Equatorial Coriolis deflection in free fall ($x_E={\Omega }_E(2h{)}^{3/2}/(3\sqrt{g})$)

A body released from rest relative to Earth at the equator has unperturbed downward velocity $v_U=-gt$. The Coriolis acceleration in local Earth coordinates gives eastward acceleration $a_E=-2{\Omega }_E{v}_U=2{\Omega }_{E}gt$. Integration gives $x_E={\Omega }_{E}g{t}^3/3$ and impact time $t_f=\sqrt{2h/g}$, proving the title formula. This is first order in Earth's rotation, neglecting air resistance and the height dependence of the effective local gravitational acceleration. For a short fall at latitude $\phi$, its leading eastward term is multiplied by $\cos \phi$.