An Innovative Solution to Nasa's Neo Impact Threat
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On the Rotation Rates and Axis Ratios of the Smallest Known Near-Earth
On the rotation rates and axis ratios of the smallest known near-Earth asteroids—the archetypes of the Asteroid Redirect Mission targets Patrick Hatcha, Paul A. Wiegerta,b,∗ aDepartment of Physics and Astronomy, The University of Western Ontario, London, N6A 3K7 CANADA bCentre for Planetary Science and Exploration, The University of Western Ontario, London, N6A 3K7 CANADA Abstract NASA’s Asteroid Redirect Mission (ARM) has been proposed with the aim to capture a small asteroid a few meters in size and redirect it into an orbit around the Moon. There it can be investigated at leisure by astronauts aboard an Orion or other spacecraft. The target for the mission has not yet been selected, and there are very few potential targets currently known. Though sufficiently small near-Earth asteroids (NEAs) are thought to be numerous, they are also difficult to detect and characterize with current observational facilities. Here we collect the most up-to-date information on near-Earth asteroids in this size range to outline the state of understanding of the properties of these small NEAs. Observational biases certainly mean that our sample is not an ideal representation of the true population of small NEAs. However our sample is representative of the eventual target list for the ARM mission, which will be compiled under very similar observational constraints unless dramatic changes are made to the way near-Earth asteroids are searched for and studied. We collect here information on 88 near-Earth asteroids with diameters less than 60 meters and with high quality light curves. We find that the typical rotation period is 40 minutes. -
The Orbital Evolution of Asteroid 367943 Duende (2012 Da14) Under Yarkovsky Effect Influence and Its Implications for Collision with the Earth
Journal of Engineering Science and Technology Special Issue on AASEC’2016, October (2017) 42 - 52 © School of Engineering, Taylor’s University THE ORBITAL EVOLUTION OF ASTEROID 367943 DUENDE (2012 DA14) UNDER YARKOVSKY EFFECT INFLUENCE AND ITS IMPLICATIONS FOR COLLISION WITH THE EARTH JUDHISTIRA ARIA UTAMA1,2,*, TAUFIQ HIDAYAT3, UMAR FAUZI4 1Astronomy Post Graduate Study Program, Institut Teknologi Bandung, Jl. Ganesha 10, Bandung 40132, Indonesia 2Physics Education Department, Universitas Pendidikan Indonesia, Jl. Dr. Setiabudhi 229, Bandung, 40154, Indonesia 3Astronomy Research Division, Institut Teknologi Bandung, Jl. Ganesha 10, Bandung 40132, Indonesia 4Geophysics & Complex System Research Division, Institut Teknologi Bandung, Jl. Ganesha 10, Bandung 40132, Indonesia *Corresponding Author: [email protected] Abstract Asteroid 367943 Duende (2012 DA14) holds the record as the one of Aten subpopulation with H 24 that had experienced deep close encounter event to the Earth (0.09x Earth-Moon distance) as informed in NASA website. In this work, we studied the orbital evolution of 120 asteroid clones and the nominal up to 5 Megayears (Myr) in the future using Swift integrator package with and without the Yarkovsky effect inclusion. At the end of orbital integration with both integrators, we found as many as 17 asteroid clones end their lives as Earth impactor. The prediction of maximum semimajor axis drift for this subkilometer-sized asteroid from diurnal and seasonal variants of Yarkovsky effect was 9.0×10-3 AU/Myr and 2.6×10-4 AU/Myr, respectively. By using the MOID (Minimum Orbital Intersection Distance) data set calculated from our integrators of entire clones and nominal asteroids, we obtained the value of impact rate with the Earth of 2.35×10-7 per year (with Yarkovsky effect) and 2.37×10-7 per year (without Yarkovsky effect), which corresponds to a mean lifetime of 4.25 Myr and 4.22 Myr, respectively. -
