Tidal Deformation of Europa and Phobos: Implications on Their Structure and History
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The Geology of the Rocky Bodies Inside Enceladus, Europa, Titan, and Ganymede
49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083) 2905.pdf THE GEOLOGY OF THE ROCKY BODIES INSIDE ENCELADUS, EUROPA, TITAN, AND GANYMEDE. Paul K. Byrne1, Paul V. Regensburger1, Christian Klimczak2, DelWayne R. Bohnenstiehl1, Steven A. Hauck, II3, Andrew J. Dombard4, and Douglas J. Hemingway5, 1Planetary Research Group, Department of Marine, Earth, and Atmospheric Sciences, North Carolina State University, Raleigh, NC 27695, USA ([email protected]), 2Department of Geology, University of Georgia, Athens, GA 30602, USA, 3Department of Earth, Environmental, and Planetary Sciences, Case Western Reserve University, Cleveland, OH 44106, USA, 4Department of Earth and Environmental Sciences, University of Illinois at Chicago, Chicago, IL 60607, USA, 5Department of Earth & Planetary Science, University of California Berkeley, Berkeley, CA 94720, USA. Introduction: The icy satellites of Jupiter and horizontal stresses, respectively, Pp is pore fluid Saturn have been the subjects of substantial geological pressure (found from (3)), and μ is the coefficient of study. Much of this work has focused on their outer friction [12]. Finally, because equations (4) and (5) shells [e.g., 1–3], because that is the part most readily assess failure in the brittle domain, we also considered amenable to analysis. Yet many of these satellites ductile deformation with the relation n –E/RT feature known or suspected subsurface oceans [e.g., 4– ε̇ = C1σ exp , (6) 6], likely situated atop rocky interiors [e.g., 7], and where ε̇ is strain rate, C1 is a constant, σ is deviatoric several are of considerable astrobiological significance. stress, n is the stress exponent, E is activation energy, R For example, chemical reactions at the rock–water is the universal gas constant, and T is temperature [13]. -
Astronomy 330 HW 2 Presentations Outline
Astronomy 330 HW 2 •! Stanley Swat This class (Lecture 12): http://www.ufohowto.com/ Life in the Solar System •! Lucas Guthrie Next Class: http://www.crystalinks.com/abduction.html Life in the Solar System HW 5 is due Wednesday Music: We Are All Made of Stars– Moby Presentations Outline •! Daniel Borup •! Life on Venus? Futurama •! Life on Mars? Life in the Solar System? Earth – Venus comparison •! We want to examine in more detail the backyard of humans. •! What we find may change our estimates of ne. Radius 0.95 Earth Surface gravity 0.91 Earth Venus is the hottest Mass 0.81 Earth planet, the closest in Distance from Sun 0.72 AU size to Earth, the closest Average Temp 475 C in distance to Earth, and Year 224.7 Earth days the planet with the Length of Day 116.8 Earth days longest day. Atmosphere 96% CO2 What We Used to Think Turns Out that Venus is Hell Venus must be hotter, as it is closer the Sun, but the cloud •! The surface is hot enough to melt lead cover must reflect back a large amount of the heat. •! There is a runaway greenhouse effect •! There is almost no water In 1918, a Swedish chemist and Nobel laureate concluded: •! There is sulfuric acid rain •! Everything on Venus is dripping wet. •! Most of the surface is no doubt covered with swamps. •! Not a place to visit for Spring Break. •! The constantly uniform climatic conditions result in an entire absence of adaptation to changing exterior conditions. •! Only low forms of life are therefore represented, mostly no doubt, belonging to the vegetable kingdom; and the organisms are nearly of the same kind all over the planet. -
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. -
JUICE Red Book
ESA/SRE(2014)1 September 2014 JUICE JUpiter ICy moons Explorer Exploring the emergence of habitable worlds around gas giants Definition Study Report European Space Agency 1 This page left intentionally blank 2 Mission Description Jupiter Icy Moons Explorer Key science goals The emergence of habitable worlds around gas giants Characterise Ganymede, Europa and Callisto as planetary objects and potential habitats Explore the Jupiter system as an archetype for gas giants Payload Ten instruments Laser Altimeter Radio Science Experiment Ice Penetrating Radar Visible-Infrared Hyperspectral Imaging Spectrometer Ultraviolet Imaging Spectrograph Imaging System Magnetometer Particle Package Submillimetre Wave Instrument Radio and Plasma