THE 3–4 Μm SPECTRA of JUPITER TROJAN ASTEROIDS
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Origin and Evolution of Trojan Asteroids 725
Marzari et al.: Origin and Evolution of Trojan Asteroids 725 Origin and Evolution of Trojan Asteroids F. Marzari University of Padova, Italy H. Scholl Observatoire de Nice, France C. Murray University of London, England C. Lagerkvist Uppsala Astronomical Observatory, Sweden The regions around the L4 and L5 Lagrangian points of Jupiter are populated by two large swarms of asteroids called the Trojans. They may be as numerous as the main-belt asteroids and their dynamics is peculiar, involving a 1:1 resonance with Jupiter. Their origin probably dates back to the formation of Jupiter: the Trojan precursors were planetesimals orbiting close to the growing planet. Different mechanisms, including the mass growth of Jupiter, collisional diffusion, and gas drag friction, contributed to the capture of planetesimals in stable Trojan orbits before the final dispersal. The subsequent evolution of Trojan asteroids is the outcome of the joint action of different physical processes involving dynamical diffusion and excitation and collisional evolution. As a result, the present population is possibly different in both orbital and size distribution from the primordial one. No other significant population of Trojan aster- oids have been found so far around other planets, apart from six Trojans of Mars, whose origin and evolution are probably very different from the Trojans of Jupiter. 1. INTRODUCTION originate from the collisional disruption and subsequent reaccumulation of larger primordial bodies. As of May 2001, about 1000 asteroids had been classi- A basic understanding of why asteroids can cluster in fied as Jupiter Trojans (http://cfa-www.harvard.edu/cfa/ps/ the orbit of Jupiter was developed more than a century lists/JupiterTrojans.html), some of which had only been ob- before the first Trojan asteroid was discovered. -
March 21–25, 2016
FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk, -
Aas 14-267 Design of End-To-End Trojan Asteroid
AAS 14-267 DESIGN OF END-TO-END TROJAN ASTEROID RENDEZVOUS TOURS INCORPORATING POTENTIAL SCIENTIFIC VALUE Jeffrey Stuart,∗ Kathleen Howell,y and Roby Wilsonz The Sun-Jupiter Trojan asteroids are celestial bodies of great scientific interest as well as potential natural assets offering mineral resources for long-term human exploration of the solar system. Previous investigations have addressed the auto- mated design of tours within the asteroid swarm and the transition of prospective tours to higher-fidelity, end-to-end trajectories. The current development incorpo- rates the route-finding Ant Colony Optimization (ACO) algorithm into the auto- mated tour generation procedure. Furthermore, the potential scientific merit of the target asteroids is incorporated such that encounters with higher value asteroids are preferentially incorporated during sequence creation. INTRODUCTION Near Earth Objects (NEOs) are currently under consideration for manned sample return mis- sions,1 while a recent NASA feasibility assessment concludes that a mission to the Trojan asteroids can be accomplished at a projected cost of less than $900M in fiscal year 2015 dollars.2 Tour concepts within asteroid swarms allow for a broad sampling of interesting target bodies either for scientific investigation or as potential resources to support deep-space human missions. However, the multitude of asteroids within the swarms necessitates the use of automated design algorithms if a large number of potential mission options are to be surveyed. Previously, a process to automatically and rapidly generate sample tours within the Sun-Jupiter L4 Trojan asteroid swarm with a mini- mum of human interaction has been developed.3 This scheme also enables the automated transition of tours of interest into fully optimized, end-to-end trajectories using a variety of electrical power sources.4,5 This investigation extends the automated algorithm to use ant colony optimization, a heuristic search algorithm, while simultaneously incorporating a relative ‘scientific importance’ ranking into tour construction and analysis. -
A Low Density of 0.8 G Cm-3 for the Trojan Binary Asteroid 617 Patroclus
