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Question

A space vehicle of mass m is in a circular orbit of radius 2Re about the earth (me). What is the work done by an external agent to transfer it to an orbit of radius 4Re?

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Solution

Total energy T.E=Gmem2r

Work done W=T.EfT.Ei

So, W=Gmem8Re(Gmem4Re)

W=Gmem8Re

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