A Glance at the Host Galaxy of High-Redshift Quasars Using Strong Damped Lyman-Α Systems As Coronagraphs
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Nancy Grace Roman Telescope Sell Sheet
NANCY GRACE ROMAN SPACE TELESCOPE The Nancy Grace Roman Space Telescope is designed to provide data that might settle some of the most enduring mysteries of the universe – dark energy, dark matter, exoplanets and undiscovered galaxies. ROMAN SPACE TELESCOPE MISSION L3HARRIS’ ROLE ROMAN DETAILS When it launches in the mid-2020s on a L3Harris is responsible for some of the > Mission duration is approximately mission planned for five years, Roman most important tasks to create the tele- five years will survey wide areas of space with a scope, including refinishing the primary > Expected launch in the mid-2020s field of view much larger than the Hubble mirror. L3Harris is creating hardware Space Telescope or the James Webb to accommodate and interact with the > Primary mirror diameter Space Telescope. Those predecessors two instruments on the telescope, the 2.4 meters take detailed views of smaller areas of Wide Field Instrument for the mission’s > Two main instruments – Wide Field space, more like a zoomed-in view to core science goals and the Coronagraph Instrument for scientific discovery Roman’s panoramic. Instrument for future exoplanet direct- and Coronagraph Instrument to Roman will observe billions of galaxies, imaging technology development. demonstrate advanced technology detailing supernovae and other cosmic L3Harris also conducted the successful > Areas of study include dark phenomena. The data will fuel discoveries test of the primary mirror to ensure it energy, dark matter, exoplanets on dark energy and dark matter, two functions in the very cold temperatures and new galaxies mysteries of the universe that science found in space. cannot fully explain. -
SGL Coronagraph Simulation
SGL Coronagraph Simulation Hanying Zhou Jet Propulsion Laboratory/California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109 USA © 2018. California Institute of Technology. Government Sponsorship Acknowledged SGL Coronagraph • Typical exoplanet coronagraphs: Solar corona brightness . Light contamination from the unresolved, close (Lang, K.R., 2010). parent star is the limiting factor: 0.1” Earth sized: ~1e-10; 0.5” Jupiter sized:~ 1e-9 • In SGL: . Light from the parent star focused ~1e3 km away from the imaging telescope . The Sun is an extended source (Rʘ: 1~2 arcsec) . The Einstein ring overlaps w/ the solar corona The Sun light need only to be sufficiently suppressed (to < solar corona level) at the given Einstein’s ring location: ~a few e-7, notionally ~ approx. Einstein’s ring location ~ original “coronagraph” in solar astronomy (Sun angular radius size: Rʘ ~960 arcsec) Technology Requirements to Operate at and Utilize the Solar Gravity Lens for Exoplanet Imaging, 05/16/2018 2 KISS Workshop, May 15-18, Pasadena SGL Coronagraph Simulation General Setup • Classic Lyot coronagraph architecture . Occulter mask:remove central part of PSF Amplitude . Lyot stop: further remove residual part at pupil edge only . Extended source model . The Sun disk: a collection of incoherent off-axis point sources, of uniform brightness . Solar corona: ~1e-6/r^3 power law radial profile brightness (r/Rʘ >=1) . Instrument parameters considered: . Telescope diam, SGL distance, occulter mask profile, Lyot mask size • Fourier based diffraction -
Preliminary Analysis of Effect of Random Segment Errors on Coronagraph Performance
Preliminary analysis of effect of random segment errors on coronagraph performance Mark T. Stahl, H. Philip Stahl, NASA Marshall Space Flight Ctr. Stuart B. Shaklan, Jet Propulsion Laboratory California Institute of Technology SPIE Conference on Detection and Characterization of Exoplanets, 2015 Executive Summary • Telescope manufacturers need a Wavefront Error (WFE) Stability Specification derived from science requirements. Wavefront Change per Time • Develops methodology for deriving Specification. • Develop modeling tool to explore effects of segmented aperture telescope wavefront stability on coronagraph. Caveats • Monochromatic • Simple model • Band limited 4th order linear Sinc mask 2 Findings • Reconfirms 10 picometers per 10 minutes Specification. • Coronagraph Contrast Leakage is 10X more sensitivity to random segment piston WFE than to random tip/tilt error. • Concludes that few segments (i.e. 0.5 to 1 ring) or very many segments (> 16 rings) has less contrast leakage as a function of piston or tip/tilt than an aperture with 2 to 4 rings of segments. 