Short-Term Variability and Mass Loss in Be Stars I
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The History Problem: the Politics of War
History / Sociology SAITO … CONTINUED FROM FRONT FLAP … HIRO SAITO “Hiro Saito offers a timely and well-researched analysis of East Asia’s never-ending cycle of blame and denial, distortion and obfuscation concerning the region’s shared history of violence and destruction during the first half of the twentieth SEVENTY YEARS is practiced as a collective endeavor by both century. In The History Problem Saito smartly introduces the have passed since the end perpetrators and victims, Saito argues, a res- central ‘us-versus-them’ issues and confronts readers with the of the Asia-Pacific War, yet Japan remains olution of the history problem—and eventual multiple layers that bind the East Asian countries involved embroiled in controversy with its neighbors reconciliation—will finally become possible. to show how these problems are mutually constituted across over the war’s commemoration. Among the THE HISTORY PROBLEM THE HISTORY The History Problem examines a vast borders and generations. He argues that the inextricable many points of contention between Japan, knots that constrain these problems could be less like a hang- corpus of historical material in both English China, and South Korea are interpretations man’s noose and more of a supportive web if there were the and Japanese, offering provocative findings political will to determine the virtues of peaceful coexistence. of the Tokyo War Crimes Trial, apologies and that challenge orthodox explanations. Written Anything less, he explains, follows an increasingly perilous compensation for foreign victims of Japanese in clear and accessible prose, this uniquely path forward on which nationalist impulses are encouraged aggression, prime ministerial visits to the interdisciplinary book will appeal to sociol- to derail cosmopolitan efforts at engagement. -
The US Response to China's ASAT Test
Air University Allen G. Peck, Lt Gen, Commander Air Force Research Institute John A. Shaud, Gen, PhD, USAF, Retired, Director School of Advanced Air and Space Studies Gerald S. Gorman, Col, PhD, Commandant John B. Sheldon, PhD, Thesis Advisor AIR UNIVERSITY AIR FORCE RESEARCH INSTITUTE The US Response to China’s ASAT Test An International Security Space Alliance for the Future ANTHONY J. MASTALIR Lieutenant Colonel, USAF Drew Paper No. 8 Air University Press Maxwell Air Force Base, Alabama 36112-5962 August 2009 Muir S. Fairchild Research Information Center Cataloging Data Mastalir, Anthony J. The US response to China’s ASAT test : an international security space alliance for the future / Anthony J. Mastalir. p. ; cm. – (Drew paper, 1941-3785 ; no. 8) Includes bibliographical references. ISBN 978-1-58566-197-8 1. Astronautics—International cooperation. 2. Astronautics and civilization. 3. Astronautics and state. 4. United States—Foreign relations—China. 5. China— Foreign relations—United States. 6. Anti-satellite weapons—China. I. Title. II. Series. 333.94—dc22 Disclaimer Opinions, conclusions, and recommendations expressed or implied within are solely those of the author and do not necessarily represent the views of Air University, the United States Air Force, the Department of Defense, or any other US government agency. Cleared for public release: distribution unlimited. This Drew Paper and others in the series are available electronically at the Air University Research Web site http://research.maxwell.af.mil and the AU Press Web site http://aupress.au.af.mil. ii The Drew Papers The Drew Papers are occasional publications sponsored by the Air Force Research Institute (AFRI), Maxwell AFB, Alabama. -
DRAGON - 8U Nanosatellite Orbital Deployer
