IEICE Communications Society GLOBAL NEWSLETTER Vol. 10 Contents
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Japan Geoscience Union Meeting 2009 Presentation List
Japan Geoscience Union Meeting 2009 Presentation List A002: (Advances in Earth & Planetary Science) oral 201A 5/17, 9:45–10:20, *A002-001, Science of small bodies opened by Hayabusa Akira Fujiwara 5/17, 10:20–10:55, *A002-002, What has the lunar explorer ''Kaguya'' seen ? Junichi Haruyama 5/17, 10:55–11:30, *A002-003, Planetary Explorations of Japan: Past, current, and future Takehiko Satoh A003: (Geoscience Education and Outreach) oral 301A 5/17, 9:00–9:02, Introductory talk -outreach activity for primary school students 5/17, 9:02–9:14, A003-001, Learning of geological formation for pupils by Geological Museum: Part (3) Explanation of geological formation Shiro Tamanyu, Rie Morijiri, Yuki Sawada 5/17, 9:14-9:26, A003-002 YUREO: an analog experiment equipment for earthquake induced landslide Youhei Suzuki, Shintaro Hayashi, Shuichi Sasaki 5/17, 9:26-9:38, A003-003 Learning of 'geological formation' for elementary schoolchildren by the Geological Museum, AIST: Overview and Drawing worksheets Rie Morijiri, Yuki Sawada, Shiro Tamanyu 5/17, 9:38-9:50, A003-004 Collaborative educational activities with schools in the Geological Museum and Geological Survey of Japan Yuki Sawada, Rie Morijiri, Shiro Tamanyu, other 5/17, 9:50-10:02, A003-005 What did the Schoolchildren's Summer Course in Seismology and Volcanology left 400 participants something? Kazuyuki Nakagawa 5/17, 10:02-10:14, A003-006 The seacret of Kyoto : The 9th Schoolchildren's Summer Course inSeismology and Volcanology Akiko Sato, Akira Sangawa, Kazuyuki Nakagawa Working group for -
Trade Studies Towards an Australian Indigenous Space Launch System
TRADE STUDIES TOWARDS AN AUSTRALIAN INDIGENOUS SPACE LAUNCH SYSTEM A thesis submitted for the degree of Master of Engineering by Gordon P. Briggs B.Sc. (Hons), M.Sc. (Astron) School of Engineering and Information Technology, University College, University of New South Wales, Australian Defence Force Academy January 2010 Abstract During the project Apollo moon landings of the mid 1970s the United States of America was the pre-eminent space faring nation followed closely by only the USSR. Since that time many other nations have realised the potential of spaceflight not only for immediate financial gain in areas such as communications and earth observation but also in the strategic areas of scientific discovery, industrial development and national prestige. Australia on the other hand has resolutely refused to participate by instituting its own space program. Successive Australian governments have preferred to obtain any required space hardware or services by purchasing off-the-shelf from foreign suppliers. This policy or attitude is a matter of frustration to those sections of the Australian technical community who believe that the nation should be participating in space technology. In particular the provision of an indigenous launch vehicle that would guarantee the nation independent access to the space frontier. It would therefore appear that any launch vehicle development in Australia will be left to non- government organisations to at least define the requirements for such a vehicle and to initiate development of long-lead items for such a project. It is therefore the aim of this thesis to attempt to define some of the requirements for a nascent Australian indigenous launch vehicle system. -
Vom D Heft Nr. 258 / 18MB
