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Mitsubishi MC-1

From Wikipedia, the free encyclopedia
Japanese airliner prototype
MC-1
General information
TypeBiplaneairliner
National originJapan
ManufacturerMitsubishi Aircraft Company
Number built1
History
First flight1928
Retired1938
Developed fromMitsubishi B1M

TheMitsubishi MC-1 was a 1920sJapanese single-enginedbiplaneairliner designed and built by theMitsubishi Aircraft Company.[1]

Design and development

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In 1927, the Japanese Department of Communications launched a competition to design and build an indigenous passenger transport aircraft. Mitsubishi's design to meet this requirement was based on itsMitsubishi B1M torpedo bomber, using the wings of the earlier aircraft combined with a new fuselage.[2] The MC-1 was large three-bay biplane powered by a 385 hp (287 kW)Armstrong Siddeley Jaguarradial engine and it had an open cockpit behind the wings for the pilot and room for four (some sources say eight[3]) passengers in an enclosed cabin in the forward fuselage.[1] The MC-1 had a fixedconventional landing gear but could also be fitted with twin floats.[1][2]

The MC-1 was completed in April 1928, and was evaluated against the other two competitors, theAichi AB-1 andNakajima N-36, both of which were also biplanes. No production followed of any of the aircraft, as they were considered obsolete compared with foreign types, and the state-owned airlineJapan Air Transport (Nihon Koko Yuso KK) orderedFokker Universalmonoplanes instead.[2]

Operational history

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Although no production of the MC-1 followed, the prototype was used to operate an experimental air service betweenTokyo andOsaka sponsored by theAsahi Shimbun newspaper between June 1928 and April 1929, and then by Japan Air Transport for services inKorea until May 1930. It was then used as a seaplane flying sightseeing flights around the north coast ofHonshu until 1938.[2]

Specifications (Landplane)

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Data from Japanese Aircraft 1910–1941[2]

General characteristics

  • Crew: 2
  • Capacity: 4 (or 8)[3] passengers
  • Length: 10.475 m (34 ft 4 in)
  • Wingspan: 14.75 m (48 ft 5 in)
  • Height: 3.80 m (12 ft 6 in)
  • Wing area: 59 m2 (640 sq ft)
  • Empty weight: 1,550 kg (3,417 lb)
  • Gross weight: 2,600 kg (5,732 lb)
  • Powerplant: 1 ×Armstrong Siddeley Jaguar 14-cylinder air-cooledradial engine, 287 kW (385 hp)

Performance

  • Maximum speed: 191 km/h (119 mph, 103 kn)
  • Endurance: 6 hr
  • Time to altitude: 3,000 m (9850 ft) in 20 min 36 s

See also

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Related development

Aircraft of comparable role, configuration, and era

References

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Wikimedia Commons has media related toMitsubishi MC-1.

Notes

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  1. ^abcOrbis 1985, p. 2534
  2. ^abcdeMikesh and Abe 1990, p. 193.
  3. ^abWolfram Nickel:Mitsubishi Motors, page 9,ISBN 978-3-942072-06-9, 2016.

Bibliography

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Mitsubishi aircraft
Company designations
Imperial Japanese Army
early designations
Imperial Japanese Army
short designations
Imperial Japanese Navy
short designations
Carrier fighters
Carrier Torpedo Bombers
Reconnaissance aircraft
Carrier dive bombers
Observation seaplanes
Land-based Attack Bombers
Interceptors
Transports
Trainers
Patrol Aircraft
World War II Allied
reporting names
Japanese Self-Defense
Force designations
Company divisions
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