DRAGON - 8U Nanosatellite Orbital Deployer Marcin Dobrowolski*, Jerzy Grygorczuk*Â ÃB_*, Marta Tokarz* and Maciej Borys* Abstract The Space Research Centre of the Polish Academy of Sciences (SRC PAS) together with Astronika company have developed an Orbital Deployer called DRAGON for ejection of the Polish scientific nanosatellite BRITE-PL Heweliusz (Fig. 1). The device has three unique mechanisms including an adopted and scaled lock and release mechanism from the ESA Rosetta mission MUPUS instrument. This paper discusses major design restrictions of the deployer, unique design features, and lessons learned from development through testing. Introduction BRITE Constellation is a group of scientific nanosatellites whose purpose is to study oscillations in the light intensity of the most luminous stars (brighter than magnitude +3.5) in our galaxy. The observations will have a precision at least 10 times better than achievable using ground-based observations. The BRITE (BRight Target Explorer) mission formed by Austria, Canada and Poland will send to space a constellation of six nanosatelites, two from each country. BRITE-PL satellite is based on the Generic Nanosatellite Bus (GNB) from the Canadian SFL/UTIAS (Space Flight Laboratory / University of Toronto, Institute for Aerospace Studies). The spacecraft are to use the SFL XPOD (Experimental Push Out Deployer) as a separation system. Figure 1. DRAGON Orbital Deployer and BRITE-PL Heweliusz Spacecraft (in a safety box) * Space Research Centre of the Polish Academy of Sciences, Warsaw, Poland ! " # 487 The first scientific satellite, BRITE-PL Lem, is a modified version of the original SFL design. The second one, BRITE-PL Heweliusz, has the significant changes – it carries additional technological experiments implemented by SRC PAS. -
Ham Hum December 13.Pub
Ham Hum December 2013 The official newsletter of Hamilton Amateur The official newsletter of Radio Club Inc. Serving the Hamilton The Hamilton Amateur Radio Club (Inc.) Community for over 80 Years Branch 12 of NZART -- ZL1UX ZL1UX Active in Hamilton since 1923 Next Meeting : BBQ : Sat 7th December 11am start Disclaimer: The Hamilton Amateur Radio Club (Inc) accepts no responsibility f or opinions expressed in this publication. Where possible, the articles source details will be published. Copyright remains with the author or HARC. All rights reserved. Contact Details Patron: Appointment pending President: “Jono” Jonassen ZL1UPJ [email protected] Vice Presidents: Gary Lodge ZL1GA Gav in Petrie ZL1GWP 843 0326 [email protected] Secretary: Phil King ZL1PK 847 1320 [email protected] AREC Section Leader: Mike Sanders ZL2MGS 855 1612 [email protected] Deputy Section Leaders: “Jono” Jonassen ZL1UPJ Phil King ZL1PK 847 1320 [email protected] Treasurer: Tom Powell ZL1TJA 834 3461 [email protected] Committee: Robin Holdsworth ZL1IC 855 4786 Colin McEwen ZL2CMC Cameron Mumford ZL1CNM Kev in Murphy ZL1UJG Terry O’Loan ZL1TNO Mike Sanders ZL2MGS 855 1612 [email protected] Ham Hum Editor: David King ZL1DGK 579 9930 [email protected] Ham Hum Printer: John Nicholson ZL1AUB 855 5435 ATV Co-ordinators: Phil King ZL1PK 847 1320 [email protected] Robin Holdsworth ZL1IC 855 4786 Market Day Co-ordinator: [email protected] Robin Holdsworth ZL1IC 855 4786 Webmaster: Gav in Petrie ZL1GWP 843 0326 [email protected] BBS Team: Phil King (sysop) ZL1PK 847 1320 [email protected] Alan Wallace ZL1AMW 843 3738 [email protected] Doug Faulkner ZL4FS 855 1214 Gav in Petrie ZL1GWP 843 0326 [email protected] Club Custodian: Currently v acant Equipment Officer/Quartermaster: Colin McEwen ZL2CMC 849 2492 QSL Manager: Sutton Burtenshaw ZL4QJ 856 3832 [email protected] Net Controllers: 80m net—Phil King ZL1PK 847 1320 [email protected] 2m net—Phil King ZL1PK 847 1320 [email protected] NZART Examiners: ZL1IC, ZL1PK & ZL1TJA Page 1 From the Editor From our Secretary ZL1PK. -
WORLD SPACECRAFT DIGEST by Jos Heyman 2013 Version: 1 January 2014 © Copyright Jos Heyman
WORLD SPACECRAFT DIGEST by Jos Heyman 2013 Version: 1 January 2014 © Copyright Jos Heyman The spacecraft are listed, in the first instance, in the order of their International Designation, resulting in, with some exceptions, a date order. Spacecraft which did not receive an International Designation, being those spacecraft which failed to achieve orbit or those which were placed in a sub orbital trajectory, have been inserted in the date order. For each spacecraft the following information is provided: a. International Designation and NORAD number For each spacecraft the International Designation, as allocated by the International Committee on Space Research (COSPAR), has been used as the primary means to identify the spacecraft. This is followed by the NORAD catalogue number which has been assigned to each object in space, including debris etc., in