The Double Asteroid Redirection Test (Dart) A

Total Page:16

File Type:pdf, Size:1020Kb

The Double Asteroid Redirection Test (Dart) A ASTEROID IMPACT AND DEFLECTION ASSESSMENT (AIDA) MISSION: THE DOUBLE ASTEROID REDIRECTION TEST (DART) A. F. Cheng1, P. Michel2 , O. Barnouin1, A. Campo‐Bagatin3, P. Miller4, P. Pravec5, D. C. Richardson6, A.S. Rivkin1, S. R. Schwartz2, A. Stickle1, K. Tsiganis7, S. Ulamec8, 1JHU/APL, MD ([email protected]), 2Lagrange Lab., Univ. Côte d’Azur, Obs. Côte d’Azur, CNRS, Nice, France, 3Univ. Alicante, Spain, 4LLNL, 5Ondrejov Obs, Czech Rep., 6Univ. MD, 7Univ. Thessaloniki, Greece, 8DLR, Germany The Asteroid Impact and Deflection Assessment AIDA: Critical Test of Asteroid Mitigation by Kinetic Impact • The asteroid threat is international. Initially • Sophisticated models exist for simulating kinetic (AIDA) Mission: Introduction following the discovery of a hazardous asteroid, deflection, but the predicted amount of deflection depends its impact location is uncertain, spanning on physical properties that have never been measured on any The AIDA mission will provide the first demonstration and test of the effectiveness borders and continents. Eventually the predicted asteroid, and that AIDA is designed to measure. of kinetic impactors for planetary defense. AIDA is a joint project between NASA and impact is pinpointed to one nation, but even • The scale of a kinetic deflection event is much larger then its effects will be regional or even global. than can be accessed in laboratory experiments, and occurs in ESA. The NASA‐led mission element is the Double Asteroid Redirect Test (DART) a microgravity geology, so Earth‐based experiments are helpful m Prevention, preparation, and recovery must be which is a kinetic impactor, a ~300‐kg spacecraft designed to impact the moon of the coordinated internationally to benefit from but insufficient. worldwide resources and expertise. •Until kinetic deflection models are benchmarked on an binary system 65803 Didymos. The deflection of the moon will be measured by the actual asteroid, their predictions will have unknown • Techniques for deflecting a hazardous Diameter ESA‐led Asteroid Impact Mission (AIM) (which will characterize the moon) as well as asteroid require demonstration and validation uncertainties, and the possibility of unexpected behavior that by ground‐based optical and radar observations. prior to implementation against a real threat. is overlooked or unresolved by the models. AIDA is the first mission to demonstrate asteroid deflection by a kinetic Kinetic deflection (crashing a massive rocket into •AIDA will characterize the physical properties and internal structure of the target asteroid prior to the kinetic impactor and to study a binary asteroid and its internal structure, physical an asteroid to move it off course) is the most Years warning mature and capable method of deflecting most impact, providing ground truth for making quantitative properties, and origin. It will demonstrate interplanetary optical communication and asteroids, except for rare objects with short predictions of deflection. deep‐space inter‐satellite links with CubeSats and a lander in deep space (done by warning time or very large size. •AIDA will provide an end‐to‐end test of the integrated technology required to carry out an asteroid deflection AIM). mission. Spacecraft kinetic impact to change the course of an asteroid DART + AIM = AIDA (left) Schematic of the DART (NASA) 65803 Didymos AIDA mission concept. kinetic Impactor binary asteroid Although DART and AIM are independent missions, together they will provide the first measurements of aplanetary‐scale impact The next intercept opportunity experiment with known AIM (ESA) impact conditions on a as favorable as 2022 at Rendezvous Didymos is after 2040 Observer well‐characterized target Earth-based body. observations • DART impact during excellent apparition: Didymos at V ~ 14‐15, very well placed for Chile, observable from other DART: Double Asteroid observatories • Didymos primary and secondary • NASA’s DART mission is currently a are separated by up to 0.02 arcsec Redirection Test Phase‐A study. DART is a strategic technology demonstration that will when 0.08 AU from Earth HGA launch in 2020 and impact the Marginally resolvable with ALMA secondary of the Didymos binary (sub‐mm), Magellan adaptive LGA system in 2022. DART will be a full‐ optics scale demonstration of asteroid • Post‐impact brightening and ejecta deflection by kinetic impact DRACO imager stream as extended object • DART will develop our understanding of impact effects at large scales, infer (“coma”) may be observable from asteroid properties, and study long‐ Earth term dynamics of impact ejecta • Debris cloud analogous to YORP‐ • DART will use ground‐based driven Main Belt Comets? observations to measure the binary LGA period change from kinetic impact AIDA Investigation Working Groups Star Tracker with an accuracy of 10% WG 1 Modeling and Simulation of Impact Outcomes Angela Stickle, Paul Miller, Steven Schwartz • DART will return high‐resolution WG 2Remote Sensing Observations Andy Rivkin, Petr Pravec The DART payload is one instrument, a images of the target prior to impact WG 3 Dynamical and Physical Properties of Didymos Derek Richardson, Kleomenis Tsiganis, Adriano Campo‐Bagatin high resolution imager derived from New to determine the impact site and its Horizons LORRI geologic context WG 4 Science Proximity Operations Stephan Ulamec, Olivier Barnouin.
