New Earth-Space Technologies a Research Strategy
Total Page:16
File Type:pdf, Size:1020Kb

Load more
Recommended publications
-
Multiple Polar Cap Arcs: Akebono &Lpar;Exos D&Rpar; Observations
Radio Science,Volume 31, Number 3, Pages645-653, May-June 1996 Multiple polar cap arcs: Akebono (Exos D) observations T. Obara, T. Mukai, H. Hayakawa, K. Tsuruda, A. Matsuoka, and A. Nishida Institute of Spaceand AstronauticalScience, Kanagawa, Japan H. Fukunishi Department of Geophysicsand Astrophysics,Tohoku University,Sendai, Japan Center for Atmosphericand SpaceSciences, Utah State University,Logan Abstract. Akebono (Exos D) observationsdemonstrate that polar cap arcssometimes have a fine structure,that is, multiple (doubleor triple) arcswith spacingof a few tens of kilometers.The multiplepolar cap arcsare dominantlyobserved in the nightsidepolar cap region, suggestingthat low backgroundconductance favors the appearanceof the structuredarcs. A relationshipbetween the spacingand the averageenergy of the precipitatingelectrons is investigated.Results show that a higher energyleads to a wider spacing.Akebono observationsalso showthe existenceof a downwardcurrent region embeddedbetween upward current regions (arcs). Comparison of the observationswith resultsfrom a coupledmagnetosphere-ionosphere Sun-aligned arc model is made, which showsgood qualitativeagreement between the modelingand observationalresults on the spacing-energydependence and the effect of backgroundionospheric conductance. Introduction dawn-to-duskcomponent of the electric field is the major contributorto the negativedivE. These results The electronsreaching low altitudes in the polar suggestthat localized electron precipitation in the cap region were categorized as "polar -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Mp-Ist-056-32
UNCLASSIFIED/UNLIMITED The International Reference Ionosphere – Climatological Standard for the Ionosphere Dieter Bilitza Raytheon IS, Space Physics Data Facility GSFC, Code 612.4 Greenbelt, MD 20771 U.S.A. [email protected] ABSTRACT The International Reference Ionosphere (IRI) a joint project of URSI and COSPAR is the defacto standard for a climatological specification of ionospheric parameters. IRI is based on a wide range of ground and space data and has been steadily improved since its inception in 1969 with the ever-increasing volume of ionospheric data and with better mathematical descriptions of the observed global and temporal variation patterns. The IRI model has been validated with a large amount of data including data from the most recent ionospheric satellites (KOMPSAT, ROCSAT and TIMED) and data from global network of ionosondes. Several IRI teams are working on specific aspects of the IRI modeling effort including an improved representation of the topside ionosphere with a seamless transition to the plasmasphere, a new effort to represent the global variation of F2 peak parameters using the Neural Network (NN) technique, and the inclusion of several additional parameters in IRI, e.g., spread-F probability and ionospheric variability. Annual IRI workshops are the forum for discussions of these efforts and for all science activities related to IRI as well as applications of the IRI model in engineering and education. In this paper I will present a status report about the IRI effort with special emphasis on the presentations and results from the most recent IRI Workshops (Paris, 2004; Tortosa, 2005) and on the most important ongoing IRI activities. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Jaxa Today 10.Pdf
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. We examine the H3’s unique features and the development program’s pinned by this philosophy, JAXA pursues a broad range of pro- objectives. -
The Need for Detailed Ionic Composition of the Near-Earth Plasma
HeliophysicsHELIO 2050 2050 White Papers (2021) R. Ilie4094.pdf THE NEED FOR DETAILED IONIC COMPOSITION OF THE NEAR-EARTH PLASMA An impressive body of work has been devoted to the escape of H+, He+ and O+ ions from Earth’s ionosphere, and their circulation and redistribution throughout the terrestrial magneto- sphere (Schunk and Raitt, 1980; Schunk and Sojka, 1997; Winglee et al., 2002; Glocer et al., 2009; Ilie et al., 2015; Ilie and Liemohn, 2016). However, the transport and energization of N+, in addi- tion to that of O+, has not been considered by most studies, even though a number of direct and indirect measurements made to describe the ionic composition of the ionosphere-magnetosphere system, have established that N+ is a significant ion species in the ionosphere and its presence in the magnetosphere is significant. A wide range in the magnitude oftheN+ to O+ density ratio has been reported, with significant variations not only with geomagnetic activity, but also with solar cycle, season, time of day, latitude, etc (Mall et al., 2002; Christon et al., 2002). These vari- ations suggest that N+ and O+, while relatively close in mass, they obey different chemical and energization processes, and possibly follow different paths of energization. In addition, observations from the WIND STICS ISIS 2 spacecraft (Hoffman et al., 1974) indicated that not only N+, but also molecular ions were ob- served in the Earth’s magnetosphere Geotail STICS AMPTE and ionosphere. Measurements from CCE Explorer 31 Akebono SMS the Arase satellite (Miyoshi et al., MMS ISIS-2 IMS DE-1 RIMSS e-POP 2018) showed the existence of molec- OGO-6 OGOGO-2-2 IMSS Sputnik3 IMS AE-C ular ions in the Earth’s ring cur- RMS IMS rent region, even under moderate ge- omagnetic storm conditions. -
