|Engines||1*1430/1860hp AM-39B with 1(or 2???)*TK-300B|
|Wing Load (kg/m2)||167|
|Power load (kg/hp)||2.62|
|Speed at 0m||601km/h|
|Speed at 13000m||693km/h|
|Climb to 5000m||4.8min|
Almost identical to I-222/3A. Differed by improved air-air radiator (for the pressurized cockpit) under the fuselage and special high-altitude propeller with very wide blades.
During factory flight tests (Fall 1944) achieved altitude 14000m, but failed to demonstrate calculated range 1400km.
|Modified October 13, 1997||Back to|