Section: “Asteroids and Comets”
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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). -
Space Situational Awareness
→ SPACE SITUATIONAL AWARENESS OUTLINE - Background - Purpose - Aims - Composition - Space Surveillance (SST) - Space Weather (SWE) - Near-Earth Objects (NEO) - Summary 2 BACKGROUND Image: Dan Durda – FIAAA 3 INTRODUCTION PURPOSE OF THE SSA PROGRAMME “The objective of the Space Situational Awareness (SSA) programme is to support the European independent utilisation of, and access to, space for research or services, through the provision of timely and quality data, information, services and knowledge regarding the space environment, the threats and the sustainable exploitation of the outer space surrounding our planet Earth.” - ESA Ministerial Council November 2008 4 INTRODUCTION AIMS OF THE SSA PROGRAMME • Independent utilisation of Space – Space assets are critical assets • Guarantee access to Space – Diplomatic, – Political – Regulatory – Technical • Serve EU “Lisbon Objectives” – New Applications – New Jobs – New Markets 5 INTRODUCTION CUSTOMERS FOR SSA SERVICES • European Governments • Space Insurance • United Nations – EU • Space Industry • Defence – National • Energy • Civil Protection – Regional – Surveying • European Space Agencies – Electrical Grid – ESA – Power Supply – National • Network Operations • Spacecraft Operators • Telecommunications – Commercial • Air Traffic Control – Academic • Search and Rescue Entities – Governmental 6 INTRODUCTION Current Objectives 2009 – 2012 • Preparatory Programme – Governance Definition – Data Policy – Architecture – Federation – Precursor Services – Radar Breadboard – Pilot Data Centres 2012 -
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. -
YORP and Yarkovsky Effects in Asteroids (1685) Toro,(2100) Ra
Astronomy & Astrophysics manuscript no. YORP_detections c ESO 2017 November 17, 2017 YORP and Yarkovsky effects in asteroids (1685) Toro, (2100) Ra-Shalom, (3103) Eger, and (161989) Cacus J. Durechˇ 1, D. Vokrouhlický1 , P. Pravec2, J. Hanuš1, D. Farnocchia3, Yu. N. Krugly4, V. R. Ayvazian5, P. Fatka1, 2, V. G. Chiorny4, N. Gaftonyuk4, A. Galád2, R. Groom6, K. Hornoch2, R. Y. Inasaridze5, H. Kucákovᡠ1, 2, P. Kušnirák2, M. Lehký1, O. I. Kvaratskhelia5, G. Masi7, I. E. Molotov8, J. Oey9, J. T. Pollock10, V. G. Shevchenko4, J. Vraštil1, and B. D. Warner11 1 Institute of Astronomy, Faculty of Mathematics and Physics, Charles University, V Holešovickáchˇ 2, 18000, Prague, Czech Re- public e-mail: [email protected] 2 Astronomical Institute, Czech Academy of Sciences, Fricovaˇ 298, Ondrejov,ˇ Czech Republic 3 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 4 Institute of Astronomy of Kharkiv National University, Sumska Str. 35, 61022 Kharkiv, Ukraine 5 Kharadze Abastumani Astrophysical Observatory, Ilia State University, K. Cholokoshvili Av. 3/5, Tbilisi 0162, Georgia 6 Darling Range Observatory, Perth, WA, Australia 7 Physics Department, University of Rome “Tor Vergata”, Via della Ricerca Scientifica 1, 00133 Rome, Italy 8 Keldysh Institute of Applied Mathematics, RAS, Miusskaya 4, Moscow 125047, Russia 9 Blue Mountains Observatory, 94 Rawson Pde. Leura, NSW 2780, Australia 10 Physics and Astronomy Department, Appalachian State University, 525 Rivers St, Boone, NC 28608, USA 11 Center for Solar System Studies – Palmer Divide Station, 446 Sycamore Ave., Eaton, CO 80615, USA Received ???; accepted ??? ABSTRACT Context. The rotation states of small asteroids are affected by a net torque arising from an anisotropic sunlight reflection and thermal radiation from the asteroids’ surfaces. -
The Hera Mission
