Physical Characterization of the Potentially-Hazardous High-Albedo Asteroid (33342) 1998 WT from Thermal-Infrared Observations Alan W
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Index Abulfeda crater chain (Moon), 97 Aphrodite Terra (Venus), 142, 143, 144, 145, 146 Acheron Fossae (Mars), 165 Apohele asteroids, 353–354 Achilles asteroids, 351 Apollinaris Patera (Mars), 168 achondrite meteorites, 360 Apollo asteroids, 346, 353, 354, 361, 371 Acidalia Planitia (Mars), 164 Apollo program, 86, 96, 97, 101, 102, 108–109, 110, 361 Adams, John Couch, 298 Apollo 8, 96 Adonis, 371 Apollo 11, 94, 110 Adrastea, 238, 241 Apollo 12, 96, 110 Aegaeon, 263 Apollo 14, 93, 110 Africa, 63, 73, 143 Apollo 15, 100, 103, 104, 110 Akatsuki spacecraft (see Venus Climate Orbiter) Apollo 16, 59, 96, 102, 103, 110 Akna Montes (Venus), 142 Apollo 17, 95, 99, 100, 102, 103, 110 Alabama, 62 Apollodorus crater (Mercury), 127 Alba Patera (Mars), 167 Apollo Lunar Surface Experiments Package (ALSEP), 110 Aldrin, Edwin (Buzz), 94 Apophis, 354, 355 Alexandria, 69 Appalachian mountains (Earth), 74, 270 Alfvén, Hannes, 35 Aqua, 56 Alfvén waves, 35–36, 43, 49 Arabia Terra (Mars), 177, 191, 200 Algeria, 358 arachnoids (see Venus) ALH 84001, 201, 204–205 Archimedes crater (Moon), 93, 106 Allan Hills, 109, 201 Arctic, 62, 67, 84, 186, 229 Allende meteorite, 359, 360 Arden Corona (Miranda), 291 Allen Telescope Array, 409 Arecibo Observatory, 114, 144, 341, 379, 380, 408, 409 Alpha Regio (Venus), 144, 148, 149 Ares Vallis (Mars), 179, 180, 199 Alphonsus crater (Moon), 99, 102 Argentina, 408 Alps (Moon), 93 Argyre Basin (Mars), 161, 162, 163, 166, 186 Amalthea, 236–237, 238, 239, 241 Ariadaeus Rille (Moon), 100, 102 Amazonis Planitia (Mars), 161 COPYRIGHTED -
Distribution and Orientation of Boulders on Asteroid 25143 Itokawa
Distribution and Orientation of Boulders on Asteroid 25143 Itokawa Sara Mazrouei-Seidani A Thesis submitted to the Faculty of Graduate Studies in Partial Fulfillment of the Requirements for the Degree of Master of Science Graduate Program in Earth and Space Science, York University, Toronto, Ontario September 2012 © Sara Mazrouei-Seidani 2012 Library and Archives Bibliotheque et Canada Archives Canada Published Heritage Direction du 1+1 Branch Patrimoine de I'edition 395 Wellington Street 395, rue Wellington Ottawa ON K1A0N4 Ottawa ON K1A 0N4 Canada Canada Your file Votre reference ISBN: 978-0-494-91769-5 Our file Notre reference ISBN: 978-0-494-91769-5 NOTICE: AVIS: The author has granted a non L'auteur a accorde une licence non exclusive exclusive license allowing Library and permettant a la Bibliotheque et Archives Archives Canada to reproduce, Canada de reproduire, publier, archiver, publish, archive, preserve, conserve, sauvegarder, conserver, transmettre au public communicate to the public by par telecommunication ou par I'lnternet, preter, telecommunication or on the Internet, distribuer et vendre des theses partout dans le loan, distrbute and sell theses monde, a des fins commerciales ou autres, sur worldwide, for commercial or non support microforme, papier, electronique et/ou commercial purposes, in microform, autres formats. paper, electronic and/or any other formats. The author retains copyright L'auteur conserve la propriete du droit d'auteur ownership and moral rights in this et des droits moraux qui protege cette these. Ni thesis. Neither the thesis nor la these ni des extraits substantiels de celle-ci substantial extracts from it may be ne doivent etre imprimes ou autrement printed or otherwise reproduced reproduits sans son autorisation. -
Robotic Asteroid Prospector
