Evidence for Widespread Hydrated Minerals on Asteroid (101955) Bennu
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OSIRIS-Rex, Returning the Asteroid Sample
OSIRIS-REx, Returning the Asteroid Sample Thomas Ajluni Timothy Linn William Willcockson ASRC Federal Space & Defense Lockheed Martin Space Systems Lockheed Martin Space Systems 7000 Muirkirk Meadows Drive Company, P.O. Box 179 Company, P.O. Box 179 Suite 100, Beltsville, MD 20705 Denver, CO 80201 Denver, CO 80201 301.286.1831 303-977-0659 303-977-5094 [email protected] [email protected] [email protected] David Everett Ronald Mink Joshua Wood NASA Goddard Space Flight NASA Goddard Space Flight Lockheed Martin Space Systems Center, 8800 Greenbelt Road Center, 8800 Greenbelt Road Company, P.O. Box 179 Greenbelt, MD 20771 Greenbelt, MD 20771 Denver, CO 80201 301.286.1596 301.286.3524 303-977-3199 [email protected] [email protected] [email protected] Abstract—This paper addresses the technical aspects of the sample return system for the upcoming Origins, Spectral x attitude control Interpretation, Resource Identification, and Security-Regolith x propulsion Explorer (OSIRIS-REx) asteroid sample return mission. The x power overall mission design and current implementation are presented as an overview to establish a context for the x thermal control technical description of the reentry and landing segment of the x telecommunications mission. x command and data handling x structural support to ensure successful rendezvous The prime objective of the OSIRIS-REx mission is to sample a with Bennu primitive, carbonaceous asteroid and to return that sample to Earth in pristine condition for detailed laboratory analysis. x characterization of Bennu’s properties Targeting the near-Earth asteroid Bennu, the mission launches x delivery of the sampler to the surface, and return of in September 2016 with an Earth reentry date of September the spacecraft to the vicinity of the Earth 24, 2023. -
Cohesive Forces Prevent the Rotational Breakup of Rubble-Pile Asteroid (29075) 1950 DA
Open Research Online The Open University’s repository of research publications and other research outputs Cohesive forces prevent the rotational breakup of rubble-pile asteroid (29075) 1950 DA Journal Item How to cite: Rozitis, Ben; MacLennan, Eric and Emery, Joshua P. (2014). Cohesive forces prevent the rotational breakup of rubble-pile asteroid (29075) 1950 DA. Nature, 512(7513), article no. 13632. For guidance on citations see FAQs. c 2014 Macmillan Publishers Limited https://creativecommons.org/licenses/by-nc-nd/4.0/ Version: Accepted Manuscript Link(s) to article on publisher’s website: http://dx.doi.org/doi:10.1038/nature13632 Copyright and Moral Rights for the articles on this site are retained by the individual authors and/or other copyright owners. For more information on Open Research Online’s data policy on reuse of materials please consult the policies page. oro.open.ac.uk Cohesive forces preventing rotational breakup of rubble pile asteroid (29075) 1950 DA Ben Rozitis1, Eric MacLennan1 & Joshua P. Emery1 1Department of Earth and Planetary Sciences, University of Tennessee, Knoxville, TN 37996, US ([email protected]) Space missions1 and ground-based observations2 have shown that some asteroids are loose collections of rubble rather than solid bodies. The physical behavior of such ‘rubble pile’ asteroids has been traditionally described using only gravitational and frictional forces within a granular material3. Cohesive forces in the form of small van der Waals forces between constituent grains have been recently predicted to be important for small rubble piles (10- kilometer-sized or smaller), and can potentially explain fast rotation rates in the small asteroid population4-6. -
New Horizons: Reconnaissance of the Pluto-Charon System and The
