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The S-IVB also continued to thrust at a small degree by venting gaseous hydrogen, to help keep propellants settled in their tanks and stop gaseous cavities from forming in propellant feed strains. This venting also maintained Risk-free pressures as liquid hydrogen boiled off during the fuel tank. This venting https://andrezzxwt.tinyblogging.com/the-apollo2-diaries-70332367

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