PRODUCT CATALOG ABOUT COMPANY

The main products of JSC Radar mms include standard series of intelligent radioelectronic and combined control systems for high-precision sea-, air- and ground-based weapon. These systems are characterized by secrecy and immunity, have no equals in the world with respect to performance characteristics.

JSC Radar mms carries out large-scale researches regarding to development and production engineering of radioelectronic systems of a short-part millimeter-wave range, improvement of magnetic anomaly detection systems, creation of integrated optoelectronic systems, development of intelligent control and guidance systems.

The Company also develops special and civil purpose radioelectronic systems, including airborne all-round surveillance radars based on APAA in various frequency bands.

JSC Radar mms has a substantial scientific and technical expertise in designing algorithms and their application in special software for tactical command and information control systems, processing systems for geospatial, geo-intelligence and mapping data, terrain spatial modeling, control of high-precision weapon systems, and robot systems with different deployment types.

JSC Radar mms is an integrator of onboard radioelectronic systems for patrol-and-rescue aviation and aircraft monitoring systems. The search-and-targeting system “Kasatka” is designed for detection of underwater and surface objects, targeting for different antisubmarine and antiship weapon carriers, search-and-rescue operations, environmental monitoring of sea and coastal areas.

The Company’s specialists have a great experience in designing, production and operation of a parametric range of unmanned helicopters (weight-lifting from 8 to 500 kg) and aircrafts (weight-lifting up to 8 kg) for search-and-rescue operations; ice surveillance; fire source and border identification; abnormal power lines and pipelines detection; environmental monitoring; etc.

Scientific and technical expertise was created for development of devices and technologies based on ultra-wideband signals for practical tasks with regard to antijamming radars, radiocommunication and electronic countermeasures equipment.

JSC Radar mms develops and serially produces automated systems of marine and coastal autonomous information-and- measurement equipment for hydrometeorological support, as well as shipborne and coastal data collection, processing, analysis and display equipment which provides time-critical monitoring of hydrometeorological environment near naval forces and facilities.

The Company is one of the leaders on the Russian market of microelectronics and microsystems. The engineering and manufacturing base for production of micro- and acoustoelectronics is the best in North-West region. The company designs and manufactures acoustoelectronics and microsystems products with use of nanotechnologies as follows: temperature, humidity, deformation and identification sensors based on surface acoustic waves (SAW); precision quartz pressure sensors, SAW bandpass filters; acoustoelectronic dispersive delay lines; thin-film microstrip boards for UHF modules. Joint-stock company Radar mms is one of the world’s leaders in the field of developing special and civil purpose radioelectronic systems and suites, precision instruments, special software. JSC Radar mms develops high-technology command and control systems for automobile and railway transport. The Company actively participates in development of hardware and software for intelligent transport systems. Distributed information systems for monitoring, traffic control and security protection of transport facilities are developed for the Russian Federation Ministry In 2010 and 2015, JSC Radar mms was awarded the commendation by President of the Russian Federation for considerable of Transport, Federal Road Agency, JSC RZD. The Company takes part in implementation of joint Russian and Belorussian contribution in radio-electronic industry development, strengthening the defense capability of the country and achieved scientific and technical project “Automotive electronics”. work progress.

Today JSC Radar mms develops and manufactures as follows: І homing systems for high-precision weapon І airborne search-and-targeting systems І short-range radar systems І ultra-wideband radar systems І wing-in-ground effect and dynamically supported crafts І various types of unmanned aircraft systems І systems of geospatial data processing and flight mission planning І ground area and environment monitoring systems І weather support systems І microelectronics, micro systems technology products with use of nanotechnology І automotive electronics І intelligent life support systems І medical devices and equipment

RADAR-MMS.COM CONTENTS

The Сompany and JSC R.E. Alexeev’s Central Hydrofoil Design Bureau jointly develop and create high-speed air-cushion; 6 UNMANNED AIRCRAFT SYSTEMS air-cavity vessels and boats; hydrofoil crafts; transport-amphibian platforms; WIG effect crafts for defense and civil purpose. JSC Alexeev’s Design Bureau has a capability to develop a new generation of high-speed vessels for the Russian Navy and civil fleet. 16 WEATHER SUPPORT SYSTEMS

JSC Radar mms innovative solutions include intelligent technologies for buildings, offices, facilities that provide enhanced 24 AUTOMATIC FIRE SYSTEMS security, precise interaction of all systems, organization of management network structure with implementation of automatic control functions, processing and storage of data on the systems state with a common control station; resource-saving. 30 PRECISION PRESSURE SENSORS JSC Radar mms manufacturing facility has state-of-the-art precision and high-performance equipment. The engineering and manufacturing base of the Company is continuously updated; advanced information technologies are explored for product computer-assisted engineering and quality assurance during production and operation. The Company has a state-of-the-art 36 SYSTEMS FOR RADIO FREQUENCY IDENTIFICATION AND PHYSICAL QUANTITY MEASUREMENT multimedia center of information technologies for development and modeling schematic and design solutions. Own simulation and testing facility provides a full-scale cycle of reliability, mechanical and environmental tests of defense and civil products. 40 AUTOMOTIVE ELECTRONICS

JSC Radar mms has a great scientific potential. The Company’s personnel includes Laureates of State prizes, doctors and candidates of science, professors, and associate professors. In the Company there is a number of scientific and engineering 44 MAGNETIC ANOMALY DETECTION SYSTEMS schools which are influential in our country and abroad. 48 SYSTEMS FOR EARTH SURFACE AND ENVIRONMENTAL MONITORING JSC Radar mms employees have an opportunity to continue their education in PhD programs “Radar and radio guidance” and “System analysis, information management and processing”. The license for educational activity in the field of postgraduate professional education was obtained in August 2013. Since 2013 the Company’s dissertation council has been working to admit 52 RADAR SYSTEMS dissertations for a degree of candidate and doctor of sciences.

The Company holds community activities and supports the strategic partnership with St. Petersburg leading technical 60 SYSTEMS FOR GEOSPATIAL DATA PROCESSING universities, two of which have the specialized academic departments. Jointly with St. Petersburg City Government JSC Radar AND FLIGHT MISSION PLANNING mms organizes the annual all-Russian research and training conferences “The future of Russia is in high technologies” for senior school students. 62 HARDWARE-IN-THE-LOOP SIMULATION SYSTEMS The Company’s active scientific-and-technical and marketing policy, optimal combination of work in the interests of military and civil customers, tight cooperation with research and educational organizations ensure further development of the 66 ULTRA-WIDEBAND RADAR SYSTEMS Company’s potential, its successful activity on domestic and international markets. 72 UHF DEVICES

78 INTELLIGENT LIFE SUPPORT SYSTEMS

82 WING-IN-GROUND EFFECT AND DYNAMICALLY SUPPORTED CRAFTS

84 SERVICES AND MAINTENANCE

91 ALPHABETICAL INDEX

RADAR-MMS.COM UNMANNED AERIAL SYSTEM BASED ON ROTARY-WING TYPE UAV

PURPOSE PAYLOAD Time-critical air monitoring of vast and long-distance ground, І gyro-stabilized optoelectronic systems: water or ice areas at adverse terrain. – HD camera 6 – thermal imaging camera 7 The system enables to perform main tasks as follows: – laser range finder І supporting search and rescue – multi-spectral imager І patrol, protective and counterterrorist operations І environmental and radiation monitoring sensors and devices: І ice surveillance – gas-analyzer І aftermath assessment of the natural – gamma-radiation detector and human-made disasters – methane leak laser detector І power lines, pipelines and forest areas condition monitoring – digital picture camera

І exploratory fishing І special all-weather search systems: І ground and water areas ecological inspection – four-chamber quantum MAD device – quantum MAD device SYSTEM CONFIGURATION – small-sized radar І rotary-wing type UAV І lantern and audible systems: І ground control station (rugged notebook/tablet) – LED floodlight І command radio link – active loud-speaker

І information-command radio link Development and production of special payload on request. І FPV camera (fist person view) І spare parts OPERATING PRINCIPLE The system consists of rotary-wing unmanned aerial vehicle (UAV) “Briz”, ground control station (mobile or vehicle-based), SPECIFICATIONS and a set of quick removable payload units mounted on the unmanned helicopter according to the mission. Maximum take-off weight, kg 45

The unmanned helicopter is equipped with combustion engine, automatic control system, inertial navigation system, GPS/ Maximum payload weight, kg 10 GLONASS receiver, payload control unit, systems condition monitoring sensors, receive-transmit equipment for unmanned Flight endurance, h 2.5 helicopter control, payload and telemetry data transmission. Horizontal fl ight airspeed range, km/h from 0 to 75

The ground control station is designed for forming flight mission based on the electronic map, unmanned helicopter monitoring Radio communications range, km and control, as well as for receiving and displaying payload data, payload control in real-time mode. – command radio link 80 – information-command radio link 35 After installation of a unit with necessary payload and preparation of the unmanned helicopter to flight, an operator loads the Power plant internal combustion engine flight mission into the unmanned helicopter autopilot. Take-off is carried out after operator command, the unmanned helicopter Control mode аutomatic, semi-automatic performs flight mission in the automatic mode. The operators receive data from the unmanned helicopter in real-time mode that enables to take quick decisions on changing situation and transmit this information to the command center. Registration of data received from the payload with reference to coordinates is performed both onboard unmanned helicopter and at the ground control station for further analysis and processing. The operator in real time mode can change flight mission of the unmanned helicopter, as well as control the payload. MONITORING SYSTEM BASED ON UNMANNED HELICOPTER BVS VT 500

PURPOSE FIELD OF APPLICATION 8 Time-critical air monitoring of ground, water and ice surface, І handling specific tasks in the interests of the Russian 9 infrastructural facilities, including adverse terrain or areas Defense Ministry, security forces and agencies dangerous to human life, for purposes of as follows: І monitoring of oil and gas pipelines, power lines condition І support of search-and-rescue, patrol-and-security and counterterrorism operations І forest areas monitoring І ice surveillance І search-and-rescue operations І estimation of natural and technogenic disaster impact І support of geological exploration activities І monitoring of extended power lines, pipelines І ice surveillance and forest areas І mapping and topographic survey for environmental control SYSTEM CONFIGURATION of local and water areas, etc. І rotary-wing type UAV І temporary mobile radio in the specified area І ground control station, including 2 automated І relay of information signal, delivery of cargo for various workstations which can be mounted as a separate module purposes according to the specified coordinates based on surface ship or vehicle (robots, special tools, etc.) І set of payload units mounted on unmanned helicopter І chemical spraying for agriculture needs The unmanned helicopter is equipped with internal combustion engine, automatic control system, inertial navigation system, GPS/GLONASS receiver, payload control unit, a set of systems condition monitoring sensors, transceiving equipment for unmanned helicopter control, as well as for payload and telemetry data transmission.

SPECIFICATIONS Maximum take-off weight, kg 500 Maximum payload weight, kg 150 Flight endurance, h 5.5 Altitude fl ight range above the sea level, m from 0 to 3500 Flight speed range, km/h from 0 to 155 Operating range, km 320 Operating conditions: – ambient temperature, °С from -30 to +50 – wind speed at ground level, m/s up to 15 The Company’s specialists carried out research-and-development and design development work to create a parametric Engine unit ICE range of unmanned aerial vehicles. Control mode automatic (based on the program), semi-automatic The Company developed a line of monitoring systems based on small-sized unmanned helicopters with take-off weight Setup time, min 50 from 6 to 500 kg, which can be equipped with onboard payload from 0.5 to 150 kg. Dimensions, m – 4.7х1.6х2.6 – rotor diameter: 6.0 UNMANNED AERIAL VEHICLES PAYLOAD UAV APPLICATION EXPIRIENCE

The Сompany is an integrator of different types of payload The Company has practical experience in application for proprietary unmanned aerial vehicles. of UAV systems (equipped with different types of payload) for the benefit of: WIDE RANGE OF PRODUCTS І General Directorate of the Russian Emergency Ministry The multipurpose payload hardware can be mounted in St. Petersburg on the UAV upon customer’s request: І General Directorate of the Russian Emergency Ministry І photo and video equipment of different class in Leningradskaya Oblast І wide range of sensors and measuring devices І St. Petersburg Government Committee on environmental (magnetic anomaly detector, dosimeter, gas analyzer, etc.) management, environmental protection and environmental І other special purpose hardware (audible warning equipment, safety lighting equipment, searchlight, dropping and dispensing І FSUE “Emergency and Technical Center of the Russian І cargo delivery І search and exploration of minerals location device, laser scanner, sonar equipment, etc.) Ministry of Nuclear Energy” St. Petersburg І FSBEI HPE “National Mineral Resources University” І North-West Territorial Administration of the Federal Agency 10 for Fishery 11

І infrustructure facilities monitoring І unauthorizied fishing monitoring І payload unit І payload unit І payload hardware unit І payload hardware with a gas analyzer with television with a photographic unit with a gamma- and thermal recorder radiation dosimeter imaging cameras

І photo/video unit, camera, І gas analyzer І gyro stabilized І gamma-radiation moni- TV camera, thermal camera, optoelectronic system toring instrument methane leak laser detector І pipelines thermal imaging І terrain orthophotomapping

І small-sized radar І the air dust counter І audible warning І magnetic anomaly (dust meter) system detector

І pipelines mapping/pigging І environmental monitoring MOBILE CONTROL STATIONS UAV CONTROL SYSTEM

