Calculate the flow rate of LOX to the combustion chamber in a LOX-H2 – McqOptions

MCQOPTIONS

1.	Calculate the flow rate of LOX to the combustion chamber in a LOX-H2 rocket engine if the total propellant flow rate is 17 kg/s and mixture ratio is 3.2.
A.	11.33 kg/s
B.	15.92 kg/s
C.	12.95 kg/s
D.	13.67 kg/s
Answer» D. 13.67 kg/s

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