Robotic Asteroid Prospector Marc M. Cohen1 Marc M. Cohen Architect P.C. – Astrotecture™, Palo Alto, CA, USA 94306-3864 Warren W. James2 V Infinity Research LLC. – Altadena, CA, USA Kris Zacny,3 Philip Chu, Jack Craft Honeybee Robotics Spacecraft Mechanisms Corporation – Pasadena, CA, USA This paper presents the results from the nine-month, Phase 1 investigation for the Robotic Asteroid Prospector (RAP). This project investigated several aspects of developing an asteroid mining mission. It conceived a Space Infrastructure Framework that would create a demand for in space-produced resources. The resources identified as potentially feasible in the near-term were water and platinum group metals. The project’s mission design stages spacecraft from an Earth Moon Lagrange (EML) point and returns them to an EML. The spacecraft’s distinguishing design feature is its solar thermal propulsion system (STP) that provides two functions: propulsive thrust and process heat for mining and mineral processing. The preferred propellant is water since this would allow the spacecraft to refuel at an asteroid for its return voyage to Cis- Lunar space thus reducing the mass that must be launched from the EML point. The spacecraft will rendezvous with an asteroid at its pole, match rotation rate, and attach to begin mining operations. The team conducted an experiment in extracting and distilling water from frozen regolith simulant. Nomenclature C-Type = Carbonaceous Asteroid EML = Earth-Moon Lagrange Point ESL = Earth-Sun Lagrange Point IPV = Interplanetary Vehicle M-Type = Metallic Asteroid NEA = Near Earth Asteroid NEO = Near Earth Object PGM = Platinum Group Metal STP = Solar Thermal Propulsion S-Type = Stony Asteroid I. -
Near Earth Objects As Resources for Space Industrialization
Solar System Development Journal (2001) 1(1), 1-31 http://www.resonance-pub.com ISSN:1534-8016 NEAR EARTH OBJECTS AS RESOURCES FOR SPACE INDUSTRIALIZATION MARK SONTER Consultant, Asteroid Enterprises Pty Ltd, 28 Ian Bruce Crescent, Balgownie, New South Wales 2519, Australia [email protected] (Received 11 February 2001, and in final form 13 August 2001*) This paper reviews concepts for mining the Near-Earth Asteroids for supply of resources to future in-space industrial activities. It identifies Expectation Net Present Value as the appropriate measure for determining the technical and economic feasibility of a hypothetical asteroid mining venture, just as it is the appropriate measure for the feasibility of a proposed terrestrial mining venture. In turn, ENPV can obviously be used as a ‘design driver’ to sieve the alternative options, in selection of target, mission profile, mining and processing methods, propulsion for return trajectory, and earth-capture mechanism. 1. INTRODUCTION The Near Earth Asteroids are potential impact threats to Earth, but also a particularly accessible subset of them does provide potentially attractive targets for resources to support space industrialization. Robust technical and economic approaches to evaluation of the feasibility of proposed projects are necessary for assessment of such space mining ventures. This paper discusses the technical engineering and mission–planning choices and shows how the concept of probabilistic Net Present Value can be used to optimize these choices, and hence select between alternative asteroid mining mission designs. The generic mission reviewed envisages a lightweight remote (teleoperated) or semiautonomous miner, recovering products such as water or nickel-iron metal, from highly- accessible NEAs, and returning it to Low Earth Orbit (LEO), for sale and use in LEO, using solar power and some of the recovered mass as propellant. -
Spectroscopic Survey of X-Type Asteroids S
Spectroscopic Survey of X-type Asteroids S. Fornasier, B.E. Clark, E. Dotto To cite this version: S. Fornasier, B.E. Clark, E. Dotto. Spectroscopic Survey of X-type Asteroids. Icarus, Elsevier, 2011, 10.1016/j.icarus.2011.04.022. hal-00768793 HAL Id: hal-00768793 https://hal.archives-ouvertes.fr/hal-00768793 Submitted on 24 Dec 2012 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. Accepted Manuscript Spectroscopic Survey of X-type Asteroids S. Fornasier, B.E. Clark, E. Dotto PII: S0019-1035(11)00157-6 DOI: 10.1016/j.icarus.2011.04.022 Reference: YICAR 9799 To appear in: Icarus Received Date: 26 December 2010 Revised Date: 22 April 2011 Accepted Date: 26 April 2011 Please cite this article as: Fornasier, S., Clark, B.E., Dotto, E., Spectroscopic Survey of X-type Asteroids, Icarus (2011), doi: 10.1016/j.icarus.2011.04.022 This is a PDF file of an unedited manuscript that has been accepted for publication. As a service to our customers we are providing this early version of the manuscript. The manuscript will undergo copyediting, typesetting, and review of the resulting proof before it is published in its final form. -
