The Jupiter Magnetospheric Orbiter and the Trojan Asteroid Explorer in EJSM (Europa Jupiter System Mission)
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Current Status of the EJSM Jupiter Europa Orbiter Flagship Mission Design
Current Status of the EJSM Jupiter Europa Orbiter Flagship Mission Design Presentation to the International workshop: “Europa lander: science goals and experiments” 2/09 Presented by: Karla B. Clark EJSM–JEO Study Manager Jet Propulsion Laboratory California Institute of Technology Jupiter Europa Orbiter The NASA Element of the Europa Jupiter System Mission EJSM Baseline Mission Overview • NASA & ESA share mission leadership • Two independently launched and operated flight systems with complementary payloads – Jupiter Europa Orbiter (JEO): NASA-led mission element – Jupiter Ganymede Orbiter (JGO): ESA-led mission element • Mission Timeline – Nominal Launch: 2020 – Jovian system tour phase: 2–3 years – Moon orbital phase: 6–12 months – End of Prime Missions: 2029 • ~10–11 Instruments on each flight system, including Radio Science 2/8/08 Predecisional, For Planning Purposes Only 2 JGO Baseline Mission Overview • ESA-led portion of EJSM • Objectives: Jupiter System, Callisto, Ganymede • Launch vehicle: Arianne 5 • Power source: Solar Arrays • Mission timeline: – Launch: 2020 • Uses 6-year Venus-Earth-Earth gravity assist trajectory – Jovian system tour phase: ~28 months Wide Angle and Medium Resolution Camera • Multiple satellite flybys V/NIR Imaging Spectrometer – 9 Ganymede – 21 Callisto (19 close flybys) EUV/FUV Imaging Spectrometer – Ganymede orbital phase: 260 days Ka-band transponder – End of prime mission: 2029 Ultra Stable Oscillator – Spacecraft final disposition: Ganymede surface impact Magnetometer • Radiation: ~85 krad behind -
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 -
(121514) 1999 UJ7: a Primitive, Slow-Rotating Martian Trojan G
A&A 618, A178 (2018) https://doi.org/10.1051/0004-6361/201732466 Astronomy & © ESO 2018 Astrophysics ? (121514) 1999 UJ7: A primitive, slow-rotating Martian Trojan G. Borisov1,2, A. A. Christou1, F. Colas3, S. Bagnulo1, A. Cellino4, and A. Dell’Oro5 1 Armagh Observatory and Planetarium, College Hill, Armagh BT61 9DG, Northern Ireland, UK e-mail: [email protected] 2 Institute of Astronomy and NAO, Bulgarian Academy of Sciences, 72, Tsarigradsko Chaussée Blvd., 1784 Sofia, Bulgaria 3 IMCCE, Observatoire de Paris, UPMC, CNRS UMR8028, 77 Av. Denfert-Rochereau, 75014 Paris, France 4 INAF – Osservatorio Astrofisico di Torino, via Osservatorio 20, 10025 Pino Torinese (TO), Italy 5 INAF – Osservatorio Astrofisico di Arcetri, Largo E. Fermi 5, 50125, Firenze, Italy Received 15 December 2017 / Accepted 7 August 2018 ABSTRACT Aims. The goal of this investigation is to determine the origin and surface composition of the asteroid (121514) 1999 UJ7, the only currently known L4 Martian Trojan asteroid. Methods. We have obtained visible reflectance spectra and photometry of 1999 UJ7 and compared the spectroscopic results with the spectra of a number of taxonomic classes and subclasses. A light curve was obtained and analysed to determine the asteroid spin state. Results. The visible spectrum of 1999 UJ7 exhibits a negative slope in the blue region and the presence of a wide and deep absorption feature centred around ∼0.65 µm. The overall morphology of the spectrum seems to suggest a C-complex taxonomy. The photometric behaviour is fairly complex. The light curve shows a primary period of 1.936 d, but this is derived using only a subset of the photometric data. -
Origin and Evolution of Trojan Asteroids 725
Marzari et al.: Origin and Evolution of Trojan Asteroids 725 Origin and Evolution of Trojan Asteroids F. Marzari University of Padova, Italy H. Scholl Observatoire de Nice, France C. Murray University of London, England C. Lagerkvist Uppsala Astronomical Observatory, Sweden The regions around the L4 and L5 Lagrangian points of Jupiter are populated by two large swarms of asteroids called the Trojans. They may be as numerous as the main-belt asteroids and their dynamics is peculiar, involving a 1:1 resonance with Jupiter. Their origin probably dates back to the formation of Jupiter: the Trojan precursors were planetesimals orbiting close to the growing planet. Different mechanisms, including the mass growth of Jupiter, collisional diffusion, and gas drag friction, contributed to the capture of planetesimals in stable Trojan orbits before the final dispersal. The subsequent evolution of Trojan asteroids is the outcome of the joint action of different physical processes involving dynamical diffusion and excitation and collisional evolution. As a result, the present population is possibly different in both orbital and size distribution from the primordial one. No other significant population of Trojan aster- oids have been found so far around other planets, apart from six Trojans of Mars, whose origin and evolution are probably very different from the Trojans of Jupiter. 1. INTRODUCTION originate from the collisional disruption and subsequent reaccumulation of larger primordial bodies. As of May 2001, about 1000 asteroids had been classi- A basic understanding of why asteroids can cluster in fied as Jupiter Trojans (http://cfa-www.harvard.edu/cfa/ps/ the orbit of Jupiter was developed more than a century lists/JupiterTrojans.html), some of which had only been ob- before the first Trojan asteroid was discovered. -
Ganymede Science Questions and Future Exploration
