Dynamics of Tethered Asteroid Systems to Support Planetary Defense
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
7Th IAA Planetary Defense Conference – PDC 2021 26
7th IAA Planetary Defense Conference – PDC 2021 1 26-30 April 2021, Vienna, Austria IAA-PDC-21-11-37 Precautionary Planetary Defence Aaron C. Boley(1), Michael Byers(2) (1)(2)Outer Space Institute University of British Columbia 325-6224 Agricultural Road Vancouver, BC V6T 1Z1 Canada +1-604-827-2641 [email protected] Keywords: Asteroids, Precautionary Principle, Decision-Making, Active Management visiting the asteroid before the 2029 close approach Introduction: The question of whether to attempt leads us to ask, in a general sense, to what degree deflections during planetary defence emergencies has might restraint be prudent? been subject to considerable decision-making analysis As discussed by Chesley and Farnocchia (2021), if a (Schmidt 2018; SMPAG Ad-Hoc Working Group on Legal mission to an asteroid with a rich set of keyholes, like Issues 2020). Hypothetical situations usually involve a Apophis, goes awry and unintentionally collides with the newly discovered asteroid with a high impact probability asteroid, there is a risk that this will create a future on a set timescale. This paper addresses two further impact emergency. The publicity associated with the complexities: (1) limiting missions to an asteroid due to asteroid’s close approach could also prompt non-state the risk of a human-caused Earth impact; and (2) active actors to launch their own missions as technology management of asteroids to place them in “safe demonstrations and/or profile-raising exercises, much harbours”, even when impact risks are otherwise below like the infamous Tesla launch by SpaceX. “decision to act” thresholds. We use Apophis as a case Adding to these considerations is a potential traffic study, and address the two complexities in turn. -
Russia's Posture in Space
Russia’s Posture in Space: Prospects for Europe Executive Summary Prepared by the European Space Policy Institute Marco ALIBERTI Ksenia LISITSYNA May 2018 Table of Contents Background and Research Objectives ........................................................................................ 1 Domestic Developments in Russia’s Space Programme ............................................................ 2 Russia’s International Space Posture ......................................................................................... 4 Prospects for Europe .................................................................................................................. 5 Background and Research Objectives For the 50th anniversary of the launch of Sputnik-1, in 2007, the rebirth of Russian space activities appeared well on its way. After the decade-long crisis of the 1990s, the country’s political leadership guided by President Putin gave new impetus to the development of national space activities and put the sector back among the top priorities of Moscow’s domestic and foreign policy agenda. Supported by the progressive recovery of Russia’s economy, renewed political stability, and an improving external environment, Russia re-asserted strong ambitions and the resolve to regain its original position on the international scene. Towards this, several major space programmes were adopted, including the Federal Space Programme 2006-2015, the Federal Target Programme on the development of Russian cosmodromes, and the Federal Target Programme on the redeployment of GLONASS. This renewed commitment to the development of space activities was duly reflected in a sharp increase in the country’s launch rate and space budget throughout the decade. Thanks to the funds made available by flourishing energy exports, Russia’s space expenditure continued to grow even in the midst of the global financial crisis. Besides new programmes and increased funding, the spectrum of activities was also widened to encompass a new focus on space applications and commercial products. -
Planetary Science Division Status Report
