Italy Is Today Deeply Involved in Space Science with a Multifaceted Activity
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CASTOR: a Wide-Field, UV Space Telescope
Astro2020 Activities and Projects White Paper CASTOR: A Wide-Field, UV Space Telescope Thematic Areas: Space Missions Ground-Based Activities and Projects Computation Astrophysics Theoretical Astrophysics Laboratory Astrophysics Principal Author: Peter L. Capak Name: Peter L. Capak Institution: Infrared Processing and Analysis Center, California Institute of Technology, 1200 E. California Blvd, Pasadena, CA, 91125, USA Email: [email protected] Phone: (626) 395-6422 Co-authors: Michael L. Balogh (University of Waterloo), Jessie L. Christiansen (NASA Exo- planet Science Institute, Caltech), Patrick Cotˆ e´ (National Research Council of Canada), Olivier Dore´ (Caltech, JPL), Maria Drout (University of Toronto), Christopher J. Evans (UK Astronomy Technology Centre, Royal Observatory Edinburgh), Andreas L. Faisst (IPAC, Caltech), Sarah C. Gallagher (University of Western Ontario), Carl J. Grillmair (IPAC, Caltech), Paul Harrison (Magellan Aerospace), John B. Hutchings (National Research Council of Canada), JJ Kavelaars (National Research Council of Canada), J.-F. Lavigne (ABB), Janice C. Lee (IPAC, Caltech), Shouleh Nikzad (Jet Propulsion Laboratory, California Institute of Technology), Jason D. Rhodes (Jet Propulsion Laboratory, California Institute of Technology), Jason F. Rowe (Bishop’s Univer- sity), Ruben´ Sanchez-Janssen (UK Astronomy Technology Centre, Royal Observatory Edinburgh), Alan D. Scott (Honeywell Aerospace), Charles Shapiro (Jet Propulsion Laboratory, California In- stitute of Technology), Melanie Simet (University of California Riverside), Harry I. Teplitz (IPAC, Caltech), Kim A. Venn (University of Victoria), Ludovic Van Waerbeke (University of British Columbia) 1 Abstract: CASTOR (The Cosmological Advanced Survey Telescope for Optical and UV Re- search) is a proposed Canadian-led mission that would provide high-resolution imaging and spec- troscopy in the UV/optical (0.15–0.55 µm) spectral region. -
Planetary Science Division Status Report
Planetary Science Division Status Report Jim Green NASA, Planetary Science Division January 26, 2017 Astronomy and Astrophysics Advisory CommiBee Outline • Planetary Science ObjecFves • Missions and Events Overview • Flight Programs: – Discovery – New FronFers – Mars Programs – Outer Planets • Planetary Defense AcFviFes • R&A Overview • Educaon and Outreach AcFviFes • PSD Budget Overview New Horizons exploresPlanetary Science Pluto and the Kuiper Belt Ascertain the content, origin, and evoluFon of the Solar System and the potenFal for life elsewhere! 01/08/2016 As the highest resolution images continue to beam back from New Horizons, the mission is onto exploring Kuiper Belt Objects with the Long Range Reconnaissance Imager (LORRI) camera from unique viewing angles not visible from Earth. New Horizons is also beginning maneuvers to be able to swing close by a Kuiper Belt Object in the next year. Giant IcebergsObjecve 1.5.1 (water blocks) floatingObjecve 1.5.2 in glaciers of Objecve 1.5.3 Objecve 1.5.4 Objecve 1.5.5 hydrogen, mDemonstrate ethane, and other frozenDemonstrate progress gasses on the Demonstrate Sublimation pitsDemonstrate from the surface ofDemonstrate progress Pluto, potentially surface of Pluto.progress in in exploring and progress in showing a geologicallyprogress in improving active surface.in idenFfying and advancing the observing the objects exploring and understanding of the characterizing objects The Newunderstanding of Horizons missionin the Solar System to and the finding locaons origin and evoluFon in the Solar System explorationhow the chemical of Pluto wereunderstand how they voted the where life could of life on Earth to that pose threats to and physical formed and evolve have existed or guide the search for Earth or offer People’sprocesses in the Choice for Breakthrough of thecould exist today life elsewhere resources for human Year forSolar System 2015 by Science Magazine as exploraon operate, interact well as theand evolve top story of 2015 by Discover Magazine. -
Comet Interceptor: a Proposed ESA Mission to a Dynamically New Comet
