JAXA ORGANIZATION CHART As of September 1, 2021

Total Page:16

File Type:pdf, Size:1020Kb

JAXA ORGANIZATION CHART As of September 1, 2021 JAXA ORGANIZATION CHART As of September 1, 2021 PRESIDENT YAMAKAWA Hiroshi SENIOR VICE PRESIDENT SANO Hisashi ASSOCIATE DIRECTOR GENERAL 〔Chief Engineer Office, Safety and Mission Assurance Department〕 GENERAL AUDITOR FUKAI Hiroshi VICE PRESIDENT MIYAKE Masazumi NAKASHIMA Akihiko FUNO Yasuhiro KOBAYASHI Yoko FUJITA Kazushige 〔Director General, Space Transportation Technology Directorate〕 IZUMI Tatsushi TERADA Koji 〔 Director General,Space Technology Directorate Ⅰ, Director General,Space Technology Directorate Ⅱ, Space Tracking and Communications Center,Center Director of Tsukuba Space Center 〕 General Auditor Office HAMAYAMA Hirofumi SASAKI Hiroshi 〔 Director General, Human Spaceflight Technology Directorate, Exploration Innovation Hub, JAXA Space Exploration Center (JSEC)(except Martian Moons Exploration Project ) 〕 KUNINAKA Hitoshi 〔Director General, Institute of Space and Astronautical Science (ISAS), JAXA Space Exploration Center (JSEC)( Martian Moons Exploration Project ) 〕 HARIGAE Masatoshi 〔Director General, Aeronautical Technology Directorate,Director General, Research and Development Directorate, Environmental Test Technology Unit 〕 ISHI Yasuo 〔Strategic Planning and Management Department, Public Affairs Department, International Relations and Research Department, New Enterprise Promotion Department , Security and Information Systems Department, Space Education Office 〕 OYAMA Mami 〔General Affairs Department, Evaluation and Audit Department, Human Resources Department, Finance Department, Procurement Department, Ground Facilities Department, Work-Life Support and Diversity Office〕 Strategic Planning and Management Department SUZUKI Kazuhiro Space Transportation Technology Directorate Institute of Space and Astronautical Science (ISAS) (Director General) FUNO Yasuhiro 〔Director General, Institute of Space and Astronautical Science〕 KUNINAKA Hitoshi Evaluation and Audit Department SATOH Masahiko 〔Deputy Director General, Institute of Space and Astronautical Science〕 FUJIMOTO Masaki Management and Integration Department SATOH Toshiaki Work-Life Support and Diversity Office SATOH Masahiko Management and Integration Department MIYOSHI Hiroshi General Affairs Department TAKEUCHI ei 〔Senior Chief Officer of Space Transportation Technology〕 FUJITA Takeshi Director for International Strategy and Coordination TOKAKU Yoshio Human Resources Department IWAMOTO Hiroyuki Range Safety Planning and Control Unit ISHIHARA Kazutomi Director for Education and Public Outreach FUJIMOTO Masaki Finance Department OZEKI Yasuhiko Launch Capabilities Unit FUSE Ryugo 〔Research Director〕 YOSHIDA Tetsuya Department of Space Astronomy and Astrophysics YAMADA Toru Procurement Department NAIKI Satoru H3 Project Team OKADA Masashi Department of Solar System Sciences SAITO Yoshifumi Department of Interdisciplinary Space Science INATOMI Yuko Epsilon Rocket Project Team IMOTO Takayuki Department of Space Flight Systems SAWAI Shujiro Public Affairs Department SASAKI Kaori Department of Spacecraft Engineering MIZUNO Takahide Kagoshima Space Center KAWAKAMI Michio International Relations and Research Department SHOJI Yoshikazu JAXA Washington D.C. Office ONODA Masami Tanegashima Space Center KAWAKAMI