K and Cl Concentrations on the Martian Surface Determined by the Mars Odyssey Gamma Ray Spectrometer: Implications for Bulk Halogen Abundances in Mars G

Total Page:16

File Type:pdf, Size:1020Kb

K and Cl Concentrations on the Martian Surface Determined by the Mars Odyssey Gamma Ray Spectrometer: Implications for Bulk Halogen Abundances in Mars G GEOPHYSICAL RESEARCH LETTERS, VOL. 37, L12204, doi:10.1029/2010GL043528, 2010 Click Here for Full Article K and Cl concentrations on the Martian surface determined by the Mars Odyssey Gamma Ray Spectrometer: Implications for bulk halogen abundances in Mars G. Jeffrey Taylor,1 William V. Boynton,2 Scott M. McLennan,3 and Linda M. V. Martel1 Received 12 April 2010; revised 17 May 2010; accepted 21 May 2010; published 30 June 2010. [1] Orbital gamma ray spectrometry shows that the Martian of the Martian surface. As described below, although K and surface has a mean Cl/K ratio of 1.3 ± 0.2, indistinguishable Cl are not correlated, the average Cl/K is 1.3, close to the CI from the ratio in CI chondrites (1.28). Although Cl and K chondrite value of 1.28 [Palme and Jones, 2004], but very fractionate by magma degassing and aqueous processing, different from the Wänke‐Dreibus value of 0.08 (Table 1). during igneous partial melting both elements are highly We argue here that bulk silicate Mars has a CI chondrite Cl/K incompatible. Thus, if the surface Cl/K reflects the bulk ratio and that the low Cl value in the Wänke‐Dreibus model crustal value, then the mantle, hence primitive silicate is caused by Martian meteorites being depleted in Cl Mars, also has a roughly CI ratio. Martian meteorite data because of loss of this volatile during eruption or near‐ indicate that Cl/Br is also approximately chondritic, surface intrusion [also see McSween et al., 2001]. A roughly suggesting that elements that condensed in the nebula chondritic Cl/Br in Martian meteorites suggests that Cl/Br is between ∼1000 K (K and Cl) to ∼500 K (Br) are also chondritic and the small difference in the condensation uniformly depleted in Mars at about 0.6 × CI chondrite temperatures of Br and I suggests that all three halogens are concentrations. Mars clearly does not contain 0.6 × CI in chondritic proportions. levels of H2O, which would be ∼6 wt%, indicating that Mars was constructed by planetesimals rich in volatile 2. GRS Methods elements, but not in water. Citation: Taylor, G. J., W. V. Boynton, S. M. McLennan, and L. M. V. Martel (2010), K and Cl concentra- [4] The GRS determines elemental concentrations from tions on the Martian surface determined by the Mars Odyssey the intensities of gamma rays produced by neutron capture Gamma Ray Spectrometer: Implications for bulk halogen abun- and/or scattering reactions (Si, Fe, Ca, Al, Cl, H) or by dances in Mars, Geophys. Res. Lett., 37, L12204, doi:10.1029/ radioactive decay (K, Th). Details of data acquisition and 2010GL043528. reduction are given by Boynton et al. [2007, 2008]. The data we use here for Cl and K were obtained between June 8, 2002 and April 2, 2005. The GRS spatial resolution is 1. Introduction defined as the nadir‐centered region within which ∼50% of ∼ ∼ [2] The best estimate for the bulk composition of the the signal originates, which is 3.7° arc radius ( 220 km), silicate portion of Mars is that developed by Wänke and although this varies somewhat with the gamma ray energy. Dreibus in a series of papers [Dreibus and Wänke, 1984, The data were binned initially at 0.5° × 0.5°, smoothed 1987; Wänke and Dreibus, 1988, 1994]. This robust esti- using a boxcar filter over a much larger radius (5° for K, 10° mate is based on reasonable cosmochemical assumptions for Cl) and then rebinned to 5° × 5° grid points. The mea- and the compositions of Martian meteorites. However, there sured gamma rays are produced in the upper few tens of is one curious discrepancy. The