NV-6 Training aircraft. First flight: 1940

 


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TECHNICAL SPECIFICATIONS

DESIGNER Nikitin
COUNTRY Russia
TYPE Training aircraft
CREW 1
POWER-PLANT One reciprocating motor MG-11F
Thrust, h.p 1 x 165
DIMENSIONS  
Length, m 5,80
Height, m -
Wing span, m 7,00
Wing area, m2 14,00
WEIGHT  
Normal take-off, kg -
Empty aircraft, kg 560
Maximum take-off, kg 750
Internal fuel, kg -
PERFORMANCE  
Maximum speed, km/h 270
Cruising speed, km/h 230
Max speed in low height, km/h -
Rate of climb, m/min -
Service ceiling, m 4.500
Range, km -
Combat range, km -
ARMAMENT -