Planetary Space Weather: Scientific Aspects and Future Perspectives
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Space Weathering of Itokawa Particles: Implications for Regolith Evolution
46th Lunar and Planetary Science Conference (2015) 2351.pdf SPACE WEATHERING OF ITOKAWA PARTICLES: IMPLICATIONS FOR REGOLITH EVOLUTION. Eve L. Berger1 and Lindsay P. Keller2, 1Geocontrol Systems – Jacobs JETS contract – NASA Johnson Space Center, Houston TX 77058, [email protected], 2NASA Johnson Space Center Introduction: Space weathering processes such as tion rate of 4.1 ±1.2 × 104 tracks/cm2/year at 1AU [6] solar wind irradiation and micrometeorite impacts are are: ~80,000 years for 0211, ~70,000 years for 0192, known to alter the the properties of regolith materials and ~24,000 years for 0125. exposed on airless bodies [1]. The rates of space Discussion: Cosmic-ray exposure: Measurements weathering processes however, are poorly constrained of cosmic-ray exposure (CRE) ages of Itokawa parti- for asteroid regoliths, with recent estimates ranging cles [6-8] reveal that these grains are relatively young, over many orders of magnitude [e.g., 2, 3]. The return of surface samples by JAXA’s Hayabusa mission to ≤1−1.5 Ma, when compared to the distribution of ex- asteroid 25143 Itokawa, and their laboratory analysis posure ages for LL chondrite meteorites (8−50Ma) [9]. provides “ground truth” to anchor the timescales for The CRE ages for Itokawa grains are consistent with a space weathering processes on airless bodies. Here, we stable regolith at meter-depths for ~106 years. use the effects of solar wind irradiation and the Solar flare particle tracks: Based on the solar flare accumulation of solar flare tracks recorded in Itokawa particle track production rate in olivine at 1AU [6], the grains to constrain the rates of space weathering and Itokawa grains recorded solar flare tracks over time- yield information about regolith dynamics on these scales of <105 years. -
O + Escape During the Extreme Space Weather Event of 4-10 September
O + Escape During the Extreme Space Weather Event of 4-10 September 2017 Audrey Schillings, Hans Nilsson, Rikard Slapak, Peter Wintoft, Masatoshi Yamauchi, Magnus Wik, Iannis Dandouras, Chris Carr To cite this version: Audrey Schillings, Hans Nilsson, Rikard Slapak, Peter Wintoft, Masatoshi Yamauchi, et al.. O + Es- cape During the Extreme Space Weather Event of 4-10 September 2017. Journal of Space Weather and Space Climate, EDP sciences, 2018, 16 (9), pp.1363-1376. 10.1029/2018SW001881. hal-02408153 HAL Id: hal-02408153 https://hal.archives-ouvertes.fr/hal-02408153 Submitted on 12 Dec 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. SPACE WEATHER, VOL. ???, XXXX, DOI:10.1002/, + 1 O escape during the extreme space weather event of 2 September 4–10, 2017 Audrey Schillings,1,2 Hans Nilsson,1,2 Rikard Slapak,3 Peter Wintoft,4 Masatoshi Yamauchi,1 Magnus Wik,4 Iannis Dandouras,5 and Chris M. Carr,6 Corresponding author: Audrey Schillings, Swedish Institute of Space Physics, Kiruna, Sweden. ([email protected]) 1Swedish Institute of Space Physics, Kiruna, Sweden. 2Division of Space Technology, Lule˚a University of Technology, Kiruna, Sweden. -
A Three-Dimensional Time-Dependent Model of the Polar Wind
JOURNAL OF G EOPHYSICAL RESE ARCH. VO L. 94 . NO . A7. PAG E 8973-8991 , J ULY I. 1989 A Three-Dimensional Time-Dependent Model of the Polar Wind R. W. SCHUNK AND J. J. SOJKA Center for Atmospheric and Space Sciences, Utah State University, Logan A time-dependent global model of the polar wind was used to study transient polar wind per turbations during changing magnetospheric conditions. The model calculates three-dimensional distributions for the NO+, ot, Nt, N+ and 0 + densities and the ion and electron tempera tures from diffusion and heat conduction equations at altitudes between 120 and 800 km. At altitudes above 500 km, the time-dependent nonlinear hydrodynamic equations for 0 + and H+ are solved self-consistently with the ionospheric equations. The model takes account of supersonic ion outflow, shock formation, and ion energization during a plasma expansion event. During the simulation, the magnetic activity level changed from quiet to active and back to quiet again over a 4.5-hour period. The study indicates the following: (1) Plasma pressure changes due to Te , Ti or electron density variations produce perturbations in the polar wind. In particular, plasma flux tube motion through the auroral oval and high electric field regions produces transient large-scale ion upflows and downflows. At certain times and in certain regions both inside and outside the auroral oval, H+-O+ counterstreaming can occur, (2) The density structure in the polar wind is considerably more complicated than in the ionosphere because of both horizontal plasma convec tion and changing vertical propagation speeds due to spatially varying ionospheric temperatures, (3) During increasing magnetic activity, there is an overall increase in Te , Ti and the electron density in the F-region, but there is a time delay in the buildup of the electron density that is . -
