Vulcanoid Asteroids and Sun-Grazing Comets – Past Encounters and Possible Outcomes
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Comet C/2018 V1 (Machholz-Fujikawa-Iwamoto): Data Ulate About Past Visits of Interstellar Comets on the Basis of Available Using a 0.47-M Reflector, D
MNRAS 000, 1–11 (2019) Preprint 30 August 2019 Compiled using MNRAS LATEX style file v3.0 Comet C/2018 V1 (Machholz-Fujikawa-Iwamoto): dislodged from the Oort Cloud or coming from interstellar space? C. de la Fuente Marcos1⋆ and R. de la Fuente Marcos2 1 Universidad Complutense de Madrid, Ciudad Universitaria, E-28040 Madrid, Spain 2AEGORA Research Group, Facultad de Ciencias Matemáticas, Universidad Complutense de Madrid, Ciudad Universitaria, E-28040 Madrid, Spain Accepted 2019 August 3. Received 2019 July 26; in original form 2019 February 17 ABSTRACT The chance discovery of the first interstellar minor body, 1I/2017 U1 (‘Oumuamua), indicates that we may have been visited by such objects in the past and that these events may repeat in the future. Unfortunately, minor bodies following nearly parabolic or hyperbolic paths tend to receive little attention: over 3/4 of those known have data-arcs shorter than 30 d and, con- sistently, rather uncertain orbit determinations. This fact suggests that we may have observed interstellar interlopers in the past, but failed to recognize them as such due to insufficient data. Early identification of promising candidates by using N-body simulations may help in improv- ing this situation, triggering follow-up observations before they leave the Solar system. Here, we use this technique to investigate the pre- and post-perihelion dynamical evolution of the slightly hyperbolic comet C/2018 V1 (Machholz-Fujikawa-Iwamoto) to understand its origin and relevance within the context of known parabolic and hyperbolic minor bodies. Based on the available data, our calculations suggest that although C/2018 V1 may be a former mem- ber of the Oort Cloud, an origin beyond the Solar system cannot be excluded. -
Dust Near the Sun
Dust Near The Sun Ingrid Mann and Hiroshi Kimura Institut f¨urPlanetologie, Westf¨alischeWilhelms-Universit¨at,M¨unster,Germany Douglas A. Biesecker NOAA, Space Environment Center, Boulder, CO, USA Bruce T. Tsurutani Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA Eberhard Gr¨un∗ Max-Planck-Institut f¨urKernphysik, Heidelberg, Germany Bruce McKibben Department of Physics and Space Science Center, University of New Hampshire, Durham, NH, USA Jer-Chyi Liou Lockheed Martin Space Operations, Houston, TX, USA Robert M. MacQueen Rhodes College, Memphis, TN, USA Tadashi Mukai† Graduate School of Science and Technology, Kobe University, Kobe, Japan Lika Guhathakurta NASA Headquarters, Washington D.C., USA Philippe Lamy Laboratoire d’Astrophysique Marseille, France Abstract. We review the current knowledge and understanding of dust in the inner solar system. The major sources of the dust population in the inner solar system are comets and asteroids, but the relative contributions of these sources are not quantified. The production processes inward from 1 AU are: Poynting- Robertson deceleration of particles outside of 1 AU, fragmentation into dust due to particle-particle collisions, and direct dust production from comets. The loss processes are: dust collisional fragmentation, sublimation, radiation pressure acceler- ation, sputtering, and rotational bursting. These loss processes as well as dust surface processes release dust compounds in the ambient interplanetary medium. Between 1 and 0.1 AU the dust number densities and fluxes can be described by inward extrapolation of 1 AU measurements, assuming radial dependences that describe particles in close to circular orbits. Observations have confirmed the general accuracy of these assumptions for regions within 30◦ latitude of the ecliptic plane. -
Ice& Stone 2020
Ice & Stone 2020 WEEK 51: DECEMBER 13-19 Presented by The Earthrise Institute # 51 Authored by Alan Hale COMET OF THE WEEK: The Great Comet of 1680 Perihelion: 1680 December 18.49, q = 0.006 AU The Great Comet of 1680 over Rotterdam in The Netherlands, during late December 1680 as painted by the Dutch artist Lieve Verschuier. This particular comet was undoubtedly one of the brightest comets of the 17th Century, but it is also one of the most important comets in history from a scientific perspective, and perhaps even from the perspective of overall human history. While there were certainly plenty of superstitions attached to the comet’s appearance, the scientific investigations made of it were among the beginnings of the era in European history we now call The Enlightenment, and indeed, in a sense the Great Comet of 1680 can perhaps be considered as one of the sparks of that era. The significance began with the comet’s discovery, which was made on the morning of November 14, 1680, by a German astronomer residing in Coburg, Gottfried Kirch – the first comet ever to be discovered by means of a telescope. It was already around 4th magnitude at that time, and located near the star Regulus in the constellation Leo; from that point it traveled eastward and brightened rapidly, being closest to Earth (0.42 AU) on November 30. By that time it was a conspicuous naked-eye object with a tail 20 to 30 degrees long, and it remained visible for another week before disappearing into morning twilight. -