a numerical sequence, rather than a chronoligical sequence. Normally no reference has been made to spent launch vehicles, capsules ejected by the spacecraft or fragments except where such have a unique identification which warrants consideration as a separate spacecraft or in other circumstances which warrants their mention. b. Name The most common name of the spacecraft has been quoted. In some cases, such as for US military spacecraft, the name may have been deduced from published information and may not necessarily be the official name. Alternative names have, however, been mentioned in the description and have also been included in the index. c. Country/International Agency For each spacecraft the name of the country or international agency which owned or had prime responsibility for the spacecraft, or in which the owner resided, has been included. -
Space Exploration and Development Systems (SEEDS) 2014
SpacE Exploration and Development Systems (SEEDS) 2014 “Missions and Expeditions to Mars” Orpheus Executive Summary SEEDS Executive Summary 09/2014 Page 1 SEEDS Executive Summary 09/2014 Page 2 List of authors: Crescenzio Ruben Xavier AMENDOLA Portia BOWMAN Samuel BROCKSOPP Andrea D’OTTAVIO Alex GEE Samuel R. F. KENNEDY Antonio MAGARIELLO Adrian MORA BOLUDA Ignacio REY Alex ROSENBAUM Joachim STRENGE Aurthur Vimalachandran THOMAS JAYACHANDRAN SEEDS Executive Summary 09/2014 Page 3 SEEDS Executive Summary 09/2014 Page 4 ABSTRACT This six crew mission called Orpheus has been designed in order to fulfil some main objectives of space exploration: scientific advancements, technological progress, public outreach and international cooperation. This paper investigates the possibility of exploring the Martian system by using a manned spacecraft, the Crew Interplanetary Vehicle, (CIV) and a cargo vehicle, the Mars Automated Transfer Vehicle (MATV). The main payloads, carried by the high efficiency solar electric MATV, are a two-passenger spacecraft landing on Phobos; an orbital laboratory and a rover network for deployment to the surface of Mars. In order to cope with the constraints imposed for a human mission to deep space, the feasibility study has been performed using a human-centred design approach. The main output of the mission is the preliminary design of the CIV. Furthermore, the main parameters of the MATV as well as the orbital laboratory and the Phobos Lander were estimated. The manned spacecraft is designed to depart from LEO in 2036 using chemical propulsion. Once in Mars proximity, the main manoeuvres will be performed using nuclear thermal propulsion and a bi-propellant chemical system will perform the minor manoeuvres. -
Massive Pulsating Stars Observed by BRITE-Constellation I
A&A 588, A55 (2016) Astronomy DOI: 10.1051/0004-6361/201527872 & c ESO 2016 Astrophysics Massive pulsating stars observed by BRITE-Constellation I. The triple system β Centauri (Agena) A. Pigulski1, H. Cugier1, A. Popowicz2,R.Kuschnig3,A.F.J.Moffat4,S.M.Rucinski5, A. Schwarzenberg-Czerny6 , W. W. Weiss3, G. Handler6,G.A.Wade7, O. Koudelka8,J.M.Matthews9, St. Mochnacki5, P. Orleanski´ 10,H.Pablo4, T. Ramiaramanantsoa4, G. Whittaker5,E.Zocłonska´ 6, and K. Zwintz11 1 Instytut Astronomiczny, Uniwersytet Wrocławski, Kopernika 11, 51-622 Wrocław, Poland e-mail: [email protected] 2 Instytut Automatyki, Politechnika Sl˛´ aska, Akademicka 16, 44-100 Gliwice, Poland 3 Institut für Astrophysik, Universität Wien, Türkenschanzstrasse 17, 1180 Wien, Austria 4 Département de physique, Université de Montréal, CP 6128, Succursale Centre-Ville, Montréal, Québec, H3C 3J7, et Centre de recherche en astrophysique du Québec (CRAQ), Canada 5 Department of Astronomy & Astrophysics, University of Toronto, 50 St. George Street, Toronto, Ontario, M5S 3H4, Canada 6 Centrum Astronomiczne im. M. Kopernika, Polska Akademia Nauk, Bartycka 18, 00-716 Warszawa, Poland 7 Department of Physics, Royal Military College of Canada, PO Box 17000, Station Forces, Kingston, Ontario, K7K 7B4, Canada 8 Institut für Kommunikationsnetze und Satellitenkommunikation, Technische Universität Graz, Inffeldgasse 12, 8010 Graz, Austria 9 Dept. of Physics & Astronomy, The University of British Columbia, 6224 Agricultural Road, Vancouver, B.C., V6T 1Z1, Canada 10 Centrum Badan´ Kosmicznych, Polska Akademia Nauk, Bartycka 18A, 00-716 Warszawa, Poland 11 Institut für Astro- und Teilchenphysik, Universität Innsbruck, Technikerstrasse 25/8, 6020 Innsbruck, Austria Received 1 December 2015 / Accepted 14 January 2016 ABSTRACT Context. -
