CHOICE OF SCHEME OF CHAMBER COOLING OF REUSABLE OXYGEN-METHANE LIQUID PROPELLANT ROCKET ENGINES FOR THE ADVANCED LAUNCHER
Analysis of the variants of the chamber cooling of oxygen-methane engine with a curtain and without the curtain is conducted. On its basis, the scheme of the regenerative cooling of chamber, ensuring reliable operation of the liquid propellant rocket engines is selected. Description of the design of the cooling system is presented.