Jupiter-Europa Orbiter and Jupiter Science
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LISA, the Gravitational Wave Observatory
The ESA Science Programme Cosmic Vision 2015 – 25 Christian Erd Planetary Exploration Studies, Advanced Studies & Technology Preparations Division 04-10-2010 1 ESAESA spacespace sciencescience timelinetimeline JWSTJWST BepiColomboBepiColombo GaiaGaia LISALISA PathfinderPathfinder Proba-2Proba-2 PlanckPlanck HerschelHerschel CoRoTCoRoT HinodeHinode AkariAkari VenusVenus ExpressExpress SuzakuSuzaku RosettaRosetta DoubleDouble StarStar MarsMars ExpressExpress INTEGRALINTEGRAL ClusterCluster XMM-NewtonXMM-Newton CassiniCassini-H-Huygensuygens SOHOSOHO ImplementationImplementation HubbleHubble OperationalOperational 19901990 19941994 19981998 20022002 20062006 20102010 20142014 20182018 20222022 XMM-Newton • X-ray observatory, launched in Dec 1999 • Fully operational (lost 3 out of 44 X-ray CCD early in mission) • No significant loss of performances expected before 2018 • Ranked #1 at last extension review in 2008 (with HST & SOHO) • 320 refereed articles per year, with 38% in the top 10% most cited • Observing time over- subscribed by factor ~8 • 2,400 registered users • Largest X-ray catalogue (263,000 sources) • Best sensitivity in 0.2-12 keV range • Long uninterrupted obs. • Follow-up of SZ clusters 04-10-2010 3 INTEGRAL • γ-ray observatory, launched in Oct 2002 • Imager + Spectrograph (E/ΔE = 500) + X- ray monitor + Optical camera • Coded mask telescope → 12' resolution • 72 hours elliptical orbit → low background • P/L ~ nominal (lost 4 out 19 SPI detectors) • No serious degradation before 2016 • ~ 90 refereed articles per year • Obs -
Exploration of the Jovian System by EJSM (Europa Jupiter System Mission): Origin of Jupiter and Evolution of Satellites
Trans. JSASS Aerospace Tech. Japan Vol. 8, No. ists27, pp. Tk_35-Tk_38, 2010 Topics Exploration of the Jovian System by EJSM (Europa Jupiter System Mission): Origin of Jupiter and Evolution of Satellites 1) 2) 2) 2) 3) By Sho SASAKI , Masaki FUJIMOTO , Takeshi TAKASHIMA , Hajime YANO , Yasumasa KASABA , 4) 4) 2) 2) Yukihiro TAKAHASHI , Jun KIMURA , Tatsuaki OKADA , Yasuhiro KAWAKATSU , 2) 2) 2) 2) 2) Yuichi TSUDA , Jun-ichiro KAWAGUCHI , Ryu FUNASE , Osamu MORI , Mutsuko MORIMOTO , 5) 6) 7) Masahiro IKOMA , Takeshi NAGANUMA , Atsushi YAMAJI , 8) 9) Hauke HUSSMANN , Kei KURITA and JUPITER WORKING GROUP 1)National Astronomical Observatory of Japan, Oshu, Japan 2)The Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan 3)Tohoku University, Sendai, Japan 4)Hokkaido University, Sapporo, Japan 5)Tokyo Institute of Technology, Tokyo, Japan 6)Hiroshima University, Higashi-Hiroshima, Japan 7)Kyoto University, Kyoto, Japan 8)German Aerospace Center, Berlin, Germany 9)Earthquake Research Institute, The University of Tokyo, Tokyo, Japan (Received July 16th, 2009) EJSM (Europa Jupiter System Mission) is a planned Jovian system mission with three spacecraft aiming at coordinated observations of the Jovian satellites especially Europa and the magnetosphere, atmosphere and interior of Jupiter. It was formerly called "Laplace" mission. In October 2007, it was selected as one of future ESA scientific missions Cosmic Vision (2015-2025). From the beginning, Japanese group is participating in the discussion process of the mission. JAXA will take a role on the magnetosphere spinner JMO (Jupiter Magnetosphere Orbiter). On the other hand, ESA will take charge of JGO (Jupiter Ganymede Orbiter) and NASA will be responsible for JEO (Jupiter Europa Orbiter). -
From the Moon to the Moons: Encedalus, Ganymede and Europa
