WINGED MISSILE Russian patent published in 1998 - IPC

Abstract RU 2117907 C1

FIELD: missile equipment. SUBSTANCE: winged missile consists of sustainer stage with supersonic engine whose combustion chamber accommodates accelerating stage with jet engine for its ejection through nozzle. Air intake of sustainer stage is made frontal with central body. Air channel is located symmetrically along missile longitudinal axis and front part of accelerating stage is located in air channel and secured to central body. EFFECT: reduced dimensions and increased flight performance of missile. 2 cl, 2 dwg

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RU 2 117 907 C1

Authors

Artamasov O.Ja.

Efremov G.A.

Khomjakov M.A.

Dates

1998-08-20—Published

1997-03-26—Filed