(a) Derive an expression for the speed required for a satellite to move in a circular…

PHYSICS · Subjective · CBSE · Physics · Gravitation · Gravitation

Problem

(a) Derive an expression for the speed required for a satellite to move in a circular orbit of radius R+hR + h around Earth in terms of gg, RR, and hh. (b) A low-Earth satellite is required to have an orbital speed of 6.0 km s−16.0\,\text{km\,s}^{-1}. Calculate the altitude hh (in kilometres) at which this is possible. Take R=6.4×103 kmR = 6.4\times10^{3}\,\text{km} and g=9.8 m s−2g = 9.8\,\text{m\,s}^{-2}.

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