The Halloween Asteroid Prepares to Return in 2018
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Observational Constraints on Surface Characteristics of Comet Nuclei
Observational Constraints on Surface Characteristics of Comet Nuclei Humberto Campins ([email protected] u) Lunar and Planetary Laboratory, University of Arizona Yanga Fernandez University of Hawai'i Abstract. Direct observations of the nuclear surfaces of comets have b een dicult; however a growing number of studies are overcoming observational challenges and yielding new information on cometary surfaces. In this review, we fo cus on recent determi- nations of the alb edos, re ectances, and thermal inertias of comet nuclei. There is not much diversity in the geometric alb edo of the comet nuclei observed so far (a range of 0.025 to 0.06). There is a greater diversity of alb edos among the Centaurs, and the sample of prop erly observed TNOs (2) is still to o small. Based on their alb edos and Tisserand invariants, Fernandez et al. (2001) estimate that ab out 5% of the near-Earth asteroids have a cometary origin, and place an upp er limit of 10%. The agreement between this estimate and two other indep endent metho ds provide the strongest constraint to date on the fraction of ob jects that comets contribute to the p opulation of near-Earth asteroids. There is a diversity of visible colors among comets, extinct comet candidates, Centaurs and TNOs. Comet nuclei are clearly not as red as the reddest Centaurs and TNOs. What Jewitt (2002) calls ultra-red matter seems to be absent from the surfaces of comet nuclei. Rotationally resolved observations of b oth colors and alb edos are needed to disentangle the e ects of rotational variability from other intrinsic qualities. -
Photometric Study of Two Near-Earth Asteroids in the Sloan Digital Sky Survey Moving Objects Catalog
University of North Dakota UND Scholarly Commons Theses and Dissertations Theses, Dissertations, and Senior Projects January 2020 Photometric Study Of Two Near-Earth Asteroids In The Sloan Digital Sky Survey Moving Objects Catalog Christopher James Miko Follow this and additional works at: https://commons.und.edu/theses Recommended Citation Miko, Christopher James, "Photometric Study Of Two Near-Earth Asteroids In The Sloan Digital Sky Survey Moving Objects Catalog" (2020). Theses and Dissertations. 3287. https://commons.und.edu/theses/3287 This Thesis is brought to you for free and open access by the Theses, Dissertations, and Senior Projects at UND Scholarly Commons. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of UND Scholarly Commons. For more information, please contact [email protected]. PHOTOMETRIC STUDY OF TWO NEAR-EARTH ASTEROIDS IN THE SLOAN DIGITAL SKY SURVEY MOVING OBJECTS CATALOG by Christopher James Miko Bachelor of Science, Valparaiso University, 2013 A Thesis Submitted to the Graduate Faculty of the University of North Dakota in partial fulfillment of the requirements for the degree of Master of Science Grand Forks, North Dakota August 2020 Copyright 2020 Christopher J. Miko ii Christopher J. Miko Name: Degree: Master of Science This document, submitted in partial fulfillment of the requirements for the degree from the University of North Dakota, has been read by the Faculty Advisory Committee under whom the work has been done and is hereby approved. ____________________________________ Dr. Ronald Fevig ____________________________________ Dr. Michael Gaffey ____________________________________ Dr. Wayne Barkhouse ____________________________________ Dr. Vishnu Reddy ____________________________________ ____________________________________ This document is being submitted by the appointed advisory committee as having met all the requirements of the School of Graduate Studies at the University of North Dakota and is hereby approved. -
Thermophysical Modeling of 99942 Apophis: Estimations of Surface Temperature During the April 2029 Close Approach
