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Tu-121 Unmanned aerial vehicle

Tu-121 Unmanned aerial vehicle. First flight: 1959
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Technical specifications

DESIGNER OKB Tupolev
COUNTRY Russia
TYPE
Unmanned aerial vehicle
CREW -
POWER-PLANT One turbojet engine KR-15-300
Thrust, kgf -
DIMENSIONS  
Length, m 24,77
Height, m 4,61
Wing span, m 8,40
Wing area, m2 -
WEIGHT  
Maximum take-off, kg 35.000
Normal take-off, kg -
Empty aircraft, kg 11.450
Internal fuel, kg 16.600
PERFORMANCE  
Maximum speed, km/h 2.700
Cruising speed, km/h -
Rate of climb, m/min -
Service ceiling, m 19.000 / 22.800
Range, km 3.880
Combat range, km -
Endurance, min -
ARMAMENT Doesn't have (defensive).