All Figures

$\begin{figure} \par\includegraphics[width=7.1cm,bb=19 18 466 576]{8265fig1.eps}\end{figure}$ Figure 1: The transfers capable of producing the present orbits of the Uranian irregulars. A (B) is the square of the ratio of the satellite's speed just before (after) the impact to the escape velocity at the satellite's location just before (after) the impact. $e_{\rm 1m}$ ( $e_{\rm 2m}$ ) is the minimum eccentricity of the orbits before (after) collision. The full-black line A = Bdivides the upper region (the current orbits arise from inner orbits) and the lower region (the current orbits arise from outer orbits). The value of $e_{\max}$ tabulated in Table 2 is shown on the dashed line for comparation with $e_{\rm 2m}$ . Trinculo: empty downward triangles, Caliban: full circles, Sycorax: empty rhombus, Ferdinand: empty squares, Francisco: full downward triangles, Margaret: empty upward triangles, Prospero: full upward triangles, Setebos: empty hexagons, Stephano: empty circles.
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