Space Photometry with BRITE-Constellation §
universe Review Space Photometry with BRITE-Constellation § Werner W. Weiss 1,* , Konstanze Zwintz 2 , Rainer Kuschnig 3 , Gerald Handler 4 , Anthony F. J. Moffat 5 , Dietrich Baade 6 , Dominic M. Bowman 7 , Thomas Granzer 8 , Thomas Kallinger 1 , Otto F. Koudelka 3, Catherine C. Lovekin 9 , Coralie Neiner 10 , Herbert Pablo 11 , Andrzej Pigulski 12 , Adam Popowicz 13 , Tahina Ramiaramanantsoa 14 , Slavek M. Rucinski 15 , Klaus G. Strassmeier 8 and Gregg A. Wade 16 1 Institute for Astrophysics, University of Vienna, A-1180 Vienna, Austria; [email protected] 2 Institute for Astro- and Particle Physics, University of Innsbruck, A-6020 Innsbruck, Austria; [email protected] 3 Institut für Kommunikationsnetze und Satellitenkommunikation, Technische Universität Graz, A-8020 Graz, Austria; [email protected] (R.K.); [email protected] (O.F.K.) 4 Nicolaus Copernicus Astronomical Center, Polish Academy of Sciences, 00-716 Warsaw, Poland; [email protected] 5 Department of Physics, University of Montreal, Montreal, QC H3C 3J7, Canada; [email protected] 6 European Southern Observatory (ESO), D-85748 Garching bei München, Germany; [email protected] 7 Institute of Astronomy, KU Leuven, B-3001 Leuven, Belgium; [email protected] 8 Department Cosmic Magnetic Fields, Leibniz Institut fuer Astrophysik Potsdam, D-14482 Potsdam, Germany; [email protected] (T.G.); [email protected] (K.G.S.) 9 Physics Department, Mount Allison University, Sackville, NB E4L 1E6, Canada; [email protected] 10 LESIA, Paris Observatory, PSL University, -
ODQN 17-2, April 2013
National Aeronautics and Space Administration Orbital Debris Quarterly News Volume 17, Issue 2 April 2013 Small Satellite Possibly Hit by Even Smaller Object A small Russian geodetic satellite was slightly soon thereafter, the U.S. Space Surveillance Network Inside... perturbed from its orbit on 22 January 2013 and (SSN) detected a new object in a similar orbit, but shed a piece of debris after apparently being struck with an orbital period slightly greater (~0.006 min) by a very small meteoroid or orbital debris. Known than the original period of BLITS. This object, with OD Pioneer as BLITS (Ball Lens In The Space), the satellite an estimated size of 10 cm, was later cataloged with William Djinis (International Designator an International Designator of Dies at Age 91 2 2009-049G, U.S. Satellite 2009-049J and a U.S. Satellite Number 35871) was circling Number of 39119. Specialists ISS Solves EVA the Earth at an altitude of of the SSN confirmed that Problems Caused 832 km with an inclination of BLITS had not been struck by Small MMOD 98.6 degrees at the time of the by a known object in Earth event. orbit, notwithstanding some Impacts 2 The BLITS is a erroneous media reports to the completely inert object contrary. Reentry of consisting of a glass sphere Collisions between Cataloged encased in another glass satellites and very small debris Objects 5 sphere with a total mass of are common, but normally go 7.53 kg and a full diameter unnoticed and do not produce Cut-away to show the construction of the Abstracts from the of 17 cm (see figure). -
Optical Co-Orbital Measurements in Low Earth Orbit
Optical Co-orbital Measurements in Low Earth Orbit by Kevin Bernard A thesis submitted to the Faculty of Graduate and Postdoctoral Affairs in partial fulfillment of the requirements for the degree of Master of Applied Science in Aerospace Engineering Carleton University Ottawa, Ontario © 2019 Kevin Bernard For all the support my family has provided over the years, this work is dedicated to them. ii Abstract The increasing access to the space domain has led to the growth of the on-orbit object population, as well as the evolution of space surveillance capabilities. With the increased public attention paid to spacecraft proximity and rendezvous operations, is an opportunity to examine what and how current space surveillance capabilities can contribute to this field. This thesis examines the feasibility and challenges associated with re-purposing an existing on-orbit