Apophis T–9 Years 2020 (LPI Contrib. No. 2242) 2069.pdf THERMOPHYSICAL MODELING OF 99942 APOPHIS: ESTIMATIONS OF SURFACE TEMPERATURE DURING THE APRIL 2029 CLOSE APPROACH. K. C. Sorli1 and P. O. Hayne1, 1Laboratory for Atmospheric and Space Physics – University of Colorado Boulder, CO 80303 ([email protected]) Introduction: The April 13, 2029 close approach purposes of calculating temperatures and thermal IR of the ~350-meter asteroid 99942 Apophis offers an fluxes. Our predictions for surface temperatures and unprecedented opportunity to observe a large near-Earth dynamical effects will be directly testable during the asteroid in detail with ground-based observatories. As Janus mission, with an anticipated launch date of 2022. one of the best-studied hazardous objects, with Though the model was constructed with the intent of additional near-miss flybys in coming decades, it is categorizing binary thermal and dynamical behaviors, crucial to planetary defense to understand its properties including binary YORP [5][6], it is easily adaptable to and potential perturbations to its orbit. solitary asteroids. Apophis has been the subject of extensive study, and This model begins by coupling a 1-d thermophysical will continue to be so for years to come. This existing model [7] to a 3-d shape model and computing facet-by- knowledge and the promise of new data makes it an facet temperatures of the surface and near subsurface excellent candidate for modeling subject to during the time period of Apophis’s 2029 close observational constraints. The 2029 close approach will approach. To calculate temperatures, the model is given have a sizable amplifying effect on Apophis’ orbital information about the incoming solar flux on each facet uncertainty, so small dynamical perturbations will be as a function of solar distance and is set to equilibrate required to understand both the conditions of the 2029 for 1 year to allow for subsurface temperature settling. -
An Estimate of the Flux of Apophis-Particle Meteors at Earth
Apophis T–9 Years 2020 (LPI Contrib. No. 2242) 2075.pdf An Estimate of the Flux of Apophis-Particle Meteors at Earth 1 1 2 Robert Melikyan , Beth Ellen Clark , Carl Hergenrother 1 D epartment of Physics and Astronomy, Ithaca College, Ithaca, NY, USA. 2 L unar and Planetary Laboratory, University of Arizona, Tucson, AZ, USA. Near-Earth asteroid (99942) Apophis is meteoroid stream is propagated between 1900 - predicted to make a close encounter with Earth 2029 using an Apophis ephemeris that places the on April 13, 2029. This close encounter will asteroid at its most likely position for the 2029 bring Apophis within 6 Earth radii from our encounter. Unlike most meteoroid stream geocenter providing an excellent opportunity to evolution studies, our simulations release study and observe the asteroid and any particles from Apophis at a regular (~weekly) subsequent effects of the interaction. Here, we rate around its entire orbit, consistent with the bring to your attention the possibility that the Bennu observations. passage of Apophis will not be the only event worth observing. We predict a rain of Apophis Assuming similar particle production meteors that may be detectable to Earth’s meteor mechanisms at Apophis as observed at Bennu, monitoring systems. Apophis could be producing on order of 104 grams of material continuously throughout its NASA’s OSIRIS-REx mission has orbit. Of that material, we assume 30% will recently shown that near-Earth asteroid (101955) escape on hyperbolic trajectories [6]. This Bennu has been continuously producing results in roughly 3500 grams of new material 4 cm-sized ejecta at rates of ~10 grams per orbit entering the Apophis meteoroid stream annually. -
Comet Section Observing Guide
Comet Section Observing Guide 1 The British Astronomical Association Comet Section www.britastro.org/comet BAA Comet Section Observing Guide Front cover image: C/1995 O1 (Hale-Bopp) by Geoffrey Johnstone on 1997 April 10. Back cover image: C/2011 W3 (Lovejoy) by Lester Barnes on 2011 December 23. © The British Astronomical Association 2018 2018 December (rev 4) 2 CONTENTS 1 Foreword .................................................................................................................................. 6 2 An introduction to comets ......................................................................................................... 7 2.1 Anatomy and origins ............................................................................................................................ 