The OSIRIS-Rex Asteroid Sample Return Mission
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Hayabusa2 and the Formation of the Solar System PPS02-25
PPS02-25 JpGU-AGU Joint Meeting 2017 Hayabusa2 and the formation of the Solar System *Sei-ichiro WATANABE1,2, Hayabusa2 Science Team2 1. Division of Earth and Planetary Sciences, Graduate School of Science, Nagoya University, 2. JAXA/ISAS Explorations of small solar system bodies bring us direct and unique information about the formation and evolution of the Solar system. Asteroids may preserve accretion processes of planetesimals or pebbles, a sequence of destructive events induced by the gas-driven migration of giant planets, and hydrothermal processes on the parent bodies. After successful small-body missions like Rosetta to comet 67P/Churyumov-Gerasimenko, Dawn to Vesta and Ceres, and New Horizons to Pluto, two spacecraft Hayabusa2 and OSIRIS-REx are now traveling to dark primitive asteroids.The Hayabusa2 spacecraft journeys to a C-type near-earth asteroid (162173) Ryugu (1999 JU3) to conduct detailed remote sensing observations and return samples from the surface. The Haybusa2 spacecraft developed by Japan Aerospace Exploration Agency (JAXA) was successfully launched on 3 Dec. 2014 by the H-IIA Launch Vehicle and performed an Earth swing-by on 3 Dec. 2015 to set it on a course toward its target. The spacecraft will reach Ryugu in the summer of 2018, observe the asteroid for 18 months, and sample surface materials from up to three different locations. The samples will be delivered to the Earth in Nov.-Dec. 2020. Ground-based observations have obtained a variety of optical reflectance spectra for Ryugu. Some reported the 0.7 μm absorption feature and steep slope in the short wavelength region, suggesting hydrated minerals. -
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. -
Lindley Johnson (NASA HQ) – NASA HEOMD – – NASA STMD – Tibor Balint (NASA HQ) – SSERVI – Greg Schmidt (NASA ARC) 19
September 4, 2014: Planetary Science Subcommittee Nancy Chabot, SBAG Chair 11th SBAG Meeting • July 29-31, 2014: Washington, DC • Highlights of SBAG meeting presentations from major projects • Discussion of findings • New steering committee members • Future meetings 1 NEOWISE Reac,va,on • Reac,vated in Dec 2013, NEOWISE is observing, discovering, and characterizing asteroids & comets using 3.4 and 4.6 µm channels • 7239 minor planets observed, including 157 near-Earth objects (NEOs). • 89 discoveries, including 26 NEOs and 3 comets. • NEO discoveries are large, dark • First data delivery from Reac9vaon: March 2015 to IRSA: • hp://irsa.ipac.caltech.edu/Missions/wise.html • All data from prime WISE/NEOWISE mission are publicly available through IRSA and team Comet P/2014 L2 NEOWISE papers; derived physical proper9es heading to PDS Dawn prepares to encounter Ceres PI: Alan Stern (SwRI) New Horizons Status PM: JHU-APL • Spacecraft is healthy & On-Course for Pluto (Radio) § 1.3x more fuel available for KBO Extended (High-E Plasma) NH Payload Mission phase than originally expected • Payload is healthy and well-calibrated § Finishing final Annual Checkout (ACO-8) • First Pluto OpNav Campaign conducted (UV Spectral) § See image below • Enter final Hibernation on Aug 29th (Vis-Color + IR Spectral) • Pluto Encounter begins on 2015-Jan-15 (Low-E Plasma) • Pluto Closest Approach: 2015-Jul-14 (Pan Imager) Intensive searches with ground-based facilities over the past Pluto OpNav Campaign: 2 years have not yet yielded a KBO target for NH. A 194- Cleanly separate Pluto & orbit Hubble program was started in June; below Charon shows the first potentially targetable KBO found. -
The Catalina Sky Survey