W E L T R A U M - PHILATELI E Mitteilungsblatt Daheim bei Hermann Oberth: Nr. 258 ISSN 0948-6097 Jahreshauptversammlung 2015 Weltraum Philatelie e. V. 1. Vorsitzender, Geschäftsstelle : Dr. Stephen Lachhein, Schöne Aussicht 3c, 51381 Leverkusen, e-mail: [email protected] Stellv. Vorsitzender, Schriftführer, Mitteilungsblatt, Eil-Informationsdienst: Jürgen Peter Esders, Rue Paul Devigne 21-27, #6, 1030 Bruxelles, Belgien. E-mail: jpes- [email protected], Tel. +32 2 248.26.20 Schatzmeister: Michael Anderiasch, Irkensbusch 12 b, 46535 Dinslaken, Tel. 02064/970418, e-mail: [email protected] Beisitzer: Dr. Hans-Ferdinand Virnich, Bergstraße 1, 35764 Sinn, e-mail: [email protected] Siegfried Zimmerer, Stuttgarter Straße 177, 70469 Stuttgart-Feuerbach, e-mail: siegfried.zimmerer@t- online.de Mitgliedsbeitrag mit BDPh-Mitgliedschaft: 44 Euro Mitgliedsbeitrag ohne BDPh-Mitgliedschaft: 25 Euro Jugendliche: 10 Euro Bankverbindung: Kreissparkasse Waiblingen (BLZ 602 500 10), Konto Nr. 8 225 801 IBAN: DE73 6025 0010 0008 2258 01 – BIC: SOLADE S1 WBN Paypal: [email protected] Impressum : Weltraum Philatelie, Mitteilungsblatt ISSN 0948-6097 Herausgeber : Weltraum Philatelie e. V., Sitz Stuttgart, in Zusammenarbeit mit den Gmünder Weltraumfreunden, Gmünd/Österreich Verantwortlicher Redakteur (verantwortlich im Sinne der Pressegesetze): Jürgen Peter Esders, Brüssel, Belgien Auflage: bis zu 450 Exemplaren. Das Mitteilungsblatt erscheint 4 mal jährlich. Druck: Kopierbüro Schmidt, Markt 11, 01471 Radeburg, http://www.kopierschmidt.de Redaktionelle Beiträge von Vereinsmitgliedern oder Außenstehenden können ohne Begründung abge- lehnt. Kürzungen oder sinnenthaltende Textänderungen sowie eine Veröffentlichung zu einem späteren Zeitpunkt bleiben der Schriftleitung vorbehalten. Mit Verfassernamen oder Pseudonym gezeichnete Beiträge müssen nicht unbedingt mit der Meinung der Vorstandsmitglieder übereinstimmen bzw. können deren private Meinung darstellen. -
Secretariat Distr.: General 23 November 2010
United Nations ST/SG/SER.E/574 Secretariat Distr.: General 23 November 2010 Original: English Committee on the Peaceful Uses of Outer Space Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space Note verbale dated 12 August 2009 from the Permanent Mission of Japan to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of Japan to the United Nations (Vienna) presents its compliments to the Secretary-General of the United Nations and, in accordance with article IV of the Convention on Registration of Objects Launched into Outer Space (General Assembly resolution 3235 (XXIX), annex), has the honour to transmit information concerning Japanese satellites SUPERBIRD-7 (international designator 2008-038A), GOSAT “IBUKI” (international designator 2009-002A), PRISM “Hitomi” (international designator 2009-002B), SOHLA-1 “MAIDO-1” (international designator 2009-002E), SDS-1 (international designator 2009-002F) and STARS “Kukai” (international designator 2009-002G) (see annex). V.10-57969 (E) 301110 011210 *1057969* ST/SG/SER.E/574 Annex Registration data for space objects launched by Japan* SUPERBIRD-7 Committee on Space Research international 2008-038A designator: Name of flight object: SUPERBIRD-7 National designator: 2008-038A Name of launching State: Japan Date and territory or location of launch: Date and time of launch: 14 August 2008 at 20:44 hrs (GMT) Location of launch: Kourou, French Guiana Basic orbital parameters: Nodal period: 1,440 minutes Inclination: -
GPS Lessons Learned from the International Space Station, Space Shuttle and X‐38
NASA/CR‐2005‐213693 GPS Lessons Learned from the International Space Station, Space Shuttle and X‐38 John L. Goodman United Space Alliance Houston, Texas November 2005 The NASA Scientific and Technical Information Program Office ... in Profile Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. Collected advancement of aeronautics and space science. The papers from scientific and technical NASA Scientific and Technical Information (STI) conferences, symposia, seminars, or other Program Office plays a key part in helping NASA meetings sponsored or co-sponsored by maintain this important role. NASA. • SPECIAL PUBLICATION. Scientific, The NASA STI Program Office is operated by technical, or historical information from Langley Research Center, the lead center for NASA’s NASA programs, projects, and missions, scientific and technical information. The NASA STI often concerned with subjects having Program Office provides access to the NASA STI substantial public interest. Database, the largest collection of aeronautical and • TECHNICAL TRANSLATION. English- space science STI in the world. The STI Program language translations of foreign scientific Office is also NASA’s institutional