Evolution of Icy Satellites

Total Page:16

File Type:pdf, Size:1020Kb

Evolution of Icy Satellites Space Sci Rev DOI 10.1007/s11214-010-9635-1 Evolution of Icy Satellites G. Schubert · H. Hussmann · V. L a i n e y · D.L. Matson · W.B. McKinnon · F. Sohl · C. Sotin · G. Tobie · D. Turrini · T. Van Hoolst Received: 10 July 2009 / Accepted: 8 February 2010 © The Author(s) 2010 Abstract Evolutionary scenarios for the major satellites of Jupiter, Saturn, Neptune, and Pluto-Charon are discussed. In the Jovian system the challenge is to understand how the G. Schubert () Department of Earth and Space Sciences and Institute of Geophysics and Planetary Physics, University of California, Los Angeles, CA 90095, USA e-mail: [email protected] H. Hussmann · F. Sohl German Aerospace Center (DLR), Institute of Planetary Research, 12489 Berlin, Germany H. Hussmann e-mail: [email protected] F. Sohl e-mail: [email protected] V. Lainey IMCCE-Observatoire de Paris, UMR 8028 du CNRS, 77 Avenue Denfert-Rochereau, 75014 Paris, France e-mail: [email protected] D.L. Matson JPL 183-335, 4800 Oak Grove Drive, Pasadena, CA 91109, USA e-mail: [email protected] W.B. McKinnon Department of Earth and Planetary Sciences and McDonnell Center for the Space Sciences, Washington University, One Brookings Drive, Saint Louis, MO 63130, USA e-mail: [email protected] C. Sotin JPL/Caltech, 4800 Oak Grove Drive, Pasadena, CA 91109, USA e-mail: [email protected] G. Tobie University of Nante, Nantes, France e-mail: [email protected] G. Schubert et al. present Laplace resonance of Io, Europa, and Ganymede was established and to determine whether the heat being radiated by Io is in balance with the present tidal dissipation in the moon. In the Saturnian system, Enceladus and Titan are the centers of attention. Tidal heating is the likely source of activity at the south pole of Enceladus, although the details of how the heating occurs are not understood. An evolutionary scenario based on accretion and internal differentiation is presented for Titan, whose present substantial orbital eccentricity is not associated with any dynamical resonance. The source and maintenance of methane in Titan’s present atmosphere remain uncertain. Though most attention on the Saturnian moons focuses on Titan and Enceladus, the mid-size satellites Iapetus, Rhea, Tethys, and the irregular satellite Phoebe also draw our interest. An evolutionary scenario for Iapetus is presented in which spin down from an early rapidly rotating state is called upon to explain the satellite’s present oblate shape. The prominent equatorial ridge on Iapetus is unexplained by the spin down scenario. A buckling instability provides another possible explanation for the oblateness and equatorial ridge of Iapetus. Rhea is the only medium-size Saturnian satellite for which there are gravity data at present. The interpretation of these data are uncertain, however, since it is not known if Rhea is in hydrostatic equilibrium. Pluto and Charon are representative of the icy dwarf planets of the Kuiper belt. Did they differentiate as they evolved, and do either of them have a subsurface liquid water ocean? New Horizons might provide some answers when it arrives at these bodies. Keywords Outer planet moons · Io · Europa · Enceladus · Dione · Titan · Iapetus · Rhea · Tethys · Phoebe · Pluto · Charon · Satellite evolution 1 Introduction The satellites of the outer planets provide important clues about the formation and evolution of the solar system as a whole. In this chapter we discuss the evolution of the major satellites of Jupiter, Saturn and Neptune. Pluto and Charon are also included since they represent the same population of objects as Neptune’s captured moon Triton. The outer planet moons are striking in their diversity and evolutionary paths. They have experienced physical processes that are unfamiliar in the bodies of the inner solar system, and, accordingly, they comprise a fascinating collection of objects for study. 2 Satellites in Resonance: Strong Thermal/Orbital-Dynamical Coupling Resonances can play an important role in the evolution of satellites. Orbital periods of satel- lites in resonance are commensurable and their mutual gravitational perturbations at con- junction (where perturbations are near maximum) occur periodically at the same orbital phase. Perturbations to the satellites’ orbital evolution are therefore significantly stronger D. Turrini INAF-IFSI, Via del Fosso del Cavaliere 100, 00133 Rome, Italy e-mail: [email protected] T. Van Hoolst Royal Observatory of Belgium, Avenue Circulaire 3, Uccle, 1180 Brussels, Belgium e-mail: [email protected] Evolution of Icy Satellites Fig. 1 Two examples of resonances in the outer solar system involving internal heating of satellites. Rota- tional energy of the primary planet and angular momentum are transferred to the innermost satellite due to tidal torques. Because of the resonance coupling, energy and angular momentum are distributed among the satellites locked in resonance. Part