Formation of the Solar System and Other Planetary Systems
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Jjmonl 1603.Pmd
alactic Observer GJohn J. McCarthy Observatory Volume 9, No. 3 March 2016 GRAIL - On the Trail of the Moon's Missing Mass GRAIL (Gravity Recovery and Interior Laboratory) was a NASA scientific mission in 2011/12 to map the surface of the moon and collect data on gravitational anomalies. The image here is an artist's impres- sion of the twin satellites (Ebb and Flow) orbiting in tandem above a gravitational image of the moon. See inside, page 4 for information on gravitational anomalies (mascons) or visit http://solarsystem. nasa.gov/grail. The John J. McCarthy Observatory Galactic Observer 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 SUNRISE AND SUNSET ...................................................... 13 MARE HUMBOLDTIANIUM AND THE NORTHEAST LIMB ......... 5 JUPITER AND ITS MOONS ................................................. 13 ONE YEAR IN SPACE ....................................................... 6 TRANSIT OF JUPITER'S RED SPOT .................................... -
Regn Lst 1948 to 2020.Xls
AMERICAN FUCHSIA SOCIETY REGISTERED FUCHSIAS, 1948 - 2020 CULTIVAR REG NO HYBRIDIZER YEAR FORM GROWTH Jardins de France 4439 Massé 2000 sgl up All Square 2335 Adams 1988 sgl up Beatrice Ellen 2336 Adams 1988 sgl up Cardiff Rose 2337 Adams 1988 sgl up/tr Glas Lyn 2338 Adams 1988 sgl up Purple Laddie 2339 Adams 1988 dbl up Velma 1522 Adams 1979 sgl up Windmill 4556 Adams 2001 dbl up Bo Bo 1587 Adkins 1980 dbl up Bonnie Sue 1550 Adkins 1980 dbl tr Dariway 1551 Adkins 1980 sgl up Delta Rae 1552 Adkins 1980 sgl tr Grinnell Bay 1553 Adkins 1980 sgl tr Joanne Lynn 1554 Adkins 1980 sdbl up Grandma Ellen 3066 Ainsworth 1993 sgl up Percy Ainsworth 3065 Ainsworth 1993 sgl tr Tufty Joe 3063 Ainsworth 1993 dbl tr Heidi Joy 2246 Akers/Laburnum 1987 dbl up Elaine Allen 1214 Allen 1974 sdbl up Susan Allen 1215 Allen 1974 sgl up Grandpa Jack 3789 Allso 1997 dbl up/tr Amazing Maisie 4632 Allsop 2001 s-dbl up/tr Amelia Rose 8018 Allsop 2012 sgl tr Arthur C. Boggis 4629 Allsop 2001 s-dbl up Beautiful Bobbie 3781 Allsop 1997 dbl tr Beloved Brian 5689 Allsop 2005 sgl up/tr Betty’s Buddies 8610 Allsop 2015 sgl up Captivating Kelly 3782 Allsop 1997 dbl tr Cheeky Chantelle 3783 Allsop 1997 dbl tr Cinque Port Liberty 4626 Allsop 2001 dbl up/tr Clara Agnes 5572 Allsop 2004 sgl up/tr Conner's Cascade 8019 Allsop 2012 sgl tr CutieKaren 4040 Allsop 1998 dbl tr Danielle’s Dream 4630 Allsop 2001 dbl tr Darling Danielle 3784 Allsop 1997 dbl tr Doodie Dane 3785 Allsop 1997 dbl gtr Dorothy Ann 4627 Allsop 2001 sgl tr Elaine's Gem 8020 Allsop 2012 sgl up Generous Jean 4813 -
Yrfthesis.Pdf
ABSTRACT Title of Dissertation PHYSICAL PROPERTIES OF COMETARY NUCLEI Yanga Rolando Fernandez Do ctor of Philosophy Dissertation directed by Professor Michael F AHearn Department of Astronomy I present results on the physical and thermal prop erties of six cometary nuclei This is a signicant increase in the numb er of nuclei for which physical information is available I have used imaging of the thermal continuum at midinfrared and radio wavelengths and of the scattered solar continuum at optical wavelengths to study the eective radius reectivity rotation state and temp erature of these ob jects Traditionally the nucleus has b een dicult to observe owing to an obscuring coma or extreme faintness I have taken advantage of new midinfrared array detectors to observe more comets than were p ossible b efore I have also codevelop ed a technique to separate the coma and nucleus from a comet image I develop ed a simple mo del of the thermal b ehavior of a cometary nucleus to help interpret the thermal ux measurements the mo del is an extension to the Standard Thermal Mo del for aster oids We have enough nuclei now to see the rst demarcations of the cometary region on an alb edodiameter plot I make a comparison of the cometary nuclei with outer Solar System small b o dies and nearEarth asteroids All of the cometary nuclei studied in this thesis are dark with geometric alb edos b elow and have eective diameters of around to km except for comet HaleBopp C O which is in the next order of magnitude higher I give an extensive discussion of the nuclear -