Publisher: NPG; Journal: Nature:Nature; Article Type: Physics letter DOI: 10.1038/nature04350 A low density of 0.8 g cm−3 for the Trojan binary asteroid 617 Patroclus Franck Marchis1, Daniel Hestroffer2, Pascal Descamps2, Jérôme Berthier2, Antonin H. Bouchez3, Randall D. Campbell3, Jason C. Y. Chin3, Marcos A. van Dam3, Scott K. Hartman3, Erik M. Johansson3, Robert E. Lafon3, David Le Mignant3, Imke de Pater1, Paul J. Stomski3, Doug M. Summers3, Frederic Vachier2, Peter L. Wizinovich3 & Michael H. Wong1 1Department of Astronomy, University of California, 601 Campbell Hall, Berkeley, California 94720, USA. 2Institut de Mécanique Céleste et de Calculs des Éphémérides, UMR CNRS 8028, Observatoire de Paris, 77 Avenue Denfert-Rochereau, F-75014 Paris, France. 3W. M. Keck Observatory, 65-1120 Mamalahoa Highway, Kamuela, Hawaii 96743, USA. The Trojan population consists of two swarms of asteroids following the same orbit as Jupiter and located at the L4 and L5 stable Lagrange points of the Jupiter–Sun system (leading and following Jupiter by 60°). The asteroid 617 Patroclus is the only known binary Trojan1. The orbit of this double system was hitherto unknown. Here we report that the components, separated by 680 km, move around the system’s centre of mass, describing a roughly circular orbit. Using this orbital information, combined with thermal measurements to estimate +0.2 −3 the size of the components, we derive a very low density of 0.8 −0.1 g cm . The components of 617 Patroclus are therefore very porous or composed mostly of water ice, suggesting that they could have been formed in the outer part of the Solar System2. -
Direct Exploration of Jupiter Trojan Asteroid Using Solar Power Sail
Direct Exploration of Jupiter Trojan Asteroid using Solar Power Sail Osamu MORI*, Hideki KATO, Jun MATSUMOTO, Takanao SAIKI, Yuichi TSUDA, Naoko OGAWA, Yuya MIMASU, Junichiro KAWAGUCHI, Koji TANAKA, Hiroyuki TOYOTA, Nobukatsu OKUIZUMI, Fuyuto TERUI, Atsushi TOMIKI, Shigeo KAWASAKI, Hitoshi KUNINAKA, Kazutaka NISHIYAMA, Ryudo TSUKIZAKI, Satoshi HOSODA, Nobutaka BANDO, Kazuhiko YAMADA, Tatsuaki OKADA, Takahiro IWATA, Hajime YANO, Yoko KEBUKAWA, Jun AOKI, Masatsugu OTSUKI, Ryosuke NAKAMURA, Chisato OKAMOTO, Shuji MATSUURA, Daisuke YONETOKU, Ayako MATSUOKA, Reiko NOMURA, Ralf BODEN, Toshihiro CHUJO, Yusuke OKI, Yuki TAKAO, Kazuaki IKEMOTO, Kazuhiro KOYAMA, Hiroyuki KINOSHITA, Satoshi KITAO, Takuma NAKAMURA, Hirokazu ISHIDA, Keisuke UMEDA, Shuya KASHIOKA, Miyuki KADOKURA, Masaya KURAKAWA and Motoki WATANABE 1 Introduction (1) Direct exploration mission of small celestial bodies, inspired by Hayabusa, are being actively carried out Hayabusa-2, OSIRIS-REx and ARM etc • Due to constraints of resources and orbital mechanics, the current target objects are mainly near-Earth asteroids and Mars satellites. • In the near future, it can be expected that the targets will shift to higher primordial celestial bodies, located farther away from the Sun. 2 Introduction (2) • In the navigation of the outer planetary region, ensuring electric power becomes increasingly difficult and ΔV requirements become large. • It is not possible to perform sampling (direct exploration) missions beyond the main belt with combination of solar panels and chemical propulsion system. • NASA selected Jupiter Trojan multi-flyby as Discovery mission. • However, we propose a landing and sample return of Jupiter Trojan using the solar power sail-craft. L5 NASA Jupiter L4 JAXA 3 What is Solar Power Sail ? • Solar Power Sail is original Japanese concept in which electrical power is generated by thin-film solar cells on the sail membrane. -
Trojan Tour Decadal Study
SDO-12348 Trojan Tour Decadal Study Mike Brown [email protected] SDO-12348 Planetary Science Decadal Survey Mission Concept Study Final Report Executive Summary ................................................................................................................ 5 1. Scientific Objectives ......................................................................................................... 6 Science Questions and Objectives ................................................................................................................................... 6 Science Traceability ............................................................................................................................................................ 12 2. High‐Level Mission Concept ........................................................................................... 14 Study Request and Concept Maturity Level .............................................................................................................. 14 Overview ................................................................................................................................................................................. 14 Technology Maturity .......................................................................................................................................................... 16 Key Trades ............................................................................................................................................................................. -
