Space Weather in Ionosphere and Thermosphere
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Global Ionosphere-Thermosphere-Mesosphere (ITM) Mapping Across Temporal and Spatial Scales a White Paper for the NRC Decadal
Global Ionosphere-Thermosphere-Mesosphere (ITM) Mapping Across Temporal and Spatial Scales A White Paper for the NRC Decadal Survey of Solar and Space Physics Andrew Stephan, Scott Budzien, Ken Dymond, and Damien Chua NRL Space Science Division Overview In order to fulfill the pressing need for accurate near-Earth space weather forecasts, it is essential that future measurements include both temporal and spatial aspects of the evolution of the ionosphere and thermosphere. A combination of high altitude global images and low Earth orbit altitude profiles from simple, in-the-medium sensors is an optimal scenario for creating continuous, routine space weather maps for both scientific and operational interests. The method presented here adapts the vast knowledge gained using ultraviolet airglow into a suggestion for a next-generation, near-Earth space weather mapping network. Why the Ionosphere, Thermosphere, and Mesosphere? The ionosphere-thermosphere-mesosphere (ITM) region of the terrestrial atmosphere is a complex and dynamic environment influenced by solar radiation, energy transfer, winds, waves, tides, electric and magnetic fields, and plasma processes. Recent measurements showing how coupling to other regions also influences dynamics in the ITM [e.g. Immel et al., 2006; Luhr, et al, 2007; Hagan et al., 2007] has exposed the need for a full, three- dimensional characterization of this region. Yet the true level of complexity in the ITM system remains undiscovered primarily because the fundamental components of this region are undersampled on the temporal and spatial scales that are necessary to expose these details. The solar and space physics research community has been driven over the past decade toward answering scientific questions that have a high level of practical application and relevance. -
Marina Galand
Thermosphere - Ionosphere - Magnetosphere Coupling! Canada M. Galand (1), I.C.F. Müller-Wodarg (1), L. Moore (2), M. Mendillo (2), S. Miller (3) , L.C. Ray (1) (1) Department of Physics, Imperial College London, London, U.K. (2) Center for Space Physics, Boston University, Boston, MA, USA (3) Department of Physics and Astronomy, University College London, U.K. 1." Energy crisis at giant planets Credit: NASA/JPL/Space Science Institute 2." TIM coupling Cassini/ISS (false color) 3." Modeling of IT system 4." Comparison with observaons Cassini/UVIS 5." Outstanding quesAons (Pryor et al., 2011) SATURN JUPITER (Gladstone et al., 2007) Cassini/UVIS [UVIS team] Cassini/VIMS (IR) Credit: J. Clarke (BU), NASA [VIMS team/JPL, NASA, ESA] 1. SETTING THE SCENE: THE ENERGY CRISIS AT THE GIANT PLANETS THERMAL PROFILE Exosphere (EARTH) Texo 500 km Key transiLon region Thermosphere between the space environment and the lower atmosphere Ionosphere 85 km Mesosphere 50 km Stratosphere ~ 15 km Troposphere SOLAR ENERGY DEPOSITION IN THE UPPER ATMOSPHERE Solar photons ion, e- Neutral Suprathermal electrons B ion, e- Thermal e- Ionospheric Thermosphere Ne, Nion e- heang Te P, H * + Airglow Neutral atmospheric Exothermic reacAons heang IS THE SUN THE MAIN ENERGY SOURCE OF PLANERATY THERMOSPHERES? W Main energy source: UV solar radiaon Main energy source? EartH Outer planets CO2 atmospHeres Exospheric temperature (K) [aer Mendillo et al., 2002] ENERGY CRISIS AT THE GIANT PLANETS Observed values at low to mid-latudes solsce equinox Modeled values (Sun only) [Aer -
Thermosphere? Why Is It So Hot? Atmosphere Model and Thermosphere 5
