Lunar and Planetary Information Bulletin
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New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period
Hayabusa2 Extended Mission: New Voyage to Rendezvous with a Small Asteroid Rotating with a Short Period M. Hirabayashi1, Y. Mimasu2, N. Sakatani3, S. Watanabe4, Y. Tsuda2, T. Saiki2, S. Kikuchi2, T. Kouyama5, M. Yoshikawa2, S. Tanaka2, S. Nakazawa2, Y. Takei2, F. Terui2, H. Takeuchi2, A. Fujii2, T. Iwata2, K. Tsumura6, S. Matsuura7, Y. Shimaki2, S. Urakawa8, Y. Ishibashi9, S. Hasegawa2, M. Ishiguro10, D. Kuroda11, S. Okumura8, S. Sugita12, T. Okada2, S. Kameda3, S. Kamata13, A. Higuchi14, H. Senshu15, H. Noda16, K. Matsumoto16, R. Suetsugu17, T. Hirai15, K. Kitazato18, D. Farnocchia19, S.P. Naidu19, D.J. Tholen20, C.W. Hergenrother21, R.J. Whiteley22, N. A. Moskovitz23, P.A. Abell24, and the Hayabusa2 extended mission study group. 1Auburn University, Auburn, AL, USA ([email protected]) 2Japan Aerospace Exploration Agency, Kanagawa, Japan 3Rikkyo University, Tokyo, Japan 4Nagoya University, Aichi, Japan 5National Institute of Advanced Industrial Science and Technology, Tokyo, Japan 6Tokyo City University, Tokyo, Japan 7Kwansei Gakuin University, Hyogo, Japan 8Japan Spaceguard Association, Okayama, Japan 9Hosei University, Tokyo, Japan 10Seoul National University, Seoul, South Korea 11Kyoto University, Kyoto, Japan 12University of Tokyo, Tokyo, Japan 13Hokkaido University, Hokkaido, Japan 14University of Occupational and Environmental Health, Fukuoka, Japan 15Chiba Institute of Technology, Chiba, Japan 16National Astronomical Observatory of Japan, Iwate, Japan 17National Institute of Technology, Oshima College, Yamaguchi, Japan 18University of Aizu, Fukushima, Japan 19Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA 20University of Hawai’i, Manoa, HI, USA 21University of Arizona, Tucson, AZ, USA 22Asgard Research, Denver, CO, USA 23Lowell Observatory, Flagstaff, AZ, USA 24NASA Johnson Space Center, Houston, TX, USA 1 Highlights 1. -
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. -
On the Structure of Polar Faculae on the Sun
A&A 425, 321–331 (2004) Astronomy DOI: 10.1051/0004-6361:20041120 & c ESO 2004 Astrophysics On the structure of polar faculae on the Sun O. V. Okunev1,2 and F. Kneer1 1 Universitäts-Sternwarte, Geismarlandstr. 11, 37083 Göttingen, Germany e-mail: [Kneer;olok]@uni-sw.gwdg.de 2 Central Astronomical Observatory at Pulkovo, 196140 St. Petersburg, Russia Received 20 April 2004 / Accepted 25 May 2004 Abstract. Faculae on the polar caps of the Sun, in short polar faculae (PFe), are investigated. They take part in the magnetic solar cycle. Here, we study the fine structures of PFe, their magnetic fields and their dynamics on short time scales. The observations stem from several periods in 2001 and 2002. They consist of spectropolarimetric data (Stokes I and V) taken in the Fe 6301.5 and 6302.5 Å and Fe 6149.3 Å lines with the Gregory-Coudé Telescope (GCT) and the Vacuum Tower Telescope (VTT) at the Observatorio del Teide on Tenerife. At the VTT, the “Göttingen” two-dimensional Fabry-Perot spectrometer was used. It allows image reconstruction with speckle methods resulting in spatial resolution of approximately 0. 25 for broadband images and 0. 5 for magnetograms. The application of singular value decomposition yielded a polarimetric detection limit of −3 |V|≈2 × 10 Ic.WefindthatPFe,ofsizeof1 or larger, possess substantial fine structure of both brightness and magnetic fields. The brightness and the location of polar facular points change noticeably within 50 s. The facular points have strong, kilo-Gauss magnetic fields, they are unipolar with the same polarity as the global, poloidal magnetic field. -
Mars 2020 Radiological Contingency Planning
National Aeronautics and Space Administration Mars 2020 Radiological Contingency Planning NASA plans to launch the Mars 2020 rover, produce the rover’s onboard power and to Perseverance, in summer 2020 on a mission warm its internal systems during the frigid to seek signs of habitable conditions in Mars’ Martian night. ancient past and search for signs of past microbial life. The mission will lift off from Cape NASA prepares contingency response plans Canaveral Air Force Station in Florida aboard a for every launch that it conducts. Ensuring the United Launch Alliance Atlas V launch vehicle safety of launch-site workers and the public in between mid-July and August 2020. the communities surrounding the launch area is the primary