EPSC Abstracts Vol. 13, EPSC-DPS2019-1679-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Comet Interceptor: A proposed ESA Mission to a Dynamically New Comet Geraint H. Jones(1,2), Colin Snodgrass(3), and The Comet Interceptor Consortium (see www.cometinterceptor.space ) (1) UCL Mullard Space Science Laboratory, Holmbury St. Mary, Dorking, RH5 6NT, UK ([email protected]) (2) The Centre for Planetary Sciences at UCL/Birkbeck, London, UK (3) University of Edinburgh, United Kingdom ([email protected]) Abstract allow valuable multi-point measurements of the solar wind over different lengtH-scales as tHese craft In response to the recent European Space Agency’s separate. call for proposals for a Fast (F) Mission, a multi- spacecraft project has been submitted to ESA to For the comet encounter, the primary spacecraft, encounter a dynamically new comet or interstellar planned to also act as the primary communication object. SucH an encounter with a comet approacHing point for the whole constellation, would be targetted the Sun for the first time would provide valuable data to pass outside the hazardous inner coma, on the to complement that from all previous comet missions, sunward side of tHe comet. At least one sub-spacecraft whicH Have by necessity studied sHort-period comets would be targetted for tHe nucleus/inner coma region. that Have evolved from their original condition during The various component spacecraft will carry a range their time orbiting near the Sun. of miniaturised instruments for remote and in situ studies of tHe object’s composition, nucleus, coma, The mission’s primary science goal is to cHaracterise, and plasma environment. -
Secretariat Distr.: General 25 November 2014
United Nations ST/SG/SER.E/733 Secretariat Distr.: General 25 November 2014 Original: English Committee on the Peaceful Uses of Outer Space Information furnished in conformity with the Convention on Registration of Objects Launched into Outer Space Letter dated 30 October 2014 from the Legal Services Department of the European Space Agency addressed to the Secretary-General In conformity with the Convention on Registration of Objects Launched into Outer Space (General Assembly resolution 3235 (XXIX), annex), the rights and obligations of which the European Space Agency (ESA) has declared its acceptance of, the Agency has the honour to transmit information on space objects Sentinel-1A and ATV-5, which were put into orbit within the past seven months (see annex). The Agency has the further honour to note that with effect from 28 October 2014, the date of signature of the Agreement between the European Union, Represented by the European Commission, and the European Space Agency on the Implementation of the Copernicus Programme, Including the Transfer of Ownership of Sentinels, the Agency has transferred the ownership of Sentinel-1A to the European Union. (Signed) Marco Ferrazzani ESA Legal Counsel and Head of the Legal Services Department V.14-07991 (E) 031214 041214 *1407991* ST/SG/SER.E/733 Annex Registration data on space objects launched by the European Space Agency* Sentinel-1A Information provided in conformity with the Convention on Registration of Objects Launched into Outer Space Committee on Space Research 2014-016A international -
Mars Reconnaissance Orbiter
Chapter 6 Mars Reconnaissance Orbiter Jim Taylor, Dennis K. Lee, and Shervin Shambayati 6.1 Mission Overview The Mars Reconnaissance Orbiter (MRO) [1, 2] has a suite of instruments making observations at Mars, and it provides data-relay services for Mars landers and rovers. MRO was launched on August 12, 2005. The orbiter successfully went into orbit around Mars on March 10, 2006 and began reducing its orbit altitude and circularizing the orbit in preparation for the science mission. The orbit changing was accomplished through a process called aerobraking, in preparation for the “science mission” starting in November 2006, followed by the “relay mission” starting in November 2008. MRO participated in the Mars Science Laboratory touchdown and surface mission that began in August 2012 (Chapter 7). MRO communications has operated in three different frequency bands: 1) Most telecom in both directions has been with the Deep Space Network (DSN) at X-band (~8 GHz), and this band will continue to provide operational commanding, telemetry transmission, and radiometric tracking. 