SWIFTS and SWIFTS-LA: Two Concepts for High Spectral Resolution Static Micro-Imaging Spectrometers
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Matematikken Viser Vej Til Mars
S •Matematikken The viser vej til Mars Kim Plauborg © The Terma Group 2016 THE BEGINNING Terma has been in Space since man walked on the Moon! © The Terma Group 2016 FROM ESRO TO EXOMARS Terma powered the first comet landing ever! BREAKING NEWS The mission ends today when the Rosetta satellite will set down on the surface In 2014 the Rosetta satellite deployed the small lander Philae, which landed on the cometof 67P morethe than 10 comet years after Rosetta was launched. © The Terma Group 2016 FROM ESRO TO EXOMARS Rosetta Mars Express Technology Venus Express evolution and Galileo enhancement Small GEO BepiColombo ExoMars © The Terma Group 2016 Why go Mars? Getting to and landing on Mars is difficult ! © The Terma Group 2016 THE EXOMARS PROGRAMME Two ESA missions to Mars in cooperation with Roscosmos with the main objective to search for evidence of life 2016 Mission Trace Gas Orbiter Schiaparelli 2020 Mission Rover Surface platform © The Terma Group 2016 EXOMARS 2016 14th March 2016 Launched from Baikonur cosmodrome, Kazakhstan © The Terma Group 2016 EXOMARS 2016 16th October 2016 Separation of Schiaparelli from the orbiter © The Terma Group 2016 SCHIAPARELLI Schiaparelli (EDM) - an entry, descent and landing demonstrator module © The Terma Group 2016 EXOMARS 2016 19th October 2016 Landing of Schiaparelli the surface of Mars © The Terma Group 2016 EXOMARS 2016 19th October 2016 Landing of Schiaparelli the surface of Mars © The Terma Group 2016 EXOMARS 2020 © The Terma Group 2016 TERMA AND EXOMARS Terma deliveries to the ExoMars 2016 mission • Remote Terminal Power Unit for Schiaparelli • Mission Control System • Spacecraft Simulator • Support for the Launch and Early Orbit Phase © The Terma Group 2016 ExoMars RTPU The RTPU is a central unit in the Schiaparelli lander. -
How a Cartoon Series Helped the Public Care About Rosetta and Philae 13 How a Cartoon Series Helped the Public Care About Rosetta and Philae
How a Cartoon Series Helped the Public Care about Best Practice Rosetta and Philae Claudia Mignone Anne-Mareike Homfeld Sebastian Marcu Vitrociset Belgium for European Space ATG Europe for European Space Design & Data GmbH Agency (ESA) Agency (ESA) [email protected] [email protected] [email protected] Carlo Palazzari Emily Baldwin Markus Bauer Design & Data GmbH EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) [email protected] [email protected] [email protected] Keywords Karen S. O’Flaherty Mark McCaughrean Outreach, space science, public engagement, EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) visual storytelling, fairy-tale, cartoon, animation, [email protected] [email protected] anthropomorphising Once upon a time... is a series of short cartoons1 that have been developed as part of the European Space Agency’s communication campaign to raise awareness about the Rosetta mission. The series features two anthropomorphic characters depicting the Rosetta orbiter and Philae lander, introducing the mission story, goals and milestones with a fairy- tale flair. This article explores the development of the cartoon series and the level of engagement it generated, as well as presenting various issues that were encountered using this approach. We also examine how different audiences responded to our decision to anthropomorphise the spacecraft. Introduction internet before the spacecraft came out of exciting highlights to come, using the fairy- hibernation (Bauer et al., 2016). The four tale narrative as a base. The hope was that In late 2013, the European Space Agency’s short videos were commissioned from the video would help to build a degree of (ESA) team of science communicators the cross-media company Design & Data human empathy between the public and devised a number of outreach activ- GmbH (D&D). -
