a rocket travels at 1400 m/s with exhaust velocity of 1.4 km/s, nozzle exit diameter of 50 cm and the gas density of 0.6 kg/m3, throat diameter of 0.28 cm and , what is the total mass flow rate of the propellants.

a rocket travels at 1400 m/s with exhaust velocity of 1.4 km/s, nozzle exit diameter of 50 cm and the gas density of 0.6 kg/m3, throat diameter of 0.28 cm and , what is the total mass flow rate of the propellants.

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a rocket travels at 1400 m/s with exhaust velocity of 1.4 km/s, nozzle exit diameter of 50 cm and the gas density of 0.6 kg/m³, throat diameter of 0.28 cm and , what is the total mass flow rate of the propellants.

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