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Shmel-1 Unmanned aerial vehicle

Shmel-1 Unmanned aerial vehicle. First flight: 1983 © Konstantinos Panitsidis
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Technical specifications

DESIGNER OKB Yakovlev
COUNTRY Russia
TYPE
UAV
CREW -
POWER-PLANT One piston engine
Power, h.p. 1x32
DIMENSIONS  
Length, m 2,78
Height, m 1,10
Wing span, m 3,25
Wing area, m2 -
WEIGHT  
Maximum take-off, kg 130
Normal take-off, kg -
Empty aircraft, kg -
Internal fuel, kg -
PERFORMANCE  
Maximum speed, km/h -
Cruising speed, km/h 140
Rate of climb, m/min -
Service ceiling, m 3.000
Range, km -
Combat range, km -
Endurance, h 2
Preparation time for launch, min -
ARMAMENT Doesn't have (defensive).