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Ariane-5 Completes Flawless Third Test Flight
r bulletin 96 — november 1998 Ariane-5 Completes Flawless Third Test Flight A launch-readiness review conducted on Friday engine shut down and Maqsat-3 was 16 and Monday 19 October had given the go- successfully injected into GTO. The orbital ahead for the final countdown for a launch just parameters at that point were: two days later within a 90-minute launch Perigee: 1027 km, compared with the window between 13:00 to 14:30 Kourou time. 1028 ± 3 km predicted The launcher’s roll-out from the Final Assembly Apogee: 35 863 km, compared with the Building to the Launch Zone was therefore 35 898 ± 200 km predicted scheduled for Tuesday 20 October at 09:30 Inclination: 6.999 deg, compared with the Kourou time. 6.998 ± 0.05 deg predicted. On 21 October, Europe reconfirmed its lead in providing space Speaking in Kourou immediately after the flight, transportation systems for the 21st Century. Ariane-5, on its third Fredrik Engström, ESA’s Director of Launchers qualification flight, left no doubts as to its ability to deliver payloads and the Ariane-503 Flight Director, confirmed reliably and accurately to Geostationary Transfer Orbit (GTO). The new that: “The third Ariane-5 flight has been a heavy-lift launcher lifted off in glorious sunshine from the Guiana complete success. It qualifies Europe’s new Space Centre, Europe’s spaceport in Kourou, French Guiana, at heavy-lift launcher and vindicates the 13:37:21 local time (16:37:21 UT). technological options chosen by the European Space Agency.” This third Ariane-5 test flight was intended ESA’s Director -
Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object
Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object by Nathan C. Shupe B.A., Swarthmore College, 2005 A thesis submitted to the Faculty of the Graduate School of the University of Colorado in partial fulfillment of the requirements for the degree of Master of Science Department of Aerospace Engineering Sciences 2010 This thesis entitled: Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object written by Nathan C. Shupe has been approved for the Department of Aerospace Engineering Sciences Daniel Scheeres Prof. George Born Assoc. Prof. Hanspeter Schaub Date The final copy of this thesis has been examined by the signatories, and we find that both the content and the form meet acceptable presentation standards of scholarly work in the above mentioned discipline. iii Shupe, Nathan C. (M.S., Aerospace Engineering Sciences) Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object Thesis directed by Prof. Daniel Scheeres Based on the recommendations of the Augustine Commission, President Obama has pro- posed a vision for U.S. human spaceflight in the post-Shuttle era which includes a manned mission to a Near-Earth Object (NEO). A 2006-2007 study commissioned by the Constellation Program Advanced Projects Office investigated the feasibility of sending a crewed Orion spacecraft to a NEO using different combinations of elements from the latest launch system architecture at that time. The study found a number of suitable mission targets in the database of known NEOs, and pre- dicted that the number of candidate NEOs will continue to increase as more advanced observatories come online and execute more detailed surveys of the NEO population. -
Stardust Comet Flyby
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Stardust Comet Flyby Press Kit January 2004 Contacts Don Savage Policy/Program Management 202/358-1727 NASA Headquarters, Washington DC Agle Stardust Mission 818/393-9011 Jet Propulsion Laboratory, Pasadena, Calif. Vince Stricherz Science Investigation 206/543-2580 University of Washington, Seattle, WA Contents General Release ……………………………………......………….......................…...…… 3 Media Services Information ……………………….................…………….................……. 5 Quick Facts …………………………………………..................………....…........…....….. 6 Why Stardust?..................…………………………..................………….....………......... 7 Other Comet Missions ....................................................................................... 10 NASA's Discovery Program ............................................................................... 12 Mission Overview …………………………………….................……….....……........…… 15 Spacecraft ………………………………………………..................…..……........……… 25 Science Objectives …………………………………..................……………...…........….. 34 Program/Project Management …………………………...................…..…..………...... 37 1 2 GENERAL RELEASE: NASA COMET HUNTER CLOSING ON QUARRY Having trekked 3.2 billion kilometers (2 billion miles) across cold, radiation-charged and interstellar-dust-swept space in just under five years, NASA's Stardust spacecraft is closing in on the main target of its mission -- a comet flyby. "As the saying goes, 'We are good to go,'" said project manager Tom Duxbury at NASA's Jet -