DLR Developments and Application Ideas for Interplanetary Cubesats
DLR developments and application ideas for interplanetary cubesats iCubeSat, Milano 2019 Jens Biele1, Michael Maibaum1, Caroline Lange2, Thimo Grundmann2, Stephan Ulamec1, Marcus Thomas Knopp3, Frank-Cyrus Roshani3 1DLR German Aerospace Center, RB-MUSC, Cologne, Germany 2DLR German Aerospace Center, Bremen, Germany 3DLR German Aerospace Center, GSOC, Munich, Germany www.DLR.de • Chart 3 > Lecture > Author • Document > Date SKAD-Study [FRANK, MARCUS] • Orbiter as relais station for Mars-Rover • ………. Designs flown or studied (DLR) Hopper(10-25 kg) MASCOT (30, 70 kg) Philae (100 kg) Leonard MASCOT (10 kg) Folie 4 > Vortrag > Autor Folie 5 > Vortrag > Autor Study Flow of MASCOT („how to shrink a lander..“) • December 2008 – September 2009: feasibility study, with CNES, in context of Marco Polo and Hayabusa-2, with common requirements: • 3 iterations of different mass (95kg, 35kg & 10kg) and P/L • Settled on 10 kg lander package including 3 kg of P/L • Ho, T.-M., et al. (2016). "MASCOT—The Mobile Asteroid Surface Scout Onboard the Hayabusa2 Mission." Space Science Reviews 208(1-4): 339– 374. • ➔ Design of MASCOT 10 kg: a nanosat (30x30*20 cm³) . Could be a 18 U cubesat! Large ~ 95 kg, Philae hertitage Middle ~ 35 kg, Xtra Small ~ 10 kg, No post-landing Up-righting + mobility mobility MASCOT Payload (25% of total mass!) Instrument Science Goals Heritage Institute; PI/IM Mass [kg] MAG magnetization of the NEA MAG of ROMAP on Rosetta TU Braunschweig Lander (Philae), ESA VEX, 0,15 → formation history Themis K.H. Glassmeier / U. Auster mineralogical composition ESA ExoMars, Russia and characterize grains Phobos GRUNT, ESA size and structure of Rosetta, ESA ExoMars IAS Paris µOmega surface soil samples at μ- rover 2018, Rosetta / Philae J.P. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
7'Tie;T;E ~;&H ~ T,#T1tmftllsieotog
7'tie;T;e ~;&H ~ t,#t1tMftllSieotOg, UCLA VOLUME 3 1986 EDITORIAL BOARD Mark E. Forry Anne Rasmussen Daniel Atesh Sonneborn Jane Sugarman Elizabeth Tolbert The Pacific Review of Ethnomusicology is an annual publication of the UCLA Ethnomusicology Students Association and is funded in part by the UCLA Graduate Student Association. Single issues are available for $6.00 (individuals) or $8.00 (institutions). Please address correspondence to: Pacific Review of Ethnomusicology Department of Music Schoenberg Hall University of California Los Angeles, CA 90024 USA Standing orders and agencies receive a 20% discount. Subscribers residing outside the U.S.A., Canada, and Mexico, please add $2.00 per order. Orders are payable in US dollars. Copyright © 1986 by the Regents of the University of California VOLUME 3 1986 CONTENTS Articles Ethnomusicologists Vis-a-Vis the Fallacies of Contemporary Musical Life ........................................ Stephen Blum 1 Responses to Blum................. ....................................... 20 The Construction, Technique, and Image of the Central Javanese Rebab in Relation to its Role in the Gamelan ... ................... Colin Quigley 42 Research Models in Ethnomusicology Applied to the RadifPhenomenon in Iranian Classical Music........................ Hafez Modir 63 New Theory for Traditional Music in Banyumas, West Central Java ......... R. Anderson Sutton 79 An Ethnomusicological Index to The New Grove Dictionary of Music and Musicians, Part Two ............ Kenneth Culley 102 Review Irene V. Jackson. More Than Drumming: Essays on African and Afro-Latin American Music and Musicians ....................... Norman Weinstein 126 Briefly Noted Echology ..................................................................... 129 Contributors to this Issue From the Editors The third issue of the Pacific Review of Ethnomusicology continues the tradition of representing the diversity inherent in our field. -
