Mansyū Ki-98

Mansyū Ki-98
Ki-98
Role Ground-attack aircraft
National origin Japan
Manufacturer Mansyū
Primary user Imperial Japanese Army Air Force (intended)
Number built None

The Mansyū Ki-98 was a Japanese ground-attack aircraft proposed by Mansyū during World War II for use by the Imperial Japanese Army Air Force. No prototype was completed before Japan surrendered.

Contents

Design and development

Mansyū began work on the design of the Ki-98 in 1943. It was to have been a single-seat, twin-boom, low-wing monoplane with a central nacelle housing both the cockpit and a turbosupercharged 1,643-kilowatt (2,200-hp) Mitsubishi Ha-211 Ru radial engine behind the pilot driving a four-bladed pusher propeller rotating between the booms.[1] The booms were to extend aft from slightly forward of the leading edge of the wing and were mounted below the central nacelle.[1] The aircraft was to have had tricycle landing gear, a bubble canopy, and an armament of one 37-mm and two 20-mm cannon mounted in the nose.[1]

The first prototype was still under construction when Japan surrendered to the Allies on 15 August 1945, bringing the Ki-98 project to an end.[1]

Specifications

Data from Francillon, René J., Japanese Aircraft of the Pacific War, Annapolis, Maryland: Naval Institute Press, 1979, ISBN 0-87021-313-X, p. 486.

General characteristics

  • Crew: One
  • Length: 11.4 m (37 ft 4.8125 in)
  • Wingspan: 11.26 m (36 ft 11.3125 in)
  • Height: ()
  • Loaded weight: 4,500 kg (9,921 lbs)
  • Powerplant: 1 × Mitsubishi Ha-211 Ru turbosupercharged radial engine, 1,643 kW (2,200 hp)

Performance

Armament

  • 1× 37-mm cannon
  • 2× 20-mm cannon

See also

Aircraft of comparable role, configuration and era

Related lists

References

Notes

  1. ^ a b c d Francillon, p. 486.

Bibliography

  • Francillon, René J. Japanese Aircraft of the Pacific War. Annapolis, Maryland: Naval Institute Press, 1979. ISBN 0-87021-313-X.

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