(2000) Forging Asteroid-Meteorite Relationships Through Reflectance
Forging Asteroid-Meteorite Relationships through Reflectance Spectroscopy by Thomas H. Burbine Jr. B.S. Physics Rensselaer Polytechnic Institute, 1988 M.S. Geology and Planetary Science University of Pittsburgh, 1991 SUBMITTED TO THE DEPARTMENT OF EARTH, ATMOSPHERIC, AND PLANETARY SCIENCES IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY IN PLANETARY SCIENCES AT THE MASSACHUSETTS INSTITUTE OF TECHNOLOGY FEBRUARY 2000 © 2000 Massachusetts Institute of Technology. All rights reserved. Signature of Author: Department of Earth, Atmospheric, and Planetary Sciences December 30, 1999 Certified by: Richard P. Binzel Professor of Earth, Atmospheric, and Planetary Sciences Thesis Supervisor Accepted by: Ronald G. Prinn MASSACHUSES INSTMUTE Professor of Earth, Atmospheric, and Planetary Sciences Department Head JA N 0 1 2000 ARCHIVES LIBRARIES I 3 Forging Asteroid-Meteorite Relationships through Reflectance Spectroscopy by Thomas H. Burbine Jr. Submitted to the Department of Earth, Atmospheric, and Planetary Sciences on December 30, 1999 in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy in Planetary Sciences ABSTRACT Near-infrared spectra (-0.90 to ~1.65 microns) were obtained for 196 main-belt and near-Earth asteroids to determine plausible meteorite parent bodies. These spectra, when coupled with previously obtained visible data, allow for a better determination of asteroid mineralogies. Over half of the observed objects have estimated diameters less than 20 k-m. Many important results were obtained concerning the compositional structure of the asteroid belt. A number of small objects near asteroid 4 Vesta were found to have near-infrared spectra similar to the eucrite and howardite meteorites, which are believed to be derived from Vesta. -
Optimal Flight to Near-Earth Asteroids with Using Electric Propulsion and Gravity Maneuvers
OPTIMAL FLIGHT TO NEAR-EARTH ASTEROIDS WITH USING ELECTRIC PROPULSION AND GRAVITY MANEUVERS A. V. Chernov Keldysh Institute of Applied Mathematics, Miusskaya Sq. 4, Moscow, 125047, Russia, E-mail: [email protected] ABSTRACT Optimal space flight to near-Earth asteroid for using low thrust and gravity assist maneuver near Mars or Venus is investigated in this paper. The main deflection asteroids from the Earth and prevention their possible collision is investigated. The deflection is attention is given a case of the ideal low thrust. Besides realized by means of impact-kinetic effect of the optimal trajectories with the constrained low trust spacecraft on the asteroid and changing the asteroid appropriate to electric engine SPT-140 and solar orbit. The effectiveness of this method for preventing batteries as energy sources are received in vicinity of the optimal trajectories for ideal thrust. asteroid-Earth collision is estimated by means of optimal space flights, which are found. The flight of spacecraft (SC) is realized by means of using electric 2. THE PROBLEM STATEMENT propulsion system. To increase effectiveness the optimal gravity maneuvers of spacecraft near Mars and At first the SC with mass M0 moves along an initial Venus are using. Criterion of the space flight circular near-Earth parking orbit with radius R0. The optimization is maximal deflection of the asteroid from geocentric motion is realized by means of high thrust the Earth at the moment of asteroid-Earth nearest engine with the gas exhaust velocity c1. At moment t1 approach. For determination of optimal trajectories the the SC is applied the velocity impulse ∆V and the SC is maximum Pontrjagin principle is used. -
1987Aj 93. . 738T the Astronomical Journal
