To meet the IJN requirements of 1943, (18-shi-Otsu non-official specification) calling for a land-based, high-performance interceptor able to counter the new Allied fighters, Nakajima proposed the twin engine J5N1 Tenrai and Kawasaki the J6K1 Jinpu. Early in 1943 Lieutenant Commander Masaoki Tsuruno, of the First Naval Air Technical Arsenal, proposed the construction of a 18-shi-Otsu ‘canard’ fighter based on the information obtained on the Curtiss XP-55.
The Kaigun Koku Hombu ordered the firm Chigasaki Seizo K.K. the construction of three wooden experimental gliders MXY6, with ‘canard’ lifting surfaces, to prove the feasibility of the concept. Glider tests, towed by one Nakajima B5N bomber, began at Yokosuka in the fall of 1943, demonstrating good flight characteristics. One of the prototypes was finally fitted with a 22 hp Nihon Semi Ha-90/11 four-cylinder-boxer, air-cooled engine, driving a two-bladed wooden airscrew from a Kugisho MXY4 anti-aircraft target.
In 1945 the MXY6 was proposed to the IJN as a prototype suicide plane, but the project was not carried out because of the priority given to the construction of the Showa Toka bomber.
MXY6 3rd prototype technical data
Wingspan: 9.14 m, length: 7.3 m, height: 2.95 m, wing area: 17 sq. m, max weight: 500 kg, max speed: 320 kph.