Wave Instrument Overall mission profile 06/2022 - Launch by Ariane-5 ECA + EVEE Cruise 01/2030 - Jupiter orbit insertion Jupiter tour Transfer to Callisto (11 months) Europa phase: 2 Europa and 3 Callisto flybys (1 month) Jupiter High Latitude Phase: 9 Callisto flybys (9 months) Transfer to Ganymede (11 months) 09/2032 – Ganymede orbit insertion Ganymede tour Elliptical and high altitude circular phases (5 months) Low altitude (500 km) circular orbit (4 months) 06/2033 – End of nominal mission Spacecraft 3-axis stabilised Power: solar panels: ~900 W HGA: ~3 m, body fixed X and Ka bands Downlink ≥ 1.4 Gbit/day High Δv capability (2700 m/s) Radiation tolerance: 50 krad at equipment level Dry mass: ~1800 kg Ground TM stations ESTRAC network Key mission drivers Radiation tolerance and technology Power budget and solar arrays challenges Mass budget Responsibilities ESA: manufacturing, launch, operations of the spacecraft and data archiving PI Teams: science payload provision, operations, and data analysis 3 Foreword The JUICE (JUpiter ICy moon Explorer) mission, selected by ESA in May 2012 to be the first large mission within the Cosmic Vision Program 2015–2025, will provide the most comprehensive exploration to date of the Jovian system in all its complexity, with particular emphasis on Ganymede as a planetary body and potential habitat. -
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 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. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes. -
Asteroid Retrieval Mission
Where you can put your asteroid Nathan Strange, Damon Landau, and ARRM team NASA/JPL-CalTech © 2014 California Institute of Technology. Government sponsorship acknowledged. Distant Retrograde Orbits Works for Earth, Moon, Mars, Phobos, Deimos etc… very stable orbits Other Lunar Storage Orbit Options • Lagrange Points – Earth-Moon L1/L2 • Unstable; this instability enables many interesting low-energy transfers but vehicles require active station keeping to stay in vicinity of L1/L2 – Earth-Moon L4/L5 • Some orbits in this region is may be stable, but are difficult for MPCV to reach • Lunar Weakly Captured Orbits – These are the transition from high lunar orbits to Lagrange point orbits – They are a new and less well understood class of orbits that could be long term stable and could be easier for the MPCV to reach than DROs – More study is needed to determine if these are good options • Intermittent Capture – Weakly captured Earth orbit, escapes and is then recaptured a year later • Earth Orbit with Lunar Gravity Assists – Many options with Earth-Moon gravity assist tours Backflip Orbits • A backflip orbit is two flybys half a rev apart • Could be done with the Moon, Earth or Mars. Backflip orbit • Lunar backflips are nice plane because they could be used to “catch and release” asteroids • Earth backflips are nice orbits in which to construct things out of asteroids before sending them on to places like Earth- Earth or Moon orbit plane Mars cyclers 4 Example Mars Cyclers Two-Synodic-Period Cycler Three-Synodic-Period Cycler Possibly Ballistic Chen, et al., “Powered Earth-Mars Cycler with Three Synodic-Period Repeat Time,” Journal of Spacecraft and Rockets, Sept.-Oct. -
Reaching for Divinity the Role of Herakles in Relation to Dexiosis
Reaching for Divinity The role of Herakles in relation to dexiosis Florien Plasschaert Utrecht University RMA ANCIENT, MEDIEVAL, AND RENAISSANCE STUDIES thesis under the supervision of dr. R. Strootman | prof. L.V. Rutgers Cover Photo: Dexiosis relief of Antiochos I of Kommagene with Herakles at Arsameia on the Nymphaion. Photograph by Stefano Caneva, distributed under a CC-BY 2.0 license. 1 Reaching for Divinity The role of Herakles in relation to dexiosis Florien Plasschaert Utrecht 2017 2 Acknowledgements The completion of this master thesis would not have been possible were not it for the advice, input and support of several individuals. First of all, I owe a lot of gratitude to my supervisor Dr. Rolf Strootman, whose lectures not only inspired the subject for this thesis, but whose door was always open in case I needed advice or felt the need to discuss complex topics. With his incredible amount of knowledge on the Hellenistic Period provided me with valuable insights, yet always encouraged me to follow my own view on things. Over the course of this study, there were several people along the way who helped immensely by providing information, even if it was not yet published. Firstly, Prof. Dr. Miguel John Versluys, who was kind enough to send his forthcoming book on Nemrud Dagh, an important contribution to the information on Antiochos I of Kommagene. Secondly, Prof. Dr. Panagiotis Iossif who even managed to send several articles in the nick of time to help my thesis. Lastly, the National Numismatic Collection department of the Nederlandse Bank, to whom I own gratitude for sending several scans of Hellenistic coins. -