Asteroid Observations at Low Phase Angles. IV. Average Parameters for the New H, G1, G2 Magnitude System Vasilij G
Planetary and Space Science ∎ (∎∎∎∎) ∎∎∎–∎∎∎ Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss Asteroid observations at low phase angles. IV. Average parameters for the new H, G1, G2 magnitude system Vasilij G. Shevchenko a,b,n, Irina N. Belskaya a, Karri Muinonen c,d, Antti Penttilä c, Yurij N. Krugly a, Feodor P. Velichko a, Vasilij G. Chiorny a, Ivan G. Slyusarev a,b, Ninel M. Gaftonyuk e, Igor A. Tereschenko a a Institute of Astronomy of Kharkiv Karazin National University, Sumska str. 35, Kharkiv 61022, Ukraine b Department of Astronomy and Space Informatics of Kharkiv Karazin National University, Svobody sqr. 4, Kharkiv 61022, Ukraine c Department of Physics, University of Helsinki, P.O. Box 64, FI-00014, Finland d Finnish Geospatial Research Institute, P.O. Box 15, Masala, FI-02431, Finland e Crimean Astrophysical Observatory, Crimea, Simeiz 98680, Ukraine article info abstract Article history: We present new observational data for selected main-belt asteroids of different compositional types. The Received 21 January 2015 detailed magnitude–phase dependences including small phase angles (o1°) were obtained for these Received in revised form asteroids, namely: (10) Hygiea (down to the phase angle of 0.3°, C-type), (176) Iduna (0.2°, G-type), (214) 6 September 2015 Aschera (0.2°, E-type), (218) Bianca (0.3°, S-type), (250) Bettina (0.3°, M-type), (419) Aurelia (0.1°, F-type), Accepted 19 November 2015 (596) Scheila (0.2°, D-type), (635) Vundtia (0.2°, B-type), (671) Carnegia (0.2°, P-type), (717) Wisibada (0.1°, T-type), (1021) Flammario (0.6°, B-type), and (1279) Uganda (0.5°, E-type). -
Radar Observations and a Physical Model of Asteroid 4660 Nereus, a Prime Space Mission Target ∗ Marina Brozovic A, ,Stevenj.Ostroa, Lance A.M
Icarus 201 (2009) 153–166 Contents lists available at ScienceDirect Icarus www.elsevier.com/locate/icarus Radar observations and a physical model of Asteroid 4660 Nereus, a prime space mission target ∗ Marina Brozovic a, ,StevenJ.Ostroa, Lance A.M. Benner a, Jon D. Giorgini a, Raymond F. Jurgens a,RandyRosea, Michael C. Nolan b,AliceA.Hineb, Christopher Magri c, Daniel J. Scheeres d, Jean-Luc Margot e a Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109-8099, USA b Arecibo Observatory, National Astronomy and Ionosphere Center, Box 995, Arecibo, PR 00613, USA c University of Maine at Farmington, Preble Hall, 173 High St., Farmington, ME 04938, USA d Aerospace Engineering Sciences, University of Colorado, Boulder, CO 80309-0429, USA e Department of Astronomy, Cornell University, 304 Space Sciences Bldg., Ithaca, NY 14853, USA article info abstract Article history: Near–Earth Asteroid 4660 Nereus has been identified as a potential spacecraft target since its 1982 Received 11 June 2008 discovery because of the low delta-V required for a spacecraft rendezvous. However, surprisingly little Revised 1 December 2008 is known about its physical characteristics. Here we report Arecibo (S-band, 2380-MHz, 13-cm) and Accepted 2 December 2008 Goldstone (X-band, 8560-MHz, 3.5-cm) radar observations of Nereus during its 2002 close approach. Available online 6 January 2009 Analysis of an extensive dataset of delay–Doppler images and continuous wave (CW) spectra yields a = ± = ± Keywords: model that resembles an ellipsoid with principal axis dimensions X 510 20 m, Y 330 20 m and +80 Radar observations Z = 241− m. -
Navigation Strategies for Primitive Solar System Body Rendezvous and Proximity Operations Kenneth M. Getzandanner