C.T. Russell Editor New Horizons Reconnaissance of the Pluto-Charon System and the Kuiper Belt Previously published in Space Science Reviews Volume 140, Issues 1–4, 2008 C.T. Russell Institute of Geophysics & Planetary Physics University of California Los Angeles, CA, USA Cover illustration: NASA’s New Horizons spacecraft was launched on 2006 January 19, received a grav- ity assist during a close approach to Jupiter on 2007 February 28, and is now headed for a flyby with closest approach 12,500 km from the center of Pluto on 2015 July 14. This artist’s depiction shows the spacecraft shortly after passing above Pluto’s highly variegated surface, which may have black-streaked surface deposits produced from cryogenic geyser activity, and just before passing into Pluto’s shadow when solar and earth occultation experiments will probe Pluto’s tenuous, and possibly hazy, atmosphere. Sunlit crescents of Pluto’s moons Charon, Nix, and Hydra are visible in the background. After flying through the Pluto system, the New Horizons spacecraft could be re-targeted towards other Kuiper Belt Objects in an extended mission phase. This image is based on an original painting by Dan Durda. © Dan Durda 2001 All rights reserved. Back cover illustration: The New Horizons spacecraft was launched aboard an Atlas 551 rocket from the NASA Kennedy Space Center on 2008 January 19 at 19:00 UT. Library of Congress Control Number: 2008944238 DOI: 10.1007/978-0-387-89518-5 ISBN-978-0-387-89517-8 e-ISBN-978-0-387-89518-5 Printed on acid-free paper. -
The Orbital Distribution of Near-Earth Objects Inside Earth’S Orbit
Icarus 217 (2012) 355–366 Contents lists available at SciVerse ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus The orbital distribution of Near-Earth Objects inside Earth’s orbit ⇑ Sarah Greenstreet a, , Henry Ngo a,b, Brett Gladman a a Department of Physics & Astronomy, 6224 Agricultural Road, University of British Columbia, Vancouver, British Columbia, Canada b Department of Physics, Engineering Physics, and Astronomy, 99 University Avenue, Queen’s University, Kingston, Ontario, Canada article info abstract Article history: Canada’s Near-Earth Object Surveillance Satellite (NEOSSat), set to launch in early 2012, will search for Received 17 August 2011 and track Near-Earth Objects (NEOs), tuning its search to best detect objects with a < 1.0 AU. In order Revised 8 November 2011 to construct an optimal pointing strategy for NEOSSat, we needed more detailed information in the Accepted 9 November 2011 a < 1.0 AU region than the best current model (Bottke, W.F., Morbidelli, A., Jedicke, R., Petit, J.M., Levison, Available online 28 November 2011 H.F., Michel, P., Metcalfe, T.S. [2002]. Icarus 156, 399–433) provides. We present here the NEOSSat-1.0 NEO orbital distribution model with larger statistics that permit finer resolution and less uncertainty, Keywords: especially in the a < 1.0 AU region. We find that Amors = 30.1 ± 0.8%, Apollos = 63.3 ± 0.4%, Atens = Near-Earth Objects 5.0 ± 0.3%, Atiras (0.718 < Q < 0.983 AU) = 1.38 ± 0.04%, and Vatiras (0.307 < Q < 0.718 AU) = 0.22 ± 0.03% Celestial mechanics Impact processes of the steady-state NEO population. -
Constraints on the Near-Earth Asteroid Obliquity Distribution from The
Astronomy & Astrophysics manuscript no. main c ESO 2017 September 4, 2017 Constraints on the near-Earth asteroid obliquity distribution from the Yarkovsky effect C. Tardioli1,?, D. Farnocchia2, B. Rozitis3, D. Cotto-Figueroa4, S. R. Chesley2, T. S. Statler5; 6, and M. Vasile1 1 Department of Mechanical & Aerospace Engineering, University of Strathclyde, Glasgow, G1 1XJ, UK 2 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 3 School of Physical Sciences, The Open University, Milton Keynes, MK7 6AA, UK 4 Department of Physics and Electronics, University of Puerto Rico at Humacao, Humacao, 00792, Puerto Rico 5 Department of Astronomy, University of Maryland, College Park, MD, 20742, USA 6 Planetary Science Division, Science Mission Directorate, NASA Headquarters, Washington DC, 20546, USA September 4, 