Review: Far-Infrared Instrumentation and Technology Development for the Next Decade
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IVS NICT-TDC News No.39
ISSN 1882-3432 CONTENTS Proceedings of the 18th NICT TDC Symposium (Kashima, October 1, 2020) KNIFE, Kashima Nobeyama InterFErometer . 3 Makoto Miyoshi Space-Time Measurements Research Inspired by Kashima VLBI Group . 8 Mizuhiko Hosokawa ALMA High Frequency Long Baseline Phase Correction Using Band-to-band ..... 11 (B2B) Phase Referencing Yoshiharu Asaki and Luke T. Maud Development of a 6.5-22.5 GHz Very Wide Band Feed Antenna Using a New ..... 15 Quadruple-Ridged Antenna for the Traditional Radio Telescopes Yutaka Hasegawa*, Yasumasa Yamasaki, Hideo Ogawa, Taiki Kawakami, Yoshi- nori Yonekura, Kimihiro Kimura, Takuya Akahori, Masayuki Ishino, Yuki Kawa- hara Development of Wideband Antenna . 18 Hideki Ujihara Performance Survey of Superconductor Filter Introduced in Wideband Re- ..... 20 ceiver for VGOS of the Ishioka VLBI Station Tomokazu Nakakuki, Haruka Ueshiba, Saho Matsumoto, Yu Takagi, Kyonosuke Hayashi, Toru Yutsudo, Katsuhiro Mori, Tomokazu Kobayashi, and Mamoru Sekido New Calibration Method for a Radiometer Without Using Liquid Nitrogen ..... 23 Cooled Absorber Noriyuki Kawaguchi, Yuichi Chikahiro, Kenichi Harada, and Kensuke Ozeki Comparison of Atmospheric Delay Models (NMF, VMF1, and VMF3) in ..... 27 VLBI analysis Mamoru Sekido and Monia Negusini HINOTORI Status Report . 31 Hiroshi Imai On-the-Fly Interferometer Experiment with the Yamaguchi Interferometer . 34 Kenta Fujisawa, Kotaro Niinuma, Masanori Akimoto, and Hideyuki Kobayashi Superconducting Wide-band BRF for Geodetic VLBI Observation with ..... 36 VGOS Radio Telescope -
Orbital Phase Resolved Spectroscopy of 4U1538-52 with MAXI
Astronomy & Astrophysics manuscript no. jjrr-mif-maxi_rev5 c ESO 2018 September 12, 2018 Orbital phase resolved spectroscopy of 4U1538−52 with MAXI J. J. Rodes-Roca1, 2, 3,,⋆ T. Mihara3, S. Nakahira4, J. M. Torrejón1, 2, Á. Giménez-García1, 2, 5, and G. Bernabéu1, 2 1 Dept. of Physics, Systems Engineering and Sign Theory, University of Alicante, 03080 Ali- cante, Spain e-mail: [email protected] 2 University Institute of Physics Applied to Sciences and Technologies, University of Alicante, 03080 Alicante, Spain 3 MAXI team, Institute of Physical and Chemical Research (RIKEN), 2-1 Hirosawa, Wako, Saitama 351-0198, Japan e-mail: [email protected] 4 ISS Science Project Office, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan 5 School of Physics, Faculty of Science, Monash University, Clayton, Victoria 3800, Australia XX-XX-XX; XX-XX-XX ABSTRACT Context. 4U 1538−52, an absorbed high mass X-ray binary with an orbital period of ∼3.73 days, shows moderate orbital intensity modulations with a low level of counts during the eclipse. Sev- eral models have been proposed to explain the accretion at different orbital phases by a spherically arXiv:1507.04274v2 [astro-ph.HE] 18 Jul 2015 symmetric stellar wind from the companion. Aims. The aim of this work is to study both the light curve and orbital phase spectroscopy of this source in the long term. Particularly, the folded light curve and the changes of the spectral parameters with orbital phase to analyse the stellar wind of QV Nor, the mass donor of this binary system. -
Pushing the Limits of the Coronagraphic Occulters on Hubble Space Telescope/Space Telescope Imaging Spectrograph
