The Thermosphere and Ionosphere Responds to External Forcing, Both
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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 -
Episode 2: Bodies in Orbit
Episode 2: Bodies in Orbit This transcript is based on the second episode of Moonstruck, a podcast about humans in space, produced by Dra!House Media and featuring analysis from the Center for Strategic and International Studies’ Aerospace Security Project. Listen to the full episode on iTunes, Spotify, or on our website. BY Thomas González Roberts // PUBLISHED April 4, 2018 AS A DOCENT at the Smithsonian National Air & Space But before humans could use the bathroom in space, a Museum I get a lot of questions from visitors about the lot of questions needed to be answered. Understanding grittiest details of spaceflight. While part of me wants to how human bodies respond to the environment of outer believe that everyone is looking for a thoughtful Kennedy space took years of research. It was a dark, controversial quote to drive home an analysis of the complicated period in the history of spaceflight. This is Moonstruck, a relationship between nationalism and space travel, some podcast about humans in space. I’m Thomas González people are less interested in my stories and more Roberts. interested in other, equally scholarly topics: In the late 1940s, American scientists began to focus on Kids: I have a question. What if you need to go to the two important challenges of spaceflight: solar radiation bathroom while you're in a spacesuit? Is there a special and weightlessness.1 diaper? Aren't you like still wearing the diaper when you are wearing a spacesuit? Let'sThomas start González with radiation. Roberts is the host and executive producer of Moonstruck, and a space policy Alright, alright, I get it. -
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. -
Space Biology Research and Biosensor Technologies: Past, Present, and Future †
biosensors Perspective Space Biology Research and Biosensor Technologies: Past, Present, and Future † Ada Kanapskyte 1,2, Elizabeth M. Hawkins 1,3,4, Lauren C. Liddell 5,6, Shilpa R. Bhardwaj 5,7, Diana Gentry 5 and Sergio R. Santa Maria 5,8,* 1 Space Life Sciences Training Program, NASA Ames Research Center, Moffett Field, CA 94035, USA; [email protected] (A.K.); [email protected] (E.M.H.) 2 Biomedical Engineering Department, The Ohio State University, Columbus, OH 43210, USA 3 KBR Wyle, Moffett Field, CA 94035, USA 4 Mammoth Biosciences, Inc., South San Francisco, CA 94080, USA 5 NASA Ames Research Center, Moffett Field, CA 94035, USA; [email protected] (L.C.L.); [email protected] (S.R.B.); [email protected] (D.G.) 6 Logyx, LLC, Mountain View, CA 94043, USA 7 The Bionetics Corporation, Yorktown, VA 23693, USA 8 COSMIAC Research Institute, University of New Mexico, Albuquerque, NM 87131, USA * Correspondence: [email protected]; Tel.: +1-650-604-1411 † Presented at the 1st International Electronic Conference on Biosensors, 2–17 November 2020; Available online: https://iecb2020.sciforum.net/. Abstract: In light of future missions beyond low Earth orbit (LEO) and the potential establishment of bases on the Moon and Mars, the effects of the deep space environment on biology need to be examined in order to develop protective countermeasures. Although many biological experiments have been performed in space since the 1960s, most have occurred in LEO and for only short periods of time. These LEO missions have studied many biological phenomena in a variety of model organisms, and have utilized a broad range of technologies. -
The Mars Thermosphere-Ionosphere: Predictions for the Arrival of Planet-B
Earth Planets Space, 50, 247–257, 1998 The Mars thermosphere-ionosphere: Predictions for the arrival of Planet-B S. W. Bougher1 and H. Shinagawa2 1Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ 85721, U.S.A. 2Solar Terrestrial Environment Laboratory, Nagoya University, Japan (Received July 28, 1997; Revised January 6, 1998; Accepted February 12, 1998) The primary science objective of the Planet-B mission to Mars is to study the Martian upper atmosphere-ionosphere system and its interaction with the solar wind. An improved knowledge of the Martian magnetic field (whether it is induced or intrinsic) is needed, and will be provided by Planet-B. In addition, a proper characterization of the neutral thermosphere structure is essential to place the various plasma observations in context. The Neutral Mass Spectrometer (NMS) onboard Planet-B will provide the required neutral density information over the altitude range of 150–500 km. Much can be learned in advance of Planet-B data taking as multi-dimensional thermosphere-ionosphere and MHD models are exercised to predict the Mars near-space environment that might be expected during the solar maximum conditions of Cycle 23 (1999–2001). Global model simulations of the Mars thermosphere-ionosphere system are presented and analyzed in this paper. These Mars predictions pertain to the time of Planet-B arrival in October 1999 (F10.7∼200; Ls∼220). In particular, the National Center for Atmospheric Research (NCAR) Mars Thermosphere General Circulation Model (MTGCM) is exercised to calculate thermospheric neutral densities (CO2, + + + CO, N2,O,Ar,O2), photochemical ions (CO2 ,O2 ,O below 200 km), neutral temperatures, and 3-components winds over 70–300 km. -
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. -
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 -
TIMED Mission Science Overview
J-H. YEE TIMED Mission Science Overview Jeng-Hwa Yee The Thermosphere, Ionosphere, Mesosphere Energetics and Dynamics (TIMED) mission is a low-cost NASA Sun-Earth Connections mission designed to provide a basic understanding of the least explored and least understood region of the Earth’s environ- ment—the mesosphere, lower thermosphere, and ionosphere (MLTI). The MLTI region is located approximately 60 to 180 km above the surface and is a gateway between the Earth’s lower atmosphere, in which we live, and space. The TIMED suite of four remote sensing instruments measures energy inputs and outputs in the MLTI region as well as its basic structure, including seasonal and latitudinal variations. Over its 2-year mission, TIMED is investigating the relative importance of various radiative, chemical, electro- dynamic, and dynamic processes that govern the structure and variability of the MLTI region. This article presents an overview of TIMED mission science and objectives. BACKGROUND Although our knowledge of the near-Earth space program designed to quantitatively understand the environment has increased enormously since the start of energetics and dynamics of Earth’s mesosphere, lower the Space Age, many signifi cant gaps still exist, and our thermosphere, and ionosphere (MLTI), a region of ability to model the variability of the system as a whole the atmosphere about 60 and 180 km above the sur- remains rudimentary at best. The Sun, its atmosphere and face. (Complete information on the TIMED mission, heliosphere, and the Earth’s magnetosphere and atmo- including participants, status, science, etc., may be sphere are coupled by important physical processes that found at http://www.timed.jhuapl.edu/mission/.) The are only partially known (NASA Strategic Plan, 1994, MLTI is a transition region between the Sun and the http://umbra.nascom.nasa.gov/solar_connections.html).