Journal of Cosmology, 2010, Vol 5, pages xxx In PRESS Cosmology, January 13, 2010 From the Moon to the Moons: Encedalus, Ganymede and Europa. The Search for Life and Reliable Biomarkers J. Chela-Flores, Ph.D., The Abdus Salam ICTP, Strada Costiera 11, 34014 Trieste, Italia, and Instituto de Estudios Avanzados, IDEA, Caracas 1015A, República Bolivariana de Venezuela Abstract The recent renewal of interest in exploring the Moon has led to further novel possibilities for the exploration of the Solar System. It is in the outer Solar System where the biggest challenges await our efforts, both in the development of instrumentation and in the clarification of the biosignatures that should be clear indications of life, as opposed to non-life signals. We argue that in the present-day larger scope of cosmology we can undertake one of the most important missions of the space sciences within our own solar system, namely the search for and discovery of a second genesis. This may be accomplished by landing on Europa's surface. We conclude that the implementation of penetrators in future exploration of the outer solar system is worthy of all the financial and technical support that will be needed, both at the national, as well as at the international level. Keywords: Astrobiology, instrumentation, exploration of the solar system, Europa, Enceladus, Biosignatures 1. Introduction It seems appropriate for a journal devoted to cosmology to encompass the field of astrobiology and to move beyond the "anthropic principle" of quantum physics, the standard astroparticle physics and astrophysics that dominate the field of classical cosmology. -
Title: Exploration of Europa Cynthia B
Title: Exploration of Europa Cynthia B. Phillips1, D. L. Blaney2, R. T. Pappalardo2, H. Hussman3, G. Collins4, R. M. Mastrapa1, J. F. Cooper5, R. Greeley6, J. B. Dalton2, T. A. Hurford5, E. B. Bierhaus7, F. Nimmo8, D. A. Williams6, D. A. Senske2, W. B. McKinnon9 1SETI Institute, 2NASA JPL/Caltech, 3DLR Institute of Planetary Research, Berlin, 4Wheaton College, 5NASA Goddard, 6Arizona State University, 7Lockheed Martin Corporation, 8 Univ. Calif. Santa Cruz, 9Washington University in St. Louis Corresponding Author: Cynthia B. Phillips Carl Sagan Center for the Study of Life in the Universe SETI Institute 515 N. Whisman Rd. Mountain View, CA 94043 [email protected] 650-810-0230 1. Introduction Data from the Galileo spacecraft revealed that Europa's icy surface likely hides a global subsurface ocean with a volume nearly three times that of Earth's oceans. The existence of liquid water in the outer solar system was once thought a remote possibility, but the combination of geological, gravitational, and magnetic field observations and theory make it appear likely that liquid water exists beneath Europa's icy surface. It is now recognized that oceans may exist within many large icy moons and potentially even within icy dwarf planets, but Europa's inferred thin ice shell, potentially active surface- ocean and ocean-silicate mantle exchange, and chemical resources from surface irradiation elevate its priority for astrobiological exploration. A Europa mission is the first step in understanding the potential for icy satellites as abodes for life. Many unanswered questions remain following the Galileo mission. How thick is the ice shell? Is Europa currently geologically active? How does the ocean interact with the ice shell and with the underlying rocky layer? What is the composition of Europa’s surface and ocean? Are there organic or inorganic biosignatures? These questions can only be answered by a new mission to Europa and the Jupiter system. -
Leonid Gurvits JIVE and TU Delft June 3, 2021 ©Cristian Fattinanzi Piter Y Moons Xplorer