The special software, installed on the operator workstations, enables to provide all phases of UAV operation and performs the functions as follows: І display of agreed mapping data volume І automated generation of UAV flight route І building a spatial (three-dimensional) model of the operation area terrain. Flight simulation based on the generated model І automatic reception and display of the airspace structure in the area of UAV flight operation І telemetry data receiving and display PURPOSE І formation of UAV control commands, as well as with use JSC Radar mms uses a comprehensive approach to development SYSTEM CONFIGURATION of a remote control unit of UAV control systems, i.e. from a mathematical model Mobile control stations are designed to provide control І onboard computer of automatic control system (ACS) of unmanned aerial vehicles (UAVs), receiving and processing І formation of UAV payload hardware (PH) control commands to a finished product and flight development tests. of the data from UAV payload hardware. І payload control system (PCS) І display and logging of UAV payload hardware data The Company has to its credit the unique algorithms І hardware system of ground control station of an onboard with reference to the digital terrain map of operation and integration of different types of sensors 12 SYSTEM CONFIGURATION computer 13 І simultaneous playback of all flight data according and actuators included in the UAV control system, І one or more operator automated work stations (AWS) to the logging data as well as the developed ideology of application software І special software of onboard computer for data processing from payload hardware for UAV control. І possibility of post-flight data processing І special software of PCS І data transmit/receive equipment (including a “cross-link” of photographs) PURPOSE І special software of ground control station (GCS) І airband radio station І operation of UAV control operator workstation І to control flight in automatic, semi-automatic І weather station in the simulator mode and manual modes І to connect and control any type of payload ADVANTAGES І to transmit telemetry and control data between UAV І mobility and ground control station І rapid deployment І proprietary integrated software HARDWARE VERSIONS

І portable UAV control station

І universal multipurpose UAV control module І mobile UAV control station MULTIPURPOSE UAV ONBOARD COMPUTER “SMENA-5” RADIO MODEM “LORA-1”

MAIN SPECIFICATIONS І PINS on the micromechanical sensor elements with built-in SNS GPS/GLONASS receiver and barometric sensor correction І autopilot for fixed-wing and rotary-wing UAVs, and dynamically supported crafts І automatic calibration of gyroscopes, accelerometers and magnetic anomaly detectors in time of UAV motion І automatic correction of the built-in clock according to the SNS signals І built-in non-volatile memory with a volume of 2 MB for recording telemetry PURPOSE PURPOSE SOFTWARE І two CAN 2.0B buses for avionics control Radio modems “Lora” are designed for narrowband telemetry The software “MMS Configurator” is designed to display Multipurpose onboard computer “Smena-5” is designed data transmission and control between unmanned aerial and change computer settings, as well as to replace software to automatically control the motion of unmanned aerial І wide communication capabilities: Bluetooth 2.0, RS422, vehicle and ground control station. from ground control station. vehicles according to a flight mission predetermined Futaba from a ground control station. І ability of calculator and avionics control bus duplication 14 ADVANTAGES 15 SOFTWARE І ability to change the settings and update software without І ability of operation under negative values removal of the computer via wireless and wired interfaces of a signal/noise ratio І MMS Control software with an intuitive interface for UAV motion control from ground control station І full galvanic isolation of all interfaces and power supply І communication range for direct radio visibility of up to 80 km І MMS Configurator software to display and change computer І IP67 waterproof housing settings from a ground control station І wide communication capabilities: USB, RS232, RS485 І software interface with Simulink for mathematical simulation І ability to change settings and update software without of the UAV control system in the HIL mode removal of a radio modem via wireless and wired interfaces І mathematical models of fixed-wing and rotary-wing UAVs, І IP67 waterproof housing as well as dynamically supported UAVs І no under certification of Russian State Commision for Radio Frequences SPECIFICATIONS Smena-5 Smena-5m SPECIFICATIONS Acceleration measurement range, g ±10 ±18 Frequency range, MHz from 860 to 915 Angular velocity measurement range, degree/s ±450 ±2000 Output power, dBm 20 Angular random drift of the gyroscope, degree/h, no more than 6 20 Sensitivity, dBm -130 Upper range limit of speed measurement, m/s 500 Frequency band, kHz from 12.5 to 500 Upper range limit of altitude measurement, m 11000 Streaming rate, Kbit/s 150 Output frequency of navigation solutions, control signals and telemetry Receive-transmit switching delay, ms 10 records, Hz 100 Power supply voltage, V from 4 to 30 Number of PWM channels - 8 Power consumption, W, no more than 1.25 Number of CAN channels 2 1 Lora-1 140 Number of RS232 channels 1 Weight, g, no more than Lora-1m 30 Radio modem Futaba yes Lora-1 109x36x30 Radio modem Bluetooth yes Dimensions without antenna (LxWxH), mm Lora-1m 87x12x21 Radio modem Lora no yes Volume of non-volatile memory for recording telemetry, GB 1 0.5 Power supply voltage, V from 9 to 36 Galvanic isolation yes no Power consumption, W, no more than 6 3 Weight, kg, no more than 0.5 0.2 Dimensions (LxWxH), mm 190x109x30 125x81x35 SHIPBORNE HYDROMETEOROLOGICAL STATION “KHARAKTER-K”

A list of HMS “Kharakter-K” measuring devices І air temperature and humidity sensor І wind speed and direction sensor І atmosphere pressure sensor І sensor of meteorological visibility range І cloud base sensor All these sensors are connected to the processor unit BPR which receives, processes and visualizes information on a computer screen or display.

ADVANTAGES І high automation degree of data measurement, processing and display in the format of meteo panel and graphic form PURPOSE Hydrometeorological station “Kharakter-K” is designed І transmission of meteorological data to consumers via wire to measure main meteorological parameters. With use and wireless (radio, GSM and satellite) communication of its own hardware and software it enables measurement channels and display of the data on values of meteorological parameters, І modular construction design enables to configure as well as their registration in the non-volatile medium the product for solution of any hydrometeorological 17 and transmission via communication channels. support issues

It can be equipped with additional devices as follows: І satellite data reception equipment SDRE — reception FIELD OF APPLICATION of cloud image from polar-orbiting weather satellites Hydrometeorological support of the Navy and civil market. overlaid on the geographic grid CERTIFICATION І hydrological probe for measurement of hydrological The number in State Register: SI 64220-16. variables (pressure and water temperature, relative electrical conductivity)

OPERATING PRINCIPLE The operating principle of HMS “Kharakter-K” is based on transformation of meteorological and hydrological parameters into electrical signals and then into digital codes to be further processed, stored and visualized.

SPECIFICATIONS Measurement range Measurement accuracy Air temperature, °C from -40 to +50 ± 0.5 Relative humidity,% from 30 to 100 ±8 Atmosphere pressure, hPa from 880 to 1050 ±0.15 Wind speed (W), m/s from 1 to 50 0.(0.5 + 0.05 W) Wind direction, º from 0 to 360 ±6 (when W is more than 5 m/s) Meteorological (optical) visibility range (S), m from 10 to 5000 ±(10+0.2S) Cloud base h, m from 15 to 5000 ± (15+0.05h) AUTOMATED WEATHER STATION TEMPERATURE AND HUMIDITY SENSOR DTVV-01

І organization of observation network: – the data from all weather stations are transmitted to the control center; – prompt response to changing weather conditions; – weather conditions forecasting. І possibility of integration with other environmental monitoring devices І open architecture І modular design

OPERATING PRINCIPLE PURPOSE OPERATING PRINCIPLE The operating principle is based on transformation Air temperature and relative humidity sensor DTVV-01 The sensor is based on a sorption capacity sensor element of meteorological parameters into electrical signals is designed for use in automated meteorological conditions manufactured by JSC Radar mms. A signal from the sensor and then into digital codes to be further processed, monitoring systems (road, marine, stationary and mobile). element is converted into a digital code and transmitted stored and visualized by special software. to the secondary devices via RS-485 interface. FIELD OF APPLICATION LIST OF MEASURING DEVICES The sensors are applied in various meteorological condi- ADVANTAGES tions monitoring systems: PURPOSE І meteorological (optical) visibility range sensor І fully domestic component and material base І measurement of environment meteorological parameters І road weather stations І it has no equals in Russia 18 (air temperature and humidity, atmosphere pressure, І wind speed and direction sensor 19 І shipborne and shore hydrometeorological stations wind speed and direction, meteorological visibility range) І air temperature and humidity sensor І a wide range of humidity and temperature measurement І automated aerodrome weather stations І automatic collection and transmission of meteorological І atmosphere pressure sensor І resistance to salt spray, high chemical resistance parameters to the control center via a GSM communication І IP66 version channel (a satellite channel is optional) І road surface condition sensor

The sensors are connected to a processor unit which SPECIFICATIONS ADVANTAGES receives, processes and visualizes on a computer screen І high automation degree of data measurement, or display. Relative humidity measurement range, % from 0 to 100 processing and display Temperature measurement range, °C from - 50 to + 60 І transmission of meteorological data to consumers FIELD OF APPLICATION RH measurement error (hysteresis, non-linearity), no more than, %: via wireless (GSM or satellite) communication channels Road industry, agriculture and other sectors of economy. within RH range from 10 to 90% ±2 within RH range from 0 to 10% and from 90 to 100% ±5 І provided integration with a groundwater measurement system Temperature measurement error, °C 0.4 Response time, no more than, s: RH threshold 63% in still air V≤3 m/s 20 SPECIFICATIONS RH threshold 90% in still air V≤3 m/s 60 Measurement range Measurement accuracy Long-term instability in a year, no more than, % RH 1.2 Ambient temperature, °C from -40 to +50 ±0.5 Dimensions, mm 330х66х33 Relative humidity, % from 30 to 100 ±8 Weight, g 250 Atmosphere pressure, hPa from 500 to 1100 ±0.15 Data transmission interface RS-485 Wind speed (W), m/s from 0.4 to 75 ±0.17 Product material plastics Wind direction, º from 0 to 360 ±3 Meteorological (optical) visibility range (S), m from 10 to 5000 ±(10+0.2S) Road surface condition dry/moist/wet or snow/salt content/ice formation Temperature on the road surface and at a depth of 5 cm from -50 to +70 ±0.2 (from -10 to +10) and 30 cm, °C ±0.5 (remaining range) Water fi lm thickness on the road surface, mm from 0 to 4 ±0.1 (±20%) of the measured value

Specifi cations of sensors as part of ARWS Dimensions, mm Weight, kg Anemometer 240х90 0.57 Wind spinner 270х90 0.9 Temperature and humidity sensor 200х105 2.0 Atmosphere pressure sensor 240х126х260 3.0 Meteorological visibility range sensor 404х695х199 3.0 Road surface condition sensor 120х5 0.8 HYDROMETEOROLOGICAL BUOY WIND SPEED AND DIRECTION SENSOR

OPERATING PRINCIPLE It consists of a hydrological unit, mounted on a wire-cable The operating principle is based on transformation of me- at a depth of 30-50 m, which measures as follows: teorological parameters into electrical signals and then into І water temperature digital codes to be further processed, stored and transmitted І water salinity to consumers via communication channels. OPERATING PRINCIPLE FIELD OF APPLICATION І flow speed and direction 20 A digital transducer converts discrete readings received The sensor is applied in various meteorological conditions 21 SYSTEM CONFIGURATION І hydrostatic pressure from anemometer and wind spinner into a digital code monitoring systems: І wind speed and direction measurement sensor for wind speed and direction measurement channels, І road weather stations transmitted to the processor unit via RS-485 interface. І air temperature measurement sensor FIELD OF APPLICATION І shipborne and shore hydrometeorological stations Environmental monitoring. І atmosphere pressure measurement sensor The sensor comprises heating elements, built І automated aerodrome weather stations in the anemometer and wind spinner, which activate І hydrological device ADVANTAGES when the temperature drops below 4°C and maintain І high automation degree of data measurement, the sensor internal operating temperature required ADVANTAGES PURPOSE processing and transmission to avoid ice formation. І fully domestic technology and hardware components The hydrological buoy is installed on the sea surface І reduced weight and dimensional characteristics, improved І transmission of meteorological data to consumers PURPOSE in the coastal zone. via wireless (UHF, GSM or satellite) corrosion resistance as compared to the foreign analogs The wind speed and direction sensor is designed for wind The surface buoy is equipped with as follows: communication channels speed and direction measurement and use in meteorological І wide range of operating temperatures and conditions І meteorological sensors (wind speed and direction, conditions monitoring systems. of operation atmosphere pressure and air temperature) І the sensor design provides quick replacement І flashing beacon and adjustment of operational parameters in the place І antennas of communication channels of installation that is especially relevant to the marine (GSM, satellite and VHF) weather stations І GPS-GLONASS antenna І solar batteries SPECIFICATIONS Wind speed measurement range, m/s from 0.4 to 75 SPECIFICATIONS Wind speed measurement error, m/s ±(0.05+0.05W) Wind direction measurement range, degree from 0 to 360 Measurement range Measurement accuracy Wind direction measurement error, degree ±4 (at V equal more than 5 m/s) Ambient temperature from -50 to +50 ±0.5 Dimensions, mm 366x250x639 Atmosphere pressure from 880 to 1080 ±0.5 Weight, kg 3.8 Wind speed (W) from 1 to 50 ±(0.5+0.05·W) Interface RS-485 Wind direction from 0 to 360 ±6 Product material titanium alloy VT1-0 Specifications of sensors Dimensions, mm Weight, kg Wind speed and direction sensor Ø 115х211 0.62 Temperature sensor Ø 105х349 0.9 Atmosphere pressure sensor 230х240х126 5.0 ATMOSPHERE PRESSURE SENSOR DADS-1 METEOROLOGICAL (OPTICAL) VISIBILITY RANGE SENSOR

