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TS EAMCET · Physics · Gravitation

A satellite is revolving very close to a planet of density \(\rho\). The period of revolution of satellite is

  1. A \(\sqrt{\frac{3 \pi \rho}{G}}\)
  2. B \(\sqrt{\frac{3 \pi}{2 \rho G}}\)
  3. C \(\sqrt{\frac{3 \pi}{\rho G}}\)
  4. D \(\sqrt{\frac{3 \pi G}{\rho}}\)
Verified Solution

Answer & Solution

Correct Answer

(C) \(\sqrt{\frac{3 \pi}{\rho G}}\)

Step-by-step Solution

Detailed explanation

We know that, Period of revolution Let, \(T\) be the time of one revolution of the satellite. Then,…
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