Michio JAXA Paris Office SUDO Katuya 〔Program Director〕 SATO Eiichi JAXA Bangkok Office ONO Atsushi Launch Site Safety Assessment Unit NAKANO Tetsuya ISAS Program Office MOKUNO Masaaki Business Development and Industrial Relations Department DATEKI Kyoko Flight Safety Control Unit ISHIHARA Kazutomi GEOTAIL Project Team SAITO Yoshifumi ASTRO-EII Project Team ISHIDA Manabu Range Technology Development Unit SUNASAKA Yoshinori SOLAR-B Project Team SHIMIZU Toshifumi Bepi Colombo Project Team OGAWA Hiroyuki 〔Senior Chief Engineer〕 KUBOTA Takashi Uchinoura Space Center MINESUGI Kenji Extreme Ultraviolet Spectroscope for Exospheric Dynamics Project Team YAMAZAKI Atsushi Hayabusa2 Project Team TSUDA Yuichi Chief Engineer FUJITA Takeshi SLIM Project Team (Smart Lander for Investigating Moon Project Team) SAKAI Shinichiro Chief Engineer MACHIDA Shigeru Space Technology Directorate I XRISM Project Team(X-Ray Imaging and Spectroscopy Mission Project Team) MAEJIMA Hironori Chief Engineer UEMATSU Hirohiko (Director General) TERADA Koji DESTINY+ Project Team (Demonstration and Experiment of Space Technology for Chief Engineer IWATA Takanori Interplanetary Voyage with Phaethon Flyby and Dust Science Project Team) TAKASHIMA Takashi Chief Engineer KII Tsuneo Management and Integration Department SATOH Toshiaki Chief Engineer TAKAHASHI Tetsuo [ Senior Chief Officer of Satellite Systems Development ] KOHATA Hiroki Chief Engineer SUZUKI Yusuke 〔Senior Chief Officer of Fundamental Technology for Space Science〕 MORITA Yasuhiro JDRS Project Team (Japanese Data Relay System Project Team) YAMAKAWA Shiro Inter-University Research and Facility Management Group NONAKA Satoshi 〔Senior Chief Officer of Information Systems〕 FUJITA Kazushige Engineering Test Satellite-9 Project Team FUKATSU Tsutomu Test and Operation Technology Group FUKUDA Seisuke Advanced Machining Technology Group NAKATSUBO Shunichi Security and Information Systems Department NAITO Ichiro Senior Chief Officer of Earth Observation Missions HIRABAYASHI Takeshi Scientific Ballooning Research and Operation Group FUKE Hideyuki Satellite Applications and Operations Center (SAOC) HIRABAYASHI Takeshi Sounding Rocket Research and Operation Group HABU Hiroto 〔Senior Chief Officer of Safety and Mission Assurance〕 IZUMI Tatsushi Earth Observation Research Center (EORC) HIRABAYASHI Takeshi Noshiro Rocket Testing Center ISHII Nobuaki 〔Earth Observation Center (EOC)〕 FUJISAWA Tatsuya Akiruno Experimental Facility GOTO Ken Safety and Mission Assurance Officer TORII Yoshihiro Science Satellite Operation and Data Archive Unit KAGAWA Hideshi GCOM Project Team (Global Change Observation Mission Project Team) TANAKA Kazuhiro Lunar and Planetary Exploration Data Analysis Group SATO Hiroyuki Safety and Mission Assurance Officer MINAMINO Hiroyuki Astromaterials Science Research Group USUI Tomohiro Safety and Mission Assurance Officer UESUGI Masato EarthCARE/CPR Project Team(Earth Cloud, Aerosol and Radiation Explorer/Cloud TOMITA Eichi Deep Space Tracking Technology Group YOSHIKAWA Makoto Safety and Mission Assurance Officer HONDA Masahisa Profiling Radar Project Team) Safety and Mission Assurance Officer KOBAYASHI Hideyuki ALOS-2 Project Team (Advanced Land Observing Satellite-2 Project Team) SOBUE Shinichi GOSAT-2 Project Team (Greenhouse Gases Observing Satellite-2 Project Team) KUZE Akihiko