Dynamical Evolution of Near-Earth Asteroid 1991 VG
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Spacewalch Discovery of Near-Earth Asteroids Tom Gehrele Lunar End
N9 Spacewalch Discovery of Near-Earth Asteroids Tom Gehrele Lunar end Planetary Laboratory The University of Arizona Our overall scientific goal is to survey the solar system to completion -- that is, to find the various populations and to study their statistics, interrelations, and origins. The practical benefit to SERC is that we are finding Earth-approaching asteroids that are accessible for mining. Our system can detect Earth-approachers In the 1-km size range even when they are far away, and can detect smaller objects when they are moving rapidly past Earth. Until Spacewatch, the size range of 6 - 300 meters in diameter for the near-Earth asteroids was unexplored. This important region represents the transition between the meteorites and the larger observed near-Earth asteroids (Rabinowitz 1992). One of our Spacewatch discoveries, 1991 VG, may be representative of a new orbital class of object. If it is really a natural object, and not man-made, its orbital parameters are closer to those of the Earth than we have seen before; its delta V is the lowest of all objects known thus far (J. S. Lewis, personal communication 1992). We may expect new discoveries as we continue our surveying, with fine-tuning of the techniques. III-12 Introduction The data accumulated in the following tables are the result of continuing observation conducted as a part of the Spacewatch program. T. Gehrels is the Principal Investigator and also one of the three observers, with J.V. Scotti and D.L Rabinowitz, each observing six nights per month. R.S. McMillan has been Co-Principal Investigator of our CCD-scanning since its inception; he coordinates optical, mechanical, and electronic upgrades. -
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 -
Near Earth Asteroid (NEA) Scout
https://ntrs.nasa.gov/search.jsp?R=20160007060 2019-08-08T05:23:13+00:00Z Near Earth Asteroid (NEA) Scout Les Johnson NASA MSFC Advance Concepts Office [email protected] Topics • What is a solar sail? • A brief history of solar sailing • NASA’s Near Earth Asteroid Scout mission How does a solar sail work? Solar sails use photon “pressure” or force on thin, lightweight reflective sheet to produce thrust. 3 Topics • What is a solar sail? • A brief history of solar sailing • NASA’s Near Earth Asteroid Scout mission The Planetary Society’s Cosmos-1 (2005) • 100 kg spacecraft • 8 triangular sail blades deployed from a central hub after launch by the inflating of structural tubes. • Sail blades were each 15 m long • Total surface area of 600 square meters • Launched in 2005 from a Russian Volna Rocket from a Russian Delta III submarine in the Barents Sea: The Planetary Society’s Cosmos-1 (2005) • 100 kg spacecraft • 8 triangular sail blades deployed from a central hub after launch by the inflating of structural tubes. • Sail blades were each 15 m long • Total surface area of 600 square meters • Launched in 2005 from a Russian Volna Rocket from a Russian Delta III submarine in the Barents Sea: Rocket Failed NASA Ground Tested Solar Sails in the Mid-2000’s Two 400 square meter sail were autonomously deployed and tested at Plumbrook NanoSail-D Demonstration Solar Sail Mission Description: • 10 m2 sail • Made from tested ground demonstrator hardware NanoSail-D2 Mission (2010) Interplanetary Kite-craft Accelerated by Radiation of the Sun (IKAROS) -
Discovery of Earth's Quasi-Satellite
Meteoritics & Planetary Science 39, Nr 8, 1251–1255 (2004) Abstract available online at http://meteoritics.org Discovery of Earth’s quasi-satellite Martin CONNORS,1* Christian VEILLET,2 Ramon BRASSER,3 Paul WIEGERT,4 Paul CHODAS,5 Seppo MIKKOLA,6 and Kimmo INNANEN3 1Athabasca University, Athabasca AB, Canada T9S 3A3 2Canada-France-Hawaii Telescope, P. O. Box 1597, Kamuela, Hawaii 96743, USA 3Department of Physics and Astronomy, York University, Toronto, ON M3J 1P3 Canada 4Department of Physics and Astronomy, University of Western Ontario, London, ON N6A 3K7, Canada 5Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109, USA 6Turku University Observatory, Tuorla, FIN-21500 Piikkiö, Finland *Corresponding author. E-mail: [email protected] (Received 18 February 2004; revision accepted 12 July 2004) Abstract–The newly discovered asteroid 2003 YN107 is currently a quasi-satellite of the Earth, making a satellite-like orbit of high inclination with apparent period of one year. The term quasi- satellite is used since these large orbits are not completely closed, but rather perturbed portions of the asteroid’s orbit around the Sun. Due to its extremely Earth-like orbit, this asteroid is influenced by Earth’s gravity to remain within 0.1 AU of the Earth for approximately 10 years (1997 to 2006). Prior to this, it had been on a horseshoe orbit closely following Earth’s orbit for several hundred years. It will re-enter such an orbit, and make one final libration of 123 years, after which it will have a close interaction with the Earth and transition to a circulating orbit. -
