The New Worlds Probe: a Starshade with JWST NWP Can Do Imaging
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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. -
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). -
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. -
James Webb Space Telescope Is Expected to Have As Profound and Far-Reaching an Impact on Astrophysics As Did Its Famous Predecessor
JWST Peter Jakobsen & Peter Jensen Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands nspired by the success of the Hubble Space Telescope, NASA, ESA and the Canadian I Space Agency have collaborated since 1996 on the design and construction of a scientifically worthy successor. Due to be launched from Kourou in 2013 on an Ariane-5 rocket, the James Webb Space Telescope is expected to have as profound and far-reaching an impact on astrophysics as did its famous predecessor. Introduction Astronomers cannot conduct experi- ments on the Universe, instead they must patiently observe the night sky as they find it, teasing out its secrets only by collecting and analysing the light received from celestial bodies. Since the time of Galileo, the foremost tool of astronomy has been the telescope, feeding first the human eye, and later increasingly sensitive and sophisticated instruments designed to record and dissect the captured light. With the coming of the Space Age, astronomers soon began sending their telescopes and instrumentation into orbit, to operate above the constraining window of Earth’s atmosphere. One of the most successful astronomical esa bulletin 133 - february 2008 33 Science Who was James Webb? James E. Webb (1906-92) was NASA’s second administrator. Appointed by President John F. Kennedy in 1961, Webb organised the fledgling space agency and oversaw the development of the Apollo programme until his retirement a few months before Apollo 11 successfully landed on the Moon. Although an educator and lawyer by training, with a long career in public service and industry, Webb can rightfully be considered the father of modern space science. -
THE THOUSAND-STEP MODEL Or, the Earth As a Peppercorn
THE THOUSAND-STEP MODEL or, The Earth as a Peppercorn Copyright 1989 by Guy Ottewell Universal Workshop PO Box 426 Middleburg, VA 20118-0426 ISBN 0-934546-21-5 [Converted into metric units by Malcolm Coe] This is a classic exercise for visualizing just how BIG our Solar System really is. Both the relative size and spacing of the planets are demonstrated in this outdoor exercise, using a mere peppercorn to represent the size of the Earth. Guy Ottewell has kindly given permission for this electronic presentation of The Thousand-Yard Model; his exercise is presented in its original form, indexed with a few anchors to help you find you way around the large file. Image of the planets courtesy of NASA. Introduction Pacing off the Solar System Additional Notes Beyond the Solar System Numerical Summary Introduction Can you picture the dimensions of the solar system? Probably not, for they are of an order so amazing that it is difficult either to realize or to show them. You may have seen a diagram of the Sun and planets, in a book. Or you may have seen a revolving model of the kind called an orrery (because the first was built for an Earl of Orrery in 1715). But even the largest of such models--such as those that cover the ceilings of the Hayden Planetarium in New York and the Morehead Planetarium at Chapel Hill-are far too small. They omit the three outermost planets, yet still cannot show the remaining ones far enough apart. The fact is that the planets are mighty small and the distances between them are almost ridiculously large. -
October 9-13, 2013 Alamo Drafthouse Dfw Videofest.Org 1 Contents