OPERATING PRINCIPLE PURPOSE OPERATING PRINCIPLE FIELD OF APPLICATION: The operating principle of atmosphere pressure sensor The sensor is designed for atmosphere pressure It contains an optical transmitter, i.e. LED infrared emitter The sensor is used in various meteorological conditions is based on variations of a resonant vibration frequency measurement. and photosensitive diode - receiver. Meteorological (optical) monitoring systems: of high-quality quartz resonator, which has long-term visibility evaluation is accomplished by measuring the infrared І road weather stations calibration curve stability under the barometric FIELD OF APPLICATION light attenuation caused by its scattering and absorption pressure impact. in the fixed probed space. І shipborne and shore hydrometeorological stations 22 І weather stations of meteorological conditions 23 monitoring system І automated aerodrome weather stations ADVANTAGES A measured attenuation value is converted into a meteoro- І water level measurement system logical (optical) visibility range indicator and transmitted І High precision measurements is provided throught all (for atmosphere pressure compensation) in the digital form to the processing and display devices ADVANTAGES operation temperature ranges and pressure measurement via RS-485 interface. ranges excluding additional errors in particular in initial І it has no equals in domestic market Product is a measuring instrument having registered number sections І fully domestic technology and hardware components 71288-18 in National Register of Measuring Equipment. PURPOSE І high resolution Measurement of meteorological (optical) visibility range. І wide range of operating temperatures І domestic hardware components and operating conditions

SPECIFICATIONS SPECIFICATIONS Upper measurement limit, hPa 1100 Measurement range, m from 10 to 20000 Lower measurement limit, hPa 500 from 0 to 10 ±10% Measurement error, km from 10 to 20 ±15% Maximum allowable pressure, % URL 125 Dimensions, mm 840х300х180 Limits of permissible measurement error in the operating ±0.5 temperature range, hPa Product material metal Controlled environment air Operating temperature range, °C from -50 to +60 +9 Supply voltage, V 18-8.5 Current consumption, mA, no more than 0.095 ±0.05 Output interface RS-485 Sampling time, ms, at least 200 Dimensions, mm 134х117х93 Weight, kg, no more than 1.05 SUPER EARLY WARNING SYSTEM FOR DETECTION OF FIRE DANGEROUS SITUATIONS

PURPOSE SYSTEM CONFIGURATION Super early warning system for detection of fire dangerous І fire security extender situations enables to enter a new quality level of fire safety. It provides information about situations leading to fire І local radio modem occurrence that enables to assume in-time measures І line radio modem excluding fire source occurrence. І electroinductive smoke fire detector ADVANTAGES І receiving and controlling fire security device І it has no direct equals on the Russian market and abroad FIELD OF APPLICATION І high sensitivity to fine particles of smoke formed at the stage of low-temperature pyrolysis І unique facilities І compatible with modern receiving and control devices, І administrative buildings as well as computer І warehouses І earlier detection of fire dangerous situation in comparison І archives and museums with existing fire detectors on the market І medical and child care institutions І detection of power equipment overheating, including wiring

OPERATING PRINCIPLE APPROVAL DOCUMENTATION The system design is based on the modular principle The system is developed in accordance with Technical regulation 24 and provides super early collection of the data on the aerosol of fire safety requirements (Federal Law No.123-FZ dated 25 and gas atmosphere in protected areas, its processing, 22/07/2008 and amendment No.117-FZ dated 10/07/2012). visualization and transmission to the central surveillance The electroinductive smoke fire detector IP 216-001 and external actuators control center. complies with the Russian State Standard R 53325-2012, the conformity certificate number is S-RU.AJ45.V.00016.

SPECIFICATIONS Address capacity 256 Maximum link length, m wire 1200 wireless 55 Operating temperature range, °C from 0 to 45 for sensors from -20 to +40 Operating range of relative humidity, % from 10 to 95 Average service life, years 10 Communication interface RS-485, AL, RF (F1 = (864 – 865) MHz and F2 = (868.7 – 869.2) MHz)

fire transceiving control console fire security extender line radio modem RS-485

AL1...... AL16

AL local radio modem

electroinductive smoke gas alarm device AL fire detector

electroinductive smoke fire detector gas alarm device ELECTROINDUCTIVE SMOKE FIRE DETECTOR IP 216-001 ASPIRATING FIRE DETECTOR

PURPOSE ADVANTAGES IP 216-001 enables to detect fire dangerous situations І increased probability of fire situation detection at the early stage of its generation before the fire source in comparison with existing fire detectors on the market OPERATING PRINCIPLE ADVANTAGES occurs. The detector has a high sensitivity to low concentrations The detector is based on the electroinductive principle І high sensitivity to fine particles of smoke formed of fine aerosols released at the early stages of thermal І high sensitivity to fine particles of smoke formed of operation; it provides selection through a piping system at the stage of low-temperature pyrolysis decomposition of various materials. at the stage of low-temperature pyrolysis with air inlets and shipping of air samples (aspiration) from protected space (zone) to the fire (smoke) detector. І compatible with modern receiving and control devices, І compatible with modern receiving and control devices, as well as computer OPERATING PRINCIPLE as well as computer The detector is based on the electroinductive method. PURPOSE І detection of power equipment overheating, including wiring І detection of power equipment overheating, including wiring 26 The tested aerosol is pumped through a measuring line, The aspirating fire detector, based on the electroinductive 27 in which the charging and measuring chambers are mounted method, substantially outperforms existing aspirating fire FIELD OF APPLICATION consecutively along the flow. In the charging chamber detectors manufactured abroad with regard to a speed TECHNICAL CONDITIONS Highly dangerous and technically complex facilities where the aerosol particles get an electrical charge proportional of fire dangerous situation detection as it responds The development is protected by the patent of the Russian other types of detectors cannot be used: to their size. Passing through the measuring chamber, Federation No.2459268. to the emergence of fine aerosol in the air released the charged particles form charge, the amount of which at the early stages of material pyrolysis, while its sensitivity І limited access or complex service depends on their size and number concentration. The electroinductive smoke fire detector IP 216-001 to aerosol concentrations is several orders of magnitude І large extended facilities, several premises complies with the Russian State Standard R 53325-2012, greater than the sensitivity of best foreign prototypes. FIELD OF APPLICATION the conformity certificate number is S-RU.AJ45.V.00016. І hidden installation Fire protection systems of unique facilities, administrative І complicated operating conditions buildings, warehouses, archives and museums, medical and child care institutions, and highly dangerous industrial and technically complex facilities, etc. SPECIFICATIONS Threshold of sensitivity to the aerosol concentration, mg/m³, 0.01 no more than SPECIFICATIONS Upper limit of sensitivity to the aerosol concentration, mg/m³, 100 Dimensions, mm 150x84x80 no less than Weight, kg, no more than 0.9 Maximum length of a tube in the beam, m 200 Operating range of aerosol concentration from 0.01 to 100 Operating temperature range, °C from -20 to +55 measurement, mg/m3 PC connection interface RS-485 Power supply voltage, V from 16 to 30 Weight not exceeding, kg 2 Power consumption, W, no more than 1.5 Dimensions (WxHxL), mm 300х350х450 Operating temperature range, °C from -20 to +55 PC connection interface RS-232 Fire alarm system connection relay contacts, AL PRE-EMERGENCY MONITORING EXPLOSION-PROOF SENSOR EQUIPMENT FOR TUNING AND CALIBRATION OF FIRE DETECTORS IP 216-001-EX AND GAS ANALYSIS DEVICES

Ionization

aerosol

measurement

PURPOSE ADVANTAGES Pre-emergency monitoring sensor IP-216-001-Ex is designed І ready-made solution for early fire detection at oil for detection weak concentrations of highly dispersed aerosols and fuel-power enterprises. OPERATING PRINCIPLE FIELD OF APPLICATION emitting on early stages of thermal breakdown to warn The system consists of aerosol generator, gas mixture І at the enterprises which, serially produce electroinductive, of an emergency situation at explosive facilities. І steadily reacts to smoke particles of all sizes regardless generator and personal computer. smoke and gas fire detectors, in order to ensure maximum the color or chemical composition automation (from 0,01 up to 1 micrometers) FIELD OF APPLICATION PURPOSE І at the enterprises and in research centers engaged The equipment is used to study physical and technical І fire protection systems: І pre-emergency monitoring of technological equipment in research and development in the field of fire hazard parameters, as well as to carry out setup, calibration in real time detection 28 – oil refining and pumping center and verification in the serial production of fire detectors, 29 – fuel storage sections, petrol station І operation reliability with a minimal false alarm probability including early warning fire detectors. І in educational institutions and special services – varnish-and-paint facilities warehouses І compatibility with modern chek-and-receiving panels of Emergencies Ministry – firework and pyrotechnic warehouses and computer – explosive hazardous locations ADVANTAGES І detection of power electronic equipment overheating І high-precision preparation of a gas mixture including wiring І automated process control systems: І wide range of gas mixture dilution ratio – explosion-proof electrical facilities І electroinduction technology І uniformity of generated aerosol concentration distribution – explosion-proof equipment І intellectual software – gas-turbine equipment І wide range of generated aerosol concentrations І patents: JSC “Radar mms” №2459268, №2530055 І PC control

Conformance certificate GOST R 53325-2012 І small dimensions С-RU.АЖ45.В.00021. SPECIFICATIONS Conformance certificate ТР ТС 012/2011 RU C-RU.BH02.B.00383 № 0340175. Aerosol weight concentration control range, mg/m3, from 0.05 to 50 no more than Dilution ratio range in preparation of a gas mixture from 1 to 1000 SPECIFICATIONS Maximum permissible relative error of aerosol ±20 Explosion-proof mark 1ExdIIBT6 concentration control, % Ingress protection rating IP54 Maximum permissible relative error in preparation ±4 of a gas mixture Sensitivity, mg/m3 from 0.01 to 100 Operating temperature range, °C from +15 to +30 Sensitivity, %/m from 0.0002 to 20 PC communication interface RS-485 Protected area, m2 100 Weight not exceeding, kg 219 Supply voltage, V from 10 to 28 Atmosphere pressure, kPa from 84 to 106.7 Power consumption, W 2.0 Dimension, mm 240х100х75 Operating temperature range, °С from -20 to +55 Interface RS-485, «dry relay contact» Life cycle, years 10 Warranty life, years 3 30 31

JSC Radar installed a laboratory for calibration, testing and verification of precision devices for pressure measurement, including the unique metrology equipment: І digital pressure controllers Ruska 7250xi and Ruska7252 that enable setting and measurement of pressure with a relative error of 0.005% І digital pressure controllers Wika CPC8000 with a relative error of 0.01% for various measurement ranges, the calibrator of air signal units Model 6300-M3 with a relative error of 0.007% І deadweight pressure gauge Wika CPB5000 with a relative error of 0.01% (of the measured value).

To ensure precision calibration and tests of products within the entire range of operating temperatures, the laboratory is equipped with thermal chambers and liquid thermostats that provide setting and regulation of temperature with a high accuracy of up to 0.01 °C. STABLE PRESSURE TRANSDUCERS PDS-A STABLE QUARTZ PRESSURE SENSOR DDKS-V-0.16

ADVANTAGES І high precision characteristics within the entire operating temperature range of up to 0.08% over the entire pressure measurement range, as well as in the initial section І high resolution І high resistance to external factors І domestic hardware components

PURPOSE Stable pressure transducers PDS-A are designed to operate as part of pneumatic hydraulic and other systems of ships and naval vessels for measurement and proportional transformation of measured absolute pressure of liquids and gases. OPERATING PRINCIPLE PURPOSE The sensor operating principle is based on variations of a Measurement of absolute air pressure at an altitude FIELD OF APPLICATION resonant vibration frequency of high-quality quartz resona- of aircraft flight. OPERATING PRINCIPLE Systems of surface ships and underwater vehicles. tor, which has long-term calibration curve stability, under the The operating principle of high-precision pressure transducers measured pressure impact. FIELD OF APPLICATION is based on variations of a resonant vibration frequency І existing and prospective aircrafts of high-quality quartz resonators, which have long-term ADVANTAGES calibration curve stability, under the measured environment І unmanned aerial vehicles pressure impact. І high precision characteristics within the entire operating temperature range of up to 0.02% over the entire pressure І WIG effect crafts measurement range, as well as in the initial section 32 33 SPECIFICATIONS І high resolution PDS-A-0.4-S PDS-A-6-T PDS-A-25-S І domestic hardware components Upper limit of measured absolute pressure (URL), MPa 0.40 6.00 25.00 І interference immunity in contrast to radio altimeter Lower limit of measured absolute pressure, MPa 0.03 0.03 0.10 Maximum allowable pressure, % URL 125 SPECIFICATIONS Maximum permissible error in the operating temperature ±0.08 ±0.08 ±0.08 range, % URL (±3.2 hPa) (±48 hPa) (±200 hPa) Upper limit of measured pressure (URL), kPa 160 Controlled environment Hydraulic fl uid Sea water Hydraulic fl uid Lower limit of measured pressure, kPa 0.5 (FHF) or air (FHF) Maximum allowable pressure, % URL 125 or air or air Limits of permissible error within the operating ±0.02 Controlled environment temperature range, °C from -30 to +50 from -30 to +50 from -30 to +50 temperature range, %URL from -4 to +32 (sea water) Controlled environment air Power supply voltage, V 27±5 Operating temperature range, °C from -60 to +85 Current consumption, mA, no more than 60 Power supply voltage, V 6.0+0.5 Output interface RS-485 Current consumption, mA, no more than 5 Sampling time, ms, no less than 800 Output interface CMOS, frequency Dimensions Ø 110х215 Ø 110х249 Dimensions, mm Ø 56х106 Weight, kg, no more than 2.7 2.3 3.1 Weight, no more than, kg 0.3 PRECISION PRESSURE CONTROL EQUIPMENT APKD-1 DIGITAL ELECTRONIC MODULE MDKS

OPERATING PRINCIPLE The operating principle of precision transducers is based on variations of a resonant vibration frequency of high-quality quartz resonators, which have long-term calibration curve stability, under the impact of measured environment pressure. One control unit enables to connect up to 20 transducers with a single cable and display information on screen. The display shows the pressure data from 4 transducers simultaneously with successive sampling of all transducers. Providing the external power supply, up to 31 transducers can be connected to a control unit.

