This invention discloses an open pneumatic
control system for cryogenic liquid
rocket engines, belonging to the field of liquid
rocket engine design. Compared to traditional closed pneumatic control systems, this invention eliminates the valve
assembly box and replaces the control
solenoid valve with a new type of
solenoid valve with anti-
backflow function, and replaces the
pneumatic valve with an anti-
backflow pneumatic valve. Eliminating the valve box also eliminates the need for the valve box cable, requiring only one control cable, reducing electrical interfaces and improving the reliability of electrical products. In the original
closed system, fault isolation between solenoid valves was not possible; this invention, by eliminating the valve box, eliminates mutual interference between controlled valves, achieving fault isolation. The
solenoid valve layout of this invention is more flexible, has higher
structural reliability, facilitates fault isolation, improves functional reliability, and simultaneously reduces engine weight.