THE COMPANY ASTRUM AVIA SERVICE CARRIES OUT DELIVERIES OF UNMANNED AIRCRAFT SYSTEMS
FOR VARIOUS PURPOSES
Our company is trade partner of manufacturers complexes with unmanned aerial vehicles (UAVs), helicopters and aircraft types.
Technical characteristics of UAVs provide a quality solution to a wide range of applications through real-time monitoring from the air of large areas and extensive areas of the earth, the water and the ice surface in remote areas to provide search and rescue operations, conduct ice reconnaissance, determine the foci and the areas of the fires, accidents sections of power lines and pipelines, border areas of flooding areas, unauthorized felling, accumulation of stocks of fish in the fishing area, the implementation of air patrols all areas and solving transportation problems.
Our company supplies a variety of monitoring systems with small-sized unmanned helicopter take-off weight from 6 kg to 500 kg, providing accommodation on board instrumentation payload weight from 0.5 kg to 180 kg.
The small-sized unmanned helicopter mBPV-37 ( "Breeze"). Weight equipment payload can be up to 12 kg, his flight time - up to 2 hours. The structure of the payload comprises: a digital camera, a digital TV and a thermal imaging camera, the dosimeter of gamma radiation, gas analyzer and a laser detection of methane leaks.
Unmanned helicopter coaxial mass of 500 kg, capable of carrying payload weighing up to 180 kg and provides flight time up to 7 hours, range up to 500 km and is designed for a wide range of operational tasks
Monitoring Complex (mBLA-S) "Avis" with mini UAV aircraft type, takeoff weight of 7.5 kg and the weight of the equipment payload 1 kg. Starting mBLA-C is carried out with a catapult, landing on a parachute or carried out on an aircraft.
Part of the avionics UAV Automatic Control System (ACS) allows you to operate in automatic and semi-automatic modes.
Ease of use of unmanned aerial vehicles and data processing equipment from the target load provides a special software developed by the ground control station for unified complexes with a variety of UAVs.
Currently, work is underway to expand the range of target load equipment.
PURPOSE
Environmental monitoring; monitor the status of farmland, deforestation, afforestation; identifying violations of nature, including illegal fishing resources; assessment of the impact of natural disasters, technological accidents and catastrophes; supervising the construction, repair and other works; provision of search and rescue operations; control of the state oil and gas pipelines; control of protected zones around fuel and energy facilities.
THE COMPLEX
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Two - three small UAVs aircraft type (mBLA-C) with brushless Microelectric equipped with a replaceable unit payload equipment (camera / TV camera / thermal imaging camera / monitor gamma radiation);
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The ground control station (NSO) on the basis of the type of computer "Notebook" with a set of receiving and transmitting equipment;
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Aircraft catapult;
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Portable (portable) ukladochnye containers mBLA-C and the NSO;
The principle of operation of the aircraft - autonomous flight on a given route with the possibility of adjusting the operational flight program operator ONS.
ADVANTAGES
Glider "Avis" has removable wings, tailplane and fin. The fuselage airframe is made of composite materials. Take-off is carried out with the operator's hands. Planting is carried out with or without a parachute canopy area to 75x75 m. Glider flight makes quiet, it can operate over a wide temperature range.
BASIC PARAMETERS
Length, m | 1,1 |
Wingspan, m | 2,6 |
Takeoff weight, kg | 7,5 |
Flight time, h | 1-1,2 |
Payload weight, kg | 1 |
Flight speed, km / h | 60-70 |
Flight altitude, m | 100-1000 |
Range, km | up to 15 |
OPERATING CONDITIONS
Ambient temperature, , ºC | -20 / +35 |
Relative humidity at 35 ºC % | < 98 |
Surface wind speed, m / s | < 12 |
The intensity of rain and snow, mm / h | < 5 |
MONITORING SYSTEM WITH UNMANNED HELICOPTER GSV-500
PURPOSE
Real-time monitoring of large areas from the air and of extended areas of the earth, the water and the ice surface in remote areas with a view to: providing search and rescue, patrol and security and counter-terrorism measures; conduct ice reconnaissance; determine the extent of the impact of natural disasters and man-made disasters; monitor the status of power lines, pipelines and forest lands; Intelligence stocks of commercial fish; environmental control areas, water areas, atmosphere, etc.