Recommended publications
  • 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.
    [Show full text]
  • Venona Special Studies
    - 1 - Venona Project Special Studies Transcribed by Students of the Mercyhurst College Institute for Intelligence Studies Arranged by John Earl Haynes, Library of Congress, 2010 COVER NAMES IN NEW YORK TRAFFIC p. 2 UNIDENTIFIED COVER NAMES IN NEW YORK TRAFFIC p. 86 COVER NAMES IN SAN FRANCISCO TRAFFIC p. 92 COVER NAMES IN WASHINGTON TRAFFIC p. 123 ADDITIONAL COVERNAMES AND RELATED INFORMATION IN DIPLOMATIC TRAFFIC p. 127 REVISED TRANSLATION OF MESSAGE ON ANTENNA-LIBERAL'S WIFE ETHEL p. 135 THE COVERNAMES "ANTENNA" AND "LIBERAL" IN . MESSAGES p. 139 ESSAGES IN . INVOLVING THE COVERNAME"ENORMOZ" AND THE NAMES OF NUCLEAR PHYSICISTS, ETC. p. 147 UNDATED REPORT OF MEREDITH GARDNER p. 155 DEVELOPMENT OF THE “G--“HOMER” [“GOMER”] CASE p. 158 THE KOMAR (KRAVCHENKO) AFFAIR IN . MESSAGES p. 161 REVISED TRANSLATION OF TWO . MESSAGES ON CHANGES IN COVERNAMES p. 170 THE COVERNAME "KARAS" IN. TRAFFIC p. 178 THE COVERNAMES "TÉNOR", "BAS", AND "CHETÁ" (? IN . TRAFFIC p. 181 - 2 - Special Study Cover Names in New York Traffic - 3 - cover-name Message number Date Publication reference S/ or 3/NBF/ 19 N.Y. to M. 812 29053 JKI 06 T1022 1B-1910 0027A ABRAM N.Y. to M. 992 24063 JKR 14 T872√ 1B-7518 0005A JACK SOBLE 1086 06073 JKV 48 T873√ 2A-0011 1957 29113 NNNNNN T939√ 625 04054 JHD 48 T916√ 851 15064 JIJ 40 T10.1√ 1146 10084 JHM 41 T123√ 1251 02094 JHN 12 T301√ (to ChEKh) 0005B 1353 23094 JHO 42 T289√ 1449 12104 JIL 37 T106√ 1754 14124 JHZ 49 T6√ 48 11015 JHV 37 (NSA)T1941 AVGUR 2A-0013 1638 (AUGUR) N.Y.
    [Show full text]
  • 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.
