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The S-IVB also continued to thrust in a minimal amount by venting gaseous hydrogen, to help keep propellants settled of their tanks and prevent gaseous cavities from forming in propellant feed strains. This venting also taken care of Harmless pressures as liquid hydrogen boiled off inside the gasoline tank. https://low-power-soc08639.widblog.com/88871215/5-simple-statements-about-ambiq-apollo-4-explained

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