UNIT 6, LESSON 1: EARTH LAYERS & ATMOSPHERE LET’S BUILD OUR EARTH AND THE ATMOSPHERE 1 & 2 Where is earth’s crust? What is the difference between the 1. Read/annotate the oceanic and continental crust? paragraph(s) Crust and Mantle Where is the earth’s mantle? What is a plate? What part of the 2. Answer the questions mantle is below the plates? that go with the 3 Where is the earth’s core? How is the core similar to the mantle? paragraph(s) Core 4 & 5 Where is the troposphere? What are you likely to find there? Name at least 3 things. 3. Show Mrs. Stoddard Troposphere and Stratosphere your answers Where is the stratosphere? Why would the air be warm in the 4. If you get it correct, get stratosphere? Where is the mesosphere? Why do meteors burn in this layer? a piece of your 6 & 7 Mesosphere Where is the thermosphere? Why is it so hot? atmosphere model And Thermosphere 5. Repeat until your 8 Where is the exosphere? Why do some experts ignore the exosphere and think the thermosphere is the outermost layer of Exosphere model is finished! the earth’s atmosphere? CHECK YOUR MODEL! Exosphere Thermosphere Mesosphere Stratosphere Troposphere Core Name Class Period Mantle Crust HOW DID WE DO ON THE ATMOSPHERE MODEL? LET’S SET UP OUR JOURNALS! Earth’s Layers and Atmosphere 1:301:291:281:271:261:251:241:231:221:211:201:191:181:171:161:151:141:131:121:111:101:091:081:071:061:051:041:031:021:011:000:590:580:570:560:550:540:530:520:510:500:490:480:470:460:450:440:430:420:410:400:390:380:370:360:350:340:330:320:310:300:290:280:270:260:250:240:230:220:210:200:190:180:170:160:150:140:130:120:110:100:090:080:070:060:050:040:030:020:01End -
Astrobiology in Low Earth Orbit
The O/OREOS Mission – Astrobiology in Low Earth Orbit P. Ehrenfreund1, A.J. Ricco2, D. Squires2, C. Kitts3, E. Agasid2, N. Bramall2, K. Bryson4, J. Chittenden2, C. Conley5, A. Cook2, R. Mancinelli4, A. Mattioda2, W. Nicholson6, R. Quinn7, O. Santos2, G. Tahu5, M. Voytek5, C. Beasley2, L. Bica3, M. Diaz-Aguado2, C. Friedericks2, M. Henschke2, J.W. Hines2, D. Landis8, E. Luzzi2, D. Ly2, N. Mai2, G. Minelli2, M. McIntyre2, M. Neumann3, M. Parra2, M. Piccini2, R. Rasay3, R. Ricks2, A. Schooley2, E. Stackpole2, L. Timucin2, B. Yost2, A. Young3 1Space Policy Institute, Washington, DC, USA [email protected], 2NASA Ames Research Center, Moffett Field, CA, USA, 3Robotic Systems Laboratory, Santa Clara University, Santa Clara, CA, USA, 4Bay Area Environmental Research Institute, Sonoma, CA, USA, 5NASA Headquarters, Washington DC, USA, 6University of Florida, Gainesville, FL, USA, 7SETI Institute, Mountain View, CA, USA, 8Draper Laboratory, Cambridge, MA, USA Abstract. The O/OREOS (Organism/Organic Exposure to Orbital Stresses) nanosatellite is the first science demonstration spacecraft and flight mission of the NASA Astrobiology Small- Payloads Program (ASP). O/OREOS was launched successfully on November 19, 2010, to a high-inclination (72°), 650-km Earth orbit aboard a US Air Force Minotaur IV rocket from Kodiak, Alaska. O/OREOS consists of 3 conjoined cubesat (each 1000 cm3) modules: (i) a control bus, (ii) the Space Environment Survivability of Living Organisms (SESLO) experiment, and (iii) the Space Environment Viability of Organics (SEVO) experiment. Among the innovative aspects of the O/OREOS mission are a real-time analysis of the photostability of organics and biomarkers and the collection of data on the survival and metabolic activity for micro-organisms at 3 times during the 6-month mission. -
The O/OREOS Mission—Astrobiology in Low Earth Orbit
Acta Astronautica 93 (2014) 501–508 Contents lists available at ScienceDirect Acta Astronautica journal homepage: www.elsevier.com/locate/actaastro The O/OREOS mission—Astrobiology in low Earth orbit P. Ehrenfreund a,n, A.J. Ricco b, D. Squires b, C. Kitts c, E. Agasid b, N. Bramall b, K. Bryson d, J. Chittenden b, C. Conley e, A. Cook b, R. Mancinelli d, A. Mattioda b, W. Nicholson f, R. Quinn g, O. Santos b,G.Tahue,M.Voyteke, C. Beasley b,L.Bicac, M. Diaz-Aguado b, C. Friedericks b,M.Henschkeb,D.Landish, E. Luzzi b,D.Lyb, N. Mai b, G. Minelli b,M.McIntyreb,M.Neumannc, M. Parra b, M. Piccini b, R. Rasay c,R.Ricksb, A. Schooley b, E. Stackpole b, L. Timucin b,B.Yostb, A. Young c a Space Policy Institute, Washington DC, USA b NASA Ames Research Center, Moffett Field, CA, USA c Robotic Systems Laboratory, Santa Clara University, Santa Clara, CA, USA d Bay Area Environmental Research Institute, Sonoma, CA, USA e NASA Headquarters, Washington DC, USA f University of Florida, Gainesville, FL, USA g SETI Institute, Mountain View, CA, USA h Draper Laboratory, Cambridge, MA, USA article info abstract Article history: The O/OREOS (Organism/Organic Exposure to Orbital Stresses) nanosatellite is the first Received 19 December 2011 science demonstration spacecraft and flight mission of the NASA Astrobiology Small- Received in revised form Payloads Program (ASP). O/OREOS was launched successfully on November 19, 2010, to 22 June 2012 a high-inclination (721), 650-km Earth orbit aboard a US Air Force Minotaur IV rocket Accepted 18 September 2012 from Kodiak, Alaska. -
