The Asgard and Valhalla Regions; Galileo's New Views of Callisto K.C
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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. -
1 INTRODUCTION 1.1 Document Overview 1.2 Software Overview
625-645-234011, Rev. A TABLE OF CONTENTS 1 INTRODUCTION 1.1 Document Overview 1.2 Software Overview 1.3 System Hardware/Software Requirements 1.3.1 SUN 1.3.2 Windows 3.1 or Macintosh 1.4 Packaging 1.4.1 MIRAGE System Files 1.4.2 MIRAGE Data Files 1.4.3 Sequence Delivery Directories 1.5 Typographical Conventions 2 SETTING UP TO RUN MIRAGE 2.1 Obtaining a Unix Account 2.2 Installing the X terminal Server 2.2.1 MacIntosh 2.2.2 Windows 3.1 2.2.3 What's your IP Address? 2.3 Starting and Exiting MIRAGE 2.3.1 From Donatello 2.3.2 From a MAC 2.3.3 From Windows 2.3.4 From a Sun Workstation (e.g. POINTER) 3 MIRAGE INTERFACE BASICS 3.1 The MIRAGE Display 3.1.1 Command Pane 3.1.2 History Pane 3.1.3 Display Work Area 3.1.4 The Legend 3.2 Configuring MIRAGE 3.2.1 Changing Legends 3.2.2 Zooming and Scaling 625-645-234011, Rev. A 3.2.3 Vertical Ruler 3.3 MIRAGE Commands 3.3.1 Aborting Commands 3.3.2 Command Help 3.3.3 Mouse Command Sets 3.4 The MIRAGE Menus 4 MODELING IN MIRAGE 4.1 Multi Use Buffer 4.1.1 Buffer High and Low Water Marks 4.1.2 Filling the Buffer 4.1.3 Draining the Buffer 4.1.4 Modeling the Effects of Real Time Activities on the MUB 4.1.5 Modeling the Effect of Buffer Dump to Tape on the MUB 4.1.6 Modeling the Effect of Playback on the MUB 4.1.7 Modeling the Effect of Telemetry on the MUB 4.1.8 User Control of the MUB Level 4.2 Priority Buffer 4.3 DMS 4.4 Running the Models 4.5 How Modeling Results are Displayed 4.6 OAPEL-level Resource Conflict Checking 4.7 How OAPEL-level Conflict Checking Results are Displayed 5 USING MIRAGE 5.1 Starting MIRAGE 5.1.1 Miscellaneous (But Useful) Commands 5.1.2 Moving around the screen 5.2 Create OAPEL 5.2.1 Activity ID Usage 5.2.2 Adding PAs to an OAPEL 5.3 Edit OAPEL 5.4 Create PA 5.5 Edit PA 625-645-234011, Rev. -
Impact Cratering
6 Impact cratering The dominant surface features of the Moon are approximately circular depressions, which may be designated by the general term craters … Solution of the origin of the lunar craters is fundamental to the unravel- ing of the history of the Moon and may shed much light on the history of the terrestrial planets as well. E. M. Shoemaker (1962) Impact craters are the dominant landform on the surface of the Moon, Mercury, and many satellites of the giant planets in the outer Solar System. The southern hemisphere of Mars is heavily affected by impact cratering. From a planetary perspective, the rarity or absence of impact craters on a planet’s surface is the exceptional state, one that needs further explanation, such as on the Earth, Io, or Europa. The process of impact cratering has touched every aspect of planetary evolution, from planetary accretion out of dust or planetesimals, to the course of biological evolution. The importance of impact cratering has been recognized only recently. E. M. Shoemaker (1928–1997), a geologist, was one of the irst to recognize the importance of this process and a major contributor to its elucidation. A few older geologists still resist the notion that important changes in the Earth’s structure and history are the consequences of extraterres- trial impact events. The decades of lunar and planetary exploration since 1970 have, how- ever, brought a new perspective into view, one in which it is clear that high-velocity impacts have, at one time or another, affected nearly every atom that is part of our planetary system. -
Lunar and Planetary Science XXIX 1866.Pdf