estimated abundance of Cl centimeters of the Martian surface, much deeper than is much lower than other elements with similar condensation sensed by visible to thermal infrared spectral instruments temperatures, such as K (50% condensation temperature of (10–100 mm). We use only points in regions where H contents 1006 K cf 948 K for Cl). The standard Wänke‐Dreibus are low enough not to interfere in the determination of Cl model composition for moderately volatile and volatile concentrations. Hydrogen has a high cross‐section for cap- lithophile elements are given in Table 1, along with their 50% turing thermal neutrons, significantly affecting the neutron condensation temperatures [Lodders, 2003], and listed in flux in the upper ∼30 cm of the Martian surface. The GRS order of decreasing condensation temperature. The low Cl data are corrected for this effect, but the correction is carries over to the values for the other halogens, except for F. uncertain at polar latitudes where H dominates elemental [3] The Mars Odyssey Gamma Ray Spectrometer (GRS) signatures. Accordingly, we constrained our results using a has returned data that allow us to determine the K, Cl, and mask based on H concentration, corresponding to roughly other elemental concentrations in the upper few decimeters ±45° of latitude from the equator. (The concentration of H does not affect K data because its g‐rays result from radioactive decay, but we use data only within the H mask to 1Hawaii Institute of Geophysics and Planetology, University of Hawaii at Manoa, Honolulu, Hawaii, USA. compare with Cl concentrations.) 2Lunar and Planetary Laboratory, University of Arizona, Tucson, Arizona, USA. 3. Overview of K and Halogen Geochemical 3Department of Geosciences, State University of New York at Stony Brook, Stony Brook, New York, USA. Behavior [5] Potassium, Cl, Br, and I are all large‐ion lithophile Copyright 2010 by the American Geophysical Union. elements that behave incompatibly during partial melting, 0094‐8276/10/2010GL043528 L12204 1of5 L12204 TAYLOR ET AL.: MARS BULK COMPOSITION L12204 Table 1. Standard Wänke‐Dreibus Model Mars Bulk Composi- ferent behavior after partial melting, as summarized above. tion Compared to Model Described in This Paper Nevertheless, the mean Cl/K value, 1.27 ± 0.46 (2‐sigma uncertainty), is within the uncertainties of the CI‐chondritic 50% Condensation value, 1.28, and substantially greater than the mean value in Temperaturea Wänke‐Dreibus Wänke‐Dreibusb This Work This Work Martian meteorites, 0.08, determined from data assembled (K) (ppm) (Mars/CI) (ppm) (Mars/CI) by Meyer [2009]. Figure 2 shows the Cl/K ratio divided into K 1006 305 0.56 305 0.56 six groups. One group (largest area in Figure 2) is defined Na 958 3700 0.74 3700 0.74 by the chondritic ratio plus and minus one standard devia- Cl 948 38 0.054 390 0.56 tion of the global dataset (0.2). The other ranges are one Rb 800 1.06 0.46 1.06 0.46 standard deviation wide. Figure 2 shows that the entire Cs 799 0.07 0.37 0.07 0.37 F 734 32 0.55 32 0.55 surface of Mars has a substantially higher Cl/K ratio than Br 546 0.145 0.041 2.2 0.60 reported for bulk Martian meteorites. The ratio is every- I 535 0.032 0.074 0.26 0.60 where greater than 0.6 and a substantial portion of the surface a is within one standard deviation of the chondritic ratio. Cl/K Lodders [2003]. bDreibus and Wänke [1984, 1987] and Wänke and Dreibus [1988, 1994]. is significantly higher than the chondritic range over Tharsis, CI chondrite values from Palme and Jones [2004]. west of Tharsis, and in Elysium, and lower in Utopia Planitia. Cl enrichment in volcanic regions could be caused by fairly hence preserving the mantle source rock Cl/K in the magma recent volcanic deposits, such as the high‐Cl materials in produced [Schilling et al., 1980; Deruelle et al., 1992; Pyle Medusae Fossae [Keller et