1950 Da, 205, 269 1979 Va, 230 1991 Ry16, 183 1992 Kd, 61 1992
Cambridge University Press 978-1-107-09684-4 — Asteroids Thomas H. Burbine Index More Information 356 Index 1950 DA, 205, 269 single scattering, 142, 143, 144, 145 1979 VA, 230 visual Bond, 7 1991 RY16, 183 visual geometric, 7, 27, 28, 163, 185, 189, 190, 1992 KD, 61 191, 192, 192, 253 1992 QB1, 233, 234 Alexandra, 59 1993 FW, 234 altitude, 49 1994 JR1, 239, 275 Alvarez, Luis, 258 1999 JU3, 61 Alvarez, Walter, 258 1999 RL95, 183 amino acid, 81 1999 RQ36, 61 ammonia, 223, 301 2000 DP107, 274, 304 amoeboid olivine aggregate, 83 2000 GD65, 205 Amor, 251 2001 QR322, 232 Amor group, 251 2003 EH1, 107 Anacostia, 179 2007 PA8, 207 Anand, Viswanathan, 62 2008 TC3, 264, 265 Angelina, 175 2010 JL88, 205 angrite, 87, 101, 110, 126, 168 2010 TK7, 231 Annefrank, 274, 275, 289 2011 QF99, 232 Antarctic Search for Meteorites (ANSMET), 71 2012 DA14, 108 Antarctica, 69–71 2012 VP113, 233, 244 aphelion, 30, 251 2013 TX68, 64 APL, 275, 292 2014 AA, 264, 265 Apohele group, 251 2014 RC, 205 Apollo, 179, 180, 251 Apollo group, 230, 251 absorption band, 135–6, 137–40, 145–50, Apollo mission, 129, 262, 299 163, 184 Apophis, 20, 269, 270 acapulcoite/ lodranite, 87, 90, 103, 110, 168, 285 Aquitania, 179 Achilles, 232 Arecibo Observatory, 206 achondrite, 84, 86, 116, 187 Aristarchus, 29 primitive, 84, 86, 103–4, 287 Asporina, 177 Adamcarolla, 62 asteroid chronology function, 262 Adeona family, 198 Asteroid Zoo, 54 Aeternitas, 177 Astraea, 53 Agnia family, 170, 198 Astronautica, 61 AKARI satellite, 192 Aten, 251 alabandite, 76, 101 Aten group, 251 Alauda family, 198 Atira, 251 albedo, 7, 21, 27, 185–6 Atira group, 251 Bond, 7, 8, 9, 28, 189 atmosphere, 1, 3, 8, 43, 66, 68, 265 geometric, 7 A- type, 163, 165, 167, 169, 170, 177–8, 192 356 © in this web service Cambridge University Press www.cambridge.org Cambridge University Press 978-1-107-09684-4 — Asteroids Thomas H. -
Hered in These Proceedings with the Aim to Keep Track of These Very Interesting Days
Proceedings of GAIA-FUN-SSO 2014 Third “Gaia Follow-up Network for Solar System Objects” Workshop held at IMCCE/Paris Observatory 2014, November 24 – 26 Institut de mécanique céleste et de calcul des éphémérides Observatoire de Paris Legal Deposite – June 2015 ISBN 2-910015-73-4 Foreword The observation of Solar System Objects (SSO) by the Gaia space astrometry mission will be constrained by a scanning law. Much detection of interesting objects may occur with no possibility of further observations by the probe. These objects will then require complementary ground-based observations. Among them, previously unknown Near- Earth Objects, fast moving towards the Earth or going away from it could be found. Several objects discovered by Gaia could also be Inner-Earth Objects, as the probe will observe at rather low Solar elongations. In order to confirm from the ground the discoveries made in space and to follow interesting targets, a dedicated network is organized, the Gaia Follow-Up Network. This task is performed in the frame of the Coordination Unit 4 of the Gaia Data Processing and Analysis Consortium (DPAC), devoted to data processing of specific objects. The goal of the network is to improve the knowledge of the orbit of poorly observed targets by astrometric observations on alert. This activity is coordinated by a central node