Eclipses of the Inner Satellites of Jupiter Observed in 2015? E
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Lab 7: Gravity and Jupiter's Moons
Lab 7: Gravity and Jupiter's Moons Image of Galileo Spacecraft Gravity is the force that binds all astronomical structures. Clusters of galaxies are gravitationally bound into the largest structures in the Universe, Galactic Superclusters. The galaxies themselves are held together by gravity, as are all of the star systems within them. Our own Solar System is a collection of bodies gravitationally bound to our star, Sol. Cutting edge science requires the use of Einstein's General Theory of Relativity to explain gravity. But the interactions of the bodies in our Solar System were understood long before Einstein's time. In chapter two of Chaisson McMillan's Astronomy Today, you went over Kepler's Laws. These laws of gravity were made to describe the interactions in our Solar System. P2=a3/M Where 'P' is the orbital period in Earth years, the time for the body to make one full orbit. 'a' is the length of the orbit's semi-major axis, for nearly circular orbits the orbital radius. 'M' is the total mass of the system in units of Solar Masses. Jupiter System Montage picture from NASA ID = PIA01481 Jupiter has over 60 moons at the last count, most of which are asteroids and comets captured from Written by Meagan White and Paul Lewis Page 1 the Asteroid Belt. When Galileo viewed Jupiter through his early telescope, he noticed only four moons: Io, Europa, Ganymede, and Callisto. The Jupiter System can be thought of as a miniature Solar System, with Jupiter in place of the Sun, and the Galilean moons like planets. -
Galileo and the Telescope
Galileo and the Telescope A Discussion of Galileo Galilei and the Beginning of Modern Observational Astronomy ___________________________ Billy Teets, Ph.D. Acting Director and Outreach Astronomer, Vanderbilt University Dyer Observatory Tuesday, October 20, 2020 Image Credit: Giuseppe Bertini General Outline • Telescopes/Galileo’s Telescopes • Observations of the Moon • Observations of Jupiter • Observations of Other Planets • The Milky Way • Sunspots Brief History of the Telescope – Hans Lippershey • Dutch Spectacle Maker • Invention credited to Hans Lippershey (c. 1608 - refracting telescope) • Late 1608 – Dutch gov’t: “ a device by means of which all things at a very great distance can be seen as if they were nearby” • Is said he observed two children playing with lenses • Patent not awarded Image Source: Wikipedia Galileo and the Telescope • Created his own – 3x magnification. • Similar to what was peddled in Europe. • Learned magnification depended on the ratio of lens focal lengths. • Had to learn to grind his own lenses. Image Source: Britannica.com Image Source: Wikipedia Refracting Telescopes Bend Light Refracting Telescopes Chromatic Aberration Chromatic aberration limits ability to distinguish details Dealing with Chromatic Aberration - Stop Down Aperture Galileo used cardboard rings to limit aperture – Results were dimmer views but less chromatic aberration Galileo and the Telescope • Created his own (3x, 8-9x, 20x, etc.) • Noted by many for its military advantages August 1609 Galileo and the Telescope • First observed the -
Cornell University Ithaca, New York 14650 JOSE - JUPITER ORBITING SPACECRAFT
N T Z 33854 C *?** IS81 1? JOSE - JUPITER ORBITING SPACECRAFT: A SYSTEMS STUDY Volume I '>•*,' T COLLEGE OF ENGINEERING Cornell University Ithaca, New York 14650 JOSE - JUPITER ORBITING SPACECRAFT: A SYSTEMS STUDY Volume I Prepared Under Contract No. NGR 33-010-071 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION by NASA-Cornell Doctoral Design Trainee Group (196T-TO) October 1971 College of Engineering Cornell University Ithaca, New York Table of Contents Volume I Preface Chapter I: The Planet Jupiter: A Brief Summary B 1-2 r. Mechanical Properties of the Planet Jupiter. P . T-fi r> 1-10 F T-lfi F T-lfi 0 1-29 H, 1-32 T 1-39 References ... p. I-k2 Chapter II: The Spacecraft Design and Mission Definition A. Introduction p. II-l B. Organizational Structure and the JOSE Mission p. II-l C. JOSE Components p. II-1* D. Proposed Configuration p. II-5 Bibliography and References p. 11-10 Chapter III: Mission Trajectories A. Interplanetary Trajectory Analysis .... p. III-l B. Jupiter Orbital Considerations p. III-6 Bibliography and References. p. 111-38 Chapter IV: Attitude Control A. Introduction and Summary . p. IV-1 B. Expected Disturbance Moments M in Interplanetary Space . p. IV-3 C. Radiation-Produced Impulse Results p. IV-12 D. Meteoroid-Produced Impulse Results p. IV-13 E. Inertia Wheel Analysis p. IV-15 F. Attitude System Tradeoff Analysis p. IV-19 G. Conclusion P. IV-21 References and Bibliography p. TV-26 Chapter V: Propulsion Subsystem A. Mission Requirements p. V-l B. Orbit Insertion Analysis p. -
