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Nakajima Ki-201
Nakajima Ki-201 Karyu
Role Jet Fighter Aircraft
Manufacturer Nakajima Aircraft Company
Status proposed design, no prototypes built
Developed from Nakajima J9Y

The Nakajima Ki-201 Karyu/Karyū 中島 キ-201 火龍 ("Fire Dragon"?) was a Japanese jet fighter project designed during the final stages of World War II but which was never completed.


The Karyu began as an in-house project by Nakajima in early 1945 to apply what was being learned about jet aircraft from the Nakajima Kikka attack aircraft to a fighter design. The Kikka had been inspired by the successful German Messerschmitt Me 262, but the similarities to that aircraft were limited to general configuration.[1] On the other hand, the design team led by Iwao Shibuya based the Karyu far more closely on the German aircraft, which had already proven itself quite formidable. Nakajima attempted to interest the Imperial Japanese Army Air Force in the aircraft, and seems to have succeeded at least far enough to have had an official designation ("Ki-201") applied to it,[1] but at that point, the Army had already decided to pursue derivatives of the liquid-fueled rocket powered Mitsubishi J8M, designated Mitsubishi Ki-200 and Mitsubishi Ki-202, as their way of fending off the B-29 Superfortress raids.[2] It seems that the Navy was also approached, but displayed no interest whatsoever. Undaunted, Nakajima continued development, anticipating test flights by December 1945. Most sources agree that work on the prototype had not yet begun by the time of the Japanese surrender.


Proposed versions for Japanese Army development of the Nakajima Ki-201 Karyu were an interceptor - equivalent to the Me 262A-1a - and a fighter-bomber - equivalent to the Me 262A-2a. The powerplant would have been the 8.9 kN (2,001 lb) Ishikawajima Ne-130 turbojet or the 8.7 kN (1,951 lbf) Ne-230 turbojet.

Specifications (planned specification)

Data from Japanese Aircraft of the Pacific War;[3] Famous Aircraft of the World, first series, no.76: Japanese Army Experimental Fighters (1)[4]

General characteristics

  • Crew: 1
  • Length: 11,5 m (37 ft 8¾ in)
  • Wingspan: 13.70 m (44 ft 11⅜ in)
  • Height: 4.69 m (13 ft 4 in)
  • Wing area: 25.0 m² (269 ft²)
  • Empty weight: 4,500 kg (9,920 lb)
  • Loaded weight: 7,000 kg (15,400 lb)
  • Powerplant: 2 × Ishikawajima Ne-230 turbojet, 8.7 kN (1,951 lbf) each


  • Maximum speed: 812 km/h (507 mph; 440 kt)
  • Range: 978 km (611 mi)
  • Service ceiling: 12,000 m (39,400 ft)
  • Rate of climb: 774 m/min (2,540 ft/min)


  • Interceptor: 2 × 30 mm (1.18 in) Ho-155 cannon and 2 × 20 mm Ho-5 cannon
  • Fighter bomber: as interceptor, plus 1 × 500kg (1,102 lb) or 800 kg (1,764 lb) bomb
  • See also


    1. 1.0 1.1 Mikesh 1979, p. 28.
    2. Green 1973, p. 65.
    3. Francillon 1979, p. 488.
    4. FAOW 1976, p. 42.
    • 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: Fighters, Volume Three. London: Macdonald, 1961 (Seventh impression 1973). ISBN 0-356-01447-9.
    • Mikesh, Robert C. Kikka, Monogram Close-Up 19. Bolyston, Massachusetts: Monogram Aviation Publications, 1979. ISBN 0-914144-19-7.
    • Unknown Author. Famous Aircraft of the World, first series, no.76: Japanese Army Experimental Fighters (1). Japan: Bunrin-Do Co. Ltd., August 1976.

    External links

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