AKARI in Orbit—Scientific Potential for Understanding Galaxy Evolution
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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 -
JAXA's X-Ray Astronomy Mission ASTRO-H: Launch and First
46th International Conference on Environmental Systems ICES-2016-157 10-14 July 2016, Vienna, Austria JAXA’s X-ray Astronomy Mission ASTRO-H: Launch and First Month’s In-Orbit Thermal Performance Naoko IWATA1 Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210 Tel: +81-50-3362-3592, Fax: +81-42-759-8068 E-mail: [email protected] Takashi USUI2, Akihiko MIKI3, Mizuho IKEDA4 NEC Corporation and Yoh TAKEI5, Atsushi OKAMOTO6, Hiroyuki OGAWA7, Tadayuki TAKAHASHI8 Japan Aerospace Exploration Agency In this study, the thermal performance evaluation results of JAXA’s X-ray astronomy mission ASTRO-H are presented. ASTRO-H was successfully launched on February 17, 2016 from Tanegashima Space Center using an H2A rocket. ASTRO-H houses four telescopes and six detectors. Each detector has its own radiator and heat pipes for heat dissipation. The most major mission will feature a soft X-ray spectrometer having four loop heat pipes (LHPs) for heat transport from two cryocoolers. Six fans have been mounted close to each cryocooler for ground cooling in the fairing just before the launch. Hard X-ray imagers (HXIs) are mounted on an HXI plate; this plate is expanded by 6.4 m via an extensible optical bench (EOB) in orbit to achieve the necessary focal length. The EOB was successfully expanded 11 days after the launch. Heat pipes appropriately functioned in orbit. The two LHPs for the compressors have been operated properly for more than one month Measured inflight temperatures agree well with predicted ones for an attitude condition. Nomenclature -
The AKARI/IRC Mid-Infrared All-Sky Survey*
A&A 514, A1 (2010) Astronomy DOI: 10.1051/0004-6361/200913811 & c ESO 2010 Astrophysics Science with AKARI Special feature The AKARI/IRC mid-infrared all-sky survey D. Ishihara1,2, T. Onaka2, H. Kataza3,A.Salama4, C. Alfageme4,, A. Cassatella4,5,6,N.Cox4,, P. García-Lario4, C. Stephenson4,†,M.Cohen7, N. Fujishiro3,8,‡, H. Fujiwara2, S. Hasegawa3,Y.Ita9,W.Kim3,2,§, H. Matsuhara3, H. Murakami3,T.G.Müller10, T. Nakagawa3, Y. Ohyama11,S.Oyabu3,J.Pyo12,I.Sakon2, H. Shibai13,S.Takita3, T. Tanabé14,K.Uemizu3,M.Ueno3,F.Usui3,T.Wada3, H. Watarai15, I. Yamamura3, and C. Yamauchi3 1 Department of Physics, Nagoya University, Furo-cho, Chikusa-ku, Nagoya, Aichi, 464-860, Japan e-mail: [email protected] 2 Department of Astronomy, Graduate School of Science, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, 113-0033, Japan 3 Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan 4 European Space Astronomy Center (ESAC), Villanueva de la Cañada, PO Box 78, 28691 Madrid, Spain 5 INAF, Istituto di Fisica dello Spazio Interplanetario, via del Fosso del Cavaliere 100, 00133 Roma, Italy 6 Dipartimento di Fisica, Universita’ Roma Tre, via della Vasca Navale 100, 00146 Roma, Italy 7 Radio Astronomy Laboratory, University of California, Berkeley, USA 8 Department of Physics, Faculty of Science, University of Tokyo, 3-1-1 Hongo, Bunkyo-ku, Tokyo, 113-0003, Japan 9 National Astronomical Observatory of Japan, Mitaka, Tokyo, 181-8588, Japan 10 Max-Planck-Institut -
THE ASTRO-D MISSION Y. TANAKA Institute of Space and Astronautical
