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The S-IVB also ongoing to thrust at a small degree by venting gaseous hydrogen, to maintain propellants settled within their tanks and forestall gaseous cavities from forming in propellant feed traces. This venting also managed Protected pressures as liquid hydrogen boiled off from the fuel tank. This venting thrust https://conneroponj.onzeblog.com/33954283/not-known-facts-about-apollo4-plus

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