Dr. Patrick Michel Hera Investigation Team PI Université Côte d’Azur Observatoire de la Côte d’Azur CNRS, Lagrange Laboratory Nice, France The Hera Mission ESA UNCLASSIFIED - For Official Use Hera main aspects Role of space missions at ESA in NEO hazard mitigation • Understanding the problem (deflection modeling and simulations) 2001 • Ground versus space solutions analyses • Assessment of space component options 2002- • 6 parallel phase-0 studies (3 space telescopes, 3 rendezvous) Euneos Nero Earthguard 1 2004 • ESA’s NEO Mission Advisory Panel (NEOMAP) established • Kinetic impactor validation ranked highest importance 2004- • Don Quijote mission selected and studied up to phase-A level 2006 • SANCHO / Proba-IP orbiter up to phase A level studies, small deep-space Don Quijote Ishtar Simone 2008- mission to investigate impactor’s result 2009 • AIDA proposed by NASA: USA/impactor + ESA/impact assessment • ESA phase 0 and phase A studies on the observer spacecraft "AIM” (GSP) 2011- Proba-IP 2016 • Phase B1 study and “consolidation phase” for mission definition (GSTP) • HERA: impact observer spacecraft reformulation and optimization AIM 2017- • Phase B1 implementation + payload + technology breadboards (GSTP+SSA) Several concepts 2019 • DART phase-C kick-off on 15 May 2018 Hera iterated AIDA: An International Planetary Defense Mission U.S. National Research Council Committee “Defending Planet Earth: Near-Earth Object Surveys and Hazard Mitigation Strategies” Recommendation: “If [U.S.] Congress chooses to fund mitigation research at an appropriately high level, the first priority for a space mission in the mitigation area is an experimental test of a kinetic impactor along with a characterization, monitoring, and verification system, such as the Don Quixote mission that was previously considered, but not funded, by the European Space Agency. -
Argops) Solution to the 2017 Astrodynamics Specialist Conference Student Competition
AAS 17-621 THE ASTRODYNAMICS RESEARCH GROUP OF PENN STATE (ARGOPS) SOLUTION TO THE 2017 ASTRODYNAMICS SPECIALIST CONFERENCE STUDENT COMPETITION Jason A. Reiter,* Davide Conte,1 Andrew M. Goodyear,* Ghanghoon Paik,* Guanwei. He,* Peter C. Scarcella,* Mollik Nayyar,* Matthew J. Shaw* We present the methods and results of the Astrodynamics Research Group of Penn State (ARGoPS) team in the 2017 Astrodynamics Specialist Conference Student Competition. A mission (named Minerva) was designed to investigate Asteroid (469219) 2016 HO3 in order to determine its mass and volume and to map and characterize its surface. This data would prove useful in determining the necessity and usefulness of future missions to the asteroid. The mission was designed such that a balance between cost and maximizing objectives was found. INTRODUCTION Asteroid (469219) 2016 HO3 was discovered recently and has yet to be explored. It lies in a quasi-orbit about the Earth such that it will follow the Earth around the Sun for at least the next several hundred years providing many opportunities for relatively low-cost missions to the body. Not much is known about 2016 HO3 except a general size range, but its close proximity to Earth makes a scientific mission more feasible than other near-Earth objects. A Request For Proposal (RFP) was provided to university teams searching for cost-efficient mission design solutions to assist in the characterization of the asteroid and the assessment of its potential for future, more in-depth missions and possible resource utilization. The RFP provides constraints on launch mass, bus size as well as other mission architecture decisions, and sets goals for scientific mapping and characterization. -
Asteroid Retrieval Feasibility Study
Asteroid Retrieval Feasibility Study 2 April 2012 Prepared for the: Keck Institute for Space Studies California Institute of Technology Jet Propulsion Laboratory Pasadena, California 1 2 Authors and Study Participants NAME Organization E-Mail Signature John Brophy Co-Leader / NASA JPL / Caltech [email protected] Fred Culick Co-Leader / Caltech [email protected] Co -Leader / The Planetary Louis Friedman [email protected] Society Carlton Allen NASA JSC [email protected] David Baughman Naval Postgraduate School [email protected] NASA ARC/Carnegie Mellon Julie Bellerose [email protected] University Bruce Betts The Planetary Society [email protected] Mike Brown Caltech [email protected] Michael Busch UCLA [email protected] John Casani NASA JPL [email protected] Marcello Coradini ESA [email protected] John Dankanich NASA GRC [email protected] Paul Dimotakis Caltech [email protected] Harvard -Smithsonian Center for Martin Elvis [email protected] Astrophysics Ian Garrick-Bethel UCSC [email protected] Bob Gershman NASA JPL [email protected] Florida Institute for Human and Tom Jones [email protected] Machine Cognition Damon Landau NASA JPL [email protected] Chris Lewicki Arkyd Astronautics [email protected] John Lewis University of Arizona [email protected] Pedro Llanos USC [email protected] Mark Lupisella NASA GSFC [email protected] Dan Mazanek NASA LaRC [email protected] Prakhar Mehrotra Caltech [email protected] -
