A satellite with kinetic energy ${E_k}$ is revolving round the earth in a circular orbit. How much more kinetic energy should be given to it so that it may just escape into outer space
${E_k}$
$2{E_k}$
$\frac{1}{2}{E_k}$
$3{E_k}$
A satellite with kinetic energy ${E_k}$ is revolving round the earth in a circular orbit. How much more kinetic energy should be given to it so that it may just escape into outer space
Binding energy = $-$ kinetic energy
And if this amount of energy $({E_k})$ given to satellite then it will escape into outer space
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