The Design Reference Asteroid for the OSIRIS-Rex Mission Target (101955) Bennu

Total Page:16

File Type:pdf, Size:1020Kb

The Design Reference Asteroid for the OSIRIS-Rex Mission Target (101955) Bennu The Design Reference Asteroid for the OSIRIS-REx Mission Target (101955) Bennu An OSIRIS-REx DOCUMENT 2014-April-14 Carl W. Hergenrother1, Maria Antonietta Barucci2, Olivier Barnouin3, Beau Bierhaus4, Richard P. Binzel5, William F. Bottke6, Steve Chesley7, Ben C. Clark4, Beth E. Clark8, Ed Cloutis9, Christian Drouet d’Aubigny1, Marco Delbo10, Josh Emery11, Bob Gaskell12, Ellen Howell13, Lindsay Keller14, Michael Kelley15, John Marshall16, Patrick Michel10, Michael Nolan13, Bashar Rizk1, Dan Scheeres17, Driss Takir8, David D. Vokrouhlický18, Ed Beshore1, Dante S. Lauretta1 E-mail contact: [email protected] 1Lunar and Planetary Laboratory, University of Arizona, Tucson, Arizona 2LESIA-Observatoire de Paris, CNRS, Univ. Paris-Diderot, Meudon, France 3Applied Physics Laboratory, John Hopkins University, Laurel, Maryland 4Space Systems Company, Lockheed Martin, Denver, Colorado 5Dept. of Earth, Atmospheric and Planetary Sciences, Massachusetts Institute of Technology, Cambridge, Massachusetts 6Southwest Research Institute, Boulder, Colorado 7Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 8Dept. of Physics, Ithaca College, Ithaca, New York 9Dept. of Geography, University of Winnipeg, Winnipeg, Canada 10Laboratoire Lagrange, UNS-CNRS, Observatoire de la Cote d'Azur, Nice, France 11Earth and Planetary Science Dept., University of Tennessee, Knoxville, Tennessee 12Planetary Science Institute, Tucson, Arizona 13Arecibo Observatory, Arecibo, Puerto Rico 14NASA Johnson Space Center, Houston, Texas 15Dept. of Astronomy, University of Maryland, College Park, Maryland 16SETI Institute, Mountain View, California 17Dept. of Aerospace Engineering Sciences, University of Colorado-Boulder, Boulder, Colorado 18Astronomical Institute, Charles University, Prague, Czech Republic Table of Contents I. Background on Bennu .................................................................................................... 5 II. Design Reference Asteroid ............................................................................................ 7 1 Orbital Properties ................................................................................................................... 8 1.1 Orbital Elements .............................................................................................................. 8 1.1.1 Reference Frame ...................................................................................................................... 10 1.1.2 Epoch Date (JD/ET) ................................................................................................................. 10 1.1.3 Epoch Date (Calendar Date/ET) ................................................................................................. 10 1.1.4 Semi-major Axis ...................................................................................................................... 11 1.1.5 Perihelion ................................................................................................................................ 11 1.1.6 Aphelion .................................................................................................................................. 11 1.1.7 Eccentricity .............................................................................................................................. 11 1.1.8 Inclination ............................................................................................................................... 11 1.1.9 Longitude of Ascending Node ................................................................................................... 11 1.1.10 Argument of Perihelion ........................................................................................................... 12 1.1.11 Mean Anomaly ....................................................................................................................... 12 1.1.12 Time of Perihelion (JD/ET) ..................................................................................................... 12 1.1.13 Time of Perihelion (Calendar Date/ET) ..................................................................................... 12 1.1.14 Orbital Period ......................................................................................................................... 12 1.1.15 Minimum Orbit Intercept Distance (MOID) .............................................................................. 13 1.2 Ephemerides ................................................................................................................. 13 1.2.1 Ephemerides ............................................................................................................................ 13 1.3 Positional Uncertainties ................................................................................................. 13 1.3.1 Positional Uncertainty Epoch (Ephemeris Time) ......................................................................... 13 1.3.2 Positional Uncertainty Epoch (Julian Date) ................................................................................. 13 1.3.3 Radial Position Uncertainty ....................................................................................................... 14 1.3.4 Transverse Position Uncertainty ................................................................................................. 