The In-Situ Exploration of Jupiter's Radiation Belts
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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. -
Mission to Jupiter
This book attempts to convey the creativity, Project A History of the Galileo Jupiter: To Mission The Galileo mission to Jupiter explored leadership, and vision that were necessary for the an exciting new frontier, had a major impact mission’s success. It is a book about dedicated people on planetary science, and provided invaluable and their scientific and engineering achievements. lessons for the design of spacecraft. This The Galileo mission faced many significant problems. mission amassed so many scientific firsts and Some of the most brilliant accomplishments and key discoveries that it can truly be called one of “work-arounds” of the Galileo staff occurred the most impressive feats of exploration of the precisely when these challenges arose. Throughout 20th century. In the words of John Casani, the the mission, engineers and scientists found ways to original project manager of the mission, “Galileo keep the spacecraft operational from a distance of was a way of demonstrating . just what U.S. nearly half a billion miles, enabling one of the most technology was capable of doing.” An engineer impressive voyages of scientific discovery. on the Galileo team expressed more personal * * * * * sentiments when she said, “I had never been a Michael Meltzer is an environmental part of something with such great scope . To scientist who has been writing about science know that the whole world was watching and and technology for nearly 30 years. His books hoping with us that this would work. We were and articles have investigated topics that include doing something for all mankind.” designing solar houses, preventing pollution in When Galileo lifted off from Kennedy electroplating shops, catching salmon with sonar and Space Center on 18 October 1989, it began an radar, and developing a sensor for examining Space interplanetary voyage that took it to Venus, to Michael Meltzer Michael Shuttle engines. -
7 Planetary Rings Matthew S
7 Planetary Rings Matthew S. Tiscareno Center for Radiophysics and Space Research, Cornell University, Ithaca, NY, USA 1Introduction..................................................... 311 1.1 Orbital Elements ..................................................... 312 1.2 Roche Limits, Roche Lobes, and Roche Critical Densities .................... 313 1.3 Optical Depth ....................................................... 316 2 Rings by Planetary System .......................................... 317 2.1 The Rings of Jupiter ................................................... 317 2.2 The Rings of Saturn ................................................... 319 2.3 The Rings of Uranus .................................................. 320 2.4 The Rings of Neptune ................................................. 323 2.5 Unconfirmed Ring Systems ............................................. 324 2.5.1 Mars ............................................................... 324 2.5.2 Pluto ............................................................... 325 2.5.3 Rhea and Other Moons ................................................ 325 2.5.4 Exoplanets ........................................................... 327 3RingsbyType.................................................... 328 3.1 Dense Broad Disks ................................................... 328 3.1.1 Spiral Waves ......................................................... 329 3.1.2 Gap Edges and Moonlet Wakes .......................................... 333 3.1.3 Radial Structure ..................................................... -
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. -
Conceptual Design for a Sputter-Type Negative Ion Source Based
MOPO-03 Proceedings of ECRIS08, Chicago, IL USA CONCEPTUAL DESIGN OF A SPUTTER-TYPE NEGATIVE ION SOURCE BASED ON ELECTRON CYCLOTRON RESONANCE PLASMA HEATING O. Tarvainen and S. Kurennoy, Los Alamos National Laboratory, Los Alamos, NM 87545, U.S.A. Abstract PHYSICS ASPECTS OF H- ION BEAM A design for a negative ion source based on electron PRODUCTION cyclotron resonance plasma heating and ionization by Modern H- ion sources are based on two important ion surface sputtering is presented. The plasma chamber of formation processes, the volume [3] and the surface [4] the source is an rf-cavity designed for TE111 eigenmode at production. The relative importance of these processes 2.45 GHz. The desired mode is excited with a loop depends on the detailed design of the ion source. antenna. The ionization process takes place on a cesiated The volume production of H- is generally accepted to surface of a biased converter electrode (cathode). The ion be due to dissociative attachment (DA) of low energy beam is further “self-extracted” through the plasma electrons to rovibrationally (ν,,) excited molecules. Two region. The magnetic field of the source is optimized for electron populations are needed in order to optimize the both, plasma generation by electron cyclotron resonance volume production process: hot electrons (few eV) heating, and beam extraction. The source can be used for creating the excited molecular states i.e. ehot + H2 Æ e + a production of a variety of negative ions ranging from v’’ H2 (v’’ > 5) and cold electrons (less than 1 eV) hydrogen to heavy ions. -
