Technical specifications
Main specifications of “Bekard-2” UAS*:
| Take-off, flight and landing control modes of the UAV
|
automatic; automated (under operator’s control)
|
| Application range, km
|
up to 25
|
| Reconnaissance altitude, m
|
from 50 to 1000
|
| Coordinates measurement error, max, m
|
50
|
| Payload type
|
photo module; IR reconnaissance module; TV reconnaissance module
|
| Time required to prepare the UAS for operation (1-2 persons), max, minutes
|
20
|
Main technical specifications of “Bekard-2” UAV*:
| Wingspan, max, m
|
2,3
|
| Height, max, m
|
0,5
|
| Length, max, m
|
1,2
|
| Take-off technique
|
catapult
|
| Landing technique
|
parachute
|
| Cruising speed with max take-off weight (at reconnaissance altitude), min, km/h
|
80**
|
| Flight duration with max take-off weight at cruising speed and reconnaissance altitude of the UAS, min, minutes
|
60
|
| Max flight speed with max take-off weight at reconnaissance altitude of the UAS, min, km/h
|
120**
|
| Service ceiling at max take-off weight, min, m
|
1500**
|
| Max take-off weight, kg
|
9
|
| Max flight altitude, m
|
2000**
|
| Max payload weight, kg
|
0,8
|
| Navigation
|
satellite radio navigation system; strap down inertial navigation system
|
| Power
|
electric motor
|
* - specifications are to be further clarified at contracting stage (manufacture agreement stage).
** - under normal weather conditions in accordance with GOST 4401-81 “Standard Atmosphere. Parameters”.
