At a distance r from the Earth’s centre, the acceleration due to gravity is given by g(r)=g0(rR)2, where g0 is the surface value and R is the Earth’s radius.
(i) Starting from this relation, derive a general formula for the altitude h(>0) at which the acceleration due to gravity falls to a fraction k of the surface value, i.e.
g(R+h)=kg0,0<k<1.
(ii) Using your formula, calculate the altitude at which the gravitational acceleration equals g0/9.
(iii) A satellite is placed in a circular orbit at this altitude. Obtain an expression for its orbital speed in terms of G, M and r, and then compute the numerical value using G=6.67×10−11N m2/kg2, M=6.0×1024kg and R=6.4×106m.