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.

Related Questions

Complete the equation. 2Res+OH– + 2– → __________ + 2OH– 2- b) (Res+)23- c) (Res+)22- d) (Res+)32-
Neha was solving a problem in which subtraction of 673–257 was required. She said, "257 plus 100 will be 357, 457, 557, 657. So, 257 plus 400 is 657". "Now 657 plus 10 is 667, 677, so, 657 plus 20 is 677 and 4 less in 677 is 673. "Therefore, 400 plus 20 minus 4 is 416". Hence 673–257 is 416. Which of the following statements is most appropriate for the strategy of Neha?