NASA NTRS · 19750025075
Computer controlled vent and pressurization system
Abstract
The Centaur space launch vehicle airborne computer, which was primarily used to perform guidance, navigation, and sequencing tasks, was further used to monitor and control inflight pressurization and venting of the cryogenic propellant tanks. Computer software flexibility also provided a failure detection and correction capability necessary to adopt and operate redundant hardware techniques and enhance the overall vehicle reliability.
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Cieslewicz, E. J.. 1975-01-01. Computer controlled vent and pressurization system. https://ntrs.nasa.gov/citations/19750025075
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