Neutral Atom Imaging of the Solar Wind‐Magnetosphere‐Exosphere
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
ASPERA-3: Analyser of Space Plasmas and Energetic Neutral Atoms
ASPERA-3: Analyser of Space Plasmas and Energetic Neutral Atoms R. Lundin1, S. Barabash1 and the ASPERA-3 team: M. Holmström1, H. Andersson1, M. Yamauchi1, H. Nilsson1, A. Grigorev, D. Winningham2, R. Frahm2, J.R. Sharber2, J.-A. Sauvaud3, A. Fedorov3, E. Budnik3, J.-J. Thocaven3, K. Asamura4, H. Hayakawa4, A.J. Coates5, Y. Soobiah5 D.R. Linder5, D.O. Kataria5, C. Curtis6, K.C. Hsieh6, B.R. Sandel6, M. Grande7, M. Carter7, D.H. Reading7, H. Koskinen8, E. Kallio8, P. Riihela8, T. Säles8, J. Kozyra9, N. Krupp10, J. Woch10, M. Fraenz10, J. Luhmann11 , D. Brain11, S. McKenna-Lawler12, R. Cerulli-Irelli13, S. Orsini13, M. Maggi13, A. Milillo13, E. Roelof14, S. Livi14, P. Brandt14, P. Wurz15, P. Bochsler15 & A. Galli15 1 Swedish Institute of Space Physics, Box 812, S-98 128 Kiruna, Sweden 2 Southwest Research Institute, San Antonio, TX 7228-0510, USA 3 Centre d’Etude Spatiale des Rayonnements, BP-4346, F-31028 Toulouse, France 4 Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamichara, Japan 5 Mullard Space Science Laboratory, University College London, Surrey RH5 6NT, UK 6 University of Arizona, Tucson, AZ 85721, USA 7 Rutherford Appleton Laboratory, Chilton, Didcot, Oxfordshire OX11 0QX, UK 8 Finnish Meteorological Institute, Box 503, FIN-00101 Helsinki, Finland; and Department of Physical Sciences, PO Box 64, University of Helsinki, FIN-00014 Helsinki, Finland 9 Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109-2143, USA 10 Max-Planck-Institut für Sonnensystemforschung, D-37191 Katlenburg-Lindau, Germany 11 Space Science Laboratory, University of California at Berkeley, Berkeley, CA 94720-7450, USA 12 Space Technology Ltd, National University of Ireland, Maynooth, Co. -
The Ionosphere of Mars and Its Importance for Climate Evolution a Community White Paper Submitted to the 2011 Planetary Science Decadal Survey
The ionosphere of Mars and its importance for climate evolution A community white paper submitted to the 2011 Planetary Science Decadal Survey Primary authors: Paul Withers (Boston University, USA, 617 353 1531, [email protected]) Jared Espley (NASA Goddard Space Flight Center, USA) Rob Lillis (University of California Berkeley, USA) Dave Morgan (University of Iowa, USA) Co-authors: Laila Andersson (University of Colorado, Francois Leblanc (Institut Pierre-Simon USA) Laplace, France) Mathieu Barthélemy (University of Grenoble, Mark Lester (University of Leicester, UK) France) Michael Liemohn (University of Michigan, Stephen Bougher (University of Michigan, USA) USA) Jean Lilensten (University of Grenoble, David Brain (University of California France) Berkeley, USA) Janet Luhmann (University of California Stephen Brecht (Bay Area Research Berkeley, USA) Corporation, USA) Rickard Lundin (Institute of Space Physics Tom Cravens (University of Kansas, USA) (IRF), Sweden) Geoff Crowley (Atmospheric and Space Anthony Mannucci (Jet Propulsion Technology Research Associates, USA) Laboratory, USA) Justin Deighan (University of Virginia, USA) Susan McKenna-Lawlor (National University Scott England (University of California of Ireland, Ireland) Berkeley, USA) Michael Mendillo (Boston University, USA) Jeffrey Forbes (University of Colorado, USA) Erling Nielsen (Max Planck Institute for Solar Matt Fillingim (University of California System Research, Germany) Berkeley, USA) Martin Pätzold (University of Cologne, Jane Fox (Wright State University, USA) -
A Comparison Study on Thermal Control Techniques for a Nanosatellite Carrying Infrared Science Instrument