The Orbital Distribution of Near-Earth Objects Inside Earth’S Orbit
Icarus 217 (2012) 355–366 Contents lists available at SciVerse ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus The orbital distribution of Near-Earth Objects inside Earth’s orbit ⇑ Sarah Greenstreet a, , Henry Ngo a,b, Brett Gladman a a Department of Physics & Astronomy, 6224 Agricultural Road, University of British Columbia, Vancouver, British Columbia, Canada b Department of Physics, Engineering Physics, and Astronomy, 99 University Avenue, Queen’s University, Kingston, Ontario, Canada article info abstract Article history: Canada’s Near-Earth Object Surveillance Satellite (NEOSSat), set to launch in early 2012, will search for Received 17 August 2011 and track Near-Earth Objects (NEOs), tuning its search to best detect objects with a < 1.0 AU. In order Revised 8 November 2011 to construct an optimal pointing strategy for NEOSSat, we needed more detailed information in the Accepted 9 November 2011 a < 1.0 AU region than the best current model (Bottke, W.F., Morbidelli, A., Jedicke, R., Petit, J.M., Levison, Available online 28 November 2011 H.F., Michel, P., Metcalfe, T.S. [2002]. Icarus 156, 399–433) provides. We present here the NEOSSat-1.0 NEO orbital distribution model with larger statistics that permit finer resolution and less uncertainty, Keywords: especially in the a < 1.0 AU region. We find that Amors = 30.1 ± 0.8%, Apollos = 63.3 ± 0.4%, Atens = Near-Earth Objects 5.0 ± 0.3%, Atiras (0.718 < Q < 0.983 AU) = 1.38 ± 0.04%, and Vatiras (0.307 < Q < 0.718 AU) = 0.22 ± 0.03% Celestial mechanics Impact processes of the steady-state NEO population. -
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1 2 Spiral Galaxy M51. Herrero, E. Image from Montsec Astronomical Observatory (OAdM) 3 4 5 CONTENTS The Institute 6 Board of trustees 8 Scientific advisory board 9 Board of Directors 9 Staff 10 Scientific Research 16 Scientific results 25 Publications SCI 31 Papers in which only one institute is participating 31 Papers published by two institutes in collaboration 39 Papers published by three institutes in collaboration 40 Publications non SCI 40 Papers in which only one institute is participating 40 Papers published by two institutes in collaboration 46 Books edited 47 Courses 47 Contribution to conferences and seminars 48 Contribution to conferences 48 Seminars 59 Internal seminars 59 External seminars 59 Theses 61 Finished Theses 61 PhD Theses 61 Master theses 62 On going theses 62 PhD Theses 62 Master theses 62 Visiting scientists 64 Technological development activities 65 Technical reports and documents 65 Technical reports and documents developed by only one institute 65 Technical reports and documents developed by three institutes in collaboration 69 Technological development activities 69 Finished activities 69 Ongoing activities 69 Projects managed by the IEEC 69 Finished projects 69 Ongoing projects 70 Other scientific activities 72 Space missions 73 Mission proposals 82 Ground instrument projects 89 Montsec Astronomical Observatoyy (OAdM) 95 European Projects 99 Workshops organized by the IEEC 103 Outreach activities 107 Objectives, indicators and achievement 114 6 IEEC ▪ THE INSTITUTE The Institute of Space Studies of Catalonia (IEEC) was founded in February of 1996 as an initiative of the Fundació Catalana per a la Recerca (FCR), in collaboration with the University of Barcelona (UB), the Autonomous University of Barcelona (UAB), the Polytechnic University of Catalonia (UPC) and the Spanish Research Council (CSIC) with the objective of creating a multi-disciplinary and multi-institutional institute devoted to space research and their applications. -
Planetary Science from a Next-Gen Suborbital Platform: Sleuthing the Long Sought After Vulcanoid Aster- Oids