Annual Report 2018
RAPPORT D'ACTIVITÉ ANNUAL REPORT 2018 Mission InSight-SEIS La France sur Mars InSight-SEIS mission France on Mars 4 ÉDITORIAL FOREWORD Avec ses coopérations sur tous les continents, le CNES est une référence incontournable 2018 a été Nous sommes aussi partis vers la steppe du Kazakhstan, au retour sur particulièrement Mercure avec le lancement de la sonde Terre de Thomas Pesquet, il avait eu BepiColombo le 26 octobre, sans oublier l’intuition de ce projet. réussie pour le CNES que le 3 octobre, l’atterrisseur Mascot Nous avons donc immédiatement s’était posé sur l’astéroïde Ryugu. avec des succès partagé cette idée avec nos Côté observation, nous avons bien partenaires du monde entier et le SCO majeurs : lancement terminé l’année avec le lancement des satellites CFOSat, de MetOp-C et auparavant, nous a été lancé par Frédérique Vidal, le MetOp-C, CSO-1 avions lancé avec la Chine, CFOSat 11 décembre 2017 lors de la première pour l’étude du vent et des vagues. édition du One Planet Summit et et de la sonde présenté à de nombreux Chefs d’État interplanétaire En matière de télécommunications, à New-York, le 26 septembre 2018. BepiColombo, l’année a aussi été intense avec le La signature de l’acte fondateur du succès planétaire de la constellation SCO sera l’un des temps forts de 2019 naissance du SCO Galileo et avec la décision de et rappellera que les satellites sont (le Space Climate développer le satellite Konnect pour incontournables dans la lutte contre Observatory), création que la totalité des habitants de le changement climatique. -
Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology
Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology Yuichi Tsuda Project Manager, Hayabusa2 Japan Aerospace ExplorationAgency 58th COPUOS, April 23, 2021 Lunar and Planetary Science Missions of Japan 1980 1990 2000 2010 2020 Future Plan Moon 2007 Kaguya 1990 Hiten SLIM Lunar-A × Venus 2010 Akatsuki 2018 Mio 1998 Nozomi × Planets Mercury (Mars) 2010 IKAROS Venus MMX Phobos/Mars 1985 Suisei 2014 Hayabusa2 Small Bodies Asteroid Ryugu 2003 Hayabusa 1985 Sakigake Asteroid Itokawa Destiny+ Comet Halley Comet Pheton 2 Hayabusa2 Mission ✓ Sample return mission to a C-type asteroid “Ryugu” ✓ 5.2 billion km interplanetary journey. Launch Earth Gravity Assist Ryugu Arrival MINERVA-II-1 Deployment Dec.3, 2014 Sep.21, 2018 Dec.3, 2015 Jun.27, 2018 MASCOT Deployment Oct.3, 2018 Ryugu Departure Nov.13.2019 Kinetic Impact Earth Return Second Dec.6, 2020 Apr.5, 2019 Target Markers Orbiting Touchdown Sep.16, 2019 Jul,11, 2019 First Touchdown Feb.22, 2019 MINERVA-II-2 Orbiting MD [D VIp srvlxp #534<# Oct.2, 2019 Hayabusa2 Spacecraft Overview Deployable Xband Xband Camera (DCAM3) HGA LGA Xband Solar Array MGA Kaba nd Ion Engine HGA Panel RCS thrusters ×12 ONC‐T, ONC‐W1 Star Trackers Near Infrared DLR MASCOT Spectrometer (NIRS3) Lander Thermal Infrared +Z Imager (TIR) Reentry Capsule +X MINERVA‐II Small Carry‐on +Z LIDAR ONC‐W2 +Y Rovers Impactor (SCI) +X Sampler Horn Target +Y Markers ×5 Launch Mass: 609kg Ion Engine: Total ΔV=3.2km/s, Thrust=5-28mN (variable), Specific Impulse=2800- 3000sec. (4 thrusters, mounted on two-axis gimbal) Chemical RCS: Bi-prop. -
Analysis of MIRO/Rosetta Data