3 Aperture Dependencies • Stability amplitude is independent of aperture diameter. It depends on required Contrast Stability as a function of IWA. • Stability time depends on detected photon rate which depends on aperture, magnitude, throughput, spectral band, etc. • For a fixed contrast at a fixed wavelength at a 40 mas angular separation, the wavefront stability requirement does have a ~4X larger amplitude for a 12-m telescope than for an 8-m telescope. And, it will have also have a shorter stability requirement for the same magnitude star. 4 Introduction 5 Exoplanet Science The search for extra-terrestrial life is probably the most compelling question in modern astronomy The AURA report: From Cosmic Birth to Living Earths call for A 12 meter class space telescope with sufficient stability and the appropriate instrumentation can find and characterize dozens of Earth-like planets and make transformational advances in astrophysics. -
WFIRST-AFTA Coronagraphic Operations: Lessons Learned from the Hubble Space Telescope and the James Webb Space Telescope1 John H
WFIRST-AFTA Technical Report Rev: B Doc #: WFIRST-STScI-TR1504 Date : September 16, 2015 WFIRST-AFTA Coronagraphic Operations: Lessons Learned from the Hubble Space Telescope and the James Webb Space Telescope1 John H. Debesa, Marie Ygoufa, Elodie Choqueta, Dean C. Hinesa, David A. Golimowskia, Charles Lajoiea, Johan Mazoyera, Marshall Perrina, Laurent Pueyo a, Remi´ Soummer a, Roeland van der Marela aSpace Telescope Science Institute, 3700 San Martin Dr., Baltimore, MD, USA, 21212 Abstract. The coronagraphic instrument currently proposed for the WFIRST-AFTA mission will be the first ex- ample of a space-based coronagraph optimized for extremely high contrasts that are required for the direct imaging of exoplanets reflecting the light of their host star. While the design of this instrument is still in progress, this early stage of development is a particularly beneficial time to consider the operation of such an instrument. In this paper, we review current or planned operations on the Hubble Space Telescope (HST) and the James Webb Space Telescope (JWST) with a focus on which operational aspects will have relevance to the planned WFIRST-AFTA coronagraphic instrument. We identify five key aspects of operations that will require attention: 1) detector health and evolution, 2) wavefront control, 3) observing strategies/post-processing, 4) astrometric precision/target acquisition, and 5) po- larimetry. We make suggestions on a path forward for each of these items. Keywords: WFIRST-AFTA, coronagraphy, operations, JWST,HST. Address all correspondence to: John Debes, Space Telescope Science Institute, 3700 San Martin Dr., Baltimore, MD 21212, USA; Tel: +1 410-338-4782; Fax: +1 410-338-5090; E-mail: [email protected] 1 Introduction The WFIRST-AFTA coronagraphic instrument (CGI) enables ground-breaking exoplanet discov- eries using optimized space-based coronagraphic high contrast imaging. -
Stellar Imaging Coronagraph and Exoplanet Coronal Spectrometer
Stellar Imaging Coronagraph and Exoplanet Coronal Spectrometer – Two Additional Instruments for Exoplanet Exploration Onboard The WSO-UV 1.7 Meter Orbital Telescope Alexander Tavrova, b, Shingo Kamedac, Andrey Yudaevb, Ilia Dzyubana, Alexander Kiseleva, Inna Shashkovaa*, Oleg Korableva, Mikhail Sachkovd, Jun Nishikawae, Motohide Tamurae, g, Go Murakamif, Keigo Enyaf, Masahiro Ikomag, Norio Naritag a IKI-RAS Space Research Institute of Russian Academy of Science, Profsoyuznaya ul. 84/32, Moscow, 117997, Russia b Moscow Institute of Physics and Technology, 9 Institutskiy per., Dolgoprudny, Moscow Region 141700, Russia c Rikkyo University, 3-34-1 Nishi-Ikebukuro, Toshima, Tokyo, 171-8501, Japan d INASAN Institute of Astronomy of the Russian Academy of Sciences, Pyatnitskaya str., 48 , Moscow, 119017, Russia e NAOJ National Astronomical Observatory of Japan, 2-21-1 Osawa, Mitaka, Tokyo 181-8588, Japan f JAXA Japan Aerospace Exploration Agency, 3-3-1 Yoshinodai, Chuo, Sagamihara, Kanagawa, 