THE ASTRO-D MISSION Y. TANAKA Institute of Space and Astronautical Science 3-1-1 Yoshinodai, Sagamihara, Kanagawa-ken 229, Japan Abstract. Astro-D, the fourth X-ray astronomy mission of IS AS following Ginga, is a high-throughput imaging and spectroscopic X-ray observatory, scheduled for launch in early 1993. It utilizes multilayer conical X-ray mirrors which provide a large effective area over a wide range energy range up to 12 keV. The focal plane instruments comprize a set of CCD cameras and Imaging gas scintillation proportional counters. Main features of Astro-D are described, and the important astrophysical objectives are discussed. 1. Introduction The Institute of Space and Astronautical Science (ISAS) has launced three X-ray astronomy satellites so far. The first small X-ray astronomy satellite "Hakucho" was launched in 1979. "Tenma", carrying for the first time the large-area gas scintilla tion proportional counters, was launched four years later (1983). The third X-ray astronomy observatory "Ginga" launched in early 1987 carries a large-area (4000 cm2) proportional counter array jointly prepared by the Japanese and the U.K. groups, and is currently operational for its fourth year in orbit. Astro-D is the fourth X-ray astronomy mission of ISAS, following Ginga. Astro- D is designed to be a high-capability X-ray observatory from which a number of important astrophysical investigations can be carried out. The main features of Astro-D are given in Table I, and the schematic view is shown in Fig. 1. It will be equipped with multilayer thin-foil telescopes which provide a large effective area over a wide energy range from below 1 keV up to 12 keV. -
AKARI Observer's Manual for Phase 3
AKARI Observer’s Manual for the Post-Helium (Phase 3) Mission Version 1.1 — for Open Time Observation Planning — AKARI User Support Team in Institute of Space and Astronautical Science / JAXA contact: iris [email protected] European Space Astronomy Centre / ESA contact: http://akari.esac.esa.int/esupport/ June 12, 2008 Revision Record 2008 May 12 Version 1.0 released, adapted from ASTRO-F Observer’s Manual Version 3.2, 2008 June 12 Version 1.1 released. Cookbook section added in Appendix. Contents 1 Introduction 1 1.1Purposeofthisdocument............................... 1 1.2RelevantInformation.................................. 3 2 Mission Overview 5 2.1 The AKARI Mission.................................. 5 2.2 Satellite . ........................................ 6 2.2.1 TheBusModule................................ 6 2.2.2 AttitudeDeterminationandControlSystem................. 7 2.2.3 Cryogenics................................... 8 2.3Telescope........................................ 9 2.3.1 Specification.................................. 9 2.3.2 Capability and Performance in Phase 3 . ................ 10 2.4Focal-PlaneInstruments................................ 11 2.4.1 SpecificationOverview............................. 11 2.4.2 Focal-PlaneLayout............................... 13 2.4.3 TheFocal-PlaneStarSensor(FSTS)..................... 14 2.5 The AKARI ObservationProgrammsinPhase3 .................. 15 2.6References........................................ 16 3 Satellite Operations 17 3.1OrbitandObservingAttitude............................ -
The ASTRO-H X-Ray Astronomy Satellite
The ASTRO-H X-ray Astronomy Satellite Tadayuki Takahashia, Kazuhisa Mitsudaa, Richard Kelleyb, Felix Aharonianc, Hiroki Akamatsud, Fumie Akimotoe, Steve Allenf, Naohisa Anabukig, Lorella Angelinib, Keith Arnaudh, Makoto Asaif, Marc Audardi, Hisamitsu Awakij, Philipp Azzarelloi, Chris Balutaa, Aya Bambak, Nobutaka Bandoa, Marshall Bautzl, Thomas Bialasb, Roger Blandfordf, Kevin Boyceb, Laura Brennemanb, Greg Brownm, Edward Cackettn, Edgar Canavanb, Maria Chernyakovac, Meng Chiaob, Paolo Coppio, Elisa Costantinid, Jelle de Plaad, Jan-Willem den Herderd, Michael DiPirrob, Chris Donep, Tadayasu Dotania, John Dotyq, Ken Ebisawaa, Megan Eckartb, Teruaki