Next-Generation Suborbital Researchers Conference (2010) (2010) 4004.pdf Planetary Science from a Next-Gen Suborbital Platform: Sleuthing the Long Sought After Vulcanoid Aster- oids. S.A. Stern1 , D.D. Durda1, M. Davis1, and C.B. Olkin1. Southwest Research Institute, Suite 300, 1050 Walnut Street, Boulder, CO 80302, [email protected]. Introduction: We are on the verge of a revolution in pheric haze and turbulence are among the daunting scientific access to space. This revolution, fueled by challenges faced by ground-based observers searching billionaire investors like Richard Branson and Jeff for objects near the Sun at twilight. Consequently, only Bezos, is fielding no less than three human flight sub- a few visible-wavelength ground-based searches for orbital systems in the coming 24 months. This new Vulcanoids have been conducted. stable of vehicles, originally intended to open up a Experiment: We will conduct a large area search space tourism market, includes Virgin Galactic’s for Vulcanoids using our SWUIS imager developed for SpacesShip2, Blue Origin’s New Shepard, and Space Shuttle and high altitude F-18 flights. We will XCOR’s Lynx. Each offers the capability to fly multi- conduct our Vulcanoid search experiment at altitudes ple humans to altitudes of 70-140 km on a frequent of 100-140 km near twilight so that the Vulcanoid re- (daily to weekly) basis for per-seat launch costs of gion is seen above a dark Earth with the Sun below the $100K-$200K/launch. The total investment in these depressed horizon. In this way we will eliminate the systems is now approaching $1B, and test flights of scattered light problems that have dogged all ground- each are set to begin in 2010. -
7 X 11 Long.P65
Cambridge University Press 978-0-521-85349-1 - Meteor Showers and their Parent Comets Peter Jenniskens Index More information Index a – semimajor axis 58 twin shower 440 A – albedo 111, 586 fragmentation index 444 A1 – radial nongravitational force 15 meteoroid density 444 A2 – transverse, in plane, nongravitational force 15 potential parent bodies 448–453 A3 – transverse, out of plane, nongravitational a-Centaurids 347–348 force 15 1980 outburst 348 A2 – effect 239 a-Circinids (1977) 198 ablation 595 predictions 617 ablation coefficient 595 a-Lyncids (1971) 198 carbonaceous chondrite 521 predictions 617 cometary matter 521 a-Monocerotids 183 ordinary chondrite 521 1925 outburst 183 absolute magnitude 592 1935 outburst 183 accretion 86 1985 outburst 183 hierarchical 86 1995 peak rate 188 activity comets, decrease with distance from Sun 1995 activity profile 188 Halley-type comets 100 activity 186 Jupiter-family comets 100 w 186 activity curve meteor shower 236, 567 dust trail width 188 air density at meteor layer 43 lack of sodium 190 airborne astronomy 161 meteoroid density 190 1899 Leonids 161 orbital period 188 1933 Leonids 162 predictions 617 1946 Draconids 165 upper mass cut-off 188 1972 Draconids 167 a-Pyxidids (1979) 199 1976 Quadrantids 167 predictions 617 1998 Leonids 221–227 a-Scorpiids 511 1999 Leonids 233–236 a-Virginids 503 2000 Leonids 240 particle density 503 2001 Leonids 244 amorphous water ice 22 2002 Leonids 248 Andromedids 153–155, 380–384 airglow 45 1872 storm 380–384 albedo (A) 16, 586 1885 storm 380–384 comet 16 1899 -
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. -
The Evolution of Long-Period Comets
Icarus 137, 84–121 (1999) Article ID icar.1998.6040, available online at http://www.idealibrary.com on The Evolution of Long-Period Comets Paul Wiegert Department of Physics and Astronomy, York University, Toronto, Ontario M3J 1P3, Canada E-mail: [email protected] and Scott Tremaine Princeton University Observatory, Peyton Hall, Princeton, New Jersey 08544-1001 Received May 16, 1997; revised September 29, 1998 the length of time over which routine telescopic observations We study the evolution of long-period comets by numerical in- have been taken—the sample of comets with longer periods is tegration of their orbits, a more realistic dynamical approach than much less complete; (iii) the planetary perturbations suffered the Monte Carlo and analytic methods previously used to study by comets with periods longer than 200 yr are uncorrelated on this problem. We follow the comets from their origin in the Oort successive perihelion passages. The orbits of typical Halley- cloud until their final escape or destruction, in a model solar sys- type and Jupiter-family comets are further distinguished by tem consisting of the Sun, the four giant planets and the Galactic (i) their inclinations, which are much larger for Halley-type tide. We also examine the effects of nongravitational forces as well comets; (ii) their Tisserand invariants T , which are typically as the gravitational forces from a hypothetical solar companion greater than 2 for Jupiter-family comets (Carusi and Valsecchi or circumsolar disk. We confirm the conclusion of Oort and other investigators that the observed distribution of long-period comet 1992; Levison 1996). -