interacting with the Gaia data reduction pipeline all along the mission. In 2010 and 2012, we had organized the first two workshops in order to initiate the network and to meet the participants. In 2014, almost one year after the launch of Gaia, we organize the third Gaia-FUN-SSO workshop in Paris in order to discuss further the coordination of the network of observing stations, to discuss the prelaunch training observations which have been performed and to prepare the network for the operating phase of the alert mode which must begin in 2015. -
Astrometry and Spectra Classification of Near Earth Asteroids with Lijiang
Astronomy and Astrophysics in the Gaia sky Proceedings IAU Symposium No. 330, 2017 A. Recio-Blanco, P. de Laverny, A.G.A. Brown c International Astronomical Union 2018 & T. Prusti, eds. doi:10.1017/S174392131700624X Astrometry and Spectra Classification of Near Earth Asteroids with Lijiang 2.4m Telescope† X. L. Zhang1,2,B.Yang1,2, and J. M. Bai1,2 1 Yunnan Observatories, Chinese Academy of Sciences, Kunming 650011, China email: [email protected] 2 Key Laboratory of the Structure and Evolution of Celestial Objects, Chinese Academy of Sciences, Kunming 650011, China Abstract. The Lijiang 2.4m telescope of Yunnan Observatories is located at longitude E100◦0151, latitude N26◦4232 and height 3250m above sea level (IAU code O44). Because of low latitude of the site, long-focus system and planetary tracking mode of telescope, high accuracy posi- tioning and spectral classification of the near Earth objects (NEAs) especially in the Southern Hemisphere can be studied with the Lijiang 2.4m telescope. As a set of observational campaigns organized by the GAIA-FUN-SSO, astrometry of several near Earth asteroids including (367943) Duende and (99942) Apophis were made with Lijiang 2.4m telescope during 2013. From Decem- ber 12, 2015, spectra of three near earth asteroids were also observed with the YFOSC terminal attached to the Lijiang 2.4m telescope. This paper will give the detailed introduction of Lijiaing 2.4m telescope and observational results of near Earth asteroids obtained with it. Keywords. methods: observational, techniques: astrometry, spectrum classification. 1. Introduction Knowledge of asteroids and comets, the relic of planet building blocks, directly sheds light on the formation of terrestrial planets, and the origin and evolution of the Solar System. -
E a R Th» »Moon Moon: Earth: Surface Area Earth » L E N Gth of Equat
k k k 363 384 405 . E EARth-MOON DISTANCE (km) V A MIN. MIN. 0 200 400 600 800 km MAX. SEA OF HUMBOLDT MARE HUMBOLDTIANUM SEA OF COLD MARE FRIGORIS PLATO CE3 G. BRUNO L1 SEA OF SHOWERS MARE IMBRIUM L2 A15 L21 SEA OF SERENITY ARISTARCHUS MARE SERENITATIS JAckSON L13 A17 SEA OF MUSCOVY ENNINUS SEA OF CRISES MARE MOSCOVIENSE MARE CRISIUM L24 MONTES Ap KEPLER SEA OF TRANQUILITY L4 COPERNICUS MARE TRANQUILLITATIS L20 OCEAN OF STORMS S5 R8 OCEANUS PROCELLARUM S4/6 1° CE1 L15 1° S1 0° 0° S3 L-1° L-1° A12 0° A14 -1° A11 +1° 179° 180° SEA OF FECUNDITY -179° HERTZSPRUNG MARE FECUNDITATIS A16 KOROLEV R7 LANGRENUS GRIMALDI R9 SEA OF NECTAR MARE NECTARIS SEA OF CLOUDS SEA MARE NUBIUM OF MOISTURE EASTERN SEA MARE HUMORUM MARE ORIENTALE S7 APOLLO TYCHO SOUTH POLE–AITKEN BASIN V E R A G E + A 16 °C H » T DENSITY R LUNa–2 A g/m3 8001 : 10 000. 1 cm km. ≈ 108 SURFACE TemPERATURE E MOON EARTH ScHRÖDINGER LP Lambert Azimuthal Equal Area Projection. A AMERICAN MANNED SPACECRAFTS . V E OON R A: Apollo E E M A E A G R R TH E T F - O 18 U H AMERICAN SPACE PROBES P °C A Commission on Planetary Cartography. Published by Eötvös Loránd University, Budapest. Text © Henrik Hargitai 2014. http://childrensmaps.wordpress.com. M Editor: Henrik Hargitai. Illustration:Europlanet 2012 OutreachLászló FundingHerbszt. Scheme,Technical Paris Observatory,review: InternationalJim Zimbelman. CartographicISBN 978-963-284-423-7, ISBN 978-963-284-422-0 Illustration [PDF]. -