Pushing the limits of the coronagraphic occulters on Hubble Space Telescope/Space Telescope Imaging Spectrograph John H. Debes Bin Ren Glenn Schneider John H. Debes, Bin Ren, Glenn Schneider, “Pushing the limits of the coronagraphic occulters on Hubble Space Telescope/Space Telescope Imaging Spectrograph,” J. Astron. Telesc. Instrum. Syst. 5(3), 035003 (2019), doi: 10.1117/1.JATIS.5.3.035003. Downloaded From: https://www.spiedigitallibrary.org/journals/Journal-of-Astronomical-Telescopes,-Instruments,-and-Systems on 02 Jul 2019 Terms of Use: https://www.spiedigitallibrary.org/terms-of-use Journal of Astronomical Telescopes, Instruments, and Systems 5(3), 035003 (Jul–Sep 2019) Pushing the limits of the coronagraphic occulters on Hubble Space Telescope/Space Telescope Imaging Spectrograph John H. Debes,a,* Bin Ren,b,c and Glenn Schneiderd aSpace Telescope Science Institute, AURA for ESA, Baltimore, Maryland, United States bJohns Hopkins University, Department of Physics and Astronomy, Baltimore, Maryland, United States cJohns Hopkins University, Department of Applied Mathematics and Statistics, Baltimore, Maryland, United States dUniversity of Arizona, Steward Observatory and the Department of Astronomy, Tucson Arizona, United States Abstract. The Hubble Space Telescope (HST)/Space Telescope Imaging Spectrograph (STIS) contains the only currently operating coronagraph in space that is not trained on the Sun. In an era of extreme-adaptive- optics-fed coronagraphs, and with the possibility of future space-based coronagraphs, we re-evaluate the con- trast performance of the STIS CCD camera. The 50CORON aperture consists of a series of occulting wedges and bars, including the recently commissioned BAR5 occulter. We discuss the latest procedures in obtaining high-contrast imaging of circumstellar disks and faint point sources with STIS. -
AATSR Frequently Asked Questions (FAQ)
AATSR Frequently Asked Questions (FAQ) Author : IDEAS+ AATSR QC Team (Telespazio VEGA UK) IDEAS+-VEG-OQC-REP-2117 Issue 3 14 December 2016 AATSR Frequently Asked Questions (FAQ) Issue 3 AMENDMENT RECORD SHEET The Amendment Record Sheet below records the history and issue status of this document. ISSUE DATE REASON 1 20 Dec 2005 Initial Issue (as AEP_REP_001) 2 02 Oct 2013 Updated with new questions and information (issued as IDEAS- VEG-OQC-REP-0955) 3 14 Dec 2016 General updates, major edits to Q37., new questions: Q17., Q25., Q26., Q28., Q32., Q38., Q39., Q48. Now issued as IDEAS+-VEG-OQC-REP-2117 TABLE OF CONTENTS 1. INTRODUCTION ........................................................................................................................ 5 1.1 The Third AATSR Reprocessing Dataset (IPF 6.05) ............................................................ 5 1.2 References ............................................................................................................................ 6 2. GENERAL QUESTIONS ........................................................................................................... 7 Q1. What does AATSR stand for? ........................................................................................ 7 Q2. What is AATSR and what does it do? ............................................................................ 7 Q3. What is Envisat? ............................................................................................................. 7 Q4. What orbit does Envisat use? ........................................................................................ -
REVIEW ARTICLE the NASA Spitzer Space Telescope
