Recent Events & Science Results

Total Page:16

File Type:pdf, Size:1020Kb

Recent Events & Science Results EIRO School CERN May 2013 ESA Science Programme: Recent events & science results David Lumb Research & Scientific Support Department European Space Agency, ESTEC SCIENCE AND ROBOTIC EXPLORATION 1 EIRO School CERN May 2013 SCIENCE AND ROBOTIC EXPLORATION 2 EIRO School CERN May 2013 SCIENCE AND ROBOTIC EXPLORATION 3 Current ESA space science missions Euclid JWST Solar Orbiter BepiColombo LISA Pathfinder Gaia PROBA-2 Planck Herschel CoRoT Hinode Venus Express Suzaku Rosetta Mars Express INTEGRAL Cluster XMM-Newton Cassini-Huygens SOHO Hubble Implementation Operational 1990 1994 1998 2002 2006 2010 2014 2018 2022 4 EIRO School CERN May 2013 PROBA-2 ESA technology demonstrator / solar observatory, launched in November 2009 SCIENCE AND ROBOTIC EXPLORATION 5 EIRO School CERN May 2013 The Sun approaching solar maximum PROBA-2 SWAP daily 17.4nm images from 2 February 2010 to 26 October 2012 SCIENCE AND ROBOTIC EXPLORATION 6 EIRO School CERN May 2013 Total solar eclipse of November 13, 2012 SCIENCE AND ROBOTIC EXPLORATION 7 EIRO School CERN May 2013 Total solar eclipse of November 13, 2012 Centre: 17.4nm Fe IX (PROBA-2); middle: ground-based white-light (Lecleire); outer: LASCO C2 (SOHO) / ESA, NASA, Koutchmy SCIENCE AND ROBOTIC EXPLORATION 8 EIRO School CERN May 2013 SOHO ESA-NASA solar heliophysics observatory, launched 1995 SCIENCE AND ROBOTIC EXPLORATION 9 EIRO School CERN May 2013 Solar meridional flow Material transported from equator to poles Carries magnetic flux with it Poleward flow at ~15–20 m s–1 Operates in convective zone Related to 11 yr solar cycle Convective zone Flux carried to poles, builds up polar fields, then returns below surface Hathaway & Rightmire Radiative ApJ, 2011 zone Core Graphic: NASA MSFC Solar Physics SCIENCE AND ROBOTIC EXPLORATION 10 EIRO School CERN May 2013 First detection of return flow Return flow not previously seen Must exist for mass conservation Slower due to higher density How slow & how deep? SOHO MDI helioseismology Use supergranules as probe Cross-correlate MDI dopplergrams as function of intervening time delay Longer times correspond to larger cells, which extend deeper Equator-ward flow seen 4.6 ± 0.4 m s–1 at 70 Mm (10% R⊙) Important for dynamo models of Sun’s magnetic cycle Hathaway 2012, ApJ SCIENCE AND ROBOTIC EXPLORATION 11 EIRO School CERN May 2013 First detection of return flow Return flow not previously seen Must exist for mass conservation Slower due to higher density How slow & how deep? SOHO MDI helioseismology Use supergranules as probe Cross-correlate MDI dopplergrams as function of intervening time delay Longer times correspond to larger cells, which extend deeper corresponding to depth of 70Mm Equator-ward flow seen 4.6 ± 0.4 m s–1 at 70 Mm (10% R⊙) Important for dynamo models of Sun’s magnetic cycle Hathaway 2012, ApJ SCIENCE AND ROBOTIC EXPLORATION 12 EIRO School CERN May 2013 Cluster ESA magnetospheric physics mission, launched 2000 SCIENCE AND ROBOTIC EXPLORATION 13 EIRO School CERN May 2013 Turbulence at the reconnection scale Turbulence a ubiquitous phenomenon Thought to play key role in heating solar wind as it crosses interplanetary space Solar wind cools as it expands, but much less than expected Simulation of decaying turbulence Perpendicular to interplanetary