Navigation Strategies for Primitive Solar System Body Rendezvous and Proximity Operations Kenneth M. Getzandanner (1) (1) Navigation & Mission Design Branch, NASA Goddard Space Flight Center, Code 595, Greenbelt, Maryland 20771, (301) 286-1327, [email protected] Abstract: A wealth of scientific knowledge regarding the composition and evolution of the solar system can be gained through reconnaissance missions to primitive solar system bodies. This paper presents analysis of a baseline navigation strategy designed to address the unique challenges of primitive body navigation. Linear covariance and Monte Carlo error analysis was performed on a baseline navigation strategy using simulated data from a design reference mission (DRM). The objective of the DRM is to approach, rendezvous, and maintain a stable orbit about the near-Earth asteroid 4660 Nereus. The outlined navigation strategy and resulting analyses, however, are not necessarily limited to this specific target asteroid as they may be applicable to a diverse range of mission scenarios. The baseline navigation strategy included simulated data from Deep Space Network (DSN) radiometric tracking and optical image processing (OpNav). Results from the linear covariance and Monte Carlo analyses suggest the DRM navigation strategy is sufficient to approach and perform proximity operations in the vicinity of the target asteroid with meter-level accuracy. Keywords: Navigation, Asteroids, Rendezvous, Proximity Operations 1. Introduction Rendezvous missions to primitive solar system bodies (asteroids and comets) can provide a wealth of scientific information and insight into the composition and origins of the solar system because they remain largely unchanged. Precision navigation to approach, rendezvous, and perform proximity operations near a primitive solar system body presents unique challenges beyond traditional Earth-based and interplanetary missions. -
Nasa Technical Memorandum .1
NASA TECHNICAL MEMORANDUM NASA TM X-64677 COMETS AND ASTEROIDS: A Strategy for Exploration REPORT OF THE COMET AND ASTEROID MISSION STUDY PANEL May 1972 .1!vP -V (NASA-TE-X- 6 q767 ) COMETS AND ASTEROIDS: A RR EXPLORATION (NASA) May 1972 CSCL 03A NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Reproduced by ' NATIONAL "TECHINICAL INFORMATION: SERVICE US Depdrtmett ofCommerce :. Springfield VA 22151 TECHNICAL REPORT STANDARD TITLE PAGE · REPORT NO. 2. GOVERNMENT ACCESSION NO. 3, RECIPIENT'S CATALOG NO. NASA TM X-64677 . TITLE AND SUBTITLE 5. REPORT aE COMETS AND ASTEROIDS ___1_ A Strategy for Exploration 6. PERFORMING ORGANIZATION CODE AUTHOR(S) 8. PERFORMING ORGANIZATION REPORT # Comet and Asteroid Mission Study Panel PERFORMING ORGANIZATION NAME AND ADDRESS 10. WORK UNIT NO. 11. CONTRACT OR GRANT NO. 13. TYPE OF REPORT & PERIOD COVERED 2. SPONSORING AGENCY NAME AND ADDRESS National Aeronautics and Space Administration Technical Memorandum Washington, D. C. 20546 14. SPONSORING AGENCY CODE 5. SUPPLEMENTARY NOTES ABSTRACT Many of the asteroids probably formed near the orbits where they are found today. They accreted from gases and particles that represented the primordial solar system cloud at that location. Comets, in contrast to asteroids, probably formed far out in the solar system, and at very low temperatures; since they have retained their volatile components they are probably the most primordial matter that presently can be found anywhere in the solar system. Exploration and detailed study of comets and asteroids, therefore, should be a significant part of NASA's efforts to understand the solar system. A comet and asteroid program should consist of six major types of projects: ground-based observations;Earth-orbital observations; flybys; rendezvous; landings; and sample returns. -
E-Type Asteroid (2867) Steins: Flyby Target for Rosetta
A&A 473, L33–L36 (2007) Astronomy DOI: 10.1051/0004-6361:20078272 & c ESO 2007 Astrophysics Letter to the Editor E-type asteroid (2867) Steins: flyby target for Rosetta D. A. Nedelcu1,2, M. Birlan1, P. Vernazza3,R.P.Binzel1,4,, M. Fulchignoni3, and M. A. Barucci3 1 Institut de Mécanique Céleste et de Calcul des Éphémérides (IMCCE), Observatoire de Paris, 77 avenue Denfert-Rochereau, 75014 Paris Cedex, France e-mail: [Mirel.Birlan]@imcce.fr 2 Astronomical Institute of the Romanian Academy, 5 Cu¸titul de Argint, 040557 Bucharest, Romania e-mail: [email protected] 3 LESIA, Observatoire de Paris-Meudon, 5 place Jules Janssen, 92195 Meudon Cedex, France e-mail: [Antonella.Barucci;Pierre.Vernazza;Marcelo.Fulchignoni]@obspm.fr 4 Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge MA 02139, USA e-mail: [email protected] Received 13 July 2007 / Accepted 27 August 2007 ABSTRACT Aims. The mineralogy of the asteroid (2867) Steins was investigated in the framework of a ground-based science campaign dedicated to the future encounter with Rosetta spacecraft. Methods. Near-infrared (NIR) spectra of the asteroid in the 0.8−2.5 µm spectral range have been obtained with SpeX/IRTF in remote- observing mode from Meudon, France, and Cambridge, MA, in December 2006 and in January and March 2007. A spectrum with a combined wavelength coverage from 0.4 to 2.5 µm was constructed using previously obtained visible data. To constrain the possible composition of the surface, we constructed a simple mixing model using a linear (areal) mix of three components obtained from the RELAB database. -
