The WIG Page Datasheet no. 17

The SM-4 appears to be a further development of the SM-2P7. It is a two-seater with a remarkable dorsal nose rudder. It was used as a trainer and had two turbojet engines, both internally mounted in the fuselage, one forward for providing PAR thrust (KR7-300) and one aft (RU19-300) for cruise thrust. Its wing has an aspect ratio of about 2.
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