of the energy is dissipated as heat in the satellites’ interiors due to tidal flexing. This affects mainly the inner satellites close to the primary, in the first case Io and, to a lesser extent, Europa, and in the second example Enceladus (sizes and distances not to scale) compared with the non-resonant (stochastic) case (see Greenberg 1982 and Peale 1986 for a general description). The main implication for the evolution of satellites is that the orbital eccentricities are forced and maintained as long as a resonance is stable, i.e., on geological timescales if the coupling is strong. Because the global tidal heating rate (due to tidal inter- action with the primary) depends on the eccentricity squared, long-term internal heat pro- duction is strongly linked to the occurrence of resonances. In some cases when the primary is close—for instance, Io and Jupiter—this type of tidal heating can significantly exceed the heat production due to radiogenic heating. In addition to the high eccentricities associated with stable resonant equilibrium configurations, orbital eccentricities can vary considerably when the satellites pass through resonances or when oscillatory states (strongly varying orbital and thermal states) occur. Oscillatory behavior results from the disequilibrium of ec- centricity forcing in a resonance and involves eccentricity damping due to tidal dissipation in the satellite. Mean motion resonances and tidal heating play an important role in the Jupiter system, mainly for Io and Europa, and in the Saturn system in the case of Enceladus (Fig. 1). Both examples are discussed below. G. Schubert et al. 2.1 Io, Europa, Ganymede 2.1.1 The Laplace Resonance The three inner Galilean satellites are locked in various resonances. For the thermal-orbital evolution the 2:1 Io–Europa mean-motion resonance and the 2:1 Europa–Ganymede mean- motion resonance are the most important ones. Conjunctions of Io and Europa are locked to Io’s perijove (resonance angle librating about 0°) and to Europa’s apojove (resonance angle librating about 180°). Conjunctions of Europa and Ganymede are locked to Europa’s peri- jove (resonance angle librating about 0°) but to neither apsis of Ganymede (resonance angle circulating through 360°). The combination of the two 2:1 resonances yields the libration of the Laplace angle l1 − 3l2 + 2l3 about 180°. The li (i = 1, 2, 3) are the mean longitudes of Io, Europa, and Ganymede, respectively. This implies that whenever Europa and Ganymede are in conjunction, Io is on the opposite side of Jupiter. The Laplace configuration is stable and, after differentiating the mean longitudes with respect to time dli /dt = ni , is usually expressed by n1 − 3n2 + 2n3 = 0(1) where the ni are the mean motions of Io, Europa and Ganymede, respectively. This three- body coupling is called the Laplace resonance, named after Pierre Simon de Laplace, who first demonstrated the stability of the orbital commensurabilities on theoretical grounds. Detailed reviews of the dynamics of the Galilean satellite system are given by Greenberg (1982) and Peale (1986). The forced eccentricities associated with the above mentioned 2:1 resonances are 0.0041, 0.0101 and 0.0006 for Io, Europa and Ganymede, respectively. In the case of Europa the ec- centricity is forced by both the 2:1 resonance with its inner neighbor Io and the 2:1 resonance with its outer neighbor Ganymede. Whereas the free eccentricities are negligible for Io and Europa (order of 10−5), the free eccentricity of 0.0015 is the major contribution to the ec- centricity of Ganymede. The free eccentricity is the remnant of the initial eccentricity after satellite formation (or after an unusual event, e.g., a major impact or a former resonance passage), which decreases with time due to tidal dissipation in the satellite. However, Show- man and Malhotra (1997) have shown that an impactor capable of creating Ganymede’s free eccentricity would have to have had a mass 102 to 103 times greater than the mass of the impactor that formed Gilgamesh, the largest impact basin on Ganymede. The free ec- centricity is not associated with any resonance and can be regarded as the eccentricity that would persist if all the other satellites in the system were removed. Because of their forced eccentricities and their vicinity to Jupiter, Io and Europa are tidally heated on geological timescales up to the present. 2.1.2 Origin and Evolution of the Laplace Resonance At present it is unclear how the three-body resonance has formed. There are two conceivable scenarios: (a) a primordial origin by migration of the newly formed satellites due to inter- actions with the circumjovian disk (Peale and Lee 2002) and (b) a subsequent formation of the resonances by differential expansion of the orbits due to tidal torques from Jupiter (Yoder 1979; Yoder and Peale 1981). The latter is the ‘classical scenario’ in which Io spirals outwards more rapidly than Europa because Io is closer to Jupiter and experiences larger tidal torques.
