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A satellite of earth is moving in a circular orbit. It is observed that at point B which is nearest to earth weight of astronaut of mass m is zero and at point A weight of astronaut is found to be n(mgDR) where D is width of satellite, R is radius of circular orbit and g is acceleration due to gravity at satellite. If R>>D, then n is

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A satellite of earth is moving in a circular orbit. It is observed that at point B which is nearest to earth weight of astronaut of mass m is zero and at point A weight of astronaut is found to be n(mgDR) where D is width of satellite, R is radius of circular orbit and g is acceleration due to gravity at satellite. If R>>D, then n is



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