2) During cruise, the functional characteristics of a separate Ka-band (~32 GHz) downlink system were verified in preparation for an operational demonstration during orbit operations. After a Ka-band hardware anomaly in cruise, the project has elected not to initiate the originally planned operational demonstration (with yet-to-be used redundant Ka-band hardware). 201 202 Chapter 6 3) A new-generation ultra-high frequency (UHF) (~400 MHz) system was verified with the Mars Exploration Rovers in preparation for the successful relay communications with the Phoenix lander in 2008 and the later Mars Science Laboratory relay operations. -
Precollimator for X-Ray Telescope (Stray-Light Baffle) Mindrum Precision, Inc Kurt Ponsor Mirror Tech/SBIR Workshop Wednesday, Nov 2017
Mindrum.com Precollimator for X-Ray Telescope (stray-light baffle) Mindrum Precision, Inc Kurt Ponsor Mirror Tech/SBIR Workshop Wednesday, Nov 2017 1 Overview Mindrum.com Precollimator •Past •Present •Future 2 Past Mindrum.com • Space X-Ray Telescopes (XRT) • Basic Structure • Effectiveness • Past Construction 3 Space X-Ray Telescopes Mindrum.com • XMM-Newton 1999 • Chandra 1999 • HETE-2 2000-07 • INTEGRAL 2002 4 ESA/NASA Space X-Ray Telescopes Mindrum.com • Swift 2004 • Suzaku 2005-2015 • AGILE 2007 • NuSTAR 2012 5 NASA/JPL/ASI/JAXA Space X-Ray Telescopes Mindrum.com • Astrosat 2015 • Hitomi (ASTRO-H) 2016-2016 • NICER (ISS) 2017 • HXMT/Insight 慧眼 2017 6 NASA/JPL/CNSA Space X-Ray Telescopes Mindrum.com NASA/JPL-Caltech Harrison, F.A. et al. (2013; ApJ, 770, 103) 7 doi:10.1088/0004-637X/770/2/103 Basic Structure XRT Mindrum.com Grazing Incidence 8 NASA/JPL-Caltech Basic Structure: NuSTAR Mirrors Mindrum.com 9 NASA/JPL-Caltech Basic Structure XRT Mindrum.com • XMM Newton XRT 10 ESA Basic Structure XRT Mindrum.com • XMM-Newton mirrors D. de Chambure, XMM Project (ESTEC)/ESA 11 Basic Structure XRT Mindrum.com • Thermal Precollimator on ROSAT 12 http://www.xray.mpe.mpg.de/ Basic Structure XRT Mindrum.com • AGILE Precollimator 13 http://agile.asdc.asi.it Basic Structure Mindrum.com • Spektr-RG 2018 14 MPE Basic Structure: Stray X-Rays Mindrum.com 15 NASA/JPL-Caltech Basic Structure: Grazing Mindrum.com 16 NASA X-Ray Effectiveness: Straylight Mindrum.com • Correct Reflection • Secondary Only • Backside Reflection • Primary Only 17 X-Ray Effectiveness Mindrum.com • The Crab Nebula by: ROSAT (1990) Chandra 18 S. -
ATHENA COMMUNITY NEWSLETTER #4 December 2017 Contents
ATHENA COMMUNITY NEWSLETTER #4 December 2017 Contents Welcome.......................................................................................... 1 Fourth Announcement of Opportunity to join the Athena Community Working Groups/Topical Panels .................................................... 1 Discovery of Electromagnetic Counterparts to Gravitational Waves .......... 2 Athena Project Status .......................................................................... 2 News from the Instruments ................................................................. 4 News from the WFI ......................................................................... 4 News from X-IFU ............................................................................ 4 The SKA-Athena Synergy Exercise Coming to the End.............................. 6 Athena End-to-End Simulations ............................................................ 7 Unveiling the Hot, High Redshift Universe with the Athena WFI ................. 8 Athena Community People .................................................................. 9 Conferences ................................................................................... 10 Athena in Conferences (January-July 2018) ....................................... 10 Coming conferences of interest ...................................................... 10 Edited by Athena Community Office: F.J. Carrera, M.T. Ceballos, S. Martínez-Núñez, M.P. Monterde Instituto de Física de Cantabria (CSIC-UC) Avda Los Castros s/n 39005 Santander -
Astrophysics
