E-Region Auroral Ionosphere Model
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Appendix I Glossary
Appendix I Glossary Editor: A.P.M. Baede A → indicates that the following term is also contained in this Glossary. Adjustment time centrimetric precision. Altimetry has the advantage of being a See: →Lifetime; see also: →Response time. measurement relative to a geocentric reference frame, rather than relative to land level as for a →tide gauge, and of affording quasi- Aerosols global coverage. A collection of airborne solid or liquid particles, with a typical size between 0.01 and 10 µm and residing in the atmosphere for Anthropogenic at least several hours. Aerosols may be of either natural or Resulting from or produced by human beings. anthropogenic origin. Aerosols may influence climate in two ways: directly through scattering and absorbing radiation, and Atmosphere indirectly through acting as condensation nuclei for cloud The gaseous envelope surrounding the Earth. The dry formation or modifying the optical properties and lifetime of atmosphere consists almost entirely of nitrogen (78.1% volume clouds. See: →Indirect aerosol effect. mixing ratio) and oxygen (20.9% volume mixing ratio), The term has also come to be associated, erroneously, with together with a number of trace gases, such as argon (0.93% the propellant used in “aerosol sprays”. volume mixing ratio), helium, and radiatively active →greenhouse gases such as →carbon dioxide (0.035% volume Afforestation mixing ratio), and ozone. In addition the atmosphere contains Planting of new forests on lands that historically have not water vapour, whose amount is highly variable but typically 1% contained forests. For a discussion of the term →forest and volume mixing ratio. The atmosphere also contains clouds and related terms such as afforestation, →reforestation, and →aerosols. -
Global X-Ray Emission During an Isolated Substorm Р a Case Study
Journal of Atmospheric and Solar-Terrestrial Physics 62 (2000) 889±900 Global X-ray emission during an isolated substorm Ð a case study N. éstgaard a,*, J. Stadsnes a, J. Bjordal a, R.R. Vondrak b, S.A. Cummer b, D.L. Chenette c, M. Schulz c, G.K. Parks d, M.J. Brittnacher d, D.L. McKenzie e, J.G. Pronko f aDepartment of Physics, University of Bergen, Bergen, Norway bLaboratory for Extraterrestrial Physics, Goddard Space Flight Center, Greenbelt, MD, USA cLockheed-Martin Advanced Technology Center, Palo Alto, CA, USA dGeophysics Program, University of Washington, Seattle, WA, USA eThe Aerospace Corporation, Los Angeles, CA, USA fPhysics Department, University of Nevada, Reno, NV, USA Received 30 July 1999; accepted 10 December 1999 Abstract The polar ionospheric X-ray imaging experiment (PIXIE) and the UV imager (UVI) onboard the Polar satellite have provided the ®rst simultaneous global scale views of the patterns of electron precipitation through imaging of the atmospheric X-ray bremsstrahlung and the auroral UV emissions. While the UV images in the Lyman±Birge± Hop®eld-long band used in this study respond to the total electron energy ¯ux which is usually dominated by low- energy electrons (<10 keV), the PIXIE images of X-ray bremsstrahlung above 02.7 keV respond to electrons of energy above 03 keV. Comparison of precipitation features seen by UVI and PIXIE provides information on essentially complementary energy ranges of the precipitating electrons. In this study an isolated substorm is examined using data from PIXIE, UVI, ground-based measurements, and in situ measurements from high- and low- altitude satellites to obtain information about the global characteristics during the event. -
Pitch Angle Dependence of Energetic Electron Precipitation: Energy