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. -
Adaptive Multibody Gravity Assist Tours Design in Jovian System for the Ganymede Landing
TO THE ADAPTIVE MULTIBODY GRAVITY ASSIST TOURS DESIGN IN JOVIAN SYSTEM FOR THE GANYMEDE LANDING Grushevskii A.V.(1), Golubev Yu.F.(2), Koryanov V.V.(3), and Tuchin A.G.(4) (1)KIAM (Keldysh Institute of Applied Mathematics), Miusskaya sq., 4, Moscow, 125047, Russia, +7 495 333 8067, E-mail: [email protected] (2)KIAM, Miusskaya sq., 4, Moscow, 125047, Russia, E-mail: [email protected] (3)KIAM, Miusskaya sq., 4, Moscow, 125047, Russia, E-mail: [email protected] (4)KIAM, Miusskaya sq., 4, Moscow, 125047, Russia, E-mail: [email protected] Keywords: gravity assist, adaptive mission design, trajectory design, TID, phase beam Introduction Modern space missions inside Jovian system are not possible without multiple gravity assists (as well as in Saturnian system, etc.). The orbit design for real upcoming very complicated missions by NASA, ESA, RSA should be adaptive to mission parameters, such as: the time of Jovian system arrival, incomplete information about ephemeris of Galilean Moons and their gravitational fields, errors of flybys implementation, instrumentation deflections. Limited dynamic capabilities, taking place in case of maneuvering around Jupiter's moons, demand multiple encounters (about 15-30 times) for these purposes. Flexible algorithm of current mission scenarios synthesis (specially selected) and their operative transformation is required. Mission design is complicated due to requirements of the Ganymede Orbit Insertion (GOI) ("JUICE" ESA) and also Ganymede Landing implementation ("Laplas-P" RSA [1]) comparing to the ordinary early ―velocity gain" missions since ―Pioneers‖ and "Voyagers‖. Thus such scenario splits in two parts. Part 1(P1), as usually, would be used to reduce the spacecraft’s orbital energy with respect to Jupiter and set up the conditions for more frequent flybys. -
Our Planetary System (Chapter 7) Based on Chapter 7
Our Planetary System (Chapter 7) Based on Chapter 7 • This material will be useful for understanding Chapters 8, 9, 10, 11, and 12 on “Formation of the solar system”, “Planetary geology”, “Planetary atmospheres”, “Jovian planet systems”, and “Remnants of ice and rock” • Chapters 3 and 6 on “The orbits of the planets” and “Telescopes” will be useful for understanding this chapter Goals for Learning • How do planets rotate on their axes and orbit the Sun? • What are the planets made of? • What other classes of objects are there in the solar system? Orbits mostly lie in the same flat plane All planets go around the Sun in the same direction Most orbits are close to circular Not coincidences! Most planets rotate in the same “sense” as they orbit the Sun Coincidence? Planetary equators mostly lie in the same plane as their orbits Coincidence? • Interactive Figure: Orbital and Rotational Properties of the Planets Rotation and Orbits of Moons • Most moons (especially the larger ones) orbit in near-circular orbits in the same plane as the equator of their parent planet • Most moons rotate so that their equator is in the plane of their orbit • Most moons rotate in the same “sense” as their orbit around the parent planet • Everything is rotating/orbiting in the same direction A Brief Tour • Distance from Sun •Size •Mass • Composition • Temperature • Rings/Moons Sun 695000 km = 108 RE 333000 MEarth 98% Hydrogen and helium 99.9% total mass of solar system Surface = 5800K Much hotter inside Giant ball of gas Gravity => orbits Heat/light => weather -
Jupiter Mass
CESAR Science Case Jupiter Mass Calculating a planet’s mass from the motion of its moons Student’s Guide Mass of Jupiter 2 CESAR Science Case Table of Contents The Mass of Jupiter ........................................................................... ¡Error! Marcador no definido. Kepler’s Three Laws ...................................................................................................................................... 4 Activity 1: Properties of the Galilean Moons ................................................................................................. 6 Activity 2: Calculate the period of your favourite moon ................................................................................. 