Planetary Science Division Status Report Jim Green NASA, Planetary Science Division January 26, 2017 Astronomy and Astrophysics Advisory CommiBee Outline • Planetary Science ObjecFves • Missions and Events Overview • Flight Programs: – Discovery – New FronFers – Mars Programs – Outer Planets • Planetary Defense AcFviFes • R&A Overview • Educaon and Outreach AcFviFes • PSD Budget Overview New Horizons exploresPlanetary Science Pluto and the Kuiper Belt Ascertain the content, origin, and evoluFon of the Solar System and the potenFal for life elsewhere! 01/08/2016 As the highest resolution images continue to beam back from New Horizons, the mission is onto exploring Kuiper Belt Objects with the Long Range Reconnaissance Imager (LORRI) camera from unique viewing angles not visible from Earth. New Horizons is also beginning maneuvers to be able to swing close by a Kuiper Belt Object in the next year. Giant IcebergsObjecve 1.5.1 (water blocks) floatingObjecve 1.5.2 in glaciers of Objecve 1.5.3 Objecve 1.5.4 Objecve 1.5.5 hydrogen, mDemonstrate ethane, and other frozenDemonstrate progress gasses on the Demonstrate Sublimation pitsDemonstrate from the surface ofDemonstrate progress Pluto, potentially surface of Pluto.progress in in exploring and progress in showing a geologicallyprogress in improving active surface.in idenFfying and advancing the observing the objects exploring and understanding of the characterizing objects The Newunderstanding of Horizons missionin the Solar System to and the finding locaons origin and evoluFon in the Solar System explorationhow the chemical of Pluto wereunderstand how they voted the where life could of life on Earth to that pose threats to and physical formed and evolve have existed or guide the search for Earth or offer People’sprocesses in the Choice for Breakthrough of thecould exist today life elsewhere resources for human Year forSolar System 2015 by Science Magazine as exploraon operate, interact well as theand evolve top story of 2015 by Discover Magazine. -
The Orbits of Saturn's Small Satellites Derived From
The Astronomical Journal, 132:692–710, 2006 August A # 2006. The American Astronomical Society. All rights reserved. Printed in U.S.A. THE ORBITS OF SATURN’S SMALL SATELLITES DERIVED FROM COMBINED HISTORIC AND CASSINI IMAGING OBSERVATIONS J. N. Spitale CICLOPS, Space Science Institute, 4750 Walnut Street, Suite 205, Boulder, CO 80301; [email protected] R. A. Jacobson Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099 C. C. Porco CICLOPS, Space Science Institute, 4750 Walnut Street, Suite 205, Boulder, CO 80301 and W. M. Owen, Jr. Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099 Received 2006 February 28; accepted 2006 April 12 ABSTRACT We report on the orbits of the small, inner Saturnian satellites, either recovered or newly discovered in recent Cassini imaging observations. The orbits presented here reflect improvements over our previously published values in that the time base of Cassini observations has been extended, and numerical orbital integrations have been performed in those cases in which simple precessing elliptical, inclined orbit solutions were found to be inadequate. Using combined Cassini and Voyager observations, we obtain an eccentricity for Pan 7 times smaller than previously reported because of the predominance of higher quality Cassini data in the fit. The orbit of the small satellite (S/2005 S1 [Daphnis]) discovered by Cassini in the Keeler gap in the outer A ring appears to be circular and coplanar; no external perturbations are appar- ent. Refined orbits of Atlas, Prometheus, Pandora, Janus, and Epimetheus are based on Cassini , Voyager, Hubble Space Telescope, and Earth-based data and a numerical integration perturbed by all the massive satellites and each other. -
Enhanced Gravity Tractor Technique for Planetary Defense
4th IAA Planetary Defense Conference – PDC 2015 13-17 April 2015, Frascati, Roma, Italy IAA-PDC-15-04-11 ENHANCED GRAVITY TRACTOR TECHNIQUE FOR PLANETARY DEFENSE Daniel D. Mazanek(1), David M. Reeves(2), Joshua B. Hopkins(3), Darren W. Wade(4), Marco Tantardini(5), and Haijun Shen(6) (1)NASA Langley Research Center, Mail Stop 462, 1 North Dryden Street, Hampton, VA, 23681, USA, 1-757-864-1739, (2) NASA Langley Research Center, Mail Stop 462, 1 North Dryden Street, Hampton, VA, 23681, USA, 1-757-864-9256, (3)Lockheed Martin Space Systems Company, Mail Stop H3005, PO Box 179, Denver, CO 80201, USA, 1-303- 971-7928, (4)Lockheed Martin Space Systems Company, Mail Stop S8110, PO Box 179, Denver, CO 80201, USA, 1-303-977-4671, (5)Independent, via Tibaldi 5, Cremona, Italy, +393381003736, (6)Analytical Mechanics Associates, Inc., 21 Enterprise Parkway, Suite 300, Hampton, VA 23666, USA, 1-757-865-0000, Keywords: enhanced gravity tractor, in-situ mass augmentation, asteroid and comet deflection, planetary defense, low-thrust, high-efficiency propulsion, gravitational attraction, robotic mass collection Abstract Given sufficient warning time, Earth-impacting asteroids and comets can be deflected with a variety of different “slow push/pull” techniques. The gravity tractor is one technique that uses the gravitational attraction of a rendezvous spacecraft to the impactor and a low-thrust, high-efficiency propulsion system to provide a gradual velocity change and alter its trajectory. An innovation to this technique, known as the Enhanced Gravity Tractor (EGT), uses mass collected in-situ to augment the mass of the spacecraft, thereby greatly increasing the gravitational force between the objects. -