Confidential manuscript submitted to JGR 1 Pitch Angle Dependence of Energetic Electron Precipitation: 2 Energy Deposition, Backscatter, and the Bounce Loss Cone 1 2 3 R. A. Marshall and J. Bortnik 1 4 Ann and H. J. Smead Department of Aerospace Engineering Sciences, University of Colorado Boulder, Boulder, CO 5 80309, USA. 2 6 Department of Atmospheric and Oceanic Sciences, University of California Los Angeles, Los Angeles, CA 90095, USA. 7 Key Points: • 8 We characterize energy deposition and atmospheric backscatter of radiation belt 9 electrons as a function of energy and pitch angle • 10 We use these simulations to characterize the bounce loss cone and show that it is 11 energy dependent • 12 The simulated backscatter of precipitation is characterized by field aligned beams 13 of low energies which should be observable Corresponding author: R. A. Marshall, [email protected] –1– Confidential manuscript submitted to JGR 14 Abstract 15 Quantifying radiation belt precipitation and its consequent atmospheric effects re- 16 quires an accurate assessment of the pitch angle distribution of precipitating electrons, as 17 well as knowledge of the dependence of the atmospheric deposition on that distribution. 18 Here, Monte Carlo simulations are used to investigate the effects of the incident electron 19 energy and pitch angle on precipitation for bounce-period time scales, and the implica- 20 tions for both the loss from the radiation belts and the deposition in the upper atmosphere. 21 Simulations are conducted at discrete energies and pitch angles to assess the dependence 22 on these parameters of the atmospheric energy deposition profiles and to estimate the 23 backscattered particle distributions. -
Pos(ICRC2017)086 Eric Cascade: Electron Del
Computation of electron precipitation atmospheric ionization: updated model CRAC-EPII Alexander Mishev∗ PoS(ICRC2017)086 Space Climate Research Unit, University of Oulu, Finland. E-mail: [email protected] Anton Artamonov Space Climate Research Unit, University of Oulu, Finland. E-mail: [email protected] Genady Kovaltsov Ioffe Physical-Technical Institute of Russian Academy of Sciences, St. Petersburg, Russia. E-mail: [email protected] Irina Mironova St. Petersburg State University, Institute of Physics, St. Petersburg, Russia E-mail: [email protected] Ilya Usoskin Space Climate Research Unit; Sodankylä Geophysical Observatory (Oulu unit), University of Oulu, Finland. E-mail: [email protected] A new model of the CRAC family, CRAC:EPII (Cosmic Ray Atmospheric Cascade: Electron Precipitation Induced Ionization) is presented. The model allows one to calculate atmospheric ionization induced by precipitating electrons. The model is based on pre-computed with high- precision ionization yield functions, which are obtained using full Monte Carlo simulation of electron propagation and interaction in the Earth’s atmosphere, explicitly considering all physical processes involved in ion production. The simulations were performed using GEANT 4 simu- lation tool PLANETOCOSMICS with NRLMSISE 00 atmospheric model. A quasi-analytical approach, which allows one to compute the ionization yields for events with arbitrary incidence is also presented. It is compared with Monte Carlo simulations and good agreement between Monte Carlo simulations and quasi-analytical approach is achieved. 35th International Cosmic Ray Conference - ICRC 2017- 10-20 July, 2017 Bexco, Busan, Korea ∗Speaker. c Copyright owned by the author(s) under the terms of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License (CC BY-NC-ND 4.0). -
Miniature Space GPS Receiver by Means of Automobile-Navigation Technology
[SSC07-VIII-1] Miniature Space GPS Receiver by means of Automobile-Navigation Technology Hirobumi Saito Institute of Space and Astronautical Science, Japan Aerospace Exploration Agenc 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510 Japan; 81-42-759-8363 [email protected]/jp Takahide Mizuno*, Kousuke Kawahara*, Kenji Shinkai*, Takanao Saiki*, Yousuke Fukushima*, Yusuke Hamada**, Hiroyuki Sasaki***, Sachiko Katumoto*** and Yasuhiro Kajikawa**** *Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510 Japan **Musashi Institute of Technology, 1-28-1 Tamazutsumi, Setahaya-ku, Tokyo, 158-8557 Japan ***Soka University, 1-236 Tangi-cho, Hachioji-city, Tokyo, 192-8577 Japan ****Tokyo