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Thrust of liquid oxygen - liquid hydrogen rocket engine is 300 kN. The O/F ratio used is 5. If the fuel mass flow rate is 12.5 kg/s, the specific impulse of the rocket motor in Ns/kg is
🗓 Dec 12, 2021
votes
Victoria
🌐 India
can anyone share the explanation, please?
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Christina
🌐 India
like it
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