Safety and Mission Assurance Department KAMIMORI Norimitsu Advanced Optical Satellite Project Team SAGISAKA Masakazu Ground Facilities Department MUTO Mitsutaka Advanced Radar Satellite Project Team SUZUKI Shinichi Aeronautical Technology Directorate Spectrum Management Office WATANABE Tomonao GOSAT-GW Project Team KOJIMA Yasushi (Director General) HARIGAE Masatoshi Space Tracking and Communications Center INOUE koichi Management and Integration Department WATANABE Shigeya [Senior Chief Officer of Satellite Navigation Technology] KOGURE satoshi 〔Program Director〕 WATANABE Yasushi SSA System Project Team MATSUURA Mayumi Masuda Tracking and Communication Station ARIKAWA Kaoru Advanced Satellite Navigation System Project Team(ASNAV Project Team) MATSUMOTO Akihiro En-Core Project Team YAMANE Takashi Katsuura Tracking and Communication Station ARIKAWA Kaoru Satellite Navigation Unit KOGURE satoshi (Environmentally Compatible Core Engine Technology Research Project Team) Okinawa Tracking and Communication Station ARIKAWA Kaoru Usuda Deep Space Center MURATA Yasuhiro Aviation Systems Research Unit MAKINO Yoshikazu Space Technology Directorate Ⅱ Environmental Test Technology Unit SHIMIZU Ryuzo (Director General) TERADA Koji Next Generation Aeronautical Innovation Hub Center ITO Takeshi Space Education Office SASAKI Kaori Human Spaceflight Technology Directorate 〔Senior Chief Officer of Fundamental Aeronautics Research〕 ITO Takeshi (Director General) SASAKI Hiroshi 〔Center Director, Tsukuba Space Center〕 TERADA Koji Aerodynamics Research Unit HAMAMOTO Shigeru Tsukuba Space Center Administration Department OKADO Yasumasa 〔Program Manager of International Space Station〕 SAKAI Jyunichi Flight Research Unit FUJII Kenji 〔Program Manager of Gateway〕 TSUTSUI Fumiya Propulsion Research Unit ISHII Tatsuya Management and Integration Department KAWASAKI Kazuyoshi Structures and Advanced Composite Research Unit NAKAMURA Toshiya JEM Utilization Center OGAWA Shiho Numerial Simulation Research Unit AOYAMA Takashi Human Spaceflight Technology Center SAKAI Jyunichi HTV-X Project Team ITO Norimasa Research and Development Directorate (Director General) HARIGAE Masatoshi JAXA Docking Demonstration on HTV-X Project Team (JDOCX Project Team) MAEDA maki Research Strategy Department INABA Noriyasu Lunar Gateway Habitation Pre-Project Team TSUJI Norihito Management and Integration Department INABA Noriyasu Astronaut Operations and Technology Unit TASAKI Kazuyuki 〔KAKUDA SPACE CENTER〕 UEDA Syuichi Human Space Safety and Mission Assurance Office KOBAYASHI Ryoji Research Unit I YAMANAKA Koji JAXA Houston Office ABE Takahiro Research Unit Ⅱ SUGITA Hiroyuki JAXA Moscow Office WADA Yoshio Research Unit Ⅲ SHIMIZU Taro JAXA Space Exploration Center (JSEC) TSUTSUI Fumiya Research Unit Ⅳ OKITA Koichi Management and Integration Office NAGAI Naoki System Technology Unit IWATA Takanori Space Exploration System Technology Unit SATOH Naoki Innovative Satellite Technology Demonstration Group KANEKO Yutaka Martian Moons Exploration Project Team KAWAKATSU Yasuhiro Sensor System Research Group KIMURA Toshiyoshi Lunar Polar Exploration Pre-Project Team ASOH Dai CALLISTO Project Team (Cooperative Action Leading to Launcher Innovation for ISHIMOTO Shinji Stage Toss-back Operation Project Team) Space Exploration Innovation Hub Center (Director) FUNAKI Ikkoh.
