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The Ki-94-ll pressurised single-seat fighter, with a 1790kW Nakajima Ha-44 radial engine, was completed in August 1945, but the end of the war prevented it being test flown.
| MODEL | Ki-94 |
| CREW | 1 |
| ENGINE | 1 x Nakajima Ha-44, 1835kW |
| WEIGHTS |
| Take-off weight | 6450 kg | 14220 lb |
| Empty weight | 4690 kg | 10340 lb |
| DIMENSIONS |
| Wingspan | 14 m | 45 ft 11 in |
| Length | 12 m | 39 ft 4 in |
| Height | 4.65 m | 15 ft 3 in |
| Wing area | 28 m2 | 301.39 sq ft |
| PERFORMANCE |
| Max. speed | 712 km/h | 442 mph |
| Cruise speed | 440 km/h | 273 mph |
| Ceiling | 14680 m | 48150 ft |
| Range | 2100 km | 1305 miles |
| ARMAMENT | 2 x 30mm cannons, 2 x 20mm cannons, 500kg of bombs |
 | A three-view drawing (752 x 1042) |
| gottardi antonio, gtt916(@)libero.it, 07.03.2008 pay attention that when clicking on the picture of the Tachikawa Ki 94 I (the twin-boomed aircraft) one has the picture of the Ki 94 II on the screen. | | Jason, 06.12.2007 Its interesting that there were two KI-94 projects and that they varied so much from each other in design. |
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