THE COMPLEX
- Two unmanned helicopter GSV-500-B coaxial scheme. Equipment payload: turret optoelectronic system (TOES); on-board radar system with active and passive radar channels.
- Point the remote control (RC) type of container that is placed on the car-based all-terrain (such as "KamAZ"), or on the deck surface ship and in providing automated and real-time: BPV management; reception, display and registration information; monitoring of all elements of the complex.
- Set of technological equipment and spare parts.
- In ground-based complex - a vehicle for transportation of PFS, a set of technological equipment and spare parts.
Principle control helicopter - autonomous flight on a given route with the possibility of adjusting the operational flight program the remote operator.
ADVANTAGES
It does not require specially prepared airfields and sites; The accommodation on the basis of the automobile or on the deck of a small-size ship; autonomy of the application; high information content payload; receiving surveillance data in real time; reusability GSV; security staff.Ambient temperature , ºС | -30...+50 |
Relative ambient humidity at 35 ºС | < 98 |
The wind speed at ground level, m / s | < 12 |
The intensity of rain and snow, mm / h | < 5 |
BASIC PARAMETERS
Takeoff weight, kg | 500 |
Weight apparatus payload , kg | 180 |
The diameter of the rotor, m |
6,2 |
The flight duration, hours | 8 |
Range GSV, km | 500 |
Cruising speed horizontal flight, km / h | 180 |
Vertical ascent speed, m / sec | 7,0 |
Dynamic ceiling, m | 4000 |
GSV Dimensions (Length / Width / Height) m | 6,1/1,9/2,85 |
Technology equipment GSV: an internal combustion engine with a silencer, fuel and gasoline A-95, power supply equipment, the accumulator battery |
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Navigation Systems: Onboard an inertial navigation system, satellite navigation (GPS, GLONASS) |
MONITORING SYSTEM WITH UNMANNED HELICOPTER MBPV-37
PURPOSE
The unmanned helicopter is designed for real-time monitoring from the air of large areas and extensive areas of the earth, the water and the ice surface in remote areas with a view to: providing search and rescue, patrol and security and counter-terrorism measures; conduct ice reconnaissance; determine the extent of the impact of natural disasters and man-made disasters; monitor the status of power lines, pipelines and forest lands; Intelligence stocks of commercial fish; environmental monitoring and ground waters, etc.
THE COMPLEX
- Two small-sized unmanned helicopter "Breeze" with a two-bladed tail rotor and the rotor, equipped with on-board electronic equipment (including automatic control system) equipment and payload;
- The ground control station is composed of one or two computer workstations operators and transceiver system providing: control of the helicopter; reception, display and registration information; monitoring the functioning of the elements of the complex;
- Accessories (including gasoline-electric generator), standard packing and spare parts
BASIC PARAMETERS |
Maximum take-off weight, kg. |
37 |
Mass of payload equipment, kg. |
12 |
Flight time (with optional fuel tank), min. |
60(90) |
Operating altitudes they spread over the surface, m. |
50-1000 |
The range of airspeeds horizontal flight, km / h |
0-80 |
Communication range between mBPV-37-B and the NSO, km |
18 |
Power point |
Internal combustion engine |
Control method |
Hand (radio command), Auto (Programme), semi-automatic |
Installation of the following equipment payload |
The camera, a thermal imager, a camera, multi-spectral camera, monitor gamma radiation, gas analyzer, dust meter, laser rangefinder, laser detection of methane leaks, the laser scanner is the earth's surface, magnetometric equipment, speaker, light, drop device |
OPERATING CONDITIONS
Ambient temperature, ºС |
от -20 до +35 |
Wind speed m / s | to 10 |
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