Phobos State of Knowledge and Rationales for Future Exploration
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Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 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. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes. -
Martian Crater Morphology
ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter. -
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. -
Workshop on the Martiannorthern Plains: Sedimentological,Periglacial, and Paleoclimaticevolution
NASA-CR-194831 19940015909 WORKSHOP ON THE MARTIANNORTHERN PLAINS: SEDIMENTOLOGICAL,PERIGLACIAL, AND PALEOCLIMATICEVOLUTION MSATT ..V",,2' :o_ MarsSurfaceandAtmosphereThroughTime Lunar and PlanetaryInstitute 3600 Bay AreaBoulevard Houston TX 77058-1113 ' _ LPI/TR--93-04Technical, Part 1 Report Number 93-04, Part 1 L • DISPLAY06/6/2 94N20382"£ ISSUE5 PAGE2088 CATEGORY91 RPT£:NASA-CR-194831NAS 1.26:194831LPI-TR-93-O4-PT-ICNT£:NASW-4574 93/00/00 29 PAGES UNCLASSIFIEDDOCUMENT UTTL:Workshopon the MartianNorthernPlains:Sedimentological,Periglacial, and PaleoclimaticEvolution TLSP:AbstractsOnly AUTH:A/KARGEL,JEFFREYS.; B/MOORE,JEFFREY; C/PARKER,TIMOTHY PAA: A/(GeologicalSurvey,Flagstaff,AZ.); B/(NationalAeronauticsand Space Administration.GoddardSpaceFlightCenter,Greenbelt,MD.); C/(Jet PropulsionLab.,CaliforniaInst.of Tech.,Pasadena.) PAT:A/ed.; B/ed.; C/ed. CORP:Lunarand PlanetaryInst.,Houston,TX. SAP: Avail:CASIHC A03/MFAOI CIO: UNITEDSTATES Workshopheld in Fairbanks,AK, 12-14Aug.1993;sponsored by MSATTStudyGroupandAlaskaUniv. MAJS:/*GLACIERS/_MARSSURFACE/*PLAINS/*PLANETARYGEOLOGY/*SEDIMENTS MINS:/ HYDROLOGICALCYCLE/ICE/MARS CRATERS/MORPHOLOGY/STRATIGRAPHY ANN: Papersthathavebeen acceptedforpresentationat the Workshopon the MartianNorthernPlains:Sedimentological,Periglacial,and Paleoclimatic Evolution,on 12-14Aug. 1993in Fairbanks,Alaskaare included.Topics coveredinclude:hydrologicalconsequencesof pondedwateron Mars; morpho!ogical and morphometric studies of impact cratersin the Northern Plainsof Mars; a wet-geology and cold-climateMarsmodel:punctuation -
Thermokarst Features in Lyot Crater, Mars: Implications for Recent Surface Water Freeze-Thaw, Flow, and Cycling
Late Mars Workshop 2018 (LPI Contrib. No. 2088) 5018.pdf THERMOKARST FEATURES IN LYOT CRATER, MARS: IMPLICATIONS FOR RECENT SURFACE WATER FREEZE-THAW, FLOW, AND CYCLING. N. Glines1,2 and V. Gulick1, 1The SETI Institute / NASA Ames (MS239-20, Moffett Field, CA 94035, [email protected], [email protected]), 2 UCSC. Introduction: We previously reported [7, 10] on ESP_055252_2310 were acquired in May, 2018. The the identification of potential thermokarst depressions terrain surrounding the beads is warped, similar to connected by channel systems on the floor of Lyot dissected mantle, while the bead floors are more Crater (Fig.1, mapped in Fig.2). At first glance, these smooth and flat, with less dissection. circular depressions on the floor of Lyot resemble curiously eroded terrain or secondary crater clusters. However, closer inspection reveals these depressions are flat-floored, circular-to-oblong features without raised rims or ejecta, connected by channels. We determined that these features are morphologically similar to terrestrial thermokarst basins and channels known as paleo-beaded streams. Here, we report a possible paleolake, associated landform assemblages, and the potential for hydrologic cycling. Figure 1: These flat-floored, round depressions connected by channels trend downslope (left to right) on the floor of Lyot Crater. HiRISE image ESP_052628_2310. Analog Beaded Streams. Beaded streams are Figure 2: Map of beaded channels (blue) N/NW of the central peak, gullies (red), potential inverted material and primarily found in circum-arctic tundra with ice deposit (pink), & lake level indicators (dashed green). saturated substrates. Beaded streams are thermokarst Craters are white circles. -
Widespread Crater-Related Pitted Materials on Mars: Further Evidence for the Role of Target Volatiles During the Impact Process ⇑ Livio L
Icarus 220 (2012) 348–368 Contents lists available at SciVerse ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Widespread crater-related pitted materials on Mars: Further evidence for the role of target volatiles during the impact process ⇑ Livio L. Tornabene a, , Gordon R. Osinski a, Alfred S. McEwen b, Joseph M. Boyce c, Veronica J. Bray b, Christy M. Caudill b, John A. Grant d, Christopher W. Hamilton e, Sarah Mattson b, Peter J. Mouginis-Mark c a University of Western Ontario, Centre for Planetary Science and Exploration, Earth Sciences, London, ON, Canada N6A 5B7 b University of Arizona, Lunar and Planetary Lab, Tucson, AZ 85721-0092, USA c University of Hawai’i, Hawai’i Institute of Geophysics and Planetology, Ma¯noa, HI 96822, USA d Smithsonian Institution, Center for Earth and Planetary Studies, Washington, DC 20013-7012, USA e NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA article info abstract Article history: Recently acquired high-resolution images of martian impact craters provide further evidence for the Received 28 August 2011 interaction between subsurface volatiles and the impact cratering process. A densely pitted crater-related Revised 29 April 2012 unit has been identified in images of 204 craters from the Mars Reconnaissance Orbiter. This sample of Accepted 9 May 2012 craters are nearly equally distributed between the two hemispheres, spanning from 53°Sto62°N latitude. Available online 24 May 2012 They range in diameter from 1 to 150 km, and are found at elevations between À5.5 to +5.2 km relative to the martian datum. The pits are polygonal to quasi-circular depressions that often occur in dense clus- Keywords: ters and range in size from 10 m to as large as 3 km. -
Bethany L. Ehlmann California Institute of Technology 1200 E. California Blvd. MC 150-21 Pasadena, CA 91125 USA Ehlmann@