Of the President
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Collezione Per Genova
1958-1978: 20 anni di sperimentazioni spaziali in Occidente La collezione copre il ventennio 1958-1978 che è stato particolarmente importante nella storia della esplorazio- ne spaziale, in quanto ha posto le basi delle conoscenze tecnico-scientifiche necessarie per andare nello spa- zio in sicurezza e per imparare ad utilizzare le grandi potenzialità offerte dallo spazio per varie esigenze civili e militari. Nel clima di guerra fredda, lo spazio è stato fin dai primi tempi, utilizzato dagli Americani per tenere sotto con- trollo l’avversario e le sue dotazioni militari, in risposta ad analoghe misure adottate dai Sovietici. Per preparare le missioni umane nello spazio, era indispensabile raccogliere dati e conoscenze sull’alta atmo- sfera e sulle radiazioni che si incontrano nello spazio che circonda la Terra. Dopo la sfida lanciata da Kennedy, gli Americani dovettero anche prepararsi allo sbarco dell’uomo sulla Luna ed intensificarono gli sforzi per conoscere l’ambiente lunare. Fin dai primi anni, le sonde automatiche fecero compiere progressi giganteschi alla conoscenza del sistema solare. Ben presto si imparò ad utilizzare i satelliti per la comunicazione intercontinentale e il supporto alla navigazio- ne, per le previsioni meteorologiche, per l’osservazione della Terra. La Collezione testimonia anche i primi tentativi delle nuove “potenze spaziali” che si avvicinano al nuovo mon- do dei satelliti, che inizialmente erano monopolio delle due Superpotenze URSS e USA. L’Italia, con San Mar- co, diventò il terzo Paese al mondo a lanciare un proprio satellite e allestì a Malindi la prima base equatoriale, che fu largamente utilizzata dalla NASA. Alla fine degli anni ’60 anche l’Europa entrò attivamente nell’arena spaziale, lanciando i propri satelliti scientifici e di telecomunicazione dalla propria base equatoriale di Kourou. -
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. -
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. -
2017 – 2018 Recruitment Dates DISCLAIMER: Dates Subject to Change
2017 – 2018 Recruitment Dates DISCLAIMER: Dates subject to change. Information is listed in alphabetical by chapter name. Bid Day dates are included as available. Recommendations when mailed should be labeled ATTN: Membership Coordinator. Recruitment Recommendations from alumna members in good standing must be received prior to the second round of Primary Recruitment, recommendations from collegiate members need to be received prior to the first round of Primary Recruitment. Recommendations may also be sent to any chapter participating in Continuous Open Bidding. Please email our Membership Growth Specialists at [email protected] with any questions. Designation University Name Dates Mailing Address Alpha Beta University of Michigan September 15, 17, 24, 25, 27, 1322 Hill Street 28, October 2, Ann Arbor, MI 48104 October 3 Bid Day Alpha Eta Dalhousie University September 11, 13, 15, 17, 34 Jarrett Lane, C/O Catherine Savoie Hammonds September 22 Bid Day Plains, NS B4B1M9, CAN Alpha Iota Baldwin Wallace University September 22-24, Constitution South East, 144 Tressel September 24 Bid Day Berea, OH 44017 Alpha Pi Wayne State University September 13-14, 17, Box 4 Student Center Building- Wayne State September 17 Bid Day University Detroit, MI 48202 Alpha Tau Edinboro University September 5, 12, 19, 26, 5255 Lake View Drive September 28 Bid Day Edinboro, PA 16412 Alpha Upsilon Central Michigan University September 8-10, 15 607 South Main Street September 16 Bid Day Mt. Pleasant, MI 48858 Beta Alpha Nebraska Wesleyan University -
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 -
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. -
NEC Space Business
Japan Space industry Workshop in ILA Berlin Airshow 2014 NEC Space Business May 22nd, 2014 NEC Corporation Kentaro (Kent) Sakagami (Mr.) General Manager Satellite Systems and Equipment, Global Business Unit E-mail: [email protected] NEC Corporate Profile Company Name: NEC Corporation Established: July 17, 1899 Kaoru Yano Nobuhiro Endo Chairman of the Board: Kaoru Yano President: Nobuhiro Endo Capital: ¥ 397.2 billion (As of Mar. 31, 2013) Consolidated Net Sales: ¥ 3,071.6 billion (FY ended Mar. 31, 2013) Employees: 102,375 (As of Mar. 31, 2013) Consolidated Subsidiaries: 270 (As of Mar. 31, 2013) Financial results are based on accounting principles generally accepted in Japan Page 2 © NEC Corporation 2014 NEC Worldwide: “One NEC” formation