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Energy required to move a body of mass m from an orbit of radius 2R to 3R isA. `(GMm)/(12R)`B. `(GMm)/(3R^(2))`C. `(GMm)/(8R)`D. `(GMm)/(6R)` |
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Answer» Correct Answer - A `W=T.E_(2)-T.E_(1)=(GMm)/2(1/(r_(1))-1/(r_(2)))` |
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