Q114 / 150 · MHT CET 2022 (05 Aug Shift 1) · Physics

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

  • A
    $\sqrt{\mathrm{GMmr}}$
  • B
    $\sqrt{\mathrm{Mvr}}$
  • C
    $\sqrt{\mathrm{GMm}}$
  • Correct answer
    D
    $\sqrt{\mathrm{GMm}^2 \mathrm{r}}$

Solution

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, $\mathrm{L}=\mathrm{mvr}=\sqrt{\mathrm{GMm}^2 \mathrm{r}}$

Hence, the correct answer is option: 'D'.

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