Nereid: Light Curve for 1999-2006 and a Scenario for Its Variations
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Phases of Venus and Galileo
Galileo and the phases of Venus I) Periods of Venus 1) Synodical period and phases The synodic period1 of Venus is 584 days The superior2 conjunction occured on 11 may 1610. Calculate the date of the quadrature, of the inferior conjunction and of the next superior conjunction, supposing the motions of the Earth and Venus are circular and uniform. In fact the next superior conjunction occured on 11 december 1611 and inferior conjunction on 26 february 1611. 2) Sidereal period The sidereal period of the Earth is 365.25 days. Calculate the sidereal period of Venus. II) Phases on Venus in geo and heliocentric models 1) Phases in differents models 1) Determine the phases of Venus in geocentric models, where the Earth is at the center of the universe and planets orbit around (Venus “above” or “below” the sun) * Pseudo-Aristoteles model : Earth (center)-Moon-Sun-Mercury-Venus-Mars-Jupiter-Saturne * Ptolemeo’s model : Earth (center)-Moon-Mercury-Venus-Sun-Mars-Jupiter-Saturne 2) Determine the phases of Venus in the heliocentric model, where planets orbit around the sun. Copernican system : Sun (center)-Mercury-Venus-Earth-Mars-Jupiter-Saturne 2) Observations of Galileo Galileo (1564-1642) observed Venus in 1610-1611 with a telescope. Read the letters of Galileo. May we conclude that the Copernican model is the only one available ? When did Galileo begins to observe Venus? Give the approximate dates of the quadrature and of the inferior conjunction? What are the approximate dates of the 5 observations of Galileo supposing the figure from the Essayer, was drawn in 1610-1611 1 The synodic period is the time that it takes for the object to reappear at the same point in the sky, relative to the Sun, as observed from Earth; i.e. -
Astrometric Reduction of Cassini ISS Images of the Saturnian Satellites Mimas and Enceladus? R
A&A 551, A129 (2013) Astronomy DOI: 10.1051/0004-6361/201220831 & c ESO 2013 Astrophysics Astrometric reduction of Cassini ISS images of the Saturnian satellites Mimas and Enceladus? R. Tajeddine1;3, N. J. Cooper1;2, V. Lainey1, S. Charnoz3, and C. D. Murray2 1 IMCCE, Observatoire de Paris, UMR 8028 du CNRS, UPMC, Université de Lille 1, 77 av. Denfert-Rochereau, 75014 Paris, France e-mail: [email protected] 2 Astronomy Unit, School of Physics and Astronomy, Queen Mary University of London, Mile End Road, London E1 4NS, UK 3 Laboratoire AIM, UMR 7158, Université Paris Diderot – CEA IRFU – CNRS, Centre de l’Orme les Merisiers, 91191 Gif-sur-Yvette Cedex, France Received 2 December 2012 / Accepted 6 February 2013 ABSTRACT Aims. We provide astrometric observations of two of Saturn’s main satellites, Mimas and Enceladus, using high resolution Cassini ISS Narrow Angle Camera images. Methods. We developed a simplified astrometric reduction model for Cassini ISS images as an alternative to the one proposed by the Jet Propulsion Labratory (JPL). The particular advantage of the new model is that it is easily invertible, with only marginal loss in accuracy. We also describe our new limb detection and fitting technique. Results. We provide a total of 1790 Cassini-centred astrometric observations of Mimas and Enceladus, in right ascension (α) and declination (δ) in the International Celestial Reference Frame (ICRF). Mean residuals compared to JPL ephemerides SAT317 and SAT351 of about one kilometre for Mimas and few hundreds of metres for Enceladus were obtained, in α cos δ and δ, with a standard deviation of a few kilometres for both satellites. -
Spin-Orbit Coupling for Close-In Planets Alexandre C
A&A 630, A102 (2019) Astronomy https://doi.org/10.1051/0004-6361/201936336 & © ESO 2019 Astrophysics Spin-orbit coupling for close-in planets Alexandre C. M. Correia1,2 and Jean-Baptiste Delisle2,3 1 CFisUC, Department of Physics, University of Coimbra, 3004-516 Coimbra, Portugal e-mail: [email protected] 2 ASD, IMCCE, Observatoire de Paris, PSL Université, 77 Av. Denfert-Rochereau, 75014 Paris, France 3 Observatoire de l’Université de Genève, 51 chemin des Maillettes, 1290 Sauverny, Switzerland Received 17 July 2019 / Accepted 20 August 2019 ABSTRACT We study the spin evolution of close-in planets in multi-body systems and present a very general formulation of the spin-orbit problem. This includes a simple way to probe the spin dynamics from the orbital perturbations, a new method for computing forced librations and tidal deformation, and general expressions for the tidal torque and capture probabilities in resonance. We show that planet–planet perturbations can drive the spin of Earth-size planets into asynchronous or chaotic states, even for nearly circular orbits. We apply our results to Mercury and to the KOI-1599 system of two super-Earths in a 3/2 mean motion resonance. Key words. celestial mechanics – planets and satellites: general – chaos 1. Introduction resonant rotation with the orbital libration frequency (Correia & Robutel 2013; Leleu et al. 2016; Delisle et al. 2017). The inner planets of the solar system, like the majority of the Despite the proximity of solar system bodies, the determi- main satellites, currently present a rotation state that is differ- nation of their rotational periods has only been achieved in ent from what is believed to have been the initial state (e.g., the second half of the 20th century. -
