(EFD) of Plasma Wave Experiment (PWE) Aboard the Arase Satellite
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Peace in Vietnam! Beheiren: Transnational Activism and Gi Movement in Postwar Japan 1965-1974
PEACE IN VIETNAM! BEHEIREN: TRANSNATIONAL ACTIVISM AND GI MOVEMENT IN POSTWAR JAPAN 1965-1974 A DISSERTATION SUBMITTED TO THE GRADUATE DIVISION OF THE UNIVERSITY OF HAWAI‘I AT MĀNOA IN PARTIAL FULFILLMENT OF THE REQUIREMENT FOR THE DEGREE OF DOCTOR OF PHILOSOPHY IN POLITICAL SCIENCE AUGUST 2018 By Noriko Shiratori Dissertation Committee: Ehito Kimura, Chairperson James Dator Manfred Steger Maya Soetoro-Ng Patricia Steinhoff Keywords: Beheiren, transnational activism, anti-Vietnam War movement, deserter, GI movement, postwar Japan DEDICATION To my late father, Yasuo Shiratori Born and raised in Nihonbashi, the heart of Tokyo, I have unforgettable scenes that are deeply branded in my heart. In every alley of Ueno station, one of the main train stations in Tokyo, there were always groups of former war prisoners held in Siberia, still wearing their tattered uniforms and playing accordion, chanting, and panhandling. Many of them had lost their limbs and eyes and made a horrifying, yet curious, spectacle. As a little child, I could not help but ask my father “Who are they?” That was the beginning of a long dialogue about war between the two of us. That image has remained deep in my heart up to this day with the sorrowful sound of accordions. My father had just started work at an electrical laboratory at the University of Tokyo when he found he had been drafted into the imperial military and would be sent to China to work on electrical communications. He was 21 years old. His most trusted professor held a secret meeting in the basement of the university with the newest crop of drafted young men and told them, “Japan is engaging in an impossible war that we will never win. -
1 the Mass Spectrum Analyzer (MSA) for the Martian Moons Explorat
In Situ Observations of Ions and Magnetic Field Around Phobos: The Mass Spectrum Analyzer (MSA) for the Martian Moons eXploration (MMX) Mission Shoichiro Yokota ( [email protected] ) Osaka Univ. https://orcid.org/0000-0001-8851-9146 Naoki Terada Tohoku University Ayako Matsuoka Kyoto University: Kyoto Daigaku Naofumi Murata JAXA Yoshifumi Saito ISAS/JAXA Dominique Delcourt LPP-CNRS-Sorbonne Yoshifumi Futaana Swedish Institute of Space Physics Kanako Seki The University of Tokyo: Tokyo Daigaku Micah J Schaible Georgia Institute of Technology Kazushi Asamura ISAS/JAXA Satoshi Kasahara The University of Tokyo: Tokyo Daigaku Hiromu Nakagawa Tohoku University: Tohoku Daigaku Masaki N Nishino ISAS/JAXA Reiko Nomura ISAS/JAXA Kunihiro Keika The University of Tokyo: Tokyo Daigaku Yuki Harada Kyoto University: Kyoto Daigaku Shun Imajo Nagoya University: Nagoya Daigaku Full paper Keywords: Martian Moons eXploration (MMX), Phobos, Mars, mass spectrum analyzer, magnetometer Posted Date: December 21st, 2020 DOI: https://doi.org/10.21203/rs.3.rs-130696/v1 License: This work is licensed under a Creative Commons Attribution 4.0 International License. Read Full License 1 In situ observations of ions and magnetic field around Phobos: 2 The Mass Spectrum Analyzer (MSA) for the Martian Moons eXploration (MMX) 3 mission 4 Shoichiro Yokota1, Naoki Terada2, Ayako Matsuoka3, Naofumi Murata4, Yoshifumi 5 Saito5, Dominique Delcourt6, Yoshifumi Futaana7, Kanako Seki8, Micah J. Schaible9, 6 Kazushi Asamura5, Satoshi Kasahara8, Hiromu Nakagawa2, Masaki -
Message from the Director General September 2017 Saku Tsuneta Director General
