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Pchela Unmanned aerial vehicle

Pchela Unmanned aerial vehicle. First flight: 1990 © Konstantinos Panitsidis
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Technical specifications

DESIGNER OKB Yakovlev
COUNTRY Russia
TYPE UAV
CREW -
POWER-PLANT An engine of unknown type
Power, h.p. 1x10
DIMENSIONS  
Length, m 2,780
Height, m -
Wing span, m 3,250
Wing area, m2 -
WEIGHT  
Maximum take-off, kg 138
Normal take-off, kg -
Empty aircraft, kg -
Internal fuel, kg -
PERFORMANCE  
Maximum speed, km/h -
Cruising speed, km/h 120 - 180
Rate of climb, m/s -
Service ceiling, m 100 - 2.500
Range, km -
Combat range, km -
Endurance, h 2
Preparation time for launch, min -
ARMAMENT Doesn't have (defensive).