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La-17RM Unmanned aerial vehicle

La-17RM Unmanned aerial vehicle. First flight: 1963
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Technical specifications

DESIGNER Lavochkin
COUNTRY Russia
TYPE
Unmanned aerial vehicle
CREW -
POWER-PLANT One turbojet engine R-11K-300
Thrust, kgf -
DIMENSIONS  
Length, m 8,98
Height, m 2,98
Wing span, m 7,50
Wing area, m2 -
WEIGHT  
Maximum take-off, kg 3.100
Normal take-off, kg -
Empty aircraft, kg -
Internal fuel, kg -
Warload, kg -
PERFORMANCE  
Maximum speed, km/h 900
Maximum speed in low height, km/h -
Flight duration (endurance), min -
Rate of climb, m/min -
Service ceiling, m 15.000
Minimum flight height, m 600
Range, km 400
Maximum overload, g -
Preparation time at the technical position for departure, min -
ARMAMENT Doesn't have (defensive).