Message from the Director General September 2017 Saku Tsuneta Director General Institute of Space and Astronautical Science Japan Aerospace Exploration Agency On April 28, 2016, the Japan former ISAS project managers, and levels, the satellite was declared to Aerospace Exploration Agency an Action Plan for Reforming ISAS have entered into its scheduled orbit (JAXA) made the difficult decision Based on the Anomaly Experienced in March 2017. The successful start to terminate attempts to restore by Hitomi was developed. In of the ARASE mission is a testament communication with the X-ray addition, “town hall meetings” were to the dedication and skills across Astronomy Satellite ASTRO-H (also held to share the spirit and practice JAXA. known as HITOMI), which was of the action plan with all ISAS ISAS is currently operating six launched on February 17, 2016, due employees. The plan, which was satellites and space probes: ARASE, to the communication anomalies applied to launch preparations of Hayabusa2, HISAKI, AKATSUKI, that occurred on March 26, 2016. the geospace exploration satellite HINODE, and GEOTAIL. Asteroid Since that time, in consultation with ARASE, contributed to the successful Explorer Hayabusa2, which is experts inside as well as outside and stable operation of that satellite, currently on its planned trajectory JAXA, the Institute of Space and and will be applied to other projects towards the 162173 Ryugu asteroid Astronautical Science (ISAS) has such as the Smart Lander for under ion engine power, is equipped been making every possible effort Investigating Moon (SLIM). The plan- with new technologies for solar to determine what went wrong, and do-check-act (PDCA) cycle should system exploration such as long- what can be done to prevent this work to further refine both current distance communication using Ka- from happening again in the future. -
Planet Earth Taken by Hayabusa-2
Space Science in JAXA Planet Earth May 15, 2017 taken by Hayabusa-2 Saku Tsuneta, PhD JAXA Vice President Director General, Institute of Space and Astronautical Science 2017 IAA Planetary Defense Conference, May 15-19,1 Tokyo 1 Brief Introduction of Space Science in JAXA Introduction of ISAS and JAXA • As a national center of space science & engineering research, ISAS carries out development and in-orbit operation of space science missions with other directorates of JAXA. • ISAS is an integral part of JAXA, and has close collaboration with other directorates such as Research and Development and Human Spaceflight Technology Directorates. • As an inter-university research institute, these activities are intimately carried out with universities and research institutes inside and outside Japan. ISAS always seeks for international collaboration. • Space science missions are proposed by researchers, and incubated by ISAS. ISAS plays a strategic role for mission selection primarily based on the bottom-up process, considering strategy of JAXA and national space policy. 3 JAXA recent science missions HAYABUSA 2003-2010 AKARI(ASTRO-F)2006-2011 KAGUYA(SELENE)2007-2009 Asteroid Explorer Infrared Astronomy Lunar Exploration IKAROS 2010 HAYABUSA2 2014-2020 M-V Rocket Asteroid Explorer Solar Sail SUZAKU(ASTRO-E2)2005- AKATSUKI 2010- X-Ray Astronomy Venus Meteorogy ARASE 2016- HINODE(SOLAR-B)2006- Van Allen belt Solar Observation Hisaki 2013 4 Planetary atmosphere Close ties between space science and space technology Space Technology Divisions Space -
Theory, Modeling, and Integrated Studies in the Arase (ERG) Project
Seki et al. Earth, Planets and Space (2018) 70:17 https://doi.org/10.1186/s40623-018-0785-9 FULL PAPER Open Access Theory, modeling, and integrated studies in the Arase (ERG) project Kanako Seki1* , Yoshizumi Miyoshi2, Yusuke Ebihara3, Yuto Katoh4, Takanobu Amano1, Shinji Saito5, Masafumi Shoji2, Aoi Nakamizo6, Kunihiro Keika1, Tomoaki Hori2, Shin’ya Nakano7, Shigeto Watanabe8, Kei Kamiya5, Naoko Takahashi1, Yoshiharu Omura3, Masahito Nose9, Mei‑Ching Fok10, Takashi Tanaka11, Akimasa Ieda2 and Akimasa Yoshikawa11 Abstract Understanding of underlying mechanisms of drastic variations of the near-Earth space (geospace) is one of the current focuses of the magnetospheric physics. The science target of the geospace research project Exploration of energiza‑ tion and