DOCSLIB.ORG

Saku Tsuneta Director General

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Saku Tsuneta Director General Message from the Director General April 2015 Saku Tsuneta Director General Institute of Space and Astronautical Science Japan Aerospace Exploration Agency While the Institute of Space and Astronautical operation of the magnetosphere observation satellite Science (ISAS) is a part of the Japan Aerospace “Akebono” launched in 1989, was terminated due to Exploration Agency, at the same time, it has been deterioration of the instruments and a lowered flight operated as the Inter-University Research System altitude. “Akebono”, carried out observation activities (Institute) (*1). This makes ISAS a unique research of aurora and the Van Allen radiation belt for 26 institute. ISAS, being a research hub for research- years, and resulted in 311 refereed paper and 254 ers around the nation, has realized missions that theses (36 of them are doctoral thesis). cannot be accomplished by an individual university or institute. Under close collaboration with research- ISAS currently operates 7 satellites and probes, ers in space science and space engineering, ISAS including “Hayabusa 2”, (*2) PROCYON, “Hisaki”, has proposed and executed a series of ambitious “Akatsuki”, “Hinode”, “Suzaku”, and “GEOTAIL”. Of projects, including the “Hayabusa” mission. ISAS has these, over 700 refereed papers involving the X- been taking a major role in space science research ray astronomy satellite “SUZAKU” and over 900 (*3) alongside NASA and ESA. refereed papers involving the solar physics satellite “HINODE” have been published. ISAS has played a Research activities at ISAS in 2014 were numer- significant role in the international scientific commu- ous. The first article regarding “Hisaki” (the satellite nity. For other examples, the far infrared all sky im- launched by the first Epsilon rocket in September age data provided by the infrared astronomical satel- 2013) appeared in the journal “Science”. Also notable lite “Akari“ (operation completed in November 2011) was the successful launch of “Hayabusa 2” and a was released. The recovery effort for the Venus cli- very small probe PROCYON by the H-IIA rocket at mate orbiter “Akatsuki” is undergoing. The successful the end of 2014. In the current plan, “Hayabusa 2” inserting into the Venus orbit is expected after the will reach the asteroid 1999JU3 to collect samples first attempt at the end of 2010, was unsccessful. and return to Earth in 2020, the year of the Tokyo Olympics. PROCYON is developed mainly by the ISAS has made impressive achievements across a University of Tokyo in cooperation with JAXA. wide variety of research fields using sounding rockets This unique ISAS structure made the short term and scientific balloons, the development of a reusable development possible. PROCYON has several mission rocket, and various experiments utilizing the space objectives including demonstration of technologies environment of the International Space Station. such as a 50kg-class spacecraft bus, high-efficiency Through collaboration with the Graduate University communication amplifier, and precise VLBI naviga- for Advanced Studies and the University of Tokyo, tion as well as imaging of the geocorona. This world’ future researchers are nurtured by receiving their s first deep-space exploration micro spacecraft is graduate school education in the direct development drawing international attention. Meanwhile, the of space experiment. Also, outstanding early-career (*1) Inter-University Research System is a mechanism to allow researchers affiliated with universities and ISAS to jointly and seamlessly conduct various leading-edge collaborative researches. ISAS plays a role of the national research hub for space science. (*2) Jointly conducted with JSPEC (JAXA’s Space Exploration Center) until March 2015 (*3) Based on Thomson Reuters “Web of Science” database researchers have made remarkable achievements Based on this policy, since assuming the post in cooperation with ISAS researchers and graduate of ISAS Director General, in cooperation with the students through the JAXA International Top Young Management and Integration Department that Fellowship. has flexibility and solution proposal capabilities, I have pursued internal reforms such as reducing In addition to these activities, the following operational costs to promote new activities, clarifying