Lunar and Planetary Science XXIX 1866.pdf GALILEO AT CALLISTO: OVERVIEW OF NOMINAL MISSION RESULTS. J. E. Klemaszewski, R. Greeley, K.S. Homan, K.C. Bender, F.C. Chuang, S. Kadel;1 R.J. Sullivan;2 C. Chapman, W.J. Merline;3 J. Moore;4 R. Wagner, T. Denk, G. Neukum;5 J. Head, R. Pappalardo, L. Prockter;6 M. Belton;7 T.V. Johnson;8 C. Pilcher9 and the Galileo SSI Team. 1Dept. of Geology, Arizona State University, Tempe, AZ 871404; 2Cornell Univ., Ithaca, NY; 3SWRI, Boulder, CO; 4NASA Ames, Moffett Field, CA; 5DLR, Berlin, Germany; 6Brown Univ., Providence, RI; 7NOAO, Tucson, AZ; 8JPL, Pasadena, CA; 9NASA HQ, Washington, DC. The solid-state imaging (SSI) system on board the over 4000 and 1600 km in diameter; their Galileo orbiter acquired 118 images of the Jovian morphologies and theories concerning their origin satellite Callisto on 8 of its 11 nominal mission orbits. have been described by many investigators [e.g. On three of these orbits clear-filter imaging data were 2,3,6,8,9]. Whether or not Callisto is differentiated acquired at resolutions of 150 m/pxl or better, and on could not be determined from Voyager data [6]. five orbits color data were acquired at resolutions Galileo mission objectives for Callisto [10] include (a) between 13.7 and 1.1 km/pixel. Galileo images reveal the characterization of surface processes and that degradational processes have acted on the surface materials, (b) impact craters morphologies and of Callisto causing the erosion of crater walls and rims. evolution, (c) the search for evidence of endogenic This degradation is most likely responsible for the activity, (d) the determination of the origin and production of the dark material that appears to blanket morphology of multi-ring structures, and (e) Callisto’s surface, resulting in a lack of small (<10 km comparison of Callisto and Ganymede. -
Appendix Contains a Timeline, Galileo Mission Overview (June 1996–December 1997), and a Set of Quick–Look Orbit Facts Sheets
A P P E N D I X This appendix contains a timeline, Galileo Mission Overview (June 1996–December 1997), and a set of Quick–Look Orbit Facts sheets. The essentials of each orbit are listed. We have provided them as a handy reference while the orbiter’s tour progresses in the months to come. Appendix • Page A-1 Project Galileo Quick-Look Orbit Facts Appendix • Page A- 5 PROJECT GALILEO QUICK-LOOK ORBIT FACTS Fact Sheet Guide Title Quick Facts Indicates the target satellite and the number of the This section provides a summary listing of the orbit in the satellite tour. In this example, Ganymede is characteristics of the target satellite encounter as well the target satellite on the first orbit of the orbital tour. as the Jupiter encounter. PROJECT GALILEO QUICK-LOOK ORBIT FACTS PROJECT GALILEO QUICK-LOOK ORBIT FACTS Ganymede - Orbit 1 Ganymede - Orbit 1 Encounter Trajectory Quick Facts Ganymede Flyby Geometry +30 min Ganymede Encounter Earth Sun 27 June 1996 Ganymede C/A +15 min 06:29 UTC Ganymede C/A Altitude: 844 km Jupiter 6/27 6/26 133 times closer than VGR1 70 times closer than VGR2 Earth Speed: 7.8 km/s 0W -15 min Sun Jupiter C/A 6/28 Latitude: 30 deg N Longitude: 112 deg W 270W -30 min Perijove Io 28 June 1996 00:31 UTC Europa Jupiter Range: 11.0 Rj Time Ordered Listing Ganymede 6/29 Earth Range: 4.2 AU EVENT TIME (PDT-SCET) EVENT (continued) TIME (PDT-SCET) OWLT: 35 min Start Encounter 23 June 96 09:00 Europa C/A (156000 km) 18:22 Callisto Start Ganymede-1 real-time survey (F&P) 09:02 Europa global observation (NIMS/SSI) 18:43 -
Rituals for the Northern Tradition
