Mitsubishi_Ki-57

Mitsubishi Ki-57

Mitsubishi Ki-57

Japanese transport aircraft


The Mitsubishi Ki-57 was a Japanese passenger transport aircraft, developed from the Ki-21 bomber, during the early 1940s.

Quick Facts Ki-57, Role ...

Development

In 1938, when the Ki-21 heavy bomber began to enter service with the Imperial Japanese Army, its capability attracted the attention of the Imperial Japanese Airways. In consequence, a civil version was developed and this, generally similar to the Ki-21-I and retaining its powerplant of two 708 kW (950 hp) Nakajima Ha-5 KAI radial engines, differed primarily by having the same wings transferred from a mid- to low-wing configuration and the incorporation of a new fuselage to provide accommodation for up to 11 passengers. This transport version appealed also to the navy, and following the flight of a prototype in August 1940 and subsequent testing, the type was ordered into production for both civil and military use.[1]

This initial production Ki-57-I had the civil and military designations of MC-20-I and Army Type 100 Transport Model 1, respectively. A total of 100 production Ki-57-Is had been built by early 1942, and small numbers of them were transferred for use by the Japanese navy in a transport role, then becoming redesignated L4M1. After the last of the Ki-57s had been delivered production was switched to an improved Ki-57-II, which introduced more powerful 805 kW (1,080 hp) Mitsubishi Ha-102 14-cylinder radial engines installed in redesigned nacelles and, at the same time, incorporated a number of detail refinements and minor equipment changes. Civil and military designations of this version were the MC-20-II and Army Type 100 Transport Model 2, respectively. Only 406 were built before production ended in January 1945. Both versions were covered by the Allied reporting name "Topsy".[2]

Variants

MC-20-II with the nickname Hakutsuru (white crane) during the Sino-Japanese war
  • Ki-57-I Army Type 100 Transport Model 1: Powered by two 708 kW (950 hp) Nakajima Ha-5 KAI radial engines and a redesigned fuselage to accommodate 11 passengers. About 100 aircraft of this type were built including the civil version.
  • MC-20-I: Same as above but built for civil use with Imperial Japanese Airways (Dai Nippon Koku KK).
  • Ki-57-II Army Type 100 Transport Model 2:Powered by two 805 kW (1,080 hp) Mitsubishi Ha-102 Zuisei 14-cylinder radial engines installed in redesigned nacelles. Minor equipment and detail refinements were also incorporated. 306 aircraft of this type were produced before the end of production in January 1945.
  • MC-20-II: Same as above but built for civil use with Imperial Japanese Airways (Dai Nippon Koku KK).
  • L4M1: A small number of Ki-57-Is were transferred for test by the Japanese navy as transports and were redesignated L4M1.

Operators

A wrecked Ki-57 on Honshu in late 1945

Wartime

Military operators

 Japan
 Manchukuo

Civil operators

 Japan
 Manchukuo
Reorganized National Government of China
  • One MC-20 used as presidential transport
 Second Philippine Republic
  • One MC-20 used as presidential transport

Post-war

 China
  • The last Ki-57 was used as a trainer and retired in 1952.
 Japan
 Netherlands
  • Captured aircraft, used by the KNIL.

Accidents and incidents

  • On 20 December 1940, an Imperial Japanese Airways MC-20-I (J-BGON, Myuko) crashed into Tokyo Bay off Chiba during CAB's test flight, killing all 13 on board including 8 CAB inspectors.[citation needed]
  • On 21 June 1941, a Manchurian Air Transport MC-20 (M-604) crashed into the Sea of Japan, killing all 18 on board.[citation needed]

Specifications (Ki-57-II)

3-view drawing of the Mitsubishi Ki-57

Data from Japanese Aircraft of the Pacific War [4]

General characteristics

  • Crew: 4 (pilot, co-pilot, navigator and radio operator)
  • Capacity: 11 passengers
  • Length: 16.1 m (52 ft 10 in)
  • Wingspan: 22.6 m (74 ft 2 in)
  • Height: 4.86 m (15 ft 11 in)
  • Wing area: 70.08 m2 (754.3 sq ft)
  • Empty weight: 5,585 kg (12,313 lb)
  • Gross weight: 8,173 kg (18,018 lb)
  • Max takeoff weight: 9,120 kg (20,106 lb)
  • Powerplant: 2 × Mitsubishi Ha-102 Zuisei 14-cylinder air-cooled radial engine, 805 kW (1,080 hp) each for take-off
  • Propellers: 3-bladed variable-pitch propellers

Performance

  • Maximum speed: 470 km/h (290 mph, 250 kn) at 5,800 m (19,000 ft)
  • Range: 3,000 km (1,900 mi, 1,600 nmi)
  • Service ceiling: 8,000 m (26,000 ft)
  • Time to altitude: 5,000 m (16,000 ft) 15 minutes 45 seconds
  • Wing loading: 116.6 kg/m2 (23.9 lb/sq ft)

See also

Related development

Related lists


References

  1. Francillon 1979, pp. 182–183
  2. Francillon 1979, pp. 183–184
  3. Francillon 1979, pp. 184–185.
Bibliography
  • Francillon, Ph.D., René J. The Mitsubishi Ki-21 (Aircraft in Profile number 172). Leatherhead, Surrey, UK: Profile Publications Ltd., 1967.
  • Francillon, René J. (1979). Japanese aircraft of the Pacific War. London: Putnam. ISBN 0-370-30251-6. OCLC 6124909. (new edition 1987 by Putnam Aeronautical Books, ISBN 0-85177-801-1); 3rd edition 1987 by Putnam Aeronautical Books, 1987. ISBN 0-85177-801-1).

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