9 Activity 3: Calculate the orbital radius of your favourite moon .................................................................... 12 Activity 4: Calculate the Mass of Jupiter ..................................................................................................... 15 Additional Activity: Predict a Transit ............................................................................................................ 16 To know more… .......................................................................................................................... 19 Links ............................................................................................................................................ 19 Mass of Jupiter 3 CESAR Science Case Background Kepler’s Three Laws The three Kepler’s Laws, published between -
The Effect of Jupiter\'S Mass Growth on Satellite Capture
A&A 414, 727–734 (2004) Astronomy DOI: 10.1051/0004-6361:20031645 & c ESO 2004 Astrophysics The effect of Jupiter’s mass growth on satellite capture Retrograde case E. Vieira Neto1;?,O.C.Winter1, and T. Yokoyama2 1 Grupo de Dinˆamica Orbital & Planetologia, UNESP, CP 205 CEP 12.516-410 Guaratinguet´a, SP, Brazil e-mail: [email protected] 2 Universidade Estadual Paulista, IGCE, DEMAC, CP 178 CEP 13.500-970 Rio Claro, SP, Brazil e-mail: [email protected] Received 13 June 2003 / Accepted 12 September 2003 Abstract. Gravitational capture can be used to explain the existence of the irregular satellites of giants planets. However, it is only the first step since the gravitational capture is temporary. Therefore, some kind of non-conservative effect is necessary to to turn the temporary capture into a permanent one. In the present work we study the effects of Jupiter mass growth for the permanent capture of retrograde satellites. An analysis of the zero velocity curves at the Lagrangian point L1 indicates that mass accretion provides an increase of the confinement region (delimited by the zero velocity curve, where particles cannot escape from the planet) favoring permanent captures. Adopting the restricted three-body problem, Sun-Jupiter-Particle, we performed numerical simulations backward in time considering the decrease of M . We considered initial conditions of the particles to be retrograde, at pericenter, in the region 100 R a 400 R and 0 e 0:5. The results give Jupiter’s mass at the X moment when the particle escapes from the planet. -
Cold Plasma Diagnostics in the Jovian System
341 COLD PLASMA DIAGNOSTICS IN THE JOVIAN SYSTEM: BRIEF SCIENTIFIC CASE AND INSTRUMENTATION OVERVIEW J.-E. Wahlund(1), L. G. Blomberg(2), M. Morooka(1), M. André(1), A.I. Eriksson(1), J.A. Cumnock(2,3), G.T. Marklund(2), P.-A. Lindqvist(2) (1)Swedish Institute of Space Physics, SE-751 21 Uppsala, Sweden, E-mail: [email protected], [email protected], mats.andré@irfu.se, [email protected] (2)Alfvén Laboratory, Royal Institute of Technology, SE-100 44 Stockholm, Sweden, E-mail: [email protected], [email protected], [email protected], per- [email protected] (3)also at Center for Space Sciences, University of Texas at Dallas, U.S.A. ABSTRACT times for their atmospheres are of the order of a few The Jovian magnetosphere equatorial region is filled days at most. These atmospheres can therefore rightly with cold dense plasma that in a broad sense co-rotate with its magnetic field. The volcanic moon Io, which be termed exospheres, and their corresponding ionized expels sodium, sulphur and oxygen containing species, parts can be termed exo-ionospheres. dominates as a source for this cold plasma. The three Observations indicate that the exospheres of the three icy Galilean moons (Callisto, Ganymede, and Europa) icy Galilean moons (Europa, Ganymede and Callisto) also contribute with water group and oxygen ions. are oxygen rich [1, 2]. Several authors have also All the Galilean moons have thin atmospheres with modelled these exospheres [3, 4, 5], and the oxygen was residence times of a few days at most. -
Amalthea\'S Modulation of Jovian Decametric Radio Emission