14 1.3.5 Normal Position Uncertainty ..................................................................................................... 14 1.3.6 Radial Velocity Uncertainty ...................................................................................................... 14 1.3.7 Transverse Velocity Uncertainty ................................................................................................ 14 1.3.8 Normal Velocity Uncertainty ..................................................................................................... 15 1.4 Yarkovsky Properties ..................................................................................................... 15 1.4.1 Semi-major Axis Drift Rate ....................................................................................................... 15 1.4.2 Transverse Non-gravitational Acceleration Parameter .................................................................. 15 2 Bulk Properties ..................................................................................................................... 16 2.1 Size ................................................................................................................................ 20 2.1.1 Mean Diameter ........................................................................................................................ 20 2.1.2 Polar Dimension ....................................................................................................................... 20 2.1.3 Equatorial Dimensions .............................................................................................................. 20 2.1.4 Dynamically Equivalent Equal Volume Ellipsoid (DEEVE) Dimensions ....................................... 20 2.1.5 Volume ................................................................................................................................... 20 2.1.6 Surface Area ............................................................................................................................ 21 2.1.7 Projected Area at Equatorial Viewing Aspect .............................................................................. 21 2.2 Mass and Density .......................................................................................................... 21 2.2.1 Bulk Density ............................................................................................................................ 21 2.2.2 Mass ....................................................................................................................................... 21 2.2.3 Gravitational Parameter ............................................................................................................ 22 2.2.4 Area-to-Mass Ratio .................................................................................................................. 22 2.3 Global Models ................................................................................................................ 22 2.3.1 Global Shape Model ................................................................................................................. 22 2.3.2 Global Gravity Field Model ....................................................................................................... 22 2.3.3 Global Surface Slope Distribution Model .................................................................................... 23 2 2.3.4 Global (Tangent/Normal/Total) Surface Acceleration Model ........................................................ 23 2.3.5 Global Surface Tilt Model ......................................................................................................... 23 2.3.6 Global Surface Escape Velocity Model ....................................................................................... 23 3 Rotational Properties ............................................................................................................ 24 3.1 Rotation State ................................................................................................................ 24 3.1.1
Recommended publications
  • BENNU from OSIRIS-Rex APPROACH and PRELIMINARY SURVEY OBSERVATIONS
    50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 1956.pdf VNIR AND TIR SPECTRAL CHARACTERISTICS OF (101955) BENNU FROM OSIRIS-REx APPROACH AND PRELIMINARY SURVEY OBSERVATIONS. V. E. Hamilton1, A. A. Simon2, P. R. Christensen3, D. C. Reuter2, D. N. Della Giustina4, J. P. Emery5, R. D. Hanna6, E. Howell4, H. H. Kaplan1, B. E. Clark7, B. Rizk4, D. S. Lauretta4, and the OSIRIS-REx Team, 1Southwest Research Institute, 1050 Walnut St. #300, Boulder, CO 80302 ([email protected]), 2NASA Goddard Space Flight Center, Greenbelt, MD, 3School of Earth & Space Ex- ploration, Arizona State University, Tempe, AZ 85287, 4Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ 85721, 5Dept. Earth & Planetary Science, University of Tennessee, Knoxville, TN 37996, 6University of Texas, Austin, TX, 78712, 7Dept. Physics & Astronomy, Ithaca College, Ithaca, NY 14850. Introduction: Visible to near infrared (VNIR) and generation and application of a photometric model, thermal infrared (TIR) spectrometers onboard the Ori- production of bolometric Bond albedo, reflectance gins, Spectral Interpretation, Resource Identification, factor spectra, and the calculation of spectral indices. Security–Regolith Explorer (OSIRIS-REx) spacecraft For OTES, this includes deriving emissivity spectra have revealed evidence of hydrated phases across the and temperature information with emissivity being an surface of asteroid (101955) Bennu. Here we describe input into a linear least squares mixing model and a spectral features identified