ADVANTAGES PURPOSE І high precision characteristics within the entire operating The equipment is designed for high-precision measurement temperature range of up to 0.08% over the entire pressure and proportional transformation of measured absolute measurement range, as well as in the initial section pressure of liquids and gases into a digital binary sequential І high resolution code and its transmission to the upper level system. І sealed connector of transducers PURPOSE ADVANTAGES The pressure transducers are designed to measure outboard Measurement and converting of absolute pressure into a pressure at a depth of immersion of unmanned underwater І high precision characteristics within the entire operating digital output signal. vehicles as part of their systems for measuring pressure field FIELD OF APPLICATION temperature range of up to 0.02% over the entire pressure distribution under the cavity of air-cavity vessels or under the І autonomous unmanned underwater vehicles, measurement range, as well as in the initial section wing of a WIG effect craft, water level measurement in wells including gliders OPERATING PRINCIPLE І high resolution (when it is connected to a control unit of the atmosphere The operating principle of modules is based on variations of a І air cavity vessels resonant vibration frequency of high-quality quartz resona- 34 pressure sensor DADS-1 in order to compensate the impact 35 of atmosphere pressure), and as piezometers to control pore І WIG effect crafts tors, which have long-term calibration curve stability, under FIELD OF APPLICATION water pressure in the soil. the measured pressure impact. І portable pressure calibrators І water level measurement in wells, tanks, etc. І stationary pressure calibrators SPECIFICATIONS PDS-1 PDS-2 SPECIFICATIONS Upper limit of measured pressure, MPa 0.25; 0.6; 1,0; 2.5 Upper limit of measured pressure (URL), MPa 0.6; 1.0; 6.0 Lower limit of measured pressure, MPa 0.06 Lower limit of measured pressure, MPa 0.05 Maximum allowable pressure, % URL 125 Maximum allowable pressure, % URL 125 Limits of permissible measurement error within the operating temperature range, % f± 0.08 Limits of permissible measurement error within the operating temperature range, % URL ± 0.02; ± 0.05 Controlled environment sea water, air Controlled environment air Operating temperature range, °C – sea water from -5 to +40 Operating temperature range, °C from 5 to 50 – fresh water from 0 to +40 Power supply voltage, V 6.0+0.5 Power supply voltage, V 5.0+0.5 6.5+0.5 Current consumption, mA, no more than 45 Current consumption, mA, no more than 145 50 Dimensions, mm Ø 42х112 Output interface RS-485 Weight, kg, no more than 0.62 Sampling time, ms, no less than 200 600 Dimensions Ø 48х148 Weight, kg, no more than 0.6

CONTROL UNIT SPECIFICATIONS Operating temperature range, °C from -5 to +40 Power supply voltage, V 27±5 Note — BK-1 powers up to 20 connected PDS Current consumption (without PDS), no more than, A 0.2 Dimensions, mm 130х119.3х46.4 Weight, kg, no more than 0.35 WIRELESS BIOLOGICAL OBJECT MONITORING SYSTEM

PURPOSE OPERATING PRINCIPLE The biological condition monitoring system is based on wire- Sampling of sensors is performed by a wireless autonomous less invasive sensors designed for remote measurement of reader. The reader transmits a signal received by a sensor. local temperature inside the biological objects. The sensor emits a response signal received by the reader.

ADVANTAGES FIELD OF APPLICATION І absence of sensor power supply elements Early detection of recurrent tumors, relapse of infectious bone and visceral diseases. І no wires І medicine (traumatology, orthopedics, surgery, urology, І high accuracy oncology) 36 37 І large read range inside a biological object І agriculture (veterinary medicine, animal breeding) І biological compatibility

SPECIFICATIONS Temperature measurement error, °C ± 0.1 Temperature measurement range, °C from 35 to 42 Sensor read range, cm up to 20 Wireless reader operating time without recharging, h, more than 48 Sampling time of a sensor, s, less than 2 Dimensions, mm Ø from 5 to 18 Weight, g from 0.5 to 3 Ability of simultaneous sensor sampling, pcs 3 MICRO MOTION AND TEMPERATURE MEASUREMENT SYSTEM WITH IDENTIFICATION BASED ON SAW SENSORS*

MAIN SPECIFICATIONS OF MICRO MOTION SENSOR AD1001 Operating frequency, MHz 413 and 433 Read range, m up to 10 Micro motion measurement range, micron from 0 to 500 Micro motion measurement error, micron ±1 Micro motion measurement range up to 10 with use of a displacement transformer, mm Micro motion measurement error ±50 with use of a displacement transformer, micron Dimensions, mm 160х70х21,6 Weight, no more than, g 150 Operating temperature range, °C from -40 to +65 PURPOSE Temperature sensor AD1002: Dust and water protection rate IP54 The system is designed for wireless measurement І ambient temperature monitoring in infrastructural of the magnitude of infrastructural facility deformation facilities, explosion hazardous areas, areas with high and structural micro motions, as well as for wireless radiation, chemical and biological hazards, inside industrial MAIN SPECIFICATIONS OF THE TEMPERATURE SENSOR AD1002 measurement of ambient temperature in different facilities. installations, on equipment with strict environment conditions Operating frequency, MHz 413 Read range, m up to 10 OPERATING PRINCIPLE І temperature monitoring of high-voltage switchboards A reader generates sampling signals and radiates them Temperature measurement range, °C from -40 to +65 via an antenna. The micro motion sensor within the scope Temperature measurement error, °C ±1 of antenna in response to an interrogation signal transmits ADVANTAGES a response radio signal containing the data on the magnitude І high operating range along with permitted radiated power Dimensions, mm 256.6х26.2х5.5 of structural deformation, ambient temperature and unique Weight, no more than, g 22 38 sensor identification number (ID) which are determined І low reader radiation level 39 Dust and water protection rate IP68 by the reader and transmitted to external data processing І high radiation resistance of sensors (up to 6 Us) devices. І high resistance of sensors to high intensity electromagnetic fields SYSTEM CONFIGURATION MAIN SPECIFICATIONS OF READER І reader І wide temperature range of sensors operation Operating frequency, MHz 413 and 433 І antenna І service life of sensors no less than 10 years Read range of sensors, m up to 10 Dimensions, mm 200х114х56 І micro motion sensors AD1001 І high reliability Weight, no more than, kg 5.5 І temperature sensors AD1002 І absence of built-in power source of sensors І ability of sensors operation in severe and corrosive Operating temperature range, °C from -40 to +65 FIELD OF APPLICATION environment conditions Dust and water protection rate IP20 Micro motion sensor AD1001: Maximum radiated power, no more than, W no more than 2 І control of stress-strained state of infrastructural buildings Power supply voltage, V DC 12 and facilities, e.g. tunnels, overhead roads, bridges, oil External devices communication interface USB 2.0 pipelines, gas pipelines, railway track of roadways Number of connected antennas 1 І surveillance of critical and essential facilities

*SAW – surface acoustic waves TOUCH CONTROL CONSOLE WEIGHT SENSOR

PURPOSE ADVANTAGES PURPOSE ADVANTAGES An input device for control and delivery of various commands І possibility of using any glass (enhanced physical Control of the size of cargo carried by a vehicle І high measurement accuracy – error of no more than 0.2% to a computer and other electronic devices. and chemical methods, including armored) in time of loading. І high dynamic range: from 1.0 to 110 t І water and dust protection FIELD OF APPLICATION OPERATING PRINCIPLE І to ensure vehicle identification І tactile effect (an operator’s ability The operating principle is based on transformation of the І information control systems І possibility of remote automatic control to feel response from pressing) elastic sensor element deformation into an electrical signal, І integrated hardware control systems further conversion of the weight data into a digital format І no additional bundles for system installation І unification of touch panels by soft buttons for specific tasks І separate hardware control panels and transmission of received data via a radio channel. as part of the vehicle І ability to manufacture various sizes (up to 26 inches) FIELD OF APPLICATION SPECIFICATIONS І weight measuring equipment: measurement of large object weight Size, inch from 5 to 26 І automotive electronics: control of cargo weight transported Operating frequency, MHz 5.52 by road, vehicle axle load control 40 Response time, no more than, ms 20 41 І agricultural machinery: measurement of feed mixer Operating temperature mode, °C from -20 to +50 and transshipment silo weight Storage and transportation temperature mode, °C from -40 to +85 Service life, no less, million contacts 50 SPECIFICATIONS Connection interface USB, Ethernet, RS-485 Measurement error, no more than, % 0.2 Extended measurement range of controlled quantities up to 110 of transported cargo, t Operating range via a radio channel, m 30 Frequency range of the radio channel from 2400 to 2483.5 MHz ISM Type of design IP67 Material of elastic element stainless steel RADIO FREQUENCY IDENTIFICATION SYSTEM BLOCK DIAGRAM OF HARDWARE AND SOFTWARE SUITE BASED ON SAW RFID TAGS BASED ON A RADIO FREQUENCY IDENTIFICATION SYSTEM

Options of radio frequency identification system application: CONTROL І the stationary reader is used to control moving objects CENTER in the controlled area. The reader is mounted on a post, RFID TAG ANTENNA Ethernet the reader antennas are installed around the controlled READER perimeters. Up to two antennas can be connected RFID TAG ANTENNA to one reader.

І the mobile reader is used to identify the marking Wi-fi/3G COMMUTATOR SERVER RFID TAG PORTABLE READER of cargos and modular units SWITCH/ROUTER DB

ADVANTAGES RFID TAG ANTENNA Ethernet І open architecture READER PURPOSE RFID TAG ANTENNA AWS The system is used for wireless automated identification І modular design of objects, cargo, modular units, etc. for the purpose І the reading range is 3 times higher compared AWS of accounting, control and monitoring of the object state, with other radio frequency identification technologies organization of access control systems, integrated based on passive RFID tags AWS production automation systems. І low level of reader radiation MAIN SPECIFICATIONS OF SAW BASED RFID TAGS FIELD OF APPLICATION І high radiation resistance of RFID tags (up to 6 Us) Operating frequency, MHz 860, 915 І transport І high resistance of SAW based RFID tags to the impact RFID code information capacity, bit 32 І industry (automotive, aviation, nuclear, chemical, etc.) of strong electromagnetic fields Read range, m up to 70 І agriculture І wide operating temperature range of SAW based RFID tags in extreme conditions (from -60 °C to +125 °C) Dimensions depend on the fi eld of application І logistics І service life of the reader and RFID tags is at least 25 years Weight, g from 15, depending on the fi eld of application Operating temperature range, °C from -60 to +125, possibly up to 250 І high reliability SYSTEM CONFIGURATION Dust and water protection rate IP68 42 І reader І high interference immunity (due to new coding methods) 43 І antenna reader І impossibility of finding by a method of non-linear location MAIN SPECIFICATIONS OF STATIONARY READER І RFID tags (for various fields of application) І impossibility of unauthorized modification of a unique identification code of SAW based RFID tags Operating frequency, MHz 860, 915 RFID tags read range, m up to 70 OPERATING PRINCIPLE Dimensions, mm 250х200х112 Passive acoustoelectronic RFID tags based on surface acoustic waves are applied for object radio frequency identification Weight, kg, no more than 7 and mounted on the identifiable objects. Information about Operating temperature range, °C from -40 to +70 the object is read by the reader and transmitted to the control Dust and water protection rate IP54 unit. The request and response exchange occurs between reader antennas and transceiving antennas built in RFID tags. Average radiated power, mW, no more than 10 Power supply voltage, V AC 220, DC 24 External devices communication interface Ethernet Number of connected antennas, no more than 2

MAIN SPECIFICATIONS OF PORTABLE READER Operating frequency, MHz 915 RFID tags read range, m, no less than 2 Dimensions, mm 250х150х200 Weight, kg, no more than 1.5 Operating temperature range, °C from -10 to +50 Dust and water protection rate IP54 Average radiated power, mW, no more than 10 Power supply type from internal battery External devices communication interface USB, Wi-fi , 3G/4G, Bluetooth QUANTUM MAGNETIC ANOMALY DETECTOR QUANTUM GEOPHYSICAL MAGNETIC ANOMALY DETECTOR

PURPOSE ADVANTAGES PURPOSE ADVANTAGES Quantum magnetic anomaly detector is designed to measure High measurement accuracy. Quantum magnetic anomaly detector is designed to measure І small orientation errors the magnitude of complete induction vector of geomagnetic the magnitude of complete induction vector of geomagnetic field and its increments. FIELD OF APPLICATION field and its increments. І high sensitivity Magnetic recording, changing of magnetic variations І presence of a symmetrized line OPERATING PRINCIPLE in time, mineral exploration, search for wrecks. OPERATING PRINCIPLE The quantum magnetic anomaly detector is based The quantum magnetic anomaly detector is based on the principle of optical pumping on Mx signal on the principle of optical pumping on Mx signal FIELD OF APPLICATION (the light beam is perpendicular to the measured magnetic (the light beam is perpendicular to the measured magnetic Magnetic recording, changing of magnetic variations field) in the form of a self-generating transducer. field) in the form of a self-generating transducer. in time, mineral exploration, search for wrecks. Alkali metal vapors 133Cs are used as a working substance. Alkali metal vapors 133Cs are used as a working substance.

