State-owned Foreign Trade Unitary Enterprise "Belspetsvneshtechnika"

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Государственное внешнеторговое
унитарное предприятие
"Белспецвнештехника"

Адрес:

Республика Беларусь, 220103
г. Минск, ул. Калиновского, д. 8

Тел: +375 (17) 269-63-33

Факс: +375 (17) 269-63-43

E-mail: mail@bsvt.by

Время работы предприятия:

Понедельник - пятница
8.30-17.30

Обед:

13.00-14.00

“BEKARD-2” Unmanned aircraft system

“Bekard-2” unmanned aircraft system is intended to perform optronic terrain reconnaissance day and night, as well as to issue target designations to weapon systems.

  • Tasks solved:

  • • Observation within a preset zone, receipt of photos and television terrain imagery in real time;

  • • Search and detection of ground-based (water-based) objects, measurement of their coordinates;

  • • Automated tracking of selected ground-based (water-based) objects;

  • • Output of recon data to commanders of tactical-level units in real time mode.

  • Composition of the unmanned aircraft system (UAS):

  • • Unmanned aerial vehicle (UAV) – 2 pcs;

  • • Ground control station (GCS) of the UAS:

  • • remote automated workstation (RAWS);

  • • ground equipment of command-and-data radio link (CDRL);

  • • ground and air radio communications assets.

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”.

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