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NEET UG PHYSICS MCQ: GRAVITATION

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If ve and vo{v_e}\,and\,{v_o} represent escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R, then
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Correct option: B
2vo=ve\sqrt 2 {v_o} = {v_e}
Option B (2vo=ve\sqrt 2 {v_o} = {v_e}) is correct because the escape velocity is 2\sqrt{2} times the orbital velocity.

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