    [Show full text]
  • ESA SSA and Instrumentation Required for Space Weather Activities
    ESA SSA and instrumentation required for space weather activities Piers Jiggens, Alain Hilgers (ESTEC/TEC) Juha-Pekka Luntama, Alexi Glover (ESOC/HSO) SSA Preparatory Programme Overview (2009-2012) SSA Preparatory Programme SST NEO SWE Core CO-I CO-II Data Centre (DC-xx) Database and Prototype Requirements Architectural Portal Pilot Data and design Development Centres evaluation SN-I SN-II SN-IV SN-VI Preparation of Space Weather Space Weather Space Weather Space Weather Instruments Precursor Additional Services Implementation Service Services Design Study Operations and Development SSA Preparatory Programme Architecture studies ESA Customer Product System Req. (CRD) Spec. (PSD) Req. (SRD) CO-I Also SN-II CO-II Dedicated Space Weather Hosted SSA Spacecraft Instruments Payloads Programme Implementation Architectural Astrium Design Study Design Study (GmbH) Gather Instrument Astrium Kayser-Threde Documentation (GmbH) (GmbH) 2010 - Produce shortlist of Covering all 3 Covering only one viable missions Segments: segment: 2013 Space Surveillance Space Weather Match instruments & Tracking (other 2 are to missions Near-Earth Objects covered under a Space Weather separate contract) Determine 2012-2014 2013-2014 Development Plan SN-II: Space Weather Instrument Implementation Design Study - Inputs 1. Create database of instruments (46 originally included) Astrium (GmbH) 2. AO + instrument workshop (ESTEC, November 2010) Project Manager: Norbert Pailer 3. List of all possible mission opportunities (> 200 initially) 4. Shortlist of representative instruments based on maturity at the time and the amount of data provided (Design Descriptions, ICDs) including: • Radiation Monitors: NGRM, HMRM, EPT, SREM; Plasma instruments: SW- ChaPS, AMBER, AMBER_GEO, M-NLP • Micrometeoroids: AIDA-IS, SODA; Surface Potential: SPD; Magnetometer: MRMAG; Auroral Imager: WFAI; Solar X-rays: XFM 5.
    [Show full text]
  • Landing and Operations on Comet 67P/Churyumov–Gerasimenko
    Acta Astronautica ∎ (∎∎∎∎) ∎∎∎–∎∎∎ Contents lists available at ScienceDirect Acta Astronautica journal homepage: www.elsevier.com/locate/actaastro Rosetta Lander – Landing and operations on comet 67P/Churyumov–Gerasimenko Stephan Ulamec a,n, Cinzia Fantinati a, Michael Maibaum a, Koen Geurts a, Jens Biele a, Sven Jansen a, Oliver Küchemann a, Barbara Cozzoni a, Felix Finke a, Valentina Lommatsch a, Aurelie Moussi-Soffys b, Cedric Delmas b, Laurence O´Rourke c a DLR, D-51147 Köln, Germany b CNES, F-31055 Toulouse, France c ESA/ESAC, Urb. Villafranca del Castillo, ES-28691 Madrid, Spain article info abstract Article history: The Rosetta Lander Philae is part of the ESA Rosetta Mission which reached comet 67P/ Received 2 October 2015 Churyumov–Gerasimenko after a 10 year cruise in August 2014. Since then, Rosetta has Received in revised form been studying both its nucleus and coma with instruments aboard the Orbiter. On 16 November 2015 November 12th, 2014 the Lander, Philae, was successfully delivered to the surface of the Accepted 24 November 2015 comet and operated for approximately 64 h after separation from the mother spacecraft. Since the active cold gas system aboard the Lander as well as the anchoring harpoons did Keywords: not work, Philae bounced after the first touch-down at the planned landing site “Agilkia”.At Rosetta the final landing site, “Abydos”, a modified First Scientific Sequence was performed. Due to Philae the unexpectedly low illumination conditions and a lack of anchoring the sequence had to Lander be adapted in order to minimize risk and maximize the scientific output. All ten instru- Comet Operations ments could be activated at least once, before Philae went into hibernation.