738T . THE ASTRONOMICAL JOURNAL VOLUME 93, NUMBER 3 MARCH 1987 93. DISCOVERY OF M CLASS OBJECTS AMONG THE NEAR-EARTH ASTEROID POPULATION Edward F. TEDEScoa),b) Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 1987AJ Jonathan Gradie20 Planetary Geosciences Division, Hawaii Institute of Geophysics, University of Hawaii, Honolulu, Hawaii 96822 Received 10 September 1986; revised 17 November 1986 ABSTRACT Broadband colorimetry (0.36 to 0.85 ¡um), visual photometry, near-infrared (JHK) photometry, and 10 and 20 /urn radiometry of the near-Earth asteroids 1986 DA and 1986 EB were obtained during March and April 1986. Model radiometric visual geometric albedos of 0.14 + 0.02 and 0.19 + 0.02 and model radiometric diameters of 2.3 + 0.1 and 2.0 + 0.1 km, respectively, (on the IRAS asteroid ther- mal model system described by Lebofsky et al. 1986) were derived from the thermal infrared and visual fluxes. These albedos, together with the colorimetric and (for 1986 DA) near-infrared data, establish that both objects belong to the M taxonomic class, the first of this kind to be recognized among the near-Earth asteroid population. This discovery, together with previous detections of C and S class objects, establishes that all three of the most common main-belt asteroid classes are represented among this population. The similarity in the corrected distribution of taxonomic classes among the 38 Earth- approaching asteroids for which such classes exist is similar to those regions of the main belt between the 3:1 (2.50 AU) and 5:2 (2.82 AU) orbital resonances with Jupiter, suggesting that they have their origins among asteroids in the vicinity of these resonances. -
The Near-Earth Asteroid Rendezvous (NEAR-Shoemaker) Mission / Howard E
I-38738 NEAR BookCVR.Fin2 3/10/05 11:58 AM Page 1 d National Aeronautics and Space Administration Office of External Relations Low-CostLow-Cost History Division Washington, DC 20546 InnovationInnovation inin SpaceflightSpaceflight TheThe NearNear EarthEarth AsteroidAsteroid RendezvousRendezvous (NEAR)(NEAR) ShoemakerShoemaker MissionMission Monographs in Aerospace History No. 36 • SP-2005-4536 fld I-38738 NEAR BookCVR.Fin2 3/10/05 11:58 AM Page 2 Cover (from the top): The cover combines a closeup image of Eros, a photograph of the 1996 launch of the Near Earth Asteroid Rendezvous (NEAR) expedition, and a picture of the mission operations center taken during the second year of flight. NEAR operations manager Mark Holdridge stands behind the flight consoles. Asteroid and operations center photographs courtesy of Johns Hopkins University/Applied Physics Laboratory. Launch photograph courtesy of the National Aeronautics and Space Administration. (NASA KSC-96PC-308) Howard E. McCurdy Low-Cost Innovation in Spaceflight The Near Earth Asteroid Rendezvous (NEAR) Shoemaker Mission The NASA History Series Monographs in Aerospace History Number 36 NASA SP-2005-4536 National Aeronautics and Space Administration Office of External Relations History Division Washington, DC 2005 Library of Congress Cataloging-in-Publication Data McCurdy, Howard E. Low cost innovation in spaceflight : the Near-Earth Asteroid Rendezvous (NEAR-Shoemaker) Mission / Howard E. McCurdy. p. cm. — (Monographs in aerospace history ; no. 36) 1. Microspacecraft. 2. Eros (Asteroid) -
– Near-Earth Asteroid Mission Concept Study –
ASTEX – Near-Earth Asteroid Mission Concept Study – A. Nathues1, H. Boehnhardt1 , A. W. Harris2, W. Goetz1, C. Jentsch3, Z. Kachri4, S. Schaeff5, N. Schmitz2, F. Weischede6, and A. Wiegand5 1 MPI for Solar System Research, 37191 Katlenburg-Lindau, Germany 2 DLR, Institute for Planetary Research, 12489 Berlin, Germany 3 Astrium GmbH, 88039 Friedrichshafen, Germany 4 LSE Space AG, 82234 Oberpfaffenhofen, Germany 5 Astos Solutions, 78089 Unterkirnach, Germany 6 DLR GSOC, 82234 Weßling, Germany ASTEX Marco Polo Symposium, Paris 18.5.09, A. Nathues - 1 Primary Objectives of the ASTEX Study Identification of the required technologies for an in-situ mission to two near-Earth asteroids. ¾ Selection of realistic mission