REVIEW OF SCIENTIFIC INSTRUMENTS 78, 011302 ͑2007͒ REVIEW ARTICLE The NASA Spitzer Space Telescope ͒ R. D. Gehrza Department of Astronomy, School of Physics and Astronomy, 116 Church Street, S.E., University of Minnesota, Minneapolis, Minnesota 55455 ͒ T. L. Roelligb NASA Ames Research Center, MS 245-6, Moffett Field, California 94035-1000 ͒ M. W. Wernerc Jet Propulsion Laboratory, California Institute of Technology, MS 264-767, 4800 Oak Grove Drive, Pasadena, California 91109 ͒ G. G. Faziod Harvard-Smithsonian Center for Astrophysics, 60 Garden Street, Cambridge, Massachusetts 02138 ͒ J. R. Houcke Astronomy Department, Cornell University, Ithaca, New York 14853-6801 ͒ F. J. Lowf Steward Observatory, University of Arizona, 933 North Cherry Avenue, Tucson, Arizona 85721 ͒ G. H. Riekeg Steward Observatory, University of Arizona, 933 North Cherry Avenue, Tucson, Arizona 85721 ͒ ͒ B. T. Soiferh and D. A. Levinei Spitzer Science Center, MC 220-6, California Institute of Technology, 1200 East California Boulevard, Pasadena, California 91125 ͒ E. A. Romanaj Jet Propulsion Laboratory, California Institute of Technology, MS 264-767, 4800 Oak Grove Drive, Pasadena, California 91109 ͑Received 2 June 2006; accepted 17 September 2006; published online 30 January 2007͒ The National Aeronautics and Space Administration’s Spitzer Space Telescope ͑formerly the Space Infrared Telescope Facility͒ is the fourth and final facility in the Great Observatories Program, joining Hubble Space Telescope ͑1990͒, the Compton Gamma-Ray Observatory ͑1991–2000͒, and the Chandra X-Ray Observatory ͑1999͒. Spitzer, with a sensitivity that is almost three orders of magnitude greater than that of any previous ground-based and space-based infrared observatory, is expected to revolutionize our understanding of the creation of the universe, the formation and evolution of primitive galaxies, the origin of stars and planets, and the chemical evolution of the universe. -
JUICE Red Book
ESA/SRE(2014)1 September 2014 JUICE JUpiter ICy moons Explorer Exploring the emergence of habitable worlds around gas giants Definition Study Report European Space Agency 1 This page left intentionally blank 2 Mission Description Jupiter Icy Moons Explorer Key science goals The emergence of habitable worlds around gas giants Characterise Ganymede, Europa and Callisto as planetary objects and potential habitats Explore the Jupiter system as an archetype for gas giants Payload Ten instruments Laser Altimeter Radio Science Experiment Ice Penetrating Radar Visible-Infrared Hyperspectral Imaging Spectrometer Ultraviolet Imaging Spectrograph Imaging System Magnetometer Particle Package Submillimetre Wave Instrument Radio and Plasma Wave Instrument Overall mission profile 06/2022 - Launch by Ariane-5 ECA + EVEE Cruise 01/2030 - Jupiter orbit insertion Jupiter tour Transfer to Callisto (11 months) Europa phase: 2 Europa and 3 Callisto flybys (1 month) Jupiter High Latitude Phase: 9 Callisto flybys (9 months) Transfer to Ganymede (11 months) 09/2032 – Ganymede orbit insertion Ganymede tour Elliptical and high altitude circular phases (5 months) Low altitude (500 km) circular orbit (4 months) 06/2033 – End of nominal mission Spacecraft 3-axis stabilised Power: solar panels: ~900 W HGA: ~3 m, body fixed X and Ka bands Downlink ≥ 1.4 Gbit/day High Δv capability (2700 m/s) Radiation tolerance: 50 krad at equipment level Dry mass: ~1800 kg Ground TM stations ESTRAC network Key mission drivers Radiation tolerance and technology Power budget and solar arrays challenges Mass budget Responsibilities ESA: manufacturing, launch, operations of the spacecraft and data archiving PI Teams: science payload provision, operations, and data analysis 3 Foreword The JUICE (JUpiter ICy moon Explorer) mission, selected by ESA in May 2012 to be the first large mission within the Cosmic Vision Program 2015–2025, will provide the most comprehensive exploration to date of the Jovian system in all its complexity, with particular emphasis on Ganymede as a planetary body and potential habitat. -
Earthcare and Himawari-8 Aerosol Products
