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One Team from This State Was the First Your Writer Ever Lost to at a National Tournament
1. (Meta) One team from this state was the first your writer ever lost to at a National tournament. One coach from this state created (^) an A-set tournament solely in order to qualify his team for HSNCT after proposing an all-female tournament, Title IX Bowl. A 2009 cheating scandal in (+) this state involved a team’s gmail account being used by its treasurer to access SCT questions, which he then used to defeat such powerhouse teams as Vanderbilt B. A standing rule (*) of ILQBM bans memes from this state, and the top-ranked team from this state lost to their own B team at New Trier Varsity. For ten points, name this state home to teams such as Northview and Chattahoochee. Answer: Georgia Bonus: Name the following about other cheaters. [10] This Windhaven Park E player won a tournament with a 66/18/3 statline after improperly accessing IS-164 questions. He did not demonstrate his knowledge via skype due to a sudden attack of buzzer shyness. Answer: Ethan McBride [10] (pseudonyms acceptable) This early Ohioan cheater notably created two sock puppet forum accounts pretending to be his friend and his friend’s mother to attest to his good character and mask the fact that he played a HS tournament despite being in college. Answer: Basileus (accept dafirenze, Paul Harold, Nancydf64) [10] This most notorious of quizbowl cheaters was referred to as “the grand vizier of fuckfaces” in a hate thread dedicated to him. He won three ICTs for Harvard, all of which were rescinded. Answer: Andy Watkins 2. -
Small Solar System Bodies As Granular Media D
Small Solar System Bodies as granular media D. Hestroffer, P. Sanchez, L Staron, A. Campo Bagatin, S. Eggl, W. Losert, N. Murdoch, E. Opsomer, F. Radjai, D. C. Richardson, et al. To cite this version: D. Hestroffer, P. Sanchez, L Staron, A. Campo Bagatin, S. Eggl, et al.. Small Solar System Bodiesas granular media. Astronomy and Astrophysics Review, Springer Verlag, 2019, 27 (1), 10.1007/s00159- 019-0117-5. hal-02342853 HAL Id: hal-02342853 https://hal.archives-ouvertes.fr/hal-02342853 Submitted on 4 Nov 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Astron Astrophys Rev manuscript No. (will be inserted by the editor) Small solar system bodies as granular media D. Hestroffer · P. S´anchez · L. Staron · A. Campo Bagatin · S. Eggl · W. Losert · N. Murdoch · E. Opsomer · F. Radjai · D. C. Richardson · M. Salazar · D. J. Scheeres · S. Schwartz · N. Taberlet · H. Yano Received: date / Accepted: date Made possible by the International Space Science Institute (ISSI, Bern) support to the inter- national team \Asteroids & Self Gravitating Bodies as Granular Systems" D. Hestroffer IMCCE, Paris Observatory, universit´ePSL, CNRS, Sorbonne Universit´e,Univ. -
Mission Science Highlights and Science Objectives Assessment
CASSINI FINAL MISSION REPORT 2019 1 MISSION SCIENCE HIGHLIGHTS AND SCIENCE OBJECTIVES ASSESSMENT Cassini-Huygens, humanity’s most distant planetary orbiter and probe to date, provided the first in- depth, close up study of Saturn, its magnificent rings and unique moons, including Titan and Enceladus, and its giant magnetosphere. Discoveries from the Cassini-Huygens mission revolutionized our understanding of the Saturn system and fundamentally altered many of our concepts of where life might be found in our solar system and beyond. Cassini-Huygens arrived at Saturn in 2004, dropped the parachuted probe named Huygens to study the atmosphere and surface of Saturn’s planet-sized moon Titan, and orbited Saturn for the next 13 years making remarkable discoveries. When it was running low on fuel, the Cassini orbiter was programmed to vaporize in Saturn’s atmosphere in 2017 to protect the ocean worlds, Enceladus and Titan, where it discovered potential habitats for life. CASSINI FINAL MISSION REPORT 2019 2 CONTENTS MISSION SCIENCE HIGHLIGHTS AND SCIENCE OBJECTIVES ASSESSMENT ........................................................ 1 Executive Summary................................................................................................................................................ 5 Origin of the Cassini Mission ....................................................................................................................... 5 Instrument Teams and Interdisciplinary Investigations ............................................................................... -
