Question: A rocket files at 10.080 kmph with an effective jet velocity of 1400 m/s and the propellant flow rate of 5 kg/s. if the
A rocket files at 10.080 kmph with an effective jet velocity of 1400 m/s and the propellant flow rate of 5 kg/s. if the heat of reaction of the propellants is 6500 kj/kg of the propellent mixture, determine, a) Propulsion efficiency and propulsion power b) Engine output and thermal efficiency c) Overall efficiency
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