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Detailed Notes on apollo mcu

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The S-IVB also continued to thrust at a small degree by venting gaseous hydrogen, to maintain propellants settled of their tanks and forestall gaseous cavities from forming in propellant feed traces. This venting also maintained Harmless pressures as liquid hydrogen boiled off in the gasoline tank. This venting thrust https://juliusk395onn1.eveowiki.com/user

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