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. -
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. -
The Chaotic Rotation of Hyperion*
ICARUS 58, 137-152 (1984) The Chaotic Rotation of Hyperion* JACK WISDOM AND STANTON J. PEALE Department of Physics, University of California, Santa Barbara, California 93106 AND FRANGOIS MIGNARD Centre d'Etudes et de Recherehes G~odynamique et Astronomique, Avenue Copernic, 06130 Grasse, France Received August 22, 1983; revised November 4, 1983 A plot of spin rate versus orientation when Hyperion is at the pericenter of its orbit (surface of section) reveals a large chaotic zone surrounding the synchronous spin-orbit state of Hyperion, if the satellite is assumed to be rotating about a principal axis which is normal to its orbit plane. This means that Hyperion's rotation in this zone exhibits large, essentially random variations on a short time scale. The chaotic zone is so large that it surrounds the 1/2 and 2 states, and libration in the 3/2 state is not possible. Stability analysis shows that for libration in the synchronous and 1/2 states, the orientation of the spin axis normal to the orbit plane is unstable, whereas rotation in the 2 state is attitude stable. Rotation in the chaotic zone is also attitude unstable. A small deviation of the principal axis from the orbit normal leads to motion through all angles in both the chaotic zone and the attitude unstable libration regions. Measures of the exponential rate of separation of nearby trajectories in phase space (Lyapunov characteristic exponents) for these three-dimensional mo- tions indicate the the tumbling is chaotic and not just a regular motion through large angles. As tidal dissipation drives Hyperion's spin toward a nearly synchronous value, Hyperion necessarily enters the large chaotic zone. -
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 ................................................. -
194 Publications of the Measurements of The
194 PUBLICATIONS OF THE MEASUREMENTS OF THE RADIATION FROM THE PLANET MERCURY By Edison Pettit and Seth Β. Nicholson The total radiation from Mercury and its transmission through a water cell and through a microscope cover glass were measured with the thermocouple at the 60-inch reflector on June 17, 1923, and again at the 100-inch reflector on June 21st. Since the thermocouple is compensated for general diffuse radiation it is possible to measure the radiation from stars and planets in full daylight quite as well as at night (aside from the effect of seeing), and in the present instance Mercury and the comparison stars were observed near the meridian between th hours of 9 a. m. and 1 p. m. The thermocouple cell is provided with a rock salt window 2 mm thick obtained from the Smithsonian Institution through the kindness of Dr. Abbot. The transmission curves for the water cell and microscope cover glass have been carefully de- termined : those for the former may be found in Astrophysical Journal, 56, 344, 1922; those for the latter, together with the curves for rock salt, fluorite and the atmosphere for average observing conditions are given in Figure 1. We may consider the water cell to transmit in the region of 0.3/a to 1.3/x and the covér glass to transmit between 0.3μ and 5.5/1,, although some radiation is transmitted by the cover glass up to 7.5/a. The atmosphere acts as a screen transmitting prin- cipally in two regions 0.3μ, to 2,5μ and 8μ to 14μ, respectively. -
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). -
Ice& Stone 2020
