
- monitoring of territories and objects;
- carrying out of prospecting works;
- aerial mapping;
- target designation; protection of transport columns;
Construction of the helicopter makes it possible to transport it on board of an armored personal carrier (APC) to the place, where the specified combat task should be performed. The helicopter can also be transported on a small trailer for a car.
| Engine | two four-cycle, two-cylinder, water-cooled | |
| Takeoff power | kW | 52 |
| Volume | cub.sm | 588 |
| Hourly fuel consumption | l/h | 16 |
| Key geometric characteristics | ||
| Length with rotary screws | mm | 5850 |
| Length | mm | 4358 |
| Rotor diameter | mm | 4800 |
| Height | mm | 1534 |
| Wheelbase | mm | 1350 |
| Weight data | ||
| Maximum takeoff weight | kg | 255 |
| Useful load | kg | 55 |
| Standard fuel margin | l | 83 |
| Reserve fuel | l | 17 |
| Basic flight characteristics | ||
| Cruise speed level flight | km/h | 100 |
| Static ceiling without consideration to ground effect influence | m | 2100 |
| Maximum climbing capacity | m/s | 5 |
| Flight duration (Height 100-500 м) | h | 5 |
| Maximum permissible wind speed while takeoff and landing | m/s | 10 |
COMPLEX OPERATING STAFF:
Complex operating staff consists of 4 people:
- Calculation commander;
- UAV operator;
- Useful load operator;
- UAV technician;
| Resolution | 1920х1080 | |
| Quantity of active pixels | 2 000 000 | |
| Image sensor | 1/3 – type CMOS | |
| Signal system | HD:1080i/59.94, PAL | |
| Lens | f = 4.7 mm (wide), 94 mm(tele) F 1.6 (wide), F 3.5 (tele) | |
| Optical magnifcation, not less than | 20x | |
| Digital magniication | 10х (200 together with optical) | |
| Viewing angle | 54.1 (wide), 2.9 (wide) | |
| Camera sensitivity, not less than | 1,7 Lux | |
| Signal/noise ratio | more than 50dB | |
| Intensication | Auto/Manual/Max (from -3 dB to 28dB, 2 steps) | |
| Background light compensation | Yes | |
| Focusing system | Automatic/Manual | |
| Digital video output | HD:Y/Cb/Cr 4:2:2 EIA/CEA-861-B type via LVDS (Y:8 bit, C: 8 bit, Vsync, Hsync, Field, Clock) | |
| Analog video output | HD: Component(Y/Pb/Pr) SD: VBS | |
| Improved noise clipping | Yes | |
| Automatic stabilization of camera’s optical axis at a set direction in the geocentric coordinate system, being at rest, with accuracy, not worse than | 1,5° | |
| High-resolution infrared camera | ||
| System type | Uncooled | |
| Sensor type | Infrared thermal image converter, 640 x 512 VOx Microbolometer | |
| Pixel size | 25 μm | |
| Spectral range | 7.5 – 13.5 μm | |
| Operational characteristics | < 65mK NEdT of f/1.0 | |
| Image inversion and return | 2х and 4х digital zoom | |
| Gyro-stabilized system control | RS-485 Ethernet | |
| Tracking the object selected by the operator | Yes (limited) | |
| Fixed shooting of the coordinates specied | Yes | |
| Laser range nder | 1500 m , ±1 m | |
| Operating temperature | -20 - +70°С | |
GROUND CONTROL STATION:
Ground control station is used for UAV flight and useful load control, for the reception, processing, representation and recording of the data, received from an UAV and support of data exchange with external consumers. The UAV is designed to deliver useful load equipment to a selected place, to assure its functioning on command from a ground control station or from an on-board computer and real-time visual data transmission to a ground control station or from on-board storage devices. Ground control stations are designed to carry out all kinds of preparation, preventive maintnance of UAV, on-board equipment troubleshooting.
Ground control station ensures:
- real-time telemetric data exchange with an UAV;
- telemetric data processing and screening as text and image data;
- flight configuration and useful load operation control;
- flight task automatic preparation and its loading onto an on-board complex;
- on-board complex technical state control;
- reception, display, record, storage and real-time presentation on the monitor screens of the information received from the useful load;
- telemetric data processing and screening as text and image data;
- on-board complex technical state control;
- flight configuration and useful load operation control;
- real-time telemetric data exchange with an UAV;
- flight task automatic preparation and its loading onto an on-board complex;
The way points editing program is very convenient. If the user has an access to the Internet, there is no need in any other maps for the mission planning, way point list editing and autonomous flights. The software is translated to English, Russian and Spanish. At the customer's option the software can be translated to any language.
DETAILED COMPLEX CONFIGURATION:
«H.U.SKY-II» carrier (Robotic carrier «H.U.SKY-II» with a gyro-stabilized optoelectronic system “Indela OGD-20HIR” with TV and infrared camera and radio sighting system, designed to search for and detect UAVs in case of emergency landing.) - 2 units.
«H.U.SKY-II» complex repair packing (Repair packing is used for prompt technical maintenance of the carrier. Repair packing contains spare part kit, tools, instruments and materials necessary for the maintenance of the carrier.) - 1 kit.
“INDELA-GCS” ground control station (located in a trailer "Kupava") (Trailer "Kupava" consists of 2 sections: Control section is equipped with conditioner, heater, ventilating unit. Hermetic section is equipped with special racks necessary for transportation and storage of carriers.) - 1 unit.
Auto positioning antenna system
Field tool kit (Contains tools and equipment for UAV and ground control station servicing in field environment as well as fire-extinguishing means.) - 1 kit.
Pilot training simulator - 1 unit.





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