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The WIG Page Datasheet no. 16

SM-3

from

JSC R.E. Alexeiev Central Hydrofoil Design Bureau

The SM-3 has a very low aspect ratio wing (0.48) with endplates and an enormous horizontal stabilizer. It was a test vehicle for a very long chord design, but it was very unstable. The single seater was powered by one nose mounted RU19-300 turbojet engine.

Technical data

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Plan views

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Pictures of SM-3

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18737A. BelyaevSM-3 cruising over snow
5676A. BelyaevSM-3 gliding over snow

Movies of SM-3

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