Unmanned erial vehicle INDELA-I.N.SKY
Engine | rotory-piston engine | |
Takeoff power | kW | 26 |
Fuel consumption | kg/h | 5-8 |
Key geometric characteristics | ||
Length Nose to Tail | mm | 3052 |
Main rotor diameter | mm | 3168 |
Height | mm | 1346 |
Wheelbase | mm | 1180 |
Weight data | ||
Maximum takeoff weight | kg | 140 |
Weight | kg | 90 |
Fuel-carrying capacity | kg | 25 |
Payload weight, kg | kg | 25 |
Basic flight characteristics | ||
Cruising speed at ground level | km/h | 70 |
Static ceiling | m | 1500 |
Maximal vertical speed | m/s | 5 |
Flight duration (100-500 m high) | h | up to 5 |
Wind (takeoff and landing) | m/s | 10 |
Operating temperature | С | -35 … +55 |
Resolution | 1920х1080 | |
Quantity of active pixels | 2 000 000 | |
Image sensor | 1/3–type CMOS | |
Signal system | HD:1080p/29.97, 1080i/59.94, SD:NTSC/PAL | |
Lens | f = 5.1 mm (wide), 51.0 mm (tele)F 1.8(wide), F 2.1 (tele) | |
Optical magnification, not less than | 20x | |
Digital magnfication | 10х (200 with optical) | |
Viewing angle | 54.1 (wide), 2.9 (wide) | |
Synchronizing system | internal | |
Signal/noise ratio | more than 50dB | |
Camera sensitivity, not less than | 1,7 Lux | |
Signal/noise ratio | more 50 dB | |
Intensfication | Auto/Manual/Max(from -3 dB to 28dB, 2 steps) | |
Background light compensation | Yes | |
Focusing system | Automatic/Manual | |
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° | |
Infrared camera with high resolution | ||
Type of system | uncooled | |
Type of sensor | Infrared thermal imaging device, 640 x 512 VOx Microbolometer | |
Size of pixels | 25 μm | |
spectral range | 7.5 – 13.5 μm | |
Image inversion and return | 2х and 4х digital zoom | |
Digital improvement of image | 2х and 4х digital zoom | |
Detention of the imaging for th specified coordinates | yes | |
Lazer range finder | 1500 m, ±1 m |
GROUND CONTROL STATION:
Ground control station NDELA-GCS 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.
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