    [Show full text]
  • DART Mission Update
    Kinetic Impactor Andy Cheng JHU/APL 15 Nov 2018 DART Mission Update Goddard Space Flight Center Johnson Space Center Langley Research Center Glenn Research Center Marshall Space Flight Center Planetary Defense Coordination Office 1 Regimes of Primary Applicability for Planetary Defense Mitigation Defending Planet Earth (2010) Zero PHAs National Academy of Sciences Deep Impact Recommendation: “the first priority for a space About 150 PHAs mission in the mitigation area is an experimental test of a kinetic impactor” About 5,000 PHAs DART is the first kinetic DART impact test at a realistic scale for planetary Too small to be Defending Planet Earth (2010) considered PHAs defense 2 Launch June 15, 2021 March 6, 2022 IMPACT: October 5, 2022 2001 CB21 flyby S-type, 578 meters, 3.3-hour rotation rate LICIA (Light Italian Cubesat for Imaging of Asteroids) ASI contribution, under consideration DART Spacecraft 65803 Didymos 560 kg arrival mass Didymos-B (1996 GT) Didymos-A 12.5 m × 2.4 m × 2.0 m 163 meters 1,180-meter separation 780 meters, S-type 6 km/s closing speed 11.92-hour orbital period between centers of A and B 2.26-hour rotation period Earth-Based Observations • Target the binary asteroid Didymos system 0.07 AU range at impact Predicted ~8-minute change • Impact Didymos-B and change its orbital period in binary orbit period • Measure the period change from Earth DART – Double Asteroid Redirection Test 3 DART Program Update .DART mission confirmed by NASA in August, 2018. DART is in PHASE C-D .NASA has re-affirmed decision to use NEXT- C ion propulsion system for DART Autonomous navigation .NASA will procure launch services for DART using imager to guide to target through NLS; LV selection is in process ─ DART will have dedicated LV .LICIACube, an ASI-contributed cubesat ─ Letters exchanged between NASA and ASI ─ Studying operations concept and cubesat NEXT-C ion propulsion accommodations on DART first flight 4 DART Ion Propulsion Mission First flight of NASA NEXT-C ion engine .
    [Show full text]
  • WV Graded Music List 2011
    2011 WV Graded Music List, p. 1 2011 West Virginia Graded Music List Grade 1 Grade 2 Grade 3 Grade 4 Grade 5 Grade 6 Grade Artist Arranger Title Publisher 1 - Higgins, John Suo Gan HL 1 - McGinty Japanese Folk Trilogy QU 1 - McGinty, Anne Elizabethan Songbook, An KJ 1 - Navarre, Randy Ngiele, Ngiele NMP 1 - Ployhar Along the Western Trail BE 1 - Ployhar Minka BE 1 - Ployhar Volga Boat Song BE 1 - Smith, R.W. Appalachian Overture BE Variant on an Old English 1 - Smith, R.W. BE Carol 1 - Story A Jubilant Carol BE 1 - Story Classic Bits and Pieces BE 1 - Story Patriotic Bits and Pieces BE 1 - Swearingen Three Chorales for Band BE 1 - Sweeney Shenandoah HL 1 Adams Valse Petite SP 1 Akers Berkshire Hills BO 1 Akers Little Classic Suite CF 1 Aleicheim Schaffer Israeli Folk Songs PO 1 Anderson Ford Forgotten Dreams BE 1 Anderson Ford Sandpaper Ballet BE 1 Arcadelt Whiting Ave Maria EM 1 Arensky Powell The Cuckoo PO 1 Bach Gardner Little Bach Suite ST Grand Finale from Cantata 1 Bach Gordon BO #207 1 Bach Walters Celebrated Air RU 1 Bain, James L. M Wagner Brother James' Air BE 1 Balent Bold Adventure WB Drummin' With Reuben And 1 Balent BE Rachel 1 Balent Lonesome Tune WB 1 Balmages Gettysburg FJ 2011 WV Graded Music List, p. 2 1 Balmages Majestica FJ 1 Barnes Ivory Towers of Xanadu SP 1 Bartok Castle Hungarian Folk Suite AL 1 Beethoven Clark Theme From Fifth Symphony HL 1 Beethoven Foulkes Creation's Hymn PO 1 Beethoven Henderson Hymn to Joy PO 1 Beethoven Mitchell Ode To Joy CF 1 Beethoven Sebesky Three Beethoven Miniatures Al 1 Beethoven Tolmage
    [Show full text]
  • Robotic Asteroid Prospector
    Robotic Asteroid Prospector Marc M. Cohen1 Marc M. Cohen Architect P.C. – Astrotecture™, Palo Alto, CA, USA 94306-3864 Warren W. James2 V Infinity Research LLC. – Altadena, CA, USA Kris Zacny,3 Philip Chu, Jack Craft Honeybee Robotics Spacecraft Mechanisms Corporation – Pasadena, CA, USA This paper presents the results from the nine-month, Phase 1 investigation for the Robotic Asteroid Prospector (RAP). This project investigated several aspects of developing an asteroid mining mission. It conceived a Space Infrastructure Framework that would create a demand for in space-produced resources. The resources identified as potentially feasible in the near-term were water and platinum group metals. The project’s mission design stages spacecraft from an Earth Moon Lagrange (EML) point and returns them to an EML. The spacecraft’s distinguishing design feature is its solar thermal propulsion system (STP) that provides two functions: propulsive thrust and process heat for mining and mineral processing. The preferred propellant is water since this would allow the spacecraft to refuel at an asteroid for its return voyage to Cis- Lunar space thus reducing the mass that must be launched from the EML point. The spacecraft will rendezvous with an asteroid at its pole, match rotation rate, and attach to begin mining operations. The team conducted an experiment in extracting and distilling water from frozen regolith simulant. Nomenclature C-Type = Carbonaceous Asteroid EML = Earth-Moon Lagrange Point ESL = Earth-Sun Lagrange Point IPV = Interplanetary Vehicle M-Type = Metallic Asteroid NEA = Near Earth Asteroid NEO = Near Earth Object PGM = Platinum Group Metal STP = Solar Thermal Propulsion S-Type = Stony Asteroid I.
