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Kawasaki Ki-96

From Wikipedia, the free encyclopedia
Japanese WWII fighter aircraft
Ki-96
General information
TypeTwin engineheavy fighter
National originJapan
ManufacturerKawasaki Kōkūki Kōgyō K.K.
Number built3
History
First flightSeptember 1943
Developed fromKawasaki Ki-45
Developed intoKawasaki Ki-102

TheKawasaki Ki-96 was a Japanese single seat, twin-engineheavy fighter of World War II. It was intended to replace theKawasaki Ki-45s of theImperial Japanese Army Air Service. However, it was not adopted, and only threeprototypes were built.

Design and development

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The success of theKawasaki Ki-45 led Kawasaki to start development of an evolved version, on Kawasaki's own authority, in August 1942.[1] Like the Ki-45, the proposed design was a two-seat, twin-engine fighter but larger and using more powerful engines. In December 1942, theKoku Hombu (Imperial Japanese Army Aviation Bureau) showed interest but asked Kawasaki to complete the aircraft as single-seat fighters.[1] The first prototype, which was converted while being produced and which retained the largercockpitcanopy intended for the two-seater, flew in September 1943. The two remaining prototypes were built from the start as single-seaters and were fitted with a smaller canopy.[2]

Despite demonstrating performance exceeding estimates and excellent handling, the Army's requirements had changed back to a two-seat fighter,[3] so further development of the Ki-96 was stopped. The wings and tail unit of the Ki-96 would however form part of the structure of theKi-102 two-seat fighter.[3][4]

Specifications (Kawasaki Ki-96)

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Data fromWar Planes of the Second World War - Fighters - Vol. 3;[5] WW2 Aircraft Fact Files: Japanese Army Fighters, Part 1;[4] Japanese Aircraft of the Pacific War[3]

General characteristics

  • Crew: 1
  • Length: 11.45 m (37 ft 7 in)
  • Wingspan: 15.57 m (51 ft 1 in)
  • Height: 3.7 m (12 ft 2 in)
  • Wing area: 34 m2 (370 sq ft)
  • Airfoil:root:NACA 24015;tip:NACA 23010[6]
  • Empty weight: 4,550 kg (10,031 lb)
  • Gross weight: 6,000 kg (13,228 lb)
  • Powerplant: 2 ×Mitsubishi Ha112-II 14-cylinder air-cooledradial engines, 1,125 kW (1,509 hp) each
  • Propellers: 3-bladed constant-speed propellers

Performance

  • Maximum speed: 600 km/h (370 mph, 320 kn) at 6,000 m (20,000 ft)
  • Ferry range: 1,600 km (990 mi, 860 nmi)
  • Service ceiling: 11,500 m (37,700 ft)
  • Time to altitude: 6,000 m (20,000 ft) in 6 minutes
  • Power/mass: 0.38 kW/kg (0.23 hp/lb)

Armament

See also

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Related development

Aircraft of comparable role, configuration, and era

References

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  1. ^abGreen & Swanborough 1976, p. 37.
  2. ^Francillon 1979, p. 127.
  3. ^abcFrancillon 1979, p. 128.
  4. ^abGreen & Swanborough 1976, p. 38.
  5. ^Green 1961, p. 28.
  6. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved2019-04-16.

Bibliography

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External links

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Wikimedia Commons has media related toKawasaki Ki-96.
Kawasaki aircraft
Company designations
Imperial Japanese Army designations
Japanese Self-Defense Force designations
Joint ventures
Licensed production
World War II Allied reporting names
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