mechanism for and technical material pertinent to NASA’s disseminating the results of its research and mission. development activities. These results are published by NASA in the NASA STI Report Series, which Specialized services that complement the STI includes the following report types: Program Office’s diverse offerings include creating custom thesauri, building customized databases, • TECHNICAL PUBLICATION. Reports of organizing and publishing research results ... even completed research or a major significant providing videos. phase of research that present the results of NASA programs and include extensive data or For more information about the NASA STI theoretical analysis. -
STP-11 Keynote Talk SPACE WEATHER: a Personal View J
STP-11 Keynote Talk SPACE WEATHER: A Personal View J. H. Allen (SCOSTEP) and L.J. Lanzerotti (Bell Labs and Lucent Technology) Joe Allen: Version of 2006/02/26 – Work in Progress (updating & correcting) This “shorter talk”, co-authored with Lou Lanzerotti, was prepared as a Keynote Address for SCOSTEP’s 11th Quadrennial STP Symposium held during March 2006 in Rio de Janeiro, Brazil. It is a composite of slides selected from earlier PowerPoint talks with a few new slides added about historical information and to describe recent (2005) solar activity and its consequences. The figures were selected from a number of talks given over some 35 years on different aspects of the topic of “Space Weather”, several prepared with colleagues. About 10% of the slides in the “longer talk” version are my collected old working slides prepared from viewgraph transparencies (most are not included in the “Shorter Space Weather Keynote Talk”). These slides were scanned and merged with the bulleted outline in the “Long Version”. The “Long Version” is too long to be given as a single talk. It numbers over 130 slides. It has been on-line at the SCOSTEP website since about 2001(but does not contain the newer, slides added here). However, I can select pertinent segments for focused presentations, while making the full set available on CD if someone requests it in that format. For example, this shorter talk began by moving figures about recent anomaly events to the start of the long presentation, adding historical and update slides, and presented in a 42-slide version at the STP-11 Symposium in the Keynote talk on “Space Weather” (Allen & Lanzerotti). -
H-2 Family Home Launch Vehicles Japan
Please make a donation to support Gunter's Space Page. Thank you very much for visiting Gunter's Space Page. I hope that this site is useful a nd informative for you. If you appreciate the information provided on this site, please consider supporting my work by making a simp le and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much. H-2 Family Home Launch Vehicles Japan H-2 (ETS 6) [NASDA] H-2 with SSB (SFU / GMS 5) [NASDA] H-2S (MTSat 1) [NASDA] H-2A-202 (GPM) [JAXA] 4S fairing H-2A-2022 (SELENE) [JAXA] H-2A-2024 (MDS 1 / VEP 3) [NASDA] H-2A-204 (ETS 8) [JAXA] H-2B (HTV 3) [JAXA] Version Strap-On Stage 1 Stage 2 H-2 (2 × SRB) 2 × SRB LE-7 LE-5A H-2 (2 × SRB, 2 × SSB) 2 × SRB LE-7 LE-5A 2 × SSB H-2S (2 × SRB) 2 × SRB LE-7 LE-5B H-2A-1024 * 2 × SRB-A LE-7A - 4 × Castor-4AXL H-2A-202 2 × SRB-A LE-7A LE-5B H-2A-2022 2 × SRB-A LE-7A LE-5B 2 × Castor-4AXL H-2A-2024 2 × SRB-A LE-7A LE-5B 4 × Castor-4AXL H-2A-204 4 × SRB-A LE-7A LE-5B H-2A-212 ** 1 LRB / 2 LE-7A LE-7A LE-5B 2 × SRB-A H-2A-222 ** 2 LRB / 2 × 2 LE-7A LE-7A LE-5B 2 × SRB-A H-2A-204A ** 4 × SRB-A LE-7A Widebody / LE-5B H-2A-222A ** 2 LRB / 2 × LE-7A LE-7A Widebody / LE-5B 2 × SRB-A H-2B-304 4 × SRB-A Widebody / 2 LE-7A LE-5B H-2B-304A ** 4 × SRB-A Widebody / 2 LE-7A Widebody / LE-5B * = suborbital ** = under stud y Performance (kg) LEO LPEO SSO GTO GEO MolO IP H-2 (2 × SRB) 3800 H-2 (2 × SRB, 2 × SSB) 3930 H-2S (2 × SRB) 4000 H-2A-1024 - - - - - - - H-2A-202 10000 4100 H-2A-2022 4500 H-2A-2024 5000 H-2A-204 6000 H-2A-212 -
Orbitando Satélites Orbitando Satélites Este Es Un Manual De Nuestro Taller, Orbitando Satélites
