Hidden Planetary Friends: on the Stability of 2-Planet Systems in The
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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. -
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. -
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 . -
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. -
September 2014
September 2014 1 September 2014 Vol. 45, No. 9 The Warren Astronomical Society President: Jonathan Kade [email protected] Founded: 1961 First Vice President: Dale Partin [email protected] Second Vice President: Joe Tocco [email protected] P.O. BOX 1505 Treasurer: Dale Thieme [email protected] Secretary: Chuck Dezelah [email protected] WARREN, MICHIGAN 48090-1505 Publications: Bob Trembley [email protected] Outreach: Angelo DiDonato [email protected] http://www.warrenastro.org Entire Board [email protected] The Cassini Saturn mission has gotten funding for an extended mission through 2017. The Cassini mission was the highest- rated mission of the seven being considered for extended- mission funding. After a four year journey, Cassini arrived at Saturn on 1 July 2004, passing through the gap between the F and G rings. On 25 December 2004, the Huygens lander separated from Cassini, and touched down on Saturn’s large moon Titan on 14 January 2005. Cassini has returned thousands of awe-inspiring images, and the Credit NASA/JPL—Caltech scientific data returned from the mission would fill volumes. All good things must come to an end—the same applies to Cassini. The current end-of-mission plan is to put Cassini in an orbit that will take it between Saturn’s cloud tops, and the innermost D ring; The images returned from this position should be spectacular! Eventually, Cassini will fly low enough that it will burn up in Saturn’s atmosphere. What a bittersweet day that will be… Read Emily Lakdawalla’s blog post about Cassini’s extened mission at the Planetary Society website: http:// www.planetary.org/blogs/emily-lakdawalla/2014/cassinis- awesomeness-fully.html I would really like to see a similar orbiter missions sent to both Uranus and Neptune; some of the new ion-propulsion technologies being developed may be ideal for such missions. -
Survival of Exomoons Around Exoplanets 2
Survival of exomoons around exoplanets V. Dobos1,2,3, S. Charnoz4,A.Pal´ 2, A. Roque-Bernard4 and Gy. M. Szabo´ 3,5 1 Kapteyn Astronomical Institute, University of Groningen, 9747 AD, Landleven 12, Groningen, The Netherlands 2 Konkoly Thege Mikl´os Astronomical Institute, Research Centre for Astronomy and Earth Sciences, E¨otv¨os Lor´and Research Network (ELKH), 1121, Konkoly Thege Mikl´os ´ut 15-17, Budapest, Hungary 3 MTA-ELTE Exoplanet Research Group, 9700, Szent Imre h. u. 112, Szombathely, Hungary 4 Universit´ede Paris, Institut de Physique du Globe de Paris, CNRS, F-75005 Paris, France 5 ELTE E¨otv¨os Lor´and University, Gothard Astrophysical Observatory, Szombathely, Szent Imre h. u. 112, Hungary E-mail: [email protected] January 2020 Abstract. Despite numerous attempts, no exomoon has firmly been confirmed to date. New missions like CHEOPS aim to characterize previously detected exoplanets, and potentially to discover exomoons. In order to optimize search strategies, we need to determine those planets which are the most likely to host moons. We investigate the tidal evolution of hypothetical moon orbits in systems consisting of a star, one planet and one test moon. We study a few specific cases with ten billion years integration time where the evolution of moon orbits follows one of these three scenarios: (1) “locking”, in which the moon has a stable orbit on a long time scale (& 109 years); (2) “escape scenario” where the moon leaves the planet’s gravitational domain; and (3) “disruption scenario”, in which the moon migrates inwards until it reaches the Roche lobe and becomes disrupted by strong tidal forces. -
Number Worked As Current Name Vol-Num Pg # Authors 1 Ceres 42-2 94 Melillo, F
The "Worked As" column gives the name/designation used in the original article. If the object was subsequently named, the "Current Name" column gives the name currently in the MPCORB file. The page number gives the first page of the article in which the object appears. Only those references that include lightcurves, other photometric data, and/or shape/spin axis models are included. Number Worked As Current Name Vol-Num Pg # Authors 1 Ceres 42-2 94 Melillo, F. J. 2 Pallas 35-2 63 Higley, S. et al. (Shape/Spin Models) 5 Astraea 35-2 63 Higley, S. et al. (Shape/Spin Models) 8 Flora 36-4 133 Pilcher, F. 9 Metis 36-3 98 Timerson, B. et al. 10 Hygiea 47-2 133 Picher, F. 10 Hygiea 48-2 166 Ferrais, M. et al. 11 Parthenope 37-3 119 Pilcher, F. 11 Parthenope 38-4 183 Pilcher, F. 12 Victoria 40-3 161 Pilcher, F. 12 Victoria 42-2 94 Melillo, F. J. 13 Egeria 36-4 133 Pilcher, F. 14 Irene 36-4 133 Pilcher, F. 14 Irene 39-3 179 Aymani, J.M. 16 Psyche 38-4 200 Timerson, B. et al. 16 Psyche 43-2 137 Warner, B. D. 17 Thetis 34-4 113 Warner, B.D. (H-G, Color Index) 18 Melpomene 40-1 33 Pilcher, F. 18 Melpomene 41-3 155 Pilcher, F. 19 Fortuna 36-3 98 Timerson, B. et al. 22 Kalliope 30-2 27 Trigo-Rodriguez, J.M. 22 Kalliope 34-3 53 Gungor, C. 22 Kalliope 34-3 56 Alton, K.B. -