Recommended publications
  • Cassini Update
    Cassini Update Dr. Linda Spilker Cassini Project Scientist Outer Planets Assessment Group 22 February 2017 Sols%ce Mission Inclina%on Profile equator Saturn wrt Inclination 22 February 2017 LJS-3 Year 3 Key Flybys Since Aug. 2016 OPAG T124 – Titan flyby (1584 km) • November 13, 2016 • LAST Radio Science flyby • One of only two (cf. T106) ideal bistatic observations capturing Titan’s Northern Seas • First and only bistatic observation of Punga Mare • Western Kraken Mare not explored by RSS before T125 – Titan flyby (3158 km) • November 29, 2016 • LAST Optical Remote Sensing targeted flyby • VIMS high-resolution map of the North Pole looking for variations at and around the seas and lakes. • CIRS last opportunity for vertical profile determination of gases (e.g. water, aerosols) • UVIS limb viewing opportunity at the highest spatial resolution available outside of occultations 22 February 2017 4 Interior of Hexagon Turning “Less Blue” • Bluish to golden haze results from increased production of photochemical hazes as north pole approaches summer solstice. • Hexagon acts as a barrier that prevents haze particles outside hexagon from migrating inward. • 5 Refracting Atmosphere Saturn's• 22unlit February rings appear 2017 to bend as they pass behind the planet’s darkened limb due• 6 to refraction by Saturn's upper atmosphere. (Resolution 5 km/pixel) Dione Harbors A Subsurface Ocean Researchers at the Royal Observatory of Belgium reanalyzed Cassini RSS gravity data• 7 of Dione and predict a crust 100 km thick with a global ocean 10’s of km deep. Titan’s Summer Clouds Pose a Mystery Why would clouds on Titan be visible in VIMS images, but not in ISS images? ISS ISS VIMS High, thin cirrus clouds that are optically thicker than Titan’s atmospheric haze at longer VIMS wavelengths,• 22 February but optically 2017 thinner than the haze at shorter ISS wavelengths, could be• 8 detected by VIMS while simultaneously lost in the haze to ISS.
    [Show full text]
  • Copyrighted Material
    Index Abulfeda crater chain (Moon), 97 Aphrodite Terra (Venus), 142, 143, 144, 145, 146 Acheron Fossae (Mars), 165 Apohele asteroids, 353–354 Achilles asteroids, 351 Apollinaris Patera (Mars), 168 achondrite meteorites, 360 Apollo asteroids, 346, 353, 354, 361, 371 Acidalia Planitia (Mars), 164 Apollo program, 86, 96, 97, 101, 102, 108–109, 110, 361 Adams, John Couch, 298 Apollo 8, 96 Adonis, 371 Apollo 11, 94, 110 Adrastea, 238, 241 Apollo 12, 96, 110 Aegaeon, 263 Apollo 14, 93, 110 Africa, 63, 73, 143 Apollo 15, 100, 103, 104, 110 Akatsuki spacecraft (see Venus Climate Orbiter) Apollo 16, 59, 96, 102, 103, 110 Akna Montes (Venus), 142 Apollo 17, 95, 99, 100, 102, 103, 110 Alabama, 62 Apollodorus crater (Mercury), 127 Alba Patera (Mars), 167 Apollo Lunar Surface Experiments Package (ALSEP), 110 Aldrin, Edwin (Buzz), 94 Apophis, 354, 355 Alexandria, 69 Appalachian mountains (Earth), 74, 270 Alfvén, Hannes, 35 Aqua, 56 Alfvén waves, 35–36, 43, 49 Arabia Terra (Mars), 177, 191, 200 Algeria, 358 arachnoids (see Venus) ALH 84001, 201, 204–205 Archimedes crater (Moon), 93, 106 Allan Hills, 109, 201 Arctic, 62, 67, 84, 186, 229 Allende meteorite, 359, 360 Arden Corona (Miranda), 291 Allen Telescope Array, 409 Arecibo Observatory, 114, 144, 341, 379, 380, 408, 409 Alpha Regio (Venus), 144, 148, 149 Ares Vallis (Mars), 179, 180, 199 Alphonsus crater (Moon), 99, 102 Argentina, 408 Alps (Moon), 93 Argyre Basin (Mars), 161, 162, 163, 166, 186 Amalthea, 236–237, 238, 239, 241 Ariadaeus Rille (Moon), 100, 102 Amazonis Planitia (Mars), 161 COPYRIGHTED
    [Show full text]
  • A Deeper Look at the Colors of the Saturnian Irregular Satellites Arxiv