Horn and Banner Horn and Banner Rituals for the Northern Tradition Compiled by Raven Kaldera Hubbardston, Massachusetts Asphodel Press 12 Simond Hill Road Hubbardston, MA 01452 Horn and Banner: Rituals for the Northern Tradition © 2012 Raven Kaldera ISBN: 978-0-9825798-9-3 Cover Photo © 2011 Thorskegga Thorn All rights reserved. Unless otherwise specified, no part of this book may be reproduced in any form or by any means without the permission of the author. Printed in cooperation with Lulu Enterprises, Inc. 860 Aviation Parkway, Suite 300 Morrisville, NC 27560 To all the good folk of Iron Wood Kindred, past and present, and especially for Jon Norman whose innocence and enthusiasm we will miss forever. Rest in Hela’s arms, Jon, And may you find peace. Contents Beginnings Creating Sacred Space: Opening Rites ................................... 1 World Creation Opening ....................................................... 3 Jormundgand Opening Ritual ................................................ 4 Four Directions and Nine Worlds: ........................................ 5 Cosmological Opening Rite .................................................... 5 Warding Rite of the Four Directions ..................................... 7 Divide And Conquer: Advanced Group Liturgical Design. 11 Rites of Passage Ritual to Bless a Newborn .................................................... 25 Seven-Year Rite ..................................................................... 28 A Note On Coming-Of-Age Rites ....................................... -
Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC
DOCUMENT RESUME ED 312 131 SE 050 900 AUTHOR Morrison, David; Samz, Jane TITLE Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC. Scientific and Technical Information Branch. REPORT NO NASA-SP-439 PUB DATE 80 NOTE 208p.; Colored photographs and drawings may not reproduce well. AVAILABLE FROMSuperintendent of Documents, U.S. Government Printing Office, Washington, DC 20402 ($9.00). PUB TYPE Reports - Descriptive (141) EDRS PRICE MF01/PC09 Plus Postage. DESCRIPTORS Aerospace Technology; *Astronomy; Satellites (Aerospace); Science Materials; *Science Programs; *Scientific Research; Scientists; *Space Exploration; *Space Sciences IDENTIFIERS *Jupiter; National Aeronautics and Space Administration; *Voyager Mission ABSTRACT This publication illustrates the features of Jupiter and its family of satellites pictured by the Pioneer and the Voyager missions. Chapters included are:(1) "The Jovian System" (describing the history of astronomy);(2) "Pioneers to Jupiter" (outlining the Pioneer Mission); (3) "The Voyager Mission"; (4) "Science and Scientsts" (listing 11 science investigations and the scientists in the Voyager Mission);.(5) "The Voyage to Jupiter--Cetting There" (describing the launch and encounter phase);(6) 'The First Encounter" (showing pictures of Io and Callisto); (7) "The Second Encounter: More Surprises from the 'Land' of the Giant" (including pictures of Ganymede and Europa); (8) "Jupiter--King of the Planets" (describing the weather, magnetosphere, and rings of Jupiter); (9) "Four New Worlds" (discussing the nature of the four satellites); and (10) "Return to Jupiter" (providing future plans for Jupiter exploration). Pictorial maps of the Galilean satellites, a list of Voyager science teams, and a list of the Voyager management team are appended. Eight technical and 12 non-technical references are provided as additional readings. -
Grímnismál: Acriticaledition
GRÍMNISMÁL: A CRITICAL EDITION Vittorio Mattioli A Thesis Submitted for the Degree of PhD at the University of St Andrews 2017 Full metadata for this item is available in St Andrews Research Repository at: http://research-repository.st-andrews.ac.uk/ Please use this identifier to cite or link to this item: http://hdl.handle.net/10023/12219 This item is protected by original copyright This item is licensed under a Creative Commons Licence Grímnismál: A Critical Edition Vittorio Mattioli This thesis is submitted in partial fulfilment for the degree of PhD at the University of St Andrews 12.11.2017 i 1. Candidate’s declarations: I Vittorio Mattioli, hereby certify that this thesis, which is approximately 72500 words in length, has been written by me, and that it is the record of work carried out by me, or principally by myself in collaboration with others as