$A$ spaceship of mass $2 \times 10^4 \, kg$ is launched into a circular orbit close to the Earth's surface. The additional velocity to be imparted to the spaceship in the orbit to overcome the gravitational pull will be $......$ (given $g = 10 \, m/s^2$ and radius of Earth $R = 6400 \, km$).

  • A
    $11.2(\sqrt{2}-1) \, km/s$
  • B
    $7.9(\sqrt{2}-1) \, km/s$
  • C
    $8(\sqrt{2}-1) \, km/s$
  • D
    $7.4(\sqrt{2}-1) \, km/s$

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