Infrequent Visitors of the Kozai Kind: the Dynamical Lives of 2012 FC71
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Asteroid Regolith Weathering: a Large-Scale Observational Investigation
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Doctoral Dissertations Graduate School 5-2019 Asteroid Regolith Weathering: A Large-Scale Observational Investigation Eric Michael MacLennan University of Tennessee, [email protected] Follow this and additional works at: https://trace.tennessee.edu/utk_graddiss Recommended Citation MacLennan, Eric Michael, "Asteroid Regolith Weathering: A Large-Scale Observational Investigation. " PhD diss., University of Tennessee, 2019. https://trace.tennessee.edu/utk_graddiss/5467 This Dissertation is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Doctoral Dissertations by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a dissertation written by Eric Michael MacLennan entitled "Asteroid Regolith Weathering: A Large-Scale Observational Investigation." I have examined the final electronic copy of this dissertation for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Doctor of Philosophy, with a major in Geology. Joshua P. Emery, Major Professor We have read this dissertation and recommend its acceptance: Jeffrey E. Moersch, Harry Y. McSween Jr., Liem T. Tran Accepted for the Council: Dixie L. Thompson Vice Provost and Dean of the Graduate School (Original signatures are on file with official studentecor r ds.) Asteroid Regolith Weathering: A Large-Scale Observational Investigation A Dissertation Presented for the Doctor of Philosophy Degree The University of Tennessee, Knoxville Eric Michael MacLennan May 2019 © by Eric Michael MacLennan, 2019 All Rights Reserved. -
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. -
Jjmonl 1606.Pmd
alactic Observer GJohn J. McCarthy Observatory Volume 9, No. 6 June 2016 Dead End? Conventional wisdom has long held that galaxies regenerate from the gas and debris of their own dead stars. Find out why that isn't always true - inside, page 15 http://www.mccarthyobservatory.org June 2016 • 1 The John J. McCarthy Observatory Galactic Observvvererer New Milford High School Editorial Committee 388 Danbury Road Managing Editor New Milford, CT 06776 Bill Cloutier Phone/Voice: (860) 210-4117 Production & Design Phone/Fax: (860) 354-1595 www.mccarthyobservatory.org Allan Ostergren Website Development JJMO Staff Marc Polansky It is through their efforts that the McCarthy Observatory Technical Support has established itself as a significant educational and Bob Lambert recreational resource within the western Connecticut Dr. Parker Moreland community. Steve Barone Jim Johnstone Colin Campbell Carly KleinStern Dennis Cartolano Bob Lambert Mike Chiarella Roger Moore Route Jeff Chodak Parker Moreland, PhD Bill Cloutier Allan Ostergren Cecilia Dietrich Marc Polansky Dirk Feather Joe Privitera Randy Fender Monty Robson Randy Finden Don Ross John Gebauer Gene Schilling Elaine Green Katie Shusdock Tina Hartzell Paul Woodell Tom Heydenburg Amy Ziffer In This Issue OUT THE WINDOW ON YOUR LEFT .................................... 4 ASTRONOMICAL AND HISTORICAL EVENTS ......................... 12 SURVEYOR 1 LANDING SITE .............................................. 4 COMMONLY USED TERMS ............................................... 14 2016 MERCURY TRANSIT -
The “Horseshoe” Orbit of Near-Earth Object 2013 BS45 DANIEL R
Page 20 Astrodynamics The “Horseshoe” Orbit of Near-Earth Object 2013 BS45 DANIEL R. ADAMO, ASTRODYNAMICS CONSULTANT 1. Earth-Based Discovery million km) on 12 February inbound towards the Sun. It 2013. reaches perihelion on 29 April Discovered by the Space- 2013 at 0.92 AU or 92% of watch 1.8 m telescope (see As is typical among NEO Earth’s mean distance from Figure 1) on 20 January 2013, discoveries made in the night the Sun. Figure 2 is a plot of near-Earth object (NEO) 2013 sky prior to closest Earth ap- 2013 BS45, Earth, and Mars as BS45 closely encountered proach with observations of they orbit the Sun during Earth at a range of 0.0126 AU our planet’s night sky, 2013 2013. (4.9 lunar distances or 1.88 BS45 crosses Earth’s orbit Figure 1. The 1.8 m Space- watch telescope is pictured inside its protective dome at Kitt Peak, Arizona (photograph by Robert S. McMillan). Figure 2. Orbits of 2013 BS45 (blue), Earth (green), and Mars (red) are plotted during year 2013 in a non-rotating (inertial) Sun-centered (heliocentric) coordinate system. The plot plane coincides with that of Earth’s orbit, the ecliptic, and 2013 BS45’s orbit is inclined to the ecliptic by less than 1°. Before moving into Earth’s BS45 ephemerides with maxi- planetary radar observations daytime sky circa 9 February mum position uncertainties conducted at Goldstone, CA 2013, about 80 optical obser- equivalent to hundreds of had reduced this uncertainty vations were being processed minutes in heliocentric mo- to the order of 10 minutes. -
