Physical Characterization of Equal-Mass Binary Near-Earth Asteroid 2017 YE5: a Possible Dormant Jupiter-Family Comet
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On the Origin and Evolution of the Material in 67P/Churyumov-Gerasimenko
On the Origin and Evolution of the Material in 67P/Churyumov-Gerasimenko Martin Rubin, Cécile Engrand, Colin Snodgrass, Paul Weissman, Kathrin Altwegg, Henner Busemann, Alessandro Morbidelli, Michael Mumma To cite this version: Martin Rubin, Cécile Engrand, Colin Snodgrass, Paul Weissman, Kathrin Altwegg, et al.. On the Origin and Evolution of the Material in 67P/Churyumov-Gerasimenko. Space Sci.Rev., 2020, 216 (5), pp.102. 10.1007/s11214-020-00718-2. hal-02911974 HAL Id: hal-02911974 https://hal.archives-ouvertes.fr/hal-02911974 Submitted on 9 Dec 2020 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. Space Sci Rev (2020) 216:102 https://doi.org/10.1007/s11214-020-00718-2 On the Origin and Evolution of the Material in 67P/Churyumov-Gerasimenko Martin Rubin1 · Cécile Engrand2 · Colin Snodgrass3 · Paul Weissman4 · Kathrin Altwegg1 · Henner Busemann5 · Alessandro Morbidelli6 · Michael Mumma7 Received: 9 September 2019 / Accepted: 3 July 2020 / Published online: 30 July 2020 © The Author(s) 2020 Abstract Primitive objects like comets hold important information on the material that formed our solar system. Several comets have been visited by spacecraft and many more have been observed through Earth- and space-based telescopes. -
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. -
On the V-Type Asteroids Outside the Vesta Family. I. Interplay Of
Astronomy & Astrophysics manuscript no. carruba September 16, 2018 (DOI: will be inserted by hand later) On the V-type asteroids outside the Vesta family I. Interplay of nonlinear secular resonances and the Yarkovsky effect: the cases of 956 Elisa and 809 Lundia V. Carruba1, T. A. Michtchenko1 , F. Roig2, S. Ferraz-Mello1, and D. Nesvorn´y3, 1 IAG, Universidade de S˜ao Paulo, S˜ao Paulo, SP 05508-900, Brazil e-mail: [email protected] 2 Observat´orio Nacional, Rio de Janeiro, RJ 20921-400, Brazil e-mail: [email protected] 3 Southwest Research Institute, Department of Space Studies, Boulder, Colorado 80302 e-mail: [email protected] Received May 2nd 2005; accepted June 22nd 2005. Abstract. Among the largest objects in the main belt, asteroid 4 Vesta is unique in showing a basaltic crust. It is also the biggest member of the Vesta family, which is supposed to originate from a large cratering event about 1 Gyr ago (Marzari et al. 1996). Most of the members of the Vesta family for which a spectral classification is available show a V-type spectra. Due to their characteristic infrared spectrum, V-type asteroids are easily distinguished. Before the discovery of 1459 Magnya (Lazzaro et al. 2000) and of several V-type NEA (Xu 1995), all the known V-type asteroids were members of the Vesta family. Recently two V-type asteroids, 809 Lundia and 956 Elisa, (Florczak et al. 2002) have been discovered well outside the limits of the family, near the Flora family. We currently know 22 V-type asteroids outside the family, in the inner asteroid belt (see Table 2). -
Temperature-Induced Effects and Phase Reddening on Near-Earth Asteroids
Planetologie Temperature-induced effects and phase reddening on near-Earth asteroids Inaugural-Dissertation zur Erlangung des Doktorgrades der Naturwissenschaften im Fachbereich Geowissenschaften der Mathematisch-Naturwissenschaftlichen Fakultät der Westfälischen Wilhelms-Universität Münster vorgelegt von Juan A. Sánchez aus Caracas, Venezuela -2013- Dekan: Prof. Dr. Hans Kerp Erster Gutachter: Prof. Dr. Harald Hiesinger Zweiter Gutachter: Dr. Vishnu Reddy Tag der mündlichen Prüfung: 4. Juli 2013 Tag der Promotion: 4. Juli 2013 Contents Summary 5 Preface 7 1 Introduction 11 1.1 Asteroids: origin and evolution . 11 1.2 The asteroid-meteorite connection . 13 1.3 Spectroscopy as a remote sensing technique . 16 1.4 Laboratory spectral calibration . 