Kawasaki Ki-28
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Ki-28 | |
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Kawasaki Ki-28 |
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Type | Experimental Fighter Aircraft |
Manufacturer | Kawasaki Kōkūki Kogyo KK |
Maiden flight | 1936 |
Primary user | IJA Air Force |
Number built | 1 |
The Kawasaki Ki-28 (キ28 (航空機) Ki-Nijuhachi (kōkūki)?) was an experimental fighter aircraft designed for the Japanese Imperial Army. It flew in 1936, but was never produced for actual use.
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[edit] Design & Development
The Ki-28 was initially produced by Kawasaki Kōkūki Kōgyō KK in response to Japanese army specifications for a fighter aircraft to replace the existing Kawasaki Ki-10. In mid 1935 Kawasaki, Mitsubishi and Nakajima were instructed to build competitive prototypes. The Kawasaki design was based on its earlier, but unsuccessful Ki-5. It was a cantilever low-wing monoplane of all metal construction, except for fabric covered control surfaces, with a conventional tail unit, fixed tailskid landing gear and powered a 800 hp (600 kW) Kawasaki Ha 9-2 liquid-cooled in-line engine.
Service trials proved that the Kawasaki Ki-28 was the fastest of the three contenders, but the Nakajima Ki-27 was by far the most maneuverable, and on this basis was selected by the Imperial Japanese Army Air Force.
[edit] Operators
[edit] Military operators
[edit] Specifications
General characteristics
- Crew: 1
- Length: 12 meters (39.37 feet)
- Wingspan: 7.9 meters (25.92 feet)
- Height: 2.60 meters (8.53 feet)
- Wing area: 19 sq.m. (204.52 sq.ft.)
- Empty weight: 1,420 kg (3,130 lbs)
- Max takeoff weight: 1,760 kg (3,880 lbs)
- Powerplant: 1× Kawasaki Ha-9-2, 12-cylinder, liquid-cooled in-line piston engine, 800 hp ()
Performance
- Maximum speed: 485 km/h
- Range: 1000 km (620 miles)
- Service ceiling 11000 meters (36,000 feet)
Armament
- Guns: 2x 7.7 mm machine guns
[edit] See also
[edit] References
- Mikesh, Robert (1990). Japanese Aircraft 1910-1941. Naval Institute Press. ISBN 1557505632.
[edit] External links
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