Denki University, 2-2 kanda, Nishikicyou, chiyoda-ku, Tokyo, 101-8457 Japan ABSTRACT Miniature space GPS receivers have been developed by means of automobile-navigation technology. We expanded the frequency sweep range in order to cover large Doppler shift on orbit. The GPS receiver was modified to output pseudorange data with accurate time tag. We tested the performance in low earth orbits by means of a GPS simulator. The range error caused by the receiver is measured to be 0.9 meter in RMS. Receiver was on-boarded on INDEX (“REIMEI”) satellite, which was launched in 2005. Cold start positioning was confirmed repeatedly to finish within 30 minutes on orbit. The orbit determination was performed to evaluate the random position error of GPS receiver by means of the residual error. The random error of GPS position is as large as 2 meter for PDDP=2.5 on orbit. The RMS value of range error is evaluated to be 0.6m from the flight data. -
Aeronomy and Astrophysics
Aeronomy and astrophysics A southern high-latitude geomagnetic index: AES-80 C.G. MACLENNAN, Bell Laboratories, Lucent Technologies, Murray Hill, New Jersey 07974 P. B ALLATORE, Istito de Fisica della Spazio Interplanetario, Consiglio Nazionale della Ricerche, c.p. 27, 00044 Frascati, Rome, Italy M.J. ENGEBRETSON, Department of Physics, Augsburg College, Minneapolis, Minnesota 55454 L.J. LANZEROTTI, Bell Laboratories, Lucent Technologies, Murray Hill, New Jersey 07974 eomagnetic measurements obtained at McMurdo Sta- G tion (Arrival Heights) and at two of the U.S. automatic geophysical observatories (AGO-1; AGO-4) are being com- bined with measurements made at Casey and Dumont D'Urville to construct a Southern Hemisphere geomagnetic index for the geomagnetic latitude 80°S. The calculation of the index is modeled on the calculation of the Northern Hemi- sphere auroral electrojet index AE and is thus called the AES- 80 index. The AE index was developed to monitor geomagnetic activity at auroral zone latitudes in the Northern Hemisphere (Davis and Sugiura 1966) and indicates the level of auroral electrojet currents and in particular the occurrence of sub- storms (Baumjohann 1986). It is calculated as the difference between the upper (AU) and the lower (AL) envelope of mag- netograms from 12 observatories located at northern geomag- netic latitudes between 60° and 70° and rather uniformly distributed over all longitudes. Because of the land mass dis- tribution in Antarctica, it is impossible to have ground obser- vatories located uniformly at geomagnetic latitudes between 60° and 70°S (see figure 1). Unlike in the Northern Hemisphere, Figure 1. Map of Antarctica, with the stations used to calculate the however, it is possible in Antarctica to have reasonable ground AES-80 index shown as filled circles. -
Electron Precipitation Models in Global Magnetosphere Simulations
JournalofGeophysicalResearch: SpacePhysics RESEARCH ARTICLE Electron precipitation models in global 10.1002/2014JA020615 magnetosphere simulations 1 1 1 2 3 Key Points: B. Zhang ,W.Lotko , O. Brambles , M. Wiltberger , and J. Lyon • Electron precipitation models are developed for global magnetosphere 1Thayer School of Engineering, Dartmouth College, Hanover, New Hampshire, USA, 2High Altitude Observatory, National simulations Center for Atmospheric Research, Boulder, Colorado, USA, 3Department of Physics and Astronomy, Dartmouth College, • Monoenergetic and diffuse Hanover, New Hampshire, USA precipitation exhibit nonlinear relations with SW driving • Modeled precipitation power is consistent with estimations from Abstract General methods for improving the specification of electron precipitation in global simulations UVI images are described and implemented in the Lyon-Fedder-Mobarry (LFM) global simulation model, and the quality of its predictions for precipitation is assessed. LFM’s existing diffuse and monoenergetic electron Correspondence to: precipitation models are improved, and new models are developed for lower energy, broadband, and B. Zhang, direct-entry