7.Gravitation
medium

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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