consideration in this planning. The Mars 2020 rover design is based on NASA’s Curiosity rover, which landed on Mars in 2012 This contingency planning task takes on an and greatly increased our knowledge of the added dimension when the payload being Red Planet. The Mars 2020 rover is equipped launched into space contains nuclear material. to study its landing site in detail and collect and The primary goal of radiological contingency store the most promising samples of rock and planning is to enable an efficient response in soil on the surface of Mars. the event of an accident. This planning is based on the fundamental principles of advance The system that provides electrical power for preparation (including rehearsals of simulated Mars 2020 and its scientific equipment is the launch accident responses), the timely availability same as for the Curiosity rover: a Multi- of technically accurate and reliable information, Mission Radioisotope Thermoelectric Generator and prompt external communication with the (MMRTG). -
An Assessment of Aerocapture and Applications to Future Missions
Post-Exit Atmospheric Flight Cruise Approach An Assessment of Aerocapture and Applications to Future Missions February 13, 2016 National Aeronautics and Space Administration An Assessment of Aerocapture Jet Propulsion Laboratory California Institute of Technology Pasadena, California and Applications to Future Missions Jet Propulsion Laboratory, California Institute of Technology for Planetary Science Division Science Mission Directorate NASA Work Performed under the Planetary Science Program Support Task ©2016. All rights reserved. D-97058 February 13, 2016 Authors Thomas R. Spilker, Independent Consultant Mark Hofstadter Chester S. Borden, JPL/Caltech Jessie M. Kawata Mark Adler, JPL/Caltech Damon Landau Michelle M. Munk, LaRC Daniel T. Lyons Richard W. Powell, LaRC Kim R. Reh Robert D. Braun, GIT Randii R. Wessen Patricia M. Beauchamp, JPL/Caltech NASA Ames Research Center James A. Cutts, JPL/Caltech Parul Agrawal Paul F. Wercinski, ARC Helen H. Hwang and the A-Team Paul F. Wercinski NASA Langley Research Center F. McNeil Cheatwood A-Team Study Participants Jeffrey A. Herath Jet Propulsion Laboratory, Caltech Michelle M. Munk Mark Adler Richard W. Powell Nitin Arora Johnson Space Center Patricia M. Beauchamp Ronald R. Sostaric Chester S. Borden Independent Consultant James A. Cutts Thomas R. Spilker Gregory L. Davis Georgia Institute of Technology John O. Elliott Prof. Robert D. Braun – External Reviewer Jefferey L. Hall Engineering and Science Directorate JPL D-97058 Foreword Aerocapture has been proposed for several missions over the last couple of decades, and the technologies have matured over time. This study was initiated because the NASA Planetary Science Division (PSD) had not revisited Aerocapture technologies for about a decade and with the upcoming study to send a mission to Uranus/Neptune initiated by the PSD we needed to determine the status of the technologies and assess their readiness for such a mission. -
An Overview of Hayabusa2 Mission and Asteroid 162173 Ryugu
Asteroid Science 2019 (LPI Contrib. No. 2189) 2086.pdf AN OVERVIEW OF HAYABUSA2 MISSION AND ASTEROID 162173 RYUGU. S. Watanabe1,2, M. Hira- bayashi3, N. Hirata4, N. Hirata5, M. Yoshikawa2, S. Tanaka2, S. Sugita6, K. Kitazato4, T. Okada2, N. Namiki7, S. Tachibana6,2, M. Arakawa5, H. Ikeda8, T. Morota6,1, K. Sugiura9,1, H. Kobayashi1, T. Saiki2, Y. Tsuda2, and Haya- busa2 Joint Science Team10, 1Nagoya University, Nagoya 464-8601, Japan ([email protected]), 2Institute of Space and Astronautical Science, JAXA, Japan, 3Auburn University, U.S.A., 4University of Aizu, Japan, 5Kobe University, Japan, 6University of Tokyo, Japan, 7National Astronomical Observatory of Japan, Japan, 8Research and Development Directorate, JAXA, Japan, 9Tokyo Institute of Technology, Japan, 10Hayabusa2 Project Summary: The Hayabusa2 mission reveals the na- Combined with the rotational motion of the asteroid, ture of a carbonaceous asteroid through a combination global surveys of Ryugu were conducted several times of remote-sensing observations, in situ surface meas- from ~20 km above the sub-Earth point (SEP), includ- urements by rovers and a lander, an active impact ex- ing global mapping from ONC-T (Fig. 1) and TIR, and periment, and analyses of samples returned to Earth. scan mapping from NIRS3 and LIDAR. Descent ob- Introduction: Asteroids are fossils of planetesi- servations covering the equatorial zone were performed mals, building blocks of planetary formation. In partic- from 3-7 km altitudes above SEP. Off-SEP observa- ular carbonaceous asteroids (or C-complex asteroids) tions of the polar regions were also conducted. Based are expected to have keys identifying the material mix- on these observations, we constructed two types of the ing in the early Solar System and deciphering the global shape models (using the Structure-from-Motion origin of water and organic materials on Earth [1]. -