acknowledged, and that it has not been submitted in any previous application for a higher degree. I was admitted as a research student in September, 2014 and as a candidate for the degree of Ph.D. in September, 2014; the higher study for which this is a record was carried out in the University of St Andrews between 2014 and 2017. Date signature of candidate 2. Supervisor’s declaration: I hereby certify that the candidate has fulfilled the conditions of the Resolution and Regulations appropriate for the degree of Ph.D. in the University of St Andrews and that the candidate is qualified to submit this thesis in application for that degree. Date signature of supervisors 3. -
02. Solar System (2001) 9/4/01 12:28 PM Page 2
01. Solar System Cover 9/4/01 12:18 PM Page 1 National Aeronautics and Educational Product Space Administration Educators Grades K–12 LS-2001-08-002-HQ Solar System Lithograph Set for Space Science This set contains the following lithographs: • Our Solar System • Moon • Saturn • Our Star—The Sun • Mars • Uranus • Mercury • Asteroids • Neptune • Venus • Jupiter • Pluto and Charon • Earth • Moons of Jupiter • Comets 01. Solar System Cover 9/4/01 12:18 PM Page 2 NASA’s Central Operation of Resources for Educators Regional Educator Resource Centers offer more educators access (CORE) was established for the national and international distribution of to NASA educational materials. NASA has formed partnerships with universities, NASA-produced educational materials in audiovisual format. Educators can museums, and other educational institutions to serve as regional ERCs in many obtain a catalog and an order form by one of the following methods: States. A complete list of regional ERCs is available through CORE, or electroni- cally via NASA Spacelink at http://spacelink.nasa.gov/ercn NASA CORE Lorain County Joint Vocational School NASA’s Education Home Page serves as a cyber-gateway to informa- 15181 Route 58 South tion regarding educational programs and services offered by NASA for the Oberlin, OH 44074-9799 American education community. This high-level directory of information provides Toll-free Ordering Line: 1-866-776-CORE specific details and points of contact for all of NASA’s educational efforts, Field Toll-free FAX Line: 1-866-775-1460 Center offices, and points of presence within each State. Visit this resource at the E-mail: [email protected] following address: http://education.nasa.gov Home Page: http://core.nasa.gov NASA Spacelink is one of NASA’s electronic resources specifically devel- Educator Resource Center Network (ERCN) oped for the educational community. -
Analysis of Close Encounters with Ganymede and Callisto Using A
Analysis of close encounters with Ganymede and Callisto using a genetic n-body algorithm PhilipM.Winter MattiaA.Galiazzo Thomas I. Maindl Department for Astrophysics, University of Vienna Front. Astron. Space Sci., 22 May 2018, https://doi.org/10.3389/fspas.2018.00016 Abstract In this work we describe a genetic algorithm which is used in order to study orbits of minor bodies in the frames of close encounters. We find that the algorithm in com- bination with standard orbital numerical integrators can be used as a good proxy for finding typical orbits of minor bodies in close encounters with planets and even their moons, saving a lot of computational time compared to long-term orbital numerical in- tegrations. Here, we study close encounters of Centaurs with Callisto and Ganymede in particular. We also perform n-body numerical simulations for comparison. We find typ- ical impact velocities to be between vrel = 20[vesc] and vrel = 30[vesc] for Ganymede and between vrel = 25[vesc] and vrel = 35[vesc] for Callisto. Keywords: Callisto, Ganymede, n-body, close encounters, genetic algorithm, celestial mechanics, numerical simulation, collisions 1. Introduction Jupiter’s large icy moons such