Small and Meso-Scale Properties of a Substorm Onset Auroral Arc H
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Annotated List of Works Cited Primary Sources Newspapers “Apollo 11 se Vraci na Zemi.” Rude Pravo [Czechoslovakia] 22 July 1969. 1. Print. This was helpful for us because it showed how the U.S. wasn’t the only ones effected by this event. This added more to our project so we had views from outside the US. Barbuor, John. “Alunizaron, Bajaron, Caminaron, Trabajaron: Proeza Lograda.” Excelsior [Mexico] 21 July 1969. 1. Print. The front page of this newspaper was extremely helpful to our project because we used it to see how this event impacted the whole world not just America. Beloff, Nora. “The Space Race: Experts Not Keen on Getting a Man on the Moon.” Age [Melbourne] 24 April 1962. 2. Print. This was an incredibly important article to use in out presentation so that we could see different opinions. This article talked about how some people did not want to go to the moon; we didn’t find many articles like this one. In most everything we have read it talks about the advantages of going to the moon. This is why this article was so unique and important. Canadian Press. “Half-billion Watch the Moon Spectacular.” Gazette [Montreal] 21 July 1969. 4. Print. This source gave us a clear idea about how big this event really was, not only was it a big deal in America, but everywhere else in the world. This article told how Russia and China didn’t have TV’s so they had to find other ways to hear about this event like listening to the radio. -
E-Region Auroral Ionosphere Model
atmosphere Article AIM-E: E-Region Auroral Ionosphere Model Vera Nikolaeva 1,* , Evgeny Gordeev 2 , Tima Sergienko 3, Ludmila Makarova 1 and Andrey Kotikov 4 1 Arctic and Antarctic Research Institute, 199397 Saint Petersburg, Russia; [email protected] 2 Earth’s Physics Department, Saint Petersburg State University, 199034 Saint Petersburg, Russia; [email protected] 3 Swedish Institute of Space Physics, 981 28 Kiruna, Sweden; [email protected] 4 Saint Petersburg Branch of Pushkov Institute of Terrestrial Magnetism, Ionosphere and Radio Wave Propagation of Russian Academy of Sciences (IZMIRAN), 199034 Saint Petersburg, Russia; [email protected] * Correspondence: [email protected] Abstract: The auroral oval is the high-latitude region of the ionosphere characterized by strong vari- ability of its chemical composition due to precipitation of energetic particles from the magnetosphere. The complex nature of magnetospheric processes cause a wide range of dynamic variations in the auroral zone, which are difficult to forecast. Knowledge of electron concentrations in this highly turbulent region is of particular importance because it determines the propagation conditions for the radio waves. In this work we introduce the numerical model of the auroral E-region, which evaluates density variations of the 10 ionospheric species and 39 reactions initiated by both the solar extreme UV radiation and the magnetospheric electron precipitation. The chemical reaction rates differ in more than ten orders of magnitude, resulting in the high stiffness of the ordinary differential equations system considered, which was solved using the high-performance Gear method. The AIM-E model allowed us to calculate the concentration of the neutrals NO, N(4S), and N(2D), ions + + + + + 4 + 2 + 2 N ,N2 , NO ,O2 ,O ( S), O ( D), and O ( P), and electrons Ne, in the whole auroral zone in the Citation: Nikolaeva, V.; Gordeev, E.; 90-150 km altitude range in real time. -
MTGC] Constraining Spacetime Torsion with the Moon and Mercury Theoretical Predictions and Experimental Limits on New Gravitational Physics