    [Show full text]
  • Asteroid Impact Mission (AIM)
    Asteroid Impact Mission (AIM) Andrés Gálvez, ESA HQ, Paris, France Ian Carnelli, ESA HQ, Paris, France Carlos Corral, ESTEC, Noordwijk, The Netherlands & the AIDA team (JHU/APL, NASA, OCA. DLR) NEO mission studies in ESA Near-Earth Objects (NEOs); impact probability is very low but effects can be extremely severe ; ESA addresses risk assessment and works with data users, but these users also need missions There is still very limited practical knowledge on the best technology approach to tackle NEO impact threats. NASA/JHU ESA Don Quijote study . After ESA’s Mission Advisory Panel recommendation, ESA studied Don Quijote asteroid mission . Two launches . Interceptor . Rendezvous . Not affordable techno demonstration for ESA 5/29/2012 3 AIDA Background . The Double Asteroid Redirection Test (DART) study undertaken by APL in 2011-2012 with participation of NASA NASA HQ, GSFC, JSC, LaRC, JPL Asteroid impact and deflection, . The Asteroid Impact Mission (AIM) study undertaken by ESA in 2012 with OCA, DLR Impact test and characterization 5/29/2012 4 The AIDA concept . AIDA will send two spacecraft to the binary asteroid 65803 Didymos Asteroid impactor Asteroid rendezvous . Each AIDA component is independent and has unique value AIDA = AIM + DART 5/29/2012 5 Target: Didymos Didymos Spectral type Xk Primary rotation 2.26 hr Binary orbit period 11.91 hr Binary orbit semi-major axis 1.05 km Primary diameter 800 m Secondary diameter 150 m Magnitude H 18 Pole Solutions (λ,β) = (157°,19°); (329°,-70°) Heliocentric Orbit . Spacecraft impact (in Eccentricity 0.384 2022) will change Inclination 3.41° mutual orbit of binary Semi-major axis 1.645 AU .