    A deeper look at the colors of the Saturnian irregular satellites Tommy Grav Harvard-Smithsonian Center for Astrophysics, MS51, 60 Garden St., Cambridge, MA02138 and Instiute for Astronomy, University of Hawaii, 2680 Woodlawn Dr., Honolulu, HI86822 [email protected] James Bauer Jet Propulsion Laboratory, California Institute of Technology 4800 Oak Grove Dr., MS183-501, Pasadena, CA91109 [email protected] September 13, 2018 arXiv:astro-ph/0611590v2 8 Mar 2007 Manuscript: 36 pages, with 11 figures and 5 tables. 1 Proposed running head: Colors of Saturnian irregular satellites Corresponding author: Tommy Grav MS51, 60 Garden St. Cambridge, MA02138 USA Phone: (617) 384-7689 Fax: (617) 495-7093 Email: [email protected] 2 Abstract We have performed broadband color photometry of the twelve brightest irregular satellites of Saturn with the goal of understanding their surface composition, as well as their physical relationship. We find that the satellites have a wide variety of different surface colors, from the negative spectral slopes of the two retrograde satellites S IX Phoebe (S0 = −2:5 ± 0:4) and S XXV Mundilfari (S0 = −5:0 ± 1:9) to the fairly red slope of S XXII Ijiraq (S0 = 19:5 ± 0:9). We further find that there exist a correlation between dynamical families and spectral slope, with the prograde clusters, the Gallic and Inuit, showing tight clustering in colors among most of their members. The retrograde objects are dynamically and physically more dispersed, but some internal structure is apparent. Keywords: Irregular satellites; Photometry, Satellites, Surfaces; Saturn, Satellites. 3 1 Introduction The satellites of Saturn can be divided into two distinct groups, the regular and irregular, based on their orbital characteristics.
    [Show full text]
  • Exomoon Habitability Constrained by Illumination and Tidal Heating
    submitted to Astrobiology: April 6, 2012 accepted by Astrobiology: September 8, 2012 published in Astrobiology: January 24, 2013 this updated draft: October 30, 2013 doi:10.1089/ast.2012.0859 Exomoon habitability constrained by illumination and tidal heating René HellerI , Rory BarnesII,III I Leibniz-Institute for Astrophysics Potsdam (AIP), An der Sternwarte 16, 14482 Potsdam, Germany, [email protected] II Astronomy Department, University of Washington, Box 951580, Seattle, WA 98195, [email protected] III NASA Astrobiology Institute – Virtual Planetary Laboratory Lead Team, USA Abstract The detection of moons orbiting extrasolar planets (“exomoons”) has now become feasible. Once they are discovered in the circumstellar habitable zone, questions about their habitability will emerge. Exomoons are likely to be tidally locked to their planet and hence experience days much shorter than their orbital period around the star and have seasons, all of which works in favor of habitability. These satellites can receive more illumination per area than their host planets, as the planet reflects stellar light and emits thermal photons. On the contrary, eclipses can significantly alter local climates on exomoons by reducing stellar illumination. In addition to radiative heating, tidal heating can be very large on exomoons, possibly even large enough for sterilization. We identify combinations of physical and orbital parameters for which radiative and tidal heating are strong enough to trigger a runaway greenhouse. By analogy with the circumstellar habitable zone, these constraints define a circumplanetary “habitable edge”. We apply our model to hypothetical moons around the recently discovered exoplanet Kepler-22b and the giant planet candidate KOI211.01 and describe, for the first time, the orbits of habitable exomoons.
