fbpx
Wikipedia

Mitsubishi 1MF10

The Mitsubishi 1MF10 or Mitsubishi Experimental 7-Shi Carrier Fighter (七試艦上戦闘機) was a prototype Japanese monoplane single-seat carrier-based fighter aircraft of the 1930s. Two were built for the Imperial Japanese Navy, but both were lost in crashes, with no production following.

1MF10
Mitsubishi 1MF10
Role Fighter aircraft
National origin Japan
Manufacturer Mitsubishi Kokuki KK
Designer Jiro Horikoshi
First flight March 1933
Status Prototype
Number built 2

Design and development edit

In April 1932, the Imperial Japanese Navy issued a specification for a replacement for its current carrier-based fighter, the Nakajima A2N, asking for designs from both Mitsubishi and Nakajima. Unlike the biplane which was to be replaced, both competitors submitted monoplanes, with Nakajima offering a version of its Type 91 parasol-wing fighter, already in production for the Japanese Army. Mitsubishi assigned design of its contestant to a team led by Jiro Horikoshi, which created the first low-wing cantilever monoplane to be designed in Japan, the Mitsubishi 1MF10.[1][2]

The 1MF10 was of all-metal construction, with a monocoque duralumin fuselage, with duralumin wing structure covered in fabric, with the pilot accommodated in an open cockpit. The aircraft was powered by a Mitsubishi A4 two-row 14-cylinder radial engine driving a two-bladed propeller. It had a fixed tailwheel undercarriage.[1][2]

The first prototype 1MF10, with the Navy designation Experimental 7-shi Carrier Fighter[a] made its maiden flight in March 1933.[1] It was destroyed in July 1933 when its tail broke up during diving tests, although the pilot escaped by parachute. The second prototype had a revised undercarriage, with the main wheels and undercarriage legs faired into streamlined spats. It was also destroyed in a crash, when it could not be recovered from a flat spin in June 1934 by pilot Motoharu Okamura.[1][2]

Although the design was advanced, it was rejected by the Japanese Navy, having poor handling[1] and not meeting the performance requirements of the specification.[2] It did form the basis of more advanced designs, however, with Horikoshi using elements of it such as the box-spar in the later successful Mitsubishi A5M fighter of similar layout.[4]

Specifications edit

Data from Japanese Aircraft 1910–1941[5]

General characteristics

  • Crew: 1
  • Length: 6.92 m (22 ft 8 in)
  • Wingspan: 10 m (32 ft 10 in)
  • Height: 3.31 m (10 ft 10 in)
  • Wing area: 17.70 m2 (190.5 sq ft)
  • Empty weight: 1,225 kg (2,701 lb)
  • Gross weight: 1,578 kg (3,479 lb)
  • Powerplant: 1 × Mitsubishi A4 14-cylinder air-cooled radial engine, 580 kW (780 hp)

Performance

  • Maximum speed: 320 km/h (199 mph, 173 kn) at 3,000 m (9,800 ft)
  • Endurance: 3 hr

Armament

  • Guns: 2× 7.7 mm machine guns[2]

See also edit

Related development

Aircraft of comparable role, configuration, and era

Appearances in media

Notes edit

  1. ^ In the Japanese Navy designation system, specifications were given a Shi number based on the year of the Emperor's reign it was issued. In this case 7-Shi stood for 1932, the 7th year of the Shōwa era.[3]
  1. ^ a b c d e Mikesh and Abe 1990, p. 170.
  2. ^ a b c d e Green and Swanborough 1994, p. 407.
  3. ^ Mikesh and Abe 1990, pp. 2, 286.
  4. ^ Mikesh and Abe 1990, pp. 170–171.
  5. ^ Mikesh and Abe 1990, p. 171.

