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
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineKawasaki Ha9 V-12 liquid-cooled piston engine 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Kawasaki Ki-5 (Wikipedia)
Of Make
Source Kawasaki Ki-5 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Kawasaki Ki-5 (Wikipedia)Design and development, manufacturerQuote, 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 originQuote, 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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