Physics

Physics

Problem

A satellite of mass mm is in a circular orbit of radius RR around a planet of mass MM. How much additional energy must be supplied to move it to a new circular orbit of radius 3R3R? a) GMm6R\dfrac{GMm}{6R} b) GMm3R\dfrac{GMm}{3R} c) −GMm3R-\dfrac{GMm}{3R} d) 2GMm3R\dfrac{2GMm}{3R}

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