Propulsion sizing program

Computer program was written to evaluate and define optimum design parameters of low pressure auxiliary propulsion system. APS will provide attitude and translational control of space shuttle vehicles. Program evaluates subsystem design parameters such as engine chamber pressure, mixture ratio, expansion ratio, and subsystem component weight and size

Space shuttle high pressure auxiliary propulsion subsystem definition study Subtask B report

Space shuttle high pressure, hydrogen oxygen auxiliary propulsion subsystem preliminary desig