If due to air drag,the orbital radius of a satellite decreases from $R$ to $R - \Delta R$,where $\Delta R << R$,the expression for the change in orbital velocity $\Delta v$ is (mass of Earth is $M$):

  • A
    $\frac{\Delta R}{2} \sqrt{\frac{GM}{R^3}}$
  • B
    $\frac{-\Delta R}{2} \sqrt{\frac{GM}{R^3}}$
  • C
    $\Delta R \sqrt{\frac{GM}{R^3}}$
  • D
    $-\Delta R \sqrt{\frac{GM}{R^3}}$

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