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The S-IVB also continued to thrust in a reduced amount by venting gaseous hydrogen, to keep propellants settled inside their tanks and prevent gaseous cavities from forming in propellant feed strains. This venting also preserved Risk-free pressures as liquid hydrogen boiled off within the gasoline tank. This venting thrust https://ultralowpowermicrocontrol54195.techionblog.com/33948848/5-simple-techniques-for-apollo3

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