Constraining Spacetime Torsion with Lunar Laser Ranging, Mercury Radar Ranging, LAGEOS, next lunar surface missions and BepiColombo Riccardo March1,3, Giovanni Belletini2,3, Roberto Tauraso2,3, Simone Dell’Agnello3,* 1 Istituto per le Applicazioni del Calcolo (IAC), CNR, Via dei Taurini 19, 00185 Roma, Italy 2 Dipart. di Matematica, Univ. di Roma “Tor Vergata”, via della Ricerca Scientifica 1, 00133 Roma, Italy 3 Italian National Institute for Nuclear Physics, Laboratori Nazionali di Frascati (INFN-LNF), Via Enrico Fermi 40, Frascati (Rome), 00044, Italy 17th International Laser Workshop on Laser Ranging - Bad Koetzting, Germany, May 16-20, 2011 * Presented by S. Dell’Agnello Outline • Introduction • Spacetime torsion predictions • Constraints with Moon and Mercury • Constraints with the LAser GEOdynamics Satellite (LAGEOS) • LLR prospects and opportunities • Conclusions • In the spare slides: further reference material • See also talk of Claudio Cantone (ETRUSCO-2), talk and poster by Alessandro Boni (LAGEOS Sector, Hollow reflector) and, especially, the talk of Doug Currie (LLR for the 21st century) 17th Workshop on Laser Ranging. Germany May 16, 2011 R. March, G. Bellettini, R. Tauraso, S. Dell’Agnello 2 INFN (brief and partial overview) • INFN; public research institute – Main mission: study of fundamental forces (including gravity), particle, nuclear and astroparticle physics and of its technological and industrial applications (SLR, LLR, GNSS, space geodesy…) • Prominent participation in major astroparticle physics missions: – FERMI, PAMELA, AGILE (all launched) – AMS-02, to be launched by STS-134 Endeavor to the International Space Station (ISS) on May 16, 2011 • VIRGO, gravitational wave interferometer (teamed up with LIGO) • …. More, see http://www.infn.it 17th Workshop on Laser Ranging. -
From the Editor
FROM THE EDITOR he fIrst thing I did when we click away on the computer keys, arrived home from vacation he spins around on his activity wheel Tthe other day was to look in and we both savor the classical music the den. from the stereo in the background. "The rat is still alive," I whispered At least, I think I saw him smile the to Kate, my wife. other day. "The rat" is Marvin, our 2-year- A few months ago, a French old pet hamster. Marvin joined our cable TV crew came to our house family two years ago. I was out of to document the life of a part-time town at a professional conference telecommuter. While most ofthe when Maggie, then 2, and Casey, then report focused on me typing away at 5, talked Kate into the purchase. the computer, there were fIve bizarre Casey was allowed to name the seconds of Marvin spinning around On the cover: With such rodent; she still can't explain where on his wheel. huge exposure in more than 120 countries, HP is turning she came up with the name. The analogy was eerie. the corner on sponsorships As animals go, hamsters rank right Sadly, while 2 is an extremely for many diverse sports up there with turtles and goldfIsh as young age for most ofus, it's typically teams. Team Jordan's Rubens Barrichello is shown low-maintenance pets. A little water, a lifetime for hamsters. So Kate and turning hard enough to get some hamster food and a spinning I are preparing to explain the eventu daylight under a tire of his activity wheel will keep a hamster ality of death to Casey and Maggie. -
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. -
ESA Bulletin February 2003
SMART-1/2 3/3/03 3:56 PM Page 14 Science A Solar-Powered Visit to the Moon “As the first spacecraft to use primary electric propulsion in conjunction with gravity manoeuvres,and as Europe’s first mission to the Moon, SMART-1 opens up new horizons in space engineering and scientific discovery.Moreover,we promise frequent news and pictures,so that everyone can share in our lunar adventure.” Giuseppe Racca, ESA’s Smart-1 Project Manager. 