    [Show full text]
  • Ice& Stone 2020
    Ice & Stone 2020 WEEK 34: AUGUST 16-22 Presented by The Earthrise Institute # 34 Authored by Alan Hale This week in history AUGUST 16 17 18 19 20 21 22 AUGUST 16, 1898: DeLisle Stewart at Harvard College Observatory’s Boyden Station in Arequipa, Peru, takes photographs on which Saturn’s outer moon Phoebe is discovered, although the images of Phoebe were not noticed until the following March by William Pickering. Phoebe was the first planetary moon to be discovered via photography, and it and other small planetary moons are discussed in last week’s “Special Topics” presentation. AUGUST 16, 2009: A team of scientists led by Jamie Elsila of the Goddard Space Flight Center in Maryland announces that they have detected the presence of the amino acid glycine in coma samples of Comet 81P/ Wild 2 that were returned to Earth by the Stardust mission 3½ years earlier. Glycine is utilized by life here on Earth, and the presence of it and other organic substances in the solar system’s “small bodies” is discussed in this week’s “Special Topics” presentation. AUGUST 16 17 18 19 20 21 22 AUGUST 17, 1877: Asaph Hall at the U.S. Naval Observatory in Washington, D.C. discovers Mars’ larger, inner moon, Phobos. Mars’ two moons, and the various small moons of the outer planets, are the subject of last week’s “Special Topics” presentation. AUGUST 17, 1989: In its monthly batch of Minor Planet Circulars (MPCs), the IAU’s Minor Planet Center issues MPC 14938, which formally numbers asteroid (4151), later named “Alanhale.” I have used this asteroid as an illustrative example throughout “Ice and Stone 2020” “Special Topics” presentations.
    [Show full text]
  • Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object
    Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object by Nathan C. Shupe B.A., Swarthmore College, 2005 A thesis submitted to the Faculty of the Graduate School of the University of Colorado in partial fulfillment of the requirements for the degree of Master of Science Department of Aerospace Engineering Sciences 2010 This thesis entitled: Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object written by Nathan C. Shupe has been approved for the Department of Aerospace Engineering Sciences Daniel Scheeres Prof. George Born Assoc. Prof. Hanspeter Schaub Date The final copy of this thesis has been examined by the signatories, and we find that both the content and the form meet acceptable presentation standards of scholarly work in the above mentioned discipline. iii Shupe, Nathan C. (M.S., Aerospace Engineering Sciences) Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object Thesis directed by Prof. Daniel Scheeres Based on the recommendations of the Augustine Commission, President Obama has pro- posed a vision for U.S. human spaceflight in the post-Shuttle era which includes a manned mission to a Near-Earth Object (NEO). A 2006-2007 study commissioned by the Constellation Program Advanced Projects Office investigated the feasibility of sending a crewed Orion spacecraft to a NEO using different combinations of elements from the latest launch system architecture at that time. The study found a number of suitable mission targets in the database of known NEOs, and pre- dicted that the number of candidate NEOs will continue to increase as more advanced observatories come online and execute more detailed surveys of the NEO population.
    [Show full text]
  • Bennu: Implications for Aqueous Alteration History
    RESEARCH ARTICLES Cite as: H. H. Kaplan et al., Science 10.1126/science.abc3557 (2020). Bright carbonate veins on asteroid (101955) Bennu: Implications for aqueous alteration history H. H. Kaplan1,2*, D. S. Lauretta3, A. A. Simon1, V. E. Hamilton2, D. N. DellaGiustina3, D. R. Golish3, D. C. Reuter1, C. A. Bennett3, K. N. Burke3, H. Campins4, H. C. Connolly Jr. 5,3, J. P. Dworkin1, J. P. Emery6, D. P. Glavin1, T. D. Glotch7, R. Hanna8, K. Ishimaru3, E. R. Jawin9, T. J. McCoy9, N. Porter3, S. A. Sandford10, S. Ferrone11, B. E. Clark11, J.-Y. Li12, X.-D. Zou12, M. G. Daly13, O. S. Barnouin14, J. A. Seabrook13, H. L. Enos3 1NASA Goddard Space Flight Center, Greenbelt, MD, USA. 2Southwest Research Institute, Boulder, CO, USA. 3Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ, USA. 4Department of Physics, University of Central Florida, Orlando, FL, USA. 5Department of Geology, School of Earth and Environment, Rowan University, Glassboro, NJ, USA. 6Department of Astronomy and Planetary Sciences, Northern Arizona University, Flagstaff, AZ, USA. 7Department of Geosciences, Stony Brook University, Stony Brook, NY, USA. 8Jackson School of Geosciences, University of Texas, Austin, TX, USA. 9Smithsonian Institution National Museum of Natural History, Washington, DC, USA. 10NASA Ames Research Center, Mountain View, CA, USA. 11Department of Physics and Astronomy, Ithaca College, Ithaca, NY, USA. 12Planetary Science Institute, Tucson, AZ, Downloaded from USA. 13Centre for Research in Earth and Space Science, York University, Toronto, Ontario, Canada. 14John Hopkins University Applied Physics Laboratory, Laurel, MD, USA. *Corresponding author. E-mail: Email: [email protected] The composition of asteroids and their connection to meteorites provide insight into geologic processes that occurred in the early Solar System.