Ice & Stone 2020 WEEK 33: AUGUST 9-15 Presented by The Earthrise Institute # 33 Authored by Alan Hale About Ice And Stone 2020 It is my pleasure to welcome all educators, students, topics include: main-belt asteroids, near-Earth asteroids, and anybody else who might be interested, to Ice and “Great Comets,” spacecraft visits (both past and Stone 2020. This is an educational package I have put future), meteorites, and “small bodies” in popular together to cover the so-called “small bodies” of the literature and music. solar system, which in general means asteroids and comets, although this also includes the small moons of Throughout 2020 there will be various comets that are the various planets as well as meteors, meteorites, and visible in our skies and various asteroids passing by Earth interplanetary dust. Although these objects may be -- some of which are already known, some of which “small” compared to the planets of our solar system, will be discovered “in the act” -- and there will also be they are nevertheless of high interest and importance various asteroids of the main asteroid belt that are visible for several reasons, including: as well as “occultations” of stars by various asteroids visible from certain locations on Earth’s surface. Ice a) they are believed to be the “leftovers” from the and Stone 2020 will make note of these occasions and formation of the solar system, so studying them provides appearances as they take place. The “Comet Resource valuable insights into our origins, including Earth and of Center” at the Earthrise web site contains information life on Earth, including ourselves; about the brighter comets that are visible in the sky at any given time and, for those who are interested, I will b) we have learned that this process isn’t over yet, and also occasionally share information about the goings-on that there are still objects out there that can impact in my life as I observe these comets. -
CLARK PLANETARIUM SOLAR SYSTEM FACT SHEET Data Provided by NASA/JPL and Other Official Sources
CLARK PLANETARIUM SOLAR SYSTEM FACT SHEET Data provided by NASA/JPL and other official sources. This handout ©July 2013 by Clark Planetarium (www.clarkplanetarium.org). May be freely copied by professional educators for classroom use only. The known satellites of the Solar System shown here next to their planets with their sizes (mean diameter in km) in parenthesis. The planets and satellites (with diameters above 1,000 km) are depicted in relative size (with Earth = 0.500 inches) and are arranged in order by their distance from the planet, with the closest at the top. Distances from moon to planet are not listed. Mercury Jupiter Saturn Uranus Neptune Pluto • 1- Metis (44) • 26- Hermippe (4) • 54- Hegemone (3) • 1- S/2009 S1 (1) • 33- Erriapo (10) • 1- Cordelia (40.2) (Dwarf Planet) (no natural satellites) • 2- Adrastea (16) • 27- Praxidike (6.8) • 55- Aoede (4) • 2- Pan (26) • 34- Siarnaq (40) • 2- Ophelia (42.8) • Charon (1186) • 3- Bianca (51.4) Venus • 3- Amalthea (168) • 28- Thelxinoe (2) • 56- Kallichore (2) • 3- Daphnis (7) • 35- Skoll (6) • Nix (60?) • 4- Thebe (98) • 29- Helike (4) • 57- S/2003 J 23 (2) • 4- Atlas (32) • 36- Tarvos (15) • 4- Cressida (79.6) • Hydra (50?) • 5- Desdemona (64) • 30- Iocaste (5.2) • 58- S/2003 J 5 (4) • 5- Prometheus (100.2) • 37- Tarqeq (7) • Kerberos (13-34?) • 5- Io (3,643.2) • 6- Pandora (83.8) • 38- Greip (6) • 6- Juliet (93.6) • 1- Naiad (58) • 31- Ananke (28) • 59- Callirrhoe (7) • Styx (??) • 7- Epimetheus (119) • 39- Hyrrokkin (8) • 7- Portia (135.2) • 2- Thalassa (80) • 6- Europa (3,121.6) -
Arxiv:1604.04184V1 [Astro-Ph.EP] 14 Apr 2016 Fax: +33-1-46332834 E-Mail: [email protected] 2 Valery´ Lainey the Authors Obtained an Averaged Estimation of K2/Q
Noname manuscript No. (will be inserted by the editor) Quantification of tidal parameters from Solar system data Valery´ Lainey the date of receipt and acceptance should be inserted later Abstract Tidal dissipation is the main driver of orbital evolution of natural satellites and a key point to understand the exoplanetary system configurations. Despite its importance, its quantification from observations still remains difficult for most objects of our own Solar system. In this work, we overview the method that has been used to determine, directly from observations, the tidal parameters, with emphasis on the Love number k2 and the tidal quality factor Q. Up-to-date values of these tidal parameters are summarized. Last, an assessment on the possible determination of the tidal ratio k2=Q of Uranus and Neptune is done. This may be particularly relevant for coming astrometric campaigns and future space missions focused on these systems. Keywords Tides · Astrometry · Space geodesy 1 Introduction While fundamental for our understanding of the Solar system and the long-term evolution of the exo-planetary systems, tidal parameters are difficult to determine from observations. Indeed, they provide a small dynamical signal, both on natural and artificial celestial objects, in comparison to other perturbations arising in the system (see next section). However, tides do provide large effects on the long term evolution of the natural bodies. This is why es- timations of the tidal parameters have often been done from the assumed past evolution of planets and moons. In that respect, estimation of the average tidal ratio k2=Q for the giant planets was done already back in the 60s by Goldreich & Soter (1966).