in 5 regions Marketing & Service affiliates 77 in 32 countries Manufacturing affiliates 8 in 5 countries Liaison Offices 7 in 7 countries Branch Offices 7 in 7 countries Laboratories 4 in 3 countries North America Greater China NECJ EMEA APAC Latin America (As of Apr. 1, 2014) Page 3 © NEC Corporation 2014 NEC in EMEA 1 NEC in Germany NEC Deutschland GmbH NEC Display Solutions Europe NEC Laboratories Europe (Internal division of NEC Europe Ltd.) NEC Tokin Europe NEC Scandinavia AB in Espoo, 2 NEC in Netherlands Finland NEC Logistics Europe NEC Nederland B.V. NEC Neva Communications Systems NEC Scandinavia AB in Oslo, Norway NEC in the U.K. 3 NEC Scandinavia AB NEC Europe Ltd. NEC Capital (UK) plc NEC in the UK NEC Technologies (UK) NEC in Netherlands NEC Telecom MODUS Limited 3 2 NEC (UK) Ltd. -
THE BATTLE for DOMINANCE on AIRLINERS Page 18
May 2015 THE BATTLE FOR DOMINANCE ON AIRLINERS Page 18 DARPA’s tailless cargo drone/10 Cosmonaut diary/38 A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS COSMONAUT Anatoly Berezovoy (Russian Federal Space Agency) Roscosmos DIARIES 38 AEROSPACE AMERICA/MAY 2015 Copyright 2015 by the American Institute of Aeronautics and Astronautics Soviet cosmonaut Anatoly Berezovoy made only one space flight during his career, but it was one for the books. His 1982 mission, the first expedition to the Salyut 7 space station, lasted a then-record of 211 days. That record was broken 16 months later by Leonid Kizim, Vladimir Soloviev and Oleg Atkov, the third crew aboard the Salyut-7, whose mission lasted 237 days. During much of Berezovoy’s time in space — as well as afterwards — he chronicled his observations on paper. After Berezovoy died last September at age 72, his widow, Lidia Berezovaya, contacted Aerospace America through her husband’s longtime interpreter, Olga Tunison. Berezovaya and Tunison wanted to know if we were interested in publishing excerpts of his writings in English. We were very inter- ested, because the writings give a fascinating glimpse of a budding Soviet human space flight pro- gram, from the physical travails of learning to live in space to the social breakthroughs required for men and women to work together effectively in space. As commander, Berezovoy lifted off with flight engineer Valentin Lebedev on May 13, 1982 aboard the Soyuz rocket bound for Salyut 7, the final spacecraft in the Salyut series before the launch of the Mir space station. -
Part 2 Almaz, Salyut, And
Part 2 Almaz/Salyut/Mir largely concerned with assembly in 12, 1964, Chelomei called upon his Part 2 Earth orbit of a vehicle for circumlu- staff to develop a military station for Almaz, Salyut, nar flight, but also described a small two to three cosmonauts, with a station made up of independently design life of 1 to 2 years. They and Mir launched modules. Three cosmo- designed an integrated system: a nauts were to reach the station single-launch space station dubbed aboard a manned transport spacecraft Almaz (“diamond”) and a Transport called Siber (or Sever) (“north”), Logistics Spacecraft (Russian 2.1 Overview shown in figure 2-2. They would acronym TKS) for reaching it (see live in a habitation module and section 3.3). Chelomei’s three-stage Figure 2-1 is a space station family observe Earth from a “science- Proton booster would launch them tree depicting the evolutionary package” module. Korolev’s Vostok both. Almaz was to be equipped relationships described in this rocket (a converted ICBM) was with a crew capsule, radar remote- section. tapped to launch both Siber and the sensing apparatus for imaging the station modules. In 1965, Korolev Earth’s surface, cameras, two reentry 2.1.1 Early Concepts (1903, proposed a 90-ton space station to be capsules for returning data to Earth, 1962) launched by the N-1 rocket. It was and an antiaircraft cannon to defend to have had a docking module with against American attack.5 An ports for four Soyuz spacecraft.2, 3 interdepartmental commission The space station concept is very old approved the system in 1967. -
The Evolution of Commercial Launch Vehicles