projects have commenced: the development of an the decision making mechanism, appointing younger X-ray astronomy satellite (ASTRO-H), a geospace generation people to high positions, activating per- exploration satellite (ERG), and a Mercury explora- sonnel of the academic staff, and enhancing scientific tion satellite Bepi-Colombo; the promotion of the public relations. We also continue to investigate and enhanced Epsilon rocket project in cooperation analyze the academic achievement at ISAS. The with Space Technology Directorate I (the former age distribution and promotion scheme indicate that Space Transportation Mission Directorate); and the ISAS has an aging academic staff with low mobility. development of the new deep space antenna in This requires serious effort to amend. Needless to Usuda in cooperation with the Space Tracking and say, appropriate personnel assignment of academic Communications Center (the former Space Tracking staff is vital in revitalizing the research institute. In and Data Acquisition Department), JAXA. The new JFY 2014, a number of new personnel management deep space antenna is to replace the aging current practices were adopted. The direction of ISAS and antenna and to undertake deep space communica- the necessary human resources for future new tions for the next several decades. ASTRO-H has projects are indicated in the Space Science Roadmap a Soft X-ray Spectrometer that has a very high reported to the Space Science and Exploration Pannel energy-resolution, and astronomers across the world of the Space Policy Commission under the cabinet have high hopes for its achievements. ERG, a small office. Based on these indications, we are to consider science satellite following “Hisaki”, is mounted with personnel management carefully with a long-term a newly developed “plasma wave particle interaction view point. analyzer system”. It is expected to elucidate “rela- tivistic particle acceleration” in radiation belts and to A team of experts in JAXA have analyzed the contribute to space weather forecasting based on the challenges ISAS is facing and summarized the im- findings. Bepi Colombo is planned to be launched in provement proposal in “Taskforce Proposal regarding (Japanese Fiscal Year (JFY)) 2016 and is scheduled Improvement in Executing Space Science Program”. to enter Mercury orbit in JFY 2024. Very significant (December 2012). Based on the proposal, ISAS has results are expected for Bepi Colombo as it is going created an action plan. 90 staff have participated in to conduct the first observations of Mercury’s mag- town meetings held twice to share and discuss the netosphere and surface. The consecutive launches issues. I believe that our performance will improve from ASTRO-H in JFY 2015 to Bepi Colombo by ESA as internal and external project members creatively will require a lot of energy and focus. adapt the action plan. The skeleton of the Action Plan is as follows; As described, ISAS has vigorously conducted many research activities, but we should not assume 1. In order to soundly accomplish the challenging that in future all will go smoothly. There have been mission with limited resources, return to the failures in our history. LUNAR-A and ASTRO-G were basics. Make a systematic effort to manage target driven to termination. “Nozomi” (Mars) and “Akatsu- specifications which projects should pursue, ki” (Venus) have not been inserted into their planned estimate the expendable cost and schedule. planetary orbits. The cause was considered as a 2. Manage projects with focus on “certainty”, “ten- malfunction in the propelling system and electrical ability”, and “minimization of risk”. As for the system, but the development difficulty was not high. technically challenging part, apply a step by step Also, the recent missions that are under development approach for specification determination. experience increases in cost and delays in schedule. 3. Appoint a project manager who has a high project The lesson is that approaches that may well have management capability. The appointed project worked to date still have room for improvement. manager is not always an ISAS researcher. Appro- This means that ISAS is capable of achieving break- priately allocate the responsibility for one project throughs by solving issues and reforming itself. manager. 