Surface Properties of Asteroids from Mid-Infrared Observations and Thermophysical Modeling
Dissertation zur Erlangung des akademischen Grades Doktor der Naturwissenschaften (doctor rerum naturalium) Surface Properties of Asteroids from Mid-Infrared Observations and Thermophysical Modeling Dipl.-Phys. Michael M¨uller 2007 Eingereicht und verteidigt am Fachbereich Geowissenschaften der Freien Universit¨atBerlin. Angefertigt am Institut f¨ur Planetenforschung des Deutschen Zentrums f¨urLuft- und Raumfahrt e.V. (DLR) in Berlin-Adlershof. arXiv:1208.3993v1 [astro-ph.EP] 20 Aug 2012 Gutachter Prof. Dr. Ralf Jaumann (Freie Universit¨atBerlin, DLR Berlin) Prof. Dr. Tilman Spohn (Westf¨alische Wilhems-Universit¨atM¨unster,DLR Berlin) Tag der Disputation 6. Juli 2007 In loving memory of Felix M¨uller(1948{2005). Wish you were here. Abstract The subject of this work is the physical characterization of asteroids, with an emphasis on the thermal inertia of near-Earth asteroids (NEAs). Thermal inertia governs the Yarkovsky effect, a non-gravitational force which significantly alters the orbits of asteroids up to ∼ 20 km in diameter. Yarkovsky-induced drift is important in the assessment of the impact hazard which NEAs pose to Earth. Yet, very little has previously been known about the thermal inertia of small asteroids including NEAs. Observational and theoretical work is reported. The thermal emission of aster- oids has been observed in the mid-infrared (5{35 µm) wavelength range using the Spitzer Space Telescope and the 3.0 m NASA Infrared Telescope Facility, IRTF; techniques have been established to perform IRTF observations remotely from Berlin. A detailed thermophysical model (TPM) has been developed and exten- sively tested; this is the first detailed TPM shown to be applicable to NEA data. -
Don Quijote/Marco Polo/Rosetta (PDF)
Asteroids: next step? A summary of past and present activities at ESA on the exploration of asteroids and planetary defense by Marcello Coradini Head of the Robotic Exploration Office ESA Coordinator at JPL The population of Near-Earth Objects constitutes a significant threat to mankind. The hazard caused by the NEOs is characterized by a small probability of occurrence; however, the consequences of a collision of the Earth with a NEO could be catastrophic for mankind. Protection against the threat posed by NEO's must go through at least 4 steps, which in part can be carried out in parallel: Steps 1-2: assessment of the threat, including a characterization of the NEO population; Steps 3-4: Definition and set up of a protection system. The characterisation of the NEO population should comprise at least objects with a diameter larger than 1 km, which could cause a global catastrophe, while keeping in mind that ideally a complete survey should include NEO’s with a diameter down to 50-100 meters. Ground-based and space-based facilities are needed to achieve this objective. Europe can give immediately major contributions considering existing know-how and facilities, such as European observatories in both hemispheres, and planned space missions such as GAIA. As the purpose of this activity encompasses more than merely scientific objectives, new funds outside of those destined to space research should be made available. Step 2: This phase should include more than one mission devoted both to a better understanding of the physical and geophysical characteristics of a NEO and to, at least, another mission to test some space-borne mitigation techniques. -
Promieniowanie Rentgenowskie Rozbłysków Słonecznych ^ O Nauczaniu^|Trp^^|Ii •