scenarios ¾ Definition of the strawman payload ¾ Analysis of the requirements and options for the spacecraft bus, the propulsion system, the lander system, and the launcher ASTEX ¾ Definition of the requirements for the mission’s operational ground segment Marco Polo Symposium, Paris 18.5.09, A. Nathues - 2 ASTEX Primary Mission Goals • The mission scenario foresees to visit two NEAs which have different mineralogical compositions: one “primitive'‘ object and one fragment of a differentiated asteroid. • The higher level goal is the provision of information and constraints on the formation and evolution history of our planetary system. • The immediate mission goals are the determination of: – Inner structure of the targets – Physical parameters (size, shape, mass, density, rotation period and spin vector orientation) – Geology, mineralogy, and chemistry ASTEX – Physical surface properties (thermal conductivity, roughness, strength) – Origin and collisional history of asteroids – Link between NEAs and meteorites Marco Polo Symposium, Paris 18.5.09, A. -
Manned Mission to NEO Study
National Aeronautics and Space Administration Manned Mission to NEO Study Jerry Condon, NASA/JSC/EG5 Jacob Williams, ESCG Elizabeth Davis, ESCG David Lee, NASA/JSC/EG5 Juan Senent, OSR Sept. 27, 2010 Run Methodology ΔVAD Patch conic assumptions. V∞EI ΔtAE Asteroid Earth departure epoch [1900 Cases]: Departure • Start: Jan 01, 2015 00:00:00 Earth Arrival Step: 5 days • ΔtS • End: Dec 31, 2040 00:00:00 Earth-Asteroid transfer time [72]: ΔVAA • Start: 30 days • Step: 5 days Asteroid Arrival • End: 360 days Asteroid stay time [6]: • Start: 7 days • Step 7 days • End: 42 days Asteroid-Earth transfer time [72]: • Start: 5 days Step: 5 days V∞ED • ΔtEA • End: 360 days 1900x72x6x72 = 59,097,600 cases per asteroid Earth Departure 5766 Asteroids 340,756,761,600 cases total. Run time of ~2 hrs on JSC cluster Pre-Decisional: For NASA Internal Use Only 2 Asteroid Cases JPL Small-Body Database Search Engine: http://ssd.jpl.nasa.gov/sbdb_query.cgi Export CSV file which is read by the program Input parameters: • Object group : NEOs • Object kind: Asteroids Damon Landau 9/1/2010: • Numbered state: All objects Assumed diameter > 50 m • Constraints: H (mag) ≤ 24.2 abs. vis. mag. < 24.2 • 5766 Asteroids in this set (as of 8-26-2010) - Note: without the H constraint, the total number is 7183. Output parameters: • SPK-ID • object fullname • Absolute magnitude: H (mag) • Rotation period: rot_per (h) • Keplerian elements - Epoch of osculation: epoch (MJD) - Semi-major axis: a (AU) - Eccentricity: e - Inclination: i (deg) Assuming these are in - -
UNIVERSIDADE FEDERAL DO RIO DE JANEIRO Instituto De Física
UNIVERSIDADE FEDERAL DO RIO DE JANEIRO Instituto de Física Programa de Pós-Graduação em Ensino de Física Mestrado Profissional em Ensino de Física Mestrado Nacional Profissional em Ensino de Física O ENSINO INVESTIGATIVO DO MOVIMENTO DE PEQUENOS CORPOS DO SISTEMA SOLAR A PARTIR DE RECURSOS DISPONÍVEIS NA INTERNET Gilberto Rubens de Oliveira Nobre Dissertação de Mestrado apresentada ao Programa de Pós-Graduação em Ensino de Física, Instituto de Física, da Universidade Federal do Rio de Janeiro, como parte dos requisitos necessários à obtenção do título de Mestre em Ensino de Física. Orientadora: Deise Miranda Vianna Rio de Janeiro Novembro de 2016 O ENSINO INVESTIGATIVO DO MOVIMENTO DE PEQUENOS CORPOS DO SISTEMA SOLAR A PARTIR DE RECURSOS DISPONÍVEIS NA INTERNET Gilberto Rubens de Oliveira Nobre Orientadora: Deise Miranda Vianna Dissertação de Mestrado submetida ao Programa de Pós-Graduação em Ensino de Física, Instituto de Física, da Universidade Federal do Rio de Janeiro - UFRJ, como parte dos requisitos necessários à obtenção do título de Mestre em Ensino de Física. Aprovada por: __________________________________________ Dra. Deise Miranda Vianna - UFRJ/IF (Presidente) __________________________________________ Dra. Anna Maria Pessoa de Carvalho - USP/FE __________________________________________ Dr. Ladário da Silva - UFF/ICEx __________________________________________ Dr. José Adolfo Snajdauf de Campos - UFRJ/OV Rio de Janeiro Novembro de 2016 ii FICHA CATALOGRÁFICA N754e Nobre, Gilberto Rubens de Oliveira. O ensino investigativo do movimento de pequenos corpos do Sistema Solar a partir de recursos disponíveis na internet / Gilberto Rubens de Oliveira Nobre. – Rio de Janeiro: UFRJ/IF, 2016. ix, 218 f. : il. ; 30 cm. Orientadora: Deise Miranda Vianna. Dissertação (mestrado) – UFRJ / Instituto de Física / Programa de Pós-Graduação em Ensino de Física, 2016. -