Spatial Infrastructure for the OSIRIS-Rex Sample Return Mission March 23, 2016
Spatial Infrastructure for the OSIRIS-REx Sample Return Mission March 23, 2016 Dani DellaGiustina O.S. Barnouin, M.C. Nolan, C.A. Johnson, L. Le Corre, and D.S. Lauretta Lunar & Planetary Sciences Conference The Woodlands, Texas OSIRIS-REX DEFINED • Origins . Return and analyze a sample of pristine carbonaceous asteroid regolith • Spectral Interpretation . Provide ground truth for telescopic data of the entire asteroid population • Resource Identification . Map the chemistry and mineralogy of a primitive carbonaceous asteroid • Security . Measure the Yarkovsky effect on a potentially hazardous asteroid • Regolith Explorer . Document the regolith at the sampling site at scales down to the sub-cm 1 OUR PAYLOAD PERFORMS EXTENSIVE CHARACTERIZATION AT GLOBAL AND SAMPLE-SITE-SPECIFIC SCALES SamCam images the sample site, documents sample OCAMS (UA) acquisition, and images TAGSAM to evaluate sampling success MapCam performs filter photometry, maps the surface, and images the sample site PolyCam acquires Bennu from >500K-km range, performs star- field OpNav, and performs high-resolution imaging of the surface OLA (CSA) provides ranging data out to 7 km and maps the asteroid shape and surface topography 2 OUR PAYLOAD PERFORMS EXTENSIVE CHARACTERIZATION AT GLOBAL AND SAMPLE-SITE-SPECIFIC SCALES OVIRS (GSFC) maps the reflectance albedo and spectral properties from 0.4 – 4.3 µm OTES (ASU) maps the thermal flux and spectral properties from 5 – 50 µm REXIS (MIT) trains the next generation of scientists and engineers and maps the elemental abundances -
Exploration of Mars by the European Space Agency 1
Exploration of Mars by the European Space Agency Alejandro Cardesín ESA Science Operations Mars Express, ExoMars 2016 IAC Winter School, November 20161 Credit: MEX/HRSC History of Missions to Mars Mars Exploration nowadays… 2000‐2010 2011 2013/14 2016 2018 2020 future … Mars Express MAVEN (ESA) TGO Future ESA (ESA- Studies… RUSSIA) Odyssey MRO Mars Phobos- Sample Grunt Return? (RUSSIA) MOM Schiaparelli ExoMars 2020 Phoenix (ESA-RUSSIA) Opportunity MSL Curiosity Mars Insight 2020 Spirit The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export‐controlled information. Mars Express 2003-2016 … First European Mission to orbit another Planet! First mission of the “Rosetta family” Up and running since 2003 Credit: MEX/HRSC First European Mission to orbit another Planet First European attempt to land on another Planet Original mission concept Credit: MEX/HRSC December 2003: Mars Express Lander Release and Orbit Insertion Collission trajectory Bye bye Beagle 2! Last picture Lander after release, release taken by VMC camera Insertion 19/12/2003 8:33 trajectory Credit: MEX/HRSC Beagle 2 was found in January 2015 ! Only 6km away from landing site OK Open petals indicate soft landing OK Antenna remained covered Lessons learned: comms at all time! Credit: MEX/HRSC Mars Express: so many missions at once Mars Mission Phobos Mission Relay Mission Credit: MEX/HRSC Mars Express science investigations Martian Moons: Phobos & Deimos: Ionosphere, surface, -
Range Resolution Enhancement of WISDOM/Exomars