An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand
Final Technical Report of a NIAC Phase 2 Study December 9, 2014 NASA Grant and Cooperative Agreement Number: NNX12AQ60G NIAC Phase 2 Study Period: 09/10/2012 – 09/09/2014 An Innovative Solution to NASA’s NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development PI: Dr. Bong Wie, Vance Coffman Endowed Chair Professor Asteroid Deflection Research Center Department of Aerospace Engineering Iowa State University, Ames, IA 50011 email: [email protected] (515) 294-3124 Co-I: Brent Barbee, Flight Dynamics Engineer Navigation and Mission Design Branch (Code 595) NASA Goddard Space Flight Center Greenbelt, MD 20771 email: [email protected] (301) 286-1837 Graduate Research Assistants: Alan Pitz (M.S. 2012), Brian Kaplinger (Ph.D. 2013), Matt Hawkins (Ph.D. 2013), Tim Winkler (M.S. 2013), Pavithra Premaratne (M.S. 2014), Sam Wagner (Ph.D. 2014), George Vardaxis, Joshua Lyzhoft, and Ben Zimmerman NIAC Program Executive: Dr. John (Jay) Falker NIAC Program Manager: Jason Derleth NIAC Senior Science Advisor: Dr. Ronald Turner NIAC Strategic Partnerships Manager: Katherine Reilly Contents 1 Hypervelocity Asteroid Intercept Vehicle (HAIV) Mission Concept 2 1.1 Introduction ...................................... 2 1.2 Overview of the HAIV Mission Concept ....................... 6 1.3 Enabling Space Technologies for the HAIV Mission . 12 1.3.1 Two-Body HAIV Configuration Design Tradeoffs . 12 1.3.2 Terminal Guidance Sensors/Algorithms . 13 1.3.3 Thermal Protection and Shield Issues . 14 1.3.4 Nuclear Fuzing Mechanisms ......................... 15 2 Planetary Defense Flight Validation (PDFV) Mission Design 17 2.1 The Need for a PDFV Mission ............................ 17 2.2 Preliminary PDFV Mission Design by the MDL of NASA GSFC . -
Observational Investigation of the 2013 Near-Earth Encounter By
Observational Investigation of the 2013 Near-Earth Encounter by Asteroid (367943) Duende Nicholas A. Moskovitz a, Conor James Benson b, Daniel Scheeres b, Thomas Endicott c, David Polishook d, Richard Binzel e, Francesca DeMeo e, William Ryan f, Eileen Ryan f, Mark Willman g, Carl Hergenrother h, Arie Verveer i, Tim Lister j, Peter Birtwhistle k, Amanda Sickafoose `;e;o, Takahiro Nagayama m, Alan Gilmore n, Pam Kilmartin n, Susan Bennechi o, Scott Sheppard p, Franck Marchis q, Thomas Augusteijn r, Olesja Smirnova r aLowell Observatory, 1400 West Mars Hill Road, Flagstaff, AZ 86001 (U.S.A) bUniversity of Colorado Boulder, Boulder, CO 80305 cUniversity of Massachusetts Boston, Boston, MA 02125 dWeizmann Institute of Science, 234 Herzl St. Rehovot 7610001, Israel arXiv:1911.00609v1 [astro-ph.EP] 1 Nov 2019 eMassachusetts Institute of Technology, EAPS, Cambridge, MA 02139 f New Mexico Institute of Mining and Technology, Socorro, NM 87801 gInstitute for Astronomy, University of Hawaii, Hilo, HI 96720 hUniversity of Arizona, LPL, Tucson, AZ 85721 iPerth Observatory, Bickley, WA 6076 (Australia) Preprint submitted to Icarus 5 November 2019 jLas Cumbres Observatory Global Telescope Network, Goleta, CA 93117 kGreat Shefford Observatory, Berkshire (England) `South African Astronomical Observatory (South Africa) mKagoshima University (Japan) nUniversity of Canterbury, Mt John University Observatory, Lake Tekapo (New Zealand) oPlanetary Science Institute, 1700 E. Fort Lowell Rd., Tucson, AZ 85719 pDepartment of Terrestrial Magnetism, Carnegie Institution for Science, Washington, DC 20015 qSETI Institute, Carl Sagan Center, 189 Bernardo Ave., Mountain View CA 94043 rNordic Optical Telescope, La Palma (Spain) Copyright c 2019 Nicholas A. Moskovitz Number of pages: 50 Number of tables: 5 Number of figures: 12 2 Proposed Running Head: The 2013 Near-Earth Encounter of Asteroid Duende Please send Editorial Correspondence to: Nicholas A. -