tom LXXIII marzec-kwiecień Promieniowanie rentgenowskie rozbłysków słonecznych ^ O nauczaniu^|trp^^|ii • . 125 rocznica ódllrffeia trabantów Marsa Arjpliza obrazów CCD z kamery internetowej” . , w nb, Prof, Bohdan Pa wvkhidu aukowa CAMK, Warszawa, 18 lutego 2002 r. Wykład prof. Briana G. Wyboum Wystawa archiv^ov^pftji1 Fangor rozdaje legendarny 13. ni Uczestnicy dyskusji panelowej Prof. Andrzej K. Wróble U R A N I A • POSn-!>Y ASTRONOM;! Szanowni i Drodzy Czytelnicy; Obchodzimy osiemdziesiątą rocznicą istnienia „ Uranii ’’jako oficjalnego, drukowanego organu Towarzystwa Miłośników Astronomii. Na Sesji Naukowej w dniu 18 lutego 2002 r. najznakomitsi prelegenci mówili m.in. o tym, ja k uprawiać astronomią, o jedności fizyki i astronomii i o tym, ja k 80 lat rozwoju astronomii wyglądało w „ Uranii ”, oraz dyskutowali o edukacji astronomicznej Alina fot. Dauksza-Wiśniewska społeczeństwa. Zaraz po Sesji ten zeszyt będzie już w drukarni, więc oprócz programu obchodów i być może kilku wciśniętych w ostatniej chwili zdjęć, nic więcej na jej temat nie możemy tutaj zawrzeć. Ale przypomnijmy. Muza astronomii, Urania, stała się patronką działań „organicznych” i samokształceniowych młodzieży warszawskiej już na samym początku naszej Niepodległości i II Rzeczypospolitej. W roku szkolnym 1919/1920 w Gimnazjum im. Mikołaja Reja zawiązało się Kółko Astronomiczne, które m.in. rozpoczęło w 1920 r. wydawanie powielaczowego biuletynu pt. „ Urania Wydano 4 takie kwartalne numery. Wśród aktywnych członków tego Kółka byli m.in. przyszły astronom Jan Mergentaler i przyszły fizyk światowej sławy Stanisław Mrozowski, którzy później wielokrotnie gościli na lamach naszego czasopisma. Gdyby więc liczyć owe 4 numery, to poprzedni zeszyt „ Uranii - Postępów Astronomii ” otwierał nową setkę, już ósmą, zeszytów naszego czasopisma i byłby to 82. -
Arxiv:1907.02615V1 [Astro-Ph.EP] 4 Jul 2019 Department of Astronomy, University of Maryland, College Park, MD 20742, USA M
Astron Astrophys Rev manuscript No. (will be inserted by the editor) Small solar system bodies as granular media D. Hestroffer · P. S´anchez · L. Staron · A. Campo Bagatin · S. Eggl · W. Losert · N. Murdoch · E. Opsomer · F. Radjai · D. C. Richardson · M. Salazar · D. J. Scheeres · S. Schwartz · N. Taberlet · H. Yano Received: date / Accepted: date Made possible by the International Space Science Institute (ISSI, Bern) support to the inter- national team \Asteroids & Self Gravitating Bodies as Granular Systems" D. Hestroffer IMCCE, Paris Observatory, universit´ePSL, CNRS, Sorbonne Universit´e,Univ. Lille, F-75014 Paris, France Tel.: +33 1 4051 2260 E-mail: daniel.hestroff[email protected] P. S´anchez CCAR, University of Colorado Boulder, Boulder, CO 80309, USA L. Staron Inst. Jean Le Rond d'Alembert, Sorbonne Universit´e,CNRS, F-75005 Paris, France A. Campo Bagatin Departamento de F´ısica,Ingenier´ıade Sistemas y Teor´ıa de la Se~nal, Universidad de Alicante, E-03080 Alicante, Spain Instituto Universitario de F´ısica Aplicada a las Ciencias y las Tecnolog´ıas, Universidad de Alicante, E-03080 Alicante, Spain S. Eggl IMCCE, Paris Observatory, universit´ePSL, CNRS, Sorbonne Universit´e,Univ. Lille, F-75014 Paris, France LSST / DiRAC Institute, Department of Astronomy, University of Washington, Seattle, WA 98105, USA W. Losert Institute for Physical Science and Technology, and Department of Physics, University of Mary- land, College Park, MD 20742, USA N. Murdoch DEOS/SSPA, Institut Sup´erieurde l'A´eronautiqueet de l'Espace (ISAE-SUPAERO), Univer- sit´ede Toulouse, 31400 Toulouse, France E. Opsomer GRASP, Research Unit CESAM, University of Li`ege,B-4000 Li`ege,Belgium F. -
Obliquity, Precession Rate, and Nutation Coefficients for a Set of 100 Asteroids
A&A 556, A8 (2013) Astronomy DOI: 10.1051/0004-6361/201321205 & c ESO 2013 Astrophysics Obliquity, precession rate, and nutation coefficients for a set of 100 asteroids C. Lhotka1, J. Souchay2, and A. Shahsavari2 1 Department of Mathematics, University of Rome Tor Vergata, 00133 Rome, Italy 2 Observatoire de Paris, SYRTE/UMR-8630 CNRS, 75014 Paris, France e-mail: [email protected] Received 31 January 2013 / Accepted 18 April 2013 ABSTRACT Context. Thanks to various space missions and the progress of ground-based observational techniques, the knowledge of asteroids has considerably increased in the recent years. Aims. Due to this increasing