$A$ rocket is projected in the vertically upwards direction with a velocity $kv_e$,where $v_e$ is the escape velocity and $k < 1$. The distance from the centre of the Earth up to which the rocket will reach is:

  • A
    $R_e(1 - k^2)$
  • B
    $\frac{1 - k^2}{R_e}$
  • C
    $\sqrt{R_e}(1 - k^2)$
  • D
    $\frac{R_e}{1 - k^2}$

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