Hidden Planetary Friends: on the Stability of 2-Planet Systems in The
DRAFT VERSION FEBRUARY 5, 2018 Preprint typeset using LATEX style emulateapj v. 12/16/11 HIDDEN PLANETARY FRIENDS: ON THE STABILITY OF 2-PLANET SYSTEMS IN THE PRESENCE OF A DISTANT, INCLINED COMPANION ; PAUL DENHAM1,SMADAR NAOZ1 2,BAO-MINH HOANG1,ALEXANDER P. STEPHAN1,WILL M. FARR3 1Physics and Astronomy Department, University of California, Los Angeles, CA 90024 2Mani L. Bhaumik Institute for Theoretical Physics, Department of Physics and Astronomy, UCLA, Los Angeles, CA 90095, USA and 3School of Physics and Astronomy, University of Birmingham, Birmingham, B15 2TT, UK Draft version February 5, 2018 ABSTRACT Recent observational campaigns have shown that multi-planet systems seem to be abundant in our Galaxy. Moreover, it seems that these systems might have distant companions, either planets, brown-dwarfs or other stellar objects. These companions might be inclined with respect to the inner planets, and could potentially excite the eccentricities of the inner planets through the Eccentric Kozai-Lidov mechanism. These eccentricity excitations could perhaps cause the inner orbits to cross, disrupting the inner system. We study the stability of two-planet systems in the presence of a distant, inclined, giant planet. Specifically, we derive a stability criterion, which depends on the companion’s separation and eccentricity. We show that our analytic criterion agrees with the results obtained from numerically integrating an ensemble of systems. Finally, as a potential proof-of-concept, we provide a set of predictions for the parameter space that allows the existence of planetary companions for the Kepler-56, Kepler-448, Kepler-88, Kepler-109, and Kepler-36 systems. 1. -
Planetary Defense
NIAC (NASA Innovative Advanced Concepts) Phase 2 Study (2012 – 2014) An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development Bong Wie (PI) Asteroid Deflection Research Center Iowa State University Brent Barbee (Co-I) NASA Goddard Space Flight Center Graduate Students: Alan Pitz, Brian Kaplinger, Matt Hawkins, Tim Winkler, Pavithra Premaratne, George Vardaxis, Joshua Lyzhoft, Ben Zimmerman Asteroid Deflection Research Center Presented at NASA SBAG Meeting, January 6-7, 2015 Asteroid Deflection IOWA STATE UNIVERSITY 1 Research Center 2006 NEO Report by NASA 2010 NEO Report by NRC Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 2 Research Center 2006 NEO Report by NASA 2010 NEO Report by NRC Sufficient Warning Time for Deflection Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 3 Research Center Study Justification (1/2) 17 m (diameter) An Airburst of 17-m Chelyabinsk 10,000 tons Meteor on Feb. 15, 2013 18.6 km/s impact 440 kt of TNT (30 Hiroshima bombs) Airburst @23.3 km 1,500 people were injured; 7,200 buildings damaged What if it were a 17 m nickel-iron meteorite? Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 4 Research Center Study Justification (2/2) • Asteroid 2012 DA14 (367943 Duende), discovered on Feb. 23, 2012, had a close encounter with Earth (27,700-km near-miss) on Feb. 15, 2013. • What if the 30-m DA14 were predicted to collide with Earth with its impact damage of 150 Hiroshima nuclear bombs (or 2.3 Mt of TNT)? Asteroid Deflection Research Center IOWA STATE UNIVERSITY Asteroid Deflection 5 Research Center Study Justification (2/2) • Asteroid 2012 DA14 (367943 Duende), discovered on Feb. -