SPECIFICATIONS SPECIFICATIONS Magnetic fi eld induction measurement range, nT from 20000 to 100000 Magnetic fi eld induction measurement range, nT from 20000 to 100000 Working area, degree from 10 to 80 Working area, degree from 15 to 75 RMSD of a few measurements in a frequency 0.01 RMSD of a few measurements in a frequency 0.005 range of 1 Hz, nT range of 1 Hz, nT Power supply voltage, V from 21 to 35 Power supply voltage, V from 21 to 35 44 45 Current consumption, A Current consumption, A – at the time of switching-in 1.5 – at the time of switching-in 1.5 – after warm-up at a temperature of 20 °C 0.5 – after warm-up at a temperature of 20 °C 0.5 Dimensions, mm sensor: 75x75x105 Dimensions, mm sensor: 70x70x180 electronics unit: 135x87x67 electronics unit: 135x87x67 Material aluminum, latten, textolite, fl uoropolymer Material aluminum, latten, textolite, fl uoropolymer Interface Ethernet, RS-232 Interface Ethernet, RS-232 QUANTUM FOUR-CELL MAGNETIC ANOMALY DETECTOR FLUXGATE MAGNETIC ANOMALY DETECTOR

PURPOSE ADVANTAGES Quantum magnetic anomaly detector is designed to measure All-latitude, except for a narrow dead zone at the equator. the magnitude of complete induction vector of geomagnetic field and its increments. FIELD OF APPLICATION PURPOSE ADVANTAGES The fluxgate magnetic anomaly detector is designed І ease of operation І magnetic recording for measuring the magnetic field components that OPERATING PRINCIPLE in principle enables to use it for calculation of the magnetic І low power consumption The quantum magnetic anomaly detector is based І changing of magnetic variations in time field direction. І absence of dead zones on the principle of optical pumping on Mx signal І mineral exploration (the light beam is perpendicular to the measured magnetic І wide measurement range field) in the form of a self-generating transducer. І search for wrecks OPERATING PRINCIPLE Alkali metal vapors 133Cs are used as a working substance. The fluxgate is an electric coil, sensitive to the magnitude and direction of the external magnetic field, with a core made FIELD OF APPLICATION of soft-magnetic ferromagnet (such as permalloy), Mineral exploration, its use as an auxiliary measurement fed by an alternating current. channel to compensate magnetic interference of a carrier. SPECIFICATIONS Magnetic fi eld induction measurement range, nT from 20000 to 100000 Fluxgates are a type of ferro-inductive transducers with use of magnetic excitation. Working area, degree from 5 to 90 RMSD of a few measurements in a frequency 0.01 range of 1 Hz, nT SPECIFICATIONS 46 Power supply voltage, V from 21 to 35 Magnetic fi eld induction measurement range, nT ± 100000 47 Current consumption, A RMSD of a few measurements in a frequency range of 1 Hz 10 – at the time of switching-in 1.5 – after warm-up at a temperature of 20°C 0.5 Power supply voltage, V from 12 to 35 Dimensions, mm sensor: 125x125x115 Power consumption, W 3 electronics unit: 160x90x60 Dimensions, mm sensor: 200x40x40 Material aluminum, latten, textolite, fl uoropolymer Material aluminum, latten, textolite, fl uoropolymer Interface Ethernet, RS-232 Interface Ethernet, RS-232 SEARCH-AND-TARGETING SYSTEM «KASATKA»

PURPOSE EQUIPMENT CONFIGURATION І detection and identification of surface and, in particular, І all-round surveillance and side-looking radar small objects І mm-range radar І sea lanes protection support І onboard communication system connected І search and rescue operation support with a system designed for real-time data transmission to the control stations І economic zone monitoring І electro-optical system І environmental monitoring of seas and oceans І magnetic anomaly detection system ADVANTAGES І radio sonar system І open architecture І dipping sonar system І modular design І information control (command and tactical) system І unification to various types of carriers І rescue equipment І proprietary software І electronic intelligence system 48 І intelligent decision-making support system 49

LIST OF SEARCH-AND-TARGETING SYSTEMS INFORMATION CONTROL SYSTEM KASATKA-B KASATKA-VB KASATKA-S KASATKA-SB KASATKA-BP KASATKA-A

Special search- Special search- Special search- Special search- Special search- Special and-targeting and-targeting and-targeting and-targeting and-targeting aerostat based system for system for system for system for system for search-and- shipborne shipborne short-range long-range unmanned targeting helicopters helicopters patrol aircrafts patrol aircrafts aerial vehicles system up to 6.5 t up to 12 t from 25 to 60 t more than 60 t INFORMATION CONTROL SYSTEM AUTOMATED WORKSTATION

PURPOSE FIELD OF APPLICATION І implementation of generalization and integrated processing Solving problems in the interests of law enforcement algorithms of the data received from STS systems agencies, various ministries and agencies. І formation of single information and control field for a flight crew ADVANTAGES І high system reliability provided by redundant І to provide STS systems with the data necessary for their communication lines and functional redundancy operation (piloting and navigation, mapping, geographic of computing tools and UAWS surveillance data, etc.) І modular design that ensures ease of increasing functionality Unified automated workstation (UAWS) is a tool of STS ADVANTAGES І formation of a single local area network of data and using new types of systems operators work automation. transmission to STS to ensure prompt data interaction І application of modern high-performance computing І single local computer network that ensures uniformity systems as part of UAWS between onboard systems PURPOSE of systems and suites connection І application of aircraft displays with high brightness І to provide unified tools for creating and immediate changes І automation of STS operators work on different types І principle of integrated data processing that enables and resolution that provide operators with ergonomic (corrections) of flight missions (reconnaissance plans) of aircrafts integrated situation assessment, fullest operator’s information display І to provide computing, control and information resources awareness of the relevant situation І to provide operators with information and tools І wide range of UAWS modifications required for operation of STS airborne avionics systems of STS control І inclusion of a carrier into common information control І lightweight of UAWS due to the use of composite materials І geoinformation coding of the data from the airborne space while performing search-and-rescue operations І to provide operators with the necessary comfort level reconnaissance equipment in all flight conditions according to all requirements І ability to use in severe service conditions І high automation degree achieved due to the decision- of regulations (GOST RV 20.39.304-98 group 2.4, 3.1, 3.2) 50 І formation of a tactical information display tablet (TIDT) making support system 51 І intelligent decision-making support in the typical tactical І high maintainability and availability of modernization due situations FIELD OF APPLICATION to modular construction design Application on different types of aircrafts (airplane, helicopter І formation of formal documents І versatility - in the process of ICS problem solving in case systems, etc.) to ensure interaction of operators with ICS of failure of one of workstations all its problems can be І preparation of data cards for transmission to the interacting and STS. quickly transferred to another workstation objects and control stations І STS systems and components monitoring І data recording in the documentation system І to provide formalized message exchange VHF SIDE-LOOKING RADAR “RAZREZ”

PURPOSE ADVANTAGES SL radar “Razrez” is designed to perform radar surveillance І application flexibility and operational efficiency of vast ground and water surface regardless of weather conditions, time of day and year. І high performance І ability to receive radar images for different combinations FIELD OF APPLICATION of emitted and received signal polarization І detection of various types of objects and facilities, І independence from weather conditions and time of day hidden by dense vegetation or buried in the ground І accurate geo-referencing of received images І search and rescue operations by the elements of metal structures either on the sea under severe weather conditions or on ground during the search of expeditions in distress in hard-to-reach areas, hidden by dense vegetation І environmental monitoring: monitoring of oil leaks in pipelines, defining the area of flammable and liquid chemical leakage during disasters of ships, planes and trains with flammable substances and chemicals І geological mapping during mineral exploration, designing and laying of pipelines routes І water resources control: the construction of groundwater distribution and accumulation areas, identification of the hidden process of economic land subsoil flooding І forest resources control

52 SPECIFICATIONS 53 Surface surveillance side-looking Wavelength, m 2.3 Polarization of a signal (emission/reception) H/H, H/V, V/V, V/H Width of physical antenna DD, degree – azimuth H/V 63/85 – vertical H/V 103/62 Radiated power (pulse), W 1000 Probing signal parameters: – modulation type LFM – probing pulse duration, ms 15 – repetition period, ms 250 Resolution, m from 10 to 15 Range coverage (one side), km 7.5 Operating distance range, km from 3 to 20 Weight, kg – stands with units 45 – antenna (one side) 35 Power consumption, W 500 Interface Ethernet, RS-232 AIRBORNE RADAR SYSTEMS X-BAND ALL-ROUND LOOKING HELICOPTER-BORNE AESA RADAR

SPECIFICATIONS Weight, kg 100 Dimensions, mm 980х380х510 Average power consumption, W 3800 PURPOSE ADVANTAGES External interface RS-485, Ethernet, Arinc Radar systems are designed to detect air, ground, surface І new industrial technology for creating radars Detection range, km / based on RCS, m2 150/250, 80/3 objects, as well as to identify the underlying surface based on APAA topography, weather formations. Operation modes MTI, surveillance, SAR І new beam control system which provides digital FIELD OF APPLICATION beamforming in the broad scanning sector in both planes І as surveillance radars in ground, water surface and airborne І new design of 4-channel digital receiver-transmitter module X-BAND SECTOR SCANNING AIRPLANE-BORNE AESA RADAR systems of water surface, ground and air monitoring which provides interoperability in manufacturing and operation І as ground flight support radars such as surveillance, dispatching, landing and airport area surveillance І new inertialess surveillance technology in the wide (up to 2100) sector of azimuth angles І as shipborne radars, i.e. to be mounted on marine and river vessels for passenger commercial fleet and Navy І unification, i.e. changing its software enables a tool for solving many navigation and location problems І integration of multiple radars (with different software and, as a consequence, different functionality) in the radar group (RG) significantly reduces the costs of staff / personnel training, operation of this equipment and acquisition (for bulk order) SPECIFICATIONS Weight, kg 216 Dimensions, mm 1000х800х820 X-BAND SECTOR SCANNING AIRPLANE-BORNE AESA RADAR Average power consumption, W 10000 “PODKRILOK” External interface RS-485, Ethernet Detection range, km / based on RCS, m2 250/250, 80/3 54 Operation modes MTI, surveillance, SAR 55

X-BAND ALL-ROUND LOOKING RADAR “FLUGER”

SPECIFICATIONS Weight, kg 170 Dimensions, mm 1150x500x1000 Average power consumption, W 5700 External interface RS-485, Ethernet, Arinc 2 Detection range, km / based on RCS, m 60/1 SPECIFICATIONS Operation modes MTI, surveillance, SAR Weight, kg 80 Average power consumption, W 2.5 Detection range, km – 1 m2 30 – 1000 m2 150 Operation modes MTI, circular, sector, SAR, ISAR, meteo X-BAND SIDE-LOOKING RADAR W-BAND LANDING RADAR “VIDIMOST-2000”

PURPOSE ADVANTAGES “Vidimost-2000” radar is an airborne station providing І high angular resolution that enables to display low contrast the safety of aircraft flight, takeoff and landing according (small targets) and non-contrast objects (runways, to the category 3A, 3B, 3C ICAO, taxiing on the airfields. taxiways) against the ground surface The radar provides as follows: І high accuracy of angular coordinates measurement І detection of runways and landing support under low optical visibility in adverse weather conditions І high spatial selectivity that enables to solve tasks as follows: PURPOSE ADVANTAGES І all-weather detection and, if necessary, warning the crew – autonomous all-weather, under zero optical visibility, The radar is designed for terrain radar imaging with high І calibration of radiation path/probing signal reception power about the obstacles (topographic inequalities, cables, poles, detection and reception of reliable high accuracy data resolution and measuring the reflection characteristics pipes, buildings, etc.) on the relative positions of an aircraft and a runway; І possibility of changing signal polarization of artificial and natural objects. – real-time detection and displaying of small-sized equipment І search and rescue operations at sea and on ground І possibility of changing the probing signal modulation on the land background in the aircraft motion direction; FIELD OF APPLICATION parameters within a wide range – electromagnetic compatibility; І radar monitoring of ground and sea surface І possibility of implementing various types of underlying OPERATING PRINCIPLE – approach to a boarding ramp, etc. Coherent forward-looking radar with complex 3-mm range І measuring the reflection characteristics of artificial surface scanning radar signal is installed in the nose section along the aircraft and natural objects FIELD OF APPLICATION axis. The radar has no control and data display, though Newly developed and modernized aircrafts of civil І full-sized development testing of multipurpose radar the control and data display is provided on the carrier in-built (local aviation), military and special purpose, designed operation modes tools. The radar performs functions as an element of artificial for landing on unequipped or ill-equipped airfields. vision, for what the radar data output is provided in the form of primitives and data on the windshield display. SPECIFICATIONS Surface surveillance side-looking, forward-side, sector SPECIFICATIONS Wavelength, cm 3.2 Operation distance range, km from 0.1 to 15 Polarization of a signal (emission/reception) H/H, V/V 56 Operating wavelength range W 57 Width of physical antenna DD, degree 8 Detection range in good and adverse weather conditions, km: Radiated power (pulse), W 300 – runways from 3 to 6 Probing signal parameters: – runways with ground markers (corner refl ectors) from 10 to 15 – modulation type PAM, LFM, CPM – airfi eld infrastructure (buildings, facilities) from 6 to 8 – probing pulse duration, ms from 0.2 to 25 – automotive vehicles from 4 to 6 – repetition period, ms from 100 to 1000 – aerotechnics on the ground from 4 to 6 – people from 0.5 to 1.0 Resolution, m <1 – cables from 1.5 to 2.0 – relief inequalities from 2 to 4 Coverage area on distance, km from 3 to 30 Resolution: Operating interval of distances, km from 3 to 150 - distance, m 8 Weight, kg 45 - azimuth, ° 0.3 Power consumption, W 500 Surveillance sector relative to the construction line: – azimuth, ° ±45 Interface Ethernet, RS-232 – elevation, ° ±30 Operating angles range of roll, pitch, ° ±30 Radar weight, no more than, kg 25 Radar dimensions without display/control devices, mm 380х625х500 Power supply 3-phase network 115/208 V, 400 Hz Power consumption, W, no more than 300 Interface (if necessary any other interfaces are available upon Arinc, Ethernet customer’s request) W-BAND LANDING SMALL-SIZE RADAR “PESOK” X-BAND SECTOR SCANNING SMALL-SIZE RADAR “MRLS-01”