14 SMART-1/2 3/3/03 3:56 PM Page 15 SMART-1 The SMART-1 Mission Giuseppe Racca, Bernard Foing, and the SMART-1 Project Team ESA Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands y July 2003 a hitchhiking team of engineers and scientists will be at Europe’s spaceport at Kourou in French Guiana, thumbing Ba lift for a neat little spacecraft, ESA’s SMART-1, on the next Ariane-5 launcher that has room to spare. It’s not very big - just a box a metre wide with folded solar panels attached - and six strong men could lift it. It weighs less than 370 kilograms, compared with thousands of kilos for Ariane’s usual customers’satellites. So it should pose no problems as an auxiliary passenger. SMART stands for Small Missions for Advanced Research in Technology. They pave the way for the novel and ambitious science projects of the future, by testing the new technologies that will be needed. But a SMART project is also required to be cheap - about one- fifth of the cost of a major science mission for ESA - which is why SMART-1 has no launcher of its own. -
In Situ Observations of the Preexisting Auroral Arc by THEMIS All Sky Imagers and the FAST Spacecraft
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 117, A05211, doi:10.1029/2011JA017128, 2012 In situ observations of the “preexisting auroral arc” by THEMIS all sky imagers and the FAST spacecraft Feifei Jiang,1 Robert J. Strangeway,1 Margaret G. Kivelson,1,2 James M. Weygand,1 Raymond J. Walker,1 Krishan K. Khurana,1 Yukitoshi Nishimura,3 Vassilis Angelopoulos,1 and Eric Donovan4 Received 6 September 2011; revised 25 January 2012; accepted 6 March 2012; published 5 May 2012. [1] Auroral substorms were first described more than 40 years ago, and their atmospheric and magnetospheric signatures have been investigated extensively. However, because magnetic mapping from the ionosphere to the equator is uncertain especially during active times, the magnetospheric source regions of the substorm-associated features in the upper atmosphere remain poorly understood. In optical images, auroral substorms always involve brightening followed by poleward expansion of a discrete auroral arc. The arc that brightens is usually the most equatorward of several auroral arcs that remain quiescent for 30 min or more before the break-up commences. In order to identify the magnetospheric region that is magnetically conjugate to this preexisting arc, we combine auroral images from ground-based imagers, magnetic field and particle data from low-altitude spacecraft, and maps of field-aligned currents based on ground magnetometer arrays. We surveyed data from the THEMIS all sky imager (ASI) array and the FAST spacecraft from 2007 to April 2009 and obtained 5 events in which the low altitude FAST spacecraft crossed magnetic flux tubes linked to a preexisting auroral arc imaged by THEMIS ASI prior to substorm onset. -
Next-Generation Laser Retroreflectors for Precision Tests of General
UNIVERSITA` DEGLI STUDI “ROMA TRE” DOTTORATO DI RICERCA IN FISICA XXVIII CICLO Next-generation Laser Retroreflectors for Precision Tests of General Relativity Relazione sull’attivit`adi Dottorato di Manuele Martini Relatore Interno: Prof. Aldo Altamore Relatore Esterno: Dr. Simone Dell’Agnello, LNF-INFN Coordinatore: Prof. Roberto Raimondi Anno Accademico 2015/2016 Alla mia famiglia... Contents List of Acronyms v Preface vii Why this work at LNF-INFN . vii Whatmycontributionis ............................ viii Workinthefieldofoptics ........................ ix Industrial & quality assurance . ix Physics analysis . x 1 Satellite/Lunar Laser Ranging 1 1.1 The ILRS . 2 1.2 Howitworks ............................... 4 1.3 Corner Cube Retroreflectors . 6 1.3.1 Apollo & Lunokhod Corner Cube Retroreflector (CCR) . 8 2GeneralRelativitytests 11 2.1 TestsoriginallyproposedbyEinstein . 11 2.1.1 Mercury perihelion precession . 11 2.1.2 Deflection of light . 12 2.1.3 Gravitational redshift . 18 i 2.1.4 Shapirotimedelay ........................ 20 2.2 ParametrizedPost-Newtonianformalism . 20 3 The SCF Lab 23 3.1 SCF-GCryostat.............................. 25 3.2 Vacuum & Cryogenic System . 27 3.3 Control and acquisition electronics . 30 3.4 Solar Simulator . 33 3.5 IR Thermacam . 36 3.6 Optical layout . 40 3.6.1 Angularcalibration . 42 4 The MoonLIGHT-2 experiment 45 4.1 MoonLIGHT-ILN............................. 46 4.2 MoonLIGHT-2payload. 49 4.2.1 Optical modeling . 49 4.3 Structural design . 55 4.3.1 Sunshade vs sunshade-less . 58 4.3.2 Falcon-9 test . 61 4.3.3 Actual Moon Laser Instrumentation for General relativity High accuracyTests(MoonLIGHT)-2design . 65 4.4 INRRI................................... 65 5 The SCF-TEST 69 5.1 The MoonLIGHT-2 SCF-TESTs: general description . -
