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Mass of the Kuiper Belt · 9Th Planet PACS 95.10.Ce · 96.12.De · 96.12.Fe · 96.20.-N · 96.30.-T
Celestial Mechanics and Dynamical Astronomy manuscript No. (will be inserted by the editor) Mass of the Kuiper Belt E. V. Pitjeva · N. P. Pitjev Received: 13 December 2017 / Accepted: 24 August 2018 The final publication ia available at Springer via http://doi.org/10.1007/s10569-018-9853-5 Abstract The Kuiper belt includes tens of thousands of large bodies and millions of smaller objects. The main part of the belt objects is located in the annular zone between 39.4 au and 47.8 au from the Sun, the boundaries correspond to the average distances for orbital resonances 3:2 and 2:1 with the motion of Neptune. One-dimensional, two-dimensional, and discrete rings to model the total gravitational attraction of numerous belt objects are consid- ered. The discrete rotating model most correctly reflects the real interaction of bodies in the Solar system. The masses of the model rings were determined within EPM2017—the new version of ephemerides of planets and the Moon at IAA RAS—by fitting spacecraft ranging observations. The total mass of the Kuiper belt was calculated as the sum of the masses of the 31 largest trans-neptunian objects directly included in the simultaneous integration and the estimated mass of the model of the discrete ring of TNO. The total mass −2 is (1.97 ± 0.30) · 10 m⊕. The gravitational influence of the Kuiper belt on Jupiter, Saturn, Uranus and Neptune exceeds at times the attraction of the hypothetical 9th planet with a mass of ∼ 10 m⊕ at the distances assumed for it. -
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. -
Planetary Defence Activities Beyond NASA and ESA
Planetary Defence Activities Beyond NASA and ESA Brent W. Barbee 1. Introduction The collision of a significant asteroid or comet with Earth represents a singular natural disaster for a myriad of reasons, including: its extraterrestrial origin; the fact that it is perhaps the only natural disaster that is preventable in many cases, given sufficient preparation and warning; its scope, which ranges from damaging a city to an extinction-level event; and the duality of asteroids and comets themselves---they are grave potential threats, but are also tantalising scientific clues to our ancient past and resources with which we may one day build a prosperous spacefaring future. Accordingly, the problems of developing the means to interact with asteroids and comets for purposes of defence, scientific study, exploration, and resource utilisation have grown in importance over the past several decades. Since the 1980s, more and more asteroids and comets (especially the former) have been discovered, radically changing our picture of the solar system. At the beginning of the year 1980, approximately 9,000 asteroids were known to exist. By the beginning of 2001, that number had risen to approximately 125,000 thanks to the Earth-based telescopic survey efforts of the era, particularly the emergence of modern automated telescopic search systems, pioneered by the Massachusetts Institute of Technology’s (MIT’s) LINEAR system in the mid-to-late 1990s.1 Today, in late 2019, about 840,000 asteroids have been discovered,2 with more and more being found every week, month, and year. Of those, approximately 21,400 are categorised as near-Earth asteroids (NEAs), 2,000 of which are categorised as Potentially Hazardous Asteroids (PHAs)3 and 2,749 of which are categorised as potentially accessible.4 The hazards posed to us by asteroids affect people everywhere around the world. -
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. -
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. -
Visions of the Universe: Four Centuries of Discovery One-Hour
Visions of the Universe: Four Centuries of Discovery One-Hour Exhibit Tour / Program “Visions of the Universe: Four Centuries of Discovery” was produced in December 2008 by the Space Telescope Science Institute, the American Library Association, and the Smithsonian Astrophysical Observatory, through funding from the National Aeronautics and Space Administration. Some guidelines from NGS standards 2nd – 4th grade: Science and Engineering Practices - Constructing Explanations and Designing Solutions - Constructing explanations and designing solutions in K–2 builds on prior experiences and progresses to the use of evidence and ideas in constructing evidence-based accounts of natural phenomena and designing solutions. - Make observations from several sources to construct an evidence-based account for natural phenomena. Disciplinary Core Ideas The History of Planet Earth – Some events happen very quickly; others occur very slowly, over a time period much longer than one can observe. Crosscutting Concepts Stability and Change – Things may change slowly or rapidly. In this program, the educator will guide a group through the “Visions of the Universe” exhibit, which