    [Show full text]
  • (101955) Bennu from OSIRIS-Rex Imaging and Thermal Analysis
    ARTICLES https://doi.org/10.1038/s41550-019-0731-1 Properties of rubble-pile asteroid (101955) Bennu from OSIRIS-REx imaging and thermal analysis D. N. DellaGiustina 1,26*, J. P. Emery 2,26*, D. R. Golish1, B. Rozitis3, C. A. Bennett1, K. N. Burke 1, R.-L. Ballouz 1, K. J. Becker 1, P. R. Christensen4, C. Y. Drouet d’Aubigny1, V. E. Hamilton 5, D. C. Reuter6, B. Rizk 1, A. A. Simon6, E. Asphaug1, J. L. Bandfield 7, O. S. Barnouin 8, M. A. Barucci 9, E. B. Bierhaus10, R. P. Binzel11, W. F. Bottke5, N. E. Bowles12, H. Campins13, B. C. Clark7, B. E. Clark14, H. C. Connolly Jr. 15, M. G. Daly 16, J. de Leon 17, M. Delbo’18, J. D. P. Deshapriya9, C. M. Elder19, S. Fornasier9, C. W. Hergenrother1, E. S. Howell1, E. R. Jawin20, H. H. Kaplan5, T. R. Kareta 1, L. Le Corre 21, J.-Y. Li21, J. Licandro17, L. F. Lim6, P. Michel 18, J. Molaro21, M. C. Nolan 1, M. Pajola 22, M. Popescu 17, J. L. Rizos Garcia 17, A. Ryan18, S. R. Schwartz 1, N. Shultz1, M. A. Siegler21, P. H. Smith1, E. Tatsumi23, C. A. Thomas24, K. J. Walsh 5, C. W. V. Wolner1, X.-D. Zou21, D. S. Lauretta 1 and The OSIRIS-REx Team25 Establishing the abundance and physical properties of regolith and boulders on asteroids is crucial for understanding the for- mation and degradation mechanisms at work on their surfaces. Using images and thermal data from NASA’s Origins, Spectral Interpretation, Resource Identification, and Security-Regolith Explorer (OSIRIS-REx) spacecraft, we show that asteroid (101955) Bennu’s surface is globally rough, dense with boulders, and low in albedo.
    [Show full text]
  • Untangling the Formation and Liberation of Water in the Lunar Regolith
    Untangling the formation and liberation of water in the lunar regolith Cheng Zhua,b,1, Parker B. Crandalla,b,1, Jeffrey J. Gillis-Davisc,2, Hope A. Ishiic, John P. Bradleyc, Laura M. Corleyc, and Ralf I. Kaisera,b,2 aDepartment of Chemistry, University of Hawai‘iatManoa, Honolulu, HI 96822; bW. M. Keck Laboratory in Astrochemistry, University of Hawai‘iatManoa, Honolulu, HI 96822; and cHawai‘i Institute of Geophysics and Planetology, University of Hawai‘iatManoa, Honolulu, HI 96822 Edited by Mark H. Thiemens, University of California at San Diego, La Jolla, CA, and approved April 24, 2019 (received for review November 15, 2018) −8 −6 The source of water (H2O) and hydroxyl radicals (OH), identified between 10 and 10 torr observed either an ν(O−H) stretching − − on the lunar surface, represents a fundamental, unsolved puzzle. mode in the 2.70 μm (3,700 cm 1) to 3.33 μm (3,000 cm 1) region The interaction of solar-wind protons with silicates and oxides has exploiting infrared spectroscopy (7, 25, 26) or OH/H2Osignature been proposed as a key mechanism, but laboratory experiments using secondary-ion mass spectrometry (27) and valence electron yield conflicting results that suggest that proton implantation energy loss spectroscopy (VEEL) (28). However, contradictory alone is insufficient to generate and liberate water. Here, we dem- studies yielded no evidence of H2O/OH in proton-bombarded onstrate in laboratory simulation experiments combined with minerals in experiments performed under ultrahigh vacuum − − imaging studies that water can be efficiently generated and re- (UHV) (10 10 to 10 9 torr) (29).
