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A satellite revolving round the earth in a circular orbit with orbital velocity `v_(0)`. It has kinetic energy E. The additional kinetic energy required to be given to it so that it esscapes from the earth isA. 4 EB. 3 EC. 2 ED. E

Answer» Correct Answer - d
`(E_(2))/(E_(1))=((1)/(2)mv_(e)^())/((1)/(2)mv_(e)^(2))=((2GM)/(R))/((GM)/(R))`
`(E_(1))/(E_(1))-1=2-1=1`
`E_(2)-E_(1)=E`
`DeltaE=E`


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