Physics of the Cosmos Newsletter, December 2017, Vol. 7, No. 1
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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. -
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. -
Attitude Control Dynamics of Spinning Solar Sail “IKAROS” Considering
Attitude Control Dynamics of Spinning Solar Sail “IKAROS” Considering Thruster Plume Osamu Mori, Yoji Shirasawa, Hirotaka Sawada, Ryu Funase, Yuichi Tsuda, Takanao Saiki and Takayuki Yamamoto (JAXA), Morizumi Motooka and Ryo Jifuku (Univ. of Tokyo) Abstract In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. First Mode Model of out-of-plane deformation (FMM) and Multi Particle Model (MPM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is very simple and valid for the design of attitude controller. Considering the thruster configuration of IKAROS, the force on main body and sail by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. スラスタプルームを考慮したスピン型ソーラーセイル「IKAROS」の姿勢制御運動 森 治,白澤 洋次,澤田 弘崇,船瀬 龍,津田 雄一,佐伯 孝尚,山本 高行(JAXA), 元岡 範純,地福 亮(東大) 摘要 本論文ではスピン型ソーラーセイル IKAROS の姿勢運動について示す.スピン型ソーラーセイル を解析するために一次面外変形モデルおよび多粒子モデルを導入する.まず,一次面外変形モデ ルから導出される 3 つのモードが IKAROS の面外運動を支配していることを示す.このモデルは 非常に簡易であり,姿勢制御設計に有効であると言える.一方,多粒子モデルに対しては, IKAROS のスラスタ配置を考慮して,スラスタの反力だけでなくスラスタプルームが本体や膜面 に及ぼす力を組み込み,セイル展開後およびスラスタによるマヌーバ後の姿勢運動を数値シミュ レーションにより詳細に解析する. 1. Introduction for the numerical model. Considering the thruster configuration of IKAROS, the force on main body and A solar sail 1) is a space yacht that gathers energy for sail by thruster plume as well as reaction force by propulsion from sunlight pressure by means of a thruster are integrated into MPM. The Fast Fourier membrane. The Japan Aerospace Exploration Agency Transform (FFT) results from IKAROS flight data are (JAXA) successfully achieved the world’s first solar sail compared with those from simulation data. -
Road Map of HEAPA-Related Future Missions HEAPA 4Th Future Plan Review Committee 2020/10-2022/9 Lead: Kazuhiro Nakazawa (Nagoya-U/KMI)
20th HEAPA WS 2021/3/8-10 Road map of HEAPA-related future missions HEAPA 4th Future Plan Review Committee 2020/10-2022/9 Lead: Kazuhiro Nakazawa (Nagoya-U/KMI) JAXA Summary of the 3rd committee outcome Vision Preface Astronomical X-ray and Gamma-ray observations are directly related with understanding the how matter and energy exits within the Universe, not only celestial objects, but also the volume itself. They are also key enablers to dig into the extreme physics. In the two broadest aims of astrophysical research, understand the Universe as of now, and understand how it came to be as such, high-energy astrophysics plays an essential role. Summary of the 3rd committee outcome Vision: three big goals Understand our Universe; matter, energy and spacetime, and its origin Dark matter : LSS/clusters to see where DM are, and search for DM direct signal Missing baryon : how the baryon and metals are distributed in the Universe Origins of the large diversity in Universe and celestial objects Galaxy and SMBH co-evolution and their impact on re-ionization Metal synthesis in the Universe Relativistic high-energy phenomena in the Universe Verifying fundamental physics in extreme condition Extreme gravitation : stellar-mass BH, SMBH Extreme high-density matter EoS : Neutron star, quark star Extreme magnetism : Magnetar Diffusive shock : wide variety of yet to be known interactions therein Dark Matter (Re): search for its direct signal Summary of the 3rd committee outcome Mission Categories by JAXA class How to launch Definition and budget Strategic H-IIA, H-III Top science. Flagship mission of Large class each community. -
Sg423finalreport.Pdf