consists of 12 panels mounted on foam board. Reading the text of each poster, and showing the depictions of space objects, exploration and achievements, the educator will present a big-picture view of the history of astronomy. At certain points, depending on time and group, you may connect the concepts of a given poster to one of the suggested “Earth and Space” activities. Refer to the supplemental materials in the “Visions of the Universe” binder for the background knowledge you will need to answer any questions that may come up! I. Visions of the Universe Intro “Telescopes have transformed not only our views of the universe, but also our understanding of the planets, stars, and galaxies within it.” After reading the poster, pause to let kids look through one of our Galileoscopes. -
Volume 1, #1 2021 May 14 Published on Behalf of the International Astronomical Union by the WG Small Bodies Nomenclature
Volume 1, #1 2021 May 14 Published on behalf of the International Astronomical Union by the WG Small Bodies Nomenclature. ISSN <applied for> Cover image: Navigation image of (1) Ceres, obtained by the DAWN mission. Courtesy NASA/JPL-CALTECH. WGSBN Bull. 1, #1 Table of Contents Editorial Notice.....................................................................................................................8 New Names of Minor Planets...............................................................................................8 (3708) Socus = 1974 FV1...............................................................................................9 (4035) Thestor = 1986 WD1...........................................................................................9 (4489) Dracius = 1988 AK..............................................................................................9 (4715) Medesicaste = 1989 TS1.....................................................................................9 (5258) Rhoeo = 1989 AU1..............................................................................................9 (5311) Rutherford = 1981 GD1.......................................................................................9 (5346) Benedetti = 1981 QE3.........................................................................................9 (5648) Axius = 1990 VU1...............................................................................................9 (5766) Carmelofalco = 1986 QR3..................................................................................9 -
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. -
Alien Encounters and the Alien/Human Dichotomy in Stanley Kubrick's <Em>2001: a Space Odyssey</Em> and Andrei Tark
University of South Florida Scholar Commons Graduate Theses and Dissertations Graduate School 4-1-2010 Alien Encounters and the Alien/Human Dichotomy in Stanley Kubrick‘s 2001: A Space Odyssey and Andrei Tarkovsky‘s Solaris Keith Cavedo University of South Florida Follow this and additional works at: https://scholarcommons.usf.edu/etd Part of the American Studies Commons Scholar Commons Citation Cavedo, Keith, "Alien Encounters and the Alien/Human Dichotomy in Stanley Kubrick‘s 2001: A Space Odyssey and Andrei Tarkovsky‘s Solaris" (2010). Graduate Theses and Dissertations. https://scholarcommons.usf.edu/etd/1593 This Dissertation is brought to you for free and open access by the Graduate School at Scholar Commons. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Scholar Commons. For more information, please contact [email protected]. Alien Encounters and the Alien/Human Dichotomy in Stanley Kubrick‘s 2001: A Space Odyssey and Andrei Tarkovsky‘s Solaris by Keith Cavedo A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy Department of English College of Arts and Sciences University of South Florida Major Professor: Phillip Sipiora, Ph.D. Lawrence Broer, Ph.D. Victor Peppard, Ph.D. Silvio Gaggi, Ph.D. Date of Approval: April 1, 2010 Keywords: Film Studies, Science Fiction Studies, Alien Identity, Human Identity © Copyright 2010, Keith Cavedo Dedication I dedicate this scholarly enterprise with all my heart to my parents, Vicki McCook Cavedo and Raymond Bernard Cavedo, Jr. for their unwavering love, support, and kindness through many difficult years. Each in their own way a lodestar, my parents have guided me to my particular destination. -
Planet Earth Taken by Hayabusa-2