    [Show full text]
  • Non-Principal Axis Rotation (Tumbling) Asteroids
    NON-PRINCIPAL AXIS ROTATION (TUMBLING) ASTEROIDS Asteroid PAR Per1 Amp1 Per2 Amp2 Reference 244 Sita T0 129.51 0.82 0 129.51 0.82 Brinsfield, 09 253 Mathilde T 417.7 0.50 –3 417.7 0.45 250. Mottola, 95 –3 418. 0.5 250. Pravec, 05 288 Glauke T 1170. 0.9 –1 1200. 0.9 Harris, 99 0 Pravec, 14 –2 1170. 0.37 740. Pilcher, 15 299∗ Thora T– 272.9 0.50 0 274. 0.39 Pilcher, 14 +2 272.9 0.47 Pilcher, 17 319∗ Leona T 430. 0.5 –2 430. 0.5 1084. Pilcher, 17 341∗ California T 318. 0.92 –2 318. 0.9 250. Pilcher, 17 –2 317.0 0.54 Polakis, 17 –1 317.0 0.92 Polakis, 17 408 Fama T0 202.1 0.58 0 202.1 0.58 Stephens, 08 470 Kilia T0 290. 0.26 0 290. 0.26 Stephens, 09 0 Stephens, 09 496∗ Gryphia T 1072. 1.25 –2 1072. 1.25 Pilcher, 17 571 Dulcinea T 126.3 0.50 –2 126.3 0.50 Stephens, 11 630 Euphemia T0 350. 0.45 0 350. 0.45 Warner, 11 703∗ No¨emi T? 200. 0.78 –1 201.7 0.78 Noschese, 17 0 115.108 0.28 Sada, 17 –2 200. 0.62 Franco, 17 707 Ste¨ına T0 414. 1.00 0 Pravec, 14 763∗ Cupido T 151.5 0.45 –1 151.1 0.24 Polakis, 18 –2 151.5 0.45 101. Pilcher, 18 823 Sisigambis T0 146.
    [Show full text]
  • Deep Impact As a World Observatory Event Held in Brussels, Belgium, 7–10 August 2006
    Other Astronomical News Report on the Workshop on Deep Impact as a World Observatory Event held in Brussels, Belgium, 7–10 August 2006 Hans Ulrich Käufl1 One of the spectacular deconvolved images from the Christiaan Sterken2 Deep Impact Spacecraft High Resolution Imager shown in the conference (courtesy Mike A’Hearn and the Deep Impact Team). This is a colour composite of an infrared, a green and a violet filter forced to av- 1 ESO erage grey. Note the blueish areas on the surface 2 Vrije Universiteit Brussel, Belgium close to the crater-like structure. Those were entirely unexpected. It is highly interesting to find out if those structures can be correlated with the jets which were meticulously monitored from ground-based ob- In the context of NASA’s Deep Impact servers worldwide. This aspect in the picture – en- space mission, Comet 9P/Tempel1 tirely unrelated to the impact plume – illustrates very well how comet research, apart from the impact has been at the focus of an unprece- experiment, will profit from the synergy of spacecraft dented worldwide long-term multi- data and the unprecedented worldwide coordinated wavelength observation campaign. The observing campaign. comet has been studied through its perihelion passage by various spacecraft including the Deep Impact mission it- self, HST, Spitzer, Rosetta, XMM and all To make full use of the global data set, a To inspire new ideas, it was very helpful major ground-based observatories in workshop bringing together observers and interesting to have Roberta Olson basically all wavelength bands used in across the electromagnetic spectrum and from the New York Historical Society, astronomy, i.e.
