The total propellant flow at the pump outlet is ____________ the flow in combustion chamber and the discharge pressure is __________ chamber pressure plus the other insignificant pressure losses in the system.
The total propellant flow at the pump outlet is ____________ the flow in combustion chamber and the discharge pressure is __________ chamber pressure plus the other insignificant pressure losses in the system. Correct Answer equal to; equal to
Mass flow rate remains constant. Hence the total propellant flow will be the same for the pump outlet as well as in the combustion chamber. Favorable pressure difference should be present for the flow to take place. The chamber pressure will be different from the nozzle pressure, but the discharge pressure is kept to be the same as the chamber pressure.
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Feb 20, 2025