\begin{table}%T2
      \caption{Model calculations to find the minimum speed
      and maximum deviation of the ejected particle from the solar
      direction. The parent objects are moving on circular orbits
      (cf. Wehry \& Mann \cite{wema99}).}
         \label{tab1}
         %%\centerline
\par
{
            \begin{tabular}{ccccc}
            \hline
            \hline
            \noalign{\smallskip}
             $e_{0}$ & $q({\rm AU})$ & $\beta$ & $\gamma(^{\circ})$
             & $v({\rm {km}~{s^{-1}}})$ \\
             & & & $2.5~ {\rm AU}$ & $2.5~ {\rm AU}$ \\
            \noalign{\smallskip}
                        \hline
            \noalign{\smallskip}
            0 & 0.3 & 0.5 & 14 & 19 \\
              & 0.8 & 0.5 & 24 & 19 \\
            0.3 & 0.3 & 0.4 & 11 & 27 \\
                & 0.8 & 0.4 & 21 & 27 \\
            0.6 & 0.3 & 0.2 & 14 & 24 \\
                & 0.8 & 0.2 & 24 & 24 \\
            0.9 & 0.3 & 0.2 & 9 & 38 \\
                & 0.8 & 0.2 & 19 & 38 \\
            \noalign{\smallskip}
            \hline
       \end{tabular}}
\par
      \medskip
         $e_0$~~eccentricity of the parent body;     \\
         $q$~~perihelion distance;                \\
         $\gamma$~~angle between the direction of the Sun and
                           the particle velocity;             \\
         $v$~~heliocentric speed.
\end{table}