Di-8 (ANT-46) Fighter

Di-8 (ANT-46) Fighter. First flight: 1935
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Technical specifications

DESIGNER OKB Ilyushin
COUNTRY Russia
TYPE
Fighter
CREW 3 - 4
POWER-PLANT Two piston engines Μ-34RNF
Power, h.p. 2x1.200
DIMENSIONS  
Length, m 12,24
Height, m 7,94
Wing span, m 20,30
Wing area, m2 55,70
WEIGHT  
Maximum take-off, kg -
Normal take-off, kg 5.910
Empty aircraft, kg 4.180
Internal fuel, kg 550
Warload, kg 250
PERFORMANCE  
Maximum speed, km/h 404
Max speed in low height, km/h 382
Cruising speed, km/h -
Range, km 1.800
Combat range, km -
Service ceiling, m 9.000
Rate of climb, m/min -
Maximum overload, g -
ARMAMENT Two 76,2 mm cannon APK-4 with 2x15 rounds or 4x20 mm cannon ShVAK the one 7,62 mm cannon with 800 rounds. 
1x12,7 mm machine-guns ShVAK, 1x12,7 mm machine-guns ShKAS.