7 2.2 Naming .............................................................................................................................................. 12 2.3 Comet orbits ...................................................................................................................................... 13 2.4 Orbit evolution .................................................................................................................................... 15 2.5 Magnitudes ........................................................................................................................................ 18 3 Basic visual observation ........................................................................................................ -
Small Satellite Rendezvous and Characterization of Asteroid 99942 Apophis
SSC09-IV-3 Small Satellite Rendezvous and Characterization of Asteroid 99942 Apophis James Chartres Carnegie Mellon Innovations Laboratory, Carnegie Mellon University Silicon Valley Small Spacecraft Office, NASA Ames Research Center Building 202, Moffett Field, CA 94035; (650) 604-6347 [email protected] David Dunham, Bobby Williams Space Navigation and Flight Dynamics, KinetX, Inc. 2050 E. ASU Circle, Suite 107, Tempe, AZ 85284; (480) 829-6600 [email protected], [email protected] Anthony Genova, Anthony Colaprete, Ronald Johnson, Belgacem Jaroux Small Spacecraft Office, NASA Ames Research Center Building 202, Moffett Field, CA 94035; (650) 604-6347, (650) 604-2918, (650) 604-6699, (650) 604-6312 [email protected], [email protected], [email protected], [email protected] ABSTRACT The Measurement and Analysis of Apophis Trajectory (MAAT) concept study investigated a low-cost characterization mission to the asteroid 99942 Apophis that leverage small spacecraft architectures and technologies. The mission goals were to perform physical characterization and improve the orbital model. The MAAT mission uses a small spacecraft free flyer and a bi-propellant transfer stage that can be incorporated as a secondary payload on Evolved Expendable Launch Vehicles (EELVs), Atlas V or Delta IV launches. Using the innovative secondary architecture allows the system to be launched on numerous GTO or LTO opportunities such as NASA science missions or commercial communication satellites. The trajectory takes advantage of the reduced Delta-V requirement during the 2012- 2015 time frame, with a large flexible launch opportunity, from January to November 2012 and heliocentric injection occurs in April 2013. -
Radar Images Provide Details on Halloween Asteroid 4 November 2015
Radar images provide details on Halloween asteroid 4 November 2015 California, to transmit high-power microwaves toward the asteroid. The signal bounced off the asteroid, and its radar echoes were received by the National Radio Astronomy Observatory's (NRAO) 100-meter (330-foot) Green Bank Telescope in West Virginia. The radar images achieve a spatial resolution as fine as 13 feet (4 meters) per pixel. The radar images were taken as the asteroid flew past Earth on October 31 at 1 p.m. EDT at about 1.3 lunar distances (300,000 miles, or 480,000 kilometers) from Earth. Asteroid 2015 TB145 is spherical in shape and approximately 2,000 feet (600 meters) in diameter. "The radar images of asteroid 2015 TB145 show Asteroid 2015 TB145 is depicted in eight individual radar portions of the surface not seen previously and images collected on Oct. 31, 2015 between 5:55 a.m. PDT (8:55 a.m. EDT) and 6:08 a.m. PDT (9:08 a.m. reveal pronounced concavities, bright spots that EDT). At the time the radar images were taken, the might be boulders, and other complex features that asteroid was between 440,000 miles (710,000 could be ridges," said Lance Benner of NASA's Jet kilometers) and about 430,000 miles (690,000 Propulsion Laboratory in Pasadena, California, who kilometers) distant. Asteroid 2015 TB145 safely flew past leads NASA's asteroid radar research program. Earth on Oct. 31, at 10:00 a.m. PDT (1 p.m. EDT) at "The images look distinctly different from the about 1.3 lunar distances (300,000 miles, 480,000 Arecibo radar images obtained on October 30 and kilometers). -
User Provided Data Product Upload of Herschel/PACS Near-Earth Asteroid Observations (Release Note)