In Order to Decide Whether You Like a Particular Soup, Do You
In order to decide whether you like a particular soup, do you need to eat the whole pot? Usually, you can get a good sense of the flavor of the soup by taking a small taste, or a sample. When conducting a study, it is usually not possible to survey every person or object in the population in which you are interested (for example, all the residents of the United States, all the students at your school, or all teenage shoppers). However, just as you can learn about the flavor of a soup with a small taste instead of eating the whole pot, you can learn about a population by sampling instead of taking a census. Unfortunately, large groups of people are much harder to stir than pots of soup to get a representative mix of their populations. In this lesson, you will consider ways that statisticians do the equivalent of “stirring” populations in order to take samples that represent the whole population well. As you work with your team today, consider the following questions. How should we decide what is “typical” of a group? How do random selection and intentional selection compare? 9-16. How should you choose people for your survey to make up a sample that you think represents the population for your research question? a. Discuss this question with your team and write down your ideas. Be sure to justify why your ideas will help you choose a representative sample. b. Do you think your sampling method is better than randomly selecting members of the population? Why or why not? 9-17. -
Four Billion Year Stability of the Earth-Mars Belt
MNRAS 000,1–7 (2020) Preprint 6 October 2020 Compiled using MNRAS LATEX style file v3.0 Four Billion Year Stability of the Earth–Mars Belt Yukun Huang (Ä宇d)1 and Brett Gladman1 1Department of Physics and Astronomy, University of British Columbia, 6224 Agricultural Road, Vancouver, BC V6T 1Z1, Canada Accepted XXX. Received July xx/2020; in original form ZZZ ABSTRACT Previous work has demonstrated orbital stability for 100 Myr of initially near-circular and coplanar small bodies in a region termed the ‘Earth–Mars belt’ from 1.08 au < 0 < 1.28 au. Via numerical integration of 3000 particles, we studied orbits from 1.04–1.30 au for the age of the Solar system. We show that on this time scale, except for a few locations where mean- motion resonances with Earth affect stability, only a narrower ‘Earth–Mars belt’ covering 0 ∼ ¹1.09, 1.17º au, 4 < 0.04, and 퐼 < 1◦ has over half of the initial orbits survive for 4.5 Gyr. In addition to mean-motion resonances, we are able to see how the a3, a4, and a6 secular resonances contribute to long-term instability in the outer (1.17–1.30 au) region on Gyr time scales. We show that all of the (rather small) near-Earth objects (NEOs) in or close to the Earth–Mars belt appear to be consistent with recently arrived transient objects by comparing to a NEO steady-state model. Given the < 200 m scale of these NEOs, we estimated the Yarkovsky drift rates in semimajor axis, and use these to estimate that primordial asteroids with a diameter of 100 km or larger in the Earth-Mars belt would likely survive. -
The Isabel Williamson Lunar Observing Program
The Isabel Williamson Lunar Observing Program by The RASC Observing Committee Revised Third Edition September 2015 © Copyright The Royal Astronomical Society of Canada. All Rights Reserved. TABLE OF CONTENTS FOR The Isabel Williamson Lunar Observing Program Foreword by David H. Levy vii Certificate Guidelines 1 Goals 1 Requirements 1 Program Organization 2 Equipment 2 Lunar Maps & Atlases 2 Resources 2 A Lunar Geographical Primer 3 Lunar History 3 Pre-Nectarian Era 3 Nectarian Era 3 Lower Imbrian Era 3 Upper Imbrian Era 3 Eratosthenian Era 3 Copernican Era 3 Inner Structure of the Moon 4 Crust 4 Lithosphere / Upper Mantle 4 Asthenosphere / Lower Mantle 4 Core 4 Lunar Surface Features 4 1. Impact Craters 4 Simple Craters 4 Intermediate Craters 4 Complex Craters 4 Basins 5 Secondary Craters 5 2. Main Crater Features 5 Rays 5 Ejecta Blankets 5 Central Peaks 5 Terraced Walls 5 ii Table of Contents 3. Volcanic Features 5 Domes 5 Rilles 5 Dark Mantling Materials 6 Caldera 6 4. Tectonic Features 6 Wrinkle Ridges 6 Faults or Rifts 6 Arcuate Rilles 6 Erosion & Destruction 6 Lunar Geographical Feature Names 7 Key to a Few Abbreviations Used 8 Libration 8 Observing Tips 8 Acknowledgements 9 Part One – Introducing the Moon 10 A – Lunar Phases and Orbital Motion 10 B – Major Basins (Maria) & Pickering Unaided Eye Scale 10 C – Ray System Extent 11 D – Crescent Moon Less than 24 Hours from New 11 E – Binocular & Unaided Eye Libration 11 Part Two – Main Observing List 12 1 – Mare Crisium – The “Sea of Cries” – 17.0 N, 70-50 E;