The S-IVB also continued to thrust in a minimal amount by venting gaseous hydrogen, to keep propellants settled of 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://ambiq.com/news/ambiq-apollo510-delivers-30x-power-efficiency-improvement-to-unleash-edge-ai/
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