Small Bodies: Near and Far NEA HSA UPDP upload User Provided Data Product upload of Herschel/PACS near-Earth asteroid observations (release note) Small Bodies: Near and Far; 687378 – SBNAF – RIA Cs. Kiss1, T.G. M¨uller2, and the SBNAF team 1Konkoly Observatory, Research Centre for Astronomy and Earth Sciences, Hungarian Academy of Sciences, Konkoly Thege 15-17, H-1121 Budapest, Hungary 2Max-Planck-Institut f¨ur extraterrestrische Physik, Giessenbachstrasse 1, D-85748 Garching, Germany Version 1.0 (as of December 29, 2016) Contents 1 Introduction 2 2 Herschel Space Observatory 2 3 Near-Earth asteroid observations 2 4 Data reduction and calibration 3 5Results 3 5.1 (101955) Bennu . 5 5.2 175706 (1996 FG 3) . 5 5.3 308635 (2005 YU 55) . 5 5.4 (162173) Ryugu . 6 5.5 (99942) Apophis . 6 References 7 Appendix 8 Summary of uploaded data products . 8 Summary of additional FITS keywords . 11 Page 1 Small Bodies: Near and Far NEA HSA UPDP upload 1 Introduction SMALL BODIES: NEAR AND FAR is a Horizon 2020 project (project number: 687378) that addresses critical points in reconstructing physical and thermal properties of near- Earth, main-belt, and trans-Neptunian objects (see the project webpage for details: http://www.mpe.mpg.de/ tmueller/sbnaf/). One of the goals of the SBNAF project is to produce a set of high-quality data products for Herschel observations of Solar System objects for an upload to the Herschel Science Archive (HSA). These new products will then be available for the entire scientific community, in parallel to the standard pipeline-processed Herschel archive data. -
The Atlantic Online | June 2008 | the Sky Is Falling | Gregg Easterbrook
The Atlantic Online | June 2008 | The Sky Is Falling | Gregg Easter... http://www.theatlantic.com/doc/print/200806/asteroids Print this Page Close Window JUNE 2008 ATLANTIC MONTHLY The odds that a potentially devastating space rock will hit Earth this century may be as high as one in 10. So why isn’t NASA trying harder to prevent catastrophe? BY GREGG EASTERBROOK The Sky Is Falling Image credit: Stéphane Guisard, www.astrosurf.com/sguisard ALSO SEE: reakthrough ideas have a way of seeming obvious in retrospect, and about a decade ago, a B Columbia University geophysicist named Dallas Abbott had a breakthrough idea. She had been pondering the craters left by comets and asteroids that smashed into Earth. Geologists had counted them and concluded that space strikes are rare events and had occurred mainly during the era of primordial mists. But, Abbott realized, this deduction was based on the number of craters found on land—and because 70 percent of Earth’s surface is water, wouldn’t most space objects hit the sea? So she began searching for underwater craters caused by impacts VIDEO: "TARGET EARTH" rather than by other forces, such as volcanoes. What she has found is spine-chilling: evidence Gregg Easterbrook leads an illustrated that several enormous asteroids or comets have slammed into our planet quite recently, in tour through the treacherous world of space rocks. geologic terms. If Abbott is right, then you may be here today, reading this magazine, only because by sheer chance those objects struck the ocean rather than land. Abbott believes that a space object about 300 meters in diameter hit the Gulf of Carpentaria, north of Australia, in 536 A.D. -
Head-On Impact Deflection of Neas: a Case Study for 99942 Apophis
Planetary Defense Conference 2007, Wahington D.C., USA, 05-08 March 2007 (c) 2007 by the authors Head-On Impact Deflection of NEAs: A Case Study for 99942 Apophis Bernd Dachwald∗ and Ralph Kahle† German Aerospace Center (DLR), 82234 Wessling, Germany Bong Wie‡ Arizona State University, Tempe, AZ 85287, USA Near-Earth asteroid (NEA) 99942 Apophis provides a typical example for the evolution of asteroid orbits that lead to Earth-impacts after a close Earth-encounter that results in a resonant return. Apophis will have a close Earth-encounter in 2029 with potential very close subsequent Earth-encounters (or even an impact) in 2036 or later, depending on whether it passes through one of several less than 1 km-sized gravitational keyholes during its 2029- encounter. A pre-2029 kinetic impact is a very favorable option to nudge the asteroid out of a keyhole. The highest impact velocity