WAY GONE parts department stages of launch vehicles from orbit payload DEVICE FOR ITS IMPLEMENTATION

摘要

1. A method for disposal octane-booster stage based on gasification of liquid residues nevyrabotannyh MCT in the oxidizer and fuel tanks, providing a brake pulse due to their combustion chamber RDT and high expiration of combustion products in the space, characterized in that the gasification residues nevyrabotannyh MCT solid gas generating compositions are used, in which tank serves solid oxidant gas generating compositions with an excess of oxygen and fuel in the tank - with lack of oxygen, with that the chemical composition and the amount of solid gas generating compositions at the lowest possible residues MCT determined from the conditions for implementing predetermined magnitude characteristic velocity :, somewhere pulse realized through minimal residues nevyrabotannyh MCT in tanks octane and solid gas generating compositions required for their gasification ;, - pulse realized only by the combustion of a solid gas generating gases GRD sostavov.2. A method according to claim 1, characterized in that the solid-gas generating composition for fuel tank include metal or aluminum component selected from the group of hydride compounds comprising light metals to improve energetiki.3. Device for implementing the method of the propulsion system, comprising in its structure fuel tanks oxidant and fuel tank pressurization system, the gas propellant rocket engine with the system power and system gasification propellants residues, characterized in that the controller is provided with a solid-fuel gas generators, the outputs of which are connected to devices