Precovery Observations Confirm the Capture Time of Asteroid 2020 CD3 As Earth's Minimoon
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Projekt Brána Do Vesmíru
Projekt Brána do vesmíru Hvězdárna Valašské Meziříčí, p. o. Krajská hvezdáreň v Žiline Súčasnosť a budúcnosť výskumu medziplanetárnej hmoty RNDr. Peter Vereš, PhD. University of Hawaii / Univerzita Komenského Ako sa objavila MPH ● Pôvodne iba nehybná hviezdna sféra ● Mesiac a Slnko ● Bludné planéty viditeľné voľným okom Starovek => novovek Piazzi ● 1.1.1801 ● Objekt pozorovaný 41 dní ● Stratený...predpoklad, medzi Marsom a Jupiterom ● Laplace – nemožné nájsť ● Gauss (24) vynašiel metódu, vypočítal, Ceres bol nájdený... Halley ● Kométy, odjakživa považované za poslov zlých správ, vysvetlené ako atmosferické javy ● ● ● ● Názov Kometes (dlhovlasá) ● 1577 Brahe = paralaxa, ďalej ako Mesiac ● Edmond Halley si všimol periodicitu kométy 1531, 1607, 1682 = návrat v 1758 Meteory ● Zaznamenané v -1809, - 687 (Lyridy) ● Ernst Chladni 1794 Kniha o pôvode Pallasovho železa ● 1798 Brandes, Benzenberg, paralaxa 400 meteorov, 22 spoločných ● 1803 dážď / Paríž, priznanie kozmického pôvodu ● 1833 USA dážď 20/s, LEO ● 1845/46 rozpad kométy Biela, dažde Andromedíd (72, 85, 93, 99) ● 1861 = Kirkwood, súvis rojov s kométami ● 1866 Schiaparelli: Swift-Tuttle (Perzeidy), Tempel (Leonidy) ● 1899 Adams vypočítal, že Jupiter narušil dráhu kométy, dážď nebol 1833, rytina, Leonidy 1998, foto, Leonidy, AGO Modra MPH a Slnečná sústava ● Slnko ● planéty (8) ● trpasličie planéty /Ceres, Pluto, Haumea, Makemake, Eris ● MPH = asteroidy, kométy, prach, plyn, .... Vznik a vývoj asteroidov ● -4571mil. rokov – vznik Sl. sús. ● Akrécia hmoty – nehomogenity, planetesimály, „viskózna -
ISTS-2017-D-074ⅠISSFD-2017-074
A look at the capture mechanisms of the “Temporarily Captured Asteroids” of the Earth By Hodei URRUTXUA1) and Claudio BOMBARDELLI2) 1)Astronautics Group, University of Southampton, United Kingdom 2)Space Dynamics Group, Technical University of Madrid, Spain (Received April 17th, 2017) Temporarily captured asteroids of the Earth are a newly discovered family of asteroids, which become naturally captured in the vicinity of the Earth for a limited time period. Thus, during the temporary capture these asteroids are in energetically favorable condi- tions, which makes them appealing targets for space missions to asteroids. Despite their potential interest, their capture mechanisms are not yet fully understood, and basic questions remain unanswered regarding the taxonomy of this population. The present work looks at gaining a better understanding of the key features that are relevant to the duration and nature of these asteroids, by analyzing patterns and extracting conclusions from a synthetic population of temporarily captured asteroids. Key Words: Asteroids, temporarily captured asteroids, capture dynamics, asteroid retrieval. Acronyms system. Asteroid 2006 RH120 is so far the only known mem- ber of this population, though statistical studies by Granvik et TCA : Temporarily captured asteroids al.12) support the evidence that such objects are actually com- TCO : Temporarily captured orbiters mon companions of the Earth, and thus it is expected that an TCF : Temporarily captured fly-bys increasing number of them will be found as survey technology improves.13) 1. Introduction During their temporary capture phase these asteroids are technically orbiting the Earth rather than the Sun, since their The origin of planetary satellites in the Solar System has Earth-binding energy is negative. -
Ice& Stone 2020
Ice & Stone 2020 WEEK 33: AUGUST 9-15 Presented by The Earthrise Institute # 33 Authored by Alan Hale About Ice And Stone 2020 It is my pleasure to welcome all educators, students, topics include: main-belt asteroids, near-Earth asteroids, and anybody else who might be interested, to Ice and “Great Comets,” spacecraft visits (both past and Stone 2020. This is an educational package I have put future), meteorites, and “small bodies” in popular together to cover the so-called “small bodies” of the literature and music. solar system, which in general means asteroids and comets, although this also includes the small moons of Throughout 2020 there will be various comets that are the various planets as well as meteors, meteorites, and visible in our skies and various asteroids passing by Earth interplanetary dust. Although these objects may be -- some of which