The ares rocket has a liquid oxygen tank that sits on top of the core stage. The turbopump inlet for the engines on the core stage must have a certain pressure to operate correctly. The engine designer has asked you to calculate the range of pressures he must account for.calculate the pressure at the inlet for both a full tan and a nearly empty tank. Assume the vehicle accelerates at a maximum of 4g's. The density of liquid oxygen is 71.14 lbm/ft3
Picture a rocket with liquid oxygen on top l= 50', and liquid hydrogen on bottom l=180'
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