EarthCARE and Himawari-8 Aerosol Products Maki Kikuchi, H. Murakami, T. Nagao, M. Yoshida, T. Nio, Riko Oki (JAXA/EORC), M. Eisinger and T. Wehr (ESA/ESTEC), EarthCARE project members and Himawari-8 group members 14th July 2016 Contact: [email protected] EarthCARE Earth Observation Research Center 2 CPR Observation Instruments on EarthCARE MSI CPRCPR Cloud Profiling Radar BBR ATLIDATLID Atmospheric Lidar ATLID Copyright ESA MSIMSI Multi-Spectral Imager European Space Agency(ESA)/National Institute of Institutions Information and Communications Technology(NICT)/ BBRBBR Broadband Radiometer Japan Aerospace Exploration Agency(JAXA) Launch 2018 using Soyuz or Zenit (by ESA) Mission Duration 3-years Mass Approx. 2200kg Sun-synchronous sub-recurrent orbit Orbit Altitude: approx. 400km Mean Local Solar Time (Descending): 14:00 Synergetic Observation by 4 sensors Repeat Cycle 25 days Orbit Period 5552.7 seconds Semi Major Axis 6771.28 km Eccentricity 0.001283 3 Inclination 97.050° 285m Synergetic Observation by 4 Sensors on Global Scale •3‐dimensional structureGlobal simultaneous of aerosol observations and cloud of including vertical motion ‐ Cloud & aerosol profiles, 3D structure, with vertical motions •Radiation flux at top of‐ Radiation atmosphere flux at Top of Atmosphere (TOA) •Aerosol –cloud –radiation‐ Aerosol interactions‐Cloud‐Radiation interaction 4 ATLID ATLID Global Observation of Cloud and Atmospheric Lidar Aerosol Vertical Profile and Optical Properties 355nm High Spectral Resolution Lidar ATLID is a High Spectral Resolution Lidar (HSRL) developed by Instrument (HSRL) European Space Agency. - Rayleigh Channel Channel - Mie Channel(Cross-polarization) Different from the traditional Mie lidar, it has the capability to - Mie Channel (Co-polarization) separate Rayleigh scattering signal (originate from Sampling Horizontal : 285m / Vertical : 103m atmospheric molecules) and Mie scattering signal (originate Observation 3°Off Nadir(TBD) from aerosol and cloud) by high spectral resolution filter. -
Semiconductor Detectors and Focal Plane Arrays for Far-Infrared Imaging
OPTO−ELECTRONICS REVIEW 21(4), 406–426 DOI: 10.2478/s11772−013−0110−x Semiconductor detectors and focal plane arrays for far-infrared imaging A. ROGALSKI* Institute of Applied Physics, Military University of Technology, 2 Kaliskiego Str., 00–908 Warsaw, Poland The detection of far−infrared (far−IR) and sub−mm−wave radiation is resistant to the commonly employed techniques in the neighbouring microwave and IR frequency bands. In this wavelength detection range the use of solid state detectors has been hampered for the reasons of transit time of charge carriers being larger than the time of one oscillation period of radiation. Also the energy of radiation quanta is substantially smaller than the thermal energy at room temperature and even liquid ni− trogen temperature. The realization of terahertz (THz) emitters and receivers is a challenge because the frequencies are too high for conventional electronics and the photon energies are too small for classical optics. Development of semiconductor focal plane arrays started in seventies last century and has revolutionized imaging sys− tems in the next decades. This paper presents progress in far−IR and sub−mm−wave semiconductor detector technology of fo− cal plane arrays during the past twenty years. Special attention is given on recent progress in the detector technologies for real−time uncooled THz focal plane arrays such as Schottky barrier arrays, field−effect transistor detectors, and micro− bolometers. Also cryogenically cooled silicon and germanium extrinsic photoconductor arrays, and semiconductor bolome− ter arrays are considered. Keywords: THz detectors, focal plane arrays, Schottky barrier diodes, semiconductor hot electron bolometers, extrinsic photodetectors, performance limits. -