are already known, some of which “small” compared to the planets of our solar system, will be discovered “in the act” -- and there will also be they are nevertheless of high interest and importance various asteroids of the main asteroid belt that are visible for several reasons, including: as well as “occultations” of stars by various asteroids visible from certain locations on Earth’s surface. Ice a) they are believed to be the “leftovers” from the and Stone 2020 will make note of these occasions and formation of the solar system, so studying them provides appearances as they take place. The “Comet Resource valuable insights into our origins, including Earth and of Center” at the Earthrise web site contains information life on Earth, including ourselves; about the brighter comets that are visible in the sky at any given time and, for those who are interested, I will b) we have learned that this process isn’t over yet, and also occasionally share information about the goings-on that there are still objects out there that can impact in my life as I observe these comets. -
Detecting the Yarkovsky Effect Among Near-Earth Asteroids From
Detecting the Yarkovsky effect among near-Earth asteroids from astrometric data Alessio Del Vignaa,b, Laura Faggiolid, Andrea Milania, Federica Spotoc, Davide Farnocchiae, Benoit Carryf aDipartimento di Matematica, Universit`adi Pisa, Largo Bruno Pontecorvo 5, Pisa, Italy bSpace Dynamics Services s.r.l., via Mario Giuntini, Navacchio di Cascina, Pisa, Italy cIMCCE, Observatoire de Paris, PSL Research University, CNRS, Sorbonne Universits, UPMC Univ. Paris 06, Univ. Lille, 77 av. Denfert-Rochereau F-75014 Paris, France dESA SSA-NEO Coordination Centre, Largo Galileo Galilei, 1, 00044 Frascati (RM), Italy eJet Propulsion Laboratory/California Institute of Technology, 4800 Oak Grove Drive, Pasadena, 91109 CA, USA fUniversit´eCˆote d’Azur, Observatoire de la Cˆote d’Azur, CNRS, Laboratoire Lagrange, Boulevard de l’Observatoire, Nice, France Abstract We present an updated set of near-Earth asteroids with a Yarkovsky-related semi- major axis drift detected from the orbital fit to the astrometry. We find 87 reliable detections after filtering for the signal-to-noise ratio of the Yarkovsky drift esti- mate and making sure the estimate is compatible with the physical properties of the analyzed object. Furthermore, we find a list of 24 marginally significant detec- tions, for which future astrometry could result in a Yarkovsky detection. A further outcome of the filtering procedure is a list of detections that we consider spurious because unrealistic or not explicable with the Yarkovsky effect. Among the smallest asteroids of our sample, we determined four detections of solar radiation pressure, in addition to the Yarkovsky effect. As the data volume increases in the near fu- ture, our goal is to develop methods to generate very long lists of asteroids with reliably detected Yarkovsky effect, with limited amounts of case by case specific adjustments. -
Abstract Volume
T I I II I II I I I rl I Abstract Volume LPI LPI Contribution No. 1097 II I II III I • • WORKSHOP ON MERCURY: SPACE ENVIRONMENT, SURFACE, AND INTERIOR The Field Museum Chicago, Illinois October 4-5, 2001 Conveners Mark Robinbson, Northwestern University G. Jeffrey Taylor, University of Hawai'i Sponsored by Lunar and Planetary Institute The Field Museum National Aeronautics and Space Administration Lunar and Planetary Institute 3600 Bay Area Boulevard Houston TX 77058-1113 LPI Contribution No. 1097 Compiled in 2001 by LUNAR AND PLANETARY INSTITUTE The Institute is operated by the Universities Space Research Association under Contract No. NASW-4574 with the National Aeronautics and Space Administration. Material in this volume may be copied without restraint for library, abstract service, education, or personal research purposes; however, republication of any paper or portion thereof requires the written permission of the authors as well as the appropriate acknowledgment of this publication .... This volume may be cited as Author A. B. (2001)Title of abstract. In Workshop on Mercury: Space Environment, Surface, and Interior, p. xx. LPI Contribution No. 1097, Lunar and Planetary Institute, Houston. This report is distributed by ORDER DEPARTMENT Lunar and Planetary institute 3600 Bay Area Boulevard Houston TX 77058-1113, USA Phone: 281-486-2172 Fax: 281-486-2186 E-mail: order@lpi:usra.edu Please contact the Order Department for ordering information, i,-J_,.,,,-_r ,_,,,,.r pA<.><--.,// ,: Mercury Workshop 2001 iii / jaO/ Preface This volume contains abstracts that have been accepted for presentation at the Workshop on Mercury: Space Environment, Surface, and Interior, October 4-5, 2001. -