al., 2006]. and Mather, 2009]. The fluorine ion has a much smaller ionic radius than the other halides and tends to behave 5. Cl‐Br Relationships somewhat less incompatibly during partial melting [Pyle and Mather, 2009]. Thus, Cl/K (and Br/K and I/K) in sur- [9] Cl/Br in Martian meteorites (180) is close to the CI face rocks would give a good approximation to the mantle chondrite ratio (199) (meteorite data cited by Brückner et al. values if the halogens were not lost by degassing during [2008], Banin et al. [1992], and Dreibus et al. [1992, 1994, magma ascent and eruption. Note that K is not lost via 1996, 2003a, 2003b]. If reflective of the interior, it implies magma degassing. that Br, like Cl, is much higher in Mars than the estimate [6] Loss of halogens during magma degassing depends on made by Wänke and Dreibus. This assumes, of course, Cl magma composition and H2O concentration (see summary and Br are lost from magmas by the same amount during by Aiuppa et al. [2009]), but fractionation relative to each degassing. (Rocks analyzed in Gusev crater do not appear to other is probably less affected and is related to their ionic provide additional data on Cl and Br in igneous rocks. radii. Experiments by Bureau et al. [2000] show that fluid‐ According to Gellert et al. [2006], even the abraded surfaces magma partition coefficients for the halogens increase with of these rocks have high S and Cl, suggesting either con- ionic radius: F (Df/m = 0.1, ionic radius = 1.33 Å), Cl (4.5, tamination by debris generated during grinding or that the 1.81 Å), Br (14, 1.96 Å), I (78, 2.2 Å). (Ionic radii are for rocks have experienced aqueous alteration. A compilation of 6‐fold coordination and taken from Shannon [1976]; data all abraded rocks in Gusev shows Cl up to almost 2 wt%.) for F are from Webster [1992].) On the other hand, F is retained by lavas, so its concentration in volcanic rocks 6.
Recommended publications
  • Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
    Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes.
    [Show full text]
  • Circulating Transportation Orbits Between Earth and Mars
    CIRCULATING TRANSPORTATION ORBITS BETWEEN EARTH AND MRS 1 2 Alan L. Friedlander and John C. Niehoff . Science Applications International Corporation Schaumburg, Illinois 3 Dennis V. Byrnes and James M. Longuski . Jet Propulsion Laboratory Pasadena, Cal iforni a Abstract supplies in support of a sustained Manned Mars Sur- This paper describes the basic characteristics face Base sometime during the second quarter of the of circulating (cyclical ) orbit design as applied next century. to round-trip transportation of crew and materials between Earth and Mars in support of a sustained A circulating orbit may be defined as a multi- manned Mars Surface Base. The two main types of ple-arc trajectory between two or more planets non-stopover circulating trajectories are the so- which: (1) does not stop at the terminals but called VISIT orbits and the Up/Down Escalator rather involves gravity-assist swingbys of each orbits. Access to the large transportation facili- planet; (2) is repeatable or periodic in some ties placed in these orbits is by way of taxi vehi- sense; and (3) is continuous, i.e., the process can cles using hyperbolic rendezvous techniques during be carried on indefinitely. Different types of the successive encounters with Earth and Mars. circulating orbits between Earth and Mars were Specific examples of real trajectory data are pre- identified in the 1960s 1iterat~re.l'*'~'~ Re- sented in explanation of flight times, encounter examination of this interesting problem during the frequency, hyperbol ic velocities, closest approach past year has produced new solution^.^'^'^ Some distances, and AV maneuver requirements in both involve only these two bodies while others incor- interplanetary and planetocentric space.
