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MHT CET · Physics · Gravitation

A satellite of mas ' \(m\) ' is revolving around the earth of mass ' \(M\) ' in an orbit of radius ' \(r\) '. The angular momentum of the satellite about the centre of orbit will of

  1. A \(\sqrt{\mathrm{GMmr}}\)
  2. B \(\sqrt{\mathrm{Mvr}}\)
  3. C \(\sqrt{\mathrm{GMm}}\)
  4. D \(\sqrt{\mathrm{GMm}^2 \mathrm{r}}\)
Verified Solution

Answer & Solution

Correct Answer

(D) \(\sqrt{\mathrm{GMm}^2 \mathrm{r}}\)

Step-by-step Solution

Detailed explanation

The correct option is (D).
Considering force balance in the orbit:
\(\frac{\mathrm{GMm}}{\mathrm{r}^2}=\frac{\mathrm{mv}^2}{\mathrm{r}}\)
Gravitational force balances the centrifugal force. The orbital velocity can be obtained as:
\(v=\sqrt{\frac{G M}{r}}\)
Therefore, angular momentum is equal to,
\(\mathrm{L}=\mathrm{mvr}=\sqrt{\mathrm{GMm}^2 \mathrm{r}}\)