Analysis of MIRO/Rosetta Data Dissertation zur Erlangung des mathematisch-naturwissenschaftlichen Doktorgrades “Doctor rerum naturalium” der Georg-August-Universität Göttingen im Promotionsprogramm PROPHYS der Georg-August University School of Science (GAUSS) vorgelegt von David Marshall aus Norwich, Vereinigtes Königreich Göttingen, 2018 Betreuungsausschuss Dr. Paul Hartogh Max-Planck-Institut für Sonnensystemforschung, Göttingen Prof. Dr. Stefan Dreizler Institut für Astrophysik, Georg-August-Universität Göttingen Mitglieder der Prüfungskommision Referent: Dr. Paul Hartogh Max-Planck-Institut für Sonnensystemforschung, Göttingen Korreferent: Prof. Dr. Stefan Dreizler Institut für Astrophysik, Georg-August-Universität Göttingen Weitere Mitglieder der Prüfungskommission: Prof. Dr. Ulrich Christensen Max-Planck-Institut für Sonnensystemforschung, Göttingen Prof. Dr. Ariane Frey II. Physikalisches Institut, Georg-August-Universität Göttingen Prof. Dr. Thorsten Hohage Institut für Numerische und Angewandte Mathematik, Georg-August-Universität Göttin- gen Prof. Dr. Andreas Pack Geowissenschaftliches Zentrum, Georg-August-Universität Göttingen Tag der mündlichen Prüfung: 19.12.2018 Bibliografische Information der Deutschen Nationalbibliothek Die Deutsche Nationalbibliothek verzeichnet diese Publikation in der Deutschen Nationalbibliografie; detaillierte bibliografische Daten sind im Internet über http://dnb.d-nb.de abrufbar. ISBN 978-3-944072-65-4 uni-edition GmbH 2019 http://www.uni-edition.de c David Marshall This work is distributed under a Creative Commons Attribution 3.0 License Printed in Germany Contents Summary9 Zusammenfassung 11 1 Introduction 13 1.1 Comets................................... 13 1.2 Observational history: from the stone age to the space age........ 16 1.3 The Rosetta mission............................. 21 1.4 67P/Churyumov-Gerasimenko....................... 24 1.5 The Microwave Instrument for the Rosetta orbiter............. 28 1.6 MIRO aims, results and spectra....................... 32 1.7 Thesis aims................................ -
ARIANE 5 Data Relating to Flight 225
KOUROU August 2015 ARIANE 5 Data relating to Flight 225 EUTELSAT 8 West B Intelsat 34 Data relating to Flight 225 Flight 225 Ariane 5 Satellites: EUTELSAT 8 WEST B – INTELSAT 34 Content 1. Introduction .................................................................... 3 2. Launcher L579 ............................................................... 4 3. Mission V225 ............................................................... 10 4. Payloads ...................................................................... 19 5. Launch campaign ........................................................ 32 6. Launch window ............................................................ 35 7. Final countdown .......................................................... 36 8. Flight sequence ........................................................... 40 9. Airbus Defence and Space and the ARIANE programmes ........................................................................ 42 2 Data relating to Flight 225 1. Introduction Flight 225 is the 81st Ariane 5 launch and the fourth in 2015. It follows on from a series of 66 consecutive successful Ariane 5 launches. This is the 51st ARIANE 5 ECA (Cryogenic Evolution type A), the most powerful version in the ARIANE 5 range. Flight 225 is a commercial mission for Ariane 5. The L579 launcher is the twenty-fifth to be delivered by Airbus Defence and Space to Arianespace as part of the PB production batch. The PB production contract was signed in March 2009 to guarantee continuity of the launch service after completion -
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 -
The President's Commission on Implementation of US Space Exploration Policy
The President’s Commission on Implementation of US Space Exploration Policy Testimony By Philippe Berterottière Senior Vice President Sales, Marketing & Customer Programs Arianespace SA Arianespace - May 3, 2004 Who We Are • Founded in 1980 • The world’s 1st commercial launch services provider • Signed over 250 contracts • Launched majority of commercial satellites in orbit • >50% of our business is with US manufacturers/operators • Privately held European company with 44 Shareholders from 13 European nations • Arianespace is the prime contractor to ESA for marketing, sales, integration and launch of Europe’s family of vehicles Arianespace - May 3, 2004 2 Family of Launch Vehicles • Serves European launch policy to optimize resources and address all market segments • A contract with ESA provides Arianespace with the rights to operate Europe’s family of launch vehicles • Arianespace operates 3 systems from French Guiana The heavy-lift Ariane 5 (operational) The medium-lift Soyuz ST (from 2006) The light-lift Vega (from 2006) • Arianespace is currently involved in Soyuz operations from Baikonur through our sister company Starsem Arianespace - May 3, 2004 3 Ariane 5 Current Configurations & Capabilities LEO GTO Moon (mt) (mt) (mt) Ariane 5 Generic 6.8 Ariane 5 ECA 10 7.5 Ariane 5 ES/V 21 ARIANE 5 Configuration Under Evaluation Ariane 5 ECB 23 12 9 With the two solid propellant boosters and the central core of Ariane 5, there is a tool kit to build a super-heavy vehicle, should the need arise Arianespace - May 3, 2004 Facilities • We launch -