The Trojan Asteroids: Keys to Many Locks
The Trojan Asteroids: Keys to Many Locks Andrew S. Rivkin (JHU/APL), Joshua Emery (U. Tennessee), Antonella Barucci (Observatoire de Paris), James F. Bell (Cornell University), William F. Bottke (SwRI), Elisabetta Dotto (Osservatorio Astronomico di Roma), Robert Gold (JHU/APL), Carey Lisse (JHU/APL), Javier Licandro (Instituto de Astrofísica de Canarias), Louise Prockter (JHU/APL), Charles Hibbits (JHU/APL), Michael Paul (Applied Research Laboratory, Penn State University), Alessondra Springmann (MIT), Bin Yang (University of Hawaii) Executive Summary: The Trojan asteroids of Jupiter lie at the crux of several of the most interesting outstanding issues regarding the formation and evolution of the Solar System. Jupiter’s companion asteroids hold the potential to unlock the answers to fundamental questions about planetary migration, the late heavy bombardment, the formation of the jovian system, and the origin and evolution of transneptunian objects (TNOs). Despite a population comparable in number to the main asteroid belt, they remain poorly understood. Dynamical studies over the last decade have provided evidence that they may have formed alongside TNOs and been captured into their current orbits early in solar system history, making them invaluable windows into TNO properties. Formation in place would make them equally compelling targets, as witnesses to the earliest history of the jovian system and the last remaining precursor material to the Galilean satellites. Spacecraft investigation of the Trojan population has been recognized as a current New Frontiers goal, should remain a very high priority for the coming decade, and most importantly is achievable now. Motivation and Background: Jupiter shares its orbit with a host of small bodies. -
Jupiter Trojan's Shallow Subsurface: Direct Observations by Radar on Board OKEANOS Mission
EPSC Abstracts Vol. 12, EPSC2018-526, 2018 European Planetary Science Congress 2018 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2018 Jupiter Trojan’s shallow subsurface: direct observations by radar on board OKEANOS mission Alain Herique (1), Pierre Beck (1), Patrick Michel (2), Wlodek Kofman (1,6), Atsushi Kumamoto (3), Tatsuaki Okada (4), Dirk Plettemeier (5) (1) Univ. Grenoble Alpes, IPAG, F-38000 Grenoble, France, ([email protected]) (2) UNS-CNRS-Observatoire de la Cote d'Azur, Nice, France (3) Tohoku University, Sendai, Japan (4) Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan (5) Technical University Dresden, 01187 Dresden, Germany (6) Space Research Centre PAS, Warsaw, Poland Abstract Planetary radar What are the Jupiter Trojans asteroids? Are they In complement to the optical remote sensing, radar rocky asteroids accreted in the vicinity of Jupiter? sounding of the shallow subsurface would improve Captured Icy bodies? Understanding the genetic of our understanding of these unexplored bodies [5], [6]. The Jupiter Trojans is the goal of the OKEANOS / The sounding of the first tens of meters of the surface JAXA understudy mission. The monostatic radar would give the structure of the near surface and onboard OKEANOS will be the unique opportunity allows identifying layers, ices lenses covered by a to directly access the shallow subsurface of the body, regolith, spatial variability of the constitutive imaging its internal structures. material and possible migration processes of volatile or organic materials. It would support the Trojans' Genetic identification of exogenous materials aggregated in the Lagrange-point gravitational trap in order to Dark and red objects (P- & D-types) dominate this understand the relation of Trojans with their small population of objects orbiting the Sun at Jupiter environment. -
Can Planetesimals Left Over from Terrestrial Planet Formation Produce the Lunar Late Heavy Bombardment?
