A spacecraft of mass m is launched radially outward from a planet of mass M and radius R. It leaves the planet’s surface with speed u and moves under gravity alone.
(i) Obtain an expression for the change in gravitational potential energy of the spacecraft when it travels from r1=2R to r2=4R measured from the planet’s centre.
(ii) Assuming no other forces act, determine the minimum initial speed umin at r1=2R required for the spacecraft to reach r2=4R with zero speed.
(iii) If the actual launch speed is 1.5umin, calculate the speed of the spacecraft when it reaches r2=4R.