Range resolution enhancement of WISDOM/ExoMars radar soundings by the Bandwidth Extrapolation technique: Validation and application to field campaign measurements Nicolas Oudart, Valérie Ciarletti, Alice Le Gall, Marco Mastrogiuseppe, Yann Herve, Wolf-Stefan Benedix, Dirk Plettemeier, Vivien Tranier, Rafik Hassen-Khodja, Christoph Statz, et al. To cite this version: Nicolas Oudart, Valérie Ciarletti, Alice Le Gall, Marco Mastrogiuseppe, Yann Herve, et al.. Range resolution enhancement of WISDOM/ExoMars radar soundings by the Bandwidth Extrapolation tech- nique: Validation and application to field campaign measurements. Planetary and Space Science, Elsevier, 2021, 197 (March), pp.105173. 10.1016/j.pss.2021.105173. insu-03114236v2 HAL Id: insu-03114236 https://hal-insu.archives-ouvertes.fr/insu-03114236v2 Submitted on 28 Jan 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Distributed under a Creative Commons Attribution| 4.0 International License Planetary and Space Science 197 (2021) 105173 Contents lists available at ScienceDirect Planetary -
The Role of Italian Industry in Space Exploration
THE ROLE OF ITALIAN INDUSTRY IN SPACE EXPLORATION Maria Cristina Falvella ASI, Italian Space Agency Head of Strategies and Industrial Policy 53rd Session UN COPUOS Vienna, 17 February 2016 THE ITALIAN SPACE AGENCY (ASI) ASI has been founded in 1988 with the purpose to promote, develop and disseminate the scientific research and technology applied in the Space field. • Specific attention to the competitiveness of the Italian Space Industry, including SMEs • ASI operates in “integrated teams” => industry and research teams under the supervision of ASI ITALY AND EXPLORATION • Since 1964 Italy acts as a pioneer in space • Exploration is a flagship program for Italy, enhancing the competitiveness of the national industrial and scientific community • Participation in successful ESA and NASA programs, with challenging roles for national industries ISS and Mars : the top priorities Italy considers ISS and Mars destinations as part of a single exploration process and works to maximize the technology and system synergies among these destinations as well as to exploit the respective benefits of robotic and human exploration. • Economic and intellectual return out of the investments • Worldwide international relations • Competitiveness of the whole supply chain, from Large System Integrators (LSIs) to Small and Medium Companies (SMEs) • Leader position in international supply chains • Upgrade of technology capabilities and IPR • Benefits in non-space related systems and applications THE ITALIAN SUPPLY CHAIN The strategic effort to encourage the development -
The Cassini Ultraviolet Imaging Spectrograph Investigation
THE CASSINI ULTRAVIOLET IMAGING SPECTROGRAPH INVESTIGATION 1, 1 1 LARRY W. ESPOSITO ∗, CHARLES A. BARTH , JOSHUA E. COLWELL , GEORGE M. LAWRENCE1, WILLIAM E. McCLINTOCK1,A. IAN F. STEWART1, H. UWE KELLER2, AXEL KORTH2, HANS LAUCHE2, MICHEL C. FESTOU3,ARTHUR L. LANE4, CANDICE J. HANSEN4, JUSTIN N. MAKI4,ROBERT A. WEST4, HERBERT JAHN5, RALF REULKE5, KERSTIN WARLICH5, DONALD E. SHEMANSKY6 and YUK L. YUNG7 1University of Colorado, Laboratory for Atmospheric and Space Physics, 1234 Innovation Drive, Boulder, CO 80303, U.S.A. 2Max-Planck-Institut fur¨ Aeronomie, Max-Planck-Strasse 2, 37191 Katlenburg-Lindau, Germany 3Observatoire Midi-Pyren´ ees,´ 14 avenue E. Belin, F31400 Toulouse, France 4JetPropulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91109, U.S.A. 5Deutsches Zentrum fur¨ Luft und Raumfahrt, Institut fur¨ Weltraumsensorik und Planetenerkundung, Rutherford Strasse 2, 12489 Berlin, Germany 6University of Southern California, Department of Aerospace Engineering, 854 W. 36th Place, Los Angeles, CA 90089, U.S.A. 7California Institute of Technology, Division of Geological and Planetary Sciences, MS 150-21, Pasadena, CA 91125, U.S.A. (∗Author for correspondence: E-mail: [email protected]) (Received 8 July 1999; Accepted in final form 18 October 2000) Abstract. The Cassini Ultraviolet Imaging Spectrograph (UVIS) is part of the remote sensing payload of the Cassini orbiter spacecraft. UVIS has two spectrographic channels that provide images and spectra covering the ranges from 56 to 118 nm and 110 to 190 nm. A third optical path with a solar blind CsI photocathode is used for high signal-to-noise-ratio stellar occultations by rings and atmospheres. A separate Hydrogen Deuterium Absorption Cell measures the relative abundance of deuterium and hydrogen from their Lyman-α emission. -