Space Science in JAXA Planet Earth May 15, 2017 taken by Hayabusa-2 Saku Tsuneta, PhD JAXA Vice President Director General, Institute of Space and Astronautical Science 2017 IAA Planetary Defense Conference, May 15-19,1 Tokyo 1 Brief Introduction of Space Science in JAXA Introduction of ISAS and JAXA • As a national center of space science & engineering research, ISAS carries out development and in-orbit operation of space science missions with other directorates of JAXA. • ISAS is an integral part of JAXA, and has close collaboration with other directorates such as Research and Development and Human Spaceflight Technology Directorates. • As an inter-university research institute, these activities are intimately carried out with universities and research institutes inside and outside Japan. ISAS always seeks for international collaboration. • Space science missions are proposed by researchers, and incubated by ISAS. ISAS plays a strategic role for mission selection primarily based on the bottom-up process, considering strategy of JAXA and national space policy. 3 JAXA recent science missions HAYABUSA 2003-2010 AKARI(ASTRO-F)2006-2011 KAGUYA(SELENE)2007-2009 Asteroid Explorer Infrared Astronomy Lunar Exploration IKAROS 2010 HAYABUSA2 2014-2020 M-V Rocket Asteroid Explorer Solar Sail SUZAKU(ASTRO-E2)2005- AKATSUKI 2010- X-Ray Astronomy Venus Meteorogy ARASE 2016- HINODE(SOLAR-B)2006- Van Allen belt Solar Observation Hisaki 2013 4 Planetary atmosphere Close ties between space science and space technology Space Technology Divisions Space -
Design and Validation of a Compact Radius Centrifuge Artificial Gravity Test Platform
Design and Validation of a Compact Radius Centrifuge Artificial Gravity Test Platform by Chris Trigg B.S. Environmental Engineering Northwestern University, 2008 M.S. Environmental Engineering Stanford University, 2009 SUBMITTED TO THE DEPARTMENT OF AERONAUTICS AND ASTRONAUTICS IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN AERONAUTICS AND ASTRONAUTICS AT THE MASSACHUSETTS INSTITUTE OF TEHCNOLOGY MAY 2013 ©2013 Massachusetts Institute of Technology All Rights Reserved Signature of Author: ____________________________________________________________________ Department of Aeronautics and Astronautics May 23, 2013 Certified by: __________________________________________________________________________ Prof. Laurence R. Young Apollo Program Professor of Astronautics Professor of Health Sciences and Technology Thesis Supervisor Accepted by: __________________________________________________________________________ Prof. Eytan H. Modiano Professor of Aeronautics and Astronautics Chair, Graduate Program Committee 2 Design and Validation of a Compact Radius Centrifuge Artificial Gravity Test Platform by Chris Trigg Submitted to the Department of Aeronautics and Astronautics on 23 May, 2013 in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aeronautics and Astronautics ABSTRACT Intermittent exposure to artificial gravity on a short radius centrifuge (SRC) with exercise is a promising, comprehensive countermeasure to the cardiovascular and musculoskeletal deconditioning that occurs as a result of prolonged exposure to microgravity. To date, the study of artificial gravity has been done using bedrest and SRC’s with subjects positioned radially with the head at the center of rotation. A recent proposal to put a human centrifuge on the International Space Station (ISS) highlighted the reality that near-term inflight SRC’s will likely be confined to radii shorter than has been typically used in terrestrial analogs. -
J. Lee1,2, D.-H. Kim1,2, F. Yoshida3, S.-M
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 1497.pdf ROTATIONAL AND SURFACE PROPERTIES OF NEA 3200 PHAETHON. M.-J. Kim1, H.-J. Lee1,2, D.-H. Kim1,2, F. Yoshida3, S.-M. Lee1,2, P. Bartczak4, G. Dudzinski4, J. Park1, Y.-J. Choi1,5, H.-K. Moon1, C.-H. Kim2, H.- S. Yim1, J. Choi1, E.-J. Choi1, J.-N. Yoon6, A. Serebryanskiy7, M. Krugov7, I. Reva7, K. E. Ergashev8, O. Burkhonov8, S. A. Ehgamberdiev8, Y. Turayev8, Z.-Y. Lin9, T. Arai3, K. Ohtsuka10, T. Ito11, S. Urakawa12, M. Ishi- guro13, B.-C. Lee1, D.-G. Roh1, and H.Seo1,14, 1Korea Astronomy and Space Science Institute, 776, Daedeokdae-ro, Yuseong-gu, Daejeon 34055, Korea, [email protected], 2Chungbuk National University, 1 Chungdae-ro, Seowon- gu, Cheongju, Chungbuk 28644, Korea, 3Planetary Exploration Research Center, Chiba Institute of Technology, 2- 17-1 Tsudanuma, Narashino, Chiba 275-0016, Japan, 4Astronomical Observatory Institute, Faculty of Physics, Adam Mickiewicz University, Słoneczna 36, 60-286 Poznan, Poland, 5University of Science and Technology, 217, Gajeong-ro, Yuseong-gu, Daejeon 34113, Korea, 6Chungbuk National University Observatory, 802-3 Euntan-ri, Jincheon-gun, Chungcheongbuk-do, Korea, 7Fesenkov Astrophysical Institute, Observatory 23, 050020 Almaty, Ka- zakhstan, 8Ulugh Beg Astronomical Institute of the Uzbekistan Academy of Sciences, 33 Astronomicheskaya str., Tashkent, 100052, Uzbekistan, 9Institute of Astronomy, National Central University, No. 300, Zhongda Rd., Zhongli Dist., Taoyuan City 32001, Taiwan, 10Tokyo Meteor Network, Daisawa 1–27–5, Setagaya-ku, Tokyo 155–0032, Japan, 11National Astronomical Observatory of Japan, Osawa 2-21-1, Mitaka, Tokyo 181-8588, Japan, 12Japan Spaceguard Association, Bisei Spaceguard Center, 1716-3 Okura, Bisei-cho, Ibara, Okayama 714-1411, Japan, 13Seoul National University, 1 Gwanak-ro, Gwanak-gu, Seoul 08826, Korea, 14Intelligence in Space, 96 Gajeongbuk- ro, Yuseong-gu, Daejeon, 34111, Korea.