NASA NTRS · 19720000604
Propulsion sizing program
Abstract
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.
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Kaemming, T. A., Burns, A. E.. 1972-10-01. Propulsion sizing program. https://ntrs.nasa.gov/citations/19720000604
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