Enotor, Yuichiro Ezoes, Andrew Fabiann, Carlo Ferrignoi, Adam Fostert, Ryuichi Fujimotou, Yasushi Fukazawav, Stefan Funkf, Akihiro Furuzawae, Massimiliano Galeazziw, Luigi Gallox, Poshak Gandhip, Kirk Gilmoref, Matteo Guainazziy, Daniel Haasd, Yoshito Habaz, Kenji Hamaguchih, Atsushi Harayamaa, Isamu Hatsukadeaa, Takayuki Hayashia, Katsuhiro Hayashia, Kiyoshi Hayashidag, Junko Hiragaab, Kazuyuki Hirosea, Ann Hornschemeierb, Akio Hoshinoac, John Hughesad, Una Hwangae, Ryo Iizukaa, Yoshiyuki Inouea, Kazunori Ishibashie, Manabu Ishidaa, Kumi Ishikawar, Kosei Ishimuraa, Yoshitaka Ishisakis, Masayuki Itoaf, Naoko Iwataa, Naoko Iyomotoag, Chris Jewellah, Jelle Kaastrad, Timothy Kallmanb, Tuneyoshi Kamaef, Jun Kataokaai, Satoru Katsudaa, Junichiro Katsutav, Madoka Kawaharadaa, Nobuyuki Kawaiaj, Taro Kawanoa, Shigeo Kawasakia, Dmitry Khangulyana, Caroline Kilbourneb, Mark Kimballb, Masashi Kimuraak, -
Japanese X-Ray Satellite Loses Communication with Earth Future of the Major Astronomy Probe Remains Unclear As Pieces of Space Debris Are Reported
NATURE | NEWS Japanese X-ray satellite loses communication with Earth Future of the major astronomy probe remains unclear as pieces of space debris are reported. Alexandra Witze 27 March 2016 The Japan Aerospace Exploration Agency (JAXA) lost contact with its flagship X-ray astronomical satellite, Hitomi, on 26 March. The observatory, launched on 17 February, had been going through initial check-outs and calibrations. Hitomi's status remains unknown as JAXA engineers work to re-establish communication. Ominously, the US Joint Space Operations Center, which tracks space debris, reported spotting five objects in the vicinity of the spacecraft around the time that it went silent. The centre characterized the objects as pieces of a “break-up”. The space debris could consist of minor pieces that were blown off Hitomi, as opposed to indicating complete destruction, says Jonathan McDowell, an astronomer and space analyst at the Harvard–Smithsonian Center for Astrophysics in Cambridge, Massachusetts. Hitomi, which was known before launch as ASTRO-H, is designed to study X-rays streaming from cosmic phenomena such as black holes, galaxy clusters and dark matter. It carries a high-resolution spectrometer to measure X-ray wavelengths in exquisite detail. Earlier versions of the same instrument have twice met a grim fate on JAXA missions: in 2000, the ASTRO-E telescope crashed on launch, and in 2005, a helium leak aboard the Suzaku satellite crippled its spectrometer within weeks of launch. Hope for recovery JAXA lost contact with Hitomi at 4:40 p.m. Japan time on 26 March. “The cause of the communication failure is under investigation,” the agency said. -
The Akari Project: Legacy and Data Processing Status
Publications of the Korean Astronomical Society pISSN 1225-1534 32: 005 ∼ 009, 2017 March eISSN 2287-6936 c 2017. The Korean Astronomical Society. All rights reserved. https://doi.org/10.5303/PKAS.2017.32.1.005 THE AKARI PROJECT: LEGACY AND DATA PROCESSING STATUS Takao Nakagawa & Issei Yamamura1 1Institute of Space and Astronautical Science, JAXA E-mail: [email protected] & [email protected] (Received July 21, 2015; Revised October 27, 2016; Accepted October 27, 2016) ABSTRACT This paper provides an overview of the AKARI mission, which was the first Japanese satellite dedicated to infrared astronomy. The AKARI satellite was launched in 2006, and performed both an all-sky survey and pointed observations during its 550 days in the He-cooled mission phases (Phases 1 and 2). After the He ran out, we continued near-infrared observations with mechanical cryocoolers (Phase 3). Due