PURPOSE ADVANTAGES Information support for safe takeoff and landing under low І small dimensions optical visibility, avoidance of collision with interfering and dangerous objects, monitoring of spatial position relative to І easy installation PURPOSE ADVANTAGES the ground surface, providing spot landing. It is designed for detection and position finding of sea and І small dimensions, weight and power consumption І all-weather and round-the-clock operation ground targets; radar imaging of the underlying surface with high resolution in artificial aperture antenna synthetic І open architecture, compatibility with airborne equipment OPERATING PRINCIPLE І landing under conditions of sand, dust, water splashes, snow storms mode when it is used as part of UAV and other aircraft of different aircrafts The radar consists of two horn antennas, mounted above airborne equipment. the radome, that provide the constant monitoring of space І detection of obstacles, small-sized interfering objects between a helicopter and the ground. Due to the features on the underlying surface background of 3-mm range radar waveband, a reflected radar signal, FIELD OF APPLICATION received by the antennas, after processing enables to detect І search, detection and auto tracking of ground and determine with high precision the coordinates of either FIELD OF APPLICATION and sea targets ground surface elements or hindering (dangerous) objects, Newly developed and modernized helicopters of all classes, І radar monitoring of ground and water surface including small-sized objects, which is unattainable in other sizes and purposes (civil, military and special), i.e. strike, wavebands. Information about the presence of dangerous reconnaissance, rescue, transport, medical, fire, monitoring, objects and its position, as well as the distance to the ground etc., ground-based and shipborne. SPECIFICATIONS surface and its position relative to the helicopter axes can be provided to the pilot (navigator) in a convenient form for him. Type of underlying surface surveillance side, sector Wavelength range X Moreover, it provides the safety of takeoff and landing under Width of scan sector in azimuth, degree ±45 low optical visibility, especially in particularly dangerous environment such as sand, dust, water splashes, snow Signal polarization (emission / reception) H/H storms, as well as prevents collisions with interfering or Width of physical antenna DD, degree 9 dangerous objects, provides control of the spatial position Radiated power (pulse), W 64 relative to the ground surface, spot landing. Probing signal parameters: – modulation type PAM, LFM, CPM – probing pulse duration, ms from 0.1 to 25 58 SPECIFICATIONS – repetition period, ms from 100 to 300 59 Operating distance range, m from 3 to 300 Resolution, m <1 Operating wavelength range W Maximum range, km up to 40 Detection range in good and adverse weather conditions, m: Weight, kg 8 - relief inequalities from 50 to 100 - automotive vehicles from 100 to 300 Power consumption, W 150 - corner refl ectors from 200 to 250 Dimensions, mm 412х227х127 Resolution: - azimuth, ° ~8 - distance, m ~8 Level surface range error (LSRE), m from 1 to 2 Surveillance sector: - azimuth, ° 360 - elevation, ° ± 4 Radar weight, no more than, kg 5 Radar dimensions without display device, mm Ø 270х150 Power supply, V +27 Power consumption, W ~120 Interface (if necessary any other interfaces are available Arinc, Ethernet upon customer’s request) SYSTEM OF GEOSPATIAL DATA INTERACTIVE VISUALIZATION OPERATING PRINCIPLE SPECIAL AUTOMATED OPERATOR WORKSTATION FOR SYSTEMS OF FLIGHT MISSION PLANNING AND GEOSPATIAL DATA PROCESSING

PURPOSE Operator special AWS is designed for the operator’s work with automated flight mission planning (AFMP), geospatial and special data processing systems. AFMP system is designed for solving the following tasks: І flight mission planning on the mapping basis in automated or fully manual mode І verification and control of completeness and quality of application planning data support І parameters calculation and formation of flight mission data base І feasibility testing and flight simulation according to the formed task and with account of payload operation OPERATING PRINCIPLE PURPOSE System of interactive visualization enables to display The system of interactive data visualization with multiple geospatial data, video data and other special data on the access is an interactive screen with a set of special software OPERATING PRINCIPLE CONFIGURATION shared screens. The system also enables to manage the which can also include the data display means. AFMP and geospatial and special data processing system І computer equipment displayed data structure and view, edit geospatial data, and The system is designed for: provides necessary information on the working area, І lockable metal safe for document storage solve geodetic and specific tasks. І geospatial data visualization and processing visualizes geospatial data, including three-dimensional terrain with the possibility to display and edit additional data layers model, and provides the operator with tools for flight mission І individual lighting formation and verification. ADVANTAGES І display, application and analysis of georeference data І mounting bracket for monitors І wide range of data display means, e.g. projectors І two monitors with a diagonal of 21 inches and video walls, enables to afford an access І display of specific data and its content management FIELD OF APPLICATION to the specific data for a required number of persons Command posts and centers of piloted and unmanned aerial І internal uninterruptible power supply vehicles application planning. І large touch panel enables to display the data set SYSTEM CONFIGURATION І cable set and provides an intuitive interface of data management І computer module with assembled screen and touch panel ADVANTAGES Additionally, it is possible to install a voice communication І multi touch allows several operators to work simultaneously І bearing for installation І AFMP system enables to reduce FM preparation time with the system system for operators. Special AWS doors and safe are locked І special software and minimize the error probability due to the computer- and sealed to prevent unauthorized access. controlled monitoring of flight mission feasibility FIELD OF APPLICATION І it can be supported with multiple-access data display equipment І geospatial and special data processing system enables Command posts, analytical and situational centers. using the most relevant sources of information on the area for task solution SPECIFICATIONS Software suite – operating system Windows 8.1 SPECIFICATIONS 60 – special software for geospatial data visualization Software suite – operating system Windows 7/MAFS 5.0/AstraLinux 61 and tactical situation presentation – special software for automated fl ight mission planning Screen diagonal and resolution 55”, 1920x1080 pixels and geospatial data processing Sensor type and number of touches infrared, 32 touch Dimensions, mm 1600х1200х800 Processor AMD A10 Total weight, kg up to 120 Video card Radeon R7 integrated in the processor Materials laminated chipboard, aluminum alloys RAM size, Mb 8192 ROM size, Gb SSD 120 Power consumption 300-500 Material acryl Dimensions, mm 1320х707х1156 Total weight, kg 88

Hardware-in-the-loop simulation systems developed by JSC Radar mms are designed for survey, testing and debugging SOFTWARE BUS “WBUS” of full-scale software and hardware systems, as well as consist of the hardware and software tools required to perform any work as intended. The software bus “WBUS” is designed as a universal solution SUPPORTED OPERATING SYSTEMS in the framework of developing the hardware-in-the-loop The tools for development of hardware-in-the-loop simulation systems include: І Windows (from Windows 8.1 and higher, Windows 7 simulation systems to provide high-frequency data with limited functionality) І software bus “WBUS” — cross-platform application that І scripts to connect metamathematical models, transmission with low latency that enables to safely enables to simplify work with network protocols and safely a tool for converting mathematical models performed and securely interconnect applications and systems. І Linux (32/64, Intel/ARM/MIPS/PowerPC, including special integrate any applications and systems in Matlab Simulink versions such as MAFS and AstraLinux Smolensk) The software bus “WBUS” is independent software І MacOSX (from 10.10 and higher) І universal simulator environment that enables to edit І loading system for control tools and supplied as a particular product. any settings of performed test І analog, discrete and power signal switching І RTEMS (4.11 and higher, Intel/ARM/MIPS/PowerPC/SH4) І editor MFI that enables to create graphic simulators and processing units PURPOSE І support of any operating system with working TCP/IP stack of any instrumentation with addition of metamathematical І test environment during aircraft development logic models І support of specialized low-frequency technology І basis for simulator development with TCP/IP stack І to use as “messaging systems” (message queue) that is an alternative to ZeroMQ, IBM MQ ADDITIONAL FUNCTIONALITY and its prototypes І standard screen compression algorithms with imaging of devices used in aircraft, without loss of accuracy FUNCTIONALITIES (radars, etc.) І high performance: up to 100 000 features at a frequency І method of audio data transmission and recording (for of 100 Hz aircraft communication system simulation) І guaranteed delivery І technology for rapid creating of graphic interfaces which visualize and modify the data transmitted І simulation of technologies applied in aviation, i.e. via WBUS system ARINC-429, ARINC-664 (AFDX), ARINC-818 (FC-AE) І “data spoofing” technology which enables to test failures of separate systems without making changes to them І total bus condition control which enables prompt connection to data streams І recording and subsequent reproduction of all data streams І IPv4 and IPv6 support І technology for rapid creating of graphic interfaces which visualize and modify the data transmitted via WBUS system

62 63 EDITOR MFI CONTROL LOADING SYSTEM

Editor MFI is a software system designed for developing The adaptive capability of Editor MFI is integration The control loading system is designed in the framework CONTENTS OF DELIVERY simulators of airborne instruments, displays and panels. of a mathematical model, which simulates the logic of developing hardware-in-the-loop simulation systems І servo drives and servo motors with cable network of device, panel or indicator operation, into the graphical and based on the use of readily available production Editor MFI consists of a frame editor running under the interface at the development stage. servo motors and servo drives. І computer operating system Windows 7 or higher, and software players І software bus for devices running under the operating systems Windows, The graphic device simulators developed in Editor MFI can The design is based on the use of inertialess special purpose Linux, MacOS X. be optimized for use in embedded systems and support work servo motors with a number of discretes per 1 turnover І converting model script for Matlab with SOC based on Intel Atom and ARM. not less than 1 200 000. І typical (basic-test) control law model Editor MFI enables to create graphic simulators: І any pointer indicator, including artificial horizon and flight Optimization is performed at the development stage and Typical implemented software modes (control laws) navigation instruments tested in real time mode at any stage of the simulator of operation: creation. І positioning on speed and angular coordinates І mechanical switches, toggle switches, protective caps, signal indicators of light displays, etc. І spring mechanism І frames of multifunction indicators І constant or variable load within the kinematic connection diagrams І frames of radars and meteoradars І pendulum motion І cartographic frames with mapping data drawing from both vector and raster maps І reverse reaction to the load impact І interactive mnemonic diagrams І “Shaker” mode simulation, sinusoidal vibration

SPECIFICATIONS Type of system Rated torque, Nm Rotor inertia moment, kg/m² (Е-4) Rated motor power, kW Motor weight, kg Type А from 0.64 to 12.70 from 0.177 to 0.300 from 0.20 to 0.40 from 1.2 to 2.0 Type B from 1.27 to 23.90 from 0.680 to 1.180 from 0.40 to 0.75 from 2.1 to 3.8 Type C from 3.18 to 127.40 from 2.650 to 4.953 from 1.00 to 2.00 from 4.3 to 7.2 64 65 MOBILE RADAR SYSTEM ULTRA-WIDEBAND RADARS

PURPOSE FIELD OF APPLICATION PURPOSE FIELD OF APPLICATION The mobile radar system, including ultrashort pulse radar Radar, radiocommunication. UWB radar is designed for construction of UWB radar Radar, construction of on-board UWB radars. (USP radar) and ultra-wideband radar (UWB radar), is designed based on APAA. for radar measurement of objects and environment, ADVANTAGES as well as research of communication system building OPERATING PRINCIPLE based on USP and UWB systems. І high resolution capability of USP radar. Selection of mobile and moving targets, polarization selection of background Scaleable APAA with solid state digital transmitter-receiver. USP and UWB radars can be used as separate components noise and underlying surface depending on assigned tasks. І Stealth technology overcoming, visibility beyond SPECIFICATIONS the obstacles, target detection in forest areas Frequency range Х OPERATING PRINCIPLE and dense vegetation One channel pulse power, W 10 The USP radar system uses electromagnetic pulses which І high rate of data transmission in radio communication tasks are generated by the transmitting antenna at its excitation Quantity of channels (APAA elements) from 4 to 16 І stealthiness of UWB radiated signal and actual operation by the USP generator forming a nanosecond video pulse. Range resolution, m, not less than 1 of USP radar Beam scanning mode APAA Pulses are reflected from targets, received by the receiving І integration and simultaneous operation of several patchwork antenna array and transmitted to the analog receiver input. systems under SDR technology (e.g. radar, communication PC communication interface RS-485 Next, the applied analog-to-digital converter (ADC) converts system and functional suppression) Noise ratio, dB 3.8 them to a digital form which is processed by a processing unit. І high resolution of UWB radar Bandwidth, MHz 1000 UWB radar system uses electromagnetic pulses generated І selection of mobile and moving small targets Pulse power, W 10 by the transmitting antenna, to which the phase-shift keyed signal is fed. Pulses are reflected from targets, received І detection and tracking of small-size fast maneuvering Pulse ratio 10 by the receiving antenna array and transmitted to the analog targets Weight, kg 1.8 receiver input. Next, ADC converts them to a digital form І simplicity of construction and small weight-size parameters Dimensions, m 0.4х0.2х0.04 and processed by a processing unit.

