| 摘要 |
FIELD: defense industry; production of rocket missiles. ^ SUBSTANCE: the invention is dealt with the field of arms and may find application in the guided-missile systems of a short-range radius of action. A rocket missile contains a separated engine with a sustainer stage, the rear part of which is joined with a located in the engine sleeve, in which there is an installed ignition device. Between the sustainer stage rear butt, walls of the sleeve and the ignition device there is a cavity connected with a combustion chamber of the separated engine through a throttle valve. The rear part of the sustainer stage is supplied with the heat-insulating pan linked with the sleeve with the help of a destructible element located along the axis of the rocket missile. Production of a rocket missile in compliance with the offered invention will allow to ensure reduction of the temperature dispersion of the maximum speed of the rocket missile due to application of a self-adjustable mode of operation of the offered design. ^ EFFECT: the invention will allow to ensure reduction of the temperature dispersion at the maximum speed of the rocket missile. ^ 3 cl, 1 dwg |