Preliminary Lander Cubesat Design for Small Asteroid Detumbling Mission
DEGREE PROJECT IN VEHICLE ENGINEERING, SECOND CYCLE, 30 CREDITS STOCKHOLM, SWEDEN 2018 Preliminary Lander CubeSat Design for Small Asteroid Detumbling Mission AGNE PASKEVICIUTE KTH ROYAL INSTITUTE OF TECHNOLOGY SCHOOL OF ENGINEERING SCIENCES Preliminary Lander CubeSat Design for Small Asteroid Detumbling Mission AgnėPaökevičiūtė Department of Aeronautical and Vehicle Engineering KTH Royal Institute of Technology This thesis is submitted for the degree of Master of Science October 2018 Skiriu ö˛ darbπsavo mamai Graûinai ir tėčiui Algirdui. Acknowledgements This thesis would have not been possible without the encouragement and support of numerous people in my life. I would especially like to thank Dr Michael C. F. Bazzocchi for his support and constructive advice throughout my research. In addition, I would like to express my gratitude to researchers, professors and staffat Luleå University of Technology, Space Campus, for their ideas and help in practical matters. I would like to sincerely thank my family, boyfriend, and friends for believing in me, encour- aging me to reach for my dreams, and loving me without any expectations. Last but not least, I am truly grateful for the opportunities KTH Royal Institute of Technol- ogy provided. Sammanfattning Gruvdrift på asteroider förväntas att bli verklighet inom en snar framtid. Det första steget är att omdirigera en asteroid till en stabil omloppsbana runt jorden så att gruvteknik kan demon- streras. Bromsning av asteroidens tumlande är en av de viktigaste stegen i ett rymduppdrag där en asteroid ska omdirigeras. I detta examensarbete föreslås en preliminär asteroidlandare baserad på CubeSat-teknik för ett rymduppdrag där en asteroid ska omdirigeras. En asteroid av Arjuna-typ, 2014 UR, med en diameter på mellan 10.6 och 21.2 m är vald som kandidat för rymduppdraget. -
The Palomar Transient Factory (PTF) Survey & Discovery of Small
The Palomar Transient Factory (PTF) Survey & Discovery of Small Mission-Accessible NEAs Adam Waszczak Graduate Student Division of Geological & Planetary Sciences California Institute of Technology The Palomar Transient Factory (PTF) 48-inch (1.2-m) “Oschin” robotic wide-field imaging [r-band] exposure time: 60s field-of-view: 7.3 deg2 / 11 CCDs limiting mag: r 20.5 resolution: 1.0 arcsec/pixel typical seeing: 2.0 arcsec FWHM The Palomar Transient Factory (PTF) 48-inch (1.2-m) “Oschin” robotic wide-field imaging [r-band] exposure time: 60s field-of-view: 7.3 deg2 / 11 CCDs limiting mag: r 20.5 resolution: 1.0 arcsec/pixel typical seeing: 2.0 arcsec FWHM The Palomar Transient Factory (PTF) 60-inch (1.5-m) robotic imaging follow-up [ugriz-bands & SED machine] 48-inch (1.2-m) “Oschin” robotic wide-field imaging [r-band] The Palomar Transient Factory (PTF) 60-inch (1.5-m) robotic imaging follow-up [ugriz-bands & SED machine] 48-inch (1.2-m) “Oschin” 200-inch (5.2-m) “Hale” robotic wide-field imaging spectroscopic follow-up [DBSP] [r-band] The Palomar Transient Factory (PTF) 60-inch (1.5-m) robotic imaging follow-up [ugriz-bands & SED machine] 48-inch (1.2-m) “Oschin” 200-inch (5.2-m) “Hale” robotic wide-field imaging spectroscopic follow-up [DBSP] [r-band] PTF is a world leader in the discovery and spectroscopic follow-up of extragalactic transients (e.g., supernovae). PTF detections of asteroids in general In past year, PTF submitted over 500,000 observations to the Minor Planet Center. -
A Resonant Family of Dynamically Cold Small Bodies in the Near-Earth Asteroid Belt