cusp precipitation. The LFM simulation results for combined diffuse plus monoenergetic [email protected] electron precipitation exhibit a quadratic increase in the hemispheric precipitation power as the intensity of solar wind driving increases, in contrast with the prediction from the OVATION Prime (OP) 2010 empirical Citation: precipitation model which increases linearly with driving intensity. Broadband precipitation power increases Zhang,B.,W.Lotko,O.Brambles, M. Wiltberger, and J. Lyon (2015), approximately linearly with driving intensity in both models. Comparisons of LFM and OP predictions with Electron precipitation models estimates of precipitating power derived from inversions of Polar satellite UVI images during a double in global magnetosphere substorm event (28–29 March 1998) show that the LFM peak precipitating power is > 4× larger when using simulations, J. -
UPPER ATMOSPHERE RESEARCH at INPE B.R. Clbmesha Department of Geophysics and Aeronomy Instituto De Pesquisas Espaciais
UPPER ATMOSPHERE RESEARCH AT INPE B.R. CLbMESHA Department of Geophysics and Aeronomy Instituto de Pesquisas Espaciais - INPE ABSTRACT Upper atmosphere research at INPE is mainly concerned with the chemistry and dynamics of the stratosphere, upper mesosphere and lower thermosphere, and the middle thermo- sphere. Experimental work includes lidar observations of the stratospheric aerosol, measurements of stratospheric ozone by Dobson spectrophotometers and by balloon and rocket-borne sondes, lidar measurements of atmospheric sodium, and photom- etric observations of 0, 02 , OH and Na emissions, including interferometric measurements of the 016300 emission for the purpose of determining thermospheric winds and temperature. The airglow observations also include measurements of a number of emissions produced by the precipitation of ener- getic neutral particles generated by charge exchange in the ring current. Some recent results of INPE's upper atmosphere program are presented.ii» this paper. ' ' n/ .71. 1- INTRODUCTION INPK maintains an active program of research into a number of aspects of upper atmosphere science, including both experimental and theoretical studies of the dynamics and chemistry of the stratosphere, mesosphere and lower thermosphere. Hxperimental work involves mainly ground-based optical techniques, although balloon and rocket-borne sondes are used for studies of stratospheric ozone, and a rocket-borne photometer payload is under development for measurements of a number of emissions from the thermosphere. Theoretical studies include numerical model- ling with special reference to a number of minor constituents related to the experimental measurements. In the following sec- tions we present a brief description of INPE's experimental fa- cilities in the area of upper atmosphere science, and outline some recent results. -
Status of NSF Space Physics
Status of NSF Space Physics Rich Behnke Therese Moretto, Bob Robinson, Anja Stromme, and Ray Walker National Academy – March 7,2013 • Status and Updates • NSF Response to the Academy’s “Solar and Space Physics: A Science for a Technological Society 2 The Five Geospace Programs • Solar Physics -- Paul Bellaire has retired, new PD has been selected – but not signed. • Magnetospheric Physics – Ray Walker • Aeronomy – Anja Stromme • Geospace Facilities – Bob Robinson • Space Weather and Instrumentation -- Therese Moretto Aeronomy (AER) • Typically around 95 proposals per year, about 1/3 funded. Budget is about $11M • Home of CEDAR • Program Director --Anja Stromme (SRII) 4 Magnetospheric Physics (MAG) • typically around 90 proposals per year, 1/3 funded. Budget is about $8.5M. • Home of GEM • Program Director – Ray Walker (UCLA) 5 Solar Physics Program (STR) •Typically around 80 proposals per year, 1/3 funded. Budget is about $8.5M •Home of SHINE •Program Director – Paul Bellaire/TBA 6 The Geospace Facilities Program (GS) Program Director – Bob Robinson • Six incoherent scatter radar sites (five awards:~$12M) • Lidar Consortium (six institutions: ~$1M) • Miscellaneous facility-related awards (facility supplements, CAREER, REU, Workshops, schools: ~1M) SuperDARN is being expanded • The Mid-latitude SuperDARN Array ( AGS’s first midscale project): New SuperDARN radars have been constructed and are operational at: Fort Hays, Kansas; Christmas Valley, Oregon; and Adak, Alaska • Negotiations are underway with Portuguese officials in the Azores -
