A high-performance rocket using LOX as the oxidizer might have a chamber pressure of about 21MPa. If the density of LOX is 1141kg/m³, how tall would the tank have to be to produce the same fuel pressure using gravity alone? Comment on the feasibility of such a design.
A high-performance rocket using LOX as the oxidizer might have a chamber pressure of about 21MPa. If the density of LOX is 1141kg/m³, how tall would the tank have to be to produce the same fuel pressure using gravity alone? Comment on the feasibility of such a design.
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