Icarus 190 (2007) 203–223 www.elsevier.com/locate/icarus Can planetesimals left over from terrestrial planet formation produce the lunar Late Heavy Bombardment? William F. Bottke ∗, Harold F. Levison, David Nesvorný, Luke Dones Southwest Research Institute, 1050 Walnut St., Suite 400, Boulder, CO 80302, USA Received 22 August 2006; revised 17 January 2007 Available online 12 March 2007 Abstract The lunar Late Heavy Bombardment (LHB) defines a time between 3.8 to possibly 4.1 Gy ago when the Nectarian and early-Imbrium basins on the Moon with reasonably well-constrained ages were formed. Some∼ have argued that these basins were produced by a terminal cataclysm that caused a spike in the inner Solar System impactor flux during this interval. Others have suggested the basins were formed by the tail end of a monotonically decreasing impactor population originally produced by planet formation processes in the inner Solar System. Here we investigate whether this so-called declining bombardment scenario of the LHB is consistent with constraints provided by planet formation models as well as the inferred ages of Nectaris, Serenitatis, Imbrium, and Orientale. We did this by modeling the collisional and dynamical evolution of the post-planet formation population (PPP) for a range of starting PPP masses. Using a Monte Carlo code, we computed the probability that the aforementioned basins were created at various times after the Moon-forming event approximately 4.54 Ga. Our results indicate that the likelihood that the declining bombardment scenario produced Nectaris, Serenitatis, Imbrium, and Orientale (or even just Imbrium and Orientale) at any of their predicted ages is extremely low and can be ruled out at the 3σ confidence level, regardless of the PPP’s starting mass. -
The Jupiter Magnetospheric Orbiter and the Trojan Asteroid Explorer in EJSM (Europa Jupiter System Mission)
Trans. JSASS Aerospace Tech. Japan Vol. 10, No. ists28, pp. Tk_37-Tk_40, 2012 Topics The Jupiter Magnetospheric Orbiter and the Trojan Asteroid Explorer in EJSM (Europa Jupiter System Mission) 1) 2) 2) 2) 3) By Sho SASAKI , Masaki FUJIMOTO , Hajime YANO , Takeshi TAKASHIMA , Yasumasa KASABA , 4) 4) 2) 2) 2) Yukihiro TAKAHASHI , Jun KIMURA , Yuichi TSUDA , Ryu FUNASE , Osamu MORI 2) 2) Stefano CAMPAGNOLA , Yasuhiro KAWAKATSU 1)National Astronomical Observatory of Japan, Oshu, Japan 2)The Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan 3)Tohoku University, Sendai, Japan 4)Hokkaido University, Sapporo, Japan (Received June 27th, 2011) EJSM (Europa Jupiter System Mission) is an international Jovian system mission with three spacecraft. Coordinated observation of Jovian magnetosphere is one of the important targets of the mission in addition to icy satellites, atmosphere, and the interior of Jupiter. JAXA will take a role on the magnetosphere spinner JMO (Jupiter Magnetospheric Orbiter), whereas ESA will launch JGO (Jupiter Ganymede Orbiter) and NASA will be responsible for JEO (Jupiter Europa Orbiter). One possibility is to combine JMO with a proposed solar sail mission of JAXA for Jupiter and one of Trojan asteroids. Since Trojan asteroids could be representing raw solid materials of Jupiter or at least outer solar system bodies, involvement of Trojan observation should enlarge the scope and enhance the quality of EJSM. Key Words:Jupiter, Jovian Magnetosphere, Trojan Asteroids, Europa, Ganymede 1. Introduction: EJSM to investigate the 3D spatial structure of magnetosphere, the multi-spacecraft mission is desiable1). From the beginning of Jupiter is the largest planet in the solar system. -
The Complex History of Trojan Asteroids