orbitando satélites orbitando satélites Este es un manual de nuestro taller, Orbitando satélites. En él queremos of“recer id”eas, recursos, técnicas e inspiración. Nuestro deseo es que sea utilizado también como guía para acercarnos a un procomún de cielo y ondas. Creemos que las tecnologías del espacio y del espectro electromagnético están impulsando una cultura limitada a intereses corporativos y de control, y en consecuencia, a un empobrecimiento de posibles matices y provocaciones en nuestras relaciones con los cielos y las frecuencias. Proponemos aquí algunas vías alternativas. A lo largo de cinco días, nos convertimos en una Agencia Espacial Autónoma Temporal . Este manual es una hoja d“e ruta de vuelo espacial y comunica”ciones no gubernamentales, no comerciales. Nuestro taller se articuló en tres bloques: Escucha y avistamiento aislamiento, se convierte en una poderosa metáfora. Nuestro de satélites, Poéticas de los satélites y Construcción de un satélite. trabajo con los satélites creó un imaginario de asociaciones y Al intentar escuchar y avistar satélites, encontramos nuevas formas apegos. A veces nos sentíamos abrumados, y otras teníamos que de utilizar los ya existentes, los que están ahí arriba ahora mismo obligarnos a despegarnos de las máquinas para reflexionar sobre en órbita. Por ejemplo, descubrimos que hacía falta paciencia los cambios que se estaban produciendo en nuestra forma de para localizar correctamente su ubicación y poder así apuntar pensar. El satélite en su órbita es materia y narrativa al mismo nuestras antenas para escucharlos cuando nos sobrevolaban. tiempo. Su existencia material, sus intenciones y su propiedad se Comprendimos que hay que superar varios niveles de dificultad pueden transformar a través de la narrativa. -
Space Security 2010
SPACE SECURITY 2010 spacesecurity.org SPACE 2010SECURITY SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security 2010 ISBN : 978-1-895722-78-9 © 2010 SPACESECURITY.ORG Edited by Cesar Jaramillo Design and layout: Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Artist rendition of the February 2009 satellite collision between Cosmos 2251 and Iridium 33. Artwork courtesy of Phil Smith. Printed in Canada Printer: Pandora Press, Kitchener, Ontario First published August 2010 Please direct inquires to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 708 Fax: 519-888-0018 Email: [email protected] iv Governance Group Cesar Jaramillo Managing Editor, Project Ploughshares Phillip Baines Department of Foreign Affairs and International Trade, Canada Dr. Ram Jakhu Institute of Air and Space Law, McGill University John Siebert Project Ploughshares Dr. Jennifer Simons The Simons Foundation Dr. Ray Williamson Secure World Foundation Advisory Board Hon. Philip E. Coyle III Center for Defense Information Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research Dr. John Logsdon The George Washington University (Prof. emeritus) Dr. Lucy Stojak HEC Montréal/International Space University v Table of Contents TABLE OF CONTENTS PAGE 1 Acronyms PAGE 7 Introduction PAGE 11 Acknowledgements PAGE 13 Executive Summary PAGE 29 Chapter 1 – The Space Environment: -
Acta Futura - Issue 2
ACT-PUB-AF0502 Acta Futura - Issue 2 Special Issue on Innovative System Concepts Editor: Dr. Dario Izzo Acta Futura: From ESA's Advanced Concepts Team Advanced Concepts Team http://www.esa.int/act a Contents Foreword By Dario Izzo and Nicholas Lan ii Electrodynamic Tethers for Exploration of Jupiter and its Icy Moons By Juan R. Sanmartin 1 Flower Constellations as Rigid Objects in Space By Daniele Mortari 7 Equilibrium Shaping By Dario Izzo and Lorenzo Petazzi 23 Coulomb Force Virtual Space Structures By Gordon Parker, Hanspeter Schaub, Arun Natarajan and Lyon King 39 Interstellar Precursor Missions using Advanced Dual-Stage Ion Propulsion Systems By Dave G. Fearn and Roger Walker 45 Formation Flying Picosat Swarms for Forming Extremely Large Apertures By Ivan Bekey 59 Agile Maneuvers for Near Earth Object (NEO) Fly-by Missions By Vaios Lappas, Bong Wie and Jozef van der Ha 67 Solar Kites for Earth Magneto-Tail Monitoring By Vaios Lappas, Bong Wie, Colin McInnes, Lorenzo Tarabini, Luis Gomes, Kotska Wallace 75 Panel Extension Satellite (PETSAT) - A