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The S-IVB also continued to thrust in a reduced stage by venting gaseous hydrogen, to keep propellants settled within their tanks and stop gaseous cavities from forming in propellant feed strains. This venting also maintained Risk-free pressures as liquid hydrogen boiled off in the gas tank. This venting thrust https://ambiqapollo401098.full-design.com/5-essential-elements-for-apollo4-plus-69448821

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