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Mitsubishi Q2M Taiyo

Military Aircraft

The Mitsubishi Q2M Taiyo, meaning Great Sea or Ocean, was a design derived from the Mitsubishi Ki-67-I Hiryu heavy and torpedo bomber of the Japanese Army and from its Naval variant, the Yasukuni. It was ordered for design and construction in the last stages of the Second World War. The plan called for a crew of five or six, two Mitsubishi Kasei 25 Otsu 14-cylinder radial engines of about 1,353 kilowatts each driving five-blade propellers, a length of 18.75 metres, a wingspan of 25 metres and a top speed of 490 kilometres per hour. Technical troubles and a long development of the theoretical design kept it from advancing beyond paper plans before the war ended.

Facts
Engine Class
Piston 1
Status
Design only (never built) 1
Top Speed (km/h)
490 1
Mass (kg)
8850 1
Engine
Mitsubishi Kasei 25 Otsu 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Mitsubishi Q2M Taiyo (Wikipedia)

Of Make

Source Mitsubishi Q2M Taiyo (Wikipedia)
Sources
1. Mitsubishi Q2M Taiyo (Wikipedia)
  • Development
    did not advance from paper plans
  • Specification (Q2M)
    Empty weight: 8,850 kg (19,511 lb)
  • Specification (Q2M), top speed
    Maximum speed: 490 km/h (300 mph, 260 kn)
  • Specification (Q2M), engine class
    14-cylinder air-cooled radial piston engines
  • Specification (Q2M), engine
    Mitsubishi Kasei 25 Otsu 14-cylinder
  • Lead
    heavy/torpedo bomber of the Japanese Army
  • Lead, manufacturer
    design was derived from the Mitsubishi Ki-67-I
  • Lead, country of origin
    of the Japanese Army and its Naval variant
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