Radiation in Geospace (ERG) is to understand the geospace variations with a focus on the relativistic electron acceleration and loss processes. In order to achieve the goal, the ERG project consists of the three parts: the Arase (ERG) satellite, ground-based observations, and theory/modeling/integrated studies. The role of theory/modeling/integrated studies part is to promote relevant theoretical and simulation studies as well as integrated data analysis to combine diferent kinds of observations and modeling. Here we provide technical reports on simulation and empirical models related to the ERG project together with their roles in the integrated studies of dynamic geospace variations. The simu‑ lation and empirical models covered include the radial difusion model of the radiation belt electrons, GEMSIS-RB and RBW models, CIMI model with global MHD simulation REPPU, GEMSIS-RC model, plasmasphere thermosphere model, self-consistent wave–particle interaction simulations (electron hybrid code and ion hybrid code), the ionospheric electric potential (GEMSIS-POT) model, and SuperDARN electric feld models with data assimilation. -
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 -
Overview of Micro/Nano/Pico-Satellite Part 1 Shinichi Nakasuka University of Tokyo
CanSat & Rocket Experiment(‘99~) Hodoyoshiハイブリッド-1 ‘14 ロケット Overview of Micro/nano/pico-satellite Part 1 Shinichi Nakasuka University of Tokyo PRISM ‘09 CubeSat 03,05 Nano-JASMINE (TBD) Where is Our University ? • University of Tokyo: 28,000 students, 7800 staffs – School of Engineering: 22 departments • Intelligent Space Systems Laboratory University of Tokyo in Tokyo Metropolitan Robot Statistics about University of Tokyo • The University of Tokyo – Established in 1886 – 11 Faculties/Graduate Schools – 14000 undergraduate/14000 graduate students – 3900 academic staffs/ 3900 supporting staffs – World QS ranking: 23th • School of Engineering – 1050 undergraduate students/year – 2053 master student/1066 Ph.D candidate • Including 921 foreign students from 74 countries – 453 academic staffs/ 206 supporting staffs – Yearly budget: about $ 250M – World QS ranking: 8th • Mechanical/Aerospace: 9th ranking Graduate School of Engineering 18 Departments, 2 Institutes, 7 Centers ◆ Civil Engineering ◆ Materials Engineering ◆ Architecture ◆ Applied Chemistry ◆ Urban Engineering *3 ◆ Chemical System Engineering ◆ Mechanical Engineering ◆ Chemistry and Biotechnology ◆ Aeronautics and Astronautics ◆ Advanced Interdisciplinary Studies *1 ◆ Precision Engineering ◆ Nuclear Engineering and Management ◆ Electrical Engineering and Information Systems ◆ Bioengineering ◆ Applied Physics ◆ Technology Management for Innovation ◆ Systems Innovation ◆ Nuclear Professional School *2 Institute of Engineering Innovation *1 Doctoral course only Institute of Innovation -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Design, Implementation, and Operation of a Small Satellite Mission to Explore the Space Weather Effects in LEO
aerospace Article Design, Implementation, and Operation of a Small Satellite Mission to Explore the Space Weather Effects in LEO Isai Fajardo 1,*,† , Aleksander A. Lidtke 1,† , Sidi Ahmed Bendoukha 2, Jesus Gonzalez-Llorente 1 , Rafael Rodríguez 1 , Rigoberto Morales 1 , Dmytro Faizullin 1, Misuzu Matsuoka 1, Naoya Urakami 1, Ryo Kawauchi 1, Masayuki Miyazaki 1, Naofumi Yamagata 1, Ken Hatanaka 1, Farhan Abdullah 1, Juan J. Rojas 1, Mohamed Elhady Keshk 1 , Kiruki Cosmas 1, Tuguldur Ulambayar 1, Premkumar Saganti 3, Doug Holland 4, Tsvetan Dachev 5 , Sean Tuttle 6, Roger Dudziak 7 and Kei-ichi Okuyama 1 1 Department of Applied Science for Integrated Systems Engineering, Kyushu Institute of Technology, 1-1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan; [email protected] (A.A.L.); [email protected] (J.G.-L.); [email protected] (R.R.); [email protected] (R.M.); [email protected] (D.F.); [email protected] (M.M.); [email protected] (N.U.); [email protected] (R.K.); [email protected] (M.M.); [email protected] (N.Y.); [email protected] (K.H.); [email protected] (F.A.); [email protected] (J.J.R.); [email protected] (M.E.K.); [email protected] (K.C.); [email protected] (T.U.); [email protected] (K.-i.O.) 2 Satellite Development Center CDS, POS 50 ILOT T 12 BirEl Djir, Algerian Space Agency, Oran 31130, Algeria; [email protected] -
