A satellite orbiting the earth with speed v0. To make the satellite escape, what should be the minimum percentage increase in its velocity?
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A: (a) T = 2π √(Re+h)3/√(gRe2) (Re+h)3 = T2gRe2 / 4π2
A satellite orbiting the earth with speed v0. To make the satellite escape, what should be the minimum percentage increase in its velocity?
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