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The Kawasaki Ki-64 (Allied code name: Rob) was a one-off prototype of an experimental heavy, single seat, fighter. It had two unusual design features. First; it had two Kawasaki Ha-40 engines in tandem; one in the aircraft nose, the other behind the cockpit, both being connected by a drive shaft. This combination (called the Kawasaki Ha-201) drove two, three-bladed, contra-rotating propellers.[1][2] The second feature was the use of the wing surface as a radiator for the water-cooled engines.[3] The aircraft first flew in December 1943. During the fifth flight, the rear engine caught fire; and while the aircraft made an emergency landing, it was damaged. The aircraft was subsequently abandoned in mid-1944 in favour of more promising projects. The airframe survived the war, and parts of the unique cooling system were sent to Wright Field for examination.[4]

Ki-64
Role Fighter
Manufacturer Kawasaki Kōkūki Kōgyō K.K.
First flight December 1943
Status Cancelled 1944
Primary user Imperial Japanese Army
Number built 1

Specifications (Ki-64)


Data from Warplanes of the Second World War, Volume Three: Fighters;[5] WW2 Aircraft Fact Files: Japanese Army Fighters, Part 1;[4] Japanese Aircraft of the Pacific War[6]

General characteristics

Performance

Armament


See also


Aircraft of comparable role, configuration, and era

Related lists


References



Citations


  1. FAOW 76 1976, pp. 17–18, 46–47.
  2. Green & Swanborough 1976, p. 35.
  3. Green & Swanborough 1976, p. 34.
  4. Green & Swanborough 1976, p. 36.
  5. Green 1961, p. 26.
  6. Francillon 1979, p. 122.

Bibliography





На других языках


- [en] Kawasaki Ki-64

[fr] Kawasaki Ki-64

Le Kawasaki Ki-64 « Rob » est un prototype de chasseur lourd conçu par le constructeur japonais Kawasaki lors de la Seconde Guerre mondiale, qui vola en décembre 1943, et dont le programme fut annulé en 1944.

[it] Kawasaki Ki-64

Il Kawasaki Ki-64 (川崎 キ 64?), al quale fu assegnato dagli alleati il nome in codice Rob[4], era un aereo da caccia monomotore, monoplano ad ala bassa sviluppato dall'azienda giapponese Kawasaki Kōkūki Kōgyō, divisione aeronautica della Kawasaki Heavy Industries, nella prima metà degli anni quaranta e rimasto allo stadio di prototipo.



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