CONFIGURATION І ultrashort pulse radar І ultra-wideband radar І ultra-wideband antenna module 66 67 І ultrashort pulse antenna І data processing and displaying unit І analog-to-digital converter І UWB receiving-transmitting module І USP transmitting module USP ANTENNA MODULE UWB ANTENNA MODULE

PURPOSE FIELD OF APPLICATION PURPOSE ADVANTAGES It is applied in receiving, transmitting or transmitting- Development of array antennas based The UWB antenna module can be used in receiving, І simple design and small dimensions receiving antenna devices in radio technical systems on the USP antenna module. transmitting or transmitting-receiving antenna devices of various purposes, as well as for phased array antennas in radio technical systems of various purposes, І high mechanical strength development. in particular for phased array antenna development. ADVANTAGES І design modularity which allows to easily scale the elements quantity while developing APAA It has extended functionality when using for signal radiation І simple design and small dimensions It has extended functionality when using for signal radiation (reception) with horizontal, vertical, linear and circular (reception) with horizontal, vertical, linear and circular І high mechanical strength polarization. polarization. FIELD OF APPLICATION І design modularity which allows to easily scale Construction of APAA based on the UWB antenna module. the elements quantity while developing array antennas OPERATING PRINCIPLE OPERATING PRINCIPLE The antenna module performance is based on the antenna A feature of this antenna module is that circular polarization shock excitation while giving on it an ultrashort pulse antenna module has two UHF inputs, each of which generates generated by the USP transmitter module. a free-space linearly polarized electromagnetic wave.

The electromagnetic waves, excited by a radiating element, SPECIFICATIONS are mutually orthogonal. Frequency range, GHz from 0.2 to 3 Therefore, it is possible to control the polarization of emitted Polarization linear, circular (received) signal by controlling the excitation signal phases. DD width 70 VSWR 2.0 SPECIFICATIONS Weight, kg 1.3 Frequency range, GHz from 8.8 to 9.8 Dimensions, m 0.5x0.4x0.03 Polarization linear, circular DD width 70 VSWR 2.0 Weight, kg 0.3 Dimensions, m 0.18x0.08x0.1

68 69 RECEPTION AND PROCESSING UNIT ANALOG-TO-DIGITAL CONVERTER

PURPOSE PURPOSE І radar signal reception, digitizing, primary processing І signal digitizing and primary processing І signal transmission for further processing І signal transmission for further processing

SPECIFICATIONS SPECIFICATIONS Receiver sensitivity, dB 60 ADC sampling frequency, MHz from 250 to 500 Frequency band, 1 GHz 1 Number of ADC digits до 12 ADC sampling frequency, MHz from 250 to 500 Buffer RAM, MB 40 Number of ADC digits up to 12 Interface Ethernet Buffer RAM, MB 40 Weight, kg 2 Interface Ethernet, RS-485 Dimensions, m 0.2х0.2х0.2 Weight, kg 10 Dimensions, m 0.7x0.5x0.2

DATA PROCESSING AND DISPLAYING UNIT

USP TRANSMITTING MODULE PURPOSE І secondary radar data processing PURPOSE І radar data displaying Formation of nanosecond pulses. І data recording and reproduction І displaying and diagnostics of module functional control

SPECIFICATIONS USP amplitude, V 1000 SPECIFICATIONS Repetition frequency, MHz up to 2 USP amplitude, V 1000 Minimum pulse ratio 10 70 Repetition frequency, MHz up to 2 Weight, kg 0.8 71 Minimum pulse ratio 10 Dimensions, mm 120x250x30 Weight, kg 0.8 Interface Ethernet, RS-485 Dimensions, m 0.12x0.25x0.03 CPU clock frequency, GHz 3.2 RAM size, GB 32 ROM size, TB 1 Weight, kg 12 Dimensions, m 0.7x0.5x0.2 FREQUENCY DRIVING MODULE М411239 GENERATOR GK347-TS

OPERATING PRINCIPLE FIELD OF APPLICATION PURPOSE FIELD OF APPLICATION The frequency driving module is performed on the basis The frequency driving module can be widely applied Generator GK347-TS is designed for forming continuous Generators find wide application in products which require of SAW resonator. in products which require frequency formation or conversion. sinusoidal UHF oscillations. frequency formation or conversion. These products can be signal receivers-transmitters, frequency exciters and PURPOSE These products can be signal receivers-transmitters, ADVANTAGES converters. The generators as driving or reference generators Frequency driving module M411239 is designed for forming frequency exciters and converters in radar systems. In contrast to traditional surface acoustic wave devices, can be applied as self-dependent products. continuous sinusoidal UHF oscillations as a part of devices Also the modules can be used as driving or reference a new generation of UHF acoustoelectric devices with common sealing. generators. (HBAR - high overtone acoustic resonator), with use OPERATING PRINCIPLE of thin-film piezomaterials (AlN, ZnO), enables to develop Generator GK347-TS is developed on the basis ADVANTAGES higher frequency ranges. of a thermostatic HBAR resonator. It has no similar equals. In comparison with existing prototypes the frequency driving module M411239 SPECIFICATIONS has the following advantages: І higher operating frequency range no less than no more than Operating frequencies, GHz І low relative spectral density level of phase noise power liter 1 0.7 1.1 liter 2 1.1 1.5 liter 3 1.5 1.9 SPECIFICATIONS liter 4 1.9 2.4 Range of nominal frequencies, GHz from 1.0 to 2.5 Relative frequency instability, rel. unit -2•10-4 2•10-4 Frequency instability in operating temperature range, not more than, х10-6 ±190 Output power, mW 10 – Short-term frequency instability per 1 s, 10-8, not more than ±5 Relative spectral density of phase noise power with tune-out – liter 1: no more than -120 from carrier 10 kHz, dB/Hz liter 2, Liter 3: no more than -115 Relative spectral density of phase noise power with tune-out from carrier Δf, dBc/Hz, liter 4: no more than -110 not more than – 100 Hz -80 Harmonic and sub-harmonic components, dB – -15 – 1000 Hz -100 – 5000 Hz -115 Output VSWR – 1.5 Current consumption at supply voltage 12 V, mA 50 Current consumption, mA – 300 (up to 500.0 during 1 minute) Output power, not less than, mW 0.05 Relative level of supplementary spectral components within the – -60 Load impedance, Ohm 50 output signal spectrum fp in fp band ± 5.0%, dB Dimensions, mm 40х32х12 Wireless sealing on output signal 70.0 – Weight, g 40 Generator warm-up time, min – 5 72 Dimensions, mm 85х45х68 73 Weight, g 150 CHIRP SIGNALS FORMING-COMPRESSION UNIT GENERATOR GPAV-K5

OPERATING PRINCIPLE ADVANTAGES PURPOSE FIELD OF APPLICATION The forming-compression unit forms a chirp signal The achieved duration of a compressed chirp signal is less Generator GPAV-K5 is designed for forming continuous GPAV-K5 generator is used as a part of the interrogator by the digital method and compresses a formed chirp signal than 3.5 ns that enables to increase distance resolution sinusoidal UHF oscillations as a part of devices appliance of government integrated fried or foe identification by the analog method. up to 0.5 m. with common sealing. system.

PURPOSE FIELD OF APPLICATION OPERATING PRINCIPLE ADVANTAGES The forming-compression unit is designed for using The forming-compression unit is applied in various radars. Generator GPAV-K5 is based on the generator It has no complete equals. In comparison with existing as a part of various radars. with a SAW resonator. prototypes the generator GPAV-K5 has the following advantages: SPECIFICATIONS І small dimensions Central frequency of formed chirp signal, MHz 700 І low weight Width of formed chirp signal spectrum (deviation), MHz 500 Formed chirp signal duration, ms 1.5 SPECIFICATIONS Output signal power level, mW, no less than 1.0 Output frequency, MHz 1532,0 ± 0,4 Duration of compressed chirp signal at the level of -3 dB, ns, 3.5 Supplementary spectral components cancellation in the 30.0 no more than frequency band +200 MHz from a carrier frequency, dB, no less than Compressed chirp signal side lobe rejection, dB, -26 no more than Second harmonic level of a carrier frequency, dB, -10,0 no more than Dimensions, mm 218х164х83 Current consumption via secondary power supply 80 Weight, kg 1.72 circuit 12 V, mA, no more than Output signal power level, MW from 0.77 to 3.15 Output power unevenness (within a temperature range 3.0 from -60 to 80 °C), dB, no more than Dimensions, mm 50х31.5х12 Weight, g 49

74 75 SURFACE ACOUSTIC WAVE RESONATOR SURFACE ACOUSTIC WAVE FILTER

PURPOSE ADVANTAGES PURPOSE ADVANTAGES It is used as a frequency driving element in reference І high frequency stability in time and temperature range Bandpass filtering of high-frequency electrical signals. І small dimensions (twice-third as smaller than frequency generators. electromagnetic equals) І ability to achieve low phase noise in frequency driving modules (generators) FIELD OF APPLICATION І high temperature stability FIELD OF APPLICATION Reception-transmission paths of high-frequency devices High-frequency reference frequency generators. І high quality (radars, communication systems, etc.) І wide range of operating frequencies (1.0 MHz – 3 GHz) І high level of allowable power dissipation І low insertion loss of 1.0 – 3.0 dB with bandwidth 1-3% OPERATING PRINCIPLE OPERATING PRINCIPLE In a surface acoustic wave resonator the electrical signal І high resistance to external mechanical impacts The surface acoustic wave filter has input and output. The І high reliability is converted into a surface wave which passes through the І small dimensions original signal comes to the input, then the filter cuts out a І parameter repetition and low cost of serial production system of resonant reflective structures, and then converted specified frequency band, and then the filtered signal comes again into an electrical signal. І high reproducibility to the output. І resistance to the impact of special factors with characteristics 7I1, 7I6, 7I7 in performance group 1Us Filtering is performed by converting an electrical signal into according to the Russian State Standard RV 20.39.412.2 an acoustic wave and back into the electrical signal after passing through the filter elements. SPECIFICATIONS Rated frequency, MHz up to 1600 (upon the customer’s request) Insertion loss, dB, no more than 11 SPECIFICATIONS Quality factor, no less than 5000 Pass bandwidth rated frequency under normal environmental 868, 915 conditions (F )1), MHz Long-term frequency stability ±10-6 0 Pass bandwidth at the level of -3 dB, MHz from 25 to 352) Operating temperature range, °C from -60 to +85 Insertion loss at rated frequency, dB, no more than 3 Body type TO-39, metal-and-glass Bandpass fl atness in guaranteed bandwidth, dB, 1 Dimensions, mm 6.00х9.22х9.22 no more than Weight, no more than, g 0.91 Pass bandwidth at the level of -35 dB (BW-35), MHz, 70 no more than Guaranteed attenuation in the frequency range: 35

from 100 MHz to F0 – BW-35/2 and from F0 + BW-35/2 to 1500 MHz, dB, no less than 76 77 Group delay time on the frequency F0 , ns 35±15 VSWR of input and output, no more than 2 Operating temperature range, °C from -40 to +70 Body type QLCC 6/8-1 Dimensions, mm 5х5х2 Weight, no more than, g 0.11

1) It is possible to produce fi lters with a rated frequency of up to 1700 MHz on the customer’s request 2) It is possible to produce fi lters with other values of pass bandwidth depending on a fi lter rated frequency JSC Radar mms develops control systems which enable to manage the entire object lifecycle and its sub-systems as a whole unit. Their integration provides enhanced object security (i.e. operation continuity, accident prevention), precise interaction of all systems; organization of management network structure with implementation of automatic control functions, processing and storage of the data on the systems state from a common control station; resource-saving.

Intelligent life support systems optimally combine a high level of safety, comfort and economic efficiency. These are innovative solutions for all who do not limit their plans to the present day.

ENGINEERING SYSTEM ADVANTAGES І security system (fire alarm) І energy savings: І energy saving systems - intelligent interaction of subsystems (ACS, lighting, heating, air-conditioning); І lighting control system - system work under necessity and scenarios; І engineering infrastructure system - significant opportunities in energy control analytics. І significant reduction of maintenance costs: І gasification system - single network; І climate control (heating, ventilation and air conditioning) - single accident and error monitoring center. І communication and network systems І remote service: І service systems - remote problem management and solving; - remote software update. І multimedia systems І reduction of service staff number І dispatching system І easy integration with products from other manufacturers

78 79 BMS-CLASS DISPATCH AND AUTOMATION SYSTEM “SMARTUNITY”

Functions of central server software (SmartUnity nEXT Server): І monitoring of automation controllers І system users administration І real-time database І alarm center І data collection and storage І data visualization - providing web-access to the system І caching of current system status for visualization PURPOSE The software system enables the functions of collection, Functions of configuration environment software accumulation, storage, processing and outputting of data (SmartUnity ProjectBuilder): on engineering systems which provide life activities and І configuration of automation and monitoring points successful operation of commercial equipment installed І configuration of system operation logic in a building. І development of graphic interfaces MAIN TASKS І system debugging tools І condition monitoring of business center engineering І alarm center adjustment systems which provide life support and successful operation of commercial equipment installed in a building І archiving system adjustment І saving the history of engineering system condition changes BMS SmartUnity nEXT Server software modules consist of: І storage of data on the specific physical parameter dynamics І backup module (Historian server) І providing of data on the specific parameter dynamics, І trend module (Trend server) key events and emergency situations І security module (Security Server) BMS SYSTEM STRUCTURE І alarm center (Alarm Server) BMS SmartUnity is structurally divided on software І visualization web server (GUI Server) and hardware components.