National Aeronautics and Space Administration Astrophysics Astronomy and Astrophysics Paul Hertz Advisory Committee Director, Astrophysics Division Washington, DC Science Mission Directorate January 26, 2017 @PHertzNASA www.nasa.gov Why Astrophysics? Astrophysics is humankind’s scientific endeavor to understand the universe and our place in it. 1. How did our universe 2. How did galaxies, stars, 3. Are We Alone? begin and evolve? and planets come to be? These national strategic drivers are enduring 1972 1982 1991 2001 2010 2 Astrophysics Driving Documents 2016 update includes: • Response to Midterm Assessment • Planning for 2020 Decadal Survey http://science.nasa.gov/astrophysics/documents 3 Astrophysics - Big Picture • The FY16 appropriation/FY17 continuing resolution and FY17 President’s budget request provide funding for NASA astrophysics to continue its planned programs, missions, projects, research, and technology. – The total funding (Astrophysics including Webb) remains at ~$1.35B. – Fully funds Webb for an October 2018 launch, WFIRST formulation (new start), Explorers mission development, increased funding for R&A, new suborbital capabilities. – No negative impact from FY17 continuing resolution (through April 28, 2017). – Awaiting FY18 budget guidance from new Administration. • The operating missions continue to generate important and compelling science results, and new missions are under development for the future. – Senior Review in Spring 2016 recommended continued operation of all missions. – SOFIA is adding new instruments: HAWC+ instrument being commissioned; HIRMES instrument in development; next gen instrument call in 2017. – NASA missions under development making progress toward launches: ISS-NICER (2017), ISS-CREAM (2017), TESS (2018), Webb (2018), IXPE (2020), WFIRST (mid-2020s). – Partnerships with ESA and JAXA on their future missions create additional science opportunities: Euclid (ESA), X-ray Astronomy Recovery Mission (JAXA), Athena (ESA), L3/LISA (ESA). -
Mro High Resolution Imaging Science Experiment (Hirise)
Sixth International Conference on Mars (2003) 3287.pdf MROHIGHRESOLUTIONIMAGINGSCIENCEEXPERIMENT(HIRISE): INSTRUMENTDEVELOPMENT.AlanDelamere,IraBecker,JimBergstrom,JonBurkepile,Joe Day,DavidDorn,DennisGallagher,CharlieHamp,JeffreyLasco,BillMeiers,AndrewSievers,Scott StreetmanStevenTarr,MarkTommeraasen,PaulVolmer.BallAerospaceandTechnologyCorp.,PO Box1062,Boulder,CO80306 Focus Introduction:Theprimaryfunctionalre- Mechanism PrimaryMirror quirementoftheHiRISEimager,figure1isto PrimaryMirrorBaffle 2nd Fold allowidentificationofbothpredictedandun- Mirror knownfeaturesonthesurfaceofMarstoa muchfinerresolutionandcontrastthanprevi- ouslypossible[1],[2].Thisresultsinacam- 1st Fold erawithaverywideswathwidth,6kmat Mirror 300kmaltitude,andahighsignaltonoise ratio,>100:1.Generationofterrainmaps,30 Filters cmverticalresolution,fromstereoimages Focal requiresveryaccurategeometriccalibration. Plane Theprojectlimitationsofmass,costand schedulemakethedevelopmentchallenging. FocalPlane SecondaryMirror Inaddition,thespacecraftstability[3]must Electronics TertiaryMirror SecondaryMirrorBaffle notbeamajorlimitationtoimagequality. Thenominalorbitforthesciencephaseofthe missionisa3pmorbitof255by320kmwith Figure1Cameraopticalpathoptimizedforlowmass periapsislockedtothesouthpole.Thetrack Integration(TDI)tocreateveryhigh(100:1)signalnoise velocityisapproximately3,400m/s. ratioimages. HiRISEFeatures:TheHiRISEinstrumentperformance Theimagerdesignisanall-reflectivethreemirrorastig- goalsarelistedinTable1.Thedesignfeaturesa50cm matictelescopewithlight-weightedZeroduropticsanda -
Members' Meeting Package
DPS Members Meeting 6 October 2011 Members Meeting Agenda Opening remarks Melissa McGrath Secretary’s report Athena Coustenis Treasurer’s report Diana Blaney EPO report Nick Schneider Webmaster report Tony Roman Hartmann Travel Grant recipients Dan Britt Professional Development Subcommittee report Rachel Mastrapa Federal Relations Subcommittee report Josh Emery Survey report Anne Verbiscer Icarus report Phil Nicholson Nominating Subcommittee member election Nantes Meeting report Olivier Grasset Future meetings report Melissa McGrath Press Officer report Vishnu Reddy Outgoing Chair remarks Melissa McGrath Incoming chair remarks Dan Britt New Business, discussion, questions Opening Remarks • Short reports, please hold questions until the end. Longer versions are posted on the DPS web site at: dps.aas.org/reports • Later in the meeting we’ll elect a new member