Lecture 23: Jupiter Solar System Jupiter's Orbit
Lecture 23: Jupiter Solar System Jupiter’s Orbit •The semi-major axis of Jupiter’s orbit is a = 5.2 AU Jupiter Sun a •Kepler’s third law relates the semi-major axis to the orbital period 1 Jupiter’s Orbit •Kepler’s third law relates the semi-major axis a to the orbital period P 2 3 ⎛ P ⎞ = ⎛ a ⎞ ⎜ ⎟ ⎜ ⎟ ⎝ years⎠ ⎝ AU ⎠ •Solving for the period P yields 3/ 2 ⎛ P ⎞ = ⎛ a ⎞ ⎜ ⎟ ⎜ ⎟ ⎝ years ⎠ ⎝ AU ⎠ •Since a = 5.2 AU for Jupiter, we obtain P = 11.9 Earth years •Jupiter’s orbit has eccentricity e = 0.048 Jupiter’s Orbit •The distance from the Sun varies by about 10% during an orbit Dperihelion = 4.95 AU Daphelion = 5.45 AU •Like Mars, Jupiter is easiest to observe during favorable opposition •At this time, the Earth-Jupiter distance is only about 3.95 AU Earth Jupiter Jupiter Sun (perihelion) (aphelion) •Jupiter appears full during favorable opposition Bulk Properties of Jupiter •Jupiter is the largest planet in the solar system •We have for the radius and mass of Jupiter Rjupiter = 71,400 km = 11.2 Rearth 30 Mjupiter = 1.9 x 10 g = 318 Mearth •The volume of Jupiter is therefore given by 4 V = π R 3 jupiter 3 jupiter 30 3 •Hence Vjupiter = 1.5 x 10 cm 2 Bulk Properties of Jupiter •The average density of Jupiter is therefore M × 30 ρ = jupiter = 1.9 10 g jupiter × 30 3 Vjupiter 1.5 10 cm •We obtain ρ = −3 jupiter 1.24 g cm •This is much less than the average density of the Earth •Hence there is little if any iron and no dense core inside Jupiter Bulk Properties of Jupiter •The average density of the Earth is equal to −3 ρ⊕ = 6 g cm •The density -
Geomagnetic Disturbance Intensity Dependence on the Universal Timing of the Storm Peak
Geomagnetic disturbance intensity dependence on the universal timing of the storm peak R.M. Katus1,3,2, M.W. Liemohn2, A.M. Keesee3, T.J. Immel4, R. Ilie2, D. T. Welling2, N. Yu. Ganushkina5,2, N.J. Perlongo2, and A. J. Ridley2 1. Department of Mathematics, Eastern Michigan University, Ypsilanti, MI, USA 2. Department of Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, MI, USA 3. Department of Physics and Astronomy, West Virginia University, Morgantown, WVU, USA 4. Space Sciences Laboratory, University of California, Berkeley, CA, USA 5. Finnish Meteorological Institute, Helsinki, Finland Submitted to: Journal of Geophysical Research Corresponding author email: [email protected] AGU index terms: 2730 Magnetosphere: inner 2788 Magnetic storms and substorms (4305, 7954) 4305 Space weather (2101, 2788, 7900) 4318 Statistical analysis (1984, 1986) 7954 Magnetic storms (2788) Keywords: Geomagnetic indices, ground-based magnetometers, Longitudinal dependence, magnetic storms, space weather Key points: • We statistically examine storm-time solar wind and geophysical data as a function of UT of the storm peak. • There is a significant UT dependence to large storms; larger storms occur with a peak near 02 UT. • The difference in storm magnitude is caused by substorm activity and not by solar wind driving. This is the author manuscript accepted for publication and has undergone full peer review but has not been through the copyediting, typesetting, pagination and proofreading process, which may lead to differences between this version and the Version of Record. Please cite this article as doi: 10.1002/2016JA022967 This article is protected by copyright. All rights reserved. -
Space Weathering on Mercury