2017 ABSTRACT Aims. From lightcurve and radar data we know the spin axis of only 43 near-Earth asteroids. In this paper we attempt to constrain the spin axis obliquity distribution of near-Earth asteroids by leveraging the Yarkovsky effect and its dependence on an asteroid’s obliquity. Methods. By modeling the physical parameters driving the Yarkovsky effect, we solve an inverse problem where we test different simple parametric obliquity distributions. Each distribution re- sults in a predicted Yarkovsky effect distribution that we compare with a χ2 test to a dataset of 125 Yarkovsky estimates. Results. We find different obliquity distributions that are statistically satisfactory. In particular, among the considered models, the best-fit solution is a quadratic function, which only depends on two parameters, favors extreme obliquities, consistent with the expected outcomes from the YORP effect, has a 2:1 ratio between retrograde and direct rotators, which is in agreement with theoretical predictions, and is statistically consistent with the distribution of known spin axes of near-Earth asteroids. -
GUIDANCE, NAVIGATION, and CONTROL 2020 AAS PRESIDENT Carol S
GUIDANCE, NAVIGATION, AND CONTROL 2020 AAS PRESIDENT Carol S. Lane Cynergy LLC VICE PRESIDENT – PUBLICATIONS James V. McAdams KinetX Inc. EDITOR Jastesh Sud Lockheed Martin Space SERIES EDITOR Robert H. Jacobs Univelt, Incorporated Front Cover Illustration: Image: Checkpoint-Rehearsal-Movie-1024x720.gif Caption: “OSIRIS-REx Buzzes Sample Site Nightingale” Photo and Caption Credit: NASA/Goddard/University of Arizona Public Release Approval: Per multimedia guidelines from NASA Frontispiece Illustration: Image: NASA_Orion_EarthRise.jpg Caption: “Orion Primed for Deep Space Exploration” Photo Credit: NASA Public Release Approval: Per multimedia guidelines from NASA GUIDANCE, NAVIGATION, AND CONTROL 2020 Volume 172 ADVANCES IN THE ASTRONAUTICAL SCIENCES Edited by Jastesh Sud Proceedings of the 43rd AAS Rocky Mountain Section Guidance, Navigation and Control Conference held January 30 to February 5, 2020, Breckenridge, Colorado Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Copyright 2020 by AMERICAN ASTRONAUTICAL SOCIETY AAS Publications Office P.O. Box 28130 San Diego, California 92198 Affiliated with the American Association for the Advancement of Science Member of the International Astronautical Federation First Printing 2020 Library of Congress Card No. 57-43769 ISSN 0065-3438 ISBN 978-0-87703-669-2 (Hard Cover Plus CD ROM) ISBN 978-0-87703-670-8 (Digital Version) Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Printed and Bound in the U.S.A. FOREWORD HISTORICAL SUMMARY The annual American Astronautical Society Rocky Mountain Guidance, Navigation and Control Conference began as an informal exchange of ideas and reports of achievements among local guidance and control specialists. -
1950 Da, 205, 269 1979 Va, 230 1991 Ry16, 183 1992 Kd, 61 1992
Cambridge University Press 978-1-107-09684-4 — Asteroids Thomas H. Burbine Index More Information 356 Index 1950 DA, 205, 269 single scattering, 142, 143, 144, 145 1979 VA, 230 visual Bond, 7 1991 RY16, 183 visual geometric, 7, 27, 28, 163, 185, 189, 190, 1992 KD, 61 191, 192, 192, 253 1992 QB1, 233, 234 Alexandra, 59 1993 FW, 234 altitude, 49 1994 JR1, 239, 275 Alvarez, Luis, 258 1999 JU3, 61 Alvarez, Walter, 258 1999 RL95, 183 amino acid, 81 1999 RQ36, 61 ammonia, 223, 301 2000 DP107, 274, 304 amoeboid olivine aggregate, 83 2000 GD65, 205 Amor, 251 2001 QR322, 232 Amor group, 251 2003 EH1, 107 Anacostia, 179 2007 PA8, 207 Anand, Viswanathan, 62 2008 TC3, 264, 265 Angelina, 175 2010 JL88, 205 angrite, 87, 101, 110, 126, 168 2010 TK7, 231 Annefrank, 274, 275, 289 2011 QF99, 232 Antarctic Search for Meteorites (ANSMET), 71 2012 DA14, 108 Antarctica, 69–71 2012 VP113, 233, 244 aphelion, 30, 251 2013 TX68, 64 APL, 275, 292 2014 AA, 264, 265 Apohele group, 251 2014 RC, 205 Apollo, 179, 180, 251 