space surveillance capability, the NEOSSat microsatellite, to per- form proximity operations. The ability of NEOSSat to collect a sufficient number of accurate optical observations to determine the relative orbit of a target spacecraft is explored. A variety of observation events are explored with a collection of space- craft to generate relative orbits using inertial orbit determination techniques. These practical results, to the author's knowledge, are the first in the field of relative or- bit determination using inertial techniques between two co-orbital Low Earth Orbit satellites. iii Acknowledgements I would like to sincerely thank my supervisors, Dr. Steve Ulrich and Dr. Lauchie Scott. Thank you Steve for providing guidance, and for taking a chance on someone who walked in to your office in the Spring of 2016. -
Inspiring the Next Generation of Scientists Jupiter's Aurora AGU
VOL. 97 NO. 1 1 JAN 2016 Earth & Space Science News Inspiring the Next Generation of Scientists Jupiter’s Aurora AGU Medalists Honored What Flows Beneath Housing and Registration Now Open Call for Abstracts It’s time to register and reserve your hotel in New Orleans for the 2016 Ocean Sciences Meeting, 21–26 February. Housing Deadline: 28 January 2016 osm.agu.org/2016/ Earth & Space Science News Contents 1 JANUARY 2016 PROJECT UPDATE VOLUME 97, ISSUE 1 13 Next-Generation Scientists Get a Taste of Their Future Careers High school and middle school students mingled with scientists from all over the world when they presented their posters at the Joint Aquatic Sciences Meeting. NEWS 5 Purple Hearts Honor Four Meteorologists Killed in World War II A ceremony posthumously honors the U.S. Weather Service workers 73 years after 8 they died and highlights the importance of weather forecasting during the war. COVER Breaking Internal Tides AGU NEWS Keep the Ocean in Balance Medalists Honored at 17 2015 AGU Fall Meeting By studying how underwater waves strike the continental slope off Citations for and responses from recipients Tasmania, researchers seek to uncover the mechanisms that keep the of Union medals, among AGU’s most circulation of the global ocean in balance. prestigious honors. Earth & Space Science News Eos.org // 1 Contents DEPARTMENTS Editor in Chief Barbara T. Richman: AGU, Washington, D. C., USA; eos_ [email protected] Editors Christina M. S. Cohen Wendy S. Gordon Carol A. Stein California Institute Ecologia Consulting, Department of Earth and of Technology, Pasadena, Austin, Texas, USA; Environmental Sciences, Calif., USA; wendy@ecologiaconsulting University of Illinois at cohen@srl .caltech.edu .com Chicago, Chicago, Ill., USA; [email protected] José D. -
BRITE Constellation- 5 Years of Successful Science Operations
08/02/2018 BRITE Constellation- 5 Years of Successful Science Operations O. Koudelka, R.Kuschnig, M.Wenger, P.Romano Graz University of Technology K.Zwintz W.Weiss University of Innsbruck University of Vienna Contents • Introduction • Scientific goals of BRITE Constellation • BRITE Characteristics • Scientific Results • Summary and Outlook 1 08/02/2018 BRITE – BRight Target Explorer World‘s first nanosatellite constellation dedicated to asteroseismology TUGSAT‐1 / BRITE‐A Bab 2013‐02‐25 100.36 blue UniBRITE UBr 2013‐02‐25 100.37 red 3 countries –5 (6) satellites – ONE MISSION Launch TUGSAT-1/BRITE-Austria and UniBRITE were launched by PSLV-C20 of ISRO/ANTRIX on 25 February 2013 from the Satish Dhawan Space Centre in Sriharikota Sun-synchonous LEO orbit Courtesy: ISRO 2 08/02/2018 Scientific Goals • Measurement of brightness and temperature variations of massive luminous stars (brighter than visual magnitude 4) • Observations: 6 months typ. • High duty cycle • 2-colour (blue and red): satellites operate in pairs •24°field of view Raster Photometry High pointing accuracy required: 1 arcminute 3 08/02/2018 TUGSAT-1/BRITE-Austria Flight Model magnetometer S-band antenna solar cells Generic Nanosatellite Bus telescope by star tracker BRITE Characteristics • Nanosatellite: 20 x 20 x 20 cm • Mass: 7 kg • Electrical power: 6…11 W • Transmit power: 0.5 W • Frequency bands: S-band downlink / UHF uplink • Data rates: 32…256 kbit/s downlink, 9.6 kbit/s uplink • Pointing accuracy: 1 arcmin. • Science data volume: 18…40 MB / day per satellite 4 08/02/2018