FIELD: rocketry.
SUBSTANCE: proposed jet engine has body on which one or several combustion chambers are fastened in walls of which shaped outlet channels are made. Design peculiarity of engine is that its body has at least one central power post connecting front and rear parts of body. Combustion chambers are fastened on rear end of post, their outlet channels being pointed forward towards head part of rocket or at angle to said direction, and on other end of central post pointed to side of head part of rocket gas deflecting dome-like screen is secured whose front torus like wall is pointed to side of head part of rocket, and open end of screen is pointed backwards and communicates with open space.
EFFECT: increased efficiency of engine.
8 cl, 18 dwg
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