magnetic field and direction of solar wind flow Shows evolution of small-scale sheets between larger swirls in magnetofluid Cluster observations S/C separation ~ 20 km, 450 samples s–1 Revealed existence of current sheets and energy release at very small scales Heat dissipation due to reconnection? Solar Orbiter: true closer to Sun as well? Simulations and Cluster data from Perri et al. 2012, PRL / ESA SCIENCE AND ROBOTIC EXPLORATION 14 EIRO School CERN May 2013 Turbulence at the reconnection scale Turbulence a ubiquitous phenomenon Thought to play key role in heating solar wind as it crosses interplanetary space Solar wind cools as it expands, but much less than expected Simulation of decaying turbulence Perpendicular to interplanetary magnetic field and direction of solar wind flow Shows evolution of small-scale sheets between larger swirls in magnetofluid Cluster observations S/C separation ~ 20 km, 450 samples s–1 Revealed existence of current sheets and energy release at very small scales Heat dissipation due to reconnection? Solar Orbiter: true closer to Sun as well? Simulations and Cluster data from Perri et al. 2012, PRL / ESA SCIENCE AND ROBOTIC EXPLORATION 15 EIRO School CERN May 2013 Venus Express ESA Venus planetary physics mission, launched 2005 SCIENCE AND ROBOTIC EXPLORATION 16 EIRO School CERN May 2013 A day in the life of Venus Express VEX VMC: see http://www.esa.int/Our_Activities/Space_Science/A_day_in_the_life_of_Venus_Express SCIENCE AND ROBOTIC EXPLORATION 17 EIRO School CERN May 2013 When a planet looks like a comet Magnetosphere and ionosphere of Venus as induced by the solar wind Normal solar wind dynamic pressure: Trajectory of VEX in orbit around Venus Ionosphere confined close to planet on dayside on 4 Aug 2010 in cylindrical coords √ 2 2 Ionosphere truncated and chaotic on nightside (Rcyl = Y + Z , with X, Y, Z in Venus solar orbital coordinates) Venus Express ASPERA + MAG / Wei et al. 2012, P&SS / ESA SCIENCE AND ROBOTIC EXPLORATION 18 EIRO School CERN May 2013 When a planet looks like a comet Magnetosphere and ionosphere of Venus as induced by the solar wind Normal solar wind dynamic pressure: Very low SWDP (4 Aug 2010): Ionosphere confined close to planet on dayside Ion channel opened to nightside “ ” Ionosphere truncated and chaotic on nightside Ionosphere extends into cometary tail Venus Express ASPERA + MAG / Wei et al. 2012, P&SS / ESA SCIENCE AND ROBOTIC EXPLORATION 19 EIRO School CERN May 2013 Mars Express ESA Mars planetary physics mission, launched 2003 SCIENCE AND ROBOTIC EXPLORATION 20 EIRO School CERN May 2013 MEX HRSC approaching global coverage Mosaic of 2072 HRSC swathes, covering 87.8% of planet (61.5% at < 20 m pix–1) by 30 June 2012 Mars Express HRSC, ESA / DLR / FU Berlin (G. Neukum), processed by Fred Jansen SCIENCE AND ROBOTIC EXPLORATION 21 EIRO School CERN May 2013 Mars global mineralogy I Near-infrared (1.08 μm) albedo Anhydrous nanophase ferric oxides (oxidised dusty materials) MEX OMEGA 0.36–2.5 μm spectral mapping data, January 2004 – August 2010 / Ody et al. 2012, JGR / ESA SCIENCE AND ROBOTIC EXPLORATION 22 EIRO School CERN May 2013 Mars global mineralogy II Near-infrared (1.08 μm) albedo Pyroxenes (rock-forming inosilicates, associated with igneous or metamorphic rocks) MEX OMEGA / Ody et al. 2012, JGR / ESA SCIENCE AND ROBOTIC EXPLORATION 23 EIRO School CERN May 2013 