Question:

An artificial satellite of mass \(m\) revolves around a planet in a circular orbit of radius \(R\) under the influence of an attractive central force given by \[ F\propto R^{-5/2}. \] How do the orbital velocity \(V\) and time period \(T\) depend on the orbital radius \(R\)?

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If the central force varies as \[ F\propto R^{-n}, \] then from \[ \frac{mV^2}{R}=F \] we get \[ V\propto R^{\frac{1-n}{2}}. \] After finding \(V\), use \[ T=\frac{2\pi R}{V} \] to obtain the dependence of the time period.
Updated On: Jul 29, 2026
  • \[ V\propto R^{-3/4}, \qquad T\propto R^{7/4} \]
  • \[ V\propto R^{-5/4}, \qquad T\propto R^{3/2} \]
  • \[ V\propto R^{-1/2}, \qquad T\propto R^{5/4} \]
  • \[ V\propto R^{-3/4}, \qquad T\propto R^{-7/4} \]
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The Correct Option is A

Solution and Explanation

Concept: For circular motion, the central force provides the centripetal force. \[ F=\frac{mV^2}{R}. \] Given, \[ F\propto R^{-5/2}. \]

Step 1: Find the dependence of orbital velocity on \(R\). Using \[ \frac{mV^2}{R} \propto R^{-5/2}, \] we get \[ V^2 \propto R^{-5/2}\cdot R. \] \[ V^2 \propto R^{-3/2}. \] Therefore, \[ V \propto R^{-3/4}. \]

Step 2: Find the dependence of time period on \(R\). For circular motion, \[ T=\frac{2\pi R}{V}. \] Substituting \[ V\propto R^{-3/4}, \] \[ T \propto R^{1+\frac34}. \] \[ T \propto R^{7/4}. \]

Step 3: Choose the correct option. Thus, \[ V\propto R^{-3/4} \] and \[ T\propto R^{7/4}. \] Therefore, \[ \boxed{ V\propto R^{-3/4}, \qquad T\propto R^{7/4} } \] \[ \boxed{\text{Answer = (A)}} \]
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