Moon Chosen Free
FREE MOON CHOSEN PDF P. C. Cast | 608 pages | 24 Oct 2016 | St Martin's Press | 9781250125781 | English | New York, United States How Far is the Moon? | Moon Facts Moons and rings are among the most fascinating objects in our solar system. Before the Space Race of the s, astronomers knew that Earth, Mars, Jupiter, Saturn, Moon Chosen, and Neptune had moons; at that time, only Saturn was known to have rings. With the advent of better telescopes and space-based probes that could fly to distant worlds, scientists began to discover many more moons and rings. Moons and rings are typically categorized as "natural satellites" that orbit other worlds. It's not even the largest one. Jupiter's moon Ganymede has that honor. And in addition to the moons orbiting planets, nearly asteroids are known to have moons of their own. The technical term is "natural satellite", which differentiates them from the man-made satellites launched into space by space Moon Chosen. There are dozens of these natural satellites throughout the solar system. Different moons have different origin stories. However, Mars's moons Moon Chosen to be captured asteroids. Moon materials range from rocky material to icy bodies and mixtures of both. Earth's moon is made of rock Moon Chosen volcanic. Mars's moons are the same material as rocky asteroids. Jupiter's moons Moon Chosen largely icy, but with rocky cores. The exception is Io, which is a completely rocky, highly volcanic world. Saturn's moons are mostly ice with rocky cores. Its largest moon, Titan, is predominantly rocky with an icy surface. -
Stardust Comet Flyby
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Stardust Comet Flyby Press Kit January 2004 Contacts Don Savage Policy/Program Management 202/358-1727 NASA Headquarters, Washington DC Agle Stardust Mission 818/393-9011 Jet Propulsion Laboratory, Pasadena, Calif. Vince Stricherz Science Investigation 206/543-2580 University of Washington, Seattle, WA Contents General Release ……………………………………......………….......................…...…… 3 Media Services Information ……………………….................…………….................……. 5 Quick Facts …………………………………………..................………....…........…....….. 6 Why Stardust?..................…………………………..................………….....………......... 7 Other Comet Missions ....................................................................................... 10 NASA's Discovery Program ............................................................................... 12 Mission Overview …………………………………….................……….....……........…… 15 Spacecraft ………………………………………………..................…..……........……… 25 Science Objectives …………………………………..................……………...…........….. 34 Program/Project Management …………………………...................…..…..………...... 37 1 2 GENERAL RELEASE: NASA COMET HUNTER CLOSING ON QUARRY Having trekked 3.2 billion kilometers (2 billion miles) across cold, radiation-charged and interstellar-dust-swept space in just under five years, NASA's Stardust spacecraft is closing in on the main target of its mission -- a comet flyby. "As the saying goes, 'We are good to go,'" said project manager Tom Duxbury at NASA's Jet -
Heliophysics Community of Practice for Teachers
Heliophysics Community of Practice for Teachers • A multi-mission effort currently led by THEMIS-ARTEMIS Education/Public Outreach (E/PO) and supported by Van Allen Probes and IBEX, with facilitation from the Heliophysics E/PO Forum. • A nationwide community of middle and high school teachers who work together to design and implement an active, collaborative, supportive network of educators who are interested in teaching Sun-Earth science. • Began one year ago with teachers from Hawaii, Alaska, Puerto Rico, and the Continental US. • Currently growing the community to include a wider network of teachers and empowering the original core instructors to take on greater leadership roles within the community. Structure: • Monthly meetings with a face to face virtual experience, archived for later review • Science lectures- Solar Dynamics Observatory, Van Allen Probes, MAVEN, others ??? • Classroom activity ideas shared by NASA E/PO specialists and teachers • Sharing of ideas about best practices for teaching Heliophysics • Multi-day Online Community Retreat • Community Workspace “Come Out and Play!” …..How You Can Get Involved: • Opportunity to Share Your Science- Teachers have said that hearing directly from scientists is one of the most valuable aspects of their experience in the Community of Practice. • Tell others- Let the NASA community know about the success of this program, we are excited about our growth and success and hope funding support will continue. • Ideas for including students in authentic research experiences using your data? Let us know! • Other ideas? . -