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. -
The National Aeronautics and Space Administration Planetary Astronomy Program
FRS 347320 FINAL REPORT FOR GRANT NAG5-3938 SUBMITTED TO: The National Aeronautics and Space Administration Planetary Astronomy Program TITLE: Beginning Research with the 1.8-meter Spacewatch Telescope ORGANIZATION: The University of Arizona Lunar and Planetary Laboratory PERIOD OF GRANT: 1996 Dec. 1 - 2000 Nov. 30 PERIOD REPORTED ON: 1996 Dec. I - 2001 Feb. 9 2._o[ PRINCIPAL INVESTIGATOR: Tom Gehrels Date Professor Lunar and Planetary Laboratory University of Arizona Kuiper Space Sciences Building 1629 East University Boulevard Tucson, AZ 85721-0092 Phone: 520/621-6970 FAX: 520/621-1940 Email: [email protected] BUSINESS REPRESENTATIVE: Ms. Lynn A. Lane Senior Business Manager Lunar and Planetary Laboratory University of Arizona Kuiper Space Sciences Building 1629 East University Boulevard Tucson, AZ 85721-0092 Phone: 520/621-6966 FAX: 520/621-4933 Email: [email protected] c:_w_nnsaknag53938.fnl Participating Professionals (all at the Lunar and Planetary Laboratory): Terrence H. Bressi (B. S., Astron. & Physics) Engineer Anne S. Descour (M. S., Computer Science) Senior Systems Programmer Tom Gehrels (Ph. D., Astronomy) Professor, observer, and PI Robert Jedicke (Ph.D., Physics) Principal Research Specialist Jeffrey A. Larsen (Ph. D., Astronomy) Principal Research Specialist and observer Robert S. McMiUan (Ph.D., Astronomy) Associate Research Scientist & observer Joseph L. Montani (M. S., Astronomy) Senior Research Specialist and observer Marcus L. Perry (B. A., Astronomy) (Chief) Staff Engineer James V. Scotti (B. S., Astronomy) Senior Research Specialist and observer PROJECT SUMMARY The purpose of this grant was to bring the Spacewatch 1.8-m telescope to operational status for research on asteroids and comets. -
OSIRIS-Rex Goes Asteroid Collecting
OSIRIS-REx Goes Asteroid Collecting — Scott Messenger, NASA Johnson Space Center OSIRIS-REx is NASA’s third New Frontiers mission, following the New Horizons mission, which completed a flyby of Pluto in 2015, and the Juno mission to orbit Jupiter, which has just begun science operations. The OSIRIS-REx mission’s primary objective is to collect pristine surface samples of a carbonaceous asteroid and return them to Earth for analysis. Carbonaceous asteroids and comets are considered to be L “primitive” bodies that have preserved remnants of the solar system starting materials. By studying them, scientists can learn about the origin and earliest evolution of the solar system. The OSIRIS-REx spacecraft was launched on September 8, 2016, beginning its two- year journey to asteroid 101955 Bennu (formerly designated 1999 RQ36). After more than one year of detailed remote observations, OSIRIS-REx will obtain surface samples and return them to Earth in September 2023. The OSIRIS-REx proposal, led by the late Dr. Michael J. Drake, was selected during the 2011 New Frontiers competition, and is now led by Dr. Dante Lauretta of the University of Arizona. The Pmission name OSIRIS-REx (an acronym for Origins, Spectral Interpretation, Resource Identification, Security, Regolith Explorer) embodies five objectives: (1) Origins: Return and analyze a sample of a carbonaceous asteroid; (2) Spectral Interpretation: Provide ground truth for remote observations of asteroids; (3) Resource Identification: Determine the mineral and chemical makeup of a near-Earth asteroid; (4) Security: Directly measure the non-gravitational force known as the Yarkovsky effect, which changes asteroidal orbits through its Iinteraction with sunlight; and (5) Regolith Explorer: Determine the properties of unconsolidated material that covers the asteroid surface. -
Why Atens Enjoy Enhanced Accessibility for Human Space Flight
(Preprint) AAS 11-449 WHY ATENS ENJOY ENHANCED ACCESSIBILITY FOR HUMAN SPACE FLIGHT Daniel R. Adamo* and Brent W. Barbee† Near-Earth objects can be grouped into multiple orbit classifications, among them being the Aten group, whose members have orbits crossing Earth's with semi-major axes less than 1 astronomical unit. Atens comprise well under 10% of known near-Earth objects. This is in dramatic contrast to results from recent human space flight near-Earth object accessibility studies, where the most favorable known destinations are typically almost 50% Atens. Geocentric dynamics explain this enhanced Aten accessibility and lead to an understanding of where the most accessible near-Earth objects reside. Without a com- prehensive space-based survey, however, highly accessible Atens will remain largely