James Webb Space Telescope Is Expected to Have As Profound and Far-Reaching an Impact on Astrophysics As Did Its Famous Predecessor
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Nircam Optical Analysis
NIRCam Optical Analysis Yalan Mao, Lynn W. Huff and Zachary A. Granger Lockheed Martin Advanced Technology Center, 3251 Hanover St., Palo Alto, CA 94304 ABSTRACT The Near Infrared Camera (NIRCam) instrument for NASA’s James Webb Space Telescope (JWST) is one of the four science instruments to be installed into the Integrated Science Instrument Module (ISIM) on JWST. NIRCam’s requirements include operation at 37 Kelvin to produce high-resolution images in two wave bands encompassing the range from 0.6 microns to 5 microns. In addition, NIRCam is to be used as a metrology instrument during the JWST observatory commissioning on orbit, during the precise alignment of the observatory’s multiple-segment primary mirror. This paper will present the optical analyses performed in the development of the NIRCam optical system. The Compound Reflectance concept to specify coating on optics for ghost image reduction is introduced in this paper. Key words: NIRCam, JWST, Compound Reflectance, Optical analysis, ghost image 1. INTRODUCTION NIRCam is a science instrument that will make up part of the science instrument complement of the James Webb Space Telescope (JWST). The JWST will possess a large aperture of 6.5m with several times the collecting area of the Hubble Space Telescope. JWST will have a broadband IR capability that, from the vicinity of Lagrange 2 (nine hundred thousand km from earth), will allow a view into the distant history of galaxy formation. The instrument will be required to furnish high-quality infrared imaging performance while operating in a challenging cryogenic (32 - 37 Kelvin) space environment over a minimum 5-year (10 year goal) mission. -
Status of the James Webb Space Telescope Integrated Science Instrument Module System
The 2010 STScI Calibration Workshop Space Telescope Science Institute, 2010 Susana Deustua and Cristina Oliveira, eds. Status of the James Webb Space Telescope Integrated Science Instrument Module System Matthew A. Greenhouse*, Michael P. Drury, Jamie L. Dunn, Stuart D. Glazer, Ed Greville, Gregory Henegar, Eric L. Johnson, Ray Lundquist, John C. McCloskey, Raymond G. Ohl IV, Robert A. Rashford, and Mark F. Voyton Goddard Space Flight Center, Greenbelt, MD 20771 Abstract. The Integrated Science Instrument Module (ISIM) of the JamesWebbSpace Telescope (JWST) is discussed from a systems perspective with emphasis on devel- opment status and advanced technology aspects. The ISIM is one of three elements that comprise the JWST space vehicle and is the science instrument payload of the JWST. The major subsystems of this flight element and theirbuildstatusare described. 1. Introduction The James Webb Space Telescope (Figure 1) is under development by NASA for launch during 2014 with major contributions from the European and Canadian Space Agencies. The JWST mission is designed to enable a wide range of science investigations across four broad themes: (1) observation of the first luminous objects after the Big Bang, (2) the evolution of galaxies, (3) the birth of stars and planetary systems, and (4) the formation of planets and the origins of life [1],[2],[3]. Integrated Science Instrument Module (ISIM) is the science payload of the JWST [4],[5],[6]. Along with the telescope and spacecraft, the ISIM is one of three elements that comprise the JWST space vehicle. At 1.4 mT, it makes up approximately 20% of both the observatory mass and cost to launch. -