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. -
Japanese Reflections on World War II and the American Occupation Japanese Reflections on World War II and the American Occupation Asian History
3 ASIAN HISTORY Porter & Porter and the American Occupation II War World on Reflections Japanese Edgar A. Porter and Ran Ying Porter Japanese Reflections on World War II and the American Occupation Japanese Reflections on World War II and the American Occupation Asian History The aim of the series is to offer a forum for writers of monographs and occasionally anthologies on Asian history. The Asian History series focuses on cultural and historical studies of politics and intellectual ideas and crosscuts the disciplines of history, political science, sociology and cultural studies. Series Editor Hans Hägerdal, Linnaeus University, Sweden Editorial Board Members Roger Greatrex, Lund University Angela Schottenhammer, University of Salzburg Deborah Sutton, Lancaster University David Henley, Leiden University Japanese Reflections on World War II and the American Occupation Edgar A. Porter and Ran Ying Porter Amsterdam University Press Cover illustration: 1938 Propaganda poster “Good Friends in Three Countries” celebrating the Anti-Comintern Pact Cover design: Coördesign, Leiden Lay-out: Crius Group, Hulshout Amsterdam University Press English-language titles are distributed in the US and Canada by the University of Chicago Press. isbn 978 94 6298 259 8 e-isbn 978 90 4853 263 6 doi 10.5117/9789462982598 nur 692 © Edgar A. Porter & Ran Ying Porter / Amsterdam University Press B.V., Amsterdam 2017 All rights reserved. Without limiting the rights under copyright reserved above, no part of this book may be reproduced, stored in or introduced into a retrieval system, or transmitted, in any form or by any means (electronic, mechanical, photocopying, recording or otherwise) without the written permission of both the copyright owner and the author of the book. -
JAXA's Planetary Exploration Plan
Planetary Exploration and International Collaboration Institute of Space and Astronautical Science Japan Aerospace Exploration Agency Yoshio Toukaku, Director for International Strategy and Coordination Naoya Ozaki, Assistant Professor, Dept of Spacecraft Engineering ISAS/JAXA September, 2019 The Path Japanese Planetary Exploration 1985 1995 2010 2018 Sakigake/ Nozomi Akatsuki BepiColombo Suisei MMO/MPO Comet flyby Planned and Venus Climate Mercury Orbiter launched Mars Orbiter orbiter Asteroid Sample Asteroid Sample Martian Moons Lunar probe Return Mission Return Mission explorer Hiten Hayabusa Hayabusa2 MMX 1992 2003 2014 2020s (TBD) Recent Science Missions HAYABUSA 2003-2010 HINODE(SOLAR-B)2006- KAGUYASELENE)2007-2009 Asteroid Explorer SolAr OBservAtion Lunar Exploration AKATSUKI 2010- Venus Meteorology IKAROS 2010 HisAki 2013 SolAr SAil PlAnetary atmosphere HAYABUSA2 2014-2020 Hitomi(ASTRO-H) 2016 ArAse (ERG) 2016 Asteroid Explorer X-Ray Astronomy Van Allen Belt proBe Hayabusa & Hayabusa 2 Asteroid Sample Return Missions “Hayabusa” spacecraft brought back the material of Asteroid Itokawa while establishing innovative ion engines. “Hayabusa2”, while utilizing the experience cultivated in “Hayabusa”, has arrived at the C type Asteroid Ryugu in order to elucidate the origin and evolution of the solar system and primordial materials that would have led to emergence of life. Hayabusa Hayabusa2 Target Itokawa Ryugu Launch 2003 2014 Arrival 2005 2018 Return 2010 2020 ©JAXA Asteroid Ryugu 6 Martian Moons eXploration (MMX) Sample return from Marian moon for detailed analysis. Strategic L-Class A key element in the ISAS roadmap for small body exploration. Phase A n Science Objectives 1. Origin of Mars satellites. - Captured asteroids? - Accreted debris resulting from a giant impact? 2. Preparatory processes enabling to the habitability of the solar system.