Recommended publications
  • Tupod Press Release
    G.A.U.S.S. SRL Via Lariana 5, Rome – Italy Phone: +39 06 97881440 GROUP OF ASTRODYNAMICS VAT No.: IT11900481000 FOR THE USE OF [email protected] SPACE SYSTEMS www.gaussteam.com TuPOD is ready for launch – Press Release – 5 December 2016 The TuPOD, a 3U CubeSat satellite and at the same time a deployer of TubeSat (a type of small satellite), originates from an innovative project of the Company G.A.U.S.S. Srl (Group of Astrodynamics for the Use of Space Systems), specialized in the development of satellites that are launcher platforms as well (like the previous satellites UniSat-5 and UniSat-6). The TuPOD is a CubeSat-type of satellite, with dimensions of 10x10x30cm, which will work itself as launch system for smaller satellites, the TubeSats. The TubeSats are a new type of Nanosatellites, cylindrically-shaped, not much bigger than an ordinary beverage can. To date, there wasn’t any launch possibility for this class of small satellites: with the TuPOD project, GAUSS Srl creates a new and affordable launch opportunity for the users of this new type of satellite. The TuPOD hosts two TubeSats onboard: TANCREDO I (Brazil) and OSNSAT (USA). Thanks to this specific kind of deployer – designed and built by GAUSS Srl – a couple of TubeSats are about to be UniSat-6 Platform released into Space for the first time ever. An important milestone for GAUSS Srl and for the whole Italian Aerospace Community. The TuPOD, in the middle, satellite/deployer for TubeSats from GAUSS Srl. On the right and on the left the TubeSats OSNSAT and TANCREDO I.
    [Show full text]
  • Global Exploration Roadmap
    The Global Exploration Roadmap January 2018 What is New in The Global Exploration Roadmap? This new edition of the Global Exploration robotic space exploration. Refinements in important role in sustainable human space Roadmap reaffirms the interest of 14 space this edition include: exploration. Initially, it supports human and agencies to expand human presence into the robotic lunar exploration in a manner which Solar System, with the surface of Mars as • A summary of the benefits stemming from creates opportunities for multiple sectors to a common driving goal. It reflects a coordi- space exploration. Numerous benefits will advance key goals. nated international effort to prepare for space come from this exciting endeavour. It is • The recognition of the growing private exploration missions beginning with the Inter- important that mission objectives reflect this sector interest in space exploration. national Space Station (ISS) and continuing priority when planning exploration missions. Interest from the private sector is already to the lunar vicinity, the lunar surface, then • The important role of science and knowl- transforming the future of low Earth orbit, on to Mars. The expanded group of agencies edge gain. Open interaction with the creating new opportunities as space agen- demonstrates the growing interest in space international science community helped cies look to expand human presence into exploration and the importance of coopera- identify specific scientific opportunities the Solar System. Growing capability and tion to realise individual and common goals created by the presence of humans and interest from the private sector indicate and objectives. their infrastructure as they explore the Solar a future for collaboration not only among System.
