Two satellites $P$ and $Q$ go round a planet in circular orbits having radii $3R$ and $R$ respectively. If the speed of satellite $P$ is $2V$,what will be the speed of satellite $Q$?

  • A
    $2 \sqrt{3} V$
  • B
    $\frac{2V}{\sqrt{3}}$
  • C
    $\frac{V}{2}$
  • D
    $\frac{V}{\sqrt{3}}$

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