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Kawasaki Ki-102

From Wikipedia, the free encyclopedia
Heavy fighter aircraft in Japan
Ki-102
Kawasaki Ki-102 B attack plane
General information
TypeAttacker,fighter,night fighter
National originJapan
ManufacturerKawasaki Kōkūki Kōgyō K.K.
StatusRetired
Primary userImperial Japanese Army Air Force
Number built238
History
Introduction date1944
First flight1944
Retired1945
Developed fromKawasaki Ki-96

TheKawasaki Ki-102 orType 4 Attack Plane (四式襲撃機,Yonshiki shūgeki-ki) was a twin-engine, two-seat, long-rangeheavy fighter developed to replace theKi-45Toryū. Three versions were planned: the Ki-102 Kō dayfighter, Ki-102 Bground-attack, and Ki-102 Cnight fighter. This aircraft'sAlliedreporting name was "Randy".

Design and history

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The Ki-102 entered service in 1944 but saw limited action. The main type (Ki-102 B) was kept in reserve to protect Japan, although it did see some limited duty in theOkinawa campaign. It was kept out of front line service because it was hoped that it would be the carrier of theKi-148 air-to-surface guided missile when the Allied invasion of Japan occurred.

Variants

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Ki-102
prototypes, three built
Ki-102 A (kō/甲)
Externally similar to the Ki-102 B, but withturbosuperchargers that enabled the engines to maintain their rating at higher altitudes. The 57 mm (2.24 in) cannon was swapped in favor of a 37 mm (1.46 in) cannon, and the 12.7 mm (.50 in) rear gun was deleted, 26 built.
Ki-102 B (otsu/乙)
Ground-attack variant similar to prototypes, except with revised tail wheel, 207 built
Ki-102 C (hei/丙)
Night fighter version with lengthenedfuselage and span.Radar under aPlexiglas dome, oblique-firing 20 mm cannons, and the 20 mm cannons in the belly replaced with 30 mm (1.18 in) cannons inSchräge Musik behind the cockpit, two built.
Ki-108
High-altitude fighter prototype withpressurised cabin, two conversions from Ki-102 B aircraft using the structural improvements used on the Ki-102 C.
Ki-108 Kai
Improved version of the Ki-108 with longer fuselage and enlarged wings. Two built.

Specifications (Ki-102 B)

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Ki-102 Kō in USAAF markings after the war

Data from Japanese Aircraft of the Pacific War[1]

General characteristics

  • Crew: 2
  • 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[2]
  • Empty weight: 4,950 kg (10,913 lb)
  • Gross weight: 7,300 kg (16,094 lb)
  • Powerplant: 2 ×Mitsubishi Ha112-II Ru 14-cylinder air-cooledradial engine, 1,120 kW (1,500 hp) each
  • Propellers: 3-bladed constant-speed propellers

Performance

  • Maximum speed: 580 km/h (360 mph, 310 kn)
  • Range: 2,000 km (1,200 mi, 1,100 nmi)
  • Service ceiling: 10,000 m (33,000 ft)
  • Rate of climb: 11.9 m/s (2,340 ft/min)
  • Power/mass: 0.417 kW/kg (0.254 hp/lb)

Armament

  • Guns:
    • 1 × 57 mm (2.24 in)Ho-401 cannon—replaced in the 102a with a 37 mm (1.46 in)Ho-204 cannon, deleted in the 102 C
    • 2 × 20 mmHo-5 cannon in the belly—replaced in the 102 C with 30 mm (1.18 in) cannon in the package, plus oblique-firing 2 × 20 mm cannon
    • 1 × 12.7 mm (0.50 in)Ho-103 machine gun (deleted in the Ki-102a and Ki-102)
  • Bombs:
    • 2 × 200 L (53 US gal) drop tanks;or
    • 2 × 250 kg (551 lb) bombsor
    • 1 ×Kawasaki Igo-1b guided missile

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

Footnotes

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  1. ^Francillon1979, pp. 137–138.
  2. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.

References

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  • Francillon, René J. (1979).Japanese aircraft of the Pacific War (2nd ed.). London: Putnam.ISBN 0-370-30251-6.

Further reading

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  • Green, William (1973).War Planes of the Second World War. v. 3 (Seventh impression ed.). London: Macdonald & Co.ISBN 0-356-01447-9.
  • Green, William; Swanborough, Gordon (1976).Japanese Army Fighters / 1. London: Macdonald and Jane's.ISBN 0-356-08224-5.

External links

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Wikimedia Commons has media related toKawasaki Ki-102.
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World War II Allied reporting names
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