UTI-2 (4) Training aircraft. First flight: 1937

 


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TECHNICAL SPECIFICATIONS

DESIGNER Polikarpov
COUNTRY Russia
TYPE Training aircraft
CREW 2
POWER-PLANT One reciprocating motor M-25A
Thrust, h.p 1 x 730
DIMENSIONS  
Length, m 5,99
Height, m 3,25
Wing span, m 9,00
Wing area, m2 14,45
WEIGHT  
Normal take-off, kg -
Empty aircraft, kg 1.156
Maximum take-off, kg 1.458
Internal fuel, kg -
PERFORMANCE  
Maximum speed, km/h 450
Cruising speed, km/h 398
Max speed in low height, km/h -
Rate of climb, m/min -
Service ceiling, m 8.960
Range, km 364
Combat range, km -
ARMAMENT -