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Kawanishi E11K

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E11K
Role Night reconnaissance/transport flying boat
National origin Japan
Manufacturer Kawanishi Aircraft Company
First flight 11 June 1937
Primary user Imperial Japanese Navy
Number built 2

The Kawanishi E11K was a Japanese flying boat of the 1930s. It was designed as a night reconnaissance aircraft for the Imperial Japanese Navy, but was not accepted, the two aircraft built being used as transports as the Type 96 Transport Flying Boat during the Second World War.

Development and design

In 1936 the Imperial Japanese Navy drew up a requirement for an aircraft to replace the Aichi Type 96 Reconnaissance Seaplane as a specialised night reconnaissance aircraft, intended to spot naval gunfire in night actions and to shadow enemy forces at night, allowing submarines to be directed to targets.[1] The requirement was passed to Aichi and Kawanishi, with both companies producing aircraft to meet the navy's needs. While Aichi produced a biplane similar to the aircraft that was to be replaced, Kawanishi designed a gull winged cantilever monoplane. It was powered by a single pusher Hiro Type 91 w engine strut mounted above the wing driving a four-bladed propeller, with its radiator mounted in a fairing above the rear fuselage so that it was located in the propellers slipstream.It was fitted with retractable wingtip floats, while its wings folded to aid storage aboard the cruisers of the Japanese Navy.[2][3]

Specifications (variant)

Data from Japanese Aircraft 1910-1941 [4]

General characteristics

  • Crew: 3
  • Length: 11.90 m (39 ft 1 in)
  • Wingspan: 16.19 m (53 ft 1 in)
  • Height: 4.504 m (14 ft 9 in) (Transport aircraft 4.40 m (14 ft 5.25 in))
  • Wing area: 38 m2 (410 sq ft)
  • Empty weight: 2,170 kg (4,784 lb) (Transport aircraft 2,720 kg (5,996 lb))
  • Gross weight: 3,300 kg (7,275 lb) (Transport aircraft 3,860 kg (8,509 lb))
  • Powerplant: 1 × Hiro Type 91-1 water-cooled twelve-cylinder w engine, 460 kW (620 hp)
  • Propellers: 4-bladed

Performance

  • Maximum speed: 232 km/h (144 mph, 125 kn)
  • Cruise speed: 130 km/h (81 mph, 70 kn)
  • Range: 1,520 km (940 mi, 820 nmi)
  • Endurance: 8.4 hr
  • Service ceiling: 3,795 m (12,451 ft)

Notes

  1. ^ Mikesh and Abe 1990, p.139.
  2. ^ Mikesh and Abe 1990, pp. 139–140.
  3. ^ Green 1968, p.129.
  4. ^ Mikesh and Abe 1990, p.140.

References

  • Green, William. War Planes of the Second World War: Volume Five Flying Boats. London:Macdonald, 1968. ISBN 0 356 01449 5.
  • Mikesh, Robert and Shorzoe Abe. Japanese Aircraft 1910-1941. London:Putnam, 1990. ISBN 0 85177 840 2.