5 SIMPLE TECHNIQUES FOR APOLLO3

5 Simple Techniques For apollo3

The S-IVB also continued to thrust at a lower stage by venting gaseous hydrogen, to maintain propellants settled of their tanks and forestall gaseous cavities from forming in propellant feed strains. This venting also managed safe pressures as liquid hydrogen boiled off from the gasoline tank. This venting thrust quickly exceeded aerodynamic drag.[

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