Deflecting a Hazardous Near-Earth Object 1St IAA Planetary Defense
Deflecting a Hazardous Near-Earth Object 1st IAA Planetary Defense Conference: Protecting Earth from Asteroids 27-30 April 2009 Granada, Spain D.K. Yeomans(1), S. Bhaskaran(1), S.B. Broschart(1), S.R. Chesley(1), P.W. Chodas(1), T. H. Sweetser(1), R. Schweickart(2) (1)JPL/Caltech 4800 Oak Grove Drive Pasadena, CA 91109, USA [email protected] ( 2)B612 Foundation 760 Fifth St. East Sonoma, CA 95476, USA [email protected] INTRODUCTION This short report on Near-Earth Object (NEO) hazard mitigation strategies was developed in response to a request for information by the U.S. National Research Council’s Space Sciences Board on December 17, 2008 and for the Planetary Defense Conference that took place 27-30 April 2009 in Granada Spain. Although we present example simulations for specific techniques that could be employed to deflect an Earth threatening NEO, our primary goal is to discuss some of the general principles and techniques that would be germane to all NEO deflection scenarios. This report summarizes work that was carried out in early 2009 and extends an earlier, more detailed study carried out in late 2008 [1]. STUDY OVERVIEW Because of the wide range of possible sizes, trajectories and warning times for Earth threatening NEOs, there will be a corresponding range in the levels of challenge in providing an appropriate mitigation response. Unless there are decades of warning time, hazardous NEOs larger than a few hundred meters in diameter may require large energies to deflect or fragment. In these cases, nuclear explosions, either stand- off or surface blasts, might provide a suitable response. -
Asteroid Deflection Using a Solar-Sailed Electromagnetic Gravity Tractor
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 06 | June 2020 www.irjet.net p-ISSN: 2395-0072 Asteroid Deflection using a Solar-Sailed Electromagnetic Gravity Tractor Parvati Rajesh Student, Department of Mechanical Engineering, Presidency University, Itgalpur, Rajanakunte, Yelahanka, Bengaluru, Karnataka, Pin Code- 560064, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract – An asteroid threat is one of the topics in science which gets less coverage. If an asteroid as small as 200m were to collide with earth, that would annihilate modern infrastructure and cause significant losses in biodiversity. One such theoretical solution developed to prevent this from occurring is a Gravity Tractor. A Gravity Tractor is a theoretical spacecraft which aims to alter the trajectory of an asteroid which is on the course to collide with earth. Although there have been numerous anticipated designs and alterations in this subject matter, this paper intends to suggest an idea of a gravity tractor integrated with a solar sail for solar- electric propulsion coupled with a feature of electromagnetism to exert a stronger attraction force on the asteroid if it is made out of a metallic core. Figure 1 Key Words: Asteroid, Gravity tractor, Threat Assuming the asteroid shown in the figure above is at mitigation, asteroid collision, space craft, least a 100 light years away and has been detected by Gravitational towing, Near Earth Objects, planetary defenses of various space agencies ,other electromagnetic spacecraft private industries or any other means, if a tractor is sent on time and the deflection is made at a safe 1. INTRODUCTION distance, a small deflection (α) will cause a significant amount of change in course for the asteroid to he idea of a spacecraft for altering the course of an completely omit earth. -
Leonid Gurvits JIVE and TU Delft June 3, 2021 ©Cristian Fattinanzi Piter Y Moons Xplorer