Modeling Seasonal Variations of Auroral Particle Precipitation in a Global-Scale Magnetosphere-Ionosphere Simulation M
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 114, A01204, doi:10.1029/2008JA013108, 2009 Modeling seasonal variations of auroral particle precipitation in a global-scale magnetosphere-ionosphere simulation M. Wiltberger,1 R. S. Weigel,2 W. Lotko,3 and J. A. Fedder4 Received 20 February 2008; revised 8 September 2008; accepted 6 November 2008; published 14 January 2009. [1] A variety of observations have shown strong seasonal variations in a vast array of magnetosphere-ionosphere parameters, including field-aligned currents, cross polar cap potential, and precipitating electron energy flux. In this paper we examine how these variations are modeled in the Lyon-Fedder-Mobarry (LFM) global-scale magnetohydrodynamic simulation of the coupled solar wind-magnetosphere-ionosphere system. In order to account for changes in the solar wind conditions caused by the seasonal variation of the Earth’s dipole tilt we carefully select the solar wind parameters so that the effective driving conditions are the same across the March, June, and December intervals examined. The seasonal variation of the field-aligned current strengths is in good agreement with observations, with the sunlit hemisphere having more current than the dark hemisphere in the June and December intervals. However, in order to bring the modeled precipitating electron energy flux into better agreement with the observations we need to utilize a modified current-voltage relationship which includes a proxy for illumination effects. We provide a detailed description of the LFM’s magnetosphere-ionosphere coupling interface including how illumination effects are incorporated into the model. This methodology for including these effects does not allow for determining if changes in conductance or ionospheric density are responsible for the changes. -
Introduction to the Akebono (EXOS-D) Satellite Observations
J. Geomag. Geoelectr., 42, 367-370, 1990 Introduction to the Akebono (EXOS-D) Satellite Observations By studies during the last decade of the 1970s, it has become clear that auroral particles are not directly injected from the tail region of the magnetosphere butthat there are instead two steps involved in the acceleration mechanism. The first step of the energization process occurs in the tail region of the magnetosphere while the second is found in the spatial region where the electric field is developed in a direction parallel to the earth's magnetic field. It is believed that the region of this electric fieldexists between a range of altitude of 3,000 km to 20,000km, centering around 6,000km, on fieldlines connected to the polar ionosphere. Although the general features of these acceleration processes have been identified based on previous satellite observations, there still are basic questions that remain unsolved about the physics of the acceleration region. i) What is the initial causative agent for the formation of the acceleration region? Is it induced by fast plasma injection, high energy electrons, or by magnetic field as original currents? ii) Are the particles accelerated by an electrostatic shock, a double layer, or growing large amplitude waves? iii) How is the development of the regions of acceleration related to the occurrence of magnetospheric disturbances, called substorms? The EXOS-D satellite was designed to seek solutions to these questions by conducting direct observations of the particle acceleration regions above the auroral region, with eight scientific instruments: a) Electric field detector (EFD), b) Magnetic field detector (MGF), c) Very low frequency plasma wave detectors (VLF), d) Plasma wave detectors in high frequency range and sounder (PWS), e) Low energy particle spectra analyzer (LEP), f) Suprathermal mass spectrometer (SMS), g) Temperature and energy distribution of plasma (TED), h) Auroral television camera (ATV). -
Polar Topside Ionosphere During Geomagnetic Storms: Comparison
