|Manufacturer||Tachikawa Aircraft Company Ltd|
The term Tachikawa Ki-94 refers to two designs of the Tachikawa Hikoki K.K. aircraft factory.
Design and development
The first was a twin-boom monoplane with two 1,641 kW (2,201 hp) Mitsubishi Ha211 18-cylinder engines, driving two 4-blade propellers in a push-pull configuration. The very heavy armament that should have been mounted on the aircraft (two 37 mm/1.46 in and two 30 mm/1.18 in cannon, should have been enough to make short work of most US heavy bombers of the era. Notwithstanding the outstanding prospective performance, which however was judged as "unduly optimistic" by the technical department of the Japanese Army Air Force, this design was judged too complex by the technical department and the design was discarded.
The second Ki-94 design, made by a team under Tatsuo Hasegawa, chief designer of the aircraft and responsible for the used airfoil, was a more conventional single-seat, piston-engine monoplane fighter, developed for the Imperial Japanese Army Air Force along the same requirements as the Nakajima Ki-87, which had been the Army's fall-back design for the original Ki-94. Intended to counter B-29 raids, it was optimized for high-altitude interception with a pressurized cockpit and heavy armament.
This design was approved by the Koku Hombu, and the aircraft was designated Ki-94-II (the scrapped earlier Ki-94 design was named the Ki-94-I). An order was placed for one static test airframe, three prototypes, and eighteen pre-production aircraft. Only 2 prototypes were built in the event; the first was equipped with a single 1,895 kW (2,541 hp) Nakajima Ha219 [Ha-44] engine, driving a 4-blade propeller because the 6-blade one was not ready. The second prototype was to be fitted with a 6-blade propeller. The war's end however stopped the construction of the second prototype and also found the first prototype still being readied for its maiden flight, the Ki-94-II never taking to the air.
Specifications (Ki-94-II (estimated performance))
- Crew: 1
- Length: 12 m (39 ft 4 in)
- Wingspan: 14 m (45 ft 11 in)
- Height: 4.65 m (15 ft 3 in)
- Wing area: 28 m2 (300 sq ft)
- Airfoil: root: (Tatsuo Hasegawa) TH346-8454 (17%) ; tip: (Tatsuo Hasegawa) TH346-7s505 (10%)
- Empty weight: 4,690 kg (10,340 lb)
- Gross weight: 6,450 kg (14,220 lb)
- Powerplant: 1 × Nakajima Ha219 (unified [Ha-44-12]) 18-cylinder air-cooled radial piston engine, 1,830 kW (2,450 hp) for take-off
- 1,752 kW (2,350 hp) at 1,100 m (3,609 ft)
- 1,641 kW (2,200 hp) at 4,400 m (14,436 ft)
- 1,521 kW (2,040 hp) at 11,000 m (36,089 ft)
- Propellers: 4-bladed constant-speed propeller
- Maximum speed: 712 km/h (442 mph; 384 kn)
- Cruise speed: 440 km/h (273 mph; 238 kn)
- Range: 2,100 km (1,305 mi; 1,134 nmi)
- Service ceiling: 14,680 m (48,160 ft)
- Time to altitude: 5,000 m (16,404 ft) in 5 minutes 9 seconds
- 10,000 m (32,808 ft) in 17 minutes 38 seconds
- 13,000 m (42,651 ft) in 21 minutes 3 seconds
- Wing loading: 230.4 kg/m2 (47.2 lb/sq ft)
- Power/mass: 0.283 kW/kg (0.172 hp/lb)
- Guns: 2 × fuselage mounted 30 mm (1.181 in) Ho-155 cannon and 2 × 20 mm (0.787 in) Ho-5 cannon in the wings,
- Bombs: 2 × 250 kg (551 lb) bombs or 1x 500 kg (1,102 lb) bomb
Aircraft of comparable role, configuration and era
- Francillon, René J, Ph.D (1979), Japanese Aircraft of the Pacific War (2 ed.), London: Putnam & Co, ISBN 0-370-30251-6. First edition from 1970 ISBN 0-370-00033-1.
- Green, William (1973) , War Planes of the Second World War, 3. Fighters (7th impr ed.), London: Macdonald, ISBN 0-356-01447-9.
- Famous Aircraft of the World, 1st, 1. Japanese Army Experimental Fighters (76), Japan: Bunrin-Do Co, August 1976.
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