I-26 Fighter

I-26 Fighter. First flight: 1940
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Technical specifications

DESIGNER OKB Yakovlev
COUNTRY Russia
TYPE
Fighter
CREW 1
POWER-PLANT One piston engine Μ-106P
Power, h.p. 1x1.050
DIMENSIONS  
Length, m 8,48
Height, m -
Wing span, m 10,00
Wing area, m2 17,15
WEIGHT  
Maximum take-off, kg 2.803
Normal take-off, kg -
Empty aircraft, kg 2.318
Internal fuel, kg -
Warload, kg -
PERFORMANCE  
Maximum speed, km/h 586
Max speed in low height, km/h 490
Cruising speed, km/h -
Range, km 700
Combat range, km -
Service ceiling, m 10.200
Rate of climb, m/min 833
Maximum overload, g -
ARMAMENT One 20 mm cannon ShVAK with 130 rounds and 4x7,62 mm machine-guns ShKAS.