METHOD FOR HOT STAGING OF SOLID-PROPELLED SEA-BASED MISSILE AND DEVICE FOR ITS REALIZATION Russian patent published in 2004 - IPC

FIELD: rocketry, applicable in designing of staging mechanisms of solid-propelled missiles. SUBSTANCE: in the process of starting of the power plant of the subsequent stage in the closed chamber of the interstage compartment, the front bottom of the power plant of the previous stage is destructed in the area of the nozzle of the power plant of the subsequent stage, the jet of hot gases from the power plant of the subsequent stage is passed through the combustion chamber of the power plant of the previous stage. EFFECT: reduced disturbances from the thermal and power action of the reflected jets of hot gases delivered to the sealed chamber of the interstage compartment from the power plant of the subsequent stage in the process of separation of stages. 2 cl, 3 dwg, 1 ex