Abstract-Less Paper #3
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. S TEPHAN1,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. -
The Astronomer Magazine Index
The Astronomer Magazine Index The numbers in brackets indicate approx lengths in pages (quarto to 1982 Aug, A4 afterwards) 1964 May p1-2 (1.5) Editorial (Function of CA) p2 (0.3) Retrospective meeting after 2 issues : planned date p3 (1.0) Solar Observations . James Muirden , John Larard p4 (0.9) Domes on the Mare Tranquillitatis . Colin Pither p5 (1.1) Graze Occultation of ZC620 on 1964 Feb 20 . Ken Stocker p6-8 (2.1) Artificial Satellite magnitude estimates : Jan-Apr . Russell Eberst p8-9 (1.0) Notes on Double Stars, Nebulae & Clusters . John Larard & James Muirden p9 (0.1) Venus at half phase . P B Withers p9 (0.1) Observations of Echo I, Echo II and Mercury . John Larard p10 (1.0) Note on the first issue 1964 Jun p1-2 (2.0) Editorial (Poor initial response, Magazine name comments) p3-4 (1.2) Jupiter Observations . Alan Heath p4-5 (1.0) Venus Observations . Alan Heath , Colin Pither p5 (0.7) Remarks on some observations of Venus . Colin Pither p5-6 (0.6) Atlas Coeli corrections (5 stars) . George Alcock p6 (0.6) Telescopic Meteors . George Alcock p7 (0.6) Solar Observations . John Larard p7 (0.3) R Pegasi Observations . John Larard p8 (1.0) Notes on Clusters & Double Stars . John Larard p9 (0.1) LQ Herculis bright . George Alcock p10 (0.1) Observations of 2 fireballs . John Larard 1964 Jly p2 (0.6) List of Members, Associates & Affiliations p3-4 (1.1) Editorial (Need for more members) p4 (0.2) Summary of June 19 meeting p4 (0.5) Exploding Fireball of 1963 Sep 12/13 . -
An Innovative Solution to Nasa's Neo Impact Threat
4th IAA Planetary Defense Conference – PDC 2015 13-17 April 2015, Frascati, Roma, Italy IAA-PDC-15-04-10 AN INNOVATIVE SOLUTION TO NASA’S NEO IMPACT THREAT MITIGATION GRAND CHALLENGE AND FLIGHT VALIDATION MISSION ARCHITECTURE DEVELOPMENT1 Bong Wie(1) and Brent W. Barbee(2) (1)Asteroid Deflection Research Center, Iowa State University, Ames, IA 50011, USA (515) 294-3124, [email protected] (2)NASA Goddard Space Flight Center Greenbelt, MD 20771, USA (301) 286-1837, [email protected] Keywords: NEO impact threat mitigation, nuclear subsurface explosions, hypervelocity asteroid intercept vehicle (HAIV) Abstract This paper presents the results of a NASA Innovative Advanced Concept (NIAC) Phase 2 study entitled “An Innovative Solution to NASA’s Near-Earth Object (NEO) Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development.” This NIAC Phase 2 study was con- ducted at the Asteroid Deflection Research Center (ADRC) of Iowa State University in 2012–2014. The study objective was to develop an innovative yet practically implementable mitigation strategy for the most probable impact threat of an asteroid or comet with short warning time (< 5 years). The mitigation strategy described in this paper is intended to optimally reduce the severity and catastrophic damage of the NEO impact event, especially when we don’t have sufficient warning times for non-disruptive deflec- tion of a hazardous NEO. This paper provides an executive summary of the NIAC Phase 2 study results. Detailed technical descriptions of the study results are provided in a separate final technical report, which can be downloaded from the ADRC website (www.adrc.iastate.edu). -
Oct 2014 Newsletter
Volume20, Issue 02 NWASNEWS October 2014 Newsletter for the Wiltshire, Swindon, Beckington OF COMETS AND PROBES Astronomical Societies and Salisbury Plain In the September meeting the Wiltshire As- ulated on their successful mission to Mars. tronomical Society held its AGM and report- Not many can claim that, and they did it on Wiltshire Society Page 2 ed steady account balance through the year a comparative shoe string budget. NASA Swindon Stargazers 3 with a reserve that means we will not be and the ISA are already in agreements upping fees for membership or attendance. about future combined missions. Beckington and SPOG 4 We elected a new vice chairperson, Keith NASA also inserted the Maven probe and Bruton, and agreed to elect Jon Gale and both will be at Mars ready to image the 19th Space Place 5 Tony Vale as observing coordinators. I October close pass by comet Siding Mira: Variable stars thank them all for standing, and wish them a Springs of the planet Mars. The closest fruitful period in the committee and hope we ‘miss’ to a planet we have witnessed. will all support them as the need arises. Comet Panstarrs is also still showing lots of Comets and Asteroids 6-7 One chap (ple) who has to do a lot of sort- promise as a 40,ooo year long period comet Nick Howes ing when things go wrong at the last minute but has ducked to the southern skies. What Square Kilometre Array 8-10 is our speaker secretary, Peter. He was let is the difference between a long period down last week by the listed speaker but comet and a short period comet? Well I has made alternative ‘A’ plans: have included some definitions within the Rosetta Mission landing 11-13 Due to circumstances outside our control full newsletter.