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Q. A satellite is revolving round the earth. Its kinetic energy is , How much energy $E_k$ is required by the satellite such that it escapes out of the gravitation field of earth

Gravitation

Solution:

$\frac{ E _{ k _{\text {esape }}}}{ E _{ k _{\text {rerclutian }}}}=\frac{\frac{1}{2} mV _{ e }^{2}}{\frac{1}{2} mV _{0}^{2}}=\left(\frac{ V _{ e }}{ V _{0}}\right)^{2}=2$
$E _{\text {kescape }}= E _{ k _{\text {reralŮŠtism }}}(2)=2 E _{ k }$