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The last of the "A" series high-altitude fighter prototypes
to enter flight test, the I-224 was flown for the
first time on 20 October 1944. Powered by a Mikulin
AM-39B engine rated at 1750hp for take-off, driving an
3.50m diameter propeller with 40cm chord "paddle" blades, and equipped with a single
TK-300B turbo-supercharger on the starboard side, the
I-224 carried an armament of two synchronised 20mm
ShVAK cannon. An unusual feature of the I-224 was its
exhaust system which included four fixed aft-facing
ejection "chimneys". The I-224 achieved an altitude of
14,100m during its brief flight test programme
which reportedly terminated when a malfunctioning
supercharger resulted in an uncontrollable engine fire.
| WEIGHTS |
| Take-off weight | 3921 kg | 8644 lb |
| Empty weight | 3105 kg | 6845 lb |
| DIMENSIONS |
| Wingspan | 13.00 m | 42 ft 8 in |
| Length | 9.51 m | 31 ft 2 in |
| Height | 3.60 m | 11 ft 10 in |
| Wing area | 22.44 m2 | 241.54 sq ft |
| PERFORMANCE |
| Max. speed | 693 km/h | 431 mph |
| Ceiling | 14100 m | 46250 ft |
| Range | 1000 km | 621 miles |
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