Advances in Space Research 33 (2004) 2152–2155 www.elsevier.com/locate/asr Space weathering on Mercury S. Sasaki *, E. Kurahashi Department of Earth and Planetary Science, The University of Tokyo, Tokyo 113 0033, Japan Received 16 January 2003; received in revised form 15 April 2003; accepted 16 April 2003 Abstract Space weathering is a process where formation of nanophase iron particles causes darkening of overall reflectance, spectral reddening, and weakening of absorption bands on atmosphereless bodies such as the moon and asteroids. Using pulse laser irra- diation, formation of nanophase iron particles by micrometeorite impact heating is simulated. Although Mercurian surface is poor in iron and rich in anorthite, microscopic process of nanophase iron particle formation can take place on Mercury. On the other hand, growth of nanophase iron particles through Ostwald ripening or repetitive dust impacts would moderate the weathering degree. Future MESSENGER and BepiColombo mission will unveil space weathering on Mercury through multispectral imaging observations. Ó 2003 COSPAR. Published by Elsevier Ltd. All rights reserved. 1. Introduction irradiation should change the optical properties of the uppermost regolith surface of atmosphereless bodies. Space weathering is a proposed process to explain Although Hapke et al. (1975) proposed that formation spectral mismatch between lunar soils and rocks, and of iron particles with sizes from a few to tens nanome- between asteroids (S-type) and ordinary chondrites. ters should be responsible for the optical property Most of lunar surface and asteroidal surface exhibit changes, impact-induced formation of glassy materials darkening of overall reflectance, spectral reddening had been considered as a primary cause for space (darkening of UV–Vis relative to IR), and weakening of weathering. -
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. -
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. -
Thermal Structure and Composition of Jupiter's Great Red Spot from High-Resolution Thermal Imaging
Thermal Structure and Composition of Jupiter’s Great Red Spot from High-Resolution Thermal Imaging Leigh N. Fletchera,b, G. S. Ortona, O. Mousisc,d, P. Yanamandra-Fishera, P. D. Parrishe,a, P. G. J. Irwinb, B. M. Fishera, L. Vanzif, T. Fujiyoshig, T. Fuseg, A.A. Simon-Millerh, E. Edkinsi, T.L. Haywardj, J. De Buizerk aJet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA, 91109, USA bAtmospheric, Oceanic and Planetary Physics, Department of Physics, University of Oxford, Clarendon Laboratory, Parks Road, Oxford, OX1 3PU, UK cInstitut UTINAM, CNRS-UMR 6213, Observatoire de Besan¸con, Universit´ede Franche-Comt´e, Besan¸con, France dLunar and Planetary Laboratory, University of Arizona, Tucson, AZ, USA eSchool of GeoScience, University of Edinburgh, Crew Building, King’s Buildings, Edinburgh, EH9 3JN, UK fPontificia Universidad Catolica de Chile, Department of Electrical Engineering, Av. Vicuna Makenna 4860, Santiago, Chile. gSubaru Telescope, National Astronomical Observatory of Japan, National Institutes of Natural Sciences, 650 North A’ohoku Place, Hilo, Hawaii 96720, USA hNASA/Goddard Spaceflight Center, Greenbelt, Maryland, 20771, USA iUniversity of California, Santa Barbara, Santa Barbara, CA 93106, USA jGemini Observatory, Southern Operations Center, c/o AURA, Casilla 603, La Serena, Chile. kSOFIA - USRA, NASA Ames Research Center, Moffet Field, CA 94035, USA. Abstract Thermal-IR imaging from space-borne and ground-based observatories was used to investigate the temperature, composition and aerosol structure of Jupiter’s Great Red Spot (GRS) and its temporal variability between 1995-2008. An elliptical warm core, extending over 8◦ of longitude and 3◦ of latitude, was observed within the cold anticyclonic vortex at 21◦S. -
A Comparative View of Radiation, Xa9745787 Photo and Photocatalytically Induced Oxidation of Water Pollutants
A COMPARATIVE VIEW OF RADIATION, XA9745787 PHOTO AND PHOTOCATALYTICALLY INDUCED OXIDATION OF WATER POLLUTANTS N. GETOFF Institute for Theoretical Chemistry and Radiation Chemistry, University of Vienna, Vienna, Austria Abstract Water resources are presently overloaded with biologically resistant (refractory) pollutants. Several oxidation methods have been developed for their degradation, the most efficient of which is iradiation treatment, particularly that based on e-beam processing in the presence of Q/O3. The next-best method is photoinduced pollutant oxidation with VUV- and/or UV-light, using HjO2 or H2O2/O3 as an additional source of OH radicals. The photocatalytic method, using e.g. TiQ as a catalyst in combination with oxidation agents such as If Oj or H2O2/O3, is also recommended. The suitability of these three methods is illustrated by examples and they are briefly discussed and compared on the basis of theirenergy consumption and efficiency. Other methods, such as ozone treatment, the photo-Fenton process, ultrasonic and elctrochemical treatments, as well as the well known biological process and thermal oxidation of refractory pollutants, are briefly mentioned. 