Instructions and Helpful Info
Target NEOs! Instructions and Helpful Info. (Modified and updated from the OSIRIS-REx Target Asteroids! website at https://www.asteroidmission.org) May 2021 Prerequisites for participation. • An interest in astronomy. • An interest in observing and providing data to the scientific community. • An interest in learning more about asteroids and near-Earth objects. • Appropriate observing equipment or access to equipment. • Membership in the Astronomical League through a member club or as an individual Member- at-Large. Request a registration form from the coordinators. • Complete the Target NEOs! registration form. • Periodically you will receive updated information about the program. Obtain instrumentation. The minimum instrumentation recommended to participate in this project is: • Telescope 8” or larger; • CCD/CMOS Camera, computer with internet connection; and • Data reduction software (available via Target NEOs!) If you have an appropriate telescope and camera, you will be able to observe asteroids on the Target NEOs! list. The asteroids that can be observed depend on the telescope’s aperture (diameter of the mirror or lens), light pollution, geographic location, and asteroid’s location in the sky on a given night. If you do not have a telescope, you can still participate in the program by obtaining access to observing equipment: • Team up and use a telescope owned by a friend, astronomy club, local college or planetarium observatory. • Use a commercial telescope service. • Are you a member of a local astronomy club? If not, we recommend it! Local astronomy clubs provide connections and opportunities for observations. You will meet friendly members who will be happy to help you. Check out the Astronomical League and NASA Night Sky Network to locate a club near you. -
The Minor Planet Bulletin, We Feel Safe in Al., 1989)
THE MINOR PLANET BULLETIN OF THE MINOR PLANETS SECTION OF THE BULLETIN ASSOCIATION OF LUNAR AND PLANETARY OBSERVERS VOLUME 43, NUMBER 3, A.D. 2016 JULY-SEPTEMBER 199. PHOTOMETRIC OBSERVATIONS OF ASTEROIDS star, and asteroid were determined by measuring a 5x5 pixel 3829 GUNMA, 6173 JIMWESTPHAL, AND sample centered on the asteroid or star. This corresponds to a 9.75 (41588) 2000 SC46 by 9.75 arcsec box centered upon the object. When possible, the same comparison star and check star were used on consecutive Kenneth Zeigler nights of observation. The coordinates of the asteroid were George West High School obtained from the online Lowell Asteroid Services (2016). To 1013 Houston Street compensate for the effect on the asteroid’s visual magnitude due to George West, TX 78022 USA ever changing distances from the Sun and Earth, Eq. 1 was used to [email protected] vertically align the photometric data points from different nights when constructing the composite lightcurve: Bryce Hanshaw 2 2 2 2 George West High School Δmag = –2.5 log((E2 /E1 ) (r2 /r1 )) (1) George West, TX USA where Δm is the magnitude correction between night 1 and 2, E1 (Received: 2016 April 5 Revised: 2016 April 7) and E2 are the Earth-asteroid distances on nights 1 and 2, and r1 and r2 are the Sun-asteroid distances on nights 1 and 2. CCD photometric observations of three main-belt 3829 Gunma was observed on 2016 March 3-5. Weather asteroids conducted from the George West ISD Mobile conditions on March 3 and 5 were not particularly favorable and so Observatory are described.