MNRASL 434, L1–L5 (2013) doi:10.1093/mnrasl/slt062 Advance Access publication 2013 June 18 A resonant family of dynamically cold small bodies in the near-Earth asteroid belt C. de la Fuente Marcos‹ and R. de la Fuente Marcos Universidad Complutense de Madrid, Ciudad Universitaria, E-28040 Madrid, Spain Accepted 2013 May 13. Received 2013 May 10; in original form 2013 February 25 Downloaded from https://academic.oup.com/mnrasl/article/434/1/L1/1163370 by guest on 27 September 2021 ABSTRACT Near-Earth objects (NEOs) moving in resonant, Earth-like orbits are potentially important. On the positive side, they are the ideal targets for robotic and human low-cost sample return missions and a much cheaper alternative to using the Moon as an astronomical observatory. On the negative side and even if small in size (2–50 m), they have an enhanced probability of colliding with the Earth causing local but still significant property damage and loss of life. Here, we show that the recently discovered asteroid 2013 BS45 is an Earth co-orbital, the sixth horseshoe librator to our planet. In contrast with other Earth’s co-orbitals, its orbit is strikingly similar to that of the Earth yet at an absolute magnitude of 25.8, an artificial origin seems implausible. The study of the dynamics of 2013 BS45 coupled with the analysis of NEO data show that it is one of the largest and most stable members of a previously undiscussed dynamically cold group of small NEOs experiencing repeated trappings in the 1:1 commensurability with the Earth. -
Near-Earth Object Resource
NEO Resource Near-Earth Object Resource Compiled and edited by James M. Thomas for the Museum Astronomical Resource Society http://marsastro.org and the NASA/JPL Solar System Ambassador Program http://www.jpl.nasa.gov/ambassador Updated July 15, 2006 Based upon material available through the NASA Near-Earth Object Program http://neo.jpl.nasa.gov/ 1 of 104 NEO Resource Table of Contents Section Page Introduction & Overview 5 Target Earth 6 • The Cretaceous/Tertiary (K-T) Extinction 9 • Chicxulub Crater 10 • Barringer Meteorite Crater 13 What Are Near-Earth Objects (NEOs)? 14 What Is The Purpose Of The Near-Earth Object Program? 14 How Many Near-Earth Objects Have Been Discovered So Far? 15 What Is A PHA? 16 What Are Asteroids And Comets? 17 What Are The Differences Between An Asteroid, Comet, Meteoroid, Meteor and 19 Meteorite? Why Study Asteroids? 21 Why Study Comets? 24 What Are Atens, Apollos and Amors? 27 NEO Groups 28 Near-Earth Objects And Life On Earth 29 Near-Earth Objects As Future Resources 31 Near-Earth Object Discovery Teams 32 2 of 104 NEO Resource • Lincoln Near-Earth Asteroid Research (LINEAR) 35 • Near-Earth Asteroid Tracking (NEAT) 37 • Spacewatch 39 • Lowell Observatory Near-Earth Object Search (LONEOS) 41 • Catalina Sky Surveys 42 • Japanese Spaceguard Association (JSGA) 44 • Asiago DLR Asteroid Survey (ADAS) 45 Spacecraft Missions to Comets and Asteroids 46 • Overview 46 • Mission Summaries 49 • Near-Earth Asteroid Rendezvous (NEAR) 49 • DEEP IMPACT 49 • DEEP SPACE 1 50 • STARDUST 50 • Hayabusa (MUSES-C) 51 • ROSETTA -
Deep-Space Cubesats: Thinking Inside the Box
CUBESATS Deep-space CubeSats: thinking inside the box Roger Walker and colleagues CubeSats: small but perfectly formed consider the potential for sending Downloaded from https://academic.oup.com/astrogeo/article-abstract/59/5/5.24/5099069 by guest on 22 September 2018 nanospacecraft into deep space. CubeSats are modular spacecraft, using multiple standard-sized units of 10 x 10 x 10 cm ince the introduction of the CubeSat (figure 1); the size of the resulting spacecraft standard in the early 2000s, there has is measured by the number of units, e.g. 3U Sbeen a proliferation of nano-/small or 6U. The capabilities of these satellites have microsatellites in low Earth orbit, with increased significantly in recent years, notably 100–300 or more launched annually and at in pointing, propulsion and communications a growing rate (according to reports from as well as the availability of compact optical/ SpaceWorks and Euroconsult). CubeSats radio frequency/environment payloads. have reduced entry-level costs for space CubeSats are launched inside a standard missions in low Earth orbit (LEO) by container which simplifies launcher more than an order of magnitude (see box accommodation while ensuring safety for “CubeSats: small but perfectly formed”). the primary passenger, thus facilitating 1 Example of a 1U CubeSat shell. There is a This has brought new players into the widespread low-cost piggyback launch weight standard too – the finished launch unit space sector and launch opportunities for opportunities on many different launch must not exceed 1.33 kg. (ESA/G Porter) CubeSats have increased significantly in vehicles worldwide. At the same time, the the last decade to address the associated extensive use of miniaturized electronics, entry-level costs mean that the true power of demand. -
From Horseshoe to Quasi-Satellite and Back Again: the Curious Dynamics Of