Notice: The cosmic study or position paper that is the subject of this report was approved by the Board of Trustees of the International Academy of Astronautics (IAA). Any opinions, findings, conclusions, or recommendations expressed in this report are those of the authors and do not necessarily reflect the views of the sponsoring or funding organizations. For more information about the International Academy of Astronautics, visit the IAA home page at www.iaaweb.org. Copyright 2019 by the International Academy of Astronautics. All rights reserved. The International Academy of Astronautics (IAA), an independent nongovernmental organization recognized by the United Nations, was founded in 1960. The purposes of the IAA are to foster the development of astronautics for peaceful purposes, to recognize individuals who have distinguished themselves in areas related to astronautics, and to provide a program through which the membership can contribute to international endeavours and cooperation in the advancement of aerospace activities. © International Academy of Astronautics (IAA) May 2019. This publication is protected by copyright. The information it contains cannot be reproduced without written authorization. Title: A Handbook for Post-Mission Disposal of Satellites Less Than 100 kg Editors: Darren McKnight and Rei Kawashima International Academy of Astronautics 6 rue Galilée, Po Box 1268-16, 75766 Paris Cedex 16, France www.iaaweb.org ISBN/EAN IAA : 978-2-917761-68-7 Cover Illustration: credit A Handbook for Post-Mission Disposal of Satellites -
Science Exploration and Instrumentation of the OKEANOS Mission to a Jupiter Trojan Asteroid Using the Solar Power Sail
Planetary and Space Science xxx (2018) 1–8 Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss Science exploration and instrumentation of the OKEANOS mission to a Jupiter Trojan asteroid using the solar power sail Tatsuaki Okada a,b,*, Yoko Kebukawa c,d, Jun Aoki d, Jun Matsumoto a, Hajime Yano a, Takahiro Iwata a, Osamu Mori a, Jean-Pierre Bibring e, Stephan Ulamec f, Ralf Jaumann g, Solar Power Sail Science Teama a Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, 252-5210, Japan b The University of Tokyo, Hongo, Bunkyo, Tokyo, Japan c Faculty of Engineering, Yokohama National University, Japan d Graduate School of Science, Osaka University, Toyonaka, Japan e Institut dʼAstrophysique Spatiale, Orsay, France f German Aerospace Center, Cologne, Germany g German Aerospace Center, Berlin, Germany ARTICLE INFO ABSTRACT Keywords: An engineering mission OKEANOS to explore a Jupiter Trojan asteroid, using a Solar Power Sail is currently under Solar system formation study. After a decade-long cruise, it will rendezvous with the target asteroid, conduct global mapping of the Jupiter trojans asteroid from the spacecraft, and in situ measurements on the surface, using a lander. Science goals and enabling Solar power sail instruments of the mission are introduced, as the results of the joint study between the scientists and engineers Lander from Japan and Europe. Mass spectrometry OKEANOS 1. Introduction ocean water and life. Lucy (Levison et al., 2017), a Jupiter Trojan multi-flyby mission, has Jupiter Trojan asteroids are located in the long-term stable orbits been selected as a NASA Discovery class mission, which aims for un- around the Sun-Jupiter Lagrange points (L4 or L5) Most of them are derstanding the variation and diversity of Jupiter Trojans. -
Arcus: the X-Ray Grating Spectrometer Explorer R
Arcus: The X-ray Grating Spectrometer Explorer R. K. Smith*a, M. Abrahamb, R. Allureda, M. Bautzc, J. Bookbinderd, J. Bregmane, L. Brennemana, N. S. Brickhousea, D. Burrowsf, V. Burwitzg, P. N. Cheimetsa, E. Costantinih, S. Dawsonc, C. DeRooa, A. Falconef, A. R. Fostera, L. Galloi, C. E. Grantc, H. M. Güntherc, R. K. Heilmannc, E. Hertza, B. Hined, D. Huenemoerderc, J. S. Kaastrah, I. Kreykenbohmj, K. K. Madsenk, R. McEntafferf, E. Millerc, J. Millere, E. Morsel, R. Mushotzkym, K. Nandrag, M. Nowakc, F. Paerelsn, R. Petreo, K. Poppenhaegerp, A. Ptako, P. Reida, J. Sandersg, M. Schattenburgc, N. Schulzc, A. Smaleo, P. Temid, L. Valencicq, S. Walkerd, R. Willingaler, J. Wilmsj, S. J. Wolka aSmithsonian Astrophysical Observatory, 60 Garden St, Cambridge, MA, US; bThe Aerospace Corp, Pasadena, CA, US, cMassachusetts Institute of Technology, Cambridge, MA, US; dNASA