    [Show full text]
  • Espinsights the Global Space Activity Monitor
    ESPInsights The Global Space Activity Monitor Issue 1 January–April 2019 CONTENTS SPACE POLICY AND PROGRAMMES .................................................................................... 1 Focus .................................................................................................................... 1 Europe ................................................................................................................... 4 11TH European Space Policy Conference ......................................................................... 4 EU programmatic roadmap: towards a comprehensive Regulation of the European Space Programme 4 EDA GOVSATCOM GSC demo project ............................................................................. 5 Programme Advancements: Copernicus, Galileo, ExoMars ................................................... 5 European Space Agency: partnerships continue to flourish................................................... 6 Renewed support for European space SMEs and training ..................................................... 7 UK Space Agency leverages COMPASS project for international cooperation .............................. 7 France multiplies international cooperation .................................................................... 7 Italy’s PRISMA pride ................................................................................................ 8 Establishment of the Portuguese Space Agency: Data is King ................................................ 8 Belgium and Luxembourg
    [Show full text]
  • A Mobile Asteroid Surface Scout for the AIDA Mission
    Geophysical Research Abstracts Vol. 18, EGU2016-16163, 2016 EGU General Assembly 2016 © Author(s) 2016. CC Attribution 3.0 License. A Mobile Asteroid Surface Scout for the AIDA Mission Tra Mi Ho (1), Caroline Lange (1), Christian Grimm (1), Jan Thimo Grundmann (1), Johannes Rößler (1), Silvio Schröder (1), Thomas Skoczylas (1), Christian Ziach (1), Jens Biele (2), Barbara Cozzoni (2), Christian Krause (2), Oliver Küchemann (2), Michael Maibaum (2), Stephan Ulamec (2), Michael Lange (3), Olaf Mierheim (3), Maximilian Maier (4), Alain Herique (5), and Mascot Study Team () (1) DLR RY, Bremen, Germany, (2) DLR MUSC, Cologne, Germany, (3) DLR FA, Braunschweig, Germany, (4) DLR RM, Oberpfaffenhofen, Germany, (5) IPAG UJF/CNRS, Grenoble, France The Asteroid Impact Deflection, AIDA, mission is composed of a kinetic impactor, DART and an observer, the Asteroid Impact Monitor, AIM, carrying among other payload a surface package, MASCOT2 (MSC2). Its proposed concept is based on the MASCOT lander onboard the HAYABUSA2 Mission (JAXA) to near-Earth asteroid (162173) Ryugu. MASCOT is a compact platform (‘shoe box size’) carrying a suite of 4 scientific instruments and has a landed mass of ∼10kg. Equipped with a mobility mechanism, the MASCOT lander is able to upright and relocate on the targeted asteroid; thus providing in-situ data at more than one site. In the context of the AIDA Mission, the MASCOT2 lander would be carried by the AIM spacecraft and delivered onto Didymoon, the secondary object in the (65803) Didymos binary near-Earth asteroid system. Since the mission objectives of the AIM mission within the joint AIDA mission concept differ from JAXA’s sample return mission HAYABUSA2, several design changes need to be studied and implemented.
    [Show full text]
  • BOULDERS on ASTEROIDS DIDYMOS and DIMORPHOS: FUTURE DART-Liciacube OBSERVATIONS
    52nd Lunar and Planetary Science Conference 2021 (LPI Contrib. No. 2548) 1116.pdf BOULDERS ON ASTEROIDS DIDYMOS AND DIMORPHOS: FUTURE DART-LICIACube OBSERVATIONS M. Pajola1, A. Lucchetti1, S. Ivanovski2, G. Poggiali3,4, S. Ieva5, D. Perna5, E. Dotto5, V. Della Corte6, G. Cremonese1, M. Amoroso7, S. Pirrotta7, E. Mazzotta Epifani5, A. Cheng8, N. Chabot8, A. Rivkin8, O. Barnouin8, C. Ernst8, R.T. Daly8, M. Hirabayashi9, E. Asphaug10, S.R. Schwartz10, J.M. Trigo-Rodriguez11, E.G. Fahnestock12, P. Michel13, I. Bertini14, J.R. Brucato3, A. Capannolo15, B. Cotugno16, V. Di Tana16, I. Gai17, G. Impresario7, M. Lavagna15, A. Meneghin3, F. Miglioretti16, D. Modenini17, P. Palumbo14,6, A. Rossi18, E. Simioni1, S. Simonetti16, P. Tortora17, M. Zannoni17, G. Zanotti15, A. Zinzi19,7. 1INAF-Astronomical Observatory of Padova, Vic. Osservatorio 5, 35122 Padova, Italy ([email protected]); 2INAF Osservatorio Astronomico di Trieste, Trieste, Italy; 3INAF Osservatorio Astrofisico di Arcetri, Firenze, Italy; 4Università di Firenze, Dipartimento di Fisica e Astronomia, Sesto Fiorentino (Firenze), Italy; 5INAF Osservatorio Astronomico di Roma, Monte Porzio Catone (Roma), Italy; 6INAF Istituto di Astrofisica e Planetologia Spaziali, Roma, Italy; 7Agenzia Spaziale Italiana, via del Politecnico, 00133 Roma, Italy; 8Johns Hopkins University Applied Physics Laboratory, Laurel, MD-USA; 9Auburn University, Auburn, AL-USA; 10Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ-USA; 11Institute of Space Sciences (IEEC-CSIC), Dept. of Astrophysics,
    [Show full text]