The Van Allen Probes' Contribution to the Space Weather System
L. J. Zanetti et al. The Van Allen Probes’ Contribution to the Space Weather System Lawrence J. Zanetti, Ramona L. Kessel, Barry H. Mauk, Aleksandr Y. Ukhorskiy, Nicola J. Fox, Robin J. Barnes, Michele Weiss, Thomas S. Sotirelis, and NourEddine Raouafi ABSTRACT The Van Allen Probes mission, formerly the Radiation Belt Storm Probes mission, was renamed soon after launch to honor the late James Van Allen, who discovered Earth’s radiation belts at the beginning of the space age. While most of the science data are telemetered to the ground using a store-and-then-dump schedule, some of the space weather data are broadcast continu- ously when the Probes are not sending down the science data (approximately 90% of the time). This space weather data set is captured by contributed ground stations around the world (pres- ently Korea Astronomy and Space Science Institute and the Institute of Atmospheric Physics, Czech Republic), automatically sent to the ground facility at the Johns Hopkins University Applied Phys- ics Laboratory, converted to scientific units, and published online in the form of digital data and plots—all within less than 15 minutes from the time that the data are accumulated onboard the Probes. The real-time Van Allen Probes space weather information is publicly accessible via the Van Allen Probes Gateway web interface. INTRODUCTION The overarching goal of the study of space weather ing radiation, were the impetus for implementing a space is to understand and address the issues caused by solar weather broadcast capability on NASA’s Van Allen disturbances and the effects of those issues on humans Probes’ twin pair of satellites, which were launched in and technological systems. -
Sputter Coating Technical Brief
Sputter Coating Technical Brief Document Number TB-SPUTTER Issue 2 (01/02) Introduction HP000107 Quorum Technologies Ltd main sales office: South Stour Avenue Ashford Kent U.K. Tel: ++44(0) 1233 646332 TN23 7RS Fax: ++44(0) 1233 640744 Email: [email protected] http:///www.quorumtech.com For further information regarding any of the other products designed and manufactured by Quorum Technologies, contact your local representative or directly to Quorum Technologies at the address above. Carbon and sputter coaters Plasma reactor for ashing and etching High vacuum bench top evaporators Cryo-SEM preparation systems Critical point dryers Freeze dryers for electron microscopy Service and Spares Disclaimer The components and packages described in this document are mutually compatible and guaranteed to meet or exceed the published performance specifications. No performance guarantees, however, can be given in circumstances where these component packages are used in conjunction with equipment supplied by companies other than Quorum Technologies. Quorum Technologies Limited, Company No. 04273003 Registered office: Unit 19, Charlwoods Road, East Grinstead, West Sussex, RH19 2HL, UK TB-SPUTTER Contents Contents Chapter 1 - Introduction .......................................................................................... 4 Chapter 2 - Gaseous Condition .............................................................................. 5 Chapter 3 - Glow Discharge ................................................................................... -
A Self-Sputtering Ion Source: a New Approach to Quiescent Metal Ion Beams
Lawrence Berkeley National Laboratory Lawrence Berkeley National Laboratory Title A self-sputtering ion source: A new approach to quiescent metal ion beams Permalink https://escholarship.org/uc/item/24w7z1p2 Author Oks, Efim M. Publication Date 2010-03-31 Peer reviewed eScholarship.org Powered by the California Digital Library University of California Presented at the International Conference on Ion Sources on September 24, 2009 and submitted for publication to Review of Scientific Instruments received September 3, 2009, accepted November 13, 2009 A self-sputtering ion source: A new approach to quiescent metal ion beams Efim Oks1 and André Anders2* 1High Current Electronics Institute, Russian Academy of Sciences, 2/3 Academichesky Ave., Tomsk 634055, Russia 2Lawrence Berkeley National Laboratory, 1 Cyclotron Road, Berkeley, California 94720, USA *corresponding author, email [email protected] rev. version of November 05, 2009 ACKNOWLEDGMENT The work was supported by the US Department of Energy under Contract No DE-AC02-05CH11231 with the Lawrence Berkeley National Laboratory. DISCLAIMER This document was prepared as an account of work sponsored in part by the United States Government. While this document is believed to contain correct information, neither the United States Government nor any agency thereof, nor The Regents of the University of California, nor any of their employees, makes any warranty, express or implied, or assumes any legal responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by its trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof, or The Regents of the University of California. -
+ 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