    [Show full text]
  • Size of Particles Ejected from an Artificial Impact Crater on Asteroid
    A&A 647, A43 (2021) Astronomy https://doi.org/10.1051/0004-6361/202039777 & © K. Wada et al. 2021 Astrophysics Size of particles ejected from an artificial impact crater on asteroid 162173 Ryugu K. Wada1, K. Ishibashi1, H. Kimura1, M. Arakawa2, H. Sawada3, K. Ogawa2,4, K. Shirai2, R. Honda5, Y. Iijima3, T. Kadono6, N. Sakatani7, Y. Mimasu3, T. Toda3, Y. Shimaki3, S. Nakazawa3, H. Hayakawa3, T. Saiki3, Y. Takagi8, H. Imamura3, C. Okamoto2, M. Hayakawa3, N. Hirata9, and H. Yano3 1 Planetary Exploration Research Center, Chiba Institute of Technology, Narashino 275-0016, Japan e-mail: [email protected] 2 Department of Planetology, Kobe University, Kobe 657-8501, Japan 3 Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan 4 JAXA Space Exploration Center, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan 5 Department of Science and Technology, Kochi University, Kochi 780-8520, Japan 6 Department of Basic Sciences, University of Occupational and Environmental Health, Kitakyusyu 807-8555, Japan 7 Department of Physics, Rikkyo University, Tokyo 171-8501, Japan 8 Aichi Toho University, Nagoya 465-8515, Japan 9 School of Computer Science and Engineering, The University of Aizu, Aizu-Wakamatsu 965-8580, Japan Received 28 October 2020 / Accepted 26 January 2021 ABSTRACT A projectile accelerated by the Hayabusa2 Small Carry-on Impactor successfully produced an artificial impact crater with a final apparent diameter of 14:5 0:8 m on the surface of the near-Earth asteroid 162173 Ryugu on April 5, 2019. At the time of cratering, Deployable Camera 3 took± clear time-lapse images of the ejecta curtain, an assemblage of ejected particles forming a curtain-like structure emerging from the crater.
    [Show full text]
  • CURRICULUM VITAE, ALAN W. HARRIS Personal: Born
    CURRICULUM VITAE, ALAN W. HARRIS Personal: Born: August 3, 1944, Portland, OR Married: August 22, 1970, Rose Marie Children: W. Donald (b. 1974), David (b. 1976), Catherine (b 1981) Education: B.S. (1966) Caltech, Geophysics M.S. (1967) UCLA, Earth and Space Science PhD. (1975) UCLA, Earth and Space Science Dissertation: Dynamical Studies of Satellite Origin. Advisor: W.M. Kaula Employment: 1966-1967 Graduate Research Assistant, UCLA 1968-1970 Member of Tech. Staff, Space Division Rockwell International 1970-1971 Physics instructor, Santa Monica College 1970-1973 Physics Teacher, Immaculate Heart High School, Hollywood, CA 1973-1975 Graduate Research Assistant, UCLA 1974-1991 Member of Technical Staff, Jet Propulsion Laboratory 1991-1998 Senior Member of Technical Staff, Jet Propulsion Laboratory 1998-2002 Senior Research Scientist, Jet Propulsion Laboratory 2002-present Senior Research Scientist, Space Science Institute Appointments: 1976 Member of Faculty of NATO Advanced Study Institute on Origin of the Solar System, Newcastle upon Tyne 1977-1978 Guest Investigator, Hale Observatories 1978 Visiting Assoc. Prof. of Physics, University of Calif. at Santa Barbara 1978-1980 Executive Committee, Division on Dynamical Astronomy of AAS 1979 Visiting Assoc. Prof. of Earth and Space Science, UCLA 1980 Guest Investigator, Hale Observatories 1983-1984 Guest Investigator, Lowell Observatory 1983-1985 Lunar and Planetary Review Panel (NASA) 1983-1992 Supervisor, Earth and Planetary Physics Group, JPL 1984 Science W.G. for Voyager II Uranus/Neptune Encounters (JPL/NASA) 1984-present Advisor of students in Caltech Summer Undergraduate Research Fellowship Program 1984-1985 ESA/NASA Science Advisory Group for Primitive Bodies Missions 1985-1993 ESA/NASA Comet Nucleus Sample Return Science Definition Team (Deputy Chairman, U.S.