An Impacting Descent Probe for Europa and the Other Galilean Moons of Jupiter
An Impacting Descent Probe for Europa and the other Galilean Moons of Jupiter P. Wurz1,*, D. Lasi1, N. Thomas1, D. Piazza1, A. Galli1, M. Jutzi1, S. Barabash2, M. Wieser2, W. Magnes3, H. Lammer3, U. Auster4, L.I. Gurvits5,6, and W. Hajdas7 1) Physikalisches Institut, University of Bern, Bern, Switzerland, 2) Swedish Institute of Space Physics, Kiruna, Sweden, 3) Space Research Institute, Austrian Academy of Sciences, Graz, Austria, 4) Institut f. Geophysik u. Extraterrestrische Physik, Technische Universität, Braunschweig, Germany, 5) Joint Institute for VLBI ERIC, Dwingelo, The Netherlands, 6) Department of Astrodynamics and Space Missions, Delft University of Technology, The Netherlands 7) Paul Scherrer Institute, Villigen, Switzerland. *) Corresponding author, [email protected], Tel.: +41 31 631 44 26, FAX: +41 31 631 44 05 1 Abstract We present a study of an impacting descent probe that increases the science return of spacecraft orbiting or passing an atmosphere-less planetary bodies of the solar system, such as the Galilean moons of Jupiter. The descent probe is a carry-on small spacecraft (< 100 kg), to be deployed by the mother spacecraft, that brings itself onto a collisional trajectory with the targeted planetary body in a simple manner. A possible science payload includes instruments for surface imaging, characterisation of the neutral exosphere, and magnetic field and plasma measurement near the target body down to very low-altitudes (~1 km), during the probe’s fast (~km/s) descent to the surface until impact. The science goals and the concept of operation are discussed with particular reference to Europa, including options for flying through water plumes and after-impact retrieval of very-low altitude science data. -
09 Ancient Coin Types, #9
Ancient Greek Coin Types Edward T. Newell Visual Education Committee Lecture Set #9 Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Alexander the Great Tetradrachm, 263 grs, Obv, Herakles with Lion Skin Rev. Zeus Aetophoros enthroned holding Scepter & Royal Eagle Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Alexander the Great Gold Di-stater, 266 grs, Obv, Head of Athena in Crested Corinthian Helmet//Winged Nike holding Mast with Spar Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Egypt, Alexander IV Tetradrachm, 262 grs, 323-311 BC, Obv, Alexander the Great, Elephant’s Scalp Headdress//Rev, Pallas Fighting, Eagle on Thunderbolt Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Egypt, Ptolemy I (Soter), 206 grs, 306-284 BC, Obv, Ptolemy Soter, Diademed wearing Aegis//Rev, Eagle on Thunderbolt, Inscription “Ptolemy Basileos” Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Africa, Carthago Tetradrachm, 262 grs, Obv, Head of Persephone, Dolphins in Field//Rev, Horse’s Head & Palm Tree, Inscription below reads, “Am Machanat” Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Macedonia, Lysimachos Tetradrachm, 265 grs, Obv, Head of Alexander, Deified, with Horn of Ammon//Rev, Pallas Nikephoros, Seated, Inscription reads, “Lysimachos Basileos” Fourth Period 336 BC-280 BC Period of Later Fine Art of Alexander & the Diadochi Cyrene Stater, 134 grs, Obv, -
Epigraphic Bulletin for Greek Religion 1996
Kernos Revue internationale et pluridisciplinaire de religion grecque antique 12 | 1999 Varia Epigraphic Bulletin for Greek Religion 1996 Angelos Chaniotis, Joannis Mylonopoulos and Eftychia Stavrianopoulou Electronic version URL: http://journals.openedition.org/kernos/724 DOI: 10.4000/kernos.724 ISSN: 2034-7871 Publisher Centre international d'étude de la religion grecque antique Printed version Date of publication: 1 January 1999 Number of pages: 207-292 ISSN: 0776-3824 Electronic reference Angelos Chaniotis, Joannis Mylonopoulos and Eftychia Stavrianopoulou, « Epigraphic Bulletin for Greek Religion 1996 », Kernos [Online], 12 | 1999, Online since 13 April 2011, connection on 15 