New Constraints on the Membership of the T Dwarf S Ori 70 in the Σ Orionis Cluster
A&A 477, 895–900 (2008) Astronomy DOI: 10.1051/0004-6361:20078600 & c ESO 2008 Astrophysics New constraints on the membership of the T dwarf S Ori 70 in the σ Orionis cluster M. R. Zapatero Osorio1,V.J.S.Béjar1,G.Bihain1,2, E. L. Martín1,3,R.Rebolo1,2, I. Villó-Pérez4, A. Díaz-Sánchez5, A. Pérez Garrido5, J. A. Caballero6, T. Henning6, R. Mundt6, D. Barrado y Navascués7, and C. A. L. Bailer-Jones6 1 Instituto de Astrofísica de Canarias, 38200 La Laguna, Tenerife, Spain e-mail: [email protected] 2 Consejo Superior de Investigaciones Científicas, Spain 3 University of Central Florida, Department of Physics, PO Box 162385, Orlando, FL 32816, USA 4 Departamento de Electrónica, Universidad Politécnica de Cartagena, 30202 Cartagena, Spain 5 Departamento de Física Aplicada, Universidad Politécnica de Cartagena, 30202 Cartagena, Spain 6 Max-Planck Institut für Astronomie, Königstuhl 17, 69117 Heidelberg, Germany 7 LAEFF-INTA, PO 50727, 28080 Madrid, Spain Received 2 September 2007 / Accepted 10 October 2007 ABSTRACT Aims. The nature of S Ori 70 (S Ori J053810.1−023626), a faint mid-T type object found towards the direction of the young σ Orionis cluster, is still under debate. We intend to find out whether it is a field brown dwarf or a 3-Myr old planetary-mass member of the cluster. Methods. We report on near-infrared JHKs and mid-infrared [3.6] and [4.5] IRAC/Spitzer photometry recently obtained for S Ori 70. The new near-infrared images (taken 3.82 yr after the discovery data) allowed us to derive the first proper motion measurement for this object. -
Nircam: Development and Testing of the JWST Near-Infrared Camera
NIRCam: Development and Testing of the JWST Near-Infrared Camera Thomas Greenea, Charles Beichmanb, Michael Gully-Santiagoc,DanielJaffec, Douglas Kellyd, John Kriste,MarciaRieked, and Eric H. Smithf aNASA’s Ames Research Center, MS 245-6, Moffett Field, CA, USA; bNExScI, Caltech 100-22, Pasadena, CA, USA; cUniversity of Texas Department of Astronomy, Austin, TX, USA; dSteward Observatory, University of Arizona, Tucson, AZ, USA; eJet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA, USA; fLockheed Martin Advanced Technology Ctr., 3251 Hanover St., Palo Alto, CA USA ABSTRACT The Near Infrared Camera (NIRCam) is one of the four science instruments of the James Webb Space Telescope (JWST). Its high sensitivity, high spatial resolution images over the 0.6 − 5 μm wavelength region will be essential for making significant findings in many science areas as well as for aligning the JWST primary mirror segments and telescope. The NIRCam engineering test unit was recently assembled and has undergone successful cryogenic testing. The NIRCam collimator and camera optics and their mountings are also progressing, with a brass-board system demonstrating relatively low wavefront error across a wide field of view. The flight model’s long-wavelength Si grisms have been fabricated, and its coronagraph masks are now being made. Both the short (0.6 − 2.3 μm) and long (2.4 − 5.0 μm) wavelength flight detectors show good performance and are undergoing final assembly and testing. The flight model subsystems should all be completed later this year through early 2011, and NIRCam will be cryogenically tested in the first half of 2011 before delivery to the JWST integrated science instrument module (ISIM). -
Euclid: Superluminous Supernovae in the Deep Survey? C