1. INTRODUCTION Current water resources are strongly overloaded with biologically resistant pollutants, as a result of global population growth and the development of certain industries in the past few decades. The disposal of chemical waste in rivers, seas and oceans has contributed to possibly-irrepairable destruction of marine life. The application of fertilizers, pesticides etc. in modern agriculture has exacerbated the situation. Hence, urgent measures are necessary for remediation of water resources. For the degradation of water pollutants, a number of oxidation methods, based on processes initiated by ionizing radiation, UV- and visible light, photocatalytic induced reactions, as well as combinations of these, have been developed. -
Investigations of Moon-Magnetosphere Interactions by the Europa Clipper Mission
EPSC Abstracts Vol. 13, EPSC-DPS2019-366-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Investigations of Moon-Magnetosphere Interactions by the Europa Clipper Mission Haje Korth (1), Robert T. Pappalardo (2), David A. Senske (2), Sascha Kempf (3), Margaret G. Kivelson (4,5), Kurt Retherford (6), J. Hunter Waite (6), Joseph H. Westlake (1), and the Europa Clipper Science Team (1) Johns Hopkins University Applied Physics Laboratory, Maryland, USA, (2) Jet Propulsion Laboratory, California, USA, (3) University of Colorado, Colorado, USA, (4) University of Michigan, Michigan, USA, (5) University of California, California, USA, (6) Southwest Research Institute, Texas, USA. ([email protected]) 1. Introduction magnetic fields inducing eddy currents in the ocean. By measuring the induced field response at multiple The influence of the Jovian space environment on frequencies, the ice shell thickness and the ocean Europa is multifaceted, and observations of moon- layer thickness and conductivity can be uniquely magnetosphere interaction by the Europa Clipper will determined. The ECM consists of four fluxgate provide an understanding of the satellite’s interior sensors mounted on a 5-m-long boom and a control structure and compositional makeup among others. electronics hosted in a vault shielding it from The variability of Jupiter’s magnetic field at Europa radiation damage. The use of four sensors allows for induces electric currents within the moon’s dynamic removal of higher-order spacecraft- conducting ocean layer, the magnitude of which generated magnetic fields on a boom that is short depends on the ocean’s location, extent, and compared with the spacecraft dimensions. -
PSRD | a Cosmosparks Report
PSRD | A CosmoSparks report Quick Views of Big Advances Solar Wind Interactions with a Lunar Paleo-magnetosphere How would an ancient, global magnetic field on the Moon and its associated paleo-magnetosphere interact with the incoming, charged particles in the solar wind plasma? Would a paleo-magnetosphere shield the lunar surface from solar wind bombardment? Answering these questions improves our understanding of processes that were influenced by the Moon's paleo-magnetosphere, such as the accumulation and space weathering of volatiles in the polar regions. This is the work being undertaken by Ian Garrick-Bethell (University of California, Santa Cruz/Kyung Hee University, South Korea), Andrew Poppe (University of California, Berkeley/SSERVI NASA Ames), and Shahab Fatemi (Swedish Institute of Space Physics, Kiruna). Using computer models of the plasma environment with solar wind parameters appropriate for ~2 billion years ago, Garrick-Bethell and coauthors simulated its interaction with a lunar paleo-magnetosphere. The researchers applied Amitis, a fast, 3D computer model of plasma (kinetic ions and fluid electrons). They modeled the solar wind as H+ and used lunar surface paleo-magnetic field strengths of 0.5µT, 2µT, and 5µT (microteslas) at different orientations. (Earth, by comparison, has a surface magnetic field strength ranging from ~20 to 60µT.) Shown on the left is a 2D plot of one of the Moon-modeling results of plasma density for the case of a spin-aligned 2µT equatorial surface magnetic field strength. The magnetic dipole moment is vertical, as indicated by the small black arrow. The solar wind flows from right to left. In addition to the bow shock showing where the solar wind is diverted around the lunar magnetosphere, the modeling results clearly indicate the two polar cusps (areas of focused field lines) where solar wind plasma funnels down to the lunar surface.