    [Show full text]
  • Mars Express
    sp1240cover 7/7/04 4:17 PM Page 1 SP-1240 SP-1240 M ARS E XPRESS The Scientific Payload MARS EXPRESS The Scientific Payload Contact: ESA Publications Division c/o ESTEC, PO Box 299, 2200 AG Noordwijk, The Netherlands Tel. (31) 71 565 3400 - Fax (31) 71 565 5433 AAsec1.qxd 7/8/04 3:52 PM Page 1 SP-1240 August 2004 MARS EXPRESS The Scientific Payload AAsec1.qxd 7/8/04 3:52 PM Page ii SP-1240 ‘Mars Express: A European Mission to the Red Planet’ ISBN 92-9092-556-6 ISSN 0379-6566 Edited by Andrew Wilson ESA Publications Division Scientific Agustin Chicarro Coordination ESA Research and Scientific Support Department, ESTEC Published by ESA Publications Division ESTEC, Noordwijk, The Netherlands Price €50 Copyright © 2004 European Space Agency ii AAsec1.qxd 7/8/04 3:52 PM Page iii Contents Foreword v Overview The Mars Express Mission: An Overview 3 A. Chicarro, P. Martin & R. Trautner Scientific Instruments HRSC: the High Resolution Stereo Camera of Mars Express 17 G. Neukum, R. Jaumann and the HRSC Co-Investigator and Experiment Team OMEGA: Observatoire pour la Minéralogie, l’Eau, 37 les Glaces et l’Activité J-P. Bibring, A. Soufflot, M. Berthé et al. MARSIS: Mars Advanced Radar for Subsurface 51 and Ionosphere Sounding G. Picardi, D. Biccari, R. Seu et al. PFS: the Planetary Fourier Spectrometer for Mars Express 71 V. Formisano, D. Grassi, R. Orfei et al. SPICAM: Studying the Global Structure and 95 Composition of the Martian Atmosphere J.-L. Bertaux, D. Fonteyn, O. Korablev et al.
    [Show full text]
  • Mars Activities
    MARS ACTIVITIES Teacher Resources and Classroom Activities Mars Education Program Jet Propulsion Laboratory Arizona State University Mars Missions Information and Updates Mission Information Available at Jet Propulsion Laboratory Mars Exploration Home Page http://mars.jpl.nasa.gov More Educational Activities Available at Jet Propulsion Laboratory Mars Education & Public Outreach Program http://mars.jpl.nasa.gov/classroom or Arizona State University Mars K-12 Education Program http://tes.asu.edu/neweducation.html Table of Contents 1. Earth, Moon, Mars Balloons 1 2. Rover Races 4 3. Areology - The Study of Mars 11 4. Strange New Planet 16 5. Lava Layering 24 6. Searching for Life on Mars 33 7. Mars Critters 42 8. Exploring Crustal Material from a Mystery Planet 46 - Graph Paper 48 9. Edible Mars Rover 49 - Mars Pathfinder Rover 51 10. Edible Mars Spacecraft 52 - Mars Global Surveyor 54 - Mars Pathfinder 55 - Mars Pathfinder Rover 56 11. Mars Meteorites’ Fingerprints 57 12. Introduction to Creating a Mission Plan 65 13. Out of Sight: Remote Vehicle Activity 66 - Mars Rover Websites 69 15. Probing Below the Surface of Mars 74 16. Good Vibrations 85 17. The Mathematics of Mars 90 - “I Have…Who Has?” Cards 93 18. Mars Bingo 100 19. Mud Splat Craters 112 20. Solar System Beads Distance Activity 115 21. Alka-Seltzer Rockets 118 22. Soda Straw Rockets 122 23. Mars Pathfinder: Two-Dimensional Model 126 24. Mars Pathfinder: Egg Drop and Landing 127 25. Cool Internet Sites 128 Earth, Moon, Mars Balloons 1 Introduction: How big is the Moon; how far is it relative to Earth? Earth science and astronomy books depict a moon that is much closer and much larger than in reality.
