Puneet Varma (Editor)

Nakajima Ki 201

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Top speed
  
852 km/h

Wingspan
  
14 m

Weight
  
4,500 kg

Manufacturer
  
Nakajima Aircraft Company

Range
  
978 km

Length
  
12 m

Engine type
  
Turbojet

Nakajima Ki-201 frankboluclaeduImagesKaryuKaryuDjpg

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.

Contents

Nakajima Ki-201 WINGS PALETTE Nakajima Ki201 Karyu Japan

Nakajima ki 201


Development

Nakajima Ki-201 Ki201 Karyu

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. 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 Ki-201 Nakajima KI201 Karyu Take Off a photo on Flickriver

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, 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. It seems that the Navy was also approached, but displayed no interest whatsoever.

Nakajima Ki-201 New Japanese jet planeKi 201 Karyu Passed to Development War

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.

Variants

Nakajima Ki-201 New Japanese jet planeKi 201 Karyu Passed to Development War

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)

Nakajima Ki-201 Guide at War Thunder Communities Center

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

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
  • Performance

  • Maximum speed: 852 km/h (592 mph; 514 kt)
  • Range: 980 km (609 mi)
  • Service ceiling: 12,000 m (39,400 ft)
  • Rate of climb: 774 m/min (2,540 ft/min)
  • Armament

  • 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
  • References

    Nakajima Ki-201 Wikipedia