The Space Infrared Telescope Facility (SIRTF)
header for SPIE use The Space Infrared Telescope Facility (SIRTF) James Fansona, Giovanni Faziob, James Houckc, Tim Kellyd, George Riekee, Domenick Tenerellif, and Milt Whittenf aJet Propulsion Laboratory, California Institute of Technology, Pasadena CA 91109 bSmithsonian Astrophysical Observatory, Cambridge, MA 02138 cCornell University, Ithaca, NY, 14853 dBall Aerospace and Technologies Corp., Boulder, CO 80301 eUniversity of Arizona, Tucson, AZ, 85721 fLockheed Martin Missiles and Space Co., Sunnyvale, CA 94089 ABSTRACT This paper describes the design of the Space Infrared Telescope Facility (SIRTF) as the project enters the detailed design phase. SIRTF is the fourth of NASA’s Great Observatories, and is scheduled for launch in December 2001. SIRTF provides background limited imaging and spectroscopy covering the spectral range from 3 to 180 mm, complementing the capabilities of the other Great Observatories – the Hubble Space Telescope (HST), the Advanced X-ray Astrophysics Facility (AXAF), and the Compton Gamma Ray Observatory (CGRO). SIRTF will be the first mission to combine the high sensitivity achievable from a cryogenic space telescope with the imaging and spectroscopic power of the new generation of infrared detector arrays. The scientific capabilities of this combination are so great that SIRTF was designated the highest priority major mission for all of US astronomy in the 1990s. Keywords: telescope, cryogenic, infrared, astronomy, astrophysics, Great Observatory 1. INTRODUCTION The SIRTF mission has experienced dramatic evolution in both architecture and mission design. Originally conceived as a low Earth orbiting observatory serviced by astronauts from the Space Shuttle, SIRTF passed through a phase in high Earth orbit using first the Titan and later the smaller Atlas launch vehicle, to the current concept of a deep-space mission orbiting the sun, and using the still smaller Delta launch vehicle. -
Cloud Cci ATSR-2 and AATSR Dataset Version 3: a 17-Year Climatology of Global Cloud and Radiation Properties Caroline A
Discussions https://doi.org/10.5194/essd-2019-217 Earth System Preprint. Discussion started: 11 December 2019 Science c Author(s) 2019. CC BY 4.0 License. Open Access Open Data Cloud_cci ATSR-2 and AATSR dataset version 3: a 17-year climatology of global cloud and radiation properties Caroline A. Poulsen1, Gregory R. McGarragh2, Gareth E. Thomas3,6, Martin Stengel4, Matthew W. Christensen5, Adam C. Povey7, Simon R. Proud5,6, Elisa Carboni3,6, Rainer Hollmann4, and Roy G. Grainger7 1Monash University, Melbourne, Australia 2Department of Physics, University of Oxford, Clarendon Laboratory, Parks Road, Oxford OX1 3PU, UK Now at Cooperative Institute for Research in the Atmosphere, Colorado State University 3Science Technology Facility Council, Rutherford Appleton Laboratory, Harwell, Oxfordshire, UK 4Deutscher Wetterdienst, Frankfurter Str. 135, 63067, Offenbach, Germany 5Department of Physics, University of Oxford, Clarendon Laboratory, Parks Road, Oxford OX1 3PU, UK 6National Centre for Earth Observation, Reading RG6 6BB, UK 7National Centre for Earth Observation, Atmospheric, Oceanic and Planetary Physics, University of Oxford, Parks Road, Oxford OX1 3PU, U.K. Correspondence: Caroline Poulsen ([email protected]) Abstract. We present version 3 (V3) of the Cloud_cci ATSR-2/AATSR dataset. The dataset was created for the European Space Agency (ESA) Cloud_cci (Climate Change Initiative) program. The cloud properties were retrieved from the second Along- Track Scanning Radiometer (ATSR-2) on board the second European Remote Sensing Satellite (ERS-2) spanning 1995-2003 and the Advanced ATSR (AATSR) on board Envisat, which spanned 2002-2012. The data comprises a comprehensive set 5 of cloud properties: cloud top height, temperature, pressure, spectral albedo, cloud effective emissivity, effective radius and optical thickness alongside derived liquid and ice water path. -