Apollo group, 230, 251 absorption band, 135–6, 137–40, 145–50, Apollo mission, 129, 262, 299 163, 184 Apophis, 20, 269, 270 acapulcoite/ lodranite, 87, 90, 103, 110, 168, 285 Aquitania, 179 Achilles, 232 Arecibo Observatory, 206 achondrite, 84, 86, 116, 187 Aristarchus, 29 primitive, 84, 86, 103–4, 287 Asporina, 177 Adamcarolla, 62 asteroid chronology function, 262 Adeona family, 198 Asteroid Zoo, 54 Aeternitas, 177 Astraea, 53 Agnia family, 170, 198 Astronautica, 61 AKARI satellite, 192 Aten, 251 alabandite, 76, 101 Aten group, 251 Alauda family, 198 Atira, 251 albedo, 7, 21, 27, 185–6 Atira group, 251 Bond, 7, 8, 9, 28, 189 atmosphere, 1, 3, 8, 43, 66, 68, 265 geometric, 7 A- type, 163, 165, 167, 169, 170, 177–8, 192 356 © in this web service Cambridge University Press www.cambridge.org Cambridge University Press 978-1-107-09684-4 — Asteroids Thomas H. -
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. -
Astrodynamic Fundamentals for Deflecting Hazardous Near-Earth Objects
IAC-09-C1.3.1 Astrodynamic Fundamentals for Deflecting Hazardous Near-Earth Objects∗ Bong Wie† Asteroid Deflection Research Center Iowa State University, Ames, IA 50011, United States [email protected] Abstract mate change caused by this asteroid impact may have caused the dinosaur extinction. On June 30, 1908, an The John V. Breakwell Memorial Lecture for the As- asteroid or comet estimated at 30 to 50 m in diameter trodynamics Symposium of the 60th International As- exploded in the skies above Tunguska, Siberia. Known tronautical Congress (IAC) presents a tutorial overview as the Tunguska Event, the explosion flattened trees and of the astrodynamical problem of deflecting a near-Earth killed other vegetation over a 500,000-acre area with an object (NEO) that is on a collision course toward Earth. energy level equivalent to about 500 Hiroshima nuclear This lecture focuses on the astrodynamic fundamentals bombs. of such a technically challenging, complex engineering In the early 1990s, scientists around the world initi- problem. Although various deflection technologies have ated studies to prevent NEOs from striking Earth [1]. been proposed during the past two decades, there is no However, it is now 2009, and there is no consensus on consensus on how to reliably deflect them in a timely how to reliably deflect them in a timely manner even manner. Consequently, now is the time to develop prac- though various mitigation approaches have been inves- tically viable technologies that can be used to mitigate tigated during the past two decades [1-8]. Consequently, threats from NEOs while also advancing space explo- now is the time for initiating a concerted R&D effort for ration. -
Guidance, Navigation, and Control 2014
GUIDANCE, NAVIGATION, AND CONTROL 2014 Edited by Alexander J. May Volume 151 ADVANCES IN THE ASTRONAUTICAL SCIENCES GUIDANCE, NAVIGATION, AND CONTROL 2014 AAS PRESIDENT Lyn D. Wigbels RWI International Consulting Services VICE PRESIDENT - PUBLICATIONS Richard D. Burns NASA Goddard Space Flight Center EDITOR Alexander J. May Lockheed Martin Space Systems Co. SERIES EDITOR Robert H. Jacobs Univelt, Incorporated Front Cover Illustration: Lockheed Martin is the prime contractor building the Orion multi-purpose crew vehicle, NASA’s first spacecraft designed for long-duration, human-rated deep space exploration. Orion will transport humans to interplanetary destinations beyond low Earth orbit, such as asteroids, the moon and eventually Mars, and return them safely back to Earth. Credit: Lockheed Martin. Frontispiece: Lockheed Martin’s state-of-the-art Space Operations Simulation Center (SOSC) has completed orbital simulation tests with hardware and data that was flown on NASA’s STS-134 space shut- tle Endeavour mission to the International Space Station. The tests have demonstrated the cen- ter’s ability to replicate on-orbit conditions that affect relative navigation, lighting and motion con- trol in space — providing a simulated space dynamics and lighting environment that is unparal- leled in the space industry. Credit: Lockheed Martin. iii iv GUIDANCE, NAVIGATION, AND CONTROL 2014 Volume 151 ADVANCES IN THE ASTRONAUTICAL SCIENCES Edited by Alexander J. May Proceedings of the 37th Annual AAS Rocky Mountain Section Guidance and Control Conference held January 31 – February 5, 2014, Breckenridge, Colorado. Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com v Copyright 2014 by AMERICAN ASTRONAUTICAL SOCIETY AAS Publications Office P.O. -