Novel Satellite Concept Consisting of Modular, Functional and Plug-in Panels By Shinichi Nakasuka, Yoshiki Sugawara, Hironori Sahara, Kanichi Koyama, Takanori Okada and Chisato Kobayashi 85 i ii Foreword New ideas are often slow to penetrate mainstream space science. They usually require a lengthy gestation period to become accepted as practical tools in the design of real missions. For example, discussions in scientific literature on subjects such as formation flying or electric propulsion took place years before their implementation as methods to augment capabilities and lower costs. With a critical eye, it must therefore be possible to sift through the vast body of emerging research to find the ideas that will one day take their place in space mission design. -
Financial Operational Losses in Space Launch
UNIVERSITY OF OKLAHOMA GRADUATE COLLEGE FINANCIAL OPERATIONAL LOSSES IN SPACE LAUNCH A DISSERTATION SUBMITTED TO THE GRADUATE FACULTY in partial fulfillment of the requirements for the Degree of DOCTOR OF PHILOSOPHY By TOM ROBERT BOONE, IV Norman, Oklahoma 2017 FINANCIAL OPERATIONAL LOSSES IN SPACE LAUNCH A DISSERTATION APPROVED FOR THE SCHOOL OF AEROSPACE AND MECHANICAL ENGINEERING BY Dr. David Miller, Chair Dr. Alfred Striz Dr. Peter Attar Dr. Zahed Siddique Dr. Mukremin Kilic c Copyright by TOM ROBERT BOONE, IV 2017 All rights reserved. \For which of you, intending to build a tower, sitteth not down first, and counteth the cost, whether he have sufficient to finish it?" Luke 14:28, KJV Contents 1 Introduction1 1.1 Overview of Operational Losses...................2 1.2 Structure of Dissertation.......................4 2 Literature Review9 3 Payload Trends 17 4 Launch Vehicle Trends 28 5 Capability of Launch Vehicles 40 6 Wastage of Launch Vehicle Capacity 49 7 Optimal Usage of Launch Vehicles 59 8 Optimal Arrangement of Payloads 75 9 Risk of Multiple Payload Launches 95 10 Conclusions 101 10.1 Review of Dissertation........................ 101 10.2 Future Work.............................. 106 Bibliography 108 A Payload Database 114 B Launch Vehicle Database 157 iv List of Figures 3.1 Payloads By Orbit, 2000-2013.................... 20 3.2 Payload Mass By Orbit, 2000-2013................. 21 3.3 Number of Payloads of Mass, 2000-2013.............. 21 3.4 Total Mass of Payloads in kg by Individual Mass, 2000-2013... 22 3.5 Number of LEO Payloads of Mass, 2000-2013........... 22 3.6 Number of GEO Payloads of Mass, 2000-2013.......... -
Changes to the Database for May 1, 2021 Release This Version of the Database Includes Launches Through April 30, 2021
Changes to the Database for May 1, 2021 Release This version of the Database includes launches through April 30, 2021. There are currently 4,084 active satellites in the database. The changes to this version of the database include: • The addition of 836 satellites • The deletion of 124 satellites • The addition of and corrections to some satellite data Satellites Deleted from Database for May 1, 2021 Release Quetzal-1 – 1998-057RK ChubuSat 1 – 2014-070C Lacrosse/Onyx 3 (USA 133) – 1997-064A TSUBAME – 2014-070E Diwata-1 – 1998-067HT GRIFEX – 2015-003D HaloSat – 1998-067NX Tianwang 1C – 2015-051B UiTMSAT-1 – 1998-067PD Fox-1A – 2015-058D Maya-1 -- 1998-067PE ChubuSat 2 – 2016-012B Tanyusha No. 3 – 1998-067PJ ChubuSat 3 – 2016-012C Tanyusha No. 4 – 1998-067PK AIST-2D – 2016-026B Catsat-2 -- 1998-067PV ÑuSat-1 – 2016-033B Delphini – 1998-067PW ÑuSat-2 – 2016-033C Catsat-1 – 1998-067PZ Dove 2p-6 – 2016-040H IOD-1 GEMS – 1998-067QK Dove 2p-10 – 2016-040P SWIATOWID – 1998-067QM Dove 2p-12 – 2016-040R NARSSCUBE-1 – 1998-067QX Beesat-4 – 2016-040W TechEdSat-10 – 1998-067RQ Dove 3p-51 – 2017-008E Radsat-U – 1998-067RF Dove 3p-79 – 2017-008AN ABS-7 – 1999-046A Dove 3p-86 – 2017-008AP Nimiq-2 – 2002-062A Dove 3p-35 – 2017-008AT DirecTV-7S – 2004-016A Dove 3p-68 – 2017-008BH Apstar-6 – 2005-012A Dove 3p-14 – 2017-008BS Sinah-1 – 2005-043D Dove 3p-20 – 2017-008C MTSAT-2 – 2006-004A Dove 3p-77 – 2017-008CF INSAT-4CR – 2007-037A Dove 3p-47 – 2017-008CN Yubileiny – 2008-025A Dove 3p-81 – 2017-008CZ AIST-2 – 2013-015D Dove 3p-87 – 2017-008DA Yaogan-18