Arecibo Radar Observations of 14 High-Priority Near-Earth Asteroids in CY2020 and January 2021 Patrick A
Arecibo Radar Observations of 14 High-Priority Near-Earth Asteroids in CY2020 and January 2021 Patrick A. Taylor (LPI, USRA), Anne K. Virkki, Flaviane C.F. Venditti, Sean E. Marshall, Dylan C. Hickson, Luisa F. Zambrano-Marin (Arecibo Observatory, UCF), Edgard G. Rivera-Valent´ın, Sriram S. Bhiravarasu, Betzaida Aponte-Hernandez (LPI, USRA), Michael C. Nolan, Ellen S. Howell (U. Arizona), Tracy M. Becker (SwRI), Jon D. Giorgini, Lance A. M. Benner, Marina Brozovic, Shantanu P. Naidu (JPL), Michael W. Busch (SETI), Jean-Luc Margot, Sanjana Prabhu Desai (UCLA), Agata Rozek˙ (U. Kent), Mary L. Hinkle (UCF), Michael K. Shepard (Bloomsburg U.), and Christopher Magri (U. Maine) Summary We propose the continuation of the long-running project R3037 to physically and dynamically characterize the population of near-Earth asteroids with the Arecibo S-band (2380 MHz; 12.6 cm) planetary radar system. The objectives of project R3037 are to: (1) collect high-resolution radar images of and (2) report ultra-precise radar astrometry for the strongest predicted radar targets for the 2020 calendar year plus early January 2021. Such images will be used for three-dimensional shape modeling as the data sets allow. These observations will be carried out as part of the NASA- funded Arecibo planetary radar program, Grant No. 80NSSC19K0523, to PI Anne Virkki (Arecibo Observatory, University of Central Florida) with Patrick Taylor as Institutional PI at the Lunar and Planetary Institute (Universities Space Research Association). Background Radar is arguably the most powerful Earth-based technique for post-discovery physical and dynamical characterization of near-Earth asteroids (NEAs) and plays a crucial role in the nation’s planetary defense initiatives led through the NASA Planetary Defense Coordination Office. -
General Assembly Distr.: General 7 January 2005
United Nations A/AC.105/839 General Assembly Distr.: General 7 January 2005 Original: English Committee on the Peaceful Uses of Outer Space Scientific and Technical Subcommittee Forty-second session Vienna, 21 February-4 March 2004 Item 10 of the provisional agenda∗ Near-Earth objects Information on research in the field of near-Earth objects carried out by international organizations and other entities Note by the Secretariat Contents Page I. Introduction ................................................................... 2 II. Replies received from international organizations and other entities ..................... 2 European Space Agency ......................................................... 2 The Spaceguard Foundation ...................................................... 17 __________________ ∗ A/AC.105/C.1/L.277. V.05-80067 (E) 010205 020205 *0580067* A/AC.105/839 I. Introduction In accordance with the agreement reached at the forty-first session of the Scientific and Technical Subcommittee (A/AC.105/823, annex II, para. 18) and endorsed by the Committee on the Peaceful Uses of Outer Space at its forty-seventh session (A/59/20, para. 140), the Secretariat invited international organizations, regional bodies and other entities active in the field of near-Earth object (NEO) research to submit reports on their activities relating to near-Earth object research for consideration by the Subcommittee. The present document contains reports received by 17 December 2004. II. Replies received from international organizations and other entities European Space Agency Overview of activities of the European Space Agency in the field of near-Earth object research: hazard mitigation Summary 1. Near-Earth objects (NEOs) pose a global threat. There exists overwhelming evidence showing that impacts of large objects with dimensions in the order of kilometres (km) have had catastrophic consequences in the past. -