of the Nominating Subcommittee. From our By Laws: "The Nominating Subcommittee is responsible for presenting to the DPS Secretary a list of candidates for DPS Officers and Committee members. At the business meeting each year, the DPS membership selects a new member for the Nominating Subcommittee, who serves a three-year term. In the third year of service, the member serves as Chair of the subcommittee." DPS Secretary’s Report Athena Coustenis Membership • Current active membership: 1358, same as last year at the same time (varying between 1100 and 1500). Non-US fraction 19% • Renew your membership and pay your dues TODAY and in any event before 31 December 2011 to avoid dropping from lists in Feb. – Pay your 2012 membership dues online at https://members.aas.org/ • Also, please take a moment to update your personal DPS member file. -
Arxiv:2005.12932V1 [Astro-Ph.EP] 26 May 2020 with Eccentricity, E = 1.2, ‘Oumuamua Encountered the Solar System with V∞ = 26 Km S
Draft version May 28, 2020 Typeset using LATEX default style in AASTeX63 Evidence that 1I/2017 U1 (`Oumuamua) was composed of molecular hydrogen ice. Darryl Seligman1 and Gregory Laughlin2 1 Dept. of the Geophysical Sciences, University of Chicago, Chicago, IL 60637 2Dept. of Astronomy, Yale University, New Haven, CT 06517 (Received April 14, 2020; Revised May 22, 2020; Accepted May 28, 2020) Submitted to ApJL ABSTRACT `Oumuamua (I1 2017) was the first macroscopic (l ∼ 100 m) body observed to traverse the inner solar system on an unbound hyperbolic orbit. Its light curve displayed strong periodic variation, and it showed no hint of a coma or emission from molecular outgassing. Astrometric measurements indicate that 'Oumuamua experienced non-gravitational acceleration on its outbound trajectory, but energy balance arguments indicate this acceleration is inconsistent with a water ice sublimation-driven jet of the type exhibited by solar system comets. We show that all of `Oumaumua's observed properties can be explained if it contained a significant fraction of molecular hydrogen (H2) ice. H2 sublimation at a rate proportional to the incident solar flux generates a surface-covering jet that reproduces the observed acceleration. Mass wasting from sublimation leads to monotonic increase in the body axis ratio, explaining `Oumuamua's shape. Back-tracing `Oumuamua's trajectory through the Solar System permits calculation of its mass and aspect ratio prior to encountering the Sun. We show that H2-rich bodies plausibly form in the coldest dense cores of Giant Molecular Clouds, where number densities are of order n ∼ 105, and temperatures approach the T = 3 K background. -
IEEE 2018 Paper Sunrise Draft7
2018 IEEE Aerospace Conference Big Sky, Montana, USA 3-10 March 2018 Pages 1-740 IEEE Catalog Number: CFP18AAC-POD ISBN: 978-1-5386-2015-1 1/6 Copyright © 2018 by the Institute of Electrical and Electronics Engineers, Inc. All Rights Reserved Copyright and Reprint Permissions: Abstracting is permitted with credit to the source. Libraries are permitted to photocopy beyond the limit of U.S. copyright law for private use of patrons those articles in this volume that carry a code at the bottom of the first page, provided the per-copy fee indicated in the code is paid through Copyright Clearance Center, 222 Rosewood Drive, Danvers, MA 01923. For other copying, reprint or republication permission, write to IEEE Copyrights Manager, IEEE Service Center, 445 Hoes Lane, Piscataway, NJ 08854. All rights reserved. *** This is a print representation of what appears in the IEEE Digital Library. Some format issues inherent in the e-media version may also appear in this print version. IEEE Catalog Number: CFP18AAC-POD ISBN (Print-On-Demand): 978-1-5386-2015-1 ISBN (Online): 978-1-5386-2014-4 ISSN: 1095-323X Additional Copies of This Publication Are Available From: Curran Associates, Inc 57 Morehouse Lane Red Hook, NY 12571 USA Phone: (845) 758-0400 Fax: (845) 758-2633 E-mail: [email protected] Web: www.proceedings.com TABLE OF CONTENTS DEFECT TREND ANALYSIS OF C-130 ENVIRONMENTAL CONTROL SYSTEM BY DATA MINING OF MAINTENANCE HISTORY............................................................................................................................................................................1