A&A 609, A83 (2018) Astronomy DOI: 10.1051/0004-6361/201731758 & c ESO 2018 Astrophysics Euclid: Superluminous supernovae in the Deep Survey? C. Inserra1; 2, R. C. Nichol3, D. Scovacricchi3, J. Amiaux4, M. Brescia5, C. Burigana6; 7; 8, E. Cappellaro9, C. S. Carvalho30, S. Cavuoti5; 11; 12, V. Conforti13, J.-C. Cuillandre4; 14; 15, A. da Silva10; 16, A. De Rosa13, M. Della Valle5; 17, J. Dinis10; 16, E. Franceschi13, I. Hook18, P. Hudelot19, K. Jahnke20, T. Kitching21, H. Kurki-Suonio22, I. Lloro23, G. Longo11; 12, E. Maiorano13, M. Maris24, J. D. Rhodes25, R. Scaramella26, S. J. Smartt2, M. Sullivan1, C. Tao27; 28, R. Toledo-Moreo29, I. Tereno16; 30, M. Trifoglio13, and L. Valenziano13 (Affiliations can be found after the references) Received 11 August 2017 / Accepted 3 October 2017 ABSTRACT Context. In the last decade, astronomers have found a new type of supernova called superluminous supernovae (SLSNe) due to their high peak luminosity and long light-curves. These hydrogen-free explosions (SLSNe-I) can be seen to z ∼ 4 and therefore, offer the possibility of probing the distant Universe. Aims. We aim to investigate the possibility of detecting SLSNe-I using ESA’s Euclid satellite, scheduled for launch in 2020. In particular, we study the Euclid Deep Survey (EDS) which will provide a unique combination of area, depth and cadence over the mission. Methods. We estimated the redshift distribution of Euclid SLSNe-I using the latest information on their rates and spectral energy distribution, as well as known Euclid instrument and survey parameters, including the cadence and depth of the EDS. -
Report by the ESA–ESO Working Group on Extra-Solar Planets
Report by the ESA–ESO Working Group on Extra-Solar Planets 4 March 2005 Summary Various techniques are being used to search for extra-solar planetary signatures, including accurate measurement of radial velocity and positional (astrometric) dis- placements, gravitational microlensing, and photometric transits. Planned space experiments promise a considerable increase in the detections and statistical know- ledge arising especially from transit and astrometric measurements over the years 2005–15, with some hundreds of terrestrial-type planets expected from transit mea- surements, and many thousands of Jupiter-mass planets expected from astrometric measurements. Beyond 2015, very ambitious space (Darwin/TPF) and ground (OWL) experiments are targeting direct detection of nearby Earth-mass planets in the habitable zone and the measurement of their spectral characteristics. Beyond these, ‘Life Finder’ (aiming to produce confirmatory evidence of the presence of life) and ‘Earth Imager’ (some massive interferometric array providing resolved images of a distant Earth) arXiv:astro-ph/0506163v1 8 Jun 2005 appear as distant visions. This report, to ESA and ESO, summarises the direction of exo-planet research that can be expected over the next 10 years or so, identifies the roles of the major facilities of the two organisations in the field, and concludes with some recommendations which may assist development of the field. The report has been compiled by the Working Group members and experts (page iii) over the period June–December 2004. Introduction & Background Following an agreement to cooperate on science planning issues, the executives of the European Southern Observatory (ESO) and the European Space Agency (ESA) Science Programme and representatives of their science advisory structures have met to share information and to identify potential synergies within their future projects. -
ARIEL – 13Th Appleton Space Conference PLANETS ARE UBIQUITOUS
