About apollo2

The S-IVB also continued to thrust in a low stage by venting gaseous hydrogen, to keep propellants settled of their tanks and stop gaseous cavities from forming in propellant feed strains. This venting also preserved safe pressures as liquid hydrogen boiled off from the fuel tank. This venting t
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15