A satellite of mass m is required to be shifted from an initial circular orbit of radius r1 about a planet of mass M to a higher circular orbit of radius r2 (r2>r1).
(a) Derive an expression for the work that must be done on the satellite to accomplish this transfer, expressing your answer in terms of G, M, m, r1 and r2.
(b) Using the derived expression, calculate the work needed to move a 200kg satellite from an orbit of radius 8.0×106m to an orbit of radius 1.2×107m around Earth, taking G=6.67×10−11N m2kg−2 and M⊕=6.0×1024kg.
(c) Based on your calculation, comment on whether the required work is more sensitive to the initial or to the final orbital radius.