229-8510, Japan g The University of Tokyo, 7-3-1 Hongo, Bunkyo, Tokyo, 113-8654, Japan Abstract. The World Space Observatory for Ultraviolet (WSO-UV) is an orbital optical telescope with a 1.7 m- diameter primary mirror currently under development. The WSO-UV is aimed to operate in the 115–310 nm UV spectral range. Its two major science instruments are UV spectrographs and a UV imaging field camera with filter wheels. The WSO-UV project is currently in the implementation phase, with a tentative launch date in 2023. As designed, the telescope field of view (FoV) in the focal plane is not fully occupied by instruments. Recently, two additional instruments devoted to exoplanets have been proposed for WSO-UV, which are the focus of this paper. -
The MIRI Coronagraphs
The Mid-Infrared Instrument for the James Webb Space Telescope, V: Predicted Performance of the MIRI Coronagraphs A. Boccaletti1, P.-O. Lagage2, P. Baudoz1,C.Beichman3.4.5,P.Bouchet2,C.Cavarroc6,D. Dubreuil2, Alistair Glasse7,A.M.Glauser8,D.C.Hines9, C.-P. Lajoie9, J. Lebreton3,4,M. D. Perrin9,L.Pueyo9,J.M.Reess1,G.H.Rieke10, S. Ronayette2,D.Rouan1,R. Soummer9, and G. S. Wright7 ABSTRACT The imaging channel on the Mid-Infrared Instrument (MIRI) is equipped with four coronagraphs that provide high contrast imaging capabilities for studying faint point sources and extended emission that would otherwise be overwhelmed by a bright point-source in its vicinity. Such bright sources might include stars that are orbited by exoplanets and circumstellar material, mass-loss envelopes around post-main-sequence stars, the near-nuclear environments in active galax- ies, and the host galaxies of distant quasars. This paper describes the coron- agraphic observing modes of MIRI, as well as performance estimates based on measurements of the MIRI flight model during cryo-vacuum testing. A brief 1LESIA, Observatoire de Paris-Meudon, CNRS, Universit´e Pierre et Marie Curie, Universit´eParis Diderot, 5 Place Jules Janssen, F-92195 Meudon, France 2Laboratoire AIM Paris-Saclay, CEA-IRFU/SAp, CNRS, Universit´e Paris Diderot, F-91191 Gif-sur- Yvette, France 3Infrared Processing and Analysis Center, California Institute of Technology, Pasadena, CA 91125, USA 4NASA Exoplanet Science Institute, California Institute of Technology, 770 S. Wilson Ave., Pasadena, CA 91125, USA 5Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr., Pasadena, CA 91107, USA 6Laboratoire AIM Paris-Saclay, CEA-IRFU/SAp, CNRS, Universit´e Paris Diderot, F-91191 Gif-sur- Yvette, France 7UK Astronomy Technology Centre, STFC, Royal Observatory Edinburgh, Blackford Hill, Edinburgh EH9 3HJ, UK 8ETH Zurich, Institute for Astronomy, Wolfgang-Pauli-Str. -
The WFIRST Mission Observatory WFIRST Coronagraph Instrument
WFIRST: Project Overview and Status Jeffrey Kruk / GSFC – on behalf of the WFIRST science and project teams The WFIRST Mission Observatory SNe Fields OBA DOOR SASS Key Features WFIRST is NASA’s next great observatory, designed to complement the capabilities of Hubble, • Telescope: 2.4m aperture Spitzer, and the James Webb Space Telescopes and LSST. The Wide-Field Instrument provides OBA • Instruments • Wide Field Imager/Spectrometer & high throughput and high-resolution imaging over a wide field of view; an integral field channel for Integral Field Unit FCR • Internal Coronagraph with Integral Field +54˚ supernova and galaxy spectroscopy. A coronagraph instrument will demonstrate new technologies Spectrograph +126˚ for active wavefront control and starlight suppression. Core programs include characterization of CGI • Data Downlink Rate: 275 Mbps GalacAc Bulge Keep-Out GB (Available twice Keep-Out Zone the expansion history and growth of structure in the Universe using weak lensing, a galaxy redshift • Data Volume: 11 Tb/day Zone yearly) survey, and type Ia SNe. Exoplanet demographics will be studied by gravitational microlensing. IC • Orbit: Sun-Earth L2 25% of the Prime Mission and 100% of extended mission time is dedicated to a Guest Observer • Launch Vehicle: Falcon Heavy • Mission Duration: 5 yr, 10yr goal Observing Zone AVIONICS program. All data will be public and available for Archival Research programs. MODULES X6 • Serviceability: Observatory designed to be robotically serviceable SNe Fields X Z • Starshade: S/C and coronagraph Y HGAS compatible with a future starshade WFIRST Field of Regard. Earth & WFI mission WFIRST Wide-Field Instrument Moon avoidance is a minor sporadic constraint. -