Astrodynamics of Moving Asteroids
Astrodynamics of Moving Asteroids Damon Landau, Nathan Strange, Gregory Lantoine, Tim McElrath NASA-JPL/CalTech Copyright 2014 California Institute of Technology. Government sponsorship acknowledged. Capture a NEA into Earth orbit Redirect asteroid for a close approach of the Moon natural Most of the DV is to speed up/slow down the NEA to close approach encounter Earth near their MOID (typically a node) of NEA DB Moon Lunar gravity assist captures NEA during Earth flyby 2 2 Capture C3, km /s DV ≈ DB/DT 2 2 Single flyby captures objects from up to ~3 km /s C3 2008 HU4 example, return leg only Double flyby up to ~5 km2/s2, depends on declination Natural approach of 0.15 AU, 1.3 km2/s2 4/8/2014 2 Asteroids and DV and Mass (oh my!) Returnable mass from (10,776) currently known NEAs Returnable Mass, t Returnable Earth-Sun Lunar Earth flybys Number of NEAs Mass, t Lagrange Pts Flyby & “backflips” 2 2 C3 <1 km /s C3 <2.5 C3 <25 10–50 653 NEAs 2564 4067 50–150 62 207 827 150–300 10 16 190 300–500 6 10 75 500–1000 4 8 40 1000+ 0* 0* 10 Minimum DV (km/s) between NEA & Lunar Flyby Phase-free, circular Earth orbit*, 6 t Xe, 5 t SEP, 2000 s Isp Deimos is ~7 km/s, Phobos is ~8 km/s *circular Earth orbit → up to 300 m/s DV errors 2006 RH120 is the known exception for 1000+ t to Lagrange Pts and 2000 SG344 > 1000 t for Lunar flyby Close approaches no longer factor into the equation for high-DV NEAs 4/8/2014 3 Potential Return Opportunities, 2020s Abbreviated List • Atlas 551 Launch to Asteroid Max Return Earth Return Asteroid Return C 200 x 11k km alt., Diameter 3 Capability Escape Date Launch ~1.5 yr before 2007 UN12 4–11 m 2.2 km2/s2 500 t Jun ’17 Sep ’20 escape 2009 BD 5–13 1.7 900 Jun ‘17 Jun ’23 • 40 kW array 2009 BD 5–13 1.7 500 Jan ‘19 Jun ’23 • 3000 s Isp, 60 % eff. -
Week 5: January 26-February 1, 2020
5# Ice & Stone 2020 Week 5: January 26-February 1, 2020 Presented by The Earthrise Institute About Ice And Stone 2020 It is my pleasure to welcome all educators, students, topics include: main-belt asteroids, near-Earth asteroids, and anybody else who might be interested, to Ice and “Great Comets,” spacecraft visits (both past and Stone 2020. This is an educational package I have put future), meteorites, and “small bodies” in popular together to cover the so-called “small bodies” of the literature and music. solar system, which in general means asteroids and comets, although this also includes the small moons of Throughout 2020 there will be various comets that are the various planets as well as meteors, meteorites, and visible in our skies and various asteroids passing by Earth interplanetary dust. Although these objects may be -- some of which are already known, some of which “small” compared to the planets of our solar system, will be discovered “in the act” -- and there will also be they are nevertheless of high interest and importance various asteroids of the main asteroid belt that are visible for several reasons, including: as well as “occultations” of stars by various asteroids visible from certain locations on Earth’s surface. Ice a) they are believed to be the “leftovers” from the and Stone 2020 will make note of these occasions and formation of the solar system, so studying them provides appearances as they take place. The “Comet Resource valuable insights into our origins, including Earth and of Center” at the Earthrise web site contains information life on Earth, including ourselves; about the brighter comets that are visible in the sky at any given time and, for those who are interested, I will b) we have learned that this process isn’t over yet, and also occasionally share information about the goings-on that there are still objects out there that can impact in my life as I observe these comets. -
Lehigh Preserve Institutional Repository