Fourth Quarter 2001 Quarterly Launch Report 8 The Evolution of Commercial Launch Vehicles INTRODUCTION LAUNCH VEHICLE ORIGINS On February 14, 1963, a Delta launch vehi- The initial development of launch vehicles cle placed the Syncom 1 communications was an arduous and expensive process that satellite into geosynchronous orbit (GEO). occurred simultaneously with military Thirty-five years later, another Delta weapons programs; launch vehicle and launched the Bonum 1 communications missile developers shared a large portion of satellite to GEO. Both launches originated the expenses and technology. The initial from Launch Complex 17, Pad B, at Cape generation of operational launch vehicles in Canaveral Air Force Station in Florida. both the United States and the Soviet Union Bonum 1 weighed 21 times as much as the was derived and developed from the oper- earlier Syncom 1 and the Delta launch vehicle ating country's military ballistic missile that carried it had a maximum geosynchro- programs. The Russian Soyuz launch vehicle nous transfer orbit (GTO) capacity 26.5 is a derivative of the first Soviet interconti- times greater than that of the earlier vehicle. nental ballistic missile (ICBM) and the NATO-designated SS-6 Sapwood. The Launch vehicle performance continues to United States' Atlas and Titan launch vehicles constantly improve, in large part to meet the were developed from U.S. Air Force's first demands of an increasing number of larger two ICBMs of the same names, while the satellites. Current vehicles are very likely to initial Delta (referred to in its earliest be changed from last year's versions and are versions as Thor Delta) was developed certainly not the same as ones from five from the Thor intermediate range ballistic years ago. -
Table of Manned Space Flights Spacecalc
CBS News Manned Space Flights Current through STS-117 Table of Manned Space Flights SpaceCalc Total: 260 Crew Launch Land Duration By Robert A. Braeunig* Vostok 1 Yuri Gagarin 04/12/61 04/12/61 1h:48m First manned space flight (1 orbit). MR 3 Alan Shepard 05/05/61 05/05/61 15m:22s First American in space (suborbital). Freedom 7. MR 4 Virgil Grissom 07/21/61 07/21/61 15m:37s Second suborbital flight; spacecraft sank, Grissom rescued. Liberty Bell 7. Vostok 2 Guerman Titov 08/06/61 08/07/61 1d:01h:18m First flight longer than 24 hours (17 orbits). MA 6 John Glenn 02/20/62 02/20/62 04h:55m First American in orbit (3 orbits); telemetry falsely indicated heatshield unlatched. Friendship 7. MA 7 Scott Carpenter 05/24/62 05/24/62 04h:56m Initiated space flight experiments; manual retrofire error caused 250 mile landing overshoot. Aurora 7. Vostok 3 Andrian Nikolayev 08/11/62 08/15/62 3d:22h:22m First twinned flight, with Vostok 4. Vostok 4 Pavel Popovich 08/12/62 08/15/62 2d:22h:57m First twinned flight. On first orbit came within 3 miles of Vostok 3. MA 8 Walter Schirra 10/03/62 10/03/62 09h:13m Developed techniques for long duration missions (6 orbits); closest splashdown to target to date (4.5 miles). Sigma 7. MA 9 Gordon Cooper 05/15/63 05/16/63 1d:10h:20m First U.S. evaluation of effects of one day in space (22 orbits); performed manual reentry after systems failure, landing 4 miles from target. -
ROCKETS and MISSILES Recent Titles in Greenwood Technographies
ROCKETS AND MISSILES Recent Titles in Greenwood Technographies Sound Recording: The Life Story of a Technology David L. Morton Jr. Firearms: The Life Story of a Technology Roger Pauly Cars and Culture: The Life Story of a Technology Rudi Volti Electronics: The Life Story of a Technology David L. Morton Jr. ROCKETS AND MISSILES 1 THE LIFE STORY OF A TECHNOLOGY A. Bowdoin Van Riper GREENWOOD TECHNOGRAPHIES GREENWOOD PRESS Westport, Connecticut • London Library of Congress Cataloging-in-Publication Data Van Riper, A. Bowdoin. Rockets and missiles : the life story of a technology / A. Bowdoin Van Riper. p. cm.—(Greenwood technographies, ISSN 1549–7321) Includes bibliographical references and index. ISBN 0–313–32795–5 (alk. paper) 1. Rocketry (Aeronautics)—History. 2. Ballistic missiles—History. I. Title. II. Series. TL781.V36 2004 621.43'56—dc22 2004053045 British Library Cataloguing in Publication Data is available. Copyright © 2004 by A. Bowdoin Van Riper All rights reserved. No portion of this book may be reproduced, by any process or technique, without the express written consent of the publisher. Library of Congress Catalog Card Number: 2004053045 ISBN: 0–313–32795–5 ISSN: 1549–7321 First published in 2004 Greenwood Press, 88 Post Road West,Westport, CT 06881 An imprint of Greenwood Publishing Group, Inc. www.greenwood.com Printed in the United States of America The paper used in this book complies with the Permanent Paper Standard issued by the National Information Standards Organization (Z39.48–1984). 10987654321 For Janice P. Van Riper who let a starstruck kid stay up long past his bedtime to watch Neil Armstrong take “one small step” Contents Series Foreword ix Acknowledgments xi Timeline xiii 1.