A rocket designed to place small payloads into orbit is carried to an altitude
of 12.0 \(\mathrm{km}\) above sea level by a converted airliner. When the
airliner is flying in a straight line at a constant speed of 850 \(\mathrm{km}
/ \mathrm{h}\) , the rocket is dropped. After the drop, the airliner maintains
the same altitude and speed and continues to fly in a straight line. The
rocket falls for a brief time, after which its rocket motor turns on. Once its
rocket motor is on, the combined effects of thrust and gravity give the rocket
a constant acceleration of magnitude 3.00\(g\) directed at an angle of
\(30.0^{\circ}\) above the horizontal. For reasons of safety, the rocket should
be at least 1.00 \(\mathrm{km}\) in front of the airliner when it climbs the
airliner's altitude. Your job is to determine the minimum time that the rocket
must fall before its engine starts. You can ignore air resistance. Your answer
should include (i) a diagram showing the flight paths of both the rocket and
the airliner, labeled at several points with vectors for their velocities and
accelerations; (ii) an \(x-t\) graph showing the motions of both the rocket and
the airliner; and (iii) a \(y-t\) graph showing the motions of both the rocket
and the airliner. In the diagram and the graphs, indicate when the rocket is
dropped, when the rocket motor turns on, and when the rocket climbs through
the altitude of the airliner.