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Calculate the ratio of propellant mass to initial mass required to achieve a burnout velocity equal to the escape velocity from the earth.

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1. Consider a rocket with kerosene–oxygen as the combination. The ratio of initial weight before blastoff to the final weight at burnout is 5.5. Calculate the burnout velocity. 2. A rocket using as the combination has a specific impulse of 360 s. Calculate the ratio of propellant mass to initial mass required to achieve a burnout velocity equal to the escape velocity from the earth.


 

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