to a failure of its power supply, AKARI was turned off in 2011. The AKARI data are unique in terms of the observed wavelengths as well as the sky coverage, and provide a unique legacy resource for many astronomical studies. Since April 2013, a dedicated new team has been working to refine the AKARI data processing. The goal of this activity is to provide processed datasets for most of the AKARI observations in a Science Ready form, so that more users can utilize the AKARI data in their astronomical research. The data to be released will include revised All-Sky Point Source Catalogues, All-Sky Image Maps, as well as high-sensitivity images and spectra obtained by pointed observations. -
Hard X-Ray/Soft Gamma-Ray Experiments and Missions
Noname manuscript No. (will be inserted by the editor) Hard X–ray/Soft gamma–ray experiments and missions: overview and prospects Erica Cavallari · Filippo Frontera Received: date / Accepted: date Abstract Starting from 1960s, a great number of missions and experiments have been performed for the study of the high–energy sky. This review gives a wide vision of the most important space missions and balloon experiments that have operated in the 10–600 keV band, a crucial window for the study of the most energetic and violent phenomena in the Universe. Thus it is important to take the stock of the achievements to better establish what we have still to do with future missions in order to progress in this field, to establish which are the technologies required to solve the still open issues and to extend our knowledge of the Universe. Keywords high-energy astrophysics · hard X-ray astronomy · space missions · balloon experiments 1 Introduction It is recognized that hard X–ray/soft gamma–ray astronomy (10–600 keV) is a crucial window for the study of the most energetic and violent events in the Universe. An increasing number of missions devoted to observations in this band or including instruments specifically devoted to perform hard X–ray observations have been performed (e.g., BeppoSAX , Rossi XTE) or are still operational (e.g., INTEGRAL, Swift, Fermi). Actually in the remote past this was only considered an ancillary energy band. The bands which were considered key for astrophysical observations were the 2–10 keV band, also dubbed classic en- ergy band, and the soft X–ray band (≤ 2 keV). -
Hitomi Experience Report: Investigation of Anomalies Affecting the X-Ray Astronomy Satellite “Hitomi” (ASTRO-H)
Hitomi Experience Report: Investigation of Anomalies Affecting the X-ray Astronomy Satellite “Hitomi” (ASTRO-H) June 8, 2016 JAXA All times are given in JST unless stated otherwise. 1 Agenda 1. Summary 2. Background information on ASTRO‐H 3. Anomaly description and ground‐based observations 4. Causes of the anomaly 5. Factors contributing to the anomaly (Updated in the last ver.) 6. Measures and reforms (Updated in the last ver.) 7. Summary (Added in this slide deck) 2 1. SUMMARY 3 1. Summary After the anomaly in communications with the X‐ray Astronomy Satellite “Hitomi” (ASTRO‐H), the Japan Aerospace Exploration Agency (JAXA) set up an emergency headquarters to perform investigations and consider measures for future operations. For the cause analysis, experts from every branch of JAXA collaborated in the investigations such as analysis of telemetry data sent from the satellite, simulations, examination of the design, and analysis of the ground test data. In addition, the private enterprises that developed the satellite with JAXA also helped with the investigations. JAXA have been inspecting the direct causes and extending the investigation to trace back to the design policy and process in order to determine the design of the spacecraft. In Chapter 2 and later, JAXA reports the current status of the investigation. 4 2. BACKGROUND INFORMATION ON ASTRO‐H 5 2.1 Mission Overview ASTRO-H was developed to reveal the structure and evolution of the universe by observing high-energy objects that are visible in the X-ray and gamma-ray bands, objects such as black holes, supernova remnants (SNRs), and galaxy clusters. -