    [Show full text]
  • The Formation of Mars: Building Blocks and Accretion Time Scale
    Space Sci Rev (2013) 174:11–25 DOI 10.1007/s11214-012-9904-2 The Formation of Mars: Building Blocks and Accretion Time Scale Ramon Brasser Received: 4 December 2011 / Accepted: 28 May 2012 / Published online: 12 June 2012 © Springer Science+Business Media B.V. 2012 Abstract In this review paper I address the current knowledge of the formation of Mars, focusing on its primary constituents, its formation time scale and its small mass compared to Earth and Venus. I argue that the small mass of Mars requires the terrestrial planets to have formed from a narrow annulus of material, rather than a disc extending to Jupiter. The truncation of the outer edge of the disc was most likely the result of giant planet migration, which kept Mars’ mass small. From cosmochemical constraints it is argued that Mars formed in a couple of million years and is essentially a planetary embryo that never grew to a full-fledged planet. This is in agreement with the latest dynamical models. Most of Mars’ building blocks consists of material that formed in the 2 AU to 3 AU region, and is thus more water-rich than that accreted by Earth and Venus. The putative Mars could have consisted of 0.1 % to 0.2 % by mass of water. Keywords Mars · Formation · Origin 1 Introduction The formation of the terrestrial planets of the Solar System has been an outstanding prob- lem for a long time. Significant progress has recently been made with the aid of fast com- puters and has led to a coherent picture and sequence of events.
    [Show full text]
  • UCGE Reports Number 20191
    UCGE Reports Number 20191 Department of Geomatics Engineering Simulation and Evaluation of the Performance of the Proposed Mars Network Constellation for Positioning, Orbit Improvement, and Establishment of a Spatial Reference Frame for Mars (URL: http://www.geomatics.ucalgary.ca/links/GradTheses.html) by Kyle O’Keefe April 2004 THE UNIVERSITY OF CALGARY Simulation and Evaluation of the Performance of the Proposed Mars Network Constellation for Positioning, Orbit Improvement, and Establishment of a Spatial Reference Frame for Mars by Kyle O’Keefe A THESIS SUBMITTED TO THE FACULTY OF GRADUATE STUDIES IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY DEPARTMENT OF GEOMATICS ENGINEERING CALGARY, ALBERTA April, 2004 c Kyle O’Keefe 2004 Preface This is an unaltered version of the author’s Doctoral of Philosophy thesis. The thesis was accepted by the Faculty of Graduate Studies in April, 2004. The faculty supervisor for this work was Dr. G´erard Lachapelle. The co-supervisor was Dr. Susan Skone. Other members of the examining committee were Dr. M. Elizabeth Cannon, Dr. Patrick Wu, Dr. Wayne Cannon. ii Abstract In 1999, the NASA Jet Propulsion Lab presented a proposal for a six satellite nav- igation and communication network for Mars called the Mars Network. This thesis investigates the performance of the Mars Network both theoretically, using figures of merit commonly applied to satellite navigation systems on Earth, and in the position domain using simulated observations. The Mars Network is evaluated in terms of availability, accuracy, and reliability as a function of position and time by simulating network geometry for users distributed across the planet.
    [Show full text]
  • The Blue Mars Mission Report of Group 2
    The Blue Mars Mission Report of group 2 M. Crimella, M. Dahl, G. Jufors, V. Karlsson Handledare: Nils Pokrupa A project in SD2905 - Human Spaceflight Dept. of Aeronautical and Vehicle Engineering Royal Institute of Technology, Sweden March 20th, 2014 Abstract The main work of Group 2 described in this report consists of the overall trip design, from the surface of the Earth to the surface of Mars, and back. Particular emphasis is given to the design of the interplanetary trajectory for the crew vehicle, to the design of the rockets needed for the payloads, to the propulsion system, to the ∆vrequirementsandfinallytothesequenceof launches from the Earth and to the sequence of events and vehicles needed for landing on the Red Planet. For the trajectory design the NASA Mission Design Center’s Trajectory Browser, is used. Ac- cordingly, the ∆vareobtained.Thedesignoftherocketsisbasedontheperformancesofthe propellants here considered and on the payload dimensions. Finally, on the basis of the previous results of this project, the number and sequence of launches from the Earth to LEO is calculated. The design of the events and vehicle needed to land on Mars is based on the description of reference missions, on the amount of payload that has to land on Mars and on the characteristics of Mars and its atmosphere. The chosen mission has a duration of 577 days with 112 days on Mars. The outbound trip i 304 days and include a Venus swing-by. The return trip is 161 days with crew direct entry to Earth. Total mission ∆vis10km/s.ThevehiclessenttoMarsareonecrewrocketandtwocargorockets. The Mars descent/ascent vehicle, surface habitat and equipment is pre-deployed prior to crew departure.