ICES-2020-15 A comparison study on thermal control techniques for a nanosatellite carrying infrared science instrument Shanmugasundaram Selvadurai1, Amal Chandran2, Sunil C Joshi3 and Teo Hang Tong Edwin 4 Nanyang Technological University, Singapore, 639798 David Valentini5 Thales Alenia Space, Cannes, 06150, France Friedhelm Olschewski6 University of Wuppertal, 42119 Wuppertal, Germany Based on current technological advancements and forecasts, nanosatellites will be used for both scientific and defense applications leveraging advantages on both development cost and development lifecycle. As nanosatellites become more capable, there is an increase in demand for high power applications which makes the missions complex from implementing a proper thermal control system (TCS) to dissipate the huge waste heat generated. One of the applications for nanosatellites is advanced infrared imaging for both scientific and military applications. ARCADE (Atmospheric coupling and Dynamics Explorer), a 27U satellite is being developed by Satellite Research Centre (SaRC) at Nanyang Technological University (NTU) for scientific objectives. The main payload AtmoLITE needs a detector cool down at -30°C and to meet this requirement, an appropriate classical TCS is chosen and described in this paper. Nanosatellites carrying infrared, cryogenic or other scientific instruments that need active cooling, should be equipped with a proper TCS within the highly constrained available volume. Another objective of this study is to compare the existing TCS for nanosatellites and adopt a suitable and efficient TCS for a scientific nanosatellite mission carrying a generic science instrument that needs an active cooling of up to 95K. TCS using Heat pipes (HP), single-phase mechanically pumped fluid loop (SMPFL), and two-phase mechanically pumped fluid loop systems (2ΦMPFL) have been extensively used only by larger satellites. -
Tailward Flow of Energetic Neutral Atoms Observed at Venus A
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 113, E00B15, doi:10.1029/2008JE003096, 2008 Click Here for Full Article Tailward flow of energetic neutral atoms observed at Venus A. Galli,1 M.-C. Fok,2 P. Wurz,1 S. Barabash,3 A. Grigoriev,3 Y. Futaana,3 M. Holmstro¨m,3 A. Ekenba¨ck,3 E. Kallio,4 and H. Gunell5 Received 31 January 2008; revised 11 April 2008; accepted 26 August 2008; published 2 December 2008. [1] The Analyzer of Space Plasma and Energetic Atoms (ASPERA-4) experiment on Venus Express provides the first measurements of energetic neutral atoms (ENAs) from Venus. The results improve our knowledge on the interaction of the solar wind with a nonmagnetized planet and they present an observational constraint to existing plasma models. We characterize the tailward flow of hydrogen ENAs observed on the nightside by providing global images of the ENA intensity. The images show a highly concentrated tailward flow of hydrogen ENAs tangential to the Venus limb around the Sun’s direction. No oxygen ENAs above the instrument threshold are detected. The observed ENA intensities are reproduced with a simple ENA model within a factor of 2, indicating that the observed hydrogen ENAs originate from shocked solar wind protons that charge exchange with the neutral hydrogen exosphere. Citation: Galli, A., M.-C. Fok, P. Wurz, S. Barabash, A. Grigoriev, Y. Futaana, M. Holmstro¨m, A. Ekenba¨ck, E. Kallio, and H. Gunell (2008), Tailward flow of energetic neutral atoms observed at Venus, J. Geophys. Res., 113, E00B15, doi:10.1029/2008JE003096. 1. Introduction boundary where the planetary ions start to dominate the plasma or as the boundary where the interplanetary mag- [2] As a part of the Venus Express (VEX) scientific netic field BIMF piles up around the ionosphere. -
Science Objectives May Be Summarized As Follows
MAGNETOSPHERE IMAGING INSTRUMENT (MIMI) 9 ON THE CASSINI MISSION TO SATURN/TITAN 2. Scientific Objectives MIMI science objectives may be summarized as follows: Saturn • Determine the global configuration and dynamics of hot plasma in the magneto- sphere of Saturn through energetic neutral particle imaging of ring current, radia- tion belts, and neutral clouds. • Study the sources of plasmas and energetic ions through in situ measurements of energetic ion composition, spectra, charge state, and angular distributions. • Search for, monitor, and analyze magnetospheric substorm-like activity at Saturn. • Determine through the imaging and composition studies the magnetosphere– satellite interactions at Saturn and understand the formation of clouds of neutral hydrogen, nitrogen, and water products. •Investigate the modification of satellite surfaces and atmospheres through plasma and radiation bombardment. • Study Titan’s cometary interaction with Saturn’s magnetosphere (and the solar