Astronomy Satellites
Astronomy Satellites Jonathan McDowell June 28, 1994 1 Why Space Astronomy? • SHARPER PICTURES (Spatial Resolution) The Earth’s atmosphere messes up the light coming in (stars twinkle, etc). • TECHNICOLOR (X-ray, infrared, etc) The atmosphere also absorbs light of different wavelengths (col- ors) outside the visible range. X-ray astronomy is impossible from the Earth’s surface. 2 What are the differences between satellite instruments? • Focussing optics or bare detectors • Wavelength or energy range - IR, UV, etc. Different technology used for different wavebands. • Spatial Resolution (how sharp a picture?) • Spatial Field of View (how large a piece of sky?) • Spectral Resolution (can it tell photons of different energies apart?) • Spectral Field of View (bandwidth) • Sensitivity • Pointing Accuracy • Lifetime • Orbit (hence operating efficiency, background, etc.) • Scan or Point What are the differences between satellites? • Spinning or 3-axis pointing (older satellites spun around a fixed axis, precession let them eventually see different parts of the sky) • Fixed or movable solar arrays (fixed arrays mean the spacecraft has to point near the plane perpendicular to the solar-satellite vector) 3 • Low or high orbit (low orbit has higher radiation, atmospheric drag, and more Earth occultation; high orbit has slower preces- sion and no refurbishment opportunity) • Propulsion to raise orbit? • Other consumables (proportional counter gas, attitude control gas, liquid helium coolant) 4 What are the differences in operation? • PI mission vs. GO mission PI = Principal Investigator. One of the people responsible for building the satellite. Nowadays often referred to as IPIs (In- strument PIs). GO = Guest Observer. Someone who just want to use the satel- lite. -
X‐Ray Astronomy Recovery Mission XARM
XARM X‐ray Astronomy Recovery Mission XARM Makoto S. Tashiro (ISAS/JAXA, Saitama Univ.) Rechard L. Kelley (NASA/GSFC) on behalf of XARM pre‐project preparation team at the X‐ray Universe 2017 on June 8, 2017 @ Rome 1 XARMASTRO‐H “Hitomi” Launched on 17 Feb. 2016 2 XARM Hitomi Science Results • The Soft X‐ray Spectrometer (SXS) aboard Hitomi provided spectrometry performance far exceeding requirements. • X‐ray micro‐calorimter is a powerful tool to measure plasma velocity fields, as well as to observe fine structures of lines. See papers in this symposium by: Noda, Ohashi, Gu, Sato, Nakashima, Ichinohe Hitomi collaboration, 2016, Nature, 535, 117 Unmoving gas Fig. 2 from the paper Fig. 3 from the paper Thermal movement of ionized iron (80 km/s) Thermal movement (80 km/s) + movement due to gas turbulence (164 km/s) Chandra satellite image and the detector field of view X‐ray energy (keV) 3 XARM The X-ray micro-calorimeter (ASTRO-E XRS Suzaku XRS ASTRO-H SXS/XARM Resolve Athena X-IFU) ASTRO-E Suzaku A-H/XARM Athena ASTRO-H XRS* XRS SXS/Resolve X-IFU SXI (CCD) Launch year 2000* 2005 2016/2021 2028 2016 Energy resolution 12 eV* 7 eV 5 eV/<7 eV 2.5 eV 150 eV (FWHM at 6 keV) TES Energy range 0.4-10 keV 0.3-12 keV 0.3-12 keV 0.2-12 0.4 – 13 keV keV Pixel format 2 x 16 6 x 6 6 x 6 3840 1280 x 1280 Cooing system ADR/ L-He/ S-Ne ADR/ L-He/ ADR/JT/ 1ST ADR+cryogen JT/ 2ST PT/2ST mech.