4. Form the management team centering on the highly effective because it brings the world’s best project manager, Practice high quality manage- technology, highly-skilled human resources, and the ment by sharing and cooperating in the project. budget together to jointly develop one satellite. We 5. Communicate closely with the science community are to continue enhancing international cooperation by placing scientifically excellent personnel on the with overseas space agencies to deploy post ASTRO- team. H international missions. Especially, from the last 6. Secure opportunities for young researchers in fiscal year our focus has been on the next-generation order to nurture the next generation leaders. infrared astronomical satellite, SPICA which is a 7. Clarify the evaluation axis to properly evaluate the center of attention by astronomers across the world. academic research staff that concentrates on the By
Load more

Recommended publications
  • Multiple Polar Cap Arcs: Akebono &Lpar;Exos D&Rpar; Observations
    Radio Science,Volume 31, Number 3, Pages645-653, May-June 1996 Multiple polar cap arcs: Akebono (Exos D) observations T. Obara, T. Mukai, H. Hayakawa, K. Tsuruda, A. Matsuoka, and A. Nishida Institute of Spaceand AstronauticalScience, Kanagawa, Japan H. Fukunishi Department of Geophysicsand Astrophysics,Tohoku University,Sendai, Japan Center for Atmosphericand SpaceSciences, Utah State University,Logan Abstract. Akebono (Exos D) observationsdemonstrate that polar cap arcssometimes have a fine structure,that is, multiple (doubleor triple) arcswith spacingof a few tens of kilometers.The multiplepolar cap arcsare dominantlyobserved in the nightsidepolar cap region, suggestingthat low backgroundconductance favors the appearanceof the structuredarcs. A relationshipbetween the spacingand the averageenergy of the precipitatingelectrons is investigated.Results show that a higher energyleads to a wider spacing.Akebono observationsalso showthe existenceof a downwardcurrent region embeddedbetween upward current regions (arcs). Comparison of the observationswith resultsfrom a coupledmagnetosphere-ionosphere Sun-aligned arc model is made, which showsgood qualitativeagreement between the modelingand observationalresults on the spacing-energydependence and the effect of backgroundionospheric conductance. Introduction dawn-to-duskcomponent of the electric field is the major contributorto the negativedivE. These results The electronsreaching low altitudes in the polar suggestthat localized electron precipitation in the cap region were categorized as "polar
    [Show full text]
  • New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period
    Hayabusa2 Extended Mission: New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period M. Hirabayashi1, Y. Mimasu2, N. Sakatani3, S. Watanabe4, Y. Tsuda2, T. Saiki2, S. Kikuchi2, T. Kouyama5, M. Yoshikawa2, S. Tanaka2, S. Nakazawa2, Y. Takei2, F. Terui2, H. Takeuchi2, A. Fujii2, T. Iwata2, K. Tsumura6, S. Matsuura7, Y. Shimaki2, S. Urakawa8, Y. Ishibashi9, S. Hasegawa2, M. Ishiguro10, D. Kuroda11, S. Okumura8, S. Sugita12, T. Okada2, S. Kameda3, S. Kamata13, A. Higuchi14, H. Senshu15, H. Noda16, K. Matsumoto16, R. Suetsugu17, T. Hirai15, K. Kitazato18, D. Farnocchia19, S.P. Naidu19, D.J. Tholen20, C.W. Hergenrother21, R.J. Whiteley22, N. A. Moskovitz23, P.A. Abell24, and the Hayabusa2 extended mission study group. 1Auburn University, Auburn, AL, USA ([email protected]) 2Japan Aerospace Exploration Agency, Kanagawa, Japan 3Rikkyo University, Tokyo, Japan 4Nagoya University, Aichi, Japan 5National Institute of Advanced Industrial Science and Technology, Tokyo, Japan 6Tokyo City University, Tokyo, Japan 7Kwansei Gakuin University, Hyogo, Japan 8Japan Spaceguard Association, Okayama, Japan 9Hosei University, Tokyo, Japan 10Seoul National University, Seoul, South Korea 11Kyoto University, Kyoto, Japan 12University of Tokyo, Tokyo, Japan 13Hokkaido University, Hokkaido, Japan 14University of Occupational and Environmental Health, Fukuoka, Japan 15Chiba Institute of Technology, Chiba, Japan 16National Astronomical Observatory of Japan, Iwate, Japan 17National Institute of Technology, Oshima College, Yamaguchi, Japan 18University of Aizu, Fukushima, Japan 19Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA 20University of Hawai’i, Manoa, HI, USA 21University of Arizona, Tucson, AZ, USA 22Asgard Research, Denver, CO, USA 23Lowell Observatory, Flagstaff, AZ, USA 24NASA Johnson Space Center, Houston, TX, USA 1 Highlights 1.