wind) via high-resolution imaging and in situ ion and electron measurements. • Measure the high energy (Ee > 1 MeV, Ep > 15 MeV) particle component in the inner (L < 5 RS) magnetosphere to assess cosmic ray albedo neutron decay (CRAND) source characteristics. •Investigate the absorption of energetic ions and electrons by the satellites and rings in order to determine particle losses and diffusion processes within the mag- netosphere. • Study magnetosphere–ionosphere coupling through remote sensing of aurora and in situ measurements of precipitating energetic ions and electrons. Jupiter • Study ring current(s), plasma sheet, and neutral clouds in the magnetosphere and magnetotail of Jupiter during Cassini flyby, using global imaging and in situ mea- surements. S. M. KRIMIGIS ET AL. 10 Interplanetary • Determine elemental and isotopic composition of local interstellar medium through measurements of interstellar pickup ions. -
Cubesat-Based Science Missions for Geospace and Atmospheric Research
National Aeronautics and Space Administration NATIONAL SCIENCE FOUNDATION (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH annual report October 2013 www.nasa.gov www.nsf.gov LETTERS OF SUPPORT 3 CONTACTS 5 NSF PROGRAM OBJECTIVES 6 GSFC WFF OBJECTIVES 8 2013 AND PRIOR PROJECTS 11 Radio Aurora Explorer (RAX) 12 Project Description 12 Scientific Accomplishments 14 Technology 14 Education 14 Publications 15 Contents Colorado Student Space Weather Experiment (CSSWE) 17 Project Description 17 Scientific Accomplishments 17 Technology 18 Education 18 Publications 19 Data Archive 19 Dynamic Ionosphere CubeSat Experiment (DICE) 20 Project Description 20 Scientific Accomplishments 20 Technology 21 Education 22 Publications 23 Data Archive 24 Firefly and FireStation 26 Project Description 26 Scientific Accomplishments 26 Technology 27 Education 28 Student Profiles 30 Publications 31 Cubesat for Ions, Neutrals, Electrons and MAgnetic fields (CINEMA) 32 Project Description 32 Scientific Accomplishments 32 Technology 33 Education 33 Focused Investigations of Relativistic Electron Burst, Intensity, Range, and Dynamics (FIREBIRD) 34 Project Description 34 Scientific Accomplishments 34 Education 34 2014 PROJECTS 35 Oxygen Photometry of the Atmospheric Limb (OPAL) 36 Project Description 36 Planned Scientific Accomplishments 36 Planned Technology 36 Planned Education 37 (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH [ 1 QB50/QBUS 38 Project Description 38 Planned Scientific Accomplishments 38 Planned -
Neutral Atom Imaging of Solar Wind Interaction with the Earth and Venus M.-C
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 109, A01206, doi:10.1029/2003JA010094, 2004 Neutral atom imaging of solar wind interaction with the Earth and Venus M.-C. Fok, T. E. Moore, and M. R. Collier NASA Goddard Space Flight Center, Greenbelt, Maryland, USA T. Tanaka Department of Earth and Planetary Science, Kyushu University, Fukuoka, Japan Received 18 June 2003; revised 24 September 2003; accepted 9 October 2003; published 13 January 2004. [1] Observations from the Low-Energy Neutral Atom (LENA) imager on the Imager for Magnetopause-to-Aurora Global Exploration (IMAGE) mission have emerged as a promising new tool for studying the solar wind interaction with the terrestrial magnetosphere. Strong LENA emissions are seen from the magnetosheath during magnetic storms, especially during high solar wind dynamic pressure when the magnetopause is strongly compressed and the magnetosheath penetrates deeply into the exosphere. Venus, unlike the Earth, has no intrinsic magnetic field, so the solar wind penetrates deeply and interacts directly with its upper atmosphere. Energy transfer processes enhance atomic escape and thus play a potentially important role in the evolution of the atmosphere. We have performed simulations of the solar wind interaction with both Earth and Venus and compared the results to LENA observations at the Earth. Low-energy neutral atom emissions from Venus are calculated based on the global MHD model of Tanaka. We found the simulated energetic neutral atom (ENA) emissions from Venus magnetosheath are comparable or greater than for the Earth. The Venus ionopause is clearly seen in the modeled oxygen ENA images. This simulation work demonstrates the feasibility of remotely sensing the Venusian solar wind interaction and resultant atmospheric escape using fast neutral atom imaging. -
