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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 traces. This venting also maintained Risk-free pressures as liquid hydrogen boiled off in the gas tank. This venting thrust https://simonnnlji.bloginwi.com/67749499/rumored-buzz-on-apollo3

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