Guidance and Control 2011
GUIDANCE AND CONTROL 2011 Edited by Kyle B. Miller Volume 141 ADVANCES IN THE ASTRONAUTICAL SCIENCES GUIDANCE AND CONTROL 2011 i CONFERENCE COMMITTEE Brent Abbott Surrey Space Vanessa Baez Lockheed Martin Space Systems Co. Lee Barker Lockheed Martin Space Systems Co. Jim Chapel Lockheed Martin Space Systems Co. Brian Clapp Lockheed Martin Space Systems Co. David A. Chart Lockheed Martin Space Systems Co. Michael Drews Lockheed Martin Space Systems Co. Bill Emery University of Colorado Scott Francis Lockheed Martin Space Systems Co. Kristen Francis Lockheed Martin Space Systems Co. Bill Frazier Ball Aerospace & Technologies Corp. Lis Garratt Ball Aerospace & Technologies Corp. Larry Germann Left Hand Design Ian Gravseth Ball Aerospace & Technologies Corp. Lisa Hardaway Ball Aerospace & Technologies Corp. Steven Jolly Lockheed Martin Space Systems Co. Mary A. Klaus Lockheed Martin Space Systems Co. Alex May Lockheed Martin Space Systems Co. James McQuerry Ball Aerospace & Technologies Corp. Shawn McQuerry Lockheed Martin Space Systems Co. Kyle Miller Ball Aerospace & Technologies Corp. Carolyn O’Brien Lockheed Martin Space Systems Co. Marv Odefey Left Hand Design Michael Osborne Lockheed Martin Space Systems Co. Brian Patterson Lockheed Martin Space Systems Co. Chris Randall Ball Aerospace & Technologies Corp. Ron Rausch United Launch Alliance (Retired) Jay Speed Ball Aerospace & Technologies Corp. Cheryl Walker TASC, Inc. Zach Wilson Lockheed Martin Space Systems Co. THE 35th ANNUAL ROCKY MOUNTAIN SECTION GUIDANCE AND CONTROL CONFERENCE Will be held at Breckenridge, Colorado, February 3–8, 2012, Michael Osborne, Lockheed Martin Space Systems Co., Chairing ii AAS PRESIDENT Frank A. Slazer Northrop Grumman VICE PRESIDENT - PUBLICATIONS Prof. David B. Spencer Pennsylvania State University EDITOR Kyle B. -
Guidance and Control 2013
GUIDANCE AND CONTROL 2013 Edited by Lisa R. Hardaway Volume 149 ADVANCES IN THE ASTRONAUTICAL SCIENCES GUIDANCE AND CONTROL 2013 i AAS PRESIDENT Lyn D. Wigbels RWI International Consulting Services VICE PRESIDENT - PUBLICATIONS Richard D. Burns NASA Goddard Space Flight Center EDITOR Dr. Lisa R. Hardaway Ball Aerospace & Technologies Corp. SERIES EDITOR Robert H. Jacobs Univelt, Incorporated Front Cover Illustration: The beautiful imagery and important science received from on-orbit telescopes would not be possible without the technologies of Guidance, Navigation and Control. (Photo Credit: NASA). Frontispiece: Kepler, with its star trackers visible, is installed into its launch fairing. (Image courtesy of Ball Aerospace & Technologies Corp.) iii iv GUIDANCE AND CONTROL 2013 Volume 149 ADVANCES IN THE ASTRONAUTICAL SCIENCES Edited by Lisa R. Hardaway Proceedings of the 36th Annual AAS Rocky Mountain Section Guidance and Control Conference held February 1–6, 2013, Breckenridge, Colorado. Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com v Copyright 2013 by AMERICAN ASTRONAUTICAL SOCIETY AAS Publications Office P.O. Box 28130 San Diego, California 92198 Affiliated with the American Association for the Advancement of Science Member of the International Astronautical Federation First Printing 2013 Library of Congress Card No. 57-43769 ISSN 0065-3438 ISBN 978-0-87703-601-2 (Hard Cover Plus CD ROM) ISBN 978-0-87703-602-9 (CD ROM) Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Printed and Bound in the U.S.A.