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Kawasaki Ki-60

Military Aircraft

The Kawasaki Ki-60 was an experimental Japanese fighter built just before the Pacific War around a licence-built Daimler-Benz DB 601 liquid-cooled engine, an unusual choice at a time when most Japanese aircraft used air-cooled radial engines. Takeo Doi and Shin Owada designed it from 1940 to meet an army call for a heavily armed, fast-climbing interceptor, and the first prototype appeared in March 1941. It was a compact all-metal monoplane with a very high wing loading, and flight tests showed a long take-off run, heavy controls, dangerous spinning and a top speed below what was promised. Two lighter prototypes did little better, and production plans were cancelled in late 1941 after three aircraft had been built. The lessons from its faults were used to improve the Ki-61.

Facts
Year
1941 1
Engine Class
Piston 1
Status
Cancelled 1
Power (kW)
875 1
Units Built
3 1
Top Speed (km/h)
560 2
Mass (kg)
2150 1
Maximum Mass (kg)
2750 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-60 (Wikipedia)

Of Make

Source Kawasaki Ki-60 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Kawasaki Ki-60 (Wikipedia)Design and development, manufacturer
Quote, Design and development, manufacturer
designed by Takeo Doi and his deputy Shin Owada of Kawasaki Aircraft Industries

Originated In

Also in Geography Atlas: where this subject originated.

Source Kawasaki Ki-60 (Wikipedia)Lead
Quote, Lead
was an experimental Japanese pre-World War II fighter aircraft
Sources
1. Kawasaki Ki-60 (Wikipedia)
  • Design and development
    The first prototype of the Ki-60 emerged in March 1941
  • Lead
    was an experimental Japanese pre-World War II fighter aircraft
  • Specifications
    Daimler-Benz DB 601A V-12 inverted liquid-cooled piston engine, 875 kW (1,173 hp)
  • Specifications, engine
    Daimler-Benz DB 601A V-12 inverted liquid-cooled piston engine
  • Specifications, power
    875 kW (1,173 hp)
  • Design and development, status
    Plans for production were cancelled in late 1941 after three airplanes had been built.
  • Design and development, units built
    after three airplanes had been built
  • Specifications, mass
    Empty weight: 2,150 kg (4,740 lb)
  • Specifications, maximum mass
    Gross weight: 2,750 kg (6,063 lb)
  • Specifications, top speed
    Maximum speed: 560 km/h (350 mph, 300 kn) at 4,500 m (14,800 ft)
  • Design and development, manufacturer
    designed by Takeo Doi and his deputy Shin Owada of Kawasaki Aircraft Industries
View the Source
2. Aviastar: Kawasaki Ki-60
AviastarSpecification
Quote, Specification
Max. speed 560 km/h
View the Source
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