Background image credit NASA ARIEL – 13th Appleton Space Conference PLANETS ARE UBIQUITOUS OUR GALAXY IS MADE OF GAS, STARS & PLANETS There are at least as many planets as stars Cassan et al, 2012; Batalha et al., 2015; ARIEL – 13th Appleton Space Conference 2 EXOPLANETS TODAY: HUGE DIVERSITY 3700+ PLANETS, 2700 PLANETARY SYSTEMS KNOWN IN OUR GALAXY ARIEL – 13th Appleton Space Conference 3 HUGE DIVERSITY: WHY? FORMATION & EVOLUTION PROCESSES? MIGRATION? INTERACTION WITH STAR? Accretion Gaseous planets form here Interaction with star Planet migration Ices, dust, gas ARIEL – 13th Appleton Space Conference 4 STAR & PLANET FORMATION/EVOLUTION WHAT WE KNOW: CONSTRAINTS FROM OBSERVATIONS – HERSCHEL, ALMA, SOLAR SYSTEM Measured elements in Solar system ? Image credit ESA-Herschel, ALMA (ESO/NAOJ/NRAO), Marty et al, 2016; André, 2012; ARIEL – 13th Appleton Space Conference 5 THE SUN’S PLANETS ARE COLD SOME KEY O, C, N, S MOLECULES ARE NOT IN GAS FORM T ~ 150 K Image credit NASA Juno mission, NASA Galileo ARIEL – 13th Appleton Space Conference 6 WARM/HOT EXOPLANETS O, C, N, S (TI, VO, SI) MOLECULES ARE IN GAS FORM Atmospheric pressure 0.01Bar H2O gas CO2 gas CO gas CH4 gas HCN gas TiO gas T ~ 500-2500 K Condensates VO gas H2S gas 1 Bar Gases from interior ARIEL – 13th Appleton Space Conference 7 CHEMICAL MEASUREMENTS TODAY SPECTROSCOPIC OBSERVATIONS WITH CURRENT INSTRUMENTS (HUBBLE, SPITZER,SPHERE,GPI) • Precision of 20 ppm can be reached today by Hubble-WFC3 • Current data are sparse, instruments not absolutely calibrated • ~ 40 planets analysed -
The Mid-Infrared Instrument for JWST I
When there is a discrepancy between the information in this technical report and information in JDox, assume JDox is correct. The Mid-Infrared Instrument for the James Webb Space Telescope, I: Introduction G. H. Rieke1,G.S.Wright2,T.B¨oker3,J.Bouwman4, L. Colina5, Alistair Glasse2,K.D. Gordon6,7,T.P.Greene8,ManuelG¨udel9,10, Th. Henning4,K.Justtanont11,P.-O. Lagage12,M.E.Meixner6,13, H.-U. Nørgaard-Nielsen14,T.P.Ray15,M.E.Ressler16,E.F. van Dishoeck17,&C.Waelkens18. –2– ABSTRACT MIRI (the Mid-Infrared Instrument for the James Webb Space Telescope (JWST)) operates from 5 to 28.5 μm and combines over this range: 1.) unprece- dented sensitivity levels; 2.) sub-arcsec angular resolution; 3.) freedom from atmospheric interference; 4.) the inherent stability of observing in space; and 1Steward Observatory, 933 N. Cherry Ave, University of Arizona, Tucson, AZ 85721, USA 2UK Astronomy Technology Centre, Royal Observatory, Edinburgh, Blackford Hill, Edinburgh EH9 3HJ, UK 3European Space Agency, c/o STScI, 3700 San Martin Drive, Batimore, MD 21218, USA 4Max-Planck-Institut f¨ur Astronomie, K¨onigstuhl 17, D-69117 Heidelberg, Germany 5Centro de Astrobiolog´ıa (INTA-CSIC), Dpto Astrof´ısica, Carretera de Ajalvir, km 4, 28850 Torrej´on de Ardoz, Madrid, Spain 6Space Telescope Science Institute, 3700 San Martin Drive, Baltimore, MD 21218, USA 7Sterrenkundig Observatorium, Universiteit Gent, Gent, Belgium 8Ames Research Center, M.S. 245-6, Moffett Field, CA 94035, USA 9Dept. of Astrophysics, Univ. of Vienna, T¨urkenschanzstr 17, A-1180 Vienna, Austria 10ETH Zurich, Institute for Astronomy, Wolfgang-Pauli-Str. 27, CH-8093 Zurich, Switzerland 11Chalmers University of Technology, Onsala Space Observatory, S-439 92 Onsala, Sweden 12Laboratoire AIM Paris-Saclay, CEA-IRFU/SAp, CNRS, Universit´e Paris Diderot, F-91191 Gif-sur- Yvette, France 13The Johns Hopkins University, Department of Physics and Astronomy, 366 Bloomberg Center, 3400 N. -
Stsci Newsletter: 2011 Volume 028 Issue 02