Ames Research Center, Moffet Field, CA US; eUniversity of Michigan, Ann Arbor, MI, US; fThe Pennsylvania State University, University Park, PA, US; gMax-Planck-Institut für extraterrestrische Physik, Garching, DE; hS- RON Netherlands Institute for Space Research, Utrecht, NL; iSaint Mary’s University, Halifax, Canada; jFrie- drich-Alexander-Universitaet, Erlangen-Nürnberg, DE; kCalifornia Institute of Technology, Pasadena, CA, US; lOrbital ATK, Dulles, VA, US; mUniversity of Maryland, College Park, MD, US; nColumbia University, New York, NY, US; oNASA Goddard Space Flight Center, Greenbelt, MD, US, pQueen’s University, Belfast, UK; qJohns Hopkins University, Baltimore, MD, US; rUniversity of Leicester, Leicester, UK 1. ABSTRACT Arcus, a Medium Explorer (MIDEX) mission, was selected by NASA for a Phase A study in August 2017. The observatory provides high-resolution soft X-ray spectroscopy in the 12-50Å bandpass with unprecedent- ed sensitivity: effective areas of >450 cm2 and spectral resolution >2500. -
16Th HEAD Meeting Session Table of Contents
16th HEAD Meeting Sun Valley, Idaho – August, 2017 Meeting Abstracts Session Table of Contents 99 – Public Talk - Revealing the Hidden, High Energy Sun, 204 – Mid-Career Prize Talk - X-ray Winds from Black Rachel Osten Holes, Jon Miller 100 – Solar/Stellar Compact I 205 – ISM & Galaxies 101 – AGN in Dwarf Galaxies 206 – First Results from NICER: X-ray Astrophysics from 102 – High-Energy and Multiwavelength Polarimetry: the International Space Station Current Status and New Frontiers 300 – Black Holes Across the Mass Spectrum 103 – Missions & Instruments Poster Session 301 – The Future of Spectral-Timing of Compact Objects 104 – First Results from NICER: X-ray Astrophysics from 302 – Synergies with the Millihertz Gravitational Wave the International Space Station Poster Session Universe 105 – Galaxy Clusters and Cosmology Poster Session 303 – Dissertation Prize Talk - Stellar Death by Black 106 – AGN Poster Session Hole: How Tidal Disruption Events Unveil the High 107 – ISM & Galaxies Poster Session Energy Universe, Eric Coughlin 108 – Stellar Compact Poster Session 304 – Missions & Instruments 109 – Black Holes, Neutron Stars and ULX Sources Poster 305 – SNR/GRB/Gravitational Waves Session 306 – Cosmic Ray Feedback: From Supernova Remnants 110 – Supernovae and Particle Acceleration Poster Session to Galaxy Clusters 111 – Electromagnetic & Gravitational Transients Poster 307 – Diagnosing Astrophysics of Collisional Plasmas - A Session Joint HEAD/LAD Session 112 – Physics of Hot Plasmas Poster Session 400 – Solar/Stellar Compact II 113 -
Tetsuya Nakano Safety and Mission Assurance Department Japan Aerospace Exploration Agency (JAXA)
JAXA Approach for Mission Success ~close coordination with contractors~ Tetsuya Nakano Safety and Mission Assurance Department Japan Aerospace Exploration Agency (JAXA) 2010.10.21 NASA Supply Chain Conference@NASA GSFC 1 JAXA Approach for Mission Success ~close coordination with contractors~ Contents 1. Recent JAXA Space Flights 2. JAXA’s Role and Responsibility 3. Major S&MA Activities 4. Technical Improvement Activities in Development Projects 2 1. Recent JAXA Space Flights Currently-operating JAXA’s satellites on-orbit CY2000 CY2005 CY2010 2005 Daichi (ALOS: Land observation) 2002 2009 Kodama (DRTS: Data relay) Ibuki(GOSAT: Greenhouse gas observation) 2006 Kiku8 (ETS-8: Technical Testing) 2008 Kizuna(WINDS: Super high-speed internet) 2010 2005 Michibiki (QZSS-1: Suzaku (Astro-EII:X-ray Astronomy) Global Positioning) 2006 2010 Akari (Astro-F: Infrared Akatsuki (Planet-C: Imaging) Venus Climate) 2006 2010 Hinode (SOLAR-B: Ikaros (Solar Power Solar Physics) Sail) 2003 Hayabusa (asteroid explorer) 2007 3 Kaguya (Lunar observation) 1. Recent JAXA Space Flights Japanese Launch vehicles H-2A (Standard) H-2B Epsilon(under development) GTO 4.0ton 8ton LEO 10ton 16.5ton (ISS orbit) 1.2ton 4 4 1. Recent JAXA Space Flights International Space Station Program “HTV” ISS “KIBO” Transportation Vehicle Japanese Experience Module (JEM) ©NASA ©NASA ©NASA Yamazaki 2010.4 Furukawa Noguchi Wakata 2011.Spring - 2009.12 – 2010.6 2009.3 – 2009.7 5 2. JAXA’s Role and Responsibility Emphasizing upstream process and front-loading • Apply Systems Engineering (SE) that emphasizes upstream process management in the project lifecycle • Allocate adequate resource to upstream process (front-loading) Define appropriate level of JAXA responsibilities and roles in development projects • JAXA is responsible for requirements/specification definition, and flight operations. -
