Question
An artificial satellite revolves around a planet for which gravitational force $(F)$ varies with distance $r$ from its centre as $F \propto r^2$. If $v_0$ its orbital speed, then
Gravitational force $(F)$ provides the necessary centripetal force to keep the satellite in orbit,
$\Rightarrow \frac{m v_0^2}{r} \propto F$
$\frac{m v_0^2}{r} \propto r^2$
$v_0 \rightarrow \text { Orbital speed }$
$r \rightarrow \text { Radius of orbit }$
$\Rightarrow v_0 \propto r^{3 / 2}$
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$(1\;a.m.u = 931\;MeV)$