U-5 Training aircraft. First flight: 1937

 


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TECHNICAL SPECIFICATIONS

DESIGNER Nikitin
COUNTRY Russia
TYPE Training aircraft
CREW 2
POWER-PLANT One reciprocating motor ΜG-31F (M-11)
Thrust, h.p 1 x 130 (100)
DIMENSIONS  
Length, m 7,75
Height, m 2,78
Wing span, m 9,84
Wing area, m2 25,53
WEIGHT  
Normal take-off, kg 974
Empty aircraft, kg 700
Maximum take-off, kg 1.400
Internal fuel, kg -
PERFORMANCE  
Maximum speed, km/h 272
Cruising speed, km/h 250
Max speed in low height, km/h -
Rate of climb, m/min -
Service ceiling, m 4.500
Range, km 480
Combat range, km -
ARMAMENT One 7,62 mm machine-gun ShKAS and four rockets type RS.