Dynamics Solar System Explorers 05 How does the Sun affect objects in the Solar System? 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. Basic Newton F gravity on Earth = — G mEarth m2 _______________ r2 m2 (kg) r (m) Fgravity Sun 1.99e30 1.50e11 3.52e22 Venus 4.87e24 4.14e10 1.13e18 Moon 7.35e22 3.84e08 1.98e20 Jupiter 1.90e27 6.29e11 1.91e18 Winner! 178 X Moon What about the Moon? mEarth = 5.97e24 kg Earth-Moon has FEarth ~ 1.98e20, Sun-Moon has FSun ~ 4.34e20 Dynamics: Kepler I Kepler I: planetary orbits are ellipses with the Sun at a focus a (1 - e2) rSun = ______________ 1 + e cos f e, eccentricity = (1 - b2minor/a2major)1/2 f (or θ, or ν), true anomaly = angle between perihelion and current position Dynamics: Kepler I Kepler I: planetary orbits are ellipses with the Sun at a focus a (1 - e2) rSun = ______________ 1 + e cos f e, eccentricity = (1 - b2minor/a2major)1/2 f (or θ, or ν), true anomaly = angle between perihelion and current position Newton I : both bodies move along elliptical paths, with one focus of each ellipse located at the center of mass m1r1 + m2r2 rCM = _________________ M M = m1 + m2 Application: discovery of extrasolar planets Dynamics: Kepler II Kepler II: a line between a planet and the Sun sweeps out equal areas in equal times dA/dt = constant Newton II : a line connecting two bodies (or connecting one body to the center of mass position) sweeps out equal areas in equal times dL/dt = 0 (conservation of angular momentum) Application: spectroscopic binary orbits; prediction of planet locations Dynamics: Kepler III Kepler III: planetary orbital periods and distances from the Sun are directly (and simply) related as long as you assume SS units P2 (yr) = a3 (AU) Newton III: it also works outside of the Solar System 4π2a3 P2 = __________________ G (m1 + m2) a3 or Mtotal = _______ P2 solar masses, AU, yrs Application: stellar and planetary masses need fractional mass, f, for individual masses double dirty little secret of exoplanet masses … Orbital Elements a e i P T Ω ω semimajor axis eccentricity inclination (~0 in SS, edge on = 90 outside) orbital period epoch of periastron longitude of ascending node argument of periastron size shape tilt angle time a date spin angle tωist angle Spin: Longitude of Ascending Node Tωist: Longitude of Periastron Orbital Elements a e i P T Ω ω equinox f semimajor axis size eccentricity shape inclination tilt orbital period time epoch of periastron a date longitude of ascending node flip angle longitude of periastron twist angle equinox of date sets direction of equinox fractional mass a number Two observations will not yield an orbit. Why? Each point has (position X, position Y, time). There are 7 classical unknowns, so you need a third point to give you 9 pieces of data to solve equations. 1245 AC PushingGJ Towards Exoplanets 12 New Orbits in Solar System located 44.7 AU Psun ~ 300 yrs HST WFPC2 images V = 23.1 Porb a mtot at least 77 multiple TNOs known www2.lowell.edu/users/grundy/tnbs/status.html 590 ± 40 days 22400 ± 900 km 0.02% Pluto Reality Check: 3-body Systems theory: about 7:1 ratio in semimajor axis is critical point two well-defined sets of triples: Fekel’s spectroscopic triples SETI sample projected separations our Solar System is different … why? Counter-Intuitive Dynamics Lagrangian Points: where objects feel no net force in rotating frame; gravitational force of two masses cancels centrifugal force because of rotation 5 per two body system Trojan asteroids at Jupiter (>5000), Mars (6+), Neptune (7+) small moons at Sat/Tethys (Telesto+Calypso) and Sat/Dione (Helene+Polydeuces) Earth orbiting spacecraft WMAP SOHO Gaia JWST 15 Counter-Intuitive Dynamics Tadpole orbits: librating positions around L4 and L5 (note corotating frame!) Trojan asteroids at Jupiter, Mars, and Neptune Counter-Intuitive Dynamics Horseshoe orbits: orbit swapping due to particles passing in orbits, or in resonance with larger bodies (note corotating