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Projet Shin Meiwa KJT-1


The Shin Meiwa KJT-1 basic trainer was designed for two 900 lb. thrust Marbore's ( or alternatively,  the Allison J33 turbojet ). The turbojets would be mounted side-by-side in the fuselage, were fed via lateral intakes and exhaust under the rear fuselage.

The KJT-1 had an estimated maximum speed of 478 m.p.h. and an endurance of 2.2 hours cruising at 311 m.p.h. at 26,250 ft.

The crew of two were seated side-by-side.