Ι-21 Fighter

Ι-21 Fighter. First flight: 1940
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Technical specifications

DESIGNER Pashin
COUNTRY Russia
TYPE
Fighter
CREW 1
POWER-PLANT One piston engine Μ-105P
Power, h.p. 1x1.050
DIMENSIONS  
Length, m 8,29
Height, m 3,24
Wing span, m 9,40
Wing area, m2 18,16
WEIGHT  
Maximum take-off, kg -
Normal take-off, kg 2.670
Empty aircraft, kg 1.210
Internal fuel, kg -
Warload, kg -
PERFORMANCE  
Maximum speed, km/h 573
Max speed in low height, km/h 488
Cruising speed, km/h -
Range, km 760
Combat range, km -
Endurance, h 2
Service ceiling, m 10.600
Rate of climb, m/min 1.260
Maximum overload, g -
ARMAMENT Two 7,62 mm machine-guns ShKAS and one 23 mm cannon BT-23.