Leonid Gurvits JIVE and TU Delft June 3, 2021 ©Cristian Fattinanzi piter y moons xplorer Why a mission to Jupiter? Bits of history Mission challenges Where radio astronomy comes in • ~2000–2005: success of Cassini and Huygens missions (NASA, ESA, ASI) • 2006: Europlanet meeting in Berlin – “thinking aloud” on a Jovian mission • 2008: ESA-NASA jointly exploring a mission to giant planets’ satellites • ESA "Laplace" mission proposal (Blanc et al. 2009) • ESA Titan and Enceladus Mission (TandEM, Coustenis et al., 2009) • NASA Titan Explorer • 2009: two joint (ESA+NASA) concepts selected for further studies: • Europa Jupiter System Mission (EJSM) • Titan Saturn System Mission (TSSM: Coustenis et al., 2009) • 2010: EJSM-Laplace selected, consisting of two spacecraft: • ESA’s Jupiter Ganymede Orbiter (JGO) • NASA’s Jupiter Europa Orbiter (JEO) • 2012: NASA drops off; EJSM-Laplace/JGO becomes JUICE • 2013: JUICE payload selection completed by ESA; JUICE becomes an L-class mission of ESA’s Vision 2015-2025 • 2015: NASA selects Europa Clipper mission (Pappalardo et al., 2013) Voyager 1, 1979 ©NASA HOW DOES IT SEARCH FOR ORIGINS & WORK? LIFE FORMATION HABITABILITY Introduction Overarching questions JUICE JUICE Science Themes • Emergence of habitable worlds around gas giants • Jupiter system as an archetype for gas giants JUICE concept • European-led mission to the Jovian system • First orbiter of an icy moon • JGO/Laplace scenario with two Europa flybys and moderate-inclination phase at Jupiter • Science payload selected in Feb 2013, fully compatible -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology -
Cosmic Visions
Declaration of Interest in science instrumentation in response to the Announcement of Opportunity for Europa Jupiter System Mission (EJSM/Laplace) Cosmic Vision Candidate Surface Element Penetrators Proposers: Robert Gowen1, Alan Smith1, Richard Ambrosi6, Olga Prieto Ballesteros16, Simeon Barber2, Dave Barnes11, Chris Braithwaite9, John Bridges6, Patrick Brown5, Phillip Church10, Glyn Collinson1, Andrew Coates1, Gareth Collins5, Ian Crawford3, Veronica Dehant21, Michele Dougherty5, Julian Chela--Flores17, Dominic Fortes7, George Fraser6, Yang Gao4, Manuel Grande11, Andrew Griffiths1, Peter Grindrod7, Leonid Gurvits19, Axel Hagermann2, Toby Hopf5, Hauke Hussmann13, Ralf Jaumann13, Adrian Jones7, Geraint Jones1, Katherine Joy3, Ozgur Karatekin21, Günter Kargl20, Antonella Macagnano14, Anisha Mukherjee5, Peter Muller1, Ernesto Palomba12, Tom Pike5, Bill Proud9, Derek Pullen6, Francois Raulin15, Lutz Richter18, Simon Sheridan2, Mark Sims6, Frank Sohl13, Joshua Snape7, Jon Sykes6, Vincent Tong3, Tim Stevenson6, Lionel Wilson2, Ian Wright2, John Zarnecki2. Affiliations: 1:Mullard Space Science Laboratory, University College London, UK., 2:Planetary and Space Sciences Research Institute, Open University, UK. 3:Birkbeck College, University of London, UK. 4:Surrey Space Centre, Guildford, UK. 5:Imperial College, London, UK. 6:University of Leicester, UK. 7:University College London, UK. 8:University of Lancaster, UK. 9: Cavendish Laboratory, Cambridge, UK. 10:QinetiQ, 11: University of Aberystwyth, UK. 12: Istituto di Fisica dello Spazio Interplanetario-INAF, Roma, Italy. 13: DLR, Berlin, Germany. 14:Institute of Microelectronics and Microsystem -CNR, Roma, Italy. 15: Université Paris, France. 16: Centro de Astrobiologia-INTA-CSIC, España. 17: Abdus Salam International Centre for Theoretical Physics (ICTP), Trieste, Italy. 18: DLR, Bremen, Germany. 19: Joint Institute for VLBI in Europe (JIVE), Dwingeloo, The Netherlands. 20: IAF, Space Research Institute, Graz, Austria. -
EJSM/Jupiter Europa Orbiter Design and Status Karla B
EJSM/Jupiter Europa Orbiter Design and Status Karla B. Clark NASA–JEO Study Lead Jet Propulsion Laboratory California Institute of Technology January 18, 2010 3rd EJSM Instrument Workshop Jupiter Europa Orbiter The NASA Element of the Europa Jupiter System Mission For Discussion and Planning Purposes Only © 2010. All rights reserved. JEO Baseline Mission Overview • Objectives: Jupiter System, Europa • Launch vehicle: Atlas V 551 • Power source: 5 MMRTG • Mission timeline: – Launch: 2018 to 2022, nominally 2020 • Uses 6-year Venus-Earth-Earth gravity assist trajectory – Jovian system tour phase: 30 months • Multiple satellite flybys: 4 Io, 6 Ganymede, 6 Europa, and 9 Callisto – Europa orbital phase: 9 