The Saturn \(V\) rocket, which was used to launch the Apollo spacecraft on their
way to the Moon, has an initial mass \(M_{0}=2.80 \cdot 10^{6} \mathrm{~kg}\)
and a final mass \(M_{1}=8.00 \cdot 10^{5} \mathrm{~kg}\)
and burns fuel at a constant rate for \(160 .\) s. The speed of the exhaust
relative to the rocket is about \(v=2700 . \mathrm{m} / \mathrm{s}\).
a) Find the upward acceleration of the rocket, as it lifts off the launch pad
(while its mass is the initial mass).
b) Find the upward acceleration of the rocket, just as it finishes burning its
fuel (when its mass is the final mass).
c) If the same rocket were fired in deep space, where there is negligible
gravitational force, what would be the net change in the speed of the rocket
during the time it was burning fuel?