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.
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. Correct Answer 12.95 kg/s
ṁo = ṁr/(r+1) So ṁo = 17*3.2/4.2 = 12.95 kg/s.