Magnetospheric Signatures of STEVE
RESEARCH LETTER Magnetospheric Signatures of STEVE: Implications 10.1029/2019GL082460 for the Magnetospheric Energy Source and Key Points: • Magnetosphere observations show Interhemispheric Conjugacy that STEVE corresponds to SAID, Y. Nishimura1,2 , B. Gallardo‐Lacourt3 , Y. Zou4,5 , E. Mishin6 , D. J. Knudsen3 , plasmapause, structured plasma 3 7 8 boundaries, and waves in the E. F. Donovan , V. Angelopoulos , and R. Raybell magnetosphere 1 • The picket fence is driven by Department of Electrical and Computer Engineering and Center for Space Physics, Boston University, Boston, MA, USA, electron precipitation; the red arc is 2Department of Atmospheric and Oceanic Sciences, University of California, Los Angeles, CA, USA, 3Department of fl driven by heat ux or frictional Physics and Astronomy, University of Calgary, Calgary, Alberta, Canada, 4Department of Astronomy and Center for Space heating Physics, Boston University, Boston, MA, USA, 5Cooperative Programs for the Advancement of Earth System Science, • Simultaneous conjugate 6 observations show that part of University Corporation for Atmospheric Research, Boulder, CO, USA, Space Vehicles Directorate, Air Force Research STEVE has interhemispheric Laboratory, Kirtland AFB, Albuquerque, NM, USA, 7Department of Earth, Planetary, and Space Sciences, University of conjugacy California, Los Angeles, CA, USA, 8Citizen scientist, Seattle, WA, USA Abstract We present three STEVE (strong thermal emission velocity enhancement) events in Correspondence to: Y. Nishimura, conjunction with Time History of Events and Macroscale Interactions (THEMIS) in the magnetosphere [email protected] and Defense Meteorological Satellite Program (DMSP) and Swarm in the ionosphere, for determining equatorial and interhemispheric signatures of the STEVE purple/mauve arc and picket fence. Both types of Citation: STEVE emissions are associated with subauroral ion drifts (SAID), electron heating, and plasma waves. -
Scrolls of Love Ruth and the Song of Songs Scrolls of Love
Edited by Peter S. Hawkins and Lesleigh Cushing Stahlberg Scrolls of Love ruth and the song of songs Scrolls of Love ................. 16151$ $$FM 10-13-06 10:48:57 PS PAGE i ................. 16151$ $$FM 10-13-06 10:48:57 PS PAGE ii Scrolls of Love reading ruth and the song of songs Edited by Peter S. Hawkins and Lesleigh Cushing Stahlberg FORDHAM UNIVERSITY PRESS New York / 2006 ................. 16151$ $$FM 10-13-06 10:49:01 PS PAGE iii Copyright ᭧ 2006 Fordham University Press All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form or by any means—electronic, me- chanical, photocopy, recording, or any other—except for brief quotations in printed reviews, without the prior permission of the publisher. Library of Congress Cataloging-in-Publication Data Scrolls of love : reading Ruth and the Song of songs / edited by Peter S. Hawkins and Lesleigh Cushing Stahlberg.—1st ed. p. cm. Includes bibliographical references and index. ISBN-13: 978-0-8232-2571-2 (cloth : alk. paper) ISBN-10: 0-8232-2571-2 (cloth : alk. paper) ISBN-13: 978-0-8232-2526-2 (pbk. : alk. paper) ISBN-10: 0-8232-2526-7 (pbk. : alk. paper) 1. Bible. O.T. Ruth—Criticism interpretation, etc. 2. Bible. O.T. Song of Solomon—Criticism, interpretation, etc. I. Hawkins, Peter S. II. Stahlberg, Lesleigh Cushing. BS1315.52.S37 2006 222Ј.3506—dc22 2006029474 Printed in the United States of America 08 07 06 5 4 3 2 1 First edition ................. 16151$ $$FM 10-13-06 10:49:01 PS PAGE iv For John Clayton (1943–2003), mentor and friend ................ -
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