The Catalina Sky Survey Current Operaons and Future CapabiliKes Eric J. Christensen A. Boani, A. R. Gibbs, A. D. Grauer, R. E. Hill, J. A. Johnson, R. A. Kowalski, S. M. Larson, F. C. Shelly IAWN Steering CommiJee MeeKng. MPC, Boston, MA. Jan. 13-14 2014 Catalina Sky Survey • Supported by NASA NEOO Program • Based at the University of Arizona’s Lunar and Planetary Laboratory in Tucson, Arizona • Leader of the NEO discovery effort since 2004, responsible for ~65% of new discoveries (~46% of all NEO discoveries). Currently discovering NEOs at a rate of ~600/year. • 2 survey telescopes run by a staff of 8 (observers, socware developers, engineering support, PI) Current FaciliKes Mt. Bigelow, AZ Mt. Lemmon, AZ 0.7-m Schmidt 1.5-m reflector 8.2 sq. deg. FOV 1.2 sq. deg. FOV Vlim ~ 19.5 Vlim ~ 21.3 ~250 NEOs/year ~350 NEOs/year ReKred FaciliKes Siding Spring Observatory, Australia 0.5-m Uppsala Schmidt 4.2 sq. deg. FOV Vlim ~ 19.0 2004 – 2013 ~50 NEOs/year Was the only full-Kme NEO survey located in the Southern Hemisphere Notable discoveries include Great Comet McNaught (C/2006 P1), rediscovery of Apophis Upcoming FaciliKes Mt. Lemmon, AZ 1.0-m reflector 0.3 sq. deg. FOV 1.0 arcsec/pixel Operaonal 2014 – currently in commissioning Will be primarily used for confirmaon and follow-up of newly- discovered NEOs Will remove follow-up burden from CSS survey telescopes, increasing available survey Kme by 10-20% Increased FOV for both CSS survey telescopes 5.0 deg2 1.2 ~1,100/ G96 deg2 night 19.4 deg2 2 703 8.2 deg 2 ~4,300 deg per night New 10k x 10k cameras will increase the FOV of both survey telescopes by factors of 4x and 2.4x. -
New Horizons Pluto/KBO Mission Impact Hazard
New Horizons Pluto/KBO Mission Impact Hazard Hal Weaver NH Project Scientist The Johns Hopkins University Applied Physics Laboratory Outline • Background on New Horizons mission • Description of Impact Hazard problem • Impact Hazard mitigation – Hubble Space Telescope plays a key role New Horizons: To Pluto and Beyond The Initial Reconnaissance of The Solar System’s “Third Zone” KBOs Pluto-Charon Jupiter System 2016-2020 July 2015 Feb-March 2007 Launch Jan 2006 PI: Alan Stern (SwRI) PM: JHU Applied Physics Lab New Horizons is NASA’s first New Frontiers Mission Frontier of Planetary Science Explore a whole new region of the Solar System we didn’t even know existed until the 1990s Pluto is no longer an outlier! Pluto System is prototype of KBOs New Horizons gives the first close-up view of these newly discovered worlds New Horizons Now (overhead view) NH Spacecraft & Instruments 2.1 meters Science Team: PI: Alan Stern Fran Bagenal Rick Binzel Bonnie Buratti Andy Cheng Dale Cruikshank Randy Gladstone Will Grundy Dave Hinson Mihaly Horanyi Don Jennings Ivan Linscott Jeff Moore Dave McComas Bill McKinnon Ralph McNutt Scott Murchie Cathy Olkin Carolyn Porco Harold Reitsema Dennis Reuter Dave Slater John Spencer Darrell Strobel Mike Summers Len Tyler Hal Weaver Leslie Young Pluto System Science Goals Specified by NASA or Added by New Horizons New Horizons Resolution on Pluto (Simulations of MVIC context imaging vs LORRI high-resolution "noodles”) 0.1 km/pix The Best We Can Do Now 0.6 km/pix HST/ACS-PC: 540 km/pix New Horizons Science Status • -
Curriculum Vitae
DANTE S. LAURETTA Lunar and Planetary Laboratory Department of Planetary Sciences University of Arizona Tucson, AZ 85721-0092 Cell: (520) 609-2088 Email: [email protected] CHRONOLOGY OF EDUCATION Washington University, St. Louis, MO Dept. of Earth and Planetary Sciences Ph.D. in Earth and Planetary Sciences, 1997 Thesis: Theoretical and Experimental Studies of Fe-Ni-S, Be, and B Cosmochemistry Advisor: Bruce Fegley, Jr. University of Arizona, Tucson, AZ Depts. of Physics, Mathematics, and East Asian Studies B.S. in Physics and Mathematics, Cum Laude, 1993 B.A. in Oriental Studies (emphasis: Japanese), Cum Laude, 1993 CHRONOLOGY OF EMPLOYMENT Professor, Lunar and Planetary Laboratory, Dept. of Planetary Sciences, University of Arizona, Tucson, AZ; 2012 – present. Principal Investigator, OSIRIS-REx Asteroid Sample Return Mission, NASA New Frontiers Program, 2011 – present. Deputy Principal Investigator, OSIRIS-REx Asteroid Sample Return Mission, NASA New Frontiers Program, 2008 – 2011. Associate Professor, Lunar and Planetary Laboratory, Dept. of Planetary Sciences, University of Arizona, Tucson, AZ; 2006 – 2012. Assistant Professor, Lunar and Planetary Laboratory, Dept. of Planetary Sciences, University of Arizona, Tucson, AZ; 2001 – 2006. Associate Research Scientist, Dept. of Chemistry & Biochemistry, Arizona State University, Tempe, AZ; 1999 – 2001. Postdoctoral Research Associate, Dept. of Geology, Arizona State University, Tempe, AZ Primary project: Transmission electron microscopy of meteoritic minerals. Supervisor: Peter R. Buseck; Dates: 1997 – 1999. Research Assistant, Dept. of Earth and Planetary Sciences, Washington Univ., St. Louis, MO Primary project: Experimental studies of sulfide formation in the solar nebula. Advisor: Bruce Fegley, Jr.; Dates: 1993 – 1997. Research Intern, NASA Undergraduate Research Program, University of Arizona, Tucson, AZ Primary project: Development of a logic-based language for S.E.T.I. -
