1.

Energy required to move a body of mass m from an orbit of radius 2R to 3R isA. GMm/12RB. GMm/3RC. GMm/8RD. GMm/6R

Answer» Correct Answer - A
`TE=-(GMm)/(2r)`
`=(-GMm)/(2(3R))-((-GMm)/(2(2R)))=(GMm)/(12R)`


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