Penetration of Mev Electrons Into the Mesosphere Accompanying Pulsating Aurorae Y
www.nature.com/scientificreports OPEN Penetration of MeV electrons into the mesosphere accompanying pulsating aurorae Y. Miyoshi1*, K. Hosokawa2, S. Kurita3, S.‑I. Oyama1,4,5, Y. Ogawa4,16,17, S. Saito6, I. Shinohara7, A. Kero8, E. Turunen8, P. T. Verronen8,9, S. Kasahara10, S. Yokota11, T. Mitani7, T. Takashima7, N. Higashio7, Y. Kasahara12, S. Matsuda7, F. Tsuchiya13, A. Kumamoto13, A. Matsuoka14, T. Hori1, K. Keika10, M. Shoji1, M. Teramoto15, S. Imajo14, C. Jun1 & S. Nakamura1 Pulsating aurorae (PsA) are caused by the intermittent precipitations of magnetospheric electrons (energies of a few keV to a few tens of keV) through wave‑particle interactions, thereby depositing most of their energy at altitudes ~ 100 km. However, the maximum energy of precipitated electrons and its impacts on the atmosphere are unknown. Herein, we report unique observations by the European Incoherent Scatter (EISCAT) radar showing electron precipitations ranging from a few hundred keV to a few MeV during a PsA associated with a weak geomagnetic storm. Simultaneously, the Arase spacecraft has observed intense whistler‑mode chorus waves at the conjugate location along magnetic feld lines. A computer simulation based on the EISCAT observations shows immediate catalytic ozone depletion at the mesospheric altitudes. Since PsA occurs frequently, often in daily basis, and extends its impact over large MLT areas, we anticipate that the PsA possesses a signifcant forcing to the mesospheric ozone chemistry in high latitudes through high energy electron precipitations. Therefore, the generation of PsA results in the depletion of mesospheric ozone through high‑energy electron precipitations caused by whistler‑mode chorus waves, which are similar to the well‑known efect due to solar energetic protons triggered by solar fares. -
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. -
New Year's Address January 4, 2017 Saku Tsuneta, Director General
New Year’s Address January 4, 2017 Saku Tsuneta, Director General, Institute of Space and Astronautical Science Happy New Year, everyone. I hope most of the staff members of this institute have enjoyed their New Year’s vacation although it was not so long, and I am especially thankful to those people working hard in the critical phase of the Arase mission and those preparing for the launch of SS-520-4, including the support members of manufacturers. Successful launch of Arase and Epsilon launch vehicle In late December, we successfully launched ARASE, or the Exploration of energization and Radiation in Geospace (ERG) satellite, using the Epsilon-2 Launch Vehicle. It was a truly wonderful launch experience for all of us. The Epsilon launch vehicle was developed and launched under the management of the Space Technology Directorate I of JAXA. Hence, the Project Manager, Dr. Yasuhiro Morita led the overall program management and Mr. Takayuki Imoto acted as the sub-manager to command the frontline. I would like to say special thanks to both leaders and the project members of JAXA and ISAS who have been involved in this program. The second-stage rocket of Epsilon-2 has been newly developed to give it higher performance and a lower cost, and the launch capability has increased by about 30 percent from that of Epsilon-1. These newly developed technologies will be used in the solid rocket booster, SRB-3, of the H3 launch vehicle. Then, the SRB-3 booster will be used as the first-stage rocket of Epsilon launch vehicles.