A&A 467, 353–358 (2007) Astronomy DOI: 10.1051/0004-6361:20066505 & c ESO 2007 Astrophysics Amalthea’s modulation of Jovian decametric radio emission O .V. Arkhypov1 andH.O.Rucker2 1 Institute of Radio Astronomy, National Academy of Sciences of Ukraine, Chervonopraporna 4, 61002 Kharkiv, Ukraine e-mail: [email protected] 2 Space Research Institute, Austrian Academy of Sciences, Schmidlstrasse 6, 8042 Graz, Austria e-mail: [email protected] Received 4 October 2006 / Accepted 9 February 2007 ABSTRACT Most modulation lanes in dynamic spectra of Jovian decametric emission (DAM) are formed by radiation scattering on field-aligned inhomogeneities in the Io plasma torus. The positions and frequency drift of hundreds of lanes have been measured on the DAM spectra from UFRO archives. A special 3D algorithm is used for localization of field-aligned magnetospheric inhomogeneities by the frequency drift of modulation lanes. It is found that some lanes are formed near the magnetic shell of the satellite Amalthea mainly ◦ ◦ ◦ ◦ at longitudes of 123 ≤ λIII ≤ 140 (north) and 284 ≤ λIII ≤ 305 (south). These disturbances coincide with regions of plasma compression by the rotating magnetic field of Jupiter. Such modulations are found at other longitudes too (189◦ to 236◦) with higher sensitivity. Amalthea’s plasma torus could be another argument for the ice nature of the satellite, which has a density less than that of water. Key words. planets and satellites: individual: Amalthea – planets and satellites: individual: Jupiter – scattering – plasmas – magnetic fields – radiation mechanisms: non-thermal 1. Introduction (b) The Imai model reproduces the slope and curvature of mod- ulation lanes over their whole frequency range (18–29 MHz; Amalthea (270×165×150 km), at an orbit with a 181 400 km ra- Imai et al. -
Cladistical Analysis of the Jovian Satellites. T. R. Holt1, A. J. Brown2 and D
47th Lunar and Planetary Science Conference (2016) 2676.pdf Cladistical Analysis of the Jovian Satellites. T. R. Holt1, A. J. Brown2 and D. Nesvorny3, 1Center for Astrophysics and Supercomputing, Swinburne University of Technology, Melbourne, Victoria, Australia [email protected], 2SETI Institute, Mountain View, California, USA, 3Southwest Research Institute, Department of Space Studies, Boulder, CO. USA. Introduction: Surrounding Jupiter there are multi- Results: ple satellites, 67 known to-date. The most recent classi- fication system [1,2], based on orbital characteristics, uses the largest member of the group as the name and example. The closest group to Jupiter is the prograde Amalthea group, 4 small satellites embedded in a ring system. Moving outwards there are the famous Galilean moons, Io, Europa, Ganymede and Callisto, whose mass is similar to terrestrial planets. The final and largest group, is that of the outer Irregular satel- lites. Those irregulars that show a prograde orbit are closest to Jupiter and have previously been classified into three families [2], the Themisto, Carpo and Hi- malia groups. The remainder of the irregular satellites show a retrograde orbit, counter to Jupiter's rotation. Based on similarities in semi-major axis (a), inclination (i) and eccentricity (e) these satellites have been grouped into families [1,2]. In order outward from Jupiter they are: Ananke family (a 2.13x107 km ; i 148.9o; e 0.24); Carme family (a 2.34x107 km ; i 164.9o; e 0.25) and the Pasiphae family (a 2:36x107 km ; i 151.4o; e 0.41). There are some irregular satellites, recently discovered in 2003 [3], 2010 [4] and 2011[5], that have yet to be named or officially classified. -
PDS4 Context List
Target Context List Name Type LID 136108 HAUMEA Planet urn:nasa:pds:context:target:planet.136108_haumea 136472 MAKEMAKE Planet urn:nasa:pds:context:target:planet.136472_makemake 1989N1 Satellite urn:nasa:pds:context:target:satellite.1989n1 1989N2 Satellite urn:nasa:pds:context:target:satellite.1989n2 ADRASTEA Satellite urn:nasa:pds:context:target:satellite.adrastea AEGAEON Satellite urn:nasa:pds:context:target:satellite.aegaeon AEGIR Satellite urn:nasa:pds:context:target:satellite.aegir ALBIORIX Satellite urn:nasa:pds:context:target:satellite.albiorix AMALTHEA Satellite urn:nasa:pds:context:target:satellite.amalthea ANTHE Satellite urn:nasa:pds:context:target:satellite.anthe APXSSITE Equipment urn:nasa:pds:context:target:equipment.apxssite ARIEL Satellite urn:nasa:pds:context:target:satellite.ariel ATLAS Satellite urn:nasa:pds:context:target:satellite.atlas BEBHIONN Satellite urn:nasa:pds:context:target:satellite.bebhionn BERGELMIR Satellite urn:nasa:pds:context:target:satellite.bergelmir BESTIA Satellite urn:nasa:pds:context:target:satellite.bestia BESTLA Satellite urn:nasa:pds:context:target:satellite.bestla BIAS Calibrator urn:nasa:pds:context:target:calibrator.bias BLACK SKY Calibration Field urn:nasa:pds:context:target:calibration_field.black_sky CAL Calibrator urn:nasa:pds:context:target:calibrator.cal CALIBRATION Calibrator urn:nasa:pds:context:target:calibrator.calibration CALIMG Calibrator urn:nasa:pds:context:target:calibrator.calimg CAL LAMPS Calibrator urn:nasa:pds:context:target:calibrator.cal_lamps CALLISTO Satellite urn:nasa:pds:context:target:satellite.callisto