frame!) Janus and Epimetheus (Saturn) swap orbits every 4 years Cruithne and Asteroid 2002 AA29 around Earth 17 Counter-Intuitive Dynamics Horseshoe orbits: Cruithne --- each loop takes 1 yr http://www.astro.uwo.ca/%7Ewiegert/3753/3753.html 18 Counter-Intuitive Dynamics Horseshoe orbits: Asteroid 2002 AA29 --- each vertical loop takes 1 yr http://www.astro.uwo.ca/%7Ewiegert/AA29/AA29.html “at least three others” http://www.astro.uwo.ca/%7Ewiegert/3753/3753.htm 19 Counter-Intuitive Dynamics Chaotic motion: trajectories that begin arbitrarily close together will diverge exponentially with time (note that 4.6 Gyr is often not sufficient “time”) Mars’ axis tilt Hyperion rotation in Saturn-Titan tug-of-war Resonances: orbital periods with ratios A : B (both integers) Io : Europa : Ganymede (1 : 2.008 : 4.044) … oblate? tides? Neptune : Plutinos (3:2) Asteroids : Jupiter (lots) --- pumped up e leads to Kirkwood gaps Saturn ring particles : Saturn moons (Mimas, Atlas, …) Saturn’s Rings 300,000 km wide X 10 m (!) thick 21 particles forced into plane by orbits albedo 0.8 … shiny snowballs of H2O Saturn’s Rings total mass only that of small moon young … likely formed by Roche limit crossing 22 ………………………… Saturn’s Ring Structure 6 major regions … 2 divisions … 1000s of ringlets ABC rings seen from ground … major DEF rings seen from Voyager/Cassini … minor Cassini Division A ring Encke Gap F ring (braided) E ring spokes Mimas 2:1 resonance Atlas on edge (in 3:2 with Mimas) Pan within A ring shepherds Prometheus + Pandora Enceladus volcanism (outside Roche) collisions in rings 24 The Saturn System Saturn’s Rings Details 26 Jupiter’s Rings 27 Jupiter’s Rings Details 28 Jupiter’s Rings Details 29 Tides tides are a differential gravitational force ~ 1 / r3 a. cause bulk motions of fluid components ocean tides, moonquakes, Io volcanoes 2 reasons --- bulge amplitude changes, position of bulge changes b. cause torques (~1 / r6) that lead to rotational changes Earth day lengthening, Pluto-Charon locked, Mercury 3:2 spin:orbit resonance eccentric orbit…Mercury elongation…resonance c. cause shape changes if tidal force > tensile strength/self-gravity evidence for Moon’s shape --- closer in the past d. may create rings Tidal Forces 2 x G m2 F tidal ≈ ______________ r3 r is distance between two bodies x is distance along axis separating two bodies (surface = body’s radius) tides on Earth m2 (kg) r (km) Ftidal/2RG Sun 1.99e30 1.50e08 5.90e05 Venus 4.87e24 4.14e07 6.86e01 Moon 7.35e22 3.84e05 1.30e06 Jupiter 1.90e27 6.29e08 7.63e00 Winner! 2.2 X Sun Earth-Moon tidal force is 81 X Moon-Earth tidal force Jupiter-Io tidal force is 20,000 X Moon-Earth tidal force Tides in Earth-Moon System angular momentum is conserved, but … can be swapped between rotation and revolution via tidal torques on Earth: twice per 25 hours due to Moon twice per 24 hours due to Sun (1/2 strength) on Moon: mostly fixed because of synchronous rotation but not entirely because of eccentricity … nutation bulge torque: Earth rotates faster than Moon orbits Earth not perfectly elastic, so bulge not on Earth-Moon line Moon pulls back on bulge --- Earth slows down Earth bulges pull on Moon --- torque acc. Moon outward ~ 1/r6 death spirals: moons moving retrograde, or faster than planet rotates Moon’s Shape bulge frozen at 2/3 current Moon distance Roche Limit Roche limit: point beyond which an object is ripped apart by tidal forces aRoche = 2.456 Rp (ρp/ρs)1/3 moons inside Roche limit !?!?! Jupiter has 3 + Saturn has ~ 0 Uranus has 8 + Neptune has 4 + (1) assumes fully deformable (fluid) moon (2) assumes no “tensile strength” … resulting orbital systems have … … large moons … small moons … ring particles Roche Limits and Ring Systems 35 Neptune’s Rings Adams Lassell LeVerrier Galle Billions of Years from Now… Solar System Explorers 04 How does the Sun affect objects in the Solar System? 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. …………………………