database that accompanies this evolution, we compute for a set of 100 asteroids their rotational parame- ters: the moments of inertia along the principal axes of the object, the obliquity of the axis of rotation with respect to the orbital plane, the precession rates, and the nutation coefficients. Methods. We select 100 asteroids for which the parameters for the study are well-known from observations or space missions. For each asteroid, we determine the moments of inertia, assuming an ellipsoidal shape. We calculate their obliquity from their orbit (instead of the ecliptic) and the orientation of the spin-pole. Finally, we calculate the precession rates and the largest nutation compo- nents. The number of asteroids concerned leads to some statistical studies of the output. Results. We provide a table of rotational parameters for our set of asteroids. The table includes the obliquity, their axes ratio, their dynamical ellipticity Hd, and the scaling factor K. We compute the precession rate ψ˙ and the leading nutation coefficients Δψ and Δε. -
Surveying Potential Cruise Fly-By Opportunities for an Ice Giant Mission
EPSC Abstracts Vol. 14, EPSC2020-878, 2020 https://doi.org/10.5194/epsc2020-878 Europlanet Science Congress 2020 © Author(s) 2021. This work is distributed under the Creative Commons Attribution 4.0 License. Surveying potential cruise fly-by opportunities for an Ice Giant mission Marc Costa Sitjà1, Olivier Witasse2, and Alfredo Escalante López1 1Rhea for the European Space Agency, Villanueva de la Cañada, Spain ([email protected]) 2European Space Agency, Noordwijk, The Netherlands Marc Costa Sitjà1, Olivier Witasse2, Alfredo Escalante López1 1RHEA for European Sapce Agency,2European Space Agency We present a systematic approach to analyse rapidly fly-by opportunities for the cruise phase of a mission to an Ice Giant. Such flyby would provide a unique opportunities to characterise Jupiter Trojans, Centaurs, or Jupiter Family comets. A mission to an Ice Giant (Neptune and/or Uranus) will be among the ones examined by NASA's next Planetary Sciences and Astrobiology Decadal survey. ESA was exploring in 2018-2019 a potential collaboration to a NASA-led mission to an ice giant and has carried out a concurrent engineering design study [1] for possible European contributions. In this study, a dual launch in 2031 was contemplated; after a Jupiter swingby in late 2032, one orbiter would go to Uranus while the second one would reach Neptune. The long cruise of a mission to Uranus and or Neptune would provide an excellent opportunity scientific investigations like heliophysics science [2], [3], [4]. In addition, it could provide an unexpected chance to visit an unexplored small body. Examples of such flybys by missions to the outer solar system are well known. -
Search for Life on the Moons of Saturn
Search for Life on the Moons of Saturn Leonie Schunk Mikko Pöntinen Planetary exploration, Autumn 2017 University of Helsinki Lecturer: Tomas Kohout Course assistant: Juulia-Gabrielle Moreau Search for life on the moons of Saturn Table of Contents 1. Introduction 3 2. Parameters for a habitable environment 5 3. Life conditions on the moons 7 Enceladus 9 Dione 9 Titan 10 4. Evaluation of geological maps of the moons 11 Maps of Enceladus 11 Map of Dione 12 Maps of Titan 13 Map of Mimas 14 Map of Tethys 14 Map of Rhea 15 Map of Iapetus 15 5. Detecting life 16 6. Prospects of a successful mission to different moons 20 7. Mission options and instrumentation 21 8. Preliminary mission plan 23 9. Conclusions 24 References 25 2 1. Introduction In 1997 a spacecraft, including a probe from NASA (this was a flagship project from NASA) and a lander from ESA, was launched to study Saturn and its system. This Cassini-Huygens mission was the first one to enter its orbit and only the fourth one that was sent to visit the planet. It spent 13 years orbiting Saturn, after a transit which took around seven years with four gravity assists on Earth, Venus and Jupiter, and a flyby of asteroid 2685 Masursky. The mission ended in September 2017, when Cassini burned up in Saturn’s atmosphere. The Huygens lander was able to land on Saturn’s biggest moon Titan on January 14th 2005 with a parachute, which was very unique since it was the first time a landing on a moon other than our own was successful. -