Emery J. P., Marzari F., Morbidelli A., French L. M., and Grav T. (2015) The complex history of Trojan asteroids. In Asteroids IV (P. Michel et al., eds.), pp. 203–220. Univ. of Arizona, Tucson, DOI: 10.2458/azu_uapress_9780816532131-ch011. The Complex History of Trojan Asteroids Joshua P. Emery University of Tennessee Francesco Marzari Università di Padova Alessandro Morbidelli Lagrange Laboratory, Université Côte d’Azur, Observatoire de la Côte d’Azur, CNRS Linda M. French Illinois Wesleyan University Tommy Grav Planetary Science Institute The Trojan asteroids, orbiting the Sun in Jupiter’s stable Lagrange points, provide a unique perspective on the history of our solar system. As a large population of small bodies, they record important gravitational interactions in the dynamical evolution of the solar system. As primi- tive bodies, their compositions and physical properties provide windows into the conditions in the solar nebula in the region in which they formed. In the past decade, significant advances have been made in understanding their physical properties, and there has been a revolution in thinking about the origin of Trojans. The ice and organics generally presumed to be a signifi- cant part of Trojan composition have yet to be detected directly, although the low density of the binary system Patroclus (and possibly low density of the binary/moonlet system Hektor) is consistent with an interior ice component. By contrast, fine-grained silicates that appear to be similar to cometary silicates in composition have been detected, and a color bimodality may indicate distinct compositional groups among the Trojans. Whereas Trojans had traditionally been thought to have formed near 5 AU, a new paradigm has developed in which the Trojans formed in the proto-Kuiper belt, and were scattered inward and captured in the Trojan swarms as a result of resonant interactions of the giant planets. -
The Minor Planet Bulletin 40 (2013) 125 CS3 Observations on Jan 13 and 14 Were Made with a 0.35-M Schmidt-Cassegrain and SBIG ST-9XE
THE MINOR PLANET BULLETIN OF THE MINOR PLANETS SECTION OF THE BULLETIN ASSOCIATION OF LUNAR AND PLANETARY OBSERVERS VOLUME 40, NUMBER 3, A.D. 2013 JULY-SEPTEMBER 119. SOMETHING OLD, SOMETHINGS NEW: figure shows the lightcurve after removing the rotation of the THREE BINARY DISCOVERIES primary, thus revealing the mutual events and other features due to FROM THE PALMER DIVIDE OBSERVATORY the satellite. The latter often includes an upward bowing between the events, indicating an elongated satellite that is tidally-locked to Brian D. Warner its orbital period. Palmer Divide Observatory 17995 Bakers Farm Rd., Colorado Springs, CO 80908 4383 Suruga. Observations of 4383 Suruga were made from 2013 [email protected] Feb 2-13. Initial observations were made with a 0.35-m Schmidt- Cassegrain and Finger Lakes FLI-1001E CCD camera. When (Received: 10 March) indications of a satellite were seen in those first data sets, the target was moved to a 0.5-m Ritchey-Chretien with FLI-1001E to improve the signal-to-noise ratio. Data on the order of 0.01-0.02 Analysis of new CCD photometric observations in early mag are usually required for reliable detections of mutual events 2013 of the Vestoid asteroid 4383 Suruga and Hungaria (occultations and/or eclipses) caused by a satellite. asteroid (53432) 1999 UT55 showed that the two are binary systems. A review of data from 2005 for the The results of the analysis are shown in Figures 1-3. The period of Hungaria asteroid 4440 Tchantches indicates that the the primary is 3.4068 ± 0.0003 h with an amplitude of 0.14 ± 0.01 original analysis probably overlooked a satellite.