ROCKET Russian patent published in 1999 - IPC

FIELD: rocketry, applicable for creation of rockets of various purpose. SUBSTANCE: the rocket has a solid- propellant engine with a nozzle, attached to which is a gas generator by means of calibrated components forming an ignition chamber between the nozzle, gas generator and cylindrical shell made on its body. A gas conduit connecting the ignition chamber and explosive initiator is made inside the gas generator. The gas generator combustion chamber is gas-linked with the ignition chamber and launching tube space. In the initial position, prior to launching, the rocket is retained by a locking device engageable with the gas generator. EFFECT: enhanced reliability of the rocket launching system. 1 dwg