Diffuse Electron Precipitation in Magnetosphere-Ionosphere- Thermosphere Coupling
EGU21-6342 https://doi.org/10.5194/egusphere-egu21-6342 EGU General Assembly 2021 © Author(s) 2021. This work is distributed under the Creative Commons Attribution 4.0 License. Diffuse electron precipitation in magnetosphere-ionosphere- thermosphere coupling Dong Lin1, Wenbin Wang1, Viacheslav Merkin2, Kevin Pham1, Shanshan Bao3, Kareem Sorathia2, Frank Toffoletto3, Xueling Shi1,4, Oppenheim Meers5, George Khazanov6, Adam Michael2, John Lyon7, Jeffrey Garretson2, and Brian Anderson2 1High Altitude Observatory, National Center for Atmospheric Research, Boulder CO, United States of America 2Applied Physics Laboratory, Johns Hopkins University, Laurel MD, USA 3Department of Physics and Astronomy, Rice University, Houston TX, USA 4Bradley Department of Electrical and Computer Engineering, Virginia Tech, Blacksburg VA, USA 5Astronomy Department, Boston University, Boston MA, USA 6Goddard Space Flight Center, NASA, Greenbelt MD, USA 7Department of Physics and Astronomy, Dartmouth College, Hanover NH, USA Auroral precipitation plays an important role in magnetosphere-ionosphere-thermosphere (MIT) coupling by enhancing ionospheric ionization and conductivity at high latitudes. Diffuse electron precipitation refers to scattered electrons from the plasma sheet that are lost in the ionosphere. Diffuse precipitation makes the largest contribution to the total precipitation energy flux and is expected to have substantial impacts on the ionospheric conductance and affect the electrodynamic coupling between the magnetosphere and ionosphere-thermosphere. -
Jet Streams Anomalies As Possible Short-Term Precursors Of
Research in Geophysics 2014; volume 4:4939 Jet streams anomalies as the existence of thermal fields, con nected with big linear structures and systems of crust Correspondence: Hong-Chun Wu, Institute of possible short-term precursors faults.2 Anomalous variations of latent heat Occupational Safety and Health, Safety of earthquakes with M 6.0 flow were observed for the 2003 M 7.6 Colima Department, Shijr City, Taipei, Taiwan. > (Mexico) earthquake.3 The atmospheric Tel. +886.2.22607600227 - Fax: +886.2.26607732. E-mail: [email protected] Hong-Chun Wu,1 Ivan N. Tikhonov2 effects of ionization are observed at the alti- 1Institute of Occupational Safety and tudes of top of the atmosphere (10-12 km). Key words: earthquake, epicenter, jet stream, pre- Health, Safety Department, Shijr City, Anomalous changes in outgoing longwave cursory anomaly. radiation were recorded at the height of 300 Taipei, Taiwan; 2Institute of Marine GPa before the 26 December 2004 M 9.0 Acknowledgments: the authors would like to Geology and Geophysics, FEB RAS; w express their most profound gratitude to the Indonesia earthquake.4 These anomalous ther- Yuzhno-Sakhalinsk, Russia National Center for Environmental Prediction of mal events occurred 4-20 days prior the earth- the USA and the National Earthquake quakes.5-8 Information Center on Earthquakes of the U.S. Local anomalous changes in the ionosphere Geological Survey for data on jet streams and 9-11 earthquakes on the Internet. Abstract over epicenters can precede earthquakes. Statistical analysis showed that these changes Dedications: the authors dedicate this work to occurred about 1-5 days before seismic the memory of Miss Cai Bi-Yu, who died in Satellite data of thermal images revealed events.12 To connect the listed above abnormal Taiwan during the 1999 earthquake with magni- the existence of thermal fields, connected with phenomena to preparation of earthquakes, tude M=7.3. -
A Breath of Fresh Air: Air-Scooping Electric Propulsion in Very Low Earth Orbit
