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7.Gravitation
normal
In a satellite if the time of revolution is $T$, then $P E$ is proportional to ..........
A
$T^{1 / 3}$
B
$T^3$
C
$T^{-2 / 3}$
D
$T^{-4 / 3}$
Solution
(c)
According to Kepler's third law,
$T^2 \propto r^3$
$r=$ radius of orbit
For a satellite of mass $m$ orbiting in an orbit of radius $r$ around planet of mass $M$,
Potential energy $( PE )=\frac{-G M m}{r}$
$\Rightarrow PE \propto \frac{G M m}{T^{2 / 3}}$
$\Rightarrow P E \propto T^{-2 / 3}$
Standard 11
Physics