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Kawasaki Ki-5

Military Aircraft

The Kawasaki Ki-5 was an experimental fighter built for the Imperial Japanese Army Air Force in the early 1930s, and the last Japanese design led by Richard Vogt before he returned to Germany. It was the first all-metal cantilever monoplane fighter built in Japan, built around the Kawasaki Ha9, a Japanese development of the BMW IX engine rated at about 850 horsepower, and it used an inverted gull wing to improve the pilot view downward and allow a short, simple undercarriage. It first flew in February 1934, but test pilots complained of stability and handling problems and the engine never gave enough power to reach the design speed of 380 km/h. The army cancelled the project in September 1934 after four had been built, though the work helped later Kawasaki fighters, the Ki-28, Ki-60 and Ki-61.

Facts
Year
1934 1
Engine Class
Piston 1
Status
Cancelled 1
Power (kW)
634 1
Units Built
4 1
Top Speed (km/h)
360 1
Mass (kg)
1500 1
Maximum Mass (kg)
1870 1
Engine
Kawasaki Ha9 V-12 liquid-cooled piston engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Kawasaki Ki-5 (Wikipedia)

Of Make

Source Kawasaki Ki-5 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Kawasaki Ki-5 (Wikipedia)Design and development, manufacturer
Quote, Design and development, manufacturer
initially produced by Kawasaki Kōkūki Kōgyō K.K.

Originated In

Also in Geography Atlas: where this subject originated.

Source Kawasaki Ki-5 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
designed for the Imperial Japanese Army Air Force
Sources
1. Kawasaki Ki-5 (Wikipedia)
  • Lead
    It first flew in February 1934
  • Lead, body style
    was an experimental low-wing monoplane fighter aircraft
  • Specifications
    1 × Kawasaki Ha9 V-12 liquid-cooled piston engine, 634 kW (850 hp)
  • Specifications, engine
    1 × Kawasaki Ha9 V-12 liquid-cooled piston engine
  • Specifications, power
    634 kW (850 hp)
  • Design and development
    The project was cancelled on 9 September 1934
  • Design and development, units built
    after a total of four units were produced
  • Specifications, mass
    Empty weight: 1,500 kg (3,307 lb)
  • Specifications, maximum mass
    Gross weight: 1,870 kg (4,123 lb)
  • Specifications, top speed
    Maximum speed: 360 km/h (220 mph, 190 kn) at 2,400 m (7,874 ft)
  • Design and development, manufacturer
    initially produced by Kawasaki Kōkūki Kōgyō K.K.
  • Lead, country of origin
    designed for the Imperial Japanese Army Air Force
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