    [Show full text]
  • The Planetary and Lunar Ephemeris DE 421
    IPN Progress Report 42-178 • August 15, 2009 The Planetary and Lunar Ephemeris DE 421 William M. Folkner,* James G. Williams,† and Dale H. Boggs† The planetary and lunar ephemeris DE 421 represents updated estimates of the orbits of the Moon and planets. The lunar orbit is known to submeter accuracy through fitting lunar laser ranging data. The orbits of Venus, Earth, and Mars are known to subkilometer accu- racy. Because of perturbations of the orbit of Mars by asteroids, frequent updates are needed to maintain the current accuracy into the future decade. Mercury’s orbit is determined to an accuracy of several kilometers by radar ranging. The orbits of Jupiter and Saturn are determined to accuracies of tens of kilometers as a result of spacecraft tracking and modern ground-based astrometry. The orbits of Uranus, Neptune, and Pluto are not as well deter- mined. Reprocessing of historical observations is expected to lead to improvements in their orbits in the next several years. I. Introduction The planetary and lunar ephemeris DE 421 is a significant advance over earlier ephemeri- des. Compared with DE 418, released in July 2007,1 the DE 421 ephemeris includes addi- tional data, especially range and very long baseline interferometry (VLBI) measurements of Mars spacecraft; range measurements to the European Space Agency’s Venus Express space- craft; and use of current best estimates of planetary masses in the integration process. The lunar orbit is more robust due to an expanded set of lunar geophysical solution parameters, seven additional months of laser ranging data, and complete convergence.
    [Show full text]
  • Planets Solar System Paper Contents
    Planets Solar system paper Contents 1 Jupiter 1 1.1 Structure ............................................... 1 1.1.1 Composition ......................................... 1 1.1.2 Mass and size ......................................... 2 1.1.3 Internal structure ....................................... 2 1.2 Atmosphere .............................................. 3 1.2.1 Cloud layers ......................................... 3 1.2.2 Great Red Spot and other vortices .............................. 4 1.3 Planetary rings ............................................ 4 1.4 Magnetosphere ............................................ 5 1.5 Orbit and rotation ........................................... 5 1.6 Observation .............................................. 6 1.7 Research and exploration ....................................... 6 1.7.1 Pre-telescopic research .................................... 6 1.7.2 Ground-based telescope research ............................... 7 1.7.3 Radiotelescope research ................................... 8 1.7.4 Exploration with space probes ................................ 8 1.8 Moons ................................................. 9 1.8.1 Galilean moons ........................................ 10 1.8.2 Classification of moons .................................... 10 1.9 Interaction with the Solar System ................................... 10 1.9.1 Impacts ............................................ 11 1.10 Possibility of life ........................................... 12 1.11 Mythology .............................................
    [Show full text]
  • Yarkovsky-Driven Spreading of the Eureka Family of Mars Trojans
    Icarus 252 (2015) 339–346 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Yarkovsky-driven spreading of the Eureka family of Mars Trojans a, b c Matija C´ uk *, Apostolos A. Christou , Douglas P. Hamilton a Carl Sagan Center, SETI Institute, 189 North Bernardo Avenue, Mountain View, CA 94043, United States b Armagh Observatory, College Hill, Armagh BT61 9DG, NI, United Kingdom c Department of Astronomy, University of Maryland, 1113 Physical Sciences Complex, Bldg. 415, College Park, MD 20742, United States a r t i c l e i n f o a b s t r a c t Article history: Out of nine known stable Mars Trojans, seven appear to be members of an orbital grouping including the Received 3 December 2014 largest Trojan, Eureka. In order to test if this could be a genetic family, we simulated the long term evo- Revised 6 February 2015 lution of a tight orbital cluster centered on Eureka. We explored two cases: cluster dispersal through pla- Accepted 7 February 2015 netary gravity alone over 1 Gyr, and a 1 Gyr evolution due to both gravity and the Yarkovsky effect. We Available online 17 February 2015 find that the dispersal of the cluster in eccentricity is primarily due to dynamical chaos, while the incli- nations and libration amplitudes are primarily changed by the Yarkovsky effect. Current distribution of Keywords: the cluster members orbits is indicative of an initially tight orbital grouping that was affected by a nega- Asteroids tive acceleration (i.e. one against the orbital motion) consistent with the thermal Yarkovsky effect.
