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Mitsubishi K7M

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Mitsubishi K7M
Role Experimentalcrew trainer
National origin Japan
Manufacturer Mitsubishi
First flight 1938
Primary user Imperial Japanese Navy
Number built 2

TheMitsubishi K7M(orMitsubishi Ka-18) was a 1930sJapaneseexperimentalcrew trainerbuilt byMitsubishifor theImperial Japanese Navyto replace theK3M.[1]

Design and development[edit]

The K7M was a cantilever high-wing monoplane with a cabin for five students and two instructors,[1]and was of metal construction, with fabric-covered outer wings.[2]The K7M was powered by two 340 hp (254 kW)Gasuden Tempuradial piston engines.[1]The Navy decided the twin-engined type was too costly to replace the single-engined K3M and the type was not developed further, the two prototypes did enter service as trainers with the designationK7M1.[1]

Operators[edit]

Japan

Specifications[edit]

Data from[1]

General characteristics

  • Crew:2
  • Capacity:5 students, 2 instructors.
  • Length:13.23 m (43 ft 5 in)[2]
  • Wingspan:19.96 m (65 ft 6 in)[2]
  • Height:3.45 m (11 ft 4 in)[2]
  • Empty weight:2,558 kg (5,640 lb)[2]
  • Gross weight:3,810 kg (8,400 lb)[2]
  • Powerplant:2 ×Gasuden Tempuradial piston engine, 250 kW (340 hp) each

Performance

  • Maximum speed:260 km/h (160 mph, 140 kn)
  • Range:950 km (590 mi, 510 nmi)[2]

Armament

  • Guns:2 × 7.7mm (0.303in) machine-gun
  • Bombs:up to 90kg (198lb)

See also[edit]

Related lists

References[edit]

Notes[edit]

  1. ^abcdeOrbis 1985, pp. 2519-2520
  2. ^abcdefgAir PictorialJanuary 1970, p. 29.

Bibliography[edit]

  • Richards, M.C. (1970). "Your Questions Answered...:Mitsubishi Trainers".Air Pictorial.No. January 1970. p. 29.
  • TheIllustrated Encyclopedia of Aircraft(Part Work 1982-1985).Orbis Publishing.