September 2020. URL : http://journals.openedition.org/kernos/724 Kernos Kemos, 12 (1999), p. 207-292. Epigtoaphic Bulletin for Greek Religion 1996 (EBGR 1996) The ninth issue of the BEGR contains only part of the epigraphie harvest of 1996; unforeseen circumstances have prevented me and my collaborators from covering all the publications of 1996, but we hope to close the gaps next year. We have also made several additions to previous issues. In the past years the BEGR had often summarized publications which were not primarily of epigraphie nature, thus tending to expand into an unavoidably incomplete bibliography of Greek religion. From this issue on we return to the original scope of this bulletin, whieh is to provide information on new epigraphie finds, new interpretations of inscriptions, epigraphieal corpora, and studies based p;imarily on the epigraphie material. Only if we focus on these types of books and articles, will we be able to present the newpublications without delays and, hopefully, without too many omissions. -
Long-Term Orbital and Rotational Motions of Ceres and Vesta T
A&A 622, A95 (2019) Astronomy https://doi.org/10.1051/0004-6361/201833342 & © ESO 2019 Astrophysics Long-term orbital and rotational motions of Ceres and Vesta T. Vaillant, J. Laskar, N. Rambaux, and M. Gastineau ASD/IMCCE, Observatoire de Paris, PSL Université, Sorbonne Université, 77 avenue Denfert-Rochereau, 75014 Paris, France e-mail: [email protected] Received 2 May 2018 / Accepted 24 July 2018 ABSTRACT Context. The dwarf planet Ceres and the asteroid Vesta have been studied by the Dawn space mission. They are the two heaviest bodies of the main asteroid belt and have different characteristics. Notably, Vesta appears to be dry and inactive with two large basins at its south pole. Ceres is an ice-rich body with signs of cryovolcanic activity. Aims. The aim of this paper is to determine the obliquity variations of Ceres and Vesta and to study their rotational stability. Methods. The orbital and rotational motions have been integrated by symplectic integration. The rotational stability has been studied by integrating secular equations and by computing the diffusion of the precession frequency. Results. The obliquity variations of Ceres over [ 20 : 0] Myr are between 2◦ and 20◦ and the obliquity variations of Vesta are between − 21◦ and 45◦. The two giant impacts suffered by Vesta modified the precession constant and could have put Vesta closer to the resonance with the orbital frequency 2s s . Given the uncertainty on the polar moment of inertia, the present Vesta could be in this resonance 6 − V where the obliquity variations can vary between 17◦ and 48◦. -
15:1 Resonance Effects on the Orbital Motion of Artificial Satellites
doi: 10.5028/jatm.2011.03032011 Jorge Kennety S. Formiga* FATEC - College of Technology 15:1 Resonance effects on the São José dos Campos/SP – Brazil [email protected] orbital motion of artificial satellites Rodolpho Vilhena de Moraes Abstract: The motion of an artificial satellite is studied considering Federal University of São Paulo geopotential perturbations and resonances between the frequencies of the São José dos Campos/SP – Brazil mean orbital motion and the Earth rotational motion. The behavior of the [email protected] satellite motion is analyzed in the neighborhood of the resonances 15:1. A suitable sequence of canonical transformations reduces the system of differential equations describing the orbital motion to an integrable kernel. *author for correspondence The phase space of the resulting system is studied taking into account that one resonant angle is fixed. Simulations are presented showing the variations of the semi-major axis of artificial satellites due to the resonance effects. Keywords: Resonance, Artificial satellites, Celestial mechanics. INTRODUCTION some resonance’s region. In our study, it satellites in the neighbourhood of the 15:1 resonance (Fig. 1), or satellites The problem of resonance effects on orbital motion with an orbital period of about 1.6 hours will be considered. of satellites falls under a more categorical problem In our choice, the characteristic of the 356 satellites under in astrodynamics, which is known as the one of zero this condition can be seen in Table 1 (Formiga, 2005). divisors. The influence of resonances on the orbital and translational motion of artificial satellites has been extensively discussed in the literature under several aspects.