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If ve and vo represent the escape velocity and orbital velocity of a satellite corresponding to a circular orbit of radius R respectively, then(A) ve = vo(B) \(\sqrt{2}\)vo = ve(C) ve = \(\frac{1}{\sqrt{2}}\)vo(D) ve and vo are not related |
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Answer» Correct option is: (B) \(\sqrt{2}\)vo = ve |
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