Lehigh Preserve Institutional Repository Particle Swarm Optimization of Low-Thrust, Geocentric-to-Halo-Orbit Transfers Abraham, Andrew 2014 Find more at https://preserve.lib.lehigh.edu/ This document is brought to you for free and open access by Lehigh Preserve. It has been accepted for inclusion by an authorized administrator of Lehigh Preserve. For more information, please contact [email protected]. Particle Swarm Optimization of Low-Thrust, Geocentric-to-Halo-Orbit Transfers by Andrew J. Abraham Presented to the Graduate and Research Committee of Lehigh University in Candidacy for the Degree of Doctor of Philosophy in Mechanical Engineering Lehigh University May, 2014 . Copyright by Andrew Abraham May, 2014 ii Approved and recommended for acceptance as a dissertation in partial fulfillment of the requirements for the degree of Doctor of Philosophy. ________________ Date _______________________ Professor Terry J. Hart Dissertation Adviser Mechanical Engineering Lehigh University ________________ Accepted Date _______________________ Dr. David B. Spencer Technical Adviser Aerospace Engineering The Pennsylvania State University _______________________ Dr. Nader Motee Committee Chairperson Mechanical Engineering Lehigh University _______________________ Dr. Philip A. Blythe Committee Member Mechanical Engineering Lehigh University _______________________ Dr. Gary G. DeLeo Committee Member Physics Lehigh University iii Acknowledgments Over the course of my graduate studies I have encountered many burdensome obstacles that I could not have overcome without significant help from family, friends, and advisers. I would like to take a moment to personally thank those who have helped make this dissertation a reality. First I would like to thank my parents for their support and encouragement during my graduate studies (especially low-cost housing). I would also like to thank my parents-in-law for their generous support as well. -
Capturing Near Earth Objects*
Capturing Near Earth Objects* Hexi Baoyin, Yang Chen, Junfeng Li Department of Aerospace Engineering, Tsinghua University 100084 Beijing, China Abstract: Recently, Near Earth Objects (NEOs) have been attracting great attention, and thousands of NEOs have been found to date. This paper examines the NEOs’ orbital dynamics using the framework of an accurate solar system model and a Sun-Earth-NEO three-body system when the NEOs are close to Earth to search for NEOs with low-energy orbits. It is possible for such an NEO to be temporarily captured by Earth; its orbit would thereby be changed and it would become an Earth-orbiting object after a small increase in its velocity. From the point of view of the Sun-Earth-NEO restricted three-body system, it is possible for an NEO whose Jacobian constant is slightly lower than C1 and higher than C3 to be temporarily captured by Earth. When such an NEO approaches Earth, it is possible to change its orbit energy to close up the zero velocity surface of the three-body system at point L1 and make the NEO become a small satellite of the Earth. Some such NEOs were found; the best example only required a 410m/s increase in velocity. Keywords: Near Earth Objects, temporary capture, restricted three-body system 1. Introduction Some Jovian comets, such as Oterma, are sometimes temporarily captured by Jupiter, making the transition from heliocentric orbits outside the orbit of Jupiter to heliocentric orbits inside the orbit of Jupiter. During this transition, Jupiter frequently captures the comet temporarily for one to several orbits (Koon et al. -
The First Human Asteroid Mission: Target Selection and Conceptual Mission Design
The First Human Asteroid Mission: Target Selection and Conceptual Mission Design Daniel Zimmerman,∗ Sam Wagner,∗ and Bong Wiey Asteroid Deflection Research Center - Iowa State University, Ames, IA 50011-2271 President Obama has recently declared that NASA will pursue a crewed mission to an asteroid by 2025. This paper identifies the optimum target candidates of near-Earth objects (NEOs) for a first crewed mission between 2018 and 2030. Target asteroids in the NEO database with orbital elements that meet predetermined requirements are analyzed for mission design. System architectures are then proposed to meet the require- ments for five designated NEO candidates. Additional technology which can be applied to crewed NEO mis- sions in the future is also discussed, and a previous NEO target selection study is analyzed. Although some development of heavy launch vehicles is still required for the first NEO mission, design examples show that a first mission can be achieved by 2025. The Ares V and the Orion CEV are used as the baseline system architecture for this study. Nomenclature a Semi-major Axis (AU) AU Astronomical Unit BOM Burnout Mass CEV Crew Exploration Vehicle e Eccentricity EDS Earth Departure Stage EOR Earth Orbit Rendezvous H Absolute Magnitude i Inclination (deg) Isp Specific Impulse (s) ISS International Space Station JPL Jet Propulsion Laboratory LEO Low-Earth Orbit LH2 Liquid Hydrogen LOX Liquid Oxygen MWe Megawatt Electrical MT Metric Ton NASA National Aeronautics and Space Administration NEO Near-Earth Object OT V Orbital Transfer Vehicle RSRM Reusable Solid Rocket Motor SSME Space Shuttle Main Engine T LI Trans Lunar Injection V ASIMR Variable Specific Impulse Magnetoplasma Rocket ∆V Velocity Change (km/s) ∗Graduate Research Assistant, Dept. -