Evaluation of the Implementation of WFIRST/AFTA in the Context of New Worlds, New Horizons in Astronomy and Astrophysics
Evaluation of the Implementation of WFIRST/AFTA in the Context of New Worlds, New Horizons in Astronomy and Astrophysics Space Studies Board • Board on Physics and Astronomy Division on Engineering & Physical Sciences • March 2014 The National Aeronautics and Space Administration (NASA) has considered several potential designs for the Wide Field Infrared Space Telescope (WFIRST), the highest priority, large-scale, space-based observatory recommended by the 2010 National Research Council decadal survey in astronomy and astrophysics, New Worlds, New Horizons in Astronomy and Astrophysics (NWNH). Complicating their design decision is the transfer of two 2.4-meter telescope assets from the National Reconnaissance Office to NASA in 2012. Dubbed the Astrophysics Focused Telescope Assets (AFTA), this hardware could potentially be used to implement the WFIRST mission with a larger mirror, offering the potential of substantially greater scientific return for the mission than was originally proposed in NWNH. A larger mirror would also enable the inclusion of a coronagraph, which has the potential to advance NWNH objectives for technology development toward a future Earth-like exoplanet imaging mission. However, using AFTA to implement WFIRST (WFIRST/ AFTA) comes with increased cost and technical risks— particularly if the coronagraph is also included in the mission—which is at odds with the programmatic rationale in NWNH for recommending the comparatively lower-risk baseline WFIRST mission. In response to a NASA request, this report assesses the responsiveness of the WFIRST/AFTA mission—with and without a coronagraph—to the baseline WFIRST mission on the basis of their science objectives, technical complexity, and programmatic rationale, including projected cost. -
The Exo-S Probe Class Starshade Mission
The Exo-S probe class starshade mission The MIT Faculty has made this article openly available. Please share how this access benefits you. Your story matters. Citation Seager, Sara et al. “The Exo-S Probe Class Starshade Mission.” Ed. Stuart Shaklan. N.p., 2015. 96050W. © 2015 Society of Photo-Optical Instrumentation Engineers (SPIE) As Published http://dx.doi.org/10.1117/12.2190378 Publisher SPIE Version Final published version Citable link http://hdl.handle.net/1721.1/106349 Terms of Use Article is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use. Invited Paper The Exo-S Probe Class Starshade Mission Sara Seager*a, Margaret Turnbullb, William Sparksc, Mark Thomsond, Stuart B Shakland, Aki Robergee, Marc Kuchnere, N. Jeremy Kasdinf, Shawn Domagal-Goldmane, Webster Cashg, Keith Warfieldd, Doug Lismand, Dan Scharfd, David Webbd, Rachel Trabertd, Stefan Martind, Eric Cadyd, Cate Heneghand aMassachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA, USA 02139- 4307; bGlobal Science Institute, P.O. Box 252, Antigo, WI, USA 54409; cSpace Telescope Science Institute, 3700 San Martin Drive, Baltimore, MD, USA 21218-2410; dJet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA, USA 91109-8001; eGoddard Space Flight Center, 8800 Greenbelt Road, Greenbelt, MD, USA 20771-2400; fPrinceton University, Department of Mechanical and Aerospace Engineering, Engineering Quadrangle, Olden Street, Princeton, NJ, USA 08544; gUniversity of Colorado, Center for Astrophysics and Space Astronomy, 389 UCB, Boulder, CO, USA 80309-0389 ABSTRACT Exo-S is a direct imaging space-based mission to discover and characterize exoplanets. -
Brown Dwarfs 3