    [Show full text]
  • Local Area Network and Data Network for the Advanced Earth Observing Satellite, ADEOS System Kohei Arai
    Local area network and data network for the Advanced Earth Observing Satellite, ADEOS system Kohei Arai '* * Earth Observation Center, National Space Development Agency of Japan Abstract NASDA is planning the next generation of earth observation satellite, following MOS-1, MOS-1b, JER3-1, so called Advanced Earth Observing Satellite, ADEOS. ADEOS will carry Ocean Color and Temperature Scanner, OCTS, Advanced Visible and Near Infrared Radiometer, AVNIR and Anouncement Opportunity sensors, AO sensors and will require a quicl< data distribution. Not only direct broadcasting, but also data distribution through a network are usefull for the dissemination of such data. Therefore a data network of which users can access a quicklook image data base in a quasi real time basis is now considered. In order for the preoperational data handling, a local area network is taken into account for an ADEOS ground facility. The processed data are sent to the film recorder through the LAN together with histograms for the generation of look up table for the gamma correction. Key items of the processed data are also transmitted to the information retrieval subsystem for the registration. The aquired quick look data are transmitted to not only the film recorder but also quick look image data base and the information retreival subsystem in a real time basis. The aforementioned ideas and concept for the development of the ADEOS ground facility will be described in the proposed paper. Presented at the ISPRS held in Kyoto, Japan, in July 1988. 1 1 1 .. INTRODUCTION data starting with HOS-1 through ) the Polar respond or demands for earth observation from space, earth observation system consists of not only satellite but also ground facilities including data net\.>lorks for transmission of mission data, should matured and improved.
    [Show full text]
  • JAXA's Space Exploration Activities
    JAXA’s Space Exploration Activities Jun Gomi, Deputy Director General, JAXA Hayabusa 2 ✓ Asteroid Explorer of the C-type asteroid ✓ Launched in December, 2014 ✓ Reached target asteroid “Ryugu” in 2018 ✓ First successful touchdown to Ryugu on February 22, 2019 ✓ Return to Earth in 2020 (162173) Ryugu 2 Hayabusa 2 (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, Nagoya University, Chiba Institute of Technology, Meiji University, Nagoya University, Chiba Institute of Technology, Meiji University, University of Aizu and AIST. University of Aizu, AIST Asteroid Ryugu photographed from a Asteroid Ryugu from an altitude of 6km. distance of about 20 km. The image Image was captured with the Optical was taken on June 30, 2018. Navigation Camera on July 20, 2018. Hayabusa 2 4 JAXA’s Plan for Space Exploration International • Utilization of ISS/Kibo • Cis-Lunar Platform (Gateway) Cooperation • Lunar exploration and beyond Industry & • JAXA Space Exploration Innovation Academia Hub Partnerships • Science Community discussions JAXA’s Overall Scenario for International Space Exploration Mars, others ★ Initial Exploration ★ Full Fledge Exploration MMX: JFY2024 • Science and search for life • Utilization feasibility exam. Kaguya Moon ©JAXA ©JAXA ©JAXA ©JAXA ©JAXA Full-fledged Exploration & SLIM Traversing exploration(2023- ) Sample Return(2026- ) Utilization (JFY2021) • Science exploration • S/R from far side • Cooperative science/resource • Water prospecting • Technology demo for human mission exploration by robotic and human HTV-X der.(2026- ) • Small probe deploy, data relay etc. Gateway Phase 1 Gateway (2022-) Phase 2 • Support for Lunar science Earth • Science using deep space Promote Commercialization International Space Station 6 SLIM (Smart Lander for Investigating Moon) ✓ Demonstrate pin-point landing on the moon.