An Impacting Descent Probe for Europa and the Other Galilean Moons of Jupiter
An Impacting Descent Probe for Europa and the other Galilean Moons of Jupiter P. Wurz1,*, D. Lasi1, N. Thomas1, D. Piazza1, A. Galli1, M. Jutzi1, S. Barabash2, M. Wieser2, W. Magnes3, H. Lammer3, U. Auster4, L.I. Gurvits5,6, and W. Hajdas7 1) Physikalisches Institut, University of Bern, Bern, Switzerland, 2) Swedish Institute of Space Physics, Kiruna, Sweden, 3) Space Research Institute, Austrian Academy of Sciences, Graz, Austria, 4) Institut f. Geophysik u. Extraterrestrische Physik, Technische Universität, Braunschweig, Germany, 5) Joint Institute for VLBI ERIC, Dwingelo, The Netherlands, 6) Department of Astrodynamics and Space Missions, Delft University of Technology, The Netherlands 7) Paul Scherrer Institute, Villigen, Switzerland. *) Corresponding author, [email protected], Tel.: +41 31 631 44 26, FAX: +41 31 631 44 05 1 Abstract We present a study of an impacting descent probe that increases the science return of spacecraft orbiting or passing an atmosphere-less planetary bodies of the solar system, such as the Galilean moons of Jupiter. The descent probe is a carry-on small spacecraft (< 100 kg), to be deployed by the mother spacecraft, that brings itself onto a collisional trajectory with the targeted planetary body in a simple manner. A possible science payload includes instruments for surface imaging, characterisation of the neutral exosphere, and magnetic field and plasma measurement near the target body down to very low-altitudes (~1 km), during the probe’s fast (~km/s) descent to the surface until impact. The science goals and the concept of operation are discussed with particular reference to Europa, including options for flying through water plumes and after-impact retrieval of very-low altitude science data. -
OPAG Update to the Planetary Science Advisory Committee (PAC)
OPAG Update to the Planetary Science Advisory Committee (PAC) ? Linda Spilker OPAG Vice-Chair, JPL PAC Meeting September 24, 2019 Large KBOs: Outer Planets Assessment Group (OPAG) Charter https://www.lpi.usra.edu/opag/ • NASA's community-based forum to provide science input for planning and prioritizing outer planet exploration activities for the next several decades • Evaluates outer solar system exploration goals, objectives, investigations and required measurements on the basis of the widest possible community outreach • Meets twice per year, summer and winter – Next meeting: Feb. 3-4, 2020, LPI, Houston, TX • OPAG documents are inputs to the Decadal Surveys • OPAG and Small Bodies Assessment Group (SBAG) have Joint custody of Pluto system and other planets among Kuiper Belt Objects KBO planets OPAG Steering Committee Jeff Moore Linda Spilker OPAG Chair OPAG Vice-Chair * =New Member Ames Research Center Jet Propulsion Lab Alfred McEwen Lynnae Quick* Kathleen Mandt* University of Arizona NASA Goddard Applied Physics Laboratory OPAG Steering Committee Scott Edgington Amanda Hendrix Mark Hofstadter Jet Propulsion Lab Planetary Science Institute Jet Propulsion Lab Terry Hurford Carol Paty Goddard Space Flight Center Georgia Institute of Technology OPAG Steering Committee Morgan Cable* Britney Schmidt Kunio Sayanagi Jet Propulsion Lab Georgia Institute of Technology Hampton University * =New Member Tom Spilker* Abigail Rymer* Consultant Applied Physics Lab Recent and Upcoming OPAG-related Meetings • OPAG Subsurface Needs for Ocean Worlds -
MARS 2020, CANDIDATES LANDING SITES, EXOMARS and THEIR RELATIONSHIP to MARS SAMPLE RETURN 10:25 A.M
