The additional kinetic energy to be prov...

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) gt R_(1))` is

`GmM (1/(R_(1)^(2))-1/(R_(2)^(2)))`

`GmM (1/(R_(1))-1/(R_(2)))`

`2GmM (1/(R_(1)) -1/(R_(2)))`

` 1/2 GmM (1/(R_(1))-1/(R_(2)))`

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