    [Show full text]
  • Initial Analysis Team Introduction
    Summary and contents of the press conference Overview • Since the return of the sample in December of last year, curation activities have been conducted for the initial analysis of the sample. • Curation activities are aimed at cataloguing the sample without compromising the scientific value in order to provide information that contributes to further detailed scientific analysis. • Today’s report is that part of the catalogued sample is ready for delivery. Contents 1. Report from the curation team (T. Usui, E. Nakamura, M. Ito) 2. Report from the initial analysis teamS. TachibanaH. YurimotoT. Nakamura T. NoguchiR. OkazakiH. YabutaH. Naraoka 2021/6/17 Hayabusa2 reporter briefing 2 Report from the curation team Tomohiro USUIJAXA Eizo NAKAMURAOkayama University Motoo ITOJAMSTEC Ryugu sample curation work The initial description of the Ryugu sample was performed without removing the sample from the clean chamber, in order to avoid contamination from the global environment CC3-1 Opening the sample container under vacuum environment CC3-2 Sample collection under vacuum CC3-3 Transition from vacuum to nitrogen environment CC4-1 Handling of submillimeter-sized particles CC4-2 Handling / observation / sorting of relatively large particles (> mm) 2021/6/17 Hayabusa2 reporter briefing 4 Achievement of the world’s first sample collection and storage of asteroid samples under vacuum conditions Samples collected under vacuum on December 15, 2020 will not be distributed at this time, but continued to be stored under vacuum (CC3-2) for future
    [Show full text]
  • Aqua: an Earth-Observing Satellite Mission to Examine Water and Other Climate Variables Claire L
    IEEE TRANSACTIONS ON GEOSCIENCE AND REMOTE SENSING, VOL. 41, NO. 2, FEBRUARY 2003 173 Aqua: An Earth-Observing Satellite Mission to Examine Water and Other Climate Variables Claire L. Parkinson Abstract—Aqua is a major satellite mission of the Earth Observing System (EOS), an international program centered at the U.S. National Aeronautics and Space Administration (NASA). The Aqua satellite carries six distinct earth-observing instruments to measure numerous aspects of earth’s atmosphere, land, oceans, biosphere, and cryosphere, with a concentration on water in the earth system. Launched on May 4, 2002, the satellite is in a sun-synchronous orbit at an altitude of 705 km, with a track that takes it north across the equator at 1:30 P.M. and south across the equator at 1:30 A.M. All of its earth-observing instruments are operating, and all have the ability to obtain global measurements within two days. The Aqua data will be archived and available to the research community through four Distributed Active Archive Centers (DAACs). Index Terms—Aqua, Earth Observing System (EOS), remote sensing, satellites, water cycle. I. INTRODUCTION AUNCHED IN THE early morning hours of May 4, 2002, L Aqua is a major satellite mission of the Earth Observing System (EOS), an international program for satellite observa- tions of earth, centered at the National Aeronautics and Space Administration (NASA) [1], [2]. Aqua is the second of the large satellite observatories of the EOS program, essentially a sister satellite to Terra [3], the first of the large EOS observatories, launched in December 1999. Following the phraseology of Y.
    [Show full text]
  • Launch / Tracking and Control Plan of Advanced Land Observing Satellite (ALOS) / H-IIA Launch Vehicle No
    Launch / Tracking and Control Plan of Advanced Land Observing Satellite (ALOS) / H-IIA Launch Vehicle No. 8 (H-IIA F8) November 2005 Japan Aerospace Exploration Agency (JAXA) (Independent Administrative Agency) - 1 - Table of Contents Page 1. Overview of the Launch / Tracking and Control Plan 1 1.1 Organization in Charge of Launch / Tracking and Control 1 1.2 Person in Charge of Launch / Tracking and Control Operations 1 1.3 Objectives of Launch / Tracking and Control 1 1.4 Payload and Launch Vehicle 1 1.5 Launch Window (Day and Time) 2 1.6 Facilities for Launch / Tracking and Control 2 2. Launch Plan 3 2.1 Launch Site 3 2.2 Launch Organization 4 2.3 Launch Vehicle Flight Plan 5 2.4 Major Characteristics of the Launch Vehicle 5 2.5 Outline of the Advanced Land Observing Satellite (ALOS) 5 2.6 Securing Launch Safety 5 2.7 Correspondence Method of Launch information to Parties Concerned 6 3. Tracking and Control Plan 8 3.1 Tracking and Control Plan of the ALOS 8 3.1.1 Tracking and Control Sites 8 3.1.2 Tracking and Control Organization 8 3.1.3 Tracking and Control Period 8 3.1.4 Tracking and Control Operations 10 3.1.5 ALOS Flight Plan 10 3.1.6 Tracking and Control System 10 4. Launch Result Report 11 [List of Tables] Table-1: Launch Vehicle Flight Plan 13 Table-2: Major Characteristics of the Launch Vehicle 15 Table-3: Major Characteristics of the ALOS 17 Table-4: Tracking and Control Plan (Stations) of the ALOS 23 [List of Figures] Figure-1: Map of Launch / Tracking and Control Facilities 12 Figure-2: Launch Vehicle Flight Trajectory 14 Figure-3: Configuration of the Launch Vehicle 16 Figure-4: On-orbit Configuration of the ALOS 20 Figure-5: Access Control Areas for Launch 21 Figure-6: Impact Areas of the Launch Vehicle 22 Figure-7: ALOS Flight Plan 24 Figure-8: ALOS Footprint 25 Figure-9: ALOS Tracking and Control System 26 - 2 - 1.