Planetary Science Decadal Survey Community White Paper Ganymede science questions and future exploration Geoffrey C. Collins, Wheaton College, Norton, Massachusetts [email protected] Claudia J. Alexander, Jet Propulsion Laboratory Edward B. Bierhaus, Lockheed Martin Michael T. Bland, Washington University in St. Louis Veronica J. Bray, University of Arizona John F. Cooper, NASA Goddard Space Flight Center Frank Crary, Southwest Research Institute Andrew J. Dombard, University of Illinois at Chicago Olivier Grasset, University of Nantes Gary B. Hansen, University of Washington Charles A. Hibbitts, Johns Hopkins University Applied Physics Laboratory Terry A. Hurford, NASA Goddard Space Flight Center Hauke Hussmann, DLR, Berlin Krishan K. Khurana, University of California, Los Angeles Michelle R. Kirchoff, Southwest Research Institute Jean-Pierre Lebreton, European Space Agency Melissa A. McGrath, NASA Marshall Space Flight Center William B. McKinnon, Washington University in St. Louis Jeffrey M. Moore, NASA Ames Research Center Robert T. Pappalardo, Jet Propulsion Laboratory G. Wesley Patterson, Johns Hopkins University Applied Physics Laboratory Louise M. Prockter, Johns Hopkins University Applied Physics Laboratory Kurt Retherford, Southwest Research Institute James H. Roberts, Johns Hopkins University Applied Physics Laboratory Paul M. Schenk, Lunar and Planetary Institute David A. Senske, Jet Propulsion Laboratory Adam P. Showman, University of Arizona Katrin Stephan, DLR, Berlin Federico Tosi, Istituto Nazionale di Astrofisica, Rome Roland J. Wagner, DLR, Berlin Introduction Ganymede is a planet-sized (larger than Mercury) moon of Jupiter with unique characteristics, such as being the largest satellite in the solar system, the most centrally condensed solid body in the solar system, and the only solid body in the outer solar system known to posses an internally generated magnetic field. -
Outer Planets Flagship Mission Results
Outer Planets Flagship Mission Results Curt Niebur OPF Program Scientist NASA Headquarters OPAG Meeting March 9, 2008 Study Background and Purpose • NASA and ESA are using a multistep downselection process to carefully select their next “flagship” missions – Multiple studies in this process intended to inform decisionmakers on science value, implementation risk/issues, cost and cost risk, and technology needs • Step 1 (2007): NASA and ESA operated independently of one another – PSD conducted detailed studies for several flagship missions (Europa, Titan, Enceladus, and Jovian System Observer) • AA Stern selected two of these concepts (Europa and Titan) for further study/evaluation in 2008 – ESA solicited Cosmic Vision Class L proposals • ESA selected Laplace and Tandem proposals (as well as IXO and LISA) • Step 2 (2008): NASA and ESA began a closer collaboration – Europa and Laplace concepts combined into Europa Jupiter System Mission – Titan and Tandem concepts combined into Titan Saturn System Mission • Step 3 (2009): Single concept moves forward for further work – NASA will focus on risk mitigation – ESA will conduct industry studies of 3 Class L concepts (OP, IXO, an LISA) for downselect beyond 2010 2 Organization and Implementation • Two concepts downselected for further joint NASA-ESA study in 2008 – Europa Jupiter System Mission (EJSM) consisting of a Jupiter Europa Orbiter (JEO, contributed by NASA) and a Jupiter Ganymede Orbiter (JGO, contributed by ESA) – Titan Saturn System Mission (TSSM) consisting of a Saturn Titan Orbiter -
March 21–25, 2016
FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk, -
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. -
Jupiter Magnetospheric Orbiter Trajectory Design: Reaching High Inclination in the Jovian System
Jupiter Magnetospheric Orbiter trajectory design: reaching high inclination in the Jovian system Stefano Campagnola (1), Yasuhiro Kawakatsu (2) (1)JSPS postdocrotal fellow, JAXA/ISAS, Kanagawa-ken, Sagamihara-shi, Chuo-ku, Yoshinodai 3-1-1, 252-5210, Japan, +81-50-336-23664, [email protected] (2)Associate professor, JAXA, [email protected] Abstract This paper presents the trajectory design for the Jupiter Magnetospheric Orbiter (JMO) in the Jovian system. JMO is JAXA’s contribution to the Europa Jupiter System Mission, and its science objectives include in-situ exploration of different regions of the magnetosphere and the remote sensing of the plasma torus from high latitudes. For this reason the spacecraft is initially captured into low-inclination, high-apojove orbits, and gradually increases the inclination and reduces the apojove using gravity assists. In order to minimize the mission cost and complexity, JMO avoids the high- radiation regions. At the same time, the trajectory minimizes the transfer time and the propellant mass, and maximize the final inclination to the Jupiter equator. This work analyzes the solution space of this complex multi-objective optimization problem and discusses the trade-offs by comparing two representative solutions on its Pareto front. The design approach is also presented. Keywords: Jupiter Magnetospheric Orbiter, Jovian system, multiple gravity assists,orbit plane change 1 Introduction In the last years the scientific community has become increasingly interested in the Jovian system. The scientific return from a mission devoted to the exploration of Jupiter and its environment would be enormous, addressing fundamental questions on the plasma science, and on the presence of water - and possibly life - below the surface of the moons Europa and Ganymede. -
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