A Paucity of Proto-Hot Jupiters on Super-Eccentric Orbits
Submitted to ApJ on October 26th, 2012. Accepted on October 20th, 2014. Preprint typeset using LATEX style emulateapj v. 5/2/11 THE PHOTOECCENTRIC EFFECT AND PROTO-HOT JUPITERS III: A PAUCITY OF PROTO-HOT JUPITERS ON SUPER-ECCENTRIC ORBITS Rebekah I. Dawson1,2,3,7, Ruth A. Murray-Clay3,4, and John Asher Johnson3,5,6 Submitted to ApJ on October 26th, 2012. Accepted on October 20th, 2014. ABSTRACT Gas giant planets orbiting within 0.1 AU of their host stars, unlikely to have formed in situ, are evidence for planetary migration. It is debated whether the typical hot Jupiter smoothly migrated inward from its formation location through the proto-planetary disk or was perturbed by another body onto a highly eccentric orbit, which tidal dissipation subsequently shrank and circularized during close stellar passages. Socrates and collaborators predicted that the latter class of model should produce a population of super-eccentric proto-hot Jupiters readily observable by Kepler. We find a paucity of such planets in the Kepler sample, inconsistent with the theoretical prediction with 96.9% confidence. Observational effects are unlikely to explain this discrepancy. We find that the fraction of hot Jupiters with orbital period P > 3 days produced by the star-planet Kozai mechanism does not exceed (at two-sigma) 44%. Our results may indicate that disk migration is the dominant channel for producing hot Jupiters with P > 3 days. Alternatively, the typical hot Jupiter may have been perturbed to a high eccentricity by interactions with a planetary rather than stellar companion and began tidal circularization much interior to 1 AU after multiple scatterings. -
Jjmonl 1602 A.Pmd
alactic Observer GJohn J. McCarthy Observatory Volume 9, No. 2 February 2016 Armageddon A galaxy in a cosmic death spiral. See inside, page 23 The John J. McCarthy Observatory Galactic Observvvererer New Milford High School Editorial Committee 388 Danbury Road Managing Editor New Milford, CT 06776 Bill Cloutier Phone/Voice: (860) 210-4117 Production & Design Phone/Fax: (860) 354-1595 www.mccarthyobservatory.org Allan Ostergren Website Development JJMO Staff Marc Polansky It is through their efforts that the McCarthy Observatory Technical Support has established itself as a significant educational and Bob Lambert recreational resource within the western Connecticut Dr. Parker Moreland community. Steve Barone Jim Johnstone Colin Campbell Carly KleinStern Dennis Cartolano Bob Lambert Mike Chiarella Roger Moore Route Jeff Chodak Parker Moreland, PhD Bill Cloutier Allan Ostergren Cecilia Detrich Marc Polansky Dirk Feather Joe Privitera Randy Fender Monty Robson Randy Finden Don Ross John Gebauer Gene Schilling Elaine Green Katie Shusdock Tina Hartzell Paul Woodell Tom Heydenburg Amy Ziffer In This Issue OUT THE WINDOW ON YOUR LEFT .................................... 4 SOVIET MOON PROGRAM ............................................... 17 LUNAR EXPLORATION ...................................................... 6 JUPITER AND ITS MOONS ................................................. 18 LRO EARTHRISE ........................................................... 7 TRANSIT OF THE JUPITER'S RED SPOT ............................... 18 NEUTRINOS ...................................................................