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Physics · GRAVITATION

हिन्दी

If the mean density of the Earth is \( \rho \), the time period of a satellite revolving in an orbit very close to the Earth's surface depends on \( \rho \) as:

  1. \( T_0 \propto \rho \)
  2. \( T_0 \propto \sqrt{\rho} \)
  3. \( T_0 \propto \rho^{-1} \)
  4. \( T_0 \propto \rho^{-1/2} \)

Correct answer · Option 4

\( T_0 \propto \rho^{-1/2} \)

Explanation

\( T_0 = 2\pi\sqrt{\frac{R_E}{g}} = 2\pi\sqrt{\frac{R_E}{G (\frac{4}{3}\pi R_E \rho)}} = \sqrt{\frac{3\pi}{G\rho}} \propto \rho^{-1/2} \).
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