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Kawasaki Ki-78

Supersonic and Experimental Aircraft

The Kawasaki Ki-78, first called Ken III for research aircraft number three, was a small high-speed research aircraft meant to study laminar-flow wings with heavy wing loading and to try for the world absolute speed record. The Aeronautical Research Institute of the University of Tokyo began the programme in 1938, and Kawasaki built the aircraft with a streamlined fuselage, a thin all-metal wing with a sharp leading edge and a licence-built Daimler-Benz DB 601A engine boosted for short periods with methanol and water injection. The Imperial Japanese Army took the project over and ordered two prototypes in 1941. The first flew on 26 December 1942, but a study showed it needed extensive changes, so the programme ended after the 32nd flight on 11 January 1944 and the second aircraft was never finished.

Facts
Year
1942 2
Engine Class
Piston 1
Status
Cancelled 1
Top Speed (km/h)
700 2
Mass (kg)
1930 1
Maximum Mass (kg)
2300 1
Engine
Daimler-Benz DB 601A V-12 inverted liquid-cooled piston engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Kawasaki Ki-78 (Wikipedia)

Of Make

Source Kawasaki Ki-78 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Kawasaki Ki-78 (Wikipedia)Design and development
Quote, Design and development
built at Kawasaki Kokuki Kogyo K.K.

Originated In

Also in Geography Atlas: where this subject originated.

Source Kawasaki Ki-78 (Wikipedia)Operational history, country of origin
Quote, Operational history, country of origin
the whole project was taken over by the Imperial Japanese Army
Sources
1. Kawasaki Ki-78 (Wikipedia)
  • Operational history
    was flown for the first time on 26 December 1942
  • Lead
    was a high-speed research aircraft
  • Specifications
    Daimler-Benz DB 601A V-12 inverted liquid-cooled piston engine rated at 1,160 kW (1,550 hp)
  • Specifications, engine
    Daimler-Benz DB 601A V-12 inverted liquid-cooled piston engine
  • Operational history, status
    the project was officially terminated after the 32nd flight on 11 January 1944
  • Specifications, mass
    Empty weight: 1,930 kg (4,255 lb)
  • Specifications, maximum mass
    Gross weight: 2,300 kg (5,071 lb)
  • Specifications, top speed
    Maximum speed: 700 km/h (430 mph, 380 kn) at 3,500 m (11,500 ft)
  • Design and development
    built at Kawasaki Kokuki Kogyo K.K.
  • Operational history, country of origin
    the whole project was taken over by the Imperial Japanese Army
View the Source
2. Aviastar: Kawasaki Ki-78
Aviastar
  • Summary line
    The first prototype flew on December 26, 1942.
  • Specification
    Max. speed 700 km/h
View the Source
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