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The Origin and Evolution of the Solar System

The Origin and Evolution of the Solar System

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18 <strong>The</strong> structure <strong>of</strong> <strong>the</strong> <strong>Solar</strong> <strong>System</strong>in colour, probably due to an undisturbed layer <strong>of</strong> dust from meteorites. <strong>The</strong>re arealso younger <strong>and</strong> brighter regions characterized by bundles <strong>of</strong> parallel grooves.<strong>The</strong> final Galilean satellite, Callisto, has a thick icy crust that is dark <strong>and</strong>shows a large number <strong>of</strong> impact features. <strong>The</strong>re is a very large ‘bulls-eye’ feature,Valhalla, in <strong>the</strong> form <strong>of</strong> a series <strong>of</strong> concentric rings. This is similar to <strong>the</strong> Orientalefeature on <strong>the</strong> Moon <strong>and</strong> is certainly due to a very large impact.Before Voyager I reached Jupiter in 1979 <strong>the</strong> ring system <strong>of</strong> Uranus had beendetected from Earth observation <strong>and</strong>, with two known ring systems, <strong>the</strong>re wasinterest in seeing if Jupiter also had a ring. A single thin ring was discovered—which <strong>the</strong>n raised <strong>the</strong> possibility that rings were a universal feature <strong>of</strong> major planets<strong>and</strong> that Neptune too would have rings.1.4.3 <strong>The</strong> Saturnian systemWith 18 members identified so far Saturn has <strong>the</strong> most heavily populated satellitesystem (table 1.6). Only Titan, slightly larger than Mercury, matches <strong>the</strong> Galileansbut four o<strong>the</strong>rs—Tethys, Dione, Rhea <strong>and</strong> Iapetus—have diameters greater than1000 km. <strong>The</strong> system has a number <strong>of</strong> striking commensurabilities (Roy 1977)with both Enceladus–Dione <strong>and</strong> Mimas–Tethys having mean motions in <strong>the</strong> ratio2:1. In addition <strong>the</strong> 4:3 ratio for Titan–Hyperion ensures that this pair have conjunctionsnear <strong>the</strong> aposaturnium (fur<strong>the</strong>st orbital point from Saturn) <strong>of</strong> Hyperion.<strong>The</strong> smallest separation <strong>of</strong> <strong>the</strong>se two bodies is thus about 400 000 km ra<strong>the</strong>r than<strong>the</strong> 100 000 km implied by a simple consideration <strong>of</strong> <strong>the</strong> sizes <strong>of</strong> <strong>the</strong> two orbitsSpacecraft discoveries <strong>of</strong> smaller satellites show a number <strong>of</strong> 1:1 commensurabilitieswhich are really examples <strong>of</strong> special solutions in <strong>the</strong> restricted threebodyproblem. It is well known that general solutions <strong>of</strong> <strong>the</strong> gravitational problem<strong>of</strong> Ò (¿) bodies do not exist. However, Lagrange (1736–1813) showed thatspecial configurations <strong>of</strong> three bodies do satisfy <strong>the</strong> equations <strong>of</strong> motion. <strong>The</strong>seinvolve collinear <strong>and</strong> equilateral triangular arrangements <strong>of</strong> <strong>the</strong> bodies, as illustratedin figure 1.9, in which two <strong>of</strong> <strong>the</strong> bodies are placed at <strong>the</strong> points A <strong>and</strong> B<strong>and</strong> <strong>the</strong> third (C) can occupy one <strong>of</strong> <strong>the</strong> five points, L ½ to L , known as <strong>the</strong> Lagrangepoints. <strong>The</strong> whole system must rotate about <strong>the</strong> centre <strong>of</strong> mass. Generally<strong>the</strong>se solutions are unstable <strong>and</strong> any small displacement will rapidly destroy <strong>the</strong>symmetry. Since no three-body system can properly be isolated from <strong>the</strong> perturbingeffects <strong>of</strong> o<strong>the</strong>r bodies, this suggests that <strong>the</strong> Lagrange solutions cannot beachieved in practice. In certain restricted conditions <strong>the</strong> triangular solutions arestable; <strong>the</strong>y require <strong>the</strong> third body, C, to be <strong>of</strong> negligible mass <strong>and</strong> for <strong>the</strong> ratio<strong>of</strong> <strong>the</strong> masses <strong>of</strong> A <strong>and</strong> B to exceed 25. In such cases small displacements <strong>of</strong>body C from L <strong>and</strong> L do not become unbounded <strong>and</strong>, <strong>of</strong> course, A <strong>and</strong> B executetwo-body motion. <strong>The</strong> conditions are satisfied by Saturn–Tethys–Calypso,Saturn–Tethys–Telesto <strong>and</strong> also by Saturn–Dione–Dione B. Effectively Calypso<strong>and</strong> Telesto move in <strong>the</strong> same orbit as Tethys (hence <strong>the</strong> 1:1 commensurability)but maintain a position on average ¼ Æ in front <strong>and</strong> ¼ Æ behind Tethys in its orbit.Saturn has a single very large satellite, Titan, which is very little below

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