A BREATH OF FRESH AIR: AIR-SCOOPING ELECTRIC PROPULSION IN VERY LOW EARTH ORBIT Rostislav Spektor and Karen L. Jones Air-scooping electric propulsion (ASEP) is a game-changing concept that extends the lifetime of very low Earth orbit (VLEO) satellites by providing periodic reboosting to maintain orbital altitudes. The ASEP concept consists of a solar array-powered space vehicle augmented with electric propulsion (EP) while utilizing ambient air as a propellant. First proposed in the 1960s, ASEP has attracted increased interest and research funding during the past decade. ASEP technology is designed to maintain lower orbital altitudes, which could reduce latency for a communication satellite or increase resolution for a remote sensing satellite. Furthermore, an ASEP space vehicle that stores excess gas in its fuel tank can serve as a reusable space tug, reducing the need for high-power chemical boosters that directly insert satellites into their final orbit. Air-breathing propulsion can only work within a narrow range of operational altitudes, where air molecules exist in sufficient abundance to provide propellant for the thruster but where the density of these molecules does not cause excessive drag on the vehicle. Technical hurdles remain, such as how to optimize the air-scoop design and electric propulsion system. Also, the corrosive VLEO atmosphere poses unique challenges for material durability. Despite these difficulties, both commercial and government researchers are making progress. Although ASEP technology is still immature, it is on the cusp of transitioning between research and development and demonstration phases. This paper describes the technical challenges, innovation leaders, and potential market evolution as satellite operators seek ways to improve performance and endurance. -
Cold Plasma Diagnostics in the Jovian System
341 COLD PLASMA DIAGNOSTICS IN THE JOVIAN SYSTEM: BRIEF SCIENTIFIC CASE AND INSTRUMENTATION OVERVIEW J.-E. Wahlund(1), L. G. Blomberg(2), M. Morooka(1), M. André(1), A.I. Eriksson(1), J.A. Cumnock(2,3), G.T. Marklund(2), P.-A. Lindqvist(2) (1)Swedish Institute of Space Physics, SE-751 21 Uppsala, Sweden, E-mail: [email protected], [email protected], mats.andré@irfu.se, [email protected] (2)Alfvén Laboratory, Royal Institute of Technology, SE-100 44 Stockholm, Sweden, E-mail: [email protected], [email protected], [email protected], per- [email protected] (3)also at Center for Space Sciences, University of Texas at Dallas, U.S.A. ABSTRACT times for their atmospheres are of the order of a few The Jovian magnetosphere equatorial region is filled days at most. These atmospheres can therefore rightly with cold dense plasma that in a broad sense co-rotate with its magnetic field. The volcanic moon Io, which be termed exospheres, and their corresponding ionized expels sodium, sulphur and oxygen containing species, parts can be termed exo-ionospheres. dominates as a source for this cold plasma. The three Observations indicate that the exospheres of the three icy Galilean moons (Callisto, Ganymede, and Europa) icy Galilean moons (Europa, Ganymede and Callisto) also contribute with water group and oxygen ions. are oxygen rich [1, 2]. Several authors have also All the Galilean moons have thin atmospheres with modelled these exospheres [3, 4, 5], and the oxygen was residence times of a few days at most. -
The Marshall Engineering Thermosphere (MET) Model Volume H Technical Description
NASA / CR--1998-207946 The Marshall Engineering Thermosphere (MET) Model Volume h Technical Description R.E. Smith Physitron, Inc., Huntsville, Alabama Prepared for Marshall Space Flight Center under Contract NAS8-38333 National Aeronautics and Space Administration Marshall Space Flight Center May 1998 EXECUTIVE SUMMARY Volume I of this report presents a technical description of the Marshall Engineering Thermosphere (MET) model atmosphere and a summary of its historical development. Vari- ous programs developed to augment the original capability of the model are discussed in de- tail. The report also describes each of the individual subroutines developed to enhance the model. Computer codes for these subroutines are contained in four appendices. Volume II contains a copy of each of the reference documents. If you have questions or comments or need to request additional information, contact the Chief, Electromagnetics and Aerospace Environments Branch, Systems Analysis and Inte- gration Laboratory, MSFC, AL 35812. iii TABLE OF CONTENTS Section Title I INTRODUCTION ......................................................................................................... 1 II SCOPE ........................................................................................................................... 1 HI DESCRIPTION OF THE NEUTRAL THERMOSPHERE .......................................... 1 A. Variations ............................................................................................................ 1 B. Solar Activity Parameters -