as Ganymede and Callisto show countless impact craters across their surface. Studying these craters gives deep insights into the impactors as well as the moons themselves. This is the first approach in the frame of future works of studying collisions with the outermost moon Callisto. We are especially interested in the Valhalla crater system, Callisto’s biggest crater. This impact structure measures several hundred of kilometers in diameter and shows some extraordinary features such as an extensive ring system in the outskirts of the crater (Greeley et al., 2000; Stewart and Allen, 2002). -
Reconstruction of Callisto's Valhalla Basin Using N
EPSC Abstracts Vol. 11, EPSC2017-795, 2017 European Planetary Science Congress 2017 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2017 Reconstruction of Callisto’s Valhalla basin using n-body and SPH simulations P. M. Winter (1), T. I. Maindl (1), C. Schäfer (2), M. A. Galiazzo (1) (1) Department of Astrophysics, University of Vienna, Austria, (2) Institut für Astronomie und Astrophysik, Eberhard Karls Universität Tübingen, Germany Abstract and the inner structure of Callisto. We present results of n-body and smooth particle hy- 2. Methods drodynamics (SPH) simulations, exploring the crater formation process of the Valhalla crater located on the For the n-body simulations we use the Sun, Jupiter, Jovian Moon Callisto. We compute typical impact ve- Ganymede and Callisto as massive bodies and measure locities and impact angles which we then use as input the moons collisions with a randomized set of initial for the SPH simulations to reconstruct the actual crater particles. We determine impact velocities, impact an- formation. Using a three-layered Callisto model with a gles, as well as other relevant information for further subsurface ocean, we find significant connections be- statistical analysis. We found typical, maximum, rel- tween the crater formation process and the interaction ative velocities to Jupiter to be vrel,orbital = 670 m/s, with the subsurface ocean. We also investigate the vrel,radial = 65 m/s and vrel,vertical = 4534 m/s. properties of the projectile and numerical effects of We perform the SPH simulations ([9],[14],[16],[17]) low-resolution projectiles in the context of SPH. with the miluphCUDA code ([19]), designed to accu- rately model collision events of solid bodies including 1. -
Jupiter and Its Moons
Modern Astronomy: Voyage to the Planets Lecture 6 Jupiter and its moons University of Sydney Centre for Continuing Education Autumn 2005 BOOKINGS ARE ESSENTIAL! Please call The Australian Museum Society on 9320 6225, or book online at http://www.amonline.net.au/tams There have been five Pioneer 10 1973 Flyby spacecraft which performed flybys of Jupiter, and one – Pioneer 11 1974 Flyby Galileo – which orbited Voyager 1 1979 Flyby Jupiter for eight years. Voyager 2 1979 Flyby Orbiter and Galileo 1995–2003 probe Cassini 2000 Flyby Jupiter Basic facts Jupiter Jupiter/Earth Mass 1899 x 1024 kg 317.83 Radius 71,492 km 11.21 Mean density 1.326 g/cm3 0.240 Gravity (eq., 1 bar) 24.79 m/s2 2.530 Semi-major axis 778.57 x 106 km 5.204 Period 4332.589 d 11.862 Orbital inclination 1.304o - Orbital eccentricity 0.0489 2.928 Axial tilt 3.1o 0.133 Rotation period 9.9250 h 0.415 Length of day 9.9259 h 0.414 Jupiter is the most massive of the planets, 2.5 times the mass of the other planets combined. It is the only planet whose barycentre with the Sun actually lies above the Sun’s surface (1.068 solar radii from the Sun's centre). True colour picture of Jupiter, taken by Cassini on its way to Saturn during closest approach. The smallest features visible are only 60 km across. Jupiter exhibits differential rotation – the rotational period depends on latitude, with the equatorial zones rotating a little faster (9h 50m period) than the higher latitudes (9h 55m period).