HOW MUCH YOU NEED TO EXPECT YOU'LL PAY FOR A GOOD APOLLO 3.5 BLUE PLUS PROCESSOR

The S-IVB also continued to thrust at a reduced amount by venting gaseous hydrogen, to keep propellants settled inside their tanks and prevent gaseous cavities from forming in propellant feed traces. This venting also managed Secure pressures as liquid hydrogen boiled off from the fuel tank. This venting thrust simply exceeded aerodynamic drag.[cit