$A$ rocket of mass $M$ is launched vertically from the surface of the earth with an initial speed $V$. Assuming the radius of the earth to be $R$ and negligible air resistance,the maximum height attained by the rocket above the surface of the earth is

  • A
    $R / \left( \frac{gR}{2V^2} - 1 \right)$
  • B
    $R \left( \frac{gR}{2V^2} - 1 \right)$
  • C
    $R / \left( \frac{2gR}{V^2} - 1 \right)$
  • D
    $R \left( \frac{2gR}{V^2} - 1 \right)$

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