Shape Reconstruction of the Asteroid Ryugu in Hayabusa2 Mission
Asteroid Science 2019 (LPI Contrib. No. 2189) 2093.pdf SHAPE RECONSTRUCTION OF THE ASTEROID RYUGU IN HAYABUSA2 MISSION. Naru Hirata1, Naoyuki Hirata2, S. Tanaka2, N. Nishikawa2, T. Sugiyama1, R. Noguchi3, Y. Shimaki3, R. Gaskell4, E. Palmer4, K. Matsumoto5, H. Senshu6, Y. Yamamoto3, S. Murakami3, Y. Ishihara3, 7, S. Sugita8, T. Morota8, R. Honda9, M. Arakawa2, K. Ogawa2, Y. Tsuda3, S. Watanabe10, 1ARC-Space, the University of Aizu (Aizu-Wakamatsu, Fukushima, 965-8580, Japan, [email protected]), 2Kobe University, 3ISAS/JAXA, 4Planetary Science Institute, 5NAOJ, 6Chiba Institute of Technology, 7NIES, 8University of Tokyo, 9Kochi University, 10Nagoya University. Introduction: The Hayabusa2 spacecraft arrived during initial observation campaigns from 07/2018 to at the asteroid Ryugu in 06/2018 and started its 08/2018. These campaigns include the Box-A (20 km proximity observation to select candidates of landing altitude), Box-B (6.5 km altitude), and Mid-Altitude sites for touchdown operations. The shape of the (5.1 km altitude) observations. Models were then asteroid is one of the most critical information not only revised with data from following various observations, for landing site selection but also for scientific including close-up imaging during decent operations, discussions. high- and low-phase angle observations, and high sub- We successfully reconstructed and updated the spacecraft latitude observations. Because of constraints shape models of Ryugu with images taken by the on the relative position of the spacecraft to the asteroid, optical navigation camera (ONC) onboard the the sub-spacecraft latitude is limited within ±30˚. This spacecraft and relating ancillary data acquired during limitation affects the performance of the shape model proximity observation of the asteroid [1]. -
VIRTIS/Venus Express Summary
VIRTIS for Venus Express Pierre Drossart# and Giuseppe Piccioni&, December 2002 #LESIA, Obs. Paris and &IASF,Rome VIRTIS (Visible and Infrared Thermal Imaging Spectrometer) is a complex instrument initially devoted to the remote sensing study of comet Wirtanen on the Rosetta mission, at wavelengths between 0.3 and 5 mm. The focal planes, with state of the art CCD and infrared detectors achieve high sensitivity for low emissivity sources. Due to the high flexibility of the operational modes of VIRTIS, these performances are also ideally adapted for the study of Venus atmosphere, both on night and day sides. VIRTIS is therefore aimed to provide a 4- dimensional study of Venus atmosphere (2D imaging + spectral dimension + temporal variations), the spectral variations permitting a sounding at different levels of the atmosphere, from the ground up to the thermosphere. The infrared capability of VIRTIS is especially well fitted to the thermal sounding of the night side atmosphere (Taylor et al, 1997), which give a tomography of the atmosphere down to the surface. Precursors: First attempts of imaging spectrometry on the Venus night side from space in the near infrared were made by NIMS/Galileo (Figure 1) in 1990 (Carlson et al, 1990) and VIMS/Cassini in 1999 (Baines et al, 2000). These fast fly-bys gave an idea of how powerful this method of investigation could be at Venus. Unfortunately, the limited duration of the fly- bys allowed only limited investigations, in particular on the meteorological evolution of the clouds. Observation of Venus with a new generation imaging spectrometer like VIRTIS would provide a unique opportunity to continue these investigations on an extended basis.