Five Aerojet Boosters Set to Lift New Horizons Spacecraft
January 15, 2006 Five Aerojet Boosters Set to Lift New Horizons Spacecraft Aerojet Propulsion Will Support Both Launch Vehicle and Spacecraft for Mission to Pluto SACRAMENTO, Calif., Jan. 15 /PRNewswire/ -- Aerojet, a GenCorp Inc. (NYSE: GY) company, will provide five solid rocket boosters for the launch vehicle and a propulsion system for the spacecraft when a Lockheed Martin Atlas® V launches the Pluto New Horizons spacecraft January 17 from Cape Canaveral, AFB. The launch window opens at 1:24 p.m. EST on January 17 and extends through February 14. The New Horizons mission, dubbed by NASA as the "first mission to the last planet," will study Pluto and its moon, Charon, in detail during a five-month- long flyby encounter. Pluto is the solar system's most distant planet, averaging 3.6 billion miles from the sun. Aerojet's solid rocket boosters (SRBs), each 67-feet long and providing an average of 250,000 pounds of thrust, will provide the necessary added thrust for the New Horizons mission. The SRBs have flown in previous vehicle configurations using two and three boosters; this is the first flight utilizing the five boosters. Additionally, 12 Aerojet monopropellant (hydrazine) thrusters on the Atlas V Centaur upper stage will provide roll, pitch, and yaw control settling burns for the launch vehicle main engines. Aerojet also supplies 8 retro rockets for Atlas Centaur separation. Aerojet also provided the spacecraft propulsion system, comprised of a propellant tank, 16 thrusters and various other components, which will control pointing and navigation for the spacecraft on its journey and during encounters with Pluto- Charon and, as part of a possible extended mission, to more distant, smaller objects in the Kuiper Belt. -
Modelling Bennu's Crater Development
EPSC Abstracts Vol. 14, EPSC2020-442, 2020 https://doi.org/10.5194/epsc2020-442 Europlanet Science Congress 2020 © Author(s) 2021. This work is distributed under the Creative Commons Attribution 4.0 License. Modelling Bennu's Crater Development Peter Smith, Daniella DellaGiustina, Keara Burke, Dathon Golish, and Dante Lauretta University of Arizona, Planetary Sciences, Tucson, United States of America ([email protected]) Modeling Bennu’s Crater Development P.H. Smith (1), D.N. DellaGiustina (1), K.N. Burke (1), D.R. Golish (1), D. S. Lauretta (1) (1) Lunar and Planetary Laboratory, University of Arizona, USA ([email protected]) Introduction Several hundred craters have been identified and mapped on Bennu [1]. Their spectral properties have been studied using data from the MapCam instrument onboard the OSIRIS-REx spacecraft [2]. The crater frequency versus spectral slope across the wavelength range of 0.550 µm (v band) to 0.860 µm (x band) shows a skewed distribution varying from the median spectral slope of –0.17 micron–1 (x/v = 0.948) to a neutral or flat slope (x/v = 1.0). DellaGiustina et al. [2] attribute this trend to space weathering. They suggest that freshly formed craters are red, and as they age, they evolve to the bluish slope seen across the asteroidal surface. This abstract presents the results of an age model of Bennu’s craters in the size range of 1 to 10 m. Craters in this size range were selected as having likely been formed during the time that Bennu has orbited in near-Earth space. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
An Early Warning System for Asteroid Impact