The Role of Localized Compressional Ultra-Low Frequency Waves In
PUBLICATIONS Journal of Geophysical Research: Space Physics RESEARCH ARTICLE The Role of Localized Compressional Ultra-low Frequency 10.1002/2017JA024674 Waves in Energetic Electron Precipitation Key Points: I. Jonathan Rae1 , Kyle R. Murphy2 , Clare E. J. Watt3 , Alexa J. Halford4 , Ian R. Mann5 , • We detail a new mechanism for direct 5 2 6 7 modulation of electron precipitation Louis G. Ozeke , David G. Sibeck , Mark A. Clilverd , Craig J. Rodger , 8 1 9 via localized compressional waves Alex W. Degeling , Colin Forsyth , and Howard J. Singer • Electrons encountering a time-varying and spatially localized ULF wave can 1Department of Space and Climate Physics, Mullard Space Science Laboratory, University College London, Dorking, UK, break the third invariant 2NASA Goddard Space Flight Centre, Greenbelt, MD, USA, 3Department of Meteorology, University of Reading, Reading, UK, • This localized mechanism has not 4Space Sciences Department, The Aerospace Corporation, Chantilly, VA, USA, 5Department of Physics, University of Alberta, previously been considered and may 6 7 be important for radiation belt losses Edmonton, Alberta, Canada, British Antarctic Survey (NERC), Cambridge, UK, Department of Physics, University of Otago, Dunedin, New Zealand, 8Institute of Space Science and Physics, Shandong University, Weihai, China, 9Space Weather Prediction Center, NOAA, Boulder, CO, USA Supporting Information: • Supporting Information S1 Correspondence to: Abstract Typically, ultra-low frequency (ULF) waves have historically been invoked for radial diffusive I. J. Rae, transport leading to acceleration and loss of outer radiation belt electrons. At higher frequencies, very low [email protected] frequency waves are generally thought to provide a mechanism for localized acceleration and loss through precipitation into the ionosphere of radiation belt electrons. -
A B 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21
A B 1 Name of Satellite, Alternate Names Country of Operator/Owner 2 AcrimSat (Active Cavity Radiometer Irradiance Monitor) USA 3 Afristar USA 4 Agila 2 (Mabuhay 1) Philippines 5 Akebono (EXOS-D) Japan 6 ALOS (Advanced Land Observing Satellite; Daichi) Japan 7 Alsat-1 Algeria 8 Amazonas Brazil 9 AMC-1 (Americom 1, GE-1) USA 10 AMC-10 (Americom-10, GE 10) USA 11 AMC-11 (Americom-11, GE 11) USA 12 AMC-12 (Americom 12, Worldsat 2) USA 13 AMC-15 (Americom-15) USA 14 AMC-16 (Americom-16) USA 15 AMC-18 (Americom 18) USA 16 AMC-2 (Americom 2, GE-2) USA 17 AMC-23 (Worldsat 3) USA 18 AMC-3 (Americom 3, GE-3) USA 19 AMC-4 (Americom-4, GE-4) USA 20 AMC-5 (Americom-5, GE-5) USA 21 AMC-6 (Americom-6, GE-6) USA 22 AMC-7 (Americom-7, GE-7) USA 23 AMC-8 (Americom-8, GE-8, Aurora 3) USA 24 AMC-9 (Americom 9) USA 25 Amos 1 Israel 26 Amos 2 Israel 27 Amsat-Echo (Oscar 51, AO-51) USA 28 Amsat-Oscar 7 (AO-7) USA 29 Anik F1 Canada 30 Anik F1R Canada 31 Anik F2 Canada 32 Apstar 1 China (PR) 33 Apstar 1A (Apstar 3) China (PR) 34 Apstar 2R (Telstar 10) China (PR) 35 Apstar 6 China (PR) C D 1 Operator/Owner Users 2 NASA Goddard Space Flight Center, Jet Propulsion Laboratory Government 3 WorldSpace Corp. Commercial 4 Mabuhay Philippines Satellite Corp. Commercial 5 Institute of Space and Aeronautical Science, University of Tokyo Civilian Research 6 Earth Observation Research and Application Center/JAXA Japan 7 Centre National des Techniques Spatiales (CNTS) Government 8 Hispamar (subsidiary of Hispasat - Spain) Commercial 9 SES Americom (SES Global) Commercial -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology