Suppose of the rockets initial mass m 0 that 50 kg is the mass of the fuel.

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Suppose of the rocket’s initial mass m0 that 50 kg is the mass of the fuel.

(a) What is the burnout time tb, or the time at which all the fuel is consumed?

(b) What is the velocity of the rocket at burnout?

(c) What is the height of the rocket at burnout?

(d) Why would you expect the rocket to attain an altitude higher than the number in part (b)?

(e) After burnout what is a mathematical model for the velocity of the rocket?

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