The Heliotail N
The Astrophysical Journal Letters, 812:L6 (7pp), 2015 October 10 doi:10.1088/2041-8205/812/1/L6 © 2015. The American Astronomical Society. All rights reserved. THE HELIOTAIL N. V. Pogorelov1,2, S. N. Borovikov2, J. Heerikhuisen1,2, and M. Zhang3 1 Department of Space Sciences, The University of Alabama in Huntsville, AL 35805, USA; [email protected] 2 Center for Space Plasma and Aeronomic Research, The University of Alabama in Huntsville, AL 35805, USA 3 Department of Physics and Space Sciences, Florida Institute of Technology, Melbourne, FL 32901, USA Received 2015 July 26; accepted 2015 September 18; published 2015 October 6 ABSTRACT The heliotail is formed when the solar wind (SW) interacts with the local interstellar medium (LISM) and is shaped by the interstellar magnetic field (ISMF). While there are no spacecraft available to perform in situ measurements of the SW plasma and heliospheric magnetic field (HMF) in the heliotail, it is of importance for the interpretation of measurements of energetic neutral atom fluxes performed by Interstellar Boundary Explorer. It has been shown recently that the orientation of the heliotail in space and distortions of the unperturbed LISM caused by its presence may explain the anisotropy in the TeV cosmic ray flux detected in air shower observations. The SW flow in the heliotail is a mystery itself because it is strongly affected by charge exchange between the SW ions and interstellar neutral atoms. If the angle between the Sun’s magnetic and rotation axes is constant, the SW in the tail tends to be concentrated inside the HMF spirals deflected tailward. -
Simulation of Energetic Neutral Atoms at Mars and a Comparison with ASPERA-3 Data
Simulation of Energetic Neutral atoms at Mars and a Comparison with ASPERA-3 data H. Gunell,∗ K. Brinkfeldt, S. Barabash, M. Holmstr¨om,† A. Ekenb¨ack, Y. Futaana, R. Lundin, H. Andersson, M. Yamauchi, and A. Grigoriev Swedish Institute of Space Physics, Kiruna, Sweden E. Kallio, T. S¨ales, P. Riihela, and W. Schmidt Finnish Meteorological Institute, Box 503 FIN-00101 Helsinki, Finland P. Brandt, E. Roelof, D. Williams, and S. Livi Applied Physics Laboratory, Johns Hopkins University, Laurel, MD 20723-6099, USA J. D. Winningham, R. A. Frahm, J. R. Sharber, and J. Scherrer Southwest Research Institute, San Antonio, TX 7228-0510, USA A. J. Coates, D. R. Linder, and D. O. Kataria Mullard Space Science Laboratory, University College London, Surrey RH5 6NT, UK Hannu E. J. Koskinen University of Helsinki, Department of Physical Sciences P.O. Box 64, 00014 Helsinki J. Kozyra Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109-2143, USA J. Luhmann Space Science Laboratory, University of California at Berkeley, Berkeley, CA 94720-7450, USA C. C. Curtis, K. C. Hsieh, and B. R. Sandel University of Arizona, Tucson, AZ 85721, USA M. Grande and M. Carter Rutherford Appleton Laboratory, Chilton, Didcot, Oxfordshire OX11 0QX, UK J.-A. Sauvaud, A. Fedorov, and J.-J. Thocaven Centre d’Etude Spatiale des Rayonnements, BP-4346, F-31028 Toulouse, France S. McKenna-Lawlor Space Technology Ireland., National University of Ireland, Maynooth, Co. Kildare, Ireland S. Orsini, R. Cerulli-Irelli, and M. Maggi Instituto di Fisica dello Spazio Interplanetari, I-00133 Rome, Italy P. Wurz and P. -
The Science Return from Venus Express the Science Return From
The Science Return from Venus Express Venus Express Science Håkan Svedhem & Olivier Witasse Research and Scientific Support Department, ESA Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands Dmitri V. Titov Max Planck Institute for Solar System Studies, Katlenburg-Lindau, Germany (on leave from IKI, Moscow) ince the beginning of the space era, Venus has been an attractive target for Splanetary scientists. Our nearest planetary neighbour and, in size at least, the Earth’s twin sister, Venus was expected to be very similar to our planet. However, the first phase of Venus spacecraft exploration (1962-1985) discovered an entirely different, exotic world hidden behind a curtain of dense