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JEE PHYSICS MCQ: GRAVITATION

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If vov_o be the orbital velocity of a satellite in a circular orbit close to the earth's surface and vev_e is the escape velocity from the earth, then relation between the two is
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Correct option: C
ve=2vov_e=\sqrt{2} v_o
Option C (ve=2vov_e=\sqrt{2} v_o) is correct because the escape velocity is 2\sqrt{2} times the orbital velocity near the Earth's surface.

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