24 1.5 Taxonomic classification of asteroids . 31 1.6 The NEA population . 36 1.7 Asteroid space weathering . 37 1.8 Motivation and goals of the thesis . 41 2 VNIR spectra of NEAs 43 2.1 The data set . 43 2.2 Data reduction . 45 3 Temperature-induced effects on NEAs 55 3.1 Introduction . 55 3.2 Temperature-induced spectral effects on NEAs . 59 3.2.1 Spectral band analysis of NEAs . 59 3.2.2 NEAs surface temperature . 59 3.2.3 Temperature correction to band parameters . 62 3.3 Results and discussion . 70 4 Phase reddening on NEAs 73 4.1 Introduction . 73 4.2 Phase reddening from ground-based observations of NEAs . 76 4.2.1 Phase reddening effect on the band parameters . 76 4.3 Phase reddening from laboratory measurements of ordinary chondrites . 82 4.3.1 Data and spectral band analysis . 82 4.3.2 Phase reddening effect on the band parameters . -
DART Mission Update
Kinetic Impactor Andy Cheng JHU/APL 15 Nov 2018 DART Mission Update Goddard Space Flight Center Johnson Space Center Langley Research Center Glenn Research Center Marshall Space Flight Center Planetary Defense Coordination Office 1 Regimes of Primary Applicability for Planetary Defense Mitigation Defending Planet Earth (2010) Zero PHAs National Academy of Sciences Deep Impact Recommendation: “the first priority for a space About 150 PHAs mission in the mitigation area is an experimental test of a kinetic impactor” About 5,000 PHAs DART is the first kinetic DART impact test at a realistic scale for planetary Too small to be Defending Planet Earth (2010) considered PHAs defense 2 Launch June 15, 2021 March 6, 2022 IMPACT: October 5, 2022 2001 CB21 flyby S-type, 578 meters, 3.3-hour rotation rate LICIA (Light Italian Cubesat for Imaging of Asteroids) ASI contribution, under consideration DART Spacecraft 65803 Didymos 560 kg arrival mass Didymos-B (1996 GT) Didymos-A 12.5 m × 2.4 m × 2.0 m 163 meters 1,180-meter separation 780 meters, S-type 6 km/s closing speed 11.92-hour orbital period between centers of A and B 2.26-hour rotation period Earth-Based Observations • Target the binary asteroid Didymos system 0.07 AU range at impact Predicted ~8-minute change • Impact Didymos-B and change its orbital period in binary orbit period • Measure the period change from Earth DART – Double Asteroid Redirection Test 3 DART Program Update .DART mission confirmed by NASA in August, 2018. DART is in PHASE C-D .NASA has re-affirmed decision to use NEXT- C ion propulsion system for DART Autonomous navigation .NASA will procure launch services for DART using imager to guide to target through NLS; LV selection is in process ─ DART will have dedicated LV .LICIACube, an ASI-contributed cubesat ─ Letters exchanged between NASA and ASI ─ Studying operations concept and cubesat NEXT-C ion propulsion accommodations on DART first flight 4 DART Ion Propulsion Mission First flight of NASA NEXT-C ion engine . -
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. -
Astrocladistics of the Jovian Trojan Swarms
MNRAS 000,1–26 (2020) Preprint 23 March 2021 Compiled using MNRAS LATEX style file v3.0 Astrocladistics of the Jovian Trojan Swarms Timothy R. Holt,1,2¢ Jonathan Horner,1 David Nesvorný,2 Rachel King,1 Marcel Popescu,3 Brad D. Carter,1 and Christopher C. E. Tylor,1 1Centre for Astrophysics, University of Southern Queensland, Toowoomba, QLD, Australia 2Department of Space Studies, Southwest Research Institute, Boulder, CO. USA. 3Astronomical Institute of the Romanian Academy, Bucharest, Romania. Accepted XXX. Received YYY; in original form ZZZ ABSTRACT The Jovian Trojans are two swarms of small objects that share Jupiter’s orbit, clustered around the leading and trailing Lagrange points, L4 and L5. In this work, we investigate the Jovian Trojan population using the technique of astrocladistics, an adaptation of the ‘tree of life’ approach used in biology. We combine colour data from WISE, SDSS, Gaia DR2 and MOVIS surveys with knowledge of the physical and orbital characteristics of