    [Show full text]
  • X103 H-IIB Launch Vehicle H-IIBロケット
    Outdoor Exhibition Outdoor X103 H-IIB Launch Vehicle H-IIBロケット ■Purpose of Exhibition The domestically produced large rocket "H-IIB" is exhibited in the outdoor exhibition space. Most of this rocket has the same structure as the real rocket and served as a test. You can find the real parts in the chart including the first stage engine section, the first stage fuel tank, the center body section, the interstage adapter and the fairing, which are exhibited in the exhibition. The rest of the parts were made by referring to the actual rocket. When the rocket "H-IIB" is launched, two other main engines and four fixed rocket boosters are attached to the rocket. You can see the inside structure because the tank part is cut off. For making a light but strong rocket, it is manufactured like a honeycomb. For pouring low temperature liquid- hydrogen into the tank, the exterior of the rocket is coated by a thermal material. The rocket which is exhibited is also coated by using the same thermal material. Like this, the rockets were made by using the latest manufacturing technology and design techniques. We would like you to learn the structure of rocket and feel how big it is. ■Additional Knowledge Space Station had succeeded. The Japanese high- launching technology which put the rocket into the planned orbit accurately, and the connecting technology which controlled the HTV delicately and connected to the International Space Station in outer space, has been shown to the world. [The Other Rockets Exhibition in Japan] There are rocket exhibitions in regions where JAXA developed space technology (as of 2010).The Tanegashima Space Center is where the JAXA Research Institute is located in Tanegashima, Kagoshima Prefecture.
    [Show full text]
  • Tuesday, March 2, 2010 POSTER SESSION I: MISSION PLANS and CONCEPTS 7:00 P.M
    41st Lunar and Planetary Science Conference (2010) sess336.pdf Tuesday, March 2, 2010 POSTER SESSION I: MISSION PLANS AND CONCEPTS 7:00 p.m. Town Center Exhibit Area Benkhoff J. The BepiColombo Mission to Explore Mercury [#1743] BepiColombo is an ESA, JAXA interdisciplinary mission to explore the planet Mercury. Two spacecrafts, the Mercury Planetary Orbiter (MPO) and the Mercury Magnetospheric Orbiter (MMO), will be studying the planet and its environment and launched together in July 2014. Balint T. S. Kerzhanovich V. V. Hall J. L. Baines K. H. Stephens S. K. Four Aspects of a Venus Balloon Mission Concept [#1301] Our poster explores four aspects of a typical Venus balloon mission concept using information design techniques, including a typical timeline; the atmospheric entry sequence; maps of the balloon’s traverse path; and the material selection challenges. Klaus K. Cook T. S. Smith D. B. Small Body Landers for Near Earth Object Missions [#1077] We are developing a small body lander product line that leverages the significant investments that have been made in the highly successful DARPA Orbital Express program. Smith D. B. Klaus K. Caplin G. Elsperman M. S. Horsewood J. Low Cost Multiple Near Earth Object Missions [#1464] Our Commercial spacecraft are available with efficient high power solar arrays and hybrid propulsion systems (Chemical and Solar Electric) that make possible multiple Near Earth Object Missions within Discovery budget limits. Ping J. S. Qian Z. H. Hong X. Y. Zheng W. M. Fung L. W. Liu Q. H. Zhang S. J. Shang K. Jian N. C. Shi X. Wang M.