    [Show full text]
  • The Minor Planet Bulletin, We Feel Safe in Al., 1989)
    THE MINOR PLANET BULLETIN OF THE MINOR PLANETS SECTION OF THE BULLETIN ASSOCIATION OF LUNAR AND PLANETARY OBSERVERS VOLUME 43, NUMBER 3, A.D. 2016 JULY-SEPTEMBER 199. PHOTOMETRIC OBSERVATIONS OF ASTEROIDS star, and asteroid were determined by measuring a 5x5 pixel 3829 GUNMA, 6173 JIMWESTPHAL, AND sample centered on the asteroid or star. This corresponds to a 9.75 (41588) 2000 SC46 by 9.75 arcsec box centered upon the object. When possible, the same comparison star and check star were used on consecutive Kenneth Zeigler nights of observation. The coordinates of the asteroid were George West High School obtained from the online Lowell Asteroid Services (2016). To 1013 Houston Street compensate for the effect on the asteroid’s visual magnitude due to George West, TX 78022 USA ever changing distances from the Sun and Earth, Eq. 1 was used to [email protected] vertically align the photometric data points from different nights when constructing the composite lightcurve: Bryce Hanshaw 2 2 2 2 George West High School Δmag = –2.5 log((E2 /E1 ) (r2 /r1 )) (1) George West, TX USA where Δm is the magnitude correction between night 1 and 2, E1 (Received: 2016 April 5 Revised: 2016 April 7) and E2 are the Earth-asteroid distances on nights 1 and 2, and r1 and r2 are the Sun-asteroid distances on nights 1 and 2. CCD photometric observations of three main-belt 3829 Gunma was observed on 2016 March 3-5. Weather asteroids conducted from the George West ISD Mobile conditions on March 3 and 5 were not particularly favorable and so Observatory are described.
    [Show full text]
  • The List of Asteroids Perturbing the Mars Orbit to Be Seen During Future Space Missions
    A&A 508, 479–489 (2009) Astronomy DOI: 10.1051/0004-6361/200810979 & c ESO 2009 Astrophysics The list of asteroids perturbing the Mars orbit to be seen during future space missions S. Mouret1,2,J.L.Simon2,F.Mignard3, and D. Hestroffer2 1 Lohrmann Observatory, Dresden Technical University, Institute for Planetary Geodesy, 01062 Dresden, Germany e-mail: [email protected] 2 IMCCE, UMR CNRS 8028, Paris observatory, 77 Av. Denfert-Rochereau, 75014 Paris, France e-mail: [simon;hestroffer]@imcce.fr 3 OCA/Cassiopée, UMR CNRS 6062, Observatory of the Côte d’Azur, Le Mont Gros, BP 4229, 06304 Nice Cedex 4, France e-mail: [email protected] Received 17 September 2008 / Accepted 6 July 2009 ABSTRACT Context. Over the last decade, the positional observations of Mars have reached such an accuracy that the uncertainty of the asteroid masses has become the main cause of uncertainty in its ephemeris. Currently, only about 36 masses are estimated by direct measure- ments with a formal accuracy better than 10%. However, the true errors are probably larger due to unaccounted systematic effects. Thus, asteroid masses are still a limitation in the accurate modeling of the perturbations on Mars. Nevertheless, two future space missions, Gaia and Dawn, could improve the situation by combining their results. Aims. The main objective of this paper is to identify and provide a list of major perturbers of Mars which could bring significant disturbances over the next 50 years, having in perspective the expected contribution of Gaia to asteroid mass determination. It will also point out the asteroids whose mass only could be improved from ground-based observations – by direct measurements or size and shape derivation.
    [Show full text]