Imaging of Near-Earth Asteroids
Imaging of Near-Earth Asteroids. Michael C. Nolan, Arecibo Observatory / Cornell University. [email protected] (787) 878-2612 ext 212 Lance A. M. Benner (Jet Propulsion Laboratory / California Institute of Technology) Marina Brozovič (Jet Propulsion Laboratory / California Institute of Technology) Ellen S. Howell (Arecibo Observatory / Cornell University) Jean-Luc Margot (UCLA) Abstract As remnants of accretion, building blocks of planets, space resources and potential impactors, the asteroids offer insights to solar system formation and evolution. Recent results show that this population is extremely diverse, compositionally, texturally and structurally. As a result, spacecraft cannot explore the population of asteroids in a reasonable time or at a reasonable cost without guidance from Earth-based reconnaissance. Compositional variation can be studied using remote-sensing spectroscopic techniques, either ground-based or from general-purpose space-based telescopes such as HST and JWST. Study of the textural and structural properties of asteroids requires imaging and shape determination. In addition, the largest uncertainties in orbit determination arise from non-gravitational forces, such as the Yarkovsky effect, that depend on the detailed shapes of asteroids. This shape determination can be done crudely using visible lightcurves and in detail using direct imaging (generally using adaptive optics), interferometric and radar techniques. Of these, only ground-based radar using the Arecibo and Goldstone radar systems has been routinely used for asteroid imaging, typically yielding shapes with tens to hundreds of pixels across a diameter and an absolute size accuracy of 5% or better. Other groundbased techniques are unlikely to achieve this level of precision in the upcoming decade, and space-based techniques will visit no more than a few targets. -
Defending Planet Earth: Near-Earth Object Surveys and Hazard Mitigation Strategies Final Report
PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION Defending Planet Earth: Near-Earth Object Surveys and Hazard Mitigation Strategies Final Report Committee to Review Near-Earth Object Surveys and Hazard Mitigation Strategies Space Studies Board Aeronautics and Space Engineering Board Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS Washington, D.C. www.nap.edu PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION THE NATIONAL ACADEMIES PRESS 500 Fifth Street, N.W. Washington, DC 20001 NOTICE: The project that is the subject of this report was approved by the Governing Board of the National Research Council, whose members are drawn from the councils of the National Academy of Sciences, the National Academy of Engineering, and the Institute of Medicine. The members of the committee responsible for the report were chosen for their special competences and with regard for appropriate balance. This study is based on work supported by the Contract NNH06CE15B between the National Academy of Sciences and the National Aeronautics and Space Administration. Any opinions, findings, conclusions, or recommendations expressed in this publication are those of the author(s) and do not necessarily reflect the views of the agency that provided support for the project. International Standard Book Number-13: 978-0-309-XXXXX-X International Standard Book Number-10: 0-309-XXXXX-X Copies of this report are available free of charge from: Space Studies Board National Research Council 500 Fifth Street, N.W. Washington, DC 20001 Additional copies of this report are available from the National Academies Press, 500 Fifth Street, N.W., Lockbox 285, Washington, DC 20055; (800) 624-6242 or (202) 334-3313 (in the Washington metropolitan area); Internet, http://www.nap.edu.