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The S-IVB also continued to thrust in a low stage by venting gaseous hydrogen, to maintain propellants settled within their tanks and forestall gaseous cavities from forming in propellant feed lines. This venting also preserved Harmless pressures as liquid hydrogen boiled off inside the gasoline tank. This venting thrust https://wearables68024.win-blog.com/14515627/5-essential-elements-for-apollo4-plus

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