un- known. INTRODUCTION In the context of human space flight (HSF), the concept of near-Earth object (NEO) accessibility is highly subjective (Reference 1). Whether or not a particular NEO is accessible critically depends on mass, performance, and reliability of interplanetary HSF systems yet to be designed. Such systems would cer- tainly include propulsion and crew life support with adequate shielding from both solar flares and galactic cosmic radiation. Equally critical architecture options are relevant to NEO accessibility. These options are also far from being determined and include the number of launches supporting an HSF mission, together with whether consumables are to be pre-emplaced at the destination. Until the unknowns of HSF to NEOs come into clearer focus, the notion of relative accessibility is of great utility. Imagine a group of NEOs, each with nearly equal HSF merit determined from their individual characteristics relating to crew safety, scientific return, resource utilization, and planetary defense. -
The Population of Near Earth Asteroids in Coorbital Motion with Venus
ARTICLE IN PRESS YICAR:7986 JID:YICAR AID:7986 /FLA [m5+; v 1.65; Prn:10/08/2006; 14:41] P.1 (1-10) Icarus ••• (••••) •••–••• www.elsevier.com/locate/icarus The population of Near Earth Asteroids in coorbital motion with Venus M.H.M. Morais a,∗, A. Morbidelli b a Grupo de Astrofísica da Universidade de Coimbra, Observatório Astronómico de Coimbra, Santa Clara, 3040 Coimbra, Portugal b Observatoire de la Côte d’Azur, BP 4229, Boulevard de l’Observatoire, Nice Cedex 4, France Received 13 January 2006; revised 10 April 2006 Abstract We estimate the size and orbital distributions of Near Earth Asteroids (NEAs) that are expected to be in the 1:1 mean motion resonance with Venus in a steady state scenario. We predict that the number of such objects with absolute magnitudes H<18 and H<22 is 0.14 ± 0.03 and 3.5 ± 0.7, respectively. We also map the distribution in the sky of these Venus coorbital NEAs and we see that these objects, as the Earth coorbital NEAs studied in a previous paper, are more likely to be found by NEAs search programs that do not simply observe around opposition and that scan large areas of the sky. © 2006 Elsevier Inc. All rights reserved. Keywords: Asteroids, dynamics; Resonances 1. Introduction object with a theory based on the restricted three body problem at high eccentricity and inclination. Christou (2000) performed In Morais and Morbidelli (2002), hereafter referred to as a 0.2 Myr integration of the orbits of NEAs in the vicinity of Paper I, we estimated the population of Near Earth Asteroids the terrestrial planets, namely (3362) Khufu, (10563) Izhdubar, (NEAs) that are in the 1:1 mean motion resonance (i.e., are 1994 TF2 and 1989 VA, showing that the first three could be- coorbital1) with the Earth in a steady state scenario where come coorbitals of the Earth while the fourth could become NEAs are constantly being supplied by the main belt sources coorbital of Venus. -
Opportunities for Asteroid Retrieval Missions
Opportunities for Asteroid Retrieval Missions Pre-print proof-reading copy. The final publication is available at: http://link.springer.com/chapter/10.1007/978-3-642-39244-3_21 D. García Yárnoz, J.P. Sanchez, C.R. McInnes Advanced Space Concepts Laboratory, University of Strathclyde, UK. Abstract Asteroids and comets are of strategic importance for science in an effort to uncover the formation, evolution and composition of the Solar System. Near-Earth Objects (NEOs) are of particular interest because of their ac- cessibility from Earth, but also because of their speculated wealth of mate- rial resources. The exploitation of these resources has long been discussed as a means to lower the cost of future space endeavours. In this chapter, we analyze the possibility of retrieving entire objects from accessible helio- centric orbits and moving them into the Earth’s neighbourhood. The aster- oid retrieval transfers are sought from the continuum of low energy trans- fers enabled by the dynamics of invariant manifolds; specifically, the retrieval transfers target planar, vertical Lyapunov and halo orbit families associated with the collinear equilibrium points of the Sun-Earth Circular Restricted Three Body problem. The judicious use of these dynamical fea- tures provides the best opportunity to find extremely low energy transfers for asteroidal material. With the objective to minimise transfer costs, a global search of impulsive transfers connecting the unperturbed asteroid’s orbit with the stable manifold phase of the transfer is performed. A cata- logue of asteroid retrieval opportunities of currently known NEOs is pre- sented here. Despite the highly incomplete census of very small asteroids, the catalogue can already be populated with 12 different objects retrievable with less than 500 m/s of Δv.