Near Mission Design
D. W. DUNHAM, J. V. MCADAMS, AND R. W. FARQUHAR NEAR MISSION DESIGN NEAR Mission Design David W. Dunham, James V. McAdams, and Robert W. Farquhar The Near Earth Asteroid Rendezvous (NEAR) spacecraft took 4 years from launch until it became the first spacecraft to orbit an asteroid in February 2000. A month later, the spacecraft was re-christened NEAR Shoemaker to honor the late Eugene Shoemaker. To save launch costs, the mission used a special 2-year-period trajectory with an Earth gravity assist. On the way, the spacecraft imaged the asteroid 253 Mathilde. On 20 Decem- ber 1998, NEAR’s large engine misfired, failing to brake it for entry into orbit about 433 Eros. Another attempt 2 weeks later succeeded, but the spacecraft was almost a million kilometers away and took over a year to reach the asteroid. The mission was recovered thanks to a generous fuel supply and robust contingency planning. The implementation of the spacecraft’s daring orbital maneuvers is described, including those used to land on Eros’ surface in February 2001. INTRODUCTION Rendezvous missions to near-Earth asteroids, includ- Nereus. Unfortunately, Eros’ orbit is inclined 11° to ing one to (433) Eros, were proposed as early as 1963 the ecliptic (Earth’s orbit plane), requiring, for direct but these were relatively expensive missions costing transfers, high declination of launch asymptotes and half a billion dollars or more.1–4 With the Apollo pro- launch energies that are too high for a reasonably sized gram and demands for planetary exploration, this kind spacecraft with the Discovery-baselined Delta-class of funding was not available for an asteroid mission. -
Opposition Optical Phenomena in Planetary Astrophysics: Observational Results
Opposition optical phenomena in planetary astrophysics: observational results Vera K. Rosenbush1* and Michael I. Mishchenko2 1 Main Astronomical Observatory of the National Academy of Sciences of Ukraine, 27 Akademika Zabolotnoho St., 03680 Kyiv, Ukraine 2 NASA Goddard Institute for Space Studies, 2880 Broadway, New York, NY 10025, USA Abstract. The photometric phenomenon in the form of a nonlinear increase of brightness at small phase angles and a negative branch of polarization are typical of the majority of Solar System bodies. In addition, some high-albedo objects re- veal a backscattering polarization feature in the form of a spike-like negative- polarization minimum called the polarization opposition effect. These optical phe- nomena are important tests of our theoretical descriptions of light scattering by re- golith planetary surfaces. In this chapter we review the recent progress in the study of optical opposition phenomena in planetary astrophysics. We primarily focus on the results of polarimetric observations of asteroids, the Galilean satellites of Jupi- ter, the Saturnian satellite Iapetus, Centaurs, and trans-Neptunian objects at back- scattering geometries including phase angles approaching zero. Keywords: polarimetry, opposition effects, asteroids, satellites, Centaurs, trans-Neptunian objects 1. Introduction Polarimetry and photometry are especially sensitive diagnostic tools helping to infer the physical properties of bodies whose observational characteristics are governed by small scatterers, e.g., dust and regolith grains. It is these methods that have provided convincing indications of the presence of regolith on planetary sur- faces long before the advent of space missions. Measurements of the intensity and polarization of scattered light as functions of the phase angle and wavelength have been used to gain an improved understanding of the microphysical properties of the surfaces of many Solar System bodies.