Tachikawa Ki-94

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The term Tachikawa Ki-94 refers to two designs of the Tachikawa Hikoki K.K. aircraft factory. The first was a twin-boom monoplane with two engines driving four blade tractor and pusher propellors, but this design was abandoned as being judged too complex by the technical department of the Japanese Air Force[1]. The second Ki-94 design was a more conventional single-seat, piston-engined monoplane fighter, developed for the Army. Intended as a counter to B-29 raids, it was optimized for high-altitude interception with a pressurized cockpit and heavy armament.

One aircraft was completed in August 1945 but before it flew, the war ended.

Contents

[edit] Specifications (Ki-94-II)

Data from {Virtual Aviation Museum}

General characteristics

  • 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 (301 ft²)
  • Empty weight: 4,690 kg (10,337 lb)
  • Loaded weight: kg (lb)
  • Useful load: kg (kg)
  • Max takeoff weight: 6,450 kg (14,216 lb)
  • Powerplant: 1× Nakajima Ha-44 radial 4-blade, 1,835 kW (2,461 hp)

Performance

Armament 2x30mm cannons, 2x20mm cannons, 500kg (1,102lb) bombs

[edit] References

[edit] Notes

  1. ^ Francillon 1979, p. 265.

[edit] Bibliography

  • Francillon, René J. Japanese Aircraft of the Pacific War. London, Putnam & Company, 1970 (Second edition 1979). ISBN 0-370-30251-6.
  • Green, William. War Planes of the Second World War, Volume Three: Fighters. London: Macdonald, 1961 (Seventh impression 1973). ISBN 0-356-01447-9.
  • Green, William and Swanborough, Gordon. WW2 Aircraft Fact Files: Japanese Army Fighters, part 2. London, Macdonald & Jane's, 1977. ISBN 0-354-01068-9.
  • Unknown Author Famous Aircraft of the World, no.76: Japanese Army Experimental Fighters (1). Japan: Bunrin-Do Co. Ltd., August 1976.

[edit] See also

Comparable aircraft

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