2nd International Mars Sample Return 2018 (LPI Contrib. No. 2071) sess303.pdf Thursday, April 26, 2018 MARS 2020, CANDIDATES LANDING SITES, EXOMARS AND THEIR RELATIONSHIP TO MARS SAMPLE RETURN 10:25 a.m. Forum This session will present a status report on the Mars 2020 sample-caching rover, its candidate landing sites, the Exomars rover mission, and the relationship of all of these to Mars Sample Return. Chairs: Victoria Hipkin (Canadian Space Agency, Canada) Briony Horgan (Purdue University, USA) 10:25 a.m. Williford K. * *Jet Propulsion Laboratory, California Institute of Technology, USA The NASA Mars 2020 Rover Mission The NASA Mars 2020 rover mission will explore an astrobiologically relevant site to characterize its geology, evaluate past habitability, seek signs of ancient life, and assemble a returnable cache of samples. An overview of technical capabilities and scientific strategy in development will be presented with a focus on the role envisioned for Mars 2020 in a possible Mars sample return campaign. 10:45 a.m. Schulte M. * Meyer M. Grant J. Golombek M. *NASA Headquarters, USA The Mars 2020 Rover Mission Landing Site Candidates [#6026] The number of suitable landing sites for the Mars 2020 rover mission has been narrowed to three leading candidates: Jezero Crater, NE Syrtis, and Columbia Hills. Each offers geologic settings with the potential for preservation of biosignatures. 11:00 a.m. Vago J. L. * Svedhem H. Sefton-Nash E. Kminek G. Ruesch O. Haldemann A. F. C. Rodionov D. ExoMars Science Working Team *European Space Agency ExoMars Contributions to Mars Sample Return [#6021] Each of the two ExoMars missions has the potential to make discoveries that could inform and perhaps influence our collective strategy for a future Mars Sample Return mission. -
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. -
USBC Approved Bowling Balls
USBC Approved Bowling Balls (See rulebook, Chapter VII, "USBC Equipment Specifications" for any balls manufactured prior to January 1991.) ** Bowling balls manufactured only under 13 pounds. 5/17/2011 Brand Ball Name Date Approved 900 Global Awakening Jul-08 900 Global BAM Aug-07 900 Global Bank Jun-10 900 Global Bank Pearl Jan-11 900 Global Bounty Oct-08 900 Global Bounty Hunter Jun-09 900 Global Bounty Hunter Black Jan-10 900 Global Bounty Hunter Black/Purple Feb-10 900 Global Bounty Hunter Pearl Oct-09 900 Global Break Out Dec-09 900 Global Break Pearl Jan-08 900 Global Break Point Feb-09 900 Global Break Point Pearl Jun-09 900 Global Creature Aug-07 900 Global Creature Pearl Feb-08 900 Global Day Break Jun-09 900 Global DVA Open Aug-07 900 Global Earth Ball Aug-07 900 Global Favorite May-10 900 Global Head Hunter Jul-09 900 Global Hook Dark Blue/Light Blue Feb-11 900 Global Hook Purple/Orange Pearl Feb-11 900 Global Hook Red/Yellow Solid Feb-11 900 Global Integral Break Black Nov-10 900 Global Integral Break Rose/Orange Nov-10 900 Global Integral Break Rose/Silver Nov-10 900 Global Link Jul-08 900 Global Link Black/Red Feb-09 900 Global Link Purple/Blue Pearl Dec-08 900 Global Link Rose/White Feb-09 900 Global Longshot Jul-10 900 Global Lunatic Jun-09 900 Global Mach One Blackberry Pearl Sep-10 900 Global Mach One Rose/Purple Pearl Sep-10 900 Global Maniac Oct-08 900 Global Mark Roth Ball Jan-10 900 Global Missing Link Black/Red Jul-10 900 Global Missing Link Blackberry/Silver Jul-10 900 Global Missing Link Blue/White Jul-10 900 Global -
STS-117 Press Kit STS-117 Press Kit
STS-117 Press Kit STS-117 Press Kit CONTENTS Section Page STS-117 MISSION OVERVIEW................................................................................................. 1 STS-117 TIMELINE OVERVIEW................................................................................................ 11 MISSION PRIORITIES............................................................................................................. 13 LAUNCH AND LANDING ........................................................................................................... 15 LAUNCH............................................................................................................................................... 15 ABORT-TO-ORBIT (ATO)...................................................................................................................... 15 TRANSATLANTIC ABORT LANDING (TAL)............................................................................................. 15 RETURN-TO-LAUNCH-SITE (RTLS)....................................................................................................... 15 ABORT ONCE AROUND (AOA)............................................................................................................... 15 LANDING ............................................................................................................................................. 15 MISSION PROFILE................................................................................................................... 17 STS-117