FIELD: weapons and ammunition.
SUBSTANCE: invention relates to ammunition, particularly to apparatuses with gasostatic suspension. Shell with gasostatic suspension contains military and guide part. In the guiding part of the feed cavity is made to create pressure in the carrying gas layer of gas-static suspension. Feed cavity is connected with outer cylindrical surface through feeding devices in the form of holes of small diameter. Feed cavity is filled with substance having high combustion rate, and is connected to the rear part of the missile through the hole. Guiding part is made in the form of a thick-wall shell having a hole in the bottom. Warhead is arranged partially inside said shell to form U-shaped cavity filled with substance having high combustion rate. Holes feeding the gasostatic suspension are arranged in cylindrical wall of the shell in at least two zones within the volume of U-shaped cavity.
EFFECT: higher efficiency of missile with gasostatic suspension.
1 cl, 6 dwg
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