Moon–Magnetosphere Interactions: a Tutorial
Advances in Space Research 33 (2004) 2061–2077 www.elsevier.com/locate/asr Moon–magnetosphere interactions: a tutorial M.G. Kivelson a,b,* a University of California, Institute of Geophysics and Planetary Physics, UCLA, Los Angeles, CA 90095-1567, USA b Department of Earth and Space Sciences, UCLA, Los Angeles, CA 90095-1567, USA Received 8 May 2003; received in revised form 13 August 2003; accepted 18 August 2003 Abstract The interactions between the Galilean satellites and the plasma of the Jovian magnetosphere, acting on spatial scales from that of ion gyroradii to that of magnetohydrodynamics (MHD), change the plasma momentum, temperature, and phase space distribution functions and generate strong electrical currents. In the immediate vicinity of the moons, these currents are often highly structured, possibly because of varying ionospheric conductivity and possibly because of non-uniform pickup rates. Ion pickup changes the velocity space distribution of energetic particles, f (v), where v is velocity. Distributions become more anisotropic and can become unstable to wave generation. That there would be interesting plasma responses near Io was fully anticipated, but one of the surprises of Galileo’s mission was the range of effects observed at all of the Galilean satellites. Electron beams and an assortment of MHD and plasma waves develop in the regions around the moons, although each interaction region is different. Coupling of the plasma near the moons to the Jovian ionosphere creates auroral footprints and, in the case of Io, produces a leading trail in the ionosphere that extends almost half way around Jupiter. The energy source driving the auroral signatures is not fully understood but must require field aligned electric fields that accelerate elections at the feet of the flux tubes of Io and Europa, bodies that interact directly with the incident plasma, and at the foot of the flux tube of Ganymede, a body that is shielded from direct interaction with the background plasma by its magnetospheric cavity. -
The Magnetosphere-Ionosphere Observatory (MIO)
1 The Magnetosphere-Ionosphere Observatory (MIO) …a mission concept to answer the question “What Drives Auroral Arcs” ♥ Get inside the aurora in the magnetosphere ♥ Know you’re inside the aurora ♥ Measure critical gradients writeup by: Joe Borovsky Los Alamos National Laboratory [email protected] (505)667-8368 updated April 4, 2002 Abstract: The MIO mission concept involves a tight swarm of satellites in geosynchronous orbit that are magnetically connected to a ground-based observatory, with a satellite-based electron beam establishing the precise connection to the ionosphere. The aspect of this mission that enables it to solve the outstanding auroral problem is “being in the right place at the right time – and knowing it”. Each of the many auroral-arc-generator mechanisms that have been hypothesized has a characteristic gradient in the magnetosphere as its fingerprint. The MIO mission is focused on (1) getting inside the auroral generator in the magnetosphere, (2) knowing you are inside, and (3) measuring critical gradients inside the generator. The decisive gradient measurements are performed in the magnetosphere with satellite separations of 100’s of km. The magnetic footpoint of the swarm is marked in the ionosphere with an electron gun firing into the loss cone from one satellite. The beamspot is detected from the ground optically and/or by HF radar, and ground-based auroral imagers and radar provide the auroral context of the satellite swarm. With the satellites in geosynchronous orbit, a single ground observatory can spot the beam image and monitor the aurora, with full-time conjunctions between the satellites and the aurora.