BROWN DWARFS B. R. OPPENHEIMER, S. R. KULKARNI Palomar Observatory, California Institute of Technology and J. R. STAUFFER Harvard–Smithsonian Center for Astrophysics After a discussion of the physical processes in brown dwarfs, we present a complete, precise definition of brown dwarfs and of planets inspired by the internal physics of objects between 0.1 and 0.001 M⊙. We discuss observa- tional techniques for characterizing low-luminosity objects as brown dwarfs, including the use of the lithium test and cooling curves. A brief history of the search for brown dwarfs leads to a detailed review of known isolated brown dwarfs with emphasis on those in the Pleiades star cluster. We also discuss brown dwarf companions to nearby stars, paying particular attention to Gliese 229B, the only known cool brown dwarf. I. WHAT IS A BROWN DWARF? A main sequence star is to a candle as a brown dwarf is to a hot poker recently removed from the fire. Stars and brown dwarfs, although they form in the same manner, out of the fragmentation and gravita- tional collapse of an interstellar gas cloud, are fundamentally different because a star has a long-lived internal source of energy: the fusion of hydrogen into helium. Thus, like a candle, a star will burn constantly until its fuel source is exhausted. A brown dwarf’s core temperature is insufficient to sustain the fusion reactions common to all main sequence stars. Thus brown dwarfs cool as they age. Cooling is perhaps the single most important salient feature of brown dwarfs, but an understanding of their definition and their observational properties requires a review of basic stellar physics. -
Development of Compact Diagnostic Coronagraph On
Journal of the Korean Astronomical Society https://doi.org/10.5303/JKAS.2017.50.5.139 50: 139 ∼ 149, 2017 October pISSN: 1225-4614 · eISSN: 2288-890X ⃝c 2017. The Korean Astronomical Society. All rights reserved. http://jkas.kas.org TOWARD A NEXT GENERATION SOLAR CORONAGRAPH:DEVELOPMENT OF A COMPACT DIAGNOSTIC CORONAGRAPH FOR THE ISS K.-S. Cho1,2, S.-C. Bong1, S. Choi1, H. Yang1, J. Kim1, J.-H. Baek1, J. Park1, E.-K. Lim1, R.-S. Kim1, S. Kim1, Y.-H. Kim1, Y.-D. Park1, S.W. Clarke3, J.M. Davila4, N. Gopalswamy4, V.M. Nakariakov5, B. Li6, and R.F. Pinto7 1Korea Astronomy and Space Science Institute, 776 Daedukdae-ro, Yuseong-gu, Daejeon 34055, Korea; [email protected] 2University of Science and Technology, 217 Gajeong-ro, Yuseong-gu, Daejeon 34113, Korea 3NASA Headquarters, Washington DC 20546-0001, USA 4NASA Goddard Space Flight Center, Greenbelt, Maryland, USA 5University of Warwick, Coventry CV4 7AL, UK 6Sandong University, 27 Shanda Nanlu, Jinan, Shandong 250100, China 7Universit´ede Toulouse, UPS-OMP, IRAP, 31400 Toulouse, France Received July 2, 2017; accepted August 7, 2017 Abstract: The Korea Astronomy and Space Science Institute plans to develop a coronagraph in collabo- ration with National Aeronautics and Space Administration (NASA) and to install it on the International Space Station (ISS). The coronagraph is an externally occulted one-stage coronagraph with a field of view from 3 to 15 solar radii. The observation wavelength is approximately 400 nm, where strong Fraunhofer absorption lines from the photosphere experience thermal broadening and Doppler shift through scatter- ing by coronal electrons. -
Super Lyot Exoearth Coronagraph (SLEEC)
Super Lyot ExoEarth Coronagraph (SLEEC) A Technology Development for Exoplanet Missions (TDEM) White Paper Principal Investigator: John Trauger Co-Investigators: Pin Chen, John Krist, Dwight Moody 16 March 2018 Jet Propulsion Laboratory California Institute of Technology 1 Signature Page _____________________________________________ John Trauger Date PI, SLEEC _____________________________________________ Brendan Crill Date Deputy Program Chief Technologist, ExEP _____________________________________________ Nick Siegler Date Program Chief Technologist, ExEP _____________________________________________ Doug Hudgins Date Program Scientist, ExEP 2 1 Objective __________________________________________________________ 4 2 Introduction/Background ____________________________________________ 4 2.1 Global Coronagraph Design Approach ___________________________________________________ 4 2.2 Prolate Spheroidal Basis Functions _______________________________________________________ 8 2.3 Figures of Merit (Objective Function) __________________________________________________ 10 3 Milestones Definition _______________________________________________ 11 3.1 Milestone 1a (M1a) ______________________________________________________________________ 11 3.2 Milestone 1b (M1b) ______________________________________________________________________ 12 3.3 Milestone 2a (M2a) ______________________________________________________________________ 12 3.4 Milestone 2b (M2b) ______________________________________________________________________ 12 4 Experiment