HIGH PRESSURE ROCKET LIQUID PROPELLANT FEEDING SYSTEM USING GAS-PRESSURIZED METHOD

摘要

The present invention relates to a structure and form of the system for feeding the high-pressure propellant into the combustion chamber of a liquid propellant rocket using a pressurized gas system.; The present invention by placing a small-capacity high-pressure tanks of two or more between which is a light-weight structure of the low-pressure propellant storage tanks and rocket combustion chamber, and charge the propellants in small-capacity high-pressure tank from a storage tank of the low-pressure pressurized by it to the high pressure gas the present invention relates to rocket supply to the engine combustion chamber, and which can supply a liquid propellant rocket at a high pressure, which by two or more high-pressure tank is operated in order to supply the high pressure constant for the propellant in a rocket combustion chamber gas pressure system device.