    [Show full text]
  • Chemical Composition of Pluto's Aerosols Analogues
    EPSC Abstracts Vol. 13, EPSC-DPS2019-941-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Chemical composition of Pluto’s aerosols analogues Lora Jovanovic (1), Thomas Gautier (1), Nathalie Carrasco (1), Véronique Vuitton (2), Cédric Wolters (2), François-Régis Orthous-Daunay (2), Ludovic Vettier (1), Laurène Flandinet (2) ([email protected]) (1) Laboratoire Atmosphères, Milieux, Observations Spatiales (LATMOS), Guyancourt, France (2) Institut de Planétologie et d’Astrophysique de Grenoble (IPAG), Grenoble, France Abstract Table 1: Types of Pluto’s aerosols analogues produced with the PAMPRE experiment. The discovery of haze in Pluto’s atmosphere on July 14th, 2015, has raised lots of questions. To help Corresponding understand the data provided by the New Horizons Composition of the gas mixture altitude on spacecraft, Pluto’s aerosols analogues were Pluto [2] synthetized and their chemical composition was 99% N2 : 1% CH4 : 500 ppm CO 400 km determined by high-resolution mass spectrometry 95% N2 : 5% CH4 : 500 ppm CO 600 km (Orbitrap technique). 2.2. High-resolution mass spectrometry 1. Introduction (HRMS) study On July 14th, 2015, when Pluto was flown by the New Horizons spacecraft, aerosols were detected in its We analyzed the soluble fraction of Pluto’s aerosols atmosphere, mainly composed of molecular nitrogen analogues, dissolved in a 50:50 (v/v)% methanol:acetonitrile mixture. The analytical N2, methane CH4, with around 500 ppm of carbon monoxide CO [1,2,3]. These aerosols aggregate into instrument used was the LTQ Orbitrap XL several thin haze layers that extend at more than (ThermoFisher Scientific).
    [Show full text]
  • The Subsurface Habitability of Small, Icy Exomoons J
    A&A 636, A50 (2020) Astronomy https://doi.org/10.1051/0004-6361/201937035 & © ESO 2020 Astrophysics The subsurface habitability of small, icy exomoons J. N. K. Y. Tjoa1,?, M. Mueller1,2,3, and F. F. S. van der Tak1,2 1 Kapteyn Astronomical Institute, University of Groningen, Landleven 12, 9747 AD Groningen, The Netherlands e-mail: [email protected] 2 SRON Netherlands Institute for Space Research, Landleven 12, 9747 AD Groningen, The Netherlands 3 Leiden Observatory, Leiden University, Niels Bohrweg 2, 2300 RA Leiden, The Netherlands Received 1 November 2019 / Accepted 8 March 2020 ABSTRACT Context. Assuming our Solar System as typical, exomoons may outnumber exoplanets. If their habitability fraction is similar, they would thus constitute the largest portion of habitable real estate in the Universe. Icy moons in our Solar System, such as Europa and Enceladus, have already been shown to possess liquid water, a prerequisite for life on Earth. Aims. We intend to investigate under what thermal and orbital circumstances small, icy moons may sustain subsurface oceans and thus be “subsurface habitable”. We pay specific attention to tidal heating, which may keep a moon liquid far beyond the conservative habitable zone. Methods. We made use of a phenomenological approach to tidal heating. We computed the orbit averaged flux from both stellar and planetary (both thermal and reflected stellar) illumination. We then calculated subsurface temperatures depending on illumination and thermal conduction to the surface through the ice shell and an insulating layer of regolith. We adopted a conduction only model, ignoring volcanism and ice shell convection as an outlet for internal heat.
    [Show full text]
  • Small Satellite Missions
    Distr. LIMITED A/CONF.184/BP/9 26 May 1998 ORIGINAL: ENGLISH SMALL SATELLITE MISSIONS Background paper 9 The full list of the background papers: 1. The Earth and its environment in space 2. Disaster prediction, warning and mitigation 3. Management of Earth resources 4. Satellite navigation and location systems 5. Space communications and applications 6. Basic space science and microgravity research and their benefits 7. Commercial aspects of space exploration, including spin-off benefits 8. Information systems for research and applications 9. Small satellite missions 10. Education and training in space science and technology 11. Economic and societal benefits 12. Promotion of international cooperation V.98-53862 (E) A/CONF.184/BP/9 Page 2 CONTENTS Paragraphs Page PREFACE ........................................................................... 2 SUMMARY ......................................................................... 4 I. PHILOSOPHY OF SMALL SATELLITES ................................. 1-12 5 II. COMPLEMENTARITY OF LARGE AND SMALL SATELLITE MISSIONS .... 13-17 7 III. SCOPE OF SMALL SATELLITE APPLICATIONS ......................... 18-43 8 A. Telecommunications ................................................ 19-25 8 B. Earth observations (remote sensing) .................................... 26-31 9 C. Scientific research .................................................. 32-37 10 D. Technology demonstrations .......................................... 38-39 11 E. Academic training .................................................
