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Mitsubishi A7M Reppu

Military Aircraft

The Mitsubishi A7M Reppu, meaning Strong Wind and code-named Sam by the Allies, was designed as the successor to the Imperial Japanese Navy A6M Zero, with development starting in 1942 to a 16-Shi specification. It was meant to beat the Zero in speed, climb, diving, armament and manoeuvrability, aims that were met by the end of development in 1945. The first prototype, the A7M1 with a Nakajima Homare engine, flew on 6 May 1944 and was underpowered, so the A7M2 took a Mitsubishi Ha-43 engine of about 1,600 kilowatts and reached 627 to 628 km/h. Limits on Japanese industry, an earthquake in December 1944 and bombing of Nagoya in 1945 stopped it ever entering mass production or active service.

Facts
Year
1944 1
Engine Class
Piston 1
Status
Cancelled 1
Power (kW)
1600 1
Top Speed (km/h)
628 1
Mass (kg)
3226 1
Comparison
Body Style
Aircraft (no road body style) 1
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Source Mitsubishi A7M Reppu (Wikipedia)

Of Make

Source Mitsubishi A7M Reppu (Wikipedia)
Sources
1. Mitsubishi A7M Reppu (Wikipedia)
  • Lead
    was designed as the successor to the Imperial Japanese Navy's A6M Zero
  • Design and development, first flight
    officially flew for the first time on 6 May 1944
  • Lead, status
    prevented the A7M from ever entering mass production or being deployed for active duty
  • Specifications, maximum speed
    Maximum speed: 628 km/h (390 mph, 339 kn) at 6,600 m (21,700 ft)
  • Specifications, empty weight
    Empty weight: 3,226 kg (7,112 lb)
  • Specifications, powerplant
    1,600 kW (2,200 hp)
  • Specifications, powerplant, engine class
    18-cylinder air-cooled radial piston engine
  • Design and development
    Towards the end of 1940, the Imperial Japanese Navy asked Mitsubishi to start design on a carrier-based fighter
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