robotic small–sized unmanned helicopter weighing 140 kg and with the rotor diameter 3.4 m, a gyrostabilized optoelectronic system with infrared camera and flight duration up to 6 hours.
2017 - 2020
  • SKY/BUR
    scout attack unmanned helicopter weighing 150 kg, payload mass 25 kg, a fuel reserve 38 liters, the rotor diameter 3,4 m, a gyrostabilized optoelectronic system with an infrared camera and flight duration up to 4 hours.
  • UAV 150 - A
    robotic small-sized unmanned helicopter weighing 170 kg, payload mass 30 kg, a fuel reserve 48 liters, the rotor diameter 3.4 m, a gyrostabilized optoelectronic system with an infrared camera and flight duration up to 5 hours.
  • EYE SKY
    robotic small-sized unmanned helicopter weighing 200 kg, payload mass 50 kg, a fuel reserve 52 liters, the rotor diameter 3.6 m, a gyrostabilized optoelectronic system with an infrared camera and flight duration up to 5 hours.
2017 - 2021
  • peacekeeper
    unmanned attack aircraft with a wingspan of 2.8 m, turbojet engine, take-off weight of 46 kg, maximum air speed of 450 km/h.
Development
of ground stations
  • MOBILE HEADQUARTERS
    MOBILE HEADQUARTERS
    for field meetings and conferences and police coordination.
  • GCS
    GCS
    ground control station of unmanned aerial vehicle is intended to provide the UAV remote control of UAV, its onboard equipment.
  • SC
    SC
    is a transportable ground support means intended for storage and transportation of two helicopter-type UAVs.
RELATED
EQUIPMENT DEVELOPMENT
  • KP120
    KP120
    Launcher is intended to perform pre-launch control of the UAV, starting of the main engine and launch UAVs weighing from 20-120 kg.
  • KP95
    KP95
    Launcher is intended for pre-launch control of the aerial target, starting of the main engine and target launch.
  • ATA 2400
    ATA 2400
    data acquisition system is intended to provide communication between ground control station and UAV at medium and long distances in the direct line of sight at a distance of up to 150 kilometres.
  • ATA 5800
    ATA 5800
    data acquisition system is intended to provide communication between ground control station and UAV at medium and long distances in the direct line of sight at a distance of up to 100 kilometres.
  • HD-190
    HD-190
    Optoelectronic system in sealed carbon fiber housing, the system is equipped with a 4-core processor Cortex A, thermal imager with germanium glass with DLC coating, colour HD camera protected by quartz glass with diamond-like sputtering, 3 km laser rangefinder, DaVinci video processor, two three-dimensional inertial modules, one of which is mounted directly on the optical installation, which significantly increases the accuracy of determining the coordinates of the target.
  • OGD-20HIR
    OGD-20HIR
    optoelectronic system with five modules built into a compact housing: thermal imager, colour camera, laser rangefinder, video processor, inertial module.
  • SIS1
    SIS1
    diagnostic computer stand is intended for searching of malfunctions and checking of any models of servo drives for the characteristics declared by the manufacturer.
  • TCB 210
    TCB 210
    is a diagnostic computer stand designed for troubleshooting and running-in of internal combustion engines with the volume from 50 to 650 cm³. It allows to carry out all routine engine running-in operations with the possibility to adjust the power supply and ignition systems.
ACHIEVEMENTS
  • Сертификат 1
  • Сертификат 2
  • Сертификат 3
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  • Сертификат 6