Morphological Properties Determination of Main Belt Asteroids
MORPHOLOGICAL PROPERTIES DETERMINATION OF MAIN BELT ASTEROIDS by Guillermo Cerdán Hernandez Thesis submitted as a partial requirement to obtain the degree of MASTER OF SCIENCE IN SPACE SCIENCE AND TECHNOLOGY at Instituto Nacional de Astrofísica, Óptica y Electrónica April 2019 Tonantzintla, Puebla Supervised by: Dr. José Ramón Valdés Parra Dr. José Silviano Guichard Romero c INAOE 2019 The author hereby grants to INAOE permission to reproduce and distribute copies of this thesis document in whole or in part. Abstract We used lightcurves from the Asteroid Lightcurve Photometry Database (ALCDEF), observations made at Instituto Nacional de Astrofísica, Óptica y Electrónica (INAOE, México) Schmidt telescope, and Minor Planet Observer Lightcurve Inversion software (MPO LC Invert) to make the lightcurve inversion process, deriving shape, and pole orientation for the asteroids: (22) Kallipe, (287) Nepthys, (711) Marmulla, (1117) Reginita, (1318) Nerina, (1346) Gotha, (1492) Oppozler, (3028) Zhangguoxi, (3800) Karayusuf, (4713) Steel, and (5692) Shirao. Fueron usadas curvas de luz de la base de datos de la Asteroid Photometry Database (ALCDEF), observaciones hechas en el telescopio Schmidt del Instituto Nacional de Astrofísica, Óptica y Electrónica (INAOE, México) y el software del Minor Planet Observer Lightcurve Inversion (MPO LC Invert, para aplicar el proceso de inversión de cruvas de luz, obteniendo la forma y la orientación del polo para los asteroides: (22) Kallipe, (287) Nepthys, (711) Marmulla, (1117) Reginita, (1318) Nerina, (1346) Gotha, (1492) Oppozler, (3028) Zhangguoxi, (3800) Karayusuf, (4713) Steel y (5692) Shirao. Acknowledgments I thank CONACYT for granting the financial, intellectual capital, and infrastructure support to carry out this thesis work. Likewise, I thank all the people who have contributed in my life and who have allowed me to live this experience, people like: Dolores Hernandez Gonzalez, Juan Carlos Herrera Tavera, Jose Ramón Valdes Parra, Karem Contreras Aguilera, trench companions, and the teachers with vocations who have instructed me. -
Basics of Space Flight
A paper version of the http://www.jpl.nasa.gov/basics interactive online tutorial May 2001 Jet Propulsion Laboratory California Institute of Technology JPL D-20120 TMOD 890-289 Notes and disclaimers on this paper version: This is a printout of an Adobe Acrobat (.pdf) file that was created from an interactive website tutorial. As such, it is missing many of the online interac- tive features intended to help the reader understand and retain the informa- tion. Also, as a printed document, it contains many anomalies. Examples are n Inappropriate page breaks. n Blank areas where the HTML to .pdf translation was less than optimum. n No continuous page numbers in the document. n A repeat of the online navigation tools (chapter headings, etc.) at the end of each section. n Hyperlinked picture captions and notes inserted between continu- ous text pages. n Pages inserted from other web sites (e.g., spacecraft descriptions). Despite these oddities, demand has been high for a printable version of the tutorial, so here it is. Basics of Space Flight THE FEBRUARY 2001 UPDATE ● How do you get to another planet? ● Can gravity assist you? ● What is Universal Time? The people of Caltech's Jet Propulsion Laboratory (JPL) create EDITORIAL and manage NASA projects of exploration throughout our solar system and beyond. SECTION I This is a training module designed primarily to help JPL operations ENVIRONMENT people identify the range of concepts associated with deep space 1 The Solar System missions and grasp the relationships these concepts exhibit for space 2 Reference Systems flight. It also enjoys growing popularity among high school and 3 Gravity & Mechanics 4 Trajectories college students, as well as faculty and people everywhere who are 5 Planetary Orbits interested in interplanetary space flight.