References edit

  • Green, William; Swanborough, Gordon (1994). The Complete Book of Fighters. New York: Smithmark. ISBN 0-8317-3939-8.
  • Mikesh, Robert C.; Abe, Shorzoe (1990). Japanese Aircraft 1910–1941. London: Putnam Aeronautical Books. ISBN 0-85177-840-2.


mitsubishi, 1mf10, mitsubishi, experimental, carrier, fighter, 七試艦上戦闘機, prototype, japanese, monoplane, single, seat, carrier, based, fighter, aircraft, 1930s, were, built, imperial, japanese, navy, both, were, lost, crashes, with, production, following, 1mf10. The Mitsubishi 1MF10 or Mitsubishi Experimental 7 Shi Carrier Fighter 七試艦上戦闘機 was a prototype Japanese monoplane single seat carrier based fighter aircraft of the 1930s Two were built for the Imperial Japanese Navy but both were lost in crashes with no production following 1MF10 Mitsubishi 1MF10 Role Fighter aircraft National origin Japan Manufacturer Mitsubishi Kokuki KK Designer Jiro Horikoshi First flight March 1933 Status Prototype Number built 2 Contents 1 Design and development 2 Specifications 3 See also 4 Notes 5 ReferencesDesign and development editIn April 1932 the Imperial Japanese Navy issued a specification for a replacement for its current carrier based fighter the Nakajima A2N asking for designs from both Mitsubishi and Nakajima Unlike the biplane which was to be replaced both competitors submitted monoplanes with Nakajima offering a version of its Type 91 parasol wing fighter already in production for the Japanese Army Mitsubishi assigned design of its contestant to a team led by Jiro Horikoshi which created the first low wing cantilever monoplane to be designed in Japan the Mitsubishi 1MF10 1 2 The 1MF10 was of all metal construction with a monocoque duralumin fuselage with duralumin wing structure covered in fabric with the pilot accommodated in an open cockpit The aircraft was powered by a Mitsubishi A4 two row 14 cylinder radial engine driving a two bladed propeller It had a fixed tailwheel undercarriage 1 2 The first prototype 1MF10 with the Navy designation Experimental 7 shi Carrier Fighter a made its maiden flight in March 1933 1 It was destroyed in July 1933 when its tail broke up during diving tests although the pilot escaped by parachute The second prototype had a revised undercarriage with the main wheels and undercarriage legs faired into streamlined spats It was also destroyed in a crash when it could not be recovered from a flat spin in June 1934 by pilot Motoharu Okamura 1 2 Although the design was advanced it was rejected by the Japanese Navy having poor handling 1 and not meeting the performance requirements of the specification 2 It did form the basis of more advanced designs however with Horikoshi using elements of it such as the box spar in the later successful Mitsubishi A5M fighter of similar layout 4 Specifications editData from Japanese Aircraft 1910 1941 5 General characteristicsCrew 1 Length 6 92 m 22 ft 8 in Wingspan 10 m 32 ft 10 in Height 3 31 m 10 ft 10 in Wing area 17 70 m2 190 5 sq ft Empty weight 1 225 kg 2 701 lb Gross weight 1 578 kg 3 479 lb Powerplant 1 Mitsubishi A4 14 cylinder air cooled radial engine 580 kW 780 hp Performance Maximum speed 320 km h 199 mph 173 kn at 3 000 m 9 800 ft Endurance 3 hr Armament Guns 2 7 7 mm machine guns 2 See also editRelated development Mitsubishi A5M Aircraft of comparable role configuration and era Curtiss P 36 Hawker Hurricane Heinkel He 70 Heinkel He 112 Messerschmitt Bf 109B Nakajima Ki 27 Polikarpov TsKB 12 Seversky P 35 Supermarine Spitfire Appearances in media The Wind RisesNotes edit In the Japanese Navy designation system specifications were given a Shi number based on the year of the Emperor s reign it was issued In this case 7 Shi stood for 1932 the 7th year of the Shōwa era 3 a b c d e Mikesh and Abe 1990 p 170 a b c d e Green and Swanborough 1994 p 407 Mikesh and Abe 1990 pp 2 286 Mikesh and Abe 1990 pp 170 171 Mikesh and Abe 1990 p 171 References edit nbsp Wikimedia Commons has media related to Mitsubishi 1MF10 Green William Swanborough Gordon 1994 The Complete Book of Fighters New York Smithmark ISBN 0 8317 3939 8 Mikesh Robert C Abe Shorzoe 1990 Japanese Aircraft 1910 1941 London Putnam Aeronautical Books ISBN 0 85177 840 2 Retrieved from https en wikipedia org w index php title Mitsubishi 1MF10 amp oldid 1103884944, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.