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The additional kinetic energy to be provided to a satellite of mass `m` revolving around a planet of mass `M`, to transfer it forms a circular orbit of radius `R_(1)` to another of radius `R_(2)(R_(2)gtR_(1))` isA. `GmM (1/R_(1)-1/R_(2))`B. `2 Gm M (1/R_(1) - 1/R_(2))`C. `1/2 GmM (1/R_(1)-1/R_(2))`D. `GmM(1/R_(1)^(2)-1/R_(2)^(2))` |
Answer» Correct Answer - C | |