GLM Product Evaluation and Highlights of My Research at CICS
GLM Product Evaluation and Highlights of My Research at CICS Ryo Yoshida Satellite Program Division, Observation Department Japan Meteorological Agency (JMA) STAR Seminar, October 24, 2019 Overview of my research visit • “Japanese Government Short-Term Overseas Fellowship Program” sponsored by the National Personnel Authority of Japan • Period: Nov. 5, 2018 - Nov. 3, 2019 • NESDIS accepted me at CICS, based on the framework of the NESDIS-JMA high-level letter exchange on information exchange regarding GOES-R Series & Himawari-8/9 • Research topics: GLM & NOAA’s advanced efforts on satellites I deeply appreciate NESDIS’s giving me this great opportunity Japan Meteorological Agency 2 Contents 1. Overview of JMA and Himawari satellites 2. Highlights of my research at CICS 3. GLM product evaluation Japan Meteorological Agency 3 1. Overview of JMA and Himawari satellites Japan Meteorological Agency 4 What JMA is Japan’s national meteorological service, whose ultimate goals are Safety of transportation Prevention Development and mitigation and prosperity of natural of industry disasters International cooperation Japan Meteorological Agency prescribed by the Meteorological Service Act. 5 What JMA does • Weather observations • Weather forecasts and warnings • Aviation & marine weather services • Climate & global environment services • Monitoring seismic & volcanic activity & tsunamis Japan Meteorological Agency 6 JMA’s weather observation systems 16 radiosonde stations 33 wind profilers Upper air observations Geostationary satellites Observations -
FAME-C: Cloud Property Retrieval Using Synergistic AATSR and MERIS Observations
Atmos. Meas. Tech., 7, 3873–3890, 2014 www.atmos-meas-tech.net/7/3873/2014/ doi:10.5194/amt-7-3873-2014 © Author(s) 2014. CC Attribution 3.0 License. FAME-C: cloud property retrieval using synergistic AATSR and MERIS observations C. K. Carbajal Henken, R. Lindstrot, R. Preusker, and J. Fischer Institute for Space Sciences, Freie Universität Berlin (FUB), Berlin, Germany Correspondence to: C. K. Carbajal Henken ([email protected]) Received: 29 April 2014 – Published in Atmos. Meas. Tech. Discuss.: 19 May 2014 Revised: 17 September 2014 – Accepted: 11 October 2014 – Published: 25 November 2014 Abstract. A newly developed daytime cloud property re- trievals. Biases are generally smallest for marine stratocu- trieval algorithm, FAME-C (Freie Universität Berlin AATSR mulus clouds: −0.28, 0.41 µm and −0.18 g m−2 for cloud MERIS Cloud), is presented. Synergistic observations from optical thickness, effective radius and cloud water path, re- the Advanced Along-Track Scanning Radiometer (AATSR) spectively. This is also true for the root-mean-square devia- and the Medium Resolution Imaging Spectrometer (MERIS), tion. Furthermore, both cloud top height products are com- both mounted on the polar-orbiting Environmental Satellite pared to cloud top heights derived from ground-based cloud (Envisat), are used for cloud screening. For cloudy pixels radars located at several Atmospheric Radiation Measure- two main steps are carried out in a sequential form. First, ment (ARM) sites. FAME-C mostly shows an underestima- a cloud optical and microphysical property retrieval is per- tion of cloud top heights when compared to radar observa- formed using an AATSR near-infrared and visible channel.