Leonid Gurvits JIVE and TU Delft June 3, 2021 ©Cristian Fattinanzi piter y moons xplorer Why a mission to Jupiter? Bits of history Mission challenges Where radio astronomy comes in • ~2000–2005: success of Cassini and Huygens missions (NASA, ESA, ASI) • 2006: Europlanet meeting in Berlin – “thinking aloud” on a Jovian mission • 2008: ESA-NASA jointly exploring a mission to giant planets’ satellites • ESA "Laplace" mission proposal (Blanc et al. 2009) • ESA Titan and Enceladus Mission (TandEM, Coustenis et al., 2009) • NASA Titan Explorer • 2009: two joint (ESA+NASA) concepts selected for further studies: • Europa Jupiter System Mission (EJSM) • Titan Saturn System Mission (TSSM: Coustenis et al., 2009) • 2010: EJSM-Laplace selected, consisting of two spacecraft: • ESA’s Jupiter Ganymede Orbiter (JGO) • NASA’s Jupiter Europa Orbiter (JEO) • 2012: NASA drops off; EJSM-Laplace/JGO becomes JUICE • 2013: JUICE payload selection completed by ESA; JUICE becomes an L-class mission of ESA’s Vision 2015-2025 • 2015: NASA selects Europa Clipper mission (Pappalardo et al., 2013) Voyager 1, 1979 ©NASA HOW DOES IT SEARCH FOR ORIGINS & WORK? LIFE FORMATION HABITABILITY Introduction Overarching questions JUICE JUICE Science Themes • Emergence of habitable worlds around gas giants • Jupiter system as an archetype for gas giants JUICE concept • European-led mission to the Jovian system • First orbiter of an icy moon • JGO/Laplace scenario with two Europa flybys and moderate-inclination phase at Jupiter • Science payload selected in Feb 2013, fully compatible -
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. -
HUMAN ADAPTATION to SPACEFLIGHT: the ROLE of FOOD and NUTRITION Second Edition
National Aeronautics and Human Space Administration Adaptation to Spaceflight: The Role of Food and Nutrition Second Edition Scott M. Smith Sara R. Zwart Grace L. Douglas Martina Heer National Aeronautics and Space Administration HUMAN ADAPTATION TO SPACEFLIGHT: THE ROLE OF FOOD AND NUTRITION Second Edition Scott M. Smith Grace L. Douglas Nutritionist; Advanced Food Technology Lead Scientist; Manager for Nutritional Biochemistry Manager for Exploration Food Systems Nutritional Biochemistry Laboratory Space Food Systems Laboratory Biomedical Research and Human Systems Engineering and Environmental Sciences Division Integration Division Human Health and Performance Human Health and Performance Directorate Directorate NASA Johnson Space Center NASA Johnson Space Center Houston, Texas USA Houston, Texas USA Sara R. Zwart Martina Heer Senior Scientist; Nutritionist; Deputy Manager for Nutritional Program Director Nutritional Sciences Biochemistry IU International University of Nutritional Biochemistry Laboratory Applied Sciences Biomedical Research and Bad Reichenhall, Germany Environmental Sciences Division & Human Health and Performance Adjunct Professor of Nutrition Physiology Directorate Institute of Nutritional and Food Sciences NASA Johnson Space Center University of Bonn, Germany Houston, Texas USA & Preventive Medicine and Population Health University of Texas Medical Branch Galveston, Texas USA Table of Contents Preface ......................................................................................................................... -
Janus: a Mission Concept to Explore Two NEO Binary Asteroids
Janus: A mission concept to explore two NEO Binary Asteroids D.J. Scheeres1, J.W. McMahon1, J. Hopkins2, C. Hartzell3, E.B. Bierhaus2, L.A.M. Benner4, P. Hayne1, R. Jedicke5, L. LeCorre6, S. Naidu4, P. Pravec7, and M. Ravine8 1The University of Colorado Boulder, USA; 2Lockheed Martin Inc, USA; 3University of Maryland, USA; 4Jet Propulsion Laboratory, USA; 5University of Hawaii, USA; 6Planetary Science Institute, USA; 7Astronomical Institute of the Academy of Sciences, Czech Republic; 8Malin Space Science Systems Inc, USA University of Colorado and/or Lockheed Martin Proprietary Information SIMPLEx AO: NNH17ZDA004O-SIMPLEx July 2018 Janus Mission Selected for Phase A/B! • Janus was submitted to the inaugural SIMPLEx call for proposals – Launch provided on an upcoming mission, e.g., Lucy or Psyche, for interplanetary missions – Up to $55M for a given mission • Proposals were submitted July 2018 (12 total submissions) • Announcement made last Wednesday… Janus is selected for Phase A/B! (1/3) D.J. Scheeres, A. Richard Seebass Chair, University of Colorado at Boulder !2 B-1 Use or disclosure of data contained on this sheet is subject to the restriction on the title page of this proposal University of Colorado and/or Lockheed Martin Proprietary Information University of Colorado and/or Lockheed Martin Proprietary Information SIMPLEx AO: NNH17ZDA004O-SIMPLEx July 2018 B FACT SHEET Malin SSS B-1 Use or disclosure of data contained on this sheet is subject to the restriction on the title page of this proposal University of Colorado and/or Lockheed Martin Proprietary Information University of Colorado and/or Lockheed Martin Proprietary Information SIMPLEx AO: NNH17ZDA004O-SIMPLEx July 2018 B FACT SHEET The Janus Science Objectives and corresponding Mission Implementation are focused and simple D.J. -
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.