the Trojans, to generate a classification tree composed of clans with distinctive characteristics. We identify 48 clans, indicating groups of objects that possibly share a common origin. Amongst these are several that contain members of the known collisional families, though our work identifies subtleties in that classification that bear future investigation. Our clans are often broken into subclans, and most can be grouped into 10 superclans, reflecting the hierarchical nature of the population. Outcomes from this project include the identification of several high priority objects for additional observations and as well as providing context for the objects to be visited by the forthcoming Lucy mission. -
Phobos and Deimos: Planetary Protection Knowledge Gaps for Human Missions
Planetary Protection Knowledge Gaps for Human Extraterrestrial Missions (2015) 1007.pdf PHOBOS AND DEIMOS: PLANETARY PROTECTION KNOWLEDGE GAPS FOR HUMAN MISSIONS. Pascal Lee1,2,3 and Kira Lorber1,4, 1Mars Institute, NASA Ames Research Center, MS 245-3, Moffett Field, CA 94035-1000, USA, [email protected], 2SETI Institute, 3NASA ARC, 4University of Cincinnati.. Summary: Phobos and Deimos, Mars’ two moons, are associated with significant planetary protection knowledge gaps for human missions, that may be filled by a low cost robotic reconnaissance mission focused on elucidating their origin and volatile content. Introduction: Phobos and Deimos are currently considered to be potentially worthwhile destinations Figure 1: Deimos (left) and Phobos (right), to scale. for early human missions to Mars orbit, and possibly in Deimos is 15 km long, and Phobos, 27 km long. Both the context of longer term human Mars exploration moons have, to first order, a D-type spectrum: they are strategies as well [1] (Fig. 1). Until recently, it was very dark (albedo ~ 0.07) and very red. (NASA MRO). widely considered that planetary protection (PP) con- cerns associated with the exploration of Phobos and Extinct Comet Hypothesis. As a variant of the Deimos would be fundamentally no different from “captured small body from the outer main belt” hy- those associated with the exploration of primitive pothesis, it has long been suggested that Phobos and/or NEAs [2], as the preponderance of scientific evidence Deimos might be captured comet nuclei. (now inactive suggested that 1) there was never liquid water on Pho- or extinct). Consistent with this idea, some grooves on bos and Deimos, except possibly very early in their Phobos (those resembling crater chains, or catenas) are history; 2) there is no metabolically useful energy interpreted as fissures lined with vents through which source except near their heavily irradiated surface; 3) volatiles were once outgassed [3] (Fig. -
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. -
Dynamical Erosion of the Asteroid Belt and Implications for Large Impacts in the Inner Solar System
Icarus 207 (2010) 744–757 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Dynamical erosion of the asteroid belt and implications for large impacts in the inner Solar System David A. Minton *, Renu Malhotra Lunar and Planetary Laboratory, The University of Arizona, Tucson, AZ 85721, United States article info abstract Article history: The cumulative effects of weak resonant and secular perturbations by the major planets produce chaotic Received 15 September 2009 behavior of asteroids on long timescales. Dynamical chaos is the dominant loss mechanism for asteroids Revised 2 December 2009 with diameters D J 10 km in the current asteroid belt. In a numerical analysis of the long-term evolution Accepted 3 December 2009 of test particles in the main asteroid belt region, we find that the dynamical loss history of test particles Available online 11 December 2009 from this region is well described with a logarithmic decay law. In our simulations the loss rate function that is established at t 1 Myr persists with little deviation to at least t ¼ 4 Gyr. Our study indicates that Keywords: the asteroid belt region has experienced a significant amount of depletion due to this dynamical erosion— Asteroids having lost as much as 50% of the large asteroids—since 1 Myr after the establishment of the current Asteroids, Dynamics Cratering dynamical structure of the asteroid belt. Because the dynamical depletion of asteroids from the main belt is approximately logarithmic, an equal amount of depletion occurred in the time interval 10–200 Myr as in 0.2–4 Gyr, roughly 30% of the current number of large asteroids in the main belt over each interval. -
