If vₑ and v₀ represent the escape velocity and orbital
velocity of a satellite corresponding to a circular orbit of
radius R, then
(a) vₑ = v₀ (b) vₑ = 2 v₀
(c) vₑ = (1/ √2) v₀ (d) vₑ and v₀ are not related
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Explanation:
(c) is the correct answer.
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