Detecting Earth's Temporarily Captured Natural Irregular Satellites
Detecting Earth’s Temporarily Captured Natural Irregular Satellites Bryce Bolin1 ([email protected]), Robert Jedicke1, Mikael Granvik2, Peter Brown3, Monique Chyba4, Ellen Howell5, Mike Nolan5, Geoff Patterson3, Richard Wainscoat1 Received ; accepted N Pages, N Figures, N Table 1University of Hawaii, Institute for Astronomy, 2680 Woodlawn Dr, Honolulu, HI, 96822 2Department of Physics, P.O. BOX 64, 00014 University of Helsinki, Finland 3University of Western Ontario, Physics & Astronomy Department, London, Ontario, Canada 4University of Hawaii, Department of Mathematics, Honolulu, HI, 96822 5Arecibo Observatory, Arecibo, Puerto Rico –2– ABSTRACT JEDICKE WILL WRITE ONCE REMAINDER OF PAPER IS COMPLETE. Subject headings: Near-Earth Objects; Asteroids, Dynamics –3– Proposed Running Head: Detecting Earth’s Natural Irregular Satellites Editorial correspondence to: Bryce Bolin Institute for Astronomy University of Hawaii 2680 Woodlawn Drive Honolulu, HI 96822 Phone: +1 808 294 6299 Fax: +1 808 988 2790 E-mail: [email protected] –4– 1. Introduction Granvik et al. (2012) introduced the idea that there exists a steady state population of temporarily captured orbiters (TCO) that are natural irregular satellites of the Earth. They are captured from a dynamically suitable subset of the near Earth object (NEO) population — those that are on Earth-like orbits with semi-major axis a 1.0 AU, eccentricity e 0.0 ∼ ∼ and inclinations i 0 deg — and complete an average of 2.88 0.82(rms) revolutions ∼ ± around Earth during their average capture duration of 286 18(rms) days. In this work ± we evaluate options for detecting the TCOs as they are being captured, while they are on their geocentric trajectories, and in their meteor phase (about 1% of TCOs enter Earth’s atmosphere). -
Aas 14-276 What Does It Take to Capture an Asteroid?
AAS 14-276 WHAT DOES IT TAKE TO CAPTURE AN ASTEROID? A CASE STUDY ON CAPTURING ASTEROID 2006 RH120 Hodei Urrutxua,∗ Daniel J. Scheeres,y Claudio Bombardelli∗, Juan L. Gonzalo∗ and Jes ´usPelaez´ ∗ The population of “temporarily captured asteroids” offers attractive candidates for as- teroid retrieval missions. Once captured, these asteroids have lifetimes ranging from a few months up to several years in the vicinity of the Earth.1 One could potentially extend the duration of such temporary capture phases by acting upon the asteroid with slow deflection techniques that conveniently modify their trajectories, in order to allow for an affordable access to an asteroid for in-situ study. In this paper we present a case study on asteroid 2006 RH120, which got temporarily captured in 2006-2007 and is the single known member of this category up to date. We study what it would have taken to prolong its capture and estimate that deflecting the asteroid with 0:27 N for less than 6 months and a total ∆V barely 32 m/s, would have sufficed to extend the capture for over 5 additional years. MOTIVATION The growing interest in the study of asteroids, their formation, composition or internal structure, is often hindered by the lack of material samples and the difficulty of measuring certain physical features without in-situ scientific experiments. Hence, the idea of capturing and bringing an asteroid into the vicinity of the Earth has gained popularity in recent years, as proven by many papers attempting to propose asteroid captures,2,3,4,5,6 or most recently the NASA’s Asteroid Retrieval Initiative.7 Such kind of Earth delivery missions would allow an affordable access to asteroids along with a remarkable outcome in their scientific study, the possibility of resource utilization and eventually the development of new exploration technologies for the new-coming era of manned spaceflight.