An Early Warning System for Asteroid Impact John L. Tonry(1) ABSTRACT Earth is bombarded by meteors, occasionally by one large enough to cause a significant explosion and possible loss of life. It is not possible to detect all hazardous asteroids, and the efforts to detect them years before they strike are only advancing slowly. Similarly, ideas for mitigation of the danger from an impact by moving the asteroid are in their infancy. Although the odds of a deadly asteroid strike in the next century are low, the most likely impact is by a relatively small asteroid, and we suggest that the best mitigation strategy in the near term is simply to move people out of the way. With enough warning, a small asteroid impact should not cause loss of life, and even portable property might be preserved. We describe an \early warning" system that could provide a week's notice of most sizeable asteroids or comets on track to hit the Earth. This may be all the mitigation needed or desired for small asteroids, and it can be implemented immediately for relatively low cost. This system, dubbed \Asteroid Terrestrial-impact Last Alert System" (AT- LAS), comprises two observatories separated by about 100 km that simulta- neously scan the visible sky twice a night. Software automatically registers a comparison with the unchanging sky and identifies everything which has moved or changed. Communications between the observatories lock down the orbits of anything approaching the Earth, within one night if its arrival is less than a week. The sensitivity of the system permits detection of 140 m asteroids (100 Mton impact energy) three weeks before impact, and 50 m asteroids a week be- fore arrival. -
Neofixer a Broker for Near Earth Asteroid Follow-Up Rob Seaman & Eric Christensen Catalina Sky Survey
NEOFIXER A BROKER FOR NEAR EARTH ASTEROID FOLLOW-UP ROB SEAMAN & ERIC CHRISTENSEN CATALINA SKY SURVEY Building the Infrastructure for Time-Domain Alert Science in the LSST Era • May 22-25, 2017 • Tucson CATALINA SKY SURVEY • LPL runs 2 NEO projects, CSS and SpacewatcH • Talk to Eric or me about CSS, Bob McMillan for SW • CSS demo at 3:30 pm CONGRESSIONAL MANDATE • Spaceguard goal: 1 km Near EartH Objects ✔ • George E Brown Act to find > 140m (H < 22) NEOs • 90% complete by 2020 ✘ (2017: ~ 30%) • ROSES 2017 language is > 100m • Chelyabinsk was ~20m (H ~ 25.8) or ~400 kiloton (few per century likeliHood) SUMMARY • Near EartH Asteroid inventory is “retail Big Data” • NEOfixer will be NEO-optimized targeting broker • No one broker will address all use cases • Will benefit LSST as well as current surveys • LSST not tasked to study NEOs, but ratHer tHe Solar System (slower objects and fartHer away) • What is tHe most valuable NEO observation a particular telescope can make at a particular time? CHESLEY & VERES (1705.06209) • 55 ± 5.0% for LSST baseline operating alone • But 42% of NEOs witH H < 22 will be discovered before 2022 • And witHout LSST, current surveys would discover 61% of the catalog by 2032 • Completion CH<22 will be 77% combined LSST will add 16% to CH<22 Can targeted follow-up increase this? CHESLEY & VERES (CAVEATS) • Lots of details worth reading • CH<22 degrades by ~1.8% for every 0.1 mag loss in sensitivity • Issues of linking efficiency including: • Efficiency down to H < 25 is lower • 4% false MBA-MBA links ASTROMETRIC -
Newsletter December 2016
Current NEO statistics A refinement of the method used for analysing the asteroid hazard led to an increase in the number of objects in the risk list. Known NEOs: 15 271 asteroids and 106 comets NEOs in risk list*: 576 New NEO discoveries since last month: 161 NEOs discovered since 1 January 2016: 1750 Focus on Whenever a new set of observations for an object is published, our Impact Monitoring routines perform a new search for possibly impacting orbits compatible with such set of observations. The system is capable of detecting all possibly impacting orbits down to an impact probability threshold, named “generic completeness level”. The search begins by investigating a set of initial conditions taken along a specific line of parameters, called Line of Variations (LoV), inside the orbit uncertainty region. The NEODyS impact monitoring system was recently switched to a new method to sample the LoV, which decreased the generic completeness level from 4×10-7 to 10-7 (i.e. a factor of four better than the previous approach). The whole risk list has been updated with the outcome of the new method, and it is now available on both the NEODyS and the NEOCC risk pages. Upcoming interesting close approaches To date no known object is expected to come closer than one lunar distance to our planet in December, thus deserving special attention. New discoveries likely will. The closest known approach will be 2016 WQ3 at 1.5 lunar distances on 1 December. Recent interesting close approaches Four new objects came closer than the Moon in November.