    [Show full text]
  • 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
    [Show full text]
  • Successful Mission of Tupod, an Innovative Cubesat, a Tubesats Deployer Manufactured Via Additive Manufacturing by CRP USA Using Windform® XT 2.0 Composite Material
    Successful mission of TuPOD, an innovative CubeSat, a TubeSats deployer manufactured via Additive Manufacturing by CRP USA using Windform® XT 2.0 composite material ABSTRACT Small satellites provide a responsive alternative to larger, more expensive satellites. As demand grows, engineers must adapt these “nanosatellites” or CubeSats to provide new achievements and goals. One of these achievements is deploying TubeSats from International Space Station (ISS). TubeSats are cylindrical shape and are not compatible with normal CubeSats deployer platform (P-POD) on ISS, thus, an innovative nano-satellite, TuPOD (Tubesat-POD), was developed to address the challenge. TuPOD inaugurated a new era for scientists wanting to use small, highly reliable satellites. It is the first complete 3D printed satellite launched from the ISS, made by CRP USA from CRP Technology’s proprietary material Windform® XT 2.0, the ground breaking carbon fiber reinforced composite 3D printing material known for its mechanical properties, developed with CRP USA. (shown in Figure 1) Figure 1: TuPOD deployed © JAXA / NASA OVERVIEW The story of TuPOD began when a group of Brazilian Students needed to launch their TubeSat, TANCREDO-1, from ISS. They approached G.A.U.S.S. Srl (Group of Astrodynamics for the Use of Space Systems), an Italian company with close relationship to the University of Rome, to help them overcoming the challenge of launching their TubeSat from ISS. CRP USA LLC Headquarters Office 127 Goodwin Circle, Mooresville NC 28115 Phone 704-660-0258 GAUSS was faced with the challenge of designing an innovative system to deploy the first TubeSats into orbit that could act as both a satellite and release platform.
    [Show full text]
  • JAXA's Lunar Exploration Activities
    June 17th 2019, 62nd Session of COPUOS, Vienna JAXA’s Lunar Exploration Activities Hiroshi Sasaki Director, JAXA Space Exploration Center (JSEC) Japan Aerospace Exploration Agency 1 JAXA’s Space Exploration Scenario Mars, others Activities on/beyond Mars ©JAXA MMX JFY2024 Kaguya ©JAXA ©JAXA ©JAXA ©JAXA Moon SLIM Lunar Polar Exploration Robotic Sample Return Pinpoint Landing Water Prospecting Sustainable JFY2021 (HERACLES) prox.2023- Technology Demo Exploration/Utilization Approx.2026- HTV-X derivatives Gateway Approx. 2026- Operation OMOTENASHI EQUULEUS CubeSat Innovative launched by small mission Gateway (construction phase) SLS/EM1 2022- Earth Promote Commercialization International Space Station 2 ©NASA International Space Exploration Coordination Group (ISECG): • ISECG is a non-political agency coordination forum of space organization from 18 countries and regions. • JAXA is currently the chair of ISECG. • ISECG agencies work collectively in a non-binding, consensus-driven manner towards advancing the Global Exploration Strategy. The Global Exploration Roadmap (GER3) recognizes the importance of increasing synergies with robotic missions while demonstrating the role humans play in realizing societal benefits. GER3, released in January 2018 3 Significance of Lunar Exploration Expand Human Activities Gain Knowledge International Cooperation ©NASA Promote Industry Inspire Young Generation 4 JAXA’s Lunar Exploration Roadmap (Long-Team) Lunar Base (International Space Agency, Private Sector) 2060- Sustainable Exploration (Private Utilization)
    [Show full text]