Ι-225 High-altitude fighter

I-225 High-altitude fighter. First flight: 1944
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Technical specifications

DESIGNER OKB MiG
COUNTRY Russia
TYPE
High-altitude fighter
CREW 1
POWER-PLANT One piston engine AM-42FB with turbo compressor TK-300B
Power, h.p. 1x1.900
DIMENSIONS  
Length, m 9,50
Height, m 3,70
Wing span, m 13,00
Wing area, m2 20,40
WEIGHT  
Maximum take-off, kg 3.900
Normal take-off, kg -
Empty aircraft, kg 3.010
Internal fuel, kg 325
- in the wing 127
Warload, kg -
PERFORMANCE  
Maximum speed, km/h 726
Max speed in low height, km/h 560
Cruising speed, km/h -
Range, km 1.300
Combat range, km -
Service ceiling, m 12.600
Rate of climb, m/min 1.250
Maximum overload, g -
ARMAMENT 4x20 mm cannons Ssh-20 with 4x100 rounds.