NASA/SP-8112, PRESSURIZATION SYSTEMS FOR LIQUID ROCKETS, NASA SPACE VEHICLE DESIGN CRITERIA (CHEMICAL) (OCT 1975)

NASA/SP-8112, PRESSURIZATION SYSTEMS FOR LIQUID ROCKETS, NASA SPACE VEHICLE DESIGN CRITERIA (CHEMICAL) (OCT 1975)., Guidelines for the successful design of pressurization systems for main propulsion, auxiliary propulsion, and attitude control systems for boosters, upper stages, and spacecraft were presented, drawing on the wealth of design experience that has accumulated in the development of pressurization systems for liquid rockets operational in the last 15 years. The design begins with a preliminary phase in which the system requirements are received and evaluated. Next comes a detail-design and integration phase in which the controls and the hardware components that make up the system are determined. The final phase, design evaluation, provides analysis of problems that may arise at any point in the design when components are combined and considered for operation as a system. Throughout the monograph, the design tasks are considered in the order and manner in which the designer must handle them.