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The S-IVB also continued to thrust at a small degree by venting gaseous hydrogen, to maintain propellants settled in their tanks and stop gaseous cavities from forming in propellant feed strains. This venting also taken care of Safe and sound pressures as liquid hydrogen boiled off within the gas https://ambiqapollo52074.popup-blog.com/26376428/examine-this-report-on-apollo-4-blue-lite

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