    [Show full text]
  • View Conducted by Its Standing Review Board (SRB)
    Science Committee Report Dr. Wes Huntress, Chair 1 Science Committee Members Wes Huntress, Chair Byron Tapley, (Vice Chair) University of Texas-Austin, Chair of Earth Science Alan Boss, Carnegie Institution, Chair of Astrophysics Ron Greeley, Arizona State University, Chair of Planetary Science Gene Levy, Rice University , Chair of Planetary Protection Roy Torbert, University of New Hampshire, Chair of Heliophysics Jack Burns, University of Colorado Noel Hinners, Independent Consultant *Judith Lean, Naval Research Laboratory Michael Turner, University of Chicago Charlie Kennel, Chair of Space Studies Board (ex officio member) * = resigned July 16, 2010 2 Agenda • Science Results • Programmatic Status • Findings & Recommendations 3 Unusual Thermosphere Collapse • Deep drop in Thermospheric (50 – 400 km) density • Deeper than expected from solar cycle & CO2 4 Aeronomy of Ice in the Mesosphere (AIM) unlocking the secrets of Noctilucent Clouds (NLCs) Form 50 miles above surface in polar summer vs ~ 6 miles for “norm79al” clouds. NLCs getting brighter; occurring more often. Why? Linked to global change? AIM NLC Image June 27, 2009 - AIM measured the relationship between cloud properties and temperature - Quantified for the first time, the dramatic response to small changes, 10 deg C, in temperature - T sensitivity critical for study of global change effects on mesosphere Response to Gulf Oil Spill UAVSAR 23 June 2010 MODIS 31 May 2010 ASTER 24 May 2010 Visible Visible/IR false color Satellite instruments: continually monitoring the extent of
    [Show full text]
  • Wide-Field Infrared Survey Explorer Launch Press
    PRess KIT/DECEMBER 2009 Wide-field Infrared Survey Explorer Launch Contents Media Services Information ................................................................................................................. 3 Quick Facts ............................................................................................................................................. 4 Mission Overview .................................................................................................................................. 5 Why Infrared? ....................................................................................................................................... 10 Science Goals and Objectives ......................................................................................................... 12 Spacecraft ............................................................................................................................................. 16 Science Instrument ............................................................................................................................. 19 Infrared Missions: Past and Present ............................................................................................... 23 NASA’s Explorer Program ................................................................................................................. 25 Program/Project Management .......................................................................................................... 27 Media Contacts J.D. Harrington
    [Show full text]
  • Probes to the Inferior Planets – a New Dawn for Neo and Ieo Detection Technology Demonstration from Heliocentric Orbits Interior to the Earth’S?
    PROBES TO THE INFERIOR PLANETS – A NEW DAWN FOR NEO AND IEO DETECTION TECHNOLOGY DEMONSTRATION FROM HELIOCENTRIC ORBITS INTERIOR TO THE EARTH’S? 2011 IAA Planetary Defense Conference 09-12 May 2011 Bucharest, Romania Jan Thimo Grundmann(1), Stefano Mottola(2), Maximilian Drentschew(6), Martin Drobczyk(1), Ralph Kahle(3), Volker Maiwald(4), Dominik Quantius(4), Paul Zabel(4), Tim van Zoest(5) (1)DLR German Aerospace Center - Institute of Space Systems - Department of Satellite Systems Robert-Hooke-Straße 7, 28359 Bremen, Germany Email: [email protected], [email protected] (2)DLR German Aerospace Center - Institute of Planetary Research - Department Asteroids and Comets Rutherfordstraße 2, 12489 Berlin, Germany Email: [email protected] (3)DLR German Aerospace Center - Space Operations and Astronaut Training - Space Flight Technology Dept. 82234 Oberpfaffenhofen-Wesseling, Germany Email: [email protected] (4)DLR German Aerospace Center - Institute of Space Systems - Dept. System Analysis Space Segments (SARA) Robert-Hooke-Straße 7, 28359 Bremen, Germany Email: [email protected], [email protected], [email protected] (5)DLR German Aerospace Center - Institute of Space Systems - Department of Exploration Systems Robert-Hooke-Straße 7, 28359 Bremen, Germany Email: [email protected] (6)ZFT Zentrum für Telematik Allesgrundweg 12, 97218 Gerbrunn, Germany Email: [email protected] ABSTRACT With the launch of MESSENGER and VENUS EXPRESS, a new wave of exploration of the inner solar system has begun. Noting the growing number of probes to the inner solar system, it is proposed to connect the expertise of the respective spacecraft teams and the NEO and IEO survey community to best utilize the extended cruise phases and to provide additional data return in support of pure science as well as planetary defence.