and thus deflection can be achieved from a trajectory that is retrograde to Apophis orbit. With a chemical or electric propulsion system, however, many gravity assists and thus a long time is required to achieve this. We show in this paper that the solar sail might be the better propulsion system for such a mission: a solar sail Kinetic Energy Impactor (KEI) spacecraft could impact Apophis from a retrograde trajectory with a very high relative velocity (75-80 km/s) during one of its perihelion passages. The spacecraft consists of a 160 m × 160 m, 168 kg solar sail assembly and a 150 kg impactor. Although conventional spacecraft can also achieve the required minimum deflection of 1 km for this approx. -
Oort Cloud and Scattered Disc Formation During a Late Dynamical Instability in the Solar System ⇑ R
Icarus 225 (2013) 40–49 Contents lists available at SciVerse ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Oort cloud and Scattered Disc formation during a late dynamical instability in the Solar System ⇑ R. Brasser a, , A. Morbidelli b a Institute of Astronomy and Astrophysics, Academia Sinica, P.O. Box 23-141, Taipei 106, Taiwan b Departement Lagrange, University of Nice – Sophia Antipolis, CNRS, Observatoire de la Côte d’Azur, Nice, France article info abstract Article history: One of the outstanding problems of the dynamical evolution of the outer Solar System concerns the Received 11 January 2012 observed population ratio between the Oort cloud (OC) and the Scattered Disc (SD): observations suggest Revised 21 January 2013 that this ratio lies between 100 and 1000 but simulations that produce these two reservoirs simulta- Accepted 11 March 2013 neously consistently yield a value of the order of 10. Here we stress that the populations in the OC Available online 2 April 2013 and SD are inferred from the observed fluxes of new long period comets (LPCs) and Jupiter-family comets (JFCs), brighter than some reference total magnitude. However, the population ratio estimated in the sim- Keywords: ulations of formation of the SD and OC refers to objects bigger than a given size. There are multiple indi- Origin, Solar System cations that LPCs are intrinsically brighter than JFCs, i.e. an LPC is smaller than a JFC with the same total Comets, Dynamics Planetary dynamics absolute magnitude. When taking this into account we revise the SD/JFC population ratio from our sim- ulations relative to Duncan and Levison (1997), and then deduce from the observations that the size-lim- þ54 ited population ratio between the OC and the SD is 44À34. -
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A&A 598, A63 (2017) Astronomy DOI: 10.1051/0004-6361/201629584 & c ESO 2017 Astrophysics Large Halloween asteroid at lunar distance?,?? T. G. Müller1, A. Marciniak2, M. Butkiewicz-B˛ak2, R. Duffard3, D. Oszkiewicz2, H. U. Käufl4, R. Szakáts5, T. Santana-Ros2, C. Kiss5, and P. Santos-Sanz3 1 Max-Planck-Institut für extraterrestrische Physik, Postfach 1312, Giessenbachstraße, 85741 Garching, Germany e-mail: [email protected] 2 Astronomical Observatory Institute, Faculty of Physics, A. Mickiewicz University, Słoneczna 36, 60-286 Poznan,´ Poland 3 Instituto de Astrofísica de Andalucía (CSIC) C/ Camino Bajo de Huétor, 50, 18008 Granada, Spain 4 ESO, Karl-Schwarzschild-Str. 2, 85748 Garching, Germany 5 Konkoly Observatory, Research Center for Astronomy and Earth Sciences, Hungarian Academy of Sciences, Konkoly Thege 15-17, 1121 Budapest, Hungary Received 25 August 2016 / Accepted 20 October 2016 ABSTRACT The near-Earth asteroid (NEA) 2015 TB145 had a very close encounter with Earth at 1.3 lunar distances on October 31, 2015. We obtained 3-band mid-infrared observations of this asteroid with the ESO VLT-VISIR instrument covering approximately four hours in total. We also monitored the visual lightcurve during the close-encounter phase. The NEA has a (most likely) rotation period of 2:939 ± 0:005 h and the visual lightcurve shows a peak-to-peak amplitude of approximately 0:12 ± 0:02 mag. A second rotation period of 4:779 ± 0:012 h, with an amplitude of the Fourier fit of 0:10 ± 0:02 mag, also seems compatible with the available lightcurve measurements. We estimate a V − R colour of 0:56 ± 0:05 mag from different entries in the MPC database.