    [Show full text]
  • Arecibo Radar Observations of 14 High-Priority Near-Earth Asteroids in CY2020 and January 2021 Patrick A
    Arecibo Radar Observations of 14 High-Priority Near-Earth Asteroids in CY2020 and January 2021 Patrick A. Taylor (LPI, USRA), Anne K. Virkki, Flaviane C.F. Venditti, Sean E. Marshall, Dylan C. Hickson, Luisa F. Zambrano-Marin (Arecibo Observatory, UCF), Edgard G. Rivera-Valent´ın, Sriram S. Bhiravarasu, Betzaida Aponte-Hernandez (LPI, USRA), Michael C. Nolan, Ellen S. Howell (U. Arizona), Tracy M. Becker (SwRI), Jon D. Giorgini, Lance A. M. Benner, Marina Brozovic, Shantanu P. Naidu (JPL), Michael W. Busch (SETI), Jean-Luc Margot, Sanjana Prabhu Desai (UCLA), Agata Rozek˙ (U. Kent), Mary L. Hinkle (UCF), Michael K. Shepard (Bloomsburg U.), and Christopher Magri (U. Maine) Summary We propose the continuation of the long-running project R3037 to physically and dynamically characterize the population of near-Earth asteroids with the Arecibo S-band (2380 MHz; 12.6 cm) planetary radar system. The objectives of project R3037 are to: (1) collect high-resolution radar images of and (2) report ultra-precise radar astrometry for the strongest predicted radar targets for the 2020 calendar year plus early January 2021. Such images will be used for three-dimensional shape modeling as the data sets allow. These observations will be carried out as part of the NASA- funded Arecibo planetary radar program, Grant No. 80NSSC19K0523, to PI Anne Virkki (Arecibo Observatory, University of Central Florida) with Patrick Taylor as Institutional PI at the Lunar and Planetary Institute (Universities Space Research Association). Background Radar is arguably the most powerful Earth-based technique for post-discovery physical and dynamical characterization of near-Earth asteroids (NEAs) and plays a crucial role in the nation’s planetary defense initiatives led through the NASA Planetary Defense Coordination Office.
    [Show full text]
  • Imaging of Near-Earth Asteroids
    Imaging of Near-Earth Asteroids. Michael C. Nolan, Arecibo Observatory / Cornell University. [email protected] (787) 878-2612 ext 212 Lance A. M. Benner (Jet Propulsion Laboratory / California Institute of Technology) Marina Brozovič (Jet Propulsion Laboratory / California Institute of Technology) Ellen S. Howell (Arecibo Observatory / Cornell University) Jean-Luc Margot (UCLA) Abstract As remnants of accretion, building blocks of planets, space resources and potential impactors, the asteroids offer insights to solar system formation and evolution. Recent results show that this population is extremely diverse, compositionally, texturally and structurally. As a result, spacecraft cannot explore the population of asteroids in a reasonable time or at a reasonable cost without guidance from Earth-based reconnaissance. Compositional variation can be studied using remote-sensing spectroscopic techniques, either ground-based or from general-purpose space-based telescopes such as HST and JWST. Study of the textural and structural properties of asteroids requires imaging and shape determination. In addition, the largest uncertainties in orbit determination arise from non-gravitational forces, such as the Yarkovsky effect, that depend on the detailed shapes of asteroids. This shape determination can be done crudely using visible lightcurves and in detail using direct imaging (generally using adaptive optics), interferometric and radar techniques. Of these, only ground-based radar using the Arecibo and Goldstone radar systems has been routinely used for asteroid imaging, typically yielding shapes with tens to hundreds of pixels across a diameter and an absolute size accuracy of 5% or better. Other groundbased techniques are unlikely to achieve this level of precision in the upcoming decade, and space-based techniques will visit no more than a few targets.
    [Show full text]