A satellite is to be placed in a circular orbit so that the centripetal (orbital)…

PHYSICS · Single correct · CBSE · Physics · Gravitation · Gravitation

Problem

A satellite is to be placed in a circular orbit so that the centripetal (orbital) acceleration acting on it is 0.30 g0.30\,g, where g=9.8 m s−2g=9.8\,\text{m s}^{-2} at Earth’s surface. Estimate the altitude hh above Earth’s surface required for this mission. (Take Earth’s radius RE=6.4×106 mR_{\rm E}=6.4\times10^{6}\,\text{m}.) Choose the nearest value. (a) 1.6×106 m1.6\times10^{6}\,\text{m} (b) 5.3×106 m5.3\times10^{6}\,\text{m} (c) 3.2×106 m3.2\times10^{6}\,\text{m} (d) 1.2×107 m1.2\times10^{7}\,\text{m}

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