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 -
The Future of X-Rayastronomy
The Future of X-rayAstronomy Keith Arnaud [email protected] High Energy Astrophysics Science Archive Research Center University of Maryland College Park and NASA’s Goddard Space Flight Center Themes Politics Efficient high resolution spectroscopy Mirrors Polarimetry Other missions Interferometry Themes Politics Efficient high resolution spectroscopy Mirrors Polarimetry Other missions Interferometry How do we get a new X-ray astronomy experiment? A group of scientists and engineers makes a proposal to a national (or international) space agency. This will include a science case and a description of the technology to be used (which should generally be in a mature state). In principal you can make an unsolicited proposal but in practice space agencies have proposal rounds in the same way that individual missions have observing proposal rounds. NASA : Small Explorer (SMEX) and Medium Explorer (MIDEX): every ~2 years alternating Small and Medium, three selected for study for one year from which one is selected for launch. RXTE, GALEX, NuSTAR, Swift, IXPE Arcus, a high resolution X-ray spectroscopy mission was a finalist in the latest MIDEX round but was not selected. Missions of Opportunity (MO): every ~2 years includes balloon programs, ISS instruments and contributions to foreign missions. Suzaku, Hitomi, NICER, XRISM Large missions such as HST, Chandra, JWST are not selected by such proposals but are decided as national priorities through the Astronomy Decadal process. Every ten years a survey is run by the National Academy of Sciences to decide on priorities for both land-based and space-based astronomy. 1960: HST; 1970: VLA; 1980: VLBA; 1990: Chandra and SIRTF; 2000: JWST and ALMA; 2010 WFIRST and LSST. -
Science Instruments on Hayabusa Follow-On Missions
Science Instruments on Hayabusa follow-on missions Yasuhiko Takagi (Aichi Toho University) (prepared by Masanao Abe (JAXA)) 1 Science instruments under examination Others 2 Basic concept of Hayabusa-IF* camera • Use Navigation camera as a scientific imager • Similar optics and CCD as AMICA, but with minor modifications on – Filters • ECAS -> special set for C-type • Remove ND flter , polarizer on CCD – Electronics • More flexible and autonomous operation • More effective compression • Larger onboard storage • Onboard data analysis 3 *Hayabusa-IF: Hayabusa Immediate Follow-on mission AMICA on Hayabysa Polarizer 4 Ground-based ECAS Quasi ECAS filters on AMICA5 A new filter set • Narrower band width (5~20 nm) – Remove ND filter – More accurate colorimetry • UV absorption as a thermal metamorphism indicator? • Phyllosilicate absorption around 700nm (430nm ?) • Nearby reference bands • Wide filter for imaging stars and the artificial orbiters (~TM) • Natural RGB for outreach purpose? • Several common bands with previous missions? (SSI/Galileo, MSI/NEAR, AMICA/Hayabusa, FC/ Dawn, NAC/Stardust, ??/Rosetta,etc, ) 6 Ground-based ECAS Thermal alteration Phyllosilicate absorption 7 8 Hayabusa NIRS • Wavelength range: 764-2247nm (△λ23.56nm) • FOV: 0.1x0.1deg(9m@5km distance) • Detector: InGaAs Liner Array (64channels) • F value: 1.00 • Effective diameter: 27mm • Operating temperature: 260K • A/D resolution (dynamic range) : 14bits 1 Average 0.1 Output [V] [V] Output Output 0.01 Standard Deviation 0.001 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 9 Wavelength