A Deep Search for Emission From" Rock Comet"(3200) Phaethon at 1 AU
Draft version November 23, 2020 Typeset using LATEX preprint style in AASTeX63 A Deep Search for Emission From \Rock Comet" (3200) Phaethon At 1 AU Quanzhi Ye (叶泉志),1 Matthew M. Knight,2, 1 Michael S. P. Kelley,1 Nicholas A. Moskovitz,3 Annika Gustafsson,4 and David Schleicher3 1Department of Astronomy, University of Maryland, College Park, MD 20742, USA 2Department of Physics, United States Naval Academy, 572C Holloway Rd, Annapolis, MD 21402, USA 3Lowell Observatory, 1400 W Mars Hill Road, Flagstaff, AZ 86001, USA 4Department of Astronomy and Planetary Science, P.O. Box 6010, Northern Arizona University, Flagstaff, AZ 86011, USA (Received -; Revised -; Accepted -) Submitted to PSJ ABSTRACT We present a deep imaging and spectroscopic search for emission from (3200) Phaethon, a large near-Earth asteroid that appears to be the parent of the strong Geminid meteoroid stream, using the 4.3 m Lowell Discovery Telescope. Observations were conducted on 2017 December 14{18 when Phaethon passed only 0.07 au from the Earth. We determine the 3σ upper level of dust and CN production rates to be 0.007{0.2 kg s−1 and 2:3 1022 molecule s−1 through narrowband imaging. A search × in broadband images taken through the SDSS r' filter shows no 100-m-class fragments in Phaethon's vicinity. A deeper, but star-contaminated search also shows no sign of fragments down to 15 m. Optical spectroscopy of Phaethon and comet C/2017 O1 (ASASSN) as comparison confirms the absence of cometary emission lines from 24 25 −1 Phaethon and yields 3σ upper levels of CN, C2 and C3 of 10 {10 molecule s , 2 orders of magnitude higher than the CN constraint placed∼ by narrowband imaging, due to the much narrower on-sky aperture of the spectrographic slit. -
Comet Hitchhiker
Comet Hitchhiker NIAC Phase I Final Report June 30, 2015 Masahiro Ono, Marco Quadrelli, Gregory Lantoine, Paul Backes, Alejandro Lopez Ortega, H˚avard Grip, Chen-Wan Yen Jet Propulsion Laboratory, California Institute of Technology David Jewitt University of California, Los Angeles Copyright 2015. All rights reserved. Mission Concept - Pre-decisional - for Planning and Discussion Purposes Only. This research was carried out in part at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration, and in part at University of California, Los Angeles. Comet Hitchhiker NASA Innovative Advanced Concepts Preface Yes, of course the Hitchhiker’s Guide to the Galaxy was in my mind when I came up with a concept of a tethered spacecraft hitching rides on small bodies, which I named Comet Hitchhiker. Well, this NASA-funded study is not exactly about traveling through the Galaxy; it is rather about exploring our own Solar System, which may sound a bit less exciting than visiting extraterrestrial civilizations, building a hyperspace bypass, or dining in the Restaurant at the End of the Universe. However, for the “primitive ape-descended life forms that have just begun exploring the universe merely a half century or so ago, our Solar System is still full of intellectually inspiring mysteries. So far the majority of manned and unmanned Solar System travelers solely depend on a fire breathing device called rocket, which is known to have terrible fuel efficiency. You might think there is no way other than using the gas-guzzler to accelerate or decelerate in an empty vacuum space.