    [Show full text]
  • Mp-Ist-056-32
    UNCLASSIFIED/UNLIMITED The International Reference Ionosphere – Climatological Standard for the Ionosphere Dieter Bilitza Raytheon IS, Space Physics Data Facility GSFC, Code 612.4 Greenbelt, MD 20771 U.S.A. [email protected] ABSTRACT The International Reference Ionosphere (IRI) a joint project of URSI and COSPAR is the defacto standard for a climatological specification of ionospheric parameters. IRI is based on a wide range of ground and space data and has been steadily improved since its inception in 1969 with the ever-increasing volume of ionospheric data and with better mathematical descriptions of the observed global and temporal variation patterns. The IRI model has been validated with a large amount of data including data from the most recent ionospheric satellites (KOMPSAT, ROCSAT and TIMED) and data from global network of ionosondes. Several IRI teams are working on specific aspects of the IRI modeling effort including an improved representation of the topside ionosphere with a seamless transition to the plasmasphere, a new effort to represent the global variation of F2 peak parameters using the Neural Network (NN) technique, and the inclusion of several additional parameters in IRI, e.g., spread-F probability and ionospheric variability. Annual IRI workshops are the forum for discussions of these efforts and for all science activities related to IRI as well as applications of the IRI model in engineering and education. In this paper I will present a status report about the IRI effort with special emphasis on the presentations and results from the most recent IRI Workshops (Paris, 2004; Tortosa, 2005) and on the most important ongoing IRI activities.
    [Show full text]
  • Hinode Project and Science Center (Hinode-SC)
    Hinode Project and Science Center (Hinode-SC) Shinsuke Imada (Nagoya Univ., ISEE) Characteristics of the Advanced Telescopes | Hinode Science Center at NAOJ 2019/10/13 22(30 For Researchers 日本語 シェア Tweet “Hinode” Unveils To do research Information Gallery For Researchers the Mysteries of the Sun using Hinode data TOP "Hinode" Unveils the Mysteries of the Sun Characteristics of the Advanced Telescopes Solar Observing Satellite "Hinode" (SOLAR-B) | Hinode Science Center at NAOJ 2019/10/13 22(29 "Hinode" Unveils Characteristics of the Advanced Telescopes the Mysteries of the For Researchers 日本語 Sun Tweet シェア Overview of “Hinode” “Hinode” Unveils To do research Characteristics of the Advanced Telescopes Solar Observing Information Gallery For Researchers Satellite "Hinode" the Mysteries of the Sun using Hinode data (SOLAR-B) The Sun's atmosphere is comprised of layers. The layers beneath the surface (photosphere) cannot be TOP "Hinode" UnveilsSolar the Mysteries of the Sun ObservingSolar Observing Satellite "Hinode" (SOLAR-B) Satelliteseen “ directly,Hinode but the upper layers ”above (SOLAR the photosphere each emit- differentB) wavelengths of lights. So, About the "Hinode" Project you can see each layer by changing the observing wavelength. By loading three telescopes observing in "Hinode" Unveils Solar Observing Satellite "Hinode" (SOLAR-B) different wavelengththe Mysteries ranges, of the Hinode can simultaneously observe from the photosphere to the corona (upper atmosphere).Sun Characteristics of the Advanced Telescopes Overview of “Hinode”
    [Show full text]
  • Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology
    Achievements of Hayabusa2: Unveiling the World of Asteroid by Interplanetary Round Trip Technology Yuichi Tsuda Project Manager, Hayabusa2 Japan Aerospace ExplorationAgency 58th COPUOS, April 23, 2021 Lunar and Planetary Science Missions of Japan 1980 1990 2000 2010 2020 Future Plan Moon 2007 Kaguya 1990 Hiten SLIM Lunar-A × Venus 2010 Akatsuki 2018 Mio 1998 Nozomi × Planets Mercury (Mars) 2010 IKAROS Venus MMX Phobos/Mars 1985 Suisei 2014 Hayabusa2 Small Bodies Asteroid Ryugu 2003 Hayabusa 1985 Sakigake Asteroid Itokawa Destiny+ Comet Halley Comet Pheton 2 Hayabusa2 Mission ✓ Sample return mission to a C-type asteroid “Ryugu” ✓ 5.2 billion km interplanetary journey. Launch Earth Gravity Assist Ryugu Arrival MINERVA-II-1 Deployment Dec.3, 2014 Sep.21, 2018 Dec.3, 2015 Jun.27, 2018 MASCOT Deployment Oct.3, 2018 Ryugu Departure Nov.13.2019 Kinetic Impact Earth Return Second Dec.6, 2020 Apr.5, 2019 Target Markers Orbiting Touchdown Sep.16, 2019 Jul,11, 2019 First Touchdown Feb.22, 2019 MINERVA-II-2 Orbiting MD [D VIp srvlxp #534<# Oct.2, 2019 Hayabusa2 Spacecraft Overview Deployable Xband Xband Camera (DCAM3) HGA LGA Xband Solar Array MGA Kaba nd Ion Engine HGA Panel RCS thrusters ×12 ONC‐T, ONC‐W1 Star Trackers Near Infrared DLR MASCOT Spectrometer (NIRS3) Lander Thermal Infrared +Z Imager (TIR) Reentry Capsule +X MINERVA‐II Small Carry‐on +Z LIDAR ONC‐W2 +Y Rovers Impactor (SCI) +X Sampler Horn Target +Y Markers ×5 Launch Mass: 609kg Ion Engine: Total ΔV=3.2km/s, Thrust=5-28mN (variable), Specific Impulse=2800- 3000sec. (4 thrusters, mounted on two-axis gimbal) Chemical RCS: Bi-prop.