cloud. The earlier exploration of Venus included a set of Soviet orbiters and descent probes, the Veneras 4 to14, the US Pioneer Venus mission, the Soviet Vega balloons and the Venera 15, 16 and Magellan radar-mapping orbiters, the Galileo and Cassini flybys, and a variety of ground-based observations. But despite all of this exploration by more than 20 spacecraft, the so-called ‘morning star’ remains a mysterious world! Introduction All of these earlier studies of Venus have given us a basic knowledge of the conditions prevailing on the planet, but have generated many more questions than they have answered concerning its atmospheric composition, chemistry, structure, dynamics, surface-atmosphere interactions, atmospheric and geological evolution, and plasma environment. It is now high time that we proceed from the discovery phase to a thorough -
THEMIS ESA First Science Results and Performance Issues
Space Sci Rev DOI 10.1007/s11214-008-9433-1 THEMIS ESA First Science Results and Performance Issues J.P. McFadden · C.W. Carlson · D. Larson · J. Bonnell · F. Mozer · V. Angelopoulos · K.-H. Glassmeier · U. Auster Received: 5 April 2008 / Accepted: 25 August 2008 © Springer Science+Business Media B.V. 2008 Abstract Early observations by the THEMIS ESA plasma instrument have revealed new details of the dayside magnetosphere. As an introduction to THEMIS plasma data, this pa- per presents observations of plasmaspheric plumes, ionospheric ion outflows, field line reso- nances, structure at the low latitude boundary layer, flux transfer events at the magnetopause, and wave and particle interactions at the bow shock. These observations demonstrate the ca- pabilities of the plasma sensors and the synergy of its measurements with the other THEMIS experiments. In addition, the paper includes discussions of various performance issues with the ESA instrument such as sources of sensor background, measurement limitations, and data formatting problems. These initial results demonstrate successful achievement of all measurement objectives for the plasma instrument. Keywords THEMIS · Magnetosphere · Magnetopause · Bow shock · Instrument performance PACS 94.80.+g · 06.20.Fb · 94.30.C- · 94.05.-a · 07.87.+v 1 Introduction The THEMIS mission provides the first multi-satellite measurements of the dayside mag- netosphere, magnetopause and bow shock utilizing a string of pearls orbit near the ecliptic plane (Angelopoulos 2008). During a 7 month coast phase, the instruments were commis- sioned and cross-calibrated while spacecraft separations were adjusted from a few hundred J.P. McFadden () · C.W. Carlson · D. -
ESA Space Weather STUDY Alcatel Consortium
ESA Space Weather STUDY Alcatel Consortium SPACE Weather Parameters WP 2100 Version V2.2 1 Aout 2001 C. Lathuillere, J. Lilensten, M. Menvielle With the contributions of T. Amari, A. Aylward, D. Boscher, P. Cargill and S.M. Radicella 1 2 1 INTRODUCTION........................................................................................................................................ 5 2 THE MODELS............................................................................................................................................. 6 2.1 THE SUN 6 2.1.1 Reconstruction and study of the active region static structures 7 2.1.2 Evolution of the magnetic configurations 9 2.2 THE INTERPLANETARY MEDIUM 11 2.3 THE MAGNETOSPHERE 13 2.3.1 Global magnetosphere modelling 14 2.3.2 Specific models 16 2.4 THE IONOSPHERE-THERMOSPHERE SYSTEM 20 2.4.1 Empirical and semi-empirical Models 21 2.4.2 Physics-based models 23 2.4.3 Ionospheric profilers 23 2.4.4 Convection electric field and auroral precipitation models 25 2.4.5 EUV/UV models for aeronomy 26 2.5 METEOROIDS AND SPACE DEBRIS 27 2.5.1 Space debris models 27 2.5.2 Meteoroids models 29 3 THE PARAMETERS ................................................................................................................................ 31 3.1 THE SUN 35 3.2 THE INTERPLANETARY MEDIUM 35 3.3 THE MAGNETOSPHERE 35 3.3.1 The radiation belts 36 3.4 THE IONOSPHERE-THERMOSPHERE SYSTEM 36 4 THE OBSERVATIONS ...........................................................................................................................