The software part of BMS system is based on SmartUnity DATA DISPLAYING solution, the main components of which are as follows: The system enables three basic ways of data displaying: І runtime environment of an automatization firmware installed І unified view — for displaying data on different types on CX series Beckhoff controllers (Automation Server) of objects in the tile-based global view І BMS central server SmartUnity (nEXT Server) І custom view - for displaying objects and their up- to-date data in diagrams, plans, sketches І ProjectBuilder configuration environment (mnemonic diagrams, floor plans, etc.)

Controller software functions І table view - for displaying data on similar objects (SmartUnity Automation Server): with sorting and filtration options І data collection from devices connected to the controller І software support for protocols Modbus, KNX, LON,JSON, UNAUTHORIZED ACCESS PROTECTION Ethernet TCP/IP, Bacnet BMS SmartUnity system software tools provide the multi-level protection system for both functional І primary data processing and interface thunking software and data. І control algorithm execution User access to the system is available 80 І parameter change data transmission to a central server only after authorization. 81 In August 2013 a new generation hydrofoil vessel “Kometa 120M” was layed out at the shipbuilding yard “Vympel” for the first time in the past twenty years. This vessel is developed with wide use of know-how previously applied only in the aircraft industry as follows: wireless communication and control systems, navigation systems, advanced composite materials. The focus is to provide the passengers comfort with use of the stabilization and overload minimization system.

Along with creation of civil hydrofoil crafts, JSC R.E. Alexeev’s Central Hydrofoil Design Bureau develops high-speed vessels for the Russian Navy and FSS Coast Guard. The development of WIG effect craft is another breakthrough One of the completed projects is a high-speed coast-guard in world’s shipbuilding. These are unique vehicles which hydrofoil “Antares”. combine the advantages of surface crafts and aircrafts. Their undeniable advantages are high efficiency (low fuel JSC R.E. Alexeev’s Central Hydrofoil Design Bureau has consumption), shallow draft, high speed, large cargo solid experience in developing the air-supported vessels and passenger capacity, amphibiousness. They can be and boats with displacement from 100 to 400 tons and successfully used in the open sea, coastal areas, rivers and speed from 30 to 60 knots as follows: high-speed boat lakes. “Serna”, landing boat “Dugon”, patrol boats “Mercury” and “Sokzhoy”, passenger ship “Linda”. Each of the prototypes WIG effect crafts require airfields, terminal and service has excellent performance characteristics such as high speed support in a less degree than traditional aviation. They and seaworthiness, ability to operate in the coastal areas with have the widest field of application for both civil and shallow depths (up to 2.5 m), sufficient autonomy. military purpose, and essential as an excellent vehicle for salvation. According to the technical specifications and One of the new developments in this field is high-speed aerohydrodynamic capabilities they are unrivaled throughout expedition vessel “KVK 1200”. The vessel is intended to the world. resolve a range of national economic problems such as the performance of scientific research and development activities, The idea of WIG effect flight and aerohydrodynamic design of geological exploration, environmental monitoring, transport the first domestic WIG effect crafts belongs to an outstanding support for fuel and energy industry, cargo services, rescue scientist, designer, founder and director of Central Hydrofoil operations. Based on the KVK 1200 project, the intelligent Design Bureau – Rostislav Alexeev. He started to develop vessel concept is proposed by JSC Radar mms to provide the first prototypes in the late 40s. In 1961, as a result of a high level of ship control efficiency and constant monitoring scientific-and-technical work, experiments and tests, the first of ship life support systems and crew condition. Soviet WIG effect craft SM-1 was developed. JSC R.E. Alexeev’s Central Hydrofoil Design Bureau develops By the mid-80s, our country has become the flagship the projects of the state-of-the-art transport and amphibian producer in the world’s WIG effect craft building. The WIG platforms (TAP). Their purpose is transportation of various effect crafts were developed for the Russian Navy as follows: oversized cargo and equipment, wheeled and track vehicles. lighter amphibian craft “Orlenok”, missile carrier “Lun”, legendary craft “Caspian Sea Monster”. These are high-speed vessels which can gain speed up to 250 km/h (~135 knots) with availability of year-round operation in Nowadays JSC R.E. Alexeev’s Central Hydrofoil Design shallow waters, marshlands, ice and snow-covered surface in Bureau is a steadily growing company with advanced winter. scientific-and-technical and experimental base, a team of highly-skilled professionals which have solid experience in A separate field is ultralight amphibian air-cushion vessels. research, development, creation, testing and operation of These are small-sized high-speed demountable all-terrain high-speed vessels. The current activities are intended to vehicles applied on any surface, e.g. water, ice, ground, snow. Joint-stock company Radar mms and Joint-stock company R.E. Alexeev’s Central Hydrofoil Design Bureau jointly develop develop a new generation of high-speed vessels for Russian the concept of creation and application of high-speed vessels and WIG effect crafts of new generation. Navy and civil fleet. Nowadays the designers of JSC R.E. Alexeev’s Central Hydrofoil Design Bureau develop a new generation of WIG- JSC R.E. Alexeev’s Central Hydrofoil Design Bureau, established in 1952, is the world’s leader in high-speed shipbuilding. The main products of JSC R.E. Alexeev’s Central Hydrofoil effect crafts. These are pioneering and advanced innovative The Design Bureau’s products are high-speed vehicles developed with use of various hydrodynamic support principles. Design Bureau are still high-speed boats and hydrofoil crafts. projects. These are air-cushion and hydrofoil crafts, air-supported vessels and hydrogliders with different bottom mechanization, The specialists of Central Hydrofoil Design Bureau offer the transport-amphibian platforms and WIG effect crafts. sea (“Kometa 120M”, “Cyclone 250M”) and river (“Valdai 45R”, “Albatross 120R”) types of new generation hydrofoil According to their performances and specifications, the developed crafts of JSC R.E. Alexeev’s Central Hydrofoil Design Bureau vessels with improved performances which meet the up-to- 82 outperform the world’s level of high-speed shipbuilding, show high reliability, efficiency and simplicity of operation. date requirements. 83 The legendary vessels “Roketa”, “Kometa”, “Meteor” at their time enabled to make a real breakthrough in the field of shipbuilding.

These vessel types are highly reliable. Until the present the hydrofoil crafts “Meteor” have been built without design changes, and have been in demand throughout the world for 40 years while the hydrofoil crafts “Kometa” have been in operation in the Mediterranean more than 25 years. ORGANIZATION AND PERFORMANCE OF TESTS The Company’s own test facilities are used during research work, tests and laboratory research of special equipment. The main elements of test facilities comprise testbed aircrafts based on the airplanes IL-114, L-39 and helicopter “Ansat”, WIG-effect craft “Strizh”, as well as “Buran” craft-based maritime testbed, automated motion simulation system and “Kamaz” vehicle-based mobile testbed, ground testbeds and hardware-in-the-loop simulation system.

Testing and setting up are performed in specially equipped facilities which meet all requirements and guarantee a high level of operations, primarily due to the possibility of hardware and software for simulating operating conditions of onboard radioelec- tronic systems and suites.

The development of high-tech intelligent radioelectronic products is accompanied by a full-scale cycle of mechanical and envi- ronmental tests, as well as the hardware-in-the-loop simulation. The test department is equipped with vibration stands, various thermal and environmental chambers which enable to conduct technological training of units and parts, to test for resistance to high and low temperatures, high and low pressure, as well as to hold vibration and shock tests.

The Company has a flight simulator for training navigators and operators of patrol (fixed-wing and rotary-wing) aircraft systems of naval aviation.

MONITORING ACTIVITIES WITH USE OF PILOTED AVIATION Purposes: І search and rescue operations І geological mapping during mineral resource exploration І environmental monitoring І ice reconnaissance activities І detection of forest and steppe fire fronts with its size determination and providing control of its extinguishment І formation of underground processes geographical ranges, areas of groundwater distribution and storage І monitoring and evaluation of water surface oil pollution І flood assessment

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JSC Radar mms not only manufactures unique products which have no equals in the world, but also provides services in test organization, monitoring of various objects, formation and updating of mapping information, etc. MONITORING MANAGEMENT WITH USE OF UNMANNED AVIATION Unmanned aerial vehicles, manufactured by JSC Radar mms, showed a successful performance in solving a wide range of national economic tasks. ENVIRONMENTAL MONITORING FROM AIR

Monitoring of domestic waste landfills, air pollution monitoring, monitoring of industrial and domestic waste water, monitoring of building grounds, monitoring of grounds for building construction, water objects monitoring, oil spills monitoring, pollution monitoring, algal blooms research.

SEARCH-AND-RESCUE OPERATIONS

Area patrolling, people search, stolen car search, fishermen rescue.

AEROMAGNETIC SURVEY

Geologic exploration and engineering: ore deposits search, groundwater finding, low contrast archeology.

EVALUATION OF HEAT LOSS IN BUILDINGS AND FACILITIES

Thermal imaging monitoring, monitoring of roof and chimney icing.

86 87 OIL AND GAS PIPELINES MONITORING

Illegal tapping search, accident and leakage areas search, monitoring of accident recovery activities, detection of pipeline beyond-design bedding and increased wear.

POWER LINE MONITORING

Accident area search, search of power line heating zones, search of power line breaks, unauthorized connections, design of power line laying routes, slack line analysis, creation of 3D digital relief model.

AERIAL SURVEY

Hunting resources monitoring, dimensioning images to geographic coordinates.

FORMATION AND UPDATING OF DIGITAL MAPPING INFORMATION

Formation and updating of national topographic maps and plans in the graphic form, topographic monitoring, creating and maintaining GIS. 88 89

It is possible to perform aerial photographic and video survey with use of UAVs developed by JSC Radar mms ALPHABETICAL INDEX

54 Airborne radar systems 49 Search-and-targeting system «Kasatka» ADJUSTING AND CALIBRATING OF FIRE DETECTORS 71 Analog-to-digital converter 17 Shipborne hydrometeorological station “Kharakter-K” AND GAS ANALYSIS DEVICES 27 Aspirating fire detector 63 Software bus “WBUS” 22 Atmosphere pressure sensor DADS-1 61 Special automated operator workstation for systems of flight mission planning and geospatial data processing 18 Automated weather station 32 Stable pressure transducers PDS-A 51 Automated workstation 33 Stable quartz pressure sensor DDKS-V-0.16 81 BMS-class dispatch and automation system “Smartunity” 25 Super early warning system for detection 74 Chirp signals forming-compression unit of fire dangerous situations 65 Control loading system 77 Surface acoustic wave filter Radar mms provides services for adjusting and calibrating smoke fire detectors and gas analysis devices due to the available 71 Data processing and displaying unit 76 Surface acoustic wave resonator equipment of its own production. 35 Digital electronic module MDKS 60 System of geospatial data interactive visualization The equipment for adjusting and calibrating of fire detectors and gas analysis devices include aerosol generator and gas mixture operating principle generator with enhanced accuracy characteristics. 26 Electroinductive smoke fire detector IP 216-001 19 Temperature and humidity sensor DTVV-01 3 29 Equipment for tuning and calibration of fire detectors The aerosol generator is designed for aerosol creation within mass concentration range from 0.05 to 50 mg/m . and gas analysis devices 40 Touch control console It is possible to provide services for testing, adjusting and calibrating of early warning smoke fire detectors. The equipment enables to maximum optimize the process of testing, adjusting and calibrating smoke fire detectors. 64 Editor MFI 11 UAV application expirience

The gas mixture generator (GMG) is designed for preparing a gas mixture with preset concentration of specific gas 47 Fluxgate magnetic anomaly detector 13 UAV control system (combustible and toxic gases). GMG relates to the field of analytical instrumentation and technological equipment construction, 72 Frequency driving module М411239 67 Ultra-wideband radars and can be used to ensure proper quality of development and research of gas analytical devices as well as for adjusting, calibrating and verification operations in the full-scale production of gas analytical devices. GMG enables to fulfil complex 73 Generator GK347-TS 7 Unmanned aerial system based on rotary-wing type UAV preparation and control of test moist gas mixtures with required concentrations, as well as to ensure a highest level of adjusting, calibrating and verification process automation with use of gas analysis devices. 75 Generator GPAV-K5 10 Unmanned aerial vehicles payload 20 Hydrometeorological buoy 68 USP antenna module 50 Information control system 70 USP transmitting module 23 Meteorological (optical) visibility range sensor 69 UWB antenna module 38 Micro motion and temperature measurement system 53 VHF side-looking radar “Razrez” with identification based on SAW sensors 57 W-band landing radar “Vidimost-2000” 12 Mobile control stations 58 W-band landing small-size radar “Pesok” 66 Mobile radar system 41 Weight sensor 9 Monitoring system based on unmanned helicopter BVS VT 500 21 Wind speed and direction sensor 14 Multipurpose UAV onboard computer “Smena-5” 37 Wireless biological object monitoring system 34 Precision pressure control equipment APKD-1 55 X-band all-round looking helicopter-borne AESA radar 28 Pre-emergency monitoring explosion-proof sensor 55 X-band all-round looking radar “Fluger” IP 216-001-EX 55 X-band sector scanning airplane-borne AESA radar 46 Quantum four-cell magnetic anomaly detector 54 X-band sector scanning airplane-borne AESA radar 45 Quantum geophysical magnetic anomaly detector “Podkrilok” 44 Quantum magnetic anomaly detector 59 X-band sector scanning small-size radar “MRLS-01” 42 Radio frequency identification system 56 X-band side-looking radar based on SAW RFID tags 15 Radio modem “Lora-1” 70 Reception and processing unit 90

RADAR-MMS.COM JSC RADAR MMS

37A, Novoselkovskaya str., St. Petersburg, 197375 phone: +7 (812) 777-50-51, fax: +7 (812) 600-04-49 e-mail: [email protected] www.radar-mms.com