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7.Gravitation
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The additional kinetic energy to be provided to a satellite of mass $m$ revolving around a planet of mass $M,$ to transfer it from a circular orbit of radius $R_1$ to another of radius $R_2\,(R_2 > R_1)$ is
A
$GMm$$\left( {\frac{1}{{{R_1}^2}} - \frac{1}{{{R_2}^2}}} \right)$
B
$\;{\rm{GMm}}\left( {\frac{1}{{{R_1}^{}}} - \frac{1}{{{R_2}^{}}}} \right)$
C
$\;2{\rm{GMm}}\left( {\frac{1}{{{R_1}^{}}} - \frac{1}{{{R_2}^{}}}} \right)$
D
$\frac{1}{2}{\rm{GMm}}\left( {\frac{1}{{{R_1}^{}}} - \frac{1}{{{R_2}^{}}}} \right)$
(AIPMT-2010) (AIIMS-2016)
Solution
$-\frac{GMm}{2R_1}+KE=-\frac{GMm}{2R_2}$
$KE=\frac{GMm}{2}\left[\frac{1}{R_1}-\frac{1}{R_2}\right]$
Standard 11
Physics
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