    [Show full text]
  • Building the Coolest X-Ray Satellite
    National Aeronautics and Space Administration Building the Coolest X-ray Satellite 朱雀 Suzaku A Video Guide for Teachers Grades 9-12 Probing the Structure & Evolution of the Cosmos http://suzaku-epo.gsfc.nasa.gov/ www.nasa.gov The Suzaku Learning Center Presents “Building the Coolest X-ray Satellite” Video Guide for Teachers Written by Dr. James Lochner USRA & NASA/GSFC Greenbelt, MD Ms. Sara Mitchell Mr. Patrick Keeney SP Systems & NASA/GSFC Coudersport High School Greenbelt, MD Coudersport, PA This booklet is designed to be used with the “Building the Coolest X-ray Satellite” DVD, available from the Suzaku Learning Center. http://suzaku-epo.gsfc.nasa.gov/ Table of Contents I. Introduction 1. What is Astro-E2 (Suzaku)?....................................................................................... 2 2. “Building the Coolest X-ray Satellite” ....................................................................... 2 3. How to Use This Guide.............................................................................................. 2 4. Contents of the DVD ................................................................................................. 3 5. Post-Launch Information ........................................................................................... 3 6. Pre-requisites............................................................................................................. 4 7. Standards Met by Video and Activities ...................................................................... 4 II. Video Chapter 1
    [Show full text]
  • Highlights in Space 2010
    International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no.
    [Show full text]
  • Jaxa Today 10.Pdf
    Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. We examine the H3’s unique features and the development program’s pinned by this philosophy, JAXA pursues a broad range of pro- objectives.
    [Show full text]
  • Co-Aligned IRIS, SDO and Hinode Data Cubes Release 1.0
    Co-aligned IRIS, SDO and Hinode data cubes Release 1.0 Milan Gošic´ Feb 26, 2020 CONTENTS 1 Introduction 1 1.1 About this Guide.............................................1 1.2 Synopsis of the IRIS, Hinode and SDO missions............................1 1.3 Hinode and SDO data cubes co-aligned with IRIS observations....................2 2 Finding and downloading IRIS-SDO-Hinode co-aligned data cubes5 2.1 Using the IRIS Webpage (HCR).....................................5 2.2 Using SSWIDL..............................................5 3 Reading and browsing IRIS-SDO-Hinode co-aligned data cubes 11 3.1 Reading level 2 co-aligned SDO and Hinode datasets.......................... 11 3.2 Browsing co-aligned SDO and Hinode data cubes with CRISPEX................... 13 i ii CHAPTER ONE INTRODUCTION 1.1 About this Guide The purpose of this guide is to provide detailed instructions on how users can find, download, browse, and analyze co-aligned level 2 data obtained with The Interface Region Imaging Spectrograph (IRIS), the Atmospheric Imaging Assembly (AIA) on board the Solar Dynamics Observatory (SDO), and Hinode/SOT level 2 data. The IRIS team at the Lockheed Martin Solar and Astrophysics Laboratory (LMSAL) created new data cubes consisting of the Hinode/SOT and SDO/AIA images co-aligned with the simultaneous IRIS observations. These datasets all have the same IRIS level 2 FITS format, therefore can be accessed and examined using the IRIS SolarSoft software. In this guide, we provide step by step instructions how to access, read, and visualize these newly created co-aligned data cubes. In particular, we describe: • How to find data using SolarSoft IDL routines; • How to acquire data sets using either SolarSoft or Heliophysics Coverage Registry (HCR); • How to read data and visualize them using SolarSoft routines or Crisp Spectral Explorer (CRISPEX).
    [Show full text]