months – End of prime mission: 2029 – Spacecraft final disposition: Europa surface impact • 11 Instruments, including radio science • Optimized for science, cost, and risk • Radiation dose: 2.9 Mrad (behind 100 mils of Al) – Handled using a combination of rad-hard parts and tailored component shielding – Key rad-hard parts are available, with the required heritage – Team is developing and providing design information and approved parts list for prospective suppliers of components, including instruments 1/18/10 For Discussion and Planning Purposes Only 2 Mission Radiation Challenge Launch 2020 (Si))* (Mrad Point Launch Design 2020 Launch Launch 2011 Radiation 1989 * Behind 100 mil (2.5mm) of aluminum Estimated radiation dose levels unprecedented for NASA/ESA missions 1/18/10 For Discussion and Planning Purposes Only 3 JEO Mission Design Overview -
Cassini–Huygens, New Horizons, and the Galileo Orbiter
Outline • Characteristics of Jupiter • Exploration of Jupiter • Data and Images from JUNO spacecraft 2 Characteristics of Jupiter • Orbit Size Around Sun Scientific Notation: 7.7834082 × 108 푘푚 Astronomical Units: 5.2028870 퐴. 푈. • Mass Scientific Notation: 1.8981 × 1027 푘푔 (By Comparison: 317.828 × Earth) • Equatorial Radius Scientific Notation: 6.9911 × 104 푘푚 (By Comparison: 10.9733 × Earth) • Volume Scientific Notation: 1.43128 × 1015 푘푚3 (By Comparison: 1321.337 × Earth) • Density Scientific Notation: 1.3056 × 104 푚/푠 (By Comparison: 0.438 × Earth) 1 day (Jupiter) = 9.92 hours (Earth) 1 year (Jupiter) = 11.86 years (Earth) Number of moons: 69 • Features Ring • Features Strong magnetic field • Features Red spot Exploration of Jupiter Exploration of Jupiter Exploration of Jupiter Mission type: flyby Pioneer 10&11 (先鋒者 10&11 ) Time: Pioneer 10 1972 launch 1973 flyby Pioneer 11 1973 launch 1974 flyby Launched on March 2, 1972, Pioneer 10 was the first spacecraft to pass through the asteroid belt and the first to make direct observations and obtain close-up images of Jupiter. Pioneer 11 was launched on a similar trajectory on April 5, 1973, like Pioneer 10 Pioneer 10 was the first spacecraft to pass through the asteroid belt, considered a spectacular achievement, and then headed toward Jupiter. Pioneer 10 also charted Jupiter’s intense radiation belts, located the planet’s magnetic field, and established that Jupiter is predominantly a liquid planet. Exploration of Jupiter Mission type: orbiter Time: 1989 launch 1995 Orbital insertion Galileo In October 1989, Galileo was launched from the cargo bay of the Space Shuttle Atlantis Galileo didn't have enough fuel to fly directly to Jupiter, but the spacecraft could borrow enough energy from Venus and Earth to make the long journey. -
Direct Exploration of Outer Solar System Using Solar Power Sail OKEANOS
Direct Exploration of Outer Solar System using Solar Power Sail OKEANOS *Osamu Mori1, Masanori Matsushita1, Ahmed Kiyoshi Sugihara1, Yuki Takao5, Takanao Saiki1, Yuichi Tsuda1, Tatsuaki Okada1, Takahiro Iwata1, Hajime Yano1 and Junichiro Kawaguchi1 1 JAXA, 2 The University of Tokyo 1 Exploration Missions: Past Trends 1. RTG with Chemical Propulsion Due to two factors, sample return missions beyond the asteroid belt is difficult. - The power obtainable through solar panels reduce drastically beyond the asteroid belt. - Larger ΔV is required to reach these distances. Galileo, Cassini and New Horizons have relied on RTG to generate the electric power, while chemical propulsion was used to generate ΔV. Spacecraft power and propulsion systems Power subsystem Propulsion subsystem Mission RTG Galileo, Cassini, New Horizons Chemical propulsion Rosetta, Juno Solar panel Ion thrusters Hayabusa, Hayabusa2 Solar power sail OKEANOS High-Isp Ion thrusters Nuclear power generator 2 Exploration Missions: Past Trends 2. Solar Panel with Chemical Propulsion As the performance of solar cells improved, Rosetta and Juno were able to instead rely on solar panel. Spacecraft power and propulsion systems Power subsystem Propulsion subsystem Mission RTG Galileo, Cassini, New Horizons Chemical propulsion Not sample return Rosetta, Juno Solar panel Ion thrusters Hayabusa, Hayabusa2 Solar power sail Solar power sail-craft HiGh-Isp Ion thrusters Nuclear power Generator 3 Exploration Missions: Past Trends 3. Solar Panel with Ion Thrusters Hayabusa and Hayabusa2 were -
