1.

The `K.E.` of a satellite in an orbit close to the surface of the earth is `E`. Its max `K.E.` so as to escape from the gravitational field of the earth isA. `2E`B. `4E`C. `2sqrt(2)`D. `sqrt(2)E`

Answer» Correct Answer - A
`(K_(e))/(K_(o))=(2gR)/(gR)rArr K_(e)=2K_(0)`


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