    [Show full text]
  • + New Horizons
    Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16
    [Show full text]
  • Search for Rings and Satellites Around the Exoplanet Corot-9B Using Spitzer Photometry A
    Search for rings and satellites around the exoplanet CoRoT-9b using Spitzer photometry A. Lecavelier Etangs, G. Hebrard, S. Blandin, J. Cassier, H. J. Deeg, A. S. Bonomo, F. Bouchy, J. -m. Desert, D. Ehrenreich, M. Deleuil, et al. To cite this version: A. Lecavelier Etangs, G. Hebrard, S. Blandin, J. Cassier, H. J. Deeg, et al.. Search for rings and satellites around the exoplanet CoRoT-9b using Spitzer photometry. Astronomy and Astrophysics - A&A, EDP Sciences, 2017, 603, pp.A115. 10.1051/0004-6361/201730554. hal-01678524 HAL Id: hal-01678524 https://hal.archives-ouvertes.fr/hal-01678524 Submitted on 16 Jan 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. A&A 603, A115 (2017) Astronomy DOI: 10.1051/0004-6361/201730554 & c ESO 2017 Astrophysics Search for rings and satellites around the exoplanet CoRoT-9b using Spitzer photometry A. Lecavelier des Etangs1, G. Hébrard1; 2, S. Blandin1, J. Cassier1, H. J. Deeg3; 4, A. S. Bonomo5, F. Bouchy6, J.-M. Désert7, D. Ehrenreich6, M. Deleuil8, R. F. Díaz9; 10, C. Moutou11, and A. Vidal-Madjar1 1 Institut d’astrophysique de Paris, CNRS, UMR 7095 & Sorbonne Universités, UPMC Paris 6, 98bis Bd Arago, 75014 Paris, France e-mail: [email protected] 2 Observatoire de Haute-Provence, CNRS/OAMP, 04870 Saint-Michel-l’Observatoire, France 3 Instituto de Astrofísica de Canarias, 38205 La Laguna, Tenerife, Spain 4 Universidad de La Laguna, Dept.
    [Show full text]
  • 1 the Atmosphere of Pluto As Observed by New Horizons G
    The Atmosphere of Pluto as Observed by New Horizons G. Randall Gladstone,1,2* S. Alan Stern,3 Kimberly Ennico,4 Catherine B. Olkin,3 Harold A. Weaver,5 Leslie A. Young,3 Michael E. Summers,6 Darrell F. Strobel,7 David P. Hinson,8 Joshua A. Kammer,3 Alex H. Parker,3 Andrew J. Steffl,3 Ivan R. Linscott,9 Joel Wm. Parker,3 Andrew F. Cheng,5 David C. Slater,1† Maarten H. Versteeg,1 Thomas K. Greathouse,1 Kurt D. Retherford,1,2 Henry Throop,7 Nathaniel J. Cunningham,10 William W. Woods,9 Kelsi N. Singer,3 Constantine C. C. Tsang,3 Rebecca Schindhelm,3 Carey M. Lisse,5 Michael L. Wong,11 Yuk L. Yung,11 Xun Zhu,5 Werner Curdt,12 Panayotis Lavvas,13 Eliot F. Young,3 G. Leonard Tyler,9 and the New Horizons Science Team 1Southwest Research Institute, San Antonio, TX 78238, USA 2University of Texas at San Antonio, San Antonio, TX 78249, USA 3Southwest Research Institute, Boulder, CO 80302, USA 4National Aeronautics and Space Administration, Ames Research Center, Space Science Division, Moffett Field, CA 94035, USA 5The Johns Hopkins University Applied Physics Laboratory, Laurel, MD 20723, USA 6George Mason University, Fairfax, VA 22030, USA 7The Johns Hopkins University, Baltimore, MD 21218, USA 8Search for Extraterrestrial Intelligence Institute, Mountain View, CA 94043, USA 9Stanford University, Stanford, CA 94305, USA 10Nebraska Wesleyan University, Lincoln, NE 68504 11California Institute of Technology, Pasadena, CA 91125, USA 12Max-Planck-Institut für Sonnensystemforschung, 37191 Katlenburg-Lindau, Germany 13Groupe de Spectroscopie Moléculaire et Atmosphérique, Université Reims Champagne-Ardenne, 51687 Reims, France *To whom correspondence should be addressed.