Review Article Application Prospect of Fission-Powered Spacecraft in Solar System Exploration Missions
AAAS Space: Science & Technology Volume 2021, Article ID 5245136, 15 pages https://doi.org/10.34133/2021/5245136 Review Article Application Prospect of Fission-Powered Spacecraft in Solar System Exploration Missions Y. Xia,1,2 J. Li,1 R. Zhai,1 J. Wang,1,2 B. Lin,1 and Q. Zhou3 1Beijing Institute of Spacecraft Environment Engineering, Beijing, China 2Science and Technology on Reliability and Environmental Engineering Laboratory, Beijing, China 3Institute of Nuclear and New Energy Technology of Tsinghua University, The Key Laboratory of Advanced Reactor Engineering and Safety, Ministry of Education, Beijing, China Correspondence should be addressed to Q. Zhou; [email protected] Received 9 June 2020; Accepted 29 July 2020; Published 26 February 2021 Copyright © 2021 Y. Xia et al. Exclusive Licensee Beijing Institute of Technology Press. Distributed under a Creative Commons Attribution License (CC BY 4.0). Fission power is a promising technology, and it has been proposed for several future space uses. It is being considered for high- power missions whose goal is to explore the solar system and even beyond. Space fission power has made great progress when NASA’s 1 kWe Kilowatt Reactor Using Stirling TechnologY (KRUSTY) prototype completed a full power scale nuclear test in 2018. Its success stimulated a new round of research competition among the major space countries. This article reviews the development of the Kilopower reactor and the KRUSTY system design. It summarizes the current missions that fission reactors are being considered as a power and/or propulsion source. These projects include visiting Jupiter and Saturn systems, Chiron, and Kuiper belt object; Neptune exploration missions; and lunar and Mars surface base missions. -
Planetary Science Decadal Survey: Jupiter Europa Orbiter Component of EJSM
National Aeronautics and Space Administration Mission Concept Study PlanetaryPlanetary ScienceScience DecadalDecadal SurveySurvey JupiterJupiter EuropaEuropa OrbiterOrbiter ComponentComponent ofof EJSMEJSM ScienceScience Champion:Champion: JohnJohn SSpencerpencer ([email protected])([email protected]) NASANASA HQHQ POC:POC: CurtCurt NieburNiebur ([email protected])([email protected]) MarchMarch 20102010 www.nasa.gov Jupiter Europa Orbiter Component of EJSM 1 Data Release, Distribution, and Cost Interpretation Statements This document is intended to support the SS2012 Planetary Science Decadal Survey. The data contained in this document may not be modified in any way. Cost estimates described or summarized in this document were generated as part of a preliminary concept study, are model-based, assume a JPL in-house build, and do not constitute a commitment on the part of JPL or Caltech. References to work months, work years, or FTEs generally combine multiple staff grades and experience levels. Cost reserves for development and operations were included as prescribed by the NASA ground rules for the Planetary Science Decadal Survey. Unadjusted estimate totals and cost reserve allocations would be revised as needed in future more-detailed studies as appropriate for the specific cost-risks for a given mission concept. Jupiter Europa Orbiter Component of EJSM i Planetary Science Decadal Survey Mission Concept Study Final Report Acknowledgments ........................................................................................................