OCTOBER 9-13, 2013 ALAMO DRAFTHOUSE DFW VIDEOFEST.ORG 1 CONTENTS Brought to you By ............................................................................ 2 2013 Board of directors ............................................................... 3 contriButors & sponsors .......................................................... 4 Welcome By Bart Weiss ................................................................. 8 aBout our Jurors ............................................................................10 HBO® Proudly Salutes the texas shoW Jurors .........................................................................16 Kovacs aWard .....................................................................................18 screenings ...........................................................................................20 TH 26 ANNUAL schedule ................................................................................................53 Ben Britt/Kaleta doolin art ..................................................60 DALLAS VIDEOFEST aWard shoW tWeets By Jennifer reeder ......................64 essays .......................................................................................................66 ©2013 Home Box Office, Inc. All rights reserved. HBO® and related channels and service marks are the property of Home Box Office, Inc. 406145_VideoFest_AD.indd 1 8/26/13 4:33 PM Dallas VideoFest 26 2 VIDEO ASSOCIATION OF DaLLAS 2013 3 BROUGHT TO YOU BY BOARD OF DIRECTORS Barton Weiss Kelly McNichol Interns vIdeo assocIatIon -
The Mid-Infrared Instrument for the James Webb Space Telescope, I: Introduction
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. -
Must-Carry Rules, and Access to Free-DTT
Access to TV platforms: must-carry rules, and access to free-DTT European Audiovisual Observatory for the European Commission - DG COMM Deirdre Kevin and Agnes Schneeberger European Audiovisual Observatory December 2015 1 | Page Table of Contents Introduction and context of study 7 Executive Summary 9 1 Must-carry 14 1.1 Universal Services Directive 14 1.2 Platforms referred to in must-carry rules 16 1.3 Must-carry channels and services 19 1.4 Other content access rules 28 1.5 Issues of cost in relation to must-carry 30 2 Digital Terrestrial Television 34 2.1 DTT licensing and obstacles to access 34 2.2 Public service broadcasters MUXs 37 2.3 Must-carry rules and digital terrestrial television 37 2.4 DTT across Europe 38 2.5 Channels on Free DTT services 45 Recent legal developments 50 Country Reports 52 3 AL - ALBANIA 53 3.1 Must-carry rules 53 3.2 Other access rules 54 3.3 DTT networks and platform operators 54 3.4 Summary and conclusion 54 4 AT – AUSTRIA 55 4.1 Must-carry rules 55 4.2 Other access rules 58 4.3 Access to free DTT 59 4.4 Conclusion and summary 60 5 BA – BOSNIA AND HERZEGOVINA 61 5.1 Must-carry rules 61 5.2 Other access rules 62 5.3 DTT development 62 5.4 Summary and conclusion 62 6 BE – BELGIUM 63 6.1 Must-carry rules 63 6.2 Other access rules 70 6.3 Access to free DTT 72 6.4 Conclusion and summary 73 7 BG – BULGARIA 75 2 | Page 7.1 Must-carry rules 75 7.2 Must offer 75 7.3 Access to free DTT 76 7.4 Summary and conclusion 76 8 CH – SWITZERLAND 77 8.1 Must-carry rules 77 8.2 Other access rules 79 8.3 Access to free DTT -
PRIX EUROPA Television Fiction Franz Fuchs
PRIX Television EUROPA Fiction Franz Fuchs - A Patriot 01 Franz Fuchs - Ein Patriot Entering organisation: Österreichischer Rundfunk - ORF Contact: Susanne Spellitz When the terrorist Franz Fuchs committed suicide Email: [email protected] in 2000, it seemed as if Austria had buried a painful chapter of its past. Elisabeth Scharang has taken another Author/s: Elisabeth Scharang look at the case. This programme reveals new facets Director: Elisabeth Scharang that go beyond the actual criminal case. Camera: Helmut Wimmer A feature documentary film, this psychogram of a lone Commissioning editor: Klaus Lintschinger perpetrator interwoven with documentary sequences Production company: epo-film produktionsges.m.b.h. and archival material, becomes the first film to tackle Producer: Dieter Pochlatko this subject comprehensively, questioning the political Co-Producer/s: ORF, Austrian Television Fund, climate in Austria and Europe as well. It is the story Cine Styria Kunst of an exceptionally talented person who ended up becoming a terrorist instead of a nuclear physicist. Length: 89’ Total budget: €1,000,000.- Production format: Super 16 Date of production: September 2007 First broadcast: 20:15, 2 October 2008, ORF Screened on: Monday, 20 October 2008 AUSTRIA Television PRIX Fiction EUROPA 02 The Intruder De Indringer Entering organisation: episode 1/3 Vlaamse Radio- en Televisieomroep - VRT Contact: Franky Audenaerde Tom Vansant, a 40-year-old doctor in Brussels, is Email: [email protected] desperately searching for traces of his daughter Louise who disappeared 18 months ago. In his search, he Author/s: Ward Hulselmans comes across another 16-year-old runaway who left Director: Frank Van Mechelen her hometown in the Ardennes at about the same time Camera: Lou Bergmans as Louise disappeared. -