National Aeronautics and Space Administration Interacting Galaxies UGC 1810 and UGC 1813 Credit: NASA, ESA, and the Hubble Heritage Team (STScI/AURA) 2011 VOL 28 ISSUE 02 NEWSLETTER Space Telescope Science Institute We received a total of 1,007 proposals, after accounting for duplications Hubble Cycle 19 and withdrawals. Review process Proposal Selection Members of the international astronomical community review Hubble propos- als. Grouped in panels organized by science category, each panel has one or more “mirror” panels to enable transfer of proposals in order to avoid conflicts. In Cycle 19, the panels were divided into the categories of Planets, Stars, Stellar Rachel Somerville, [email protected], Claus Leitherer, [email protected], & Brett Populations and Interstellar Medium (ISM), Galaxies, Active Galactic Nuclei and Blacker, [email protected] the Inter-Galactic Medium (AGN/IGM), and Cosmology, for a total of 14 panels. One of these panels reviewed Regular Guest Observer, Archival, Theory, and Chronology SNAP proposals. The panel chairs also serve as members of the Time Allocation Committee hen the Cycle 19 Call for Proposals was released in December 2010, (TAC), which reviews Large and Archival Legacy proposals. In addition, there Hubble had already seen a full cycle of operation with the newly are three at-large TAC members, whose broad expertise allows them to review installed and repaired instruments calibrated and characterized. W proposals as needed, and to advise panels if the panelists feel they do not have The Advanced Camera for Surveys (ACS), Cosmic Origins Spectrograph (COS), the expertise to review a certain proposal. Fine Guidance Sensor (FGS), Space Telescope Imaging Spectrograph (STIS), and The process of selecting the panelists begins with the selection of the TAC Chair, Wide Field Camera 3 (WFC3) were all close to nominal operation and were avail- about six months prior to the proposal deadline. -
Cosmic Evolution Through Uv Surveys (Cetus) Final Report
COSMIC EVOLUTION THROUGH UV SURVEYS (CETUS) FINAL REPORT Thematic Activity: Project (probe mission concept) Program: Electromagnetic observations from space Authors of Final Report: Jonathan Arenberg, Northrop Grumman Corporation Sally Heap, Univ. of Maryland, [email protected] Tony Hull, Univ. of New Mexico Steve Kendrick, Kendrick Aerospace Consulting LLC Bob Woodruff, Woodruff Consulting Scientific Contributors: Maarten Baes, Rachel Bezanson, Luciana Bianchi, David Bowen, Brad Cenko, Yi-Kuan Chiang, Rachel Cochrane, Mike Corcoran, Paul Crowther, Simon Driver, Bill Danchi, Eli Dwek, Brian Fleming, Kevin France, Pradip Gatkine, Suvi Gezari, Lea Hagen, Chris Hayward, Matthew Hayes, Tim Heckman, Edmund Hodges-Kluck, Alexander Kutyrev, Thierry Lanz, John MacKenty, Steve McCandliss, Harvey Moseley, Coralie Neiner, Goren Östlin, Camilla Pacifici, Marc Rafelski, Bernie Rauscher, Jane Rigby, Ian Roederer, David Spergel, Dan Stark, Alexander Szalay, Bryan Terrazas, Jonathan Trump, Arjun van der Wel, Sylvain Veilleux, Kate Whitaker, Isak Wold, Rosemary Wyse Technical Contributors: Jim Burge, Kelly Dodson, Chip Eckles, Brian Fleming, Jamie Kennea, Gerry Lemson, John MacKenty, Steve McCandliss, Greg Mehle, Shouleh Nikzad, Trent Newswander, Lloyd Purves, Manuel Quijada, Ossy Siegmund, Dave Sheikh, Phil Stahl, Ani Thakar, John Vallerga, Marty Valente, the Goddard IDC/MDL. September 2019 Cosmic Evolution Through UV Surveys (CETUS) TABLE OF CONTENTS INTRODUCTION TO CETUS ................................................................................................................ -
