ROCKET ON ENGINE "РД2С" Russian patent published in 2003 - IPC

FIELD: rocketry, applicable in designing of rockets within a wide range of missions: for anti-tank guided rockets (projectiles) and salvo-fire systems, air defense rockets, rockets of tactical, operational- tactical and strategic missions, for designing of rocket-space equipment and, in particular, transportation systems designed for take-off from the planet, acceleration, injection of payload to orbit and other missions in the space. SUBSTANCE: the rocket consists of a rocket body, engine representing a hollow metal tube of metal with a bottom (barrel), fuel tank for the propellant charge. Positioned in the working space of the engine are the combustion chambers with the propellant charge and electric primers connected to an electric circuit, the combustion chambers are separated by partitions. For a dynamic locking of the working space use is made of the combustion chamber nearest to the outlet from the engine body. EFFECT: reduced weight of the flight charge and enhanced mass of the payload. 3 cl, 2 dwg