A rocket is launched from a pole of the Earth with velocity Vo where Vo is the orbital velocity of rotation near the surface of

Question

A rocket is launched from a pole of the Earth with velocity Vo where Vo is the orbital velocity of rotation near the surface of the Earth in such a way that it lands at the equator The rocket s time R of flight is T x K Where R Radius of earth g acc due to gravity at the g surface Find value of K

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