The Sic Primary Mirror of the EUCLID Telescope
ICSO 2016 Biarritz, France International Conference on Space Optics 18 - 21 October 2016 The SiC Primary Mirror of the EUCLID Telescope Michel Bougoin1, Jérôme Lavenac1, Alexandre Gerbert-Gaillard2, Dominique Pierot2, 1MERSEN BOOSTEC, France, 2AIRBUS DEFENCE & SPACE, France I. INTRODUCTION Euclid is a part of the European Space Agency Cosmic Vision program. Euclid mission’s goal is to understand the origin of the accelerating expansion of the Universe. This space mission will embark a large Korsch telescope, a visible imager (VIS) and a near-infrared spectrometer and photometer (NISP). The hardware of all of them will be mainly made of Boostec® SiC material. The SiC telescope has been designed by AIRBUS Defence & Space team in Toulouse (France). Its primary mirror (M1) has been highly optimized for purpose of mass and WFE reduction. It features i) a Ø 1.25 m circular outer contour, ii) a Ø 0.37 m decentered circular inner hole, iii) a on-axis concave optical face, iv) three outer pads to be bolted on the isostatic mounts, v) a mass of only 38 kg and vi) a first eigen frequency of 140 Hz. In addition to the possibility of high mass reduction, the Boostec® SiC has been chosen for its mechanical and thermal properties at cool down operating temperature (125K). The full SiC telescope architecture gives high optical stability; having SiC mirrors and structure enables a good in-orbit behavior prediction of the instruments performance. The present paper describes the ready-to-polish M1 Flight Model blank and its manufacturing process. It has been manufactured monolithic (without any assembly); its optical face has been coated with a thin layer of non-porous and easily polish-able SiC layer obtained by MERSEN Chemical Vapor Deposition. -
NIRISS René Doyon, Université De Montréal, FGS/NIRISS PI
Transit Spectroscopy with NIRISS René Doyon, Université de Montréal, FGS/NIRISS PI ExoPAG 9 4 Jan 2014! 1 Collaborators •" David Lafrenière, UdeM (NIRISS exoplanet team lead) •" Loic Abert, UdeM •" Etienne Artigau, UdeM •" Mike Meyer, ETH, Switzerland •" Ray Jayawardhana, Toronto •" …. ExoPAG 9 4 Jan 2014! 2 Outline •" NIRISS overview •" Transit spectroscopy capability •" Simulations •" Performance limitations ExoPAG 9 4 Jan 2014! 3 FGS/NIRISS overview •" Two instruments in one box provided by CSA •" FGS (Fine Guidance Sensor) •" Provides fine guiding to the observatory •" 0.6-5 µm IR camera. No filters, single optical train with two redundant detectors each with a FOV of 2.3’x2.3’ •" Noise equivalent angle (one axis): 3.5 milliarcsec •" 95% sky coverage down to JAB=19.5 •" NIRISS (Near-Infrared Imager and Slitless Spectrograph) •" 0.7-5 µm IR camera. •" Four observing modes •" Main science drivers •" First Light: high-z galaxies •" Exoplanet detection and characterization ExoPAG 9 4 Jan 2014! ExoPAG 9 4 Jan 2014! 5 ExoPAG 9 4 Jan 2014! 6 ExoPAG 9 4 Jan 2014! 7 NIRISS SOSS (Single-Object Slitless Spectroscopy) mode •" Specifically optimized for transit spectroscopy •" Unique features •" Broad simultaneous wavelength range: 0.7-2.5 um •" Built-in weak lens to increase dynamic range and minimize systematic ‘’red noise’’ due to undersampling and flatfield errors. •" Key component is a directly ruled ZnSe grism (manufactured by Bach) combined with a ZnS prism, all AR coated except the ruled surface on the ZnSe grism. •" Two spares were manufactured by LLNL and received October 2012 (after instrument delivery in July 2012) •" Groove quality much better/sharper compared to the flight grism.