From horseshoe to quasi-satellite and back again: the curious dynamics of Earth co-orbital asteroid 2015 SO2 C. de la Fuente Marcos • R. de la Fuente Marcos Abstract Earth co-orbitals of the horseshoe type are this case is the difference between the mean longitudes interesting objects to study for practical reasons. They of the asteroid and its host planet or relative mean lon- are relatively easy to access from our planet and that gitude. The mean longitude of an object —planet or makes them attractive targets for sample return mis- minor body— is given by λ = M +Ω+ ω, where M sions. Here, we show that near-Earth asteroid (NEA) is the mean anomaly, Ω is the longitude of the ascend- 2015 SO2 is a transient co-orbital to the Earth that ing node, and ω is the argument of perihelion (see, e.g., experiences a rather peculiar orbital evolution charac- Murray & Dermott 1999). For these objects, the value terised by recurrent, alternating horseshoe and quasi- of the critical angle librates or oscillates; for a regular satellite episodes. It is currently following a horseshoe passing body, the relative mean longitude circulates or trajectory, the ninth asteroid known to do so. Besides takes any value in the range (0, 2π). Even if some of moving inside the 1:1 mean motion resonance with the them can experience relatively close flybys, co-orbital Earth, it is subjected to a Kozai resonance with the asteroids tend to be small, transient visitors and they value of the argument of perihelion librating around ◦ do not pose a particularly high hazard for their host 270 . -
The "Horseshoe" Orbit of Near-Earth Object 2013 BS45 1. Earth-Based
The "Horseshoe" Orbit Of Near-Earth Object 2013 BS45 1. Earth-Based Discovery Discovered by the Spacewatch 1.8 m telescope (see Figure 1) on 20 January 2013, near-Earth object (NEO) 2013 BS45 undergoes closest approach to Earth at a range of 0.0126 AU (4.9 lunar distances or 1.88 million km) on 12 February 2013. Figure 1. The 1.8 m Spacewatch telescope is pictured inside its protective dome at Kitt Peak, Arizona (photograph by Robert S. McMillan). As is typical among NEO discoveries made prior to Earth closest approach with observations of our planet's night sky, 2013 BS45 crosses Earth's orbit inbound towards the Sun. It reaches Daniel R. Adamo 1 17 May 2013 The "Horseshoe" Orbit Of Near-Earth Object 2013 BS45 perihelion on 29 April 2013 at 0.92 AU or 92% of Earth's mean distance from the Sun. Figure 2 is a plot of 2013 BS45, Earth, and Mars as they orbit the Sun during 2013. Figure 2. Orbits of 2013 BS45 (blue), Earth (green), and Mars (red) are plotted during year 2013 in a non-rotating (inertial) Sun-centered (heliocentric) coordinate system. The plot plane coincides with that of Earth's orbit, the ecliptic, and 2013 BS45's orbit is inclined to the ecliptic by less than 1°. Before moving into Earth's daytime sky circa 9 February 2013, about 80 optical observations were being processed by the Jet Propulsion Laboratory (JPL) to produce 2013 BS45 ephemerides with maximum position uncertainties equivalent to hundreds of minutes in heliocentric motion a century in the past or future. -
Asteroid Redirect Mission Status
National Aeronautics and Space Administration Asteroid Redirect Mission Update NAC Human Exploration and Operations Committee Dr. Michele Gates March 2, 2016 1 Last Update in July Included • Updates on contributions of the mission to exploration strategy and Journey to Mars • Guidance for ARRM formulation • A focus on external engagement and feedback 2 Asteroid Redirect Mission Progress Robotic Mission Concept Review and Formulation Authorization Mar 2015 Acquisition Strategy Decisions for Robotic Mission Aug 2015 Formulation Assessment and Support Team (FAST) Established Aug 2015 Public comments due on FAST draft report Dec 2015 • https://www.nasa.gov/feature/arm-fast Robotic mission requirements technical interchange meeting Dec 2015 Robotic spacecraft early design study contracts selected Jan 2016 Update with Small Bodies Assessment Group Jan 2016 Complete 6th of 6 total Peer Reviews for Restore-L Jan 2016 Synergy Subsystems Crewed segment operational requirements meetings at JSC Feb 2016 ARM leadership team strategy meeting on partnerships and Feb 2016 engagement FAST final report released Feb 2016 3 A Sustainable Exploration Approach Mars Split Mission Concept Getting to Mars DESTINATION SYSTEMS SEP pre-deploy to Mars orbit Transit: 2-3 Years Surface Operations: 30-500 Days TRANSIT HAB TO MARS Aggregate in Cis-lunar space 6-9 Months CREW/TRANSIT HAB CREW/TRANSIT HAB To Mars orbit via chemical propulsion Aggregation in CRE W Launch to HEO/DRO Cis-lunar space HABITATS return to staging 6-9 Months point for refurbishment CREW/TRANSIT