Radio Science RESEARCH ARTICLE Polar Topside Ionosphere During Geomagnetic Storms: 10.1029/2018RS006589 Comparison of ISIS-II With TDIM Special Section: J. J. Sojka1,2 , D. Rice2 , V. Eccles2 , M. David1 , R. W. Schunk1 , R. F. Benson3 , URSI General Assembly and and H. G. James4 Scientific Symposium (2017) 1Center for Atmospheric and Space Sciences, Utah State University, Logan, UT, USA, 2Space Environment Corporation, 3 Key Points: Logan, UT, USA, Geospace Physics Laboratory, Heliophysics Science Division, NASA Goddard Space Flight Center, • The paper focuses on prestorm and Greenbelt, MD, USA, 4Natural Resources Canada Geomagnetic Laboratory, Ottawa, Ontario, Canada main phase topside ionospheric response to a mild and a severe geomagnetic storm Abstract Space weather deposits energy into the high polar latitudes, primarily via Joule heating that is • Simulations from an extensively used associated with the Poynting flux electromagnetic energy flow between the magnetosphere and F region model, TDIM, are compared fl fi to ISIS-II topside ionosphere ionosphere. One way to observe this energy ow is to look at the ionospheric electron density pro le observations (EDP), especially that of the topside. The altitude location of the ionospheric peak provides additional • Surprisingly, the TDIM is unable to information on the net field-aligned vertical transport at high latitudes. To date, there have been few simulate the observed storm response while satisfactorily studies in which physics-based ionospheric model storm simulations have been compared with topside simulating the prestorm topside EDPs. A rich database of high-latitude topside ionograms obtained from polar orbiting satellites of the International Satellites for Ionospheric Studies (ISIS) program exists but has not been utilized in comparisons with physics-based models. -
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 -
AUTOMATED NEAR REAL TIME RADARSAT-2 IMAGE GEO-PROCESSING and ITS APPLICATION for SEA ICE and OIL SPILL MONITORING )/,( )/,( Vugy
AUTOMATED NEAR REAL TIME RADARSAT-2 IMAGE GEO-PROCESSING AND ITS APPLICATION FOR SEA ICE AND OIL SPILL MONITORING Ziqiang Ou Canadian Ice Service, Environment Canada 373 Sussex Drive, Ottawa, Canada K1A 0H3 - [email protected] KEY WORDS: RADARSAT, SAR, Georeferencing, Real-time, Pollution, Snow Ice, Detection ABSTRACT: Synthetic aperture radar (SAR) data from RADARSAT-1 are an important operational data source for several ice centres around the world. Sea ice monitoring has been the most successful real-time operational application for RADARSAT-1 data. These data are used by several national ice services as a mainstay of their programs. Most recently, Canadian Ice Service launched another new real-time operational program called ISTOP (Integrated Satellite Tracking Of Pollution). It uses the RADARSAT-1 data to monitor ocean and lakes for oil slicks and tracking the polluters. In this paper, we consider the ice information requirements for operational sea ice monitoring and the oil slick and target detection requirements for operational ISTOP program at the Canadian Ice Service (CIS), and the potential for RADARSAT-2 to meet those requirements. Primary parameters are ice-edge location, ice concentration, and stage of development; secondary parameters include leads, ice thickness, ice topography and roughness, ice decay, and snow properties. Iceberg detection is an additional ice information requirement. The oil slick and ship target detection are the basic requirements for the surveillance and pollution control. 1. INTRODUCTION 2. GEOMETRIC TRANSFORMATION RADARSAT-2 products are provided in a GeoTIFF format There are two major techniques for correcting geometric with a sets of support XML files for all products except the distortion present in an image. -
MIT Japan Program Working Paper 01.10 the GLOBAL COMMERCIAL
MIT Japan Program Working Paper 01.10 THE GLOBAL COMMERCIAL SPACE LAUNCH INDUSTRY: JAPAN IN COMPARATIVE PERSPECTIVE Saadia M. Pekkanen Assistant Professor Department of Political Science Middlebury College Middlebury, VT 05753 [email protected] I am grateful to Marco Caceres, Senior Analyst and Director of Space Studies, Teal Group Corporation; Mark Coleman, Chemical Propulsion Information Agency (CPIA), Johns Hopkins University; and Takashi Ishii, General Manager, Space Division, The Society of Japanese Aerospace Companies (SJAC), Tokyo, for providing basic information concerning launch vehicles. I also thank Richard Samuels and Robert Pekkanen for their encouragement and comments. Finally, I thank Kartik Raj for his excellent research assistance. Financial suppport for the Japan portion of this project was provided graciously through a Postdoctoral Fellowship at the Harvard Academy of International and Area Studies. MIT Japan Program Working Paper Series 01.10 Center for International Studies Massachusetts Institute of Technology Room E38-7th Floor Cambridge, MA 02139 Phone: 617-252-1483 Fax: 617-258-7432 Date of Publication: July 16, 2001 © MIT Japan Program Introduction Japan has been seriously attempting to break into the commercial space launch vehicles industry since at least the mid 1970s. Yet very little is known about this story, and about the politics and perceptions that are continuing to drive Japanese efforts despite many outright failures in the indigenization of the industry. This story, therefore, is important not just because of the widespread economic and technological merits of the space launch vehicles sector which are considerable. It is also important because it speaks directly to the ongoing debates about the Japanese developmental state and, contrary to the new wisdom in light of Japan's recession, the continuation of its high technology policy as a whole.