Theory, Modeling, and Integrated Studies in the Arase (ERG) Project
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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. -
Sun-Earth System Interaction Studies Over Vietnam: an International Cooperative Project
Ann. Geophys., 24, 3313–3327, 2006 www.ann-geophys.net/24/3313/2006/ Annales © European Geosciences Union 2006 Geophysicae Sun-Earth System Interaction studies over Vietnam: an international cooperative project C. Amory-Mazaudier1, M. Le Huy2, Y. Cohen3, V. Doumbia4,*, A. Bourdillon5, R. Fleury6, B. Fontaine7, C. Ha Duyen2, A. Kobea4, P. Laroche8, P. Lassudrie-Duchesne6, H. Le Viet2, T. Le Truong2, H. Luu Viet2, M. Menvielle1, T. Nguyen Chien2, A. Nguyen Xuan2, F. Ouattara9, M. Petitdidier1, H. Pham Thi Thu2, T. Pham Xuan2, N. Philippon**, L. Tran Thi2, H. Vu Thien10, and P. Vila1 1CETP/CNRS, 4 Avenue de Neptune, 94107 Saint-Maur-des-Fosses,´ France 2Institute of Geophysics, Vietnamese Academy of Science and Technology , 18 Hoang Quoc Viet, Cau Giay, Hano¨ı, Vietnam 3IPGP, 4 Avenue de Neptune, 94107 Saint-Maur-des-Fosses,´ France 4Laboratoire de Physique de l’Atmosphere,` Universite´ d’Abidjan Cocody 22 B.P. 582, Abidjan 22, Coteˆ d’Ivoire 5Institut d’Electronique et de Tel´ ecommunications,´ Universite´ de Rennes Batˆ 11D, Campus Beaulieu, 35042 Rennes, cedex,´ France 6ENST, Universite´ de Bretagne Occidentale, CS 83818, 29288 Brest, cedex´ 3, France 7CRC , Faculte´ des Sciences, 6 Boulevard Gabriel, F 21004 Dijon cedex´ 04, France 8Unite´ de Recherche Environnement Atmospherique,´ ONERA, 92332 Chatillon, cedex,´ France 9University of Koudougou, Burkina Faso 10Laboratoire signaux et systemes,` CNAM, 292 Rue saint Martin, 75141 Paris cedex´ 03, France *V. Doumbia previously signed V. Doumouya **affiliation unknown Received: 15 June 2006 – Revised: 19 October 2006 – Accepted: 8 November 2006 – Published: 21 December 2006 Abstract. During many past decades, scientists from var- the E, F1 and F2 ionospheric layers follow the variation of ious countries have studied separately the atmospheric mo- the sunspot cycle. -
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 -
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] -
(EFD) of Plasma Wave Experiment (PWE) Aboard the Arase Satellite
Kasaba et al. Earth, Planets and Space (2017) 69:174 https://doi.org/10.1186/s40623-017-0760-x FULL PAPER Open Access Wire Probe Antenna (WPT) and Electric Field Detector (EFD) of Plasma Wave Experiment (PWE) aboard the Arase satellite: specifcations and initial evaluation results Yasumasa Kasaba1* , Keigo Ishisaka2, Yoshiya Kasahara3, Tomohiko Imachi3, Satoshi Yagitani3, Hirotsugu Kojima4, Shoya Matsuda5, Masafumi Shoji5, Satoshi Kurita5, Tomoaki Hori5, Atsuki Shinbori5, Mariko Teramoto5, Yoshizumi Miyoshi5, Tomoko Nakagawa6, Naoko Takahashi7, Yukitoshi Nishimura8,9, Ayako Matsuoka10, Atsushi Kumamoto1, Fuminori Tsuchiya11 and Reiko Nomura12 Abstract This paper summarizes the specifcations and initial evaluation results of Wire Probe Antenna (WPT) and Electric Field Detector (EFD), the key components for the electric feld measurement of the Plasma Wave Experiment (PWE) aboard the Arase (ERG) satellite. WPT consists of two pairs of dipole antennas with ~ 31-m tip-to-tip length. Each antenna ele- ment has a spherical probe (60 mm diameter) at each end of the wire (15 m length). They are extended orthogonally in the spin plane of the spacecraft, which is roughly perpendicular to the Sun and enables to measure the electric feld in the frequency range of DC to 10 MHz. This system is almost identical to the WPT of Plasma Wave Investiga- tion aboard the BepiColombo Mercury Magnetospheric Orbiter, except for the material of the spherical probe (ERG: Al alloy, MMO: Ti alloy). EFD is a part of the EWO (EFD/WFC/OFA) receiver and measures the 2-ch electric feld at a sampling rate of 512 Hz (dynamic range: 200 mV/m) and the 4-ch spacecraft potential at a sampling rate of 128 Hz (dynamic range: 100 V and 3 V/m), with± the bias control capability of WPT. -
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. -
Locations of Chorus Emissions Observed by the Polar Plasma Wave Instrument K
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 115, A00F12, doi:10.1029/2009JA014579, 2010 Click Here for Full Article Locations of chorus emissions observed by the Polar Plasma Wave Instrument K. Sigsbee,1 J. D. Menietti,1 O. Santolík,2,3 and J. S. Pickett1 Received 18 June 2009; revised 20 November 2009; accepted 17 December 2009; published 8 June 2010. [1] We performed a statistical study of the locations of chorus emissions observed by the Polar spacecraft’s Plasma Wave Instrument (PWI) from March 1996 to September 1997, near the minimum of solar cycles 22/23. We examined how the occurrence of chorus emissions in the Polar PWI data set depends upon magnetic local time, magnetic latitude, L shell, and L*. The Polar PWI observed chorus most often over a range of magnetic local times extending from about 2100 MLT around to the dawn flank and into the dayside magnetosphere near 1500 MLT. Chorus was least likely to be observed near the dusk flank. On the dayside, near noon, the region in which Polar observed chorus extended to larger radial distances and higher latitudes than at other local times. Away from noon, the regions in which chorus occurred were more restricted in both radial and latitudinal extent. We found that for high‐latitude chorus near local noon, L* provides a more reasonable mapping to the equatorial plane than the standard L shell. Chorus was observed slightly more often when the magnitude of the solar wind magnetic field BSW was greater than 5 nT than it was for smaller interplanetary magnetic field strengths.