Mars global mineralogy III (in progress) Olivines (Mg,Fe)2SiO4 High grain grain size and/or high and/or high olivine abundance Low High = high in relative relative content = high in High iron and/or relatively large Olivines weather readily, so are relatively rare on surface of Mars Three different geological settings identified as olivine-bearing: Clusters of discontinuous patches on terraces around main basins: possibly related to excavated mantle ejectas Smooth inter-crater plains and smooth crater floors in southern highlands: possibly due to recent volcanic infilling Deposits in northern plains in dunes in crater floors, crater ejecta, exposed bedrock: primary olivine-rich basaltic units lie below sedimentary surface MEX OMEGA / Ody et al. 2012, JGR, Ody et al. in preparation / ESA SCIENCE AND ROBOTIC EXPLORATION 24 EIRO School CERN May 2013 Reull Vallis MEX HRSC / ESA, DLR, FU Berlin (G. Neukum) SCIENCE AND ROBOTIC EXPLORATION 25 EIRO School CERN May 2013 Reull Vallis perspective view MEX HRSC / ESA, DLR, FU Berlin (G. Neukum) SCIENCE AND ROBOTIC EXPLORATION 26 EIRO School CERN May 2013 Cassini-Huygens NASA-ESA-ASI mission to the Saturnian system and Titan in particular, launched October 1997 SCIENCE AND ROBOTIC EXPLORATION 27 EIRO School CERN May 2013 A scale-model of the Nile on Titan First example of extensive river system draining into a large sea Approximately 400 km long from headwaters to Ligeia Mare Likely filled with liquid methane-ethane: very low radar return Cassini radar imaging data taken in September 2012 / NASA, ESA, ASI SCIENCE AND ROBOTIC EXPLORATION 28 EIRO School CERN May 2013 ’ Titan s atmospheric reversal January 2010 September 2011 Reversal in global pole-to-pole circulation at the equinox Air above S pole began to cool and sink very soon after equinox; vortex appeared Enhancement of trace gases in high atmosphere due to photochemical reactions Vertical circulation results Thick atmosphere extends much higher than previously thought, up to ~ 600 km Titan south polar vortex, June 2012 / Cassini ISS Cassini CIRS / Teanby et al. 2012, Nature / NASA, ESA, ASI SCIENCE AND ROBOTIC EXPLORATION 29 EIRO School CERN May 2013 Hubble Space Telescope NASA-ESA UV-optical-near-IR astrophysical observatory, launched 1990, last servicing May 2009 SCIENCE AND ROBOTIC EXPLORATION 30 EIRO School CERN May 2013 Hubble eXtremely Deep Field 10 years of ACS + WFC3 VIS data on HUDF field / Illingworth et al. 2012 / NASA, ESA SCIENCE AND ROBOTIC EXPLORATION 31 EIRO School CERN May 2013 Hubble Ultra Deep Field 2012 Deeper WFC3 IR data on HUDF / Ellis et al. 2013, ApJL / NASA, ESA SCIENCE AND ROBOTIC EXPLORATION 32 EIRO School CERN May 2013 Very high-z galaxy candidates HUDF 2012 WFC3/IR, Ellis et al. 2013, ApJL / NASA, ESA SCIENCE AND ROBOTIC EXPLORATION 33 EIRO School CERN May 2013 Hubble Frontier Fields Abell 370 / HST ACS B,R,I / NASA, ESA, HST SM4 ERO team, ST-ECF SCIENCE AND ROBOTIC EXPLORATION 34 EIRO School CERN May 2013 Hubble Frontier Fields MACS J0416.1–2403 840 orbits of DDT time in 2013–2015 on six strong lensing galaxy clusters + parallel empty fields Cluster + parallel fields: ACS/WFC F435W, F606W, F814W to 3σ point source ~ AB 28.7–29.1 Cluster only: WFC3/IR F105W, F125W, F140W, F160W to 3σ point source ~ AB 28.6–29.0 ’ Intrinsic science on galaxy evolution at high-z + broad legacy for JWST, ELT s, ALMA, VLA, etc.
