High Pressure Rocket Liquid Propellant Feeding System Using Gas-Pressurized Method

摘要

gas pressurization method of the present invention is used in liquid propellant rocket propellant supply to the combustion chamber of a high pressure system relates to the structure and shape of . ; this invention is by placing two or more small-capacity high-pressure tank between the low pressure of the propellant storage tanks and rocket combustion chamber is a lightweight structure , the low-pressure store propellant and the charge in the small-capacity high-pressure tank from a supply tank and a rocket engine combustion chamber by the pressure of this gas by the high-pressure , two or more high-pressure tank at a high pressure that can be supplied to the high-pressure constant as a rocket propellant rocket combustion chamber by operating in sequence relates to a liquid propellant gas pressure device that can provide a way .