Power Distribution for Cryogenic Instruments at 6-40K the James Webb Space Telescope Case
Power Distribution for Cryogenic Instruments at 6-40K The James Webb Space Telescope Case Peter Rumler<1>, Ray Lundqu ist<2>, Jose Lorenzo Alvarez'll , Jeff Since 11<2>, Jim Tutt1e<2> fl ) ESA-ESTEC, 2200AG Noordwijk. Nether/ands, JNh'r.ru111/cr'!! l!sa.1111 <1JNASA-GSFC, Greenbelt, MD-20771 USA, my.a./1111d,111isr'if,11a.1·a .1?01· \ .. -- ABSTRA CT ISIM structure located in Region I of the JWST Observatory. Each instrument's OA is connected The Integrated Science Instrument Module (ISIM) of through a heat strap to a dedicated radiator that the James Webb Space Telescope (JWST) operates its provides passive cooling to temperatures below 40K. instruments passively cooled at around 40 Kelvin (K), In addition, the NIRSpec FPA and the SIDECAR ASIC with a warm Instrument Electronic Compartment (!EC) (System for Image Digitization, Enhancement. Control at 300K attached to it. From the wann electronics all and Retrieval) connect to a dedicated radiator separate secondary signal and power harnesses have to bridge from the NIRSpec OA radiator. The ISIM Structure is this 300-40K temperature difference and minimize the a frame made of square graphite fiber reinforced plastic power dissipation and parasitic heat leak into the cold (GFRP) tubes attached together with gussets and clips, region. and with metal fittings for the Optical Telescope After an introduction of the !SIM with its instruments, Element (OTE) and Science Instrument interfaces. The the IEC with the electronics, and the harness resistivity of the GFRP tube material has been architecture with a special radiator, this paper measured to be in the order of H'l/m, and the resistance \ elaborates on the cryogenic wire selection and tests of the joints between GFRP tubes has been measured to perfonned to establish current de-rating rules for be approximately 10-200! per joint. -
Use of a Pathfinder Optical Telescope Element for James Webb Space Telescope Risk Mitigation
Use of a Pathfinder Optical Telescope Element for James Webb Space Telescope Risk Mitigation Lee D. Feinberga*, Ritva KeskiKuhaa, Charlie Atkinsonb, Scott C. Texter” aNASA Goddard Space Flight Center, Greenbelt, MD, USA 20771; 1’Northrup Grumman, Redondo Beach, CA USA ABSTRACT A Pathfmder of the James Webb Space Telescope (JWST) Optical Telescope Element is being developed to check out critical ground support equipment and to rehearse integration and testing procedures. This paper provides a summary of the baseline Pathfmder configuration and architecture, objectives of this effort, limitations of Pathfinder, status of its development, and future plans. Special attention is paid to risks that will be mitigated by Pathfmder. Keywords: Space Telescope, JWST, OTE, James Webb Space Telescope, Pathfmder, Risk 1. INTRODUCTION The testing of JWST Optical Telescope Element 1 (OTE) and Integrated Science Instrument System (ISIM) occurs as an integrated entity called the OTE-ISIM (OTIS) at the Johnson Space Center”. In order to assure the test is successful with as few cryogenic cycles as is possible, an OTE Pathfinder is being funded by the prime contractor Northrop Grumman as an IR+D funded effort. NGAS’s current plan emphasizes optical checkout at cryogenic temperatures though an augmentation to the Pathfmder plan is in the process of being added to the program that would add thermal checkout and dynamics objectives. 2. BIsT0RY OF PATHFINDER The OTE Pathfmder has its roots in the Verification Engineering Test Articles implemented on the Chandra program wherein unfinished flight optics were used to aid in the development of, and to demonstrate the integration operations and X-ray optical testing of, the critical optical components of the telescope using GSE that was uniquely designed for the purpose.