    [Show full text]
  • Abstracts of the 50Th DDA Meeting (Boulder, CO)
    Abstracts of the 50th DDA Meeting (Boulder, CO) American Astronomical Society June, 2019 100 — Dynamics on Asteroids break-up event around a Lagrange point. 100.01 — Simulations of a Synthetic Eurybates 100.02 — High-Fidelity Testing of Binary Asteroid Collisional Family Formation with Applications to 1999 KW4 Timothy Holt1; David Nesvorny2; Jonathan Horner1; Alex B. Davis1; Daniel Scheeres1 Rachel King1; Brad Carter1; Leigh Brookshaw1 1 Aerospace Engineering Sciences, University of Colorado Boulder 1 Centre for Astrophysics, University of Southern Queensland (Boulder, Colorado, United States) (Longmont, Colorado, United States) 2 Southwest Research Institute (Boulder, Connecticut, United The commonly accepted formation process for asym- States) metric binary asteroids is the spin up and eventual fission of rubble pile asteroids as proposed by Walsh, Of the six recognized collisional families in the Jo- Richardson and Michel (Walsh et al., Nature 2008) vian Trojan swarms, the Eurybates family is the and Scheeres (Scheeres, Icarus 2007). In this theory largest, with over 200 recognized members. Located a rubble pile asteroid is spun up by YORP until it around the Jovian L4 Lagrange point, librations of reaches a critical spin rate and experiences a mass the members make this family an interesting study shedding event forming a close, low-eccentricity in orbital dynamics. The Jovian Trojans are thought satellite. Further work by Jacobson and Scheeres to have been captured during an early period of in- used a planar, two-ellipsoid model to analyze the stability in the Solar system. The parent body of the evolutionary pathways of such a formation event family, 3548 Eurybates is one of the targets for the from the moment the bodies initially fission (Jacob- LUCY spacecraft, and our work will provide a dy- son and Scheeres, Icarus 2011).
    [Show full text]
  • The Topography of Iapetus' Leading Side
    Icarus 193 (2008) 359–371 www.elsevier.com/locate/icarus The topography of Iapetus’ leading side Bernd Giese a,∗, Tilmann Denk b, Gerhard Neukum b, Thomas Roatsch a, Paul Helfenstein c, Peter C. Thomas c, Elizabeth P. Turtle d, Alfred McEwen e, Carolyn C. Porco f a DLR, Institute of Planetary Research, Rutherfordstr. 2, 12489 Berlin, Germany b Department of Earth Sciences, Freie Universität Berlin, 12249 Berlin, Germany c Center for Radiophysics and Space Research, Cornell University, Ithaca, NY 14853, USA d Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd., Laurel, MD 20723, USA e Lunar and Planetary Laboratory, University of Arizona, 1541 E. University Blvd., Tucson, AZ 85721, USA f Cassini Imaging Central Laboratory for Operations, Space Science Institute, 4750 Walnut Street, Suite 205, Boulder, CO 80301, USA Received 12 December 2006; revised 15 May 2007 Available online 18 July 2007 Abstract We have used Cassini stereo images to study the topography of Iapetus’ leading side. A terrain model derived at resolutions of 4–8 km reveals that Iapetus has substantial topography with heights in the range of −10 km to +13 km, much more than observed on the other middle-sized satellites of Saturn so far. Most of the topography is older than 4 Ga [Neukum, G., Wagner, R., Denk, T., Porco, C.C., 2005. Lunar Planet. Sci. XXXVI. Abstract 2034] which implies that Iapetus must have had a thick lithosphere early in its history to support this topography. Models of lithospheric deflection by topographic loads provide an estimate of the required elastic thickness in the range of 50–100 km.
    [Show full text]