Kyushu J7W Shinden

The first flight of the unique Kyushu J7W Shinden (magnificent lightning), a canard-configuration single-seat fighter, was made on 3 August 1945, but the end of World War II later that month brought an end to development and production plans. Designed by a team under the leadership of Captain Masaoki Tsuruno of the Imperial Japanese Navy, the configuration of this aircraft had been effectively confirmed by the flight testing of three specially designed and built MXY6 gliders. The construction of two J7W1 prototypes followed, these each having a slender fuselage and mounting in a mid-position on the nose a short-span foreplane incorporating elevators at the trailing edge. The rear-mounted cantilever monoplane wing was set low on the fuselage, had moderately swept leading edges and conventional ailerons with, just inboard of these on each wing, a fin and rudder extending above and below the trailing edge. The landing gear was of retractable tricycle type; the pilot was accommodated in an enclosed cockpit, directly above the leading edge of the wing; and power was provided by a 1588kW Mitsubishi MK9D radial engine, mounted in the rear fuselage to drive a six-blade pusher propeller. By the end of the war the second prototype had been completed but not flown.

The J7W1 spanned 11.11m, had a maximum take-off weight of 5288kg, and was estimated to have a maximum speed of 750km/h. Armament was four nose-mounted 30mm Type 5 cannon. In the planning stage was the J7W2 version to be powered by a 900kg thrust Ne-130 turbojet.

3-View

A three-view drawing (752 x 1204)