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What is the minimum energy required to launch a satellite of mass m from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 2R?A. `(2GmM)/(3R)`B. `(GmM)/(3R)`C. `(GmM)/(3R)`D. `(5GmM)/(6R)` |
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Answer» Correct Answer - D Required energy `-(GMm)/(R )=(-GMm)/(6R)` |
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