Kawasaki Ki-91

Summary

The Kawasaki Ki-91 was a Japanese heavy bomber developed by Kawasaki Aircraft Industries during the later years of World War II.

Ki-91
Mockup of the Ki-91
Role Heavy bomber
Manufacturer Kawasaki Aircraft Industries
Primary user Imperial Japanese Army Air Service (planned)
Produced 0 (1st prototype 60% complete)

Development edit

In early 1943, following the cancellation of the Nakajima Ki-68 and Kawanishi Ki-85 due to the failure of the Nakajima G5N, Kawasaki responded to the Imperial Japanese Army's requirement for a long-range bomber of similar size and performance to the B-29 Superfortress with the Ki-91. Like the G5N, Ki-68, and Ki-85, the Ki-91 was to be capable of launching attacks on the continental US from Japan. In April 1944, a wooden mockup was built for inspection, and by May production of the first prototype was ordered. Construction of the prototype began in June, but the first B-29 raids on Japan were underway beginning that month. In February 1945, the first Ki-91 prototype was 60 percent complete when a B-29 air raid damaged the facility in Gifu Prefecture where the Ki-91 prototype was being built, bringing the program to a halt.[1]

Design edit

The Ki-91 was a design for a heavy bomber similar in size and bombload to the B-29 Superfortress and Consolidated B-32. It had a bigger wingspan and fuselage than the B-29 and B-32, and featured a pressurized cabin to allow high altitude flights. The prototype was to lack a pressurized cabin, but production aircraft were to be built with the pressurized cabin.[1]

Specifications edit

Data from [1]

General characteristics

  • Crew: 8
  • Length: 32.97 m (108 ft 2 in)
  • Wingspan: 47.9 m (157 ft 2 in)
  • Height: 9.99 m (32 ft 9 in)
  • Wing area: 223.99 m2 (2,411.0 sq ft)
  • Empty weight: 33,999 kg (74,955 lb)
  • Gross weight: 57,999 kg (127,866 lb)
  • Powerplant: 4 × Mitsubishi Ha-214 Ru 18-cylinder air-cooled radial piston engines, 1,900 kW (2,500 hp) each
  • Propellers: 4-bladed constant-speed propeller

Performance

  • Maximum speed: 580 km/h (360 mph, 310 kn) at 9,808 m (32,178 ft)
  • Range: 9,000–10,000 km (5,600–6,200 mi, 4,900–5,400 nmi)
  • Service ceiling: 13,500 m (44,300 ft)
  • Time to altitude: 8,000 m (26,000 ft) in 20 minutes 30 seconds

Armament

  • Guns:
12x 20 mm (0.787 in) machine guns (8 in a double gun-mount configuration and 4 in a quadruple gun-mount configuration)
  • Bombs: up to 4,000 kg (8,800 lb) of bombs

See also edit

References edit

  1. ^ a b c Dyer, Edwin M. III (2009). Japanese Secret Projects:Experimental aircraft of the IJA and IJN 1939–1945 (1st ed.). Hinkley: Midland publishing. pp. 14–16. ISBN 978-1-85780-317-4.

Further reading edit

  • Collier, Basil. Japanese aircraft of World War II (1st American ed.). Mayflower Books. ISBN 0-8317-5137-1.
  • Francillon, René J., Ph.D (1979). Japanese aircraft of the Pacific War (2 ed.). Putnam. ISBN 0-370-30251-6.{{cite book}}: CS1 maint: multiple names: authors list (link)