Recommended publications
  • Juno Telecommunications
    The cover The cover is an artist’s conception of Juno in orbit around Jupiter.1 The photovoltaic panels are extended and pointed within a few degrees of the Sun while the high-gain antenna is pointed at the Earth. 1 The picture is titled Juno Mission to Jupiter. See http://www.jpl.nasa.gov/spaceimages/details.php?id=PIA13087 for the cover art and an accompanying mission overview. DESCANSO Design and Performance Summary Series Article 16 Juno Telecommunications Ryan Mukai David Hansen Anthony Mittskus Jim Taylor Monika Danos Jet Propulsion Laboratory California Institute of Technology Pasadena, California National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California October 2012 This research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not constitute or imply endorsement by the United States Government or the Jet Propulsion Laboratory, California Institute of Technology. Copyright 2012 California Institute of Technology. Government sponsorship acknowledged. DESCANSO DESIGN AND PERFORMANCE SUMMARY SERIES Issued by the Deep Space Communications and Navigation Systems Center of Excellence Jet Propulsion Laboratory California Institute of Technology Joseph H. Yuen, Editor-in-Chief Published Articles in This Series Article 1—“Mars Global
    [Show full text]
  • Asteroseismology with Corot, Kepler, K2 and TESS: Impact on Galactic Archaeology Talk Miglio’S
    Asteroseismology with CoRoT, Kepler, K2 and TESS: impact on Galactic Archaeology talk Miglio’s CRISTINA CHIAPPINI Leibniz-Institut fuer Astrophysik Potsdam PLATO PIC, Padova 09/2019 AsteroseismologyPlato as it is : a Legacy with CoRoT Mission, Kepler for Galactic, K2 and TESS: impactArchaeology on Galactic Archaeology talk Miglio’s CRISTINA CHIAPPINI Leibniz-Institut fuer Astrophysik Potsdam PLATO PIC, Padova 09/2019 Galactic Archaeology strives to reconstruct the past history of the Milky Way from the present day kinematical and chemical information. Why is it Challenging ? • Complex mix of populations with large overlaps in parameter space (such as Velocities, Metallicities, and Ages) & small volume sampled by current data • Stars move away from their birth places (migrate radially, or even vertically via mergers/interactions of the MW with other Galaxies). • Many are the sources of migration! • Most of information was confined to a small volume Miglio, Chiappini et al. 2017 Key: VOLUME COVERAGE & AGES Chiappini et al. 2018 IAU 334 Quantifying the impact of radial migration The Rbirth mix ! Stars that today (R_now) are in the green bins, came from different R0=birth Radial Migration Sources = bar/spirals + mergers + Inside-out formation (gas accretion) GalacJc Center Z Sun R Outer Disk R = distance from GC Minchev, Chiappini, MarJg 2013, 2014 - MCM I + II A&A A&A 558 id A09, A&A 572, id A92 Two ways to expand volume for GA • Gaia + complementary photometric information (but no ages for far away stars) – also useful for PIC! • Asteroseismology of RGs (with ages!) - also useful for core science PLATO (miglio’s talk) The properties at different places in the disk: AMR CoRoT, Gaia+, K2 + APOGEE Kepler, TESS, K2, Gaia CoRoT, Gaia+, K2 + APOGEE PLATO + 4MOST? Predicon: AMR Scatter increases towards outer regions Age scatter increasestowars outer regions ExtracGng the best froM GaiaDR2 - Anders et al.
    [Show full text]
  • Multiple Star Systems Observed with Corot and Kepler
    Multiple star systems observed with CoRoT and Kepler John Southworth Astrophysics Group, Keele University, Staffordshire, ST5 5BG, UK Abstract. The CoRoT and Kepler satellites were the first space platforms designed to perform high-precision photometry for a large number of stars. Multiple systems dis- play a wide variety of photometric variability, making them natural benefactors of these missions. I review the work arising from CoRoT and Kepler observations of multiple sys- tems, with particular emphasis on eclipsing binaries containing giant stars, pulsators, triple eclipses and/or low-mass stars. Many more results remain untapped in the data archives of these missions, and the future holds the promise of K2, TESS and PLATO. 1 Introduction The CoRoT and Kepler satellites represent the first generation of astronomical space missions capable of large-scale photometric surveys. The large quantity – and exquisite quality – of the data they pro- vided is in the process of revolutionising stellar and planetary astrophysics. In this review I highlight the immense variety of the scientific results from these concurrent missions, as well as the context provided by their precursors and implications for their successors. CoRoT was led by CNES and ESA, launched on 2006/12/27,and retired in June 2013 after an irre- trievable computer failure in November 2012. It performed 24 observing runs, each lasting between 21 and 152days, with a field of viewof 2×1.3◦ ×1.3◦, obtaining light curves of 163000 stars [42]. Kepler was a NASA mission, launched on 2009/03/07and suffering a critical pointing failure on 2013/05/11. It observed the same 105deg2 sky area for its full mission duration, obtaining high-precision light curves of approximately 191000 stars.
    [Show full text]
  • Thermal Test Campaign of the Solar Orbiter STM
    46th International Conference on Environmental Systems ICES-2016-236 10-14 July 2016, Vienna, Austria Thermal Test Campaign of the Solar Orbiter STM C. Damasio1 European Space Agency, ESA/ESTEC, Noordwijk ZH, 2201 AZ, The Netherlands A. Jacobs2, S. Morgan3, M. Sprague4, D. Wild5, Airbus Defence & Space Limited,Gunnels Wood Road, Stevenage, SG1 2AS, UK and V. Luengo6 RHEA System S.A., Av. Pasteur 23, B-1300 Wavre, Belgium Solar Orbiter is the next solar-heliospheric mission in the ESA Science Directorate. The mission will provide the next major step forward in the exploration of the Sun and the heliosphere investigating many of the fundamental problems in solar and heliospheric science. One of the main design drivers for Solar Orbiter is the thermal environment, determined by a total irradiance of 13 solar constants (17500 W/m2) due to the proximity with the Sun. The spacecraft is normally in sun-pointing attitude and is protected from severe solar energy by the Heat Shield. The Heat Shield was tested separately at subsystem level. To complete the STM thermal verification, it was decided to subject to Solar orbiter platform without heat shield to thermal balance test that was performed at IABG test facility in November- December 2015 This paper will describe the Thermal Balance Test performed on the Solar Orbiter STM and the activities performed to correlate the thermal model and to show the verification of the STM thermal design. Nomenclature AU = Astronomical Unit CE = Cold Element FM = Flight Model HE = Hot Element IABG = Industrieanlagen
    [Show full text]
  • 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
    [Show full text]
  • Data Mining in the Spanish Virtual Observatory. Applications to Corot and Gaia
    Highlights of Spanish Astrophysics VI, Proceedings of the IX Scientific Meeting of the Spanish Astronomical Society held on September 13 - 17, 2010, in Madrid, Spain. M. R. Zapatero Osorio et al. (eds.) Data mining in the Spanish Virtual Observatory. Applications to Corot and Gaia. Mauro L´opez del Fresno1, Enrique Solano M´arquez1, and Luis Manuel Sarro Baro2 1 Spanish VO. Dep. Astrof´ısica. CAB (INTA-CSIC). P.O. Box 78, 28691 Villanueva de la Ca´nada, Madrid (Spain) 2 Departamento de Inteligencia Artificial. ETSI Inform´atica.UNED. Spain Abstract Manual methods for handling data are impractical for modern space missions due to the huge amount of data they provide to the scientific community. Data mining, understood as a set of methods and algorithms that allows us to recover automatically non trivial knowledge from datasets, are required. Gaia and Corot are just a two examples of actual missions that benefits the use of data mining. In this article we present a brief summary of some data mining methods and the main results obtained for Corot, as well as a description of the future variable star classification system that it is being developed for the Gaia mission. 1 Introduction Data in Astronomy is growing almost exponentially. Whereas projects like VISTA are pro- viding more than 100 terabytes of data per year, future initiatives like LSST (to be operative in 2014) and SKY (foreseen for 2024) will reach the petabyte level. It is, thus, impossible a manual approach to process the data returned by these surveys. It is impossible a manual approach to process the data returned by these surveys.
    [Show full text]
  • Characterization of the Stray Light in a Space Borne Atmospheric AOTF Spectrometer
    Characterization of the stray light in a space borne atmospheric AOTF spectrometer Korablev Oleg 1, Fedorova Anna 1, Eric Villard 2,3, Lilian Joly 4, Alexander Kiselev 1, Denis Belyaev 1, Jean-Loup Bertaux 2 1Space Research Institute (IKI), 84/32 Profsoyuznaya, 117997 Moscow, Russia; Moscow Institute of Physics and Technology, Institutsky dr. 9, 141700 Dolgoprudnyi, Russia 2LATMOS/CNRS, 78280 Guyancourt , France. 3ALMA/European Southern Observatory, Santiago, Chile 4GSMA/CNRS Univ. de Reims, Moulin de la Housse, BP 1039, 51687 Reims, France. [email protected] Abstract : Acousto-optic tunable filter (AOTF) spectrometers are being criticized for spectral leakage, distant side lobes of their spectral response (SRF) function, or the stray light. SPICAM-IR is the AOTF spectrometer in the range 1000-1700 nm with a resolving power of 1800-2200 operating on the Mars Express interplanetary probe. It is primarily dedicated to measurements of water vapor in the Martian atmosphere. SPICAM H2O retrievals are generally lower than simultaneous measurements with other instruments, the stray light suggested as a likely explanation. We report the results of laboratory measurements of water vapor in quantity characteristic for the Mars atmosphere with the Flight Spare model of SPICAM-IR. The level of the stray light is below 1.3·10 -4, and the accuracy to measure water vapor is ~0.2 pr. µm, mostly determined by measurement uncertainties and the accuracy of the synthetic modeling. We demonstrate that the AOTF spectrometer dependably measures the water abundance and can be employed as an atmospheric spectrometer. References and links 1. N. J. Chanover, D. A.
    [Show full text]
  • The EXOD Search for Faint Transients in XMM-Newton Observations
    UvA-DARE (Digital Academic Repository) The EXOD search for faint transients in XMM-Newton observations Method and discovery of four extragalactic Type I X-ray bursters Pastor-Marazuela, I.; Webb, N.A.; Wojtowicz, D.T.; van Leeuwen, J. DOI 10.1051/0004-6361/201936869 Publication date 2020 Document Version Final published version Published in Astronomy & Astrophysics Link to publication Citation for published version (APA): Pastor-Marazuela, I., Webb, N. A., Wojtowicz, D. T., & van Leeuwen, J. (2020). The EXOD search for faint transients in XMM-Newton observations: Method and discovery of four extragalactic Type I X-ray bursters. Astronomy & Astrophysics, 640, [A124]. https://doi.org/10.1051/0004-6361/201936869 General rights It is not permitted to download or to forward/distribute the text or part of it without the consent of the author(s) and/or copyright holder(s), other than for strictly personal, individual use, unless the work is under an open content license (like Creative Commons). Disclaimer/Complaints regulations If you believe that digital publication of certain material infringes any of your rights or (privacy) interests, please let the Library know, stating your reasons. In case of a legitimate complaint, the Library will make the material inaccessible and/or remove it from the website. Please Ask the Library: https://uba.uva.nl/en/contact, or a letter to: Library of the University of Amsterdam, Secretariat, Singel 425, 1012 WP Amsterdam, The Netherlands. You will be contacted as soon as possible. UvA-DARE is a service provided by the library of the University of Amsterdam (https://dare.uva.nl) Download date:02 Oct 2021 A&A 640, A124 (2020) Astronomy https://doi.org/10.1051/0004-6361/201936869 & c ESO 2020 Astrophysics The EXOD search for faint transients in XMM-Newton observations: Method and discovery of four extragalactic Type I X-ray bursters I.
    [Show full text]
  • Survey of Juno Observations in Jupiter's Plasma Disk: Density
    RESEARCH ARTICLE Survey of Juno Observations in Jupiter's Plasma Disk: 10.1029/2021JA029446 Density Key Points: E. Huscher1, F. Bagenal1 , R. J. Wilson1 , F. Allegrini2,3 , R. W. Ebert2,3 , P. W. Valek2 , • On most orbits, the densities exhibit J. R. Szalay4 , D. J. McComas4 , J. E. P. Connerney5,6 , S. Bolton2 , and S. M. Levin7 regular behavior mapping out a disk confined close to the centrifugal 1Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, CO, USA, 2Southwest Research equator 3 • Small-scale ( minutes) variabilities Institute, San Antonio, TX, USA, Department of Physics and Astronomy, University of Texas at San Antonio, San 4 5 may indicate∼ radial transport via Antonio, TX, USA, Department of Astrophysical Sciences, Princeton University, Princeton, NJ, USA, Space Research local instabilities Corporation, Annapolis, MD, USA, 6Goddard Space Flight Center, Greenbelt, MD, USA, 7Jet Propulsion Laboratory/ • Occasionally a uniformly tenuous California Institute of Technology, Pasadena, CA, USA outer disk indicates enhanced losses, perhaps triggered by solar wind compression Abstract We explore the variation in plasma conditions through the middle magnetosphere of Jupiter with latitude and radial distance using Juno-JADE measurements of plasma density (electrons, protons, Supporting Information: sulfur, and oxygen ions) surveyed on Orbits 5–26 between March 2017 and April 2020. On most orbits, the Supporting Information may be found in the online version of this article. densities exhibit regular behavior, mapping out a disk between 10 and 50 RJ (Jovian radii). In the disk, the heavy ions are confined close to the centrifugal equator which oscillates relative to the spacecraft due to the 10° tilt of Jupiter's magnetic dipole.
    [Show full text]
  • + 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
    [Show full text]
  • Status After the Venus Flybys
    Acta Astronautica 63 (2008) 68–73 www.elsevier.com/locate/actaastro The MESSENGER mission to Mercury: Status after the Venusflybys Ralph L. McNutt Jr.a,∗, Sean C. Solomonb, David G. Granta, Eric J. Finnegana, Peter D. Bedinia, the MESSENGER Team aThe Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723, USA bDepartment of Terrestrial Magnetism, Carnegie Institution of Washington, 5241 Broad Branch Road, N.W., Washington, DC 20015, USA Available online 21 April 2008 Abstract NASA’s MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) spacecraft, launched on 3 August 2004, is well into its voyage to initiate a new era in our understanding of the terrestrial planets. The mission, spacecraft, and payload are designed to answer six fundamental questions regarding the innermost planet during three flybys and a one-year-long, near-polar-orbital observational campaign. The cruise phase to date has been used to commission the spacecraft and instruments and begin the transition to automated use of the instruments with on-board, time-tagged commands. An Earth flyby one year after launch, a large propulsive maneuver in December 2005, and Venus flybys in October 2006 and June 2007 began the process of changing MESSENGER’s heliocentric motion. The second Venus flyby was also used to complete final rehearsals for Mercury flyby operations in January 2008 while coordinating observations with the European Space Agency’s Venus Express mission. The upcoming Mercury flyby will be the first since that of Mariner 10 in 1975. Along with the second and third MESSENGER flybys in October 2008 and September 2009, that flyby will provide images of the hemisphere of Mercury never seen before by spacecraft as well as the first high-resolution information on Mercury’s surface mineralogy.
    [Show full text]
  • Navigation Challenges During Exomars Trace Gas Orbiter Aerobraking Campaign
    NON-PEER REVIEW Please select category below: Normal Paper Student Paper Young Engineer Paper Navigation Challenges during ExoMars Trace Gas Orbiter Aerobraking Campaign Gabriele Bellei 1, Francesco Castellini 2, Frank Budnik 3 and Robert Guilanyà Jané 4 1 DEIMOS Space located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 2 Telespazio VEGA located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 3 ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 4 GMV INSYEN located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany Abstract The ExoMars Trace Gas Orbiter satellite spent one year in aerobraking operations at Mars, lowering its orbit period from one sol to about two hours. This delicate phase challenged the operations team and in particular the navigation system due to the highly unpredictable Mars atmosphere, which imposed almost continuous monitoring, navigation and re-planning activities. An aerobraking navigation concept was, for the first time at ESA, designed, implemented and validated on-ground and in-flight, based on radiometric tracking data and complemented by information extracted from spacecraft telemetry. The aerobraking operations were successfully completed, on time and without major difficulties, thanks to the simplicity and robustness of the selected approach. This paper describes the navigation concept, presents a recollection of the main in-flight results and gives a retrospective of the main lessons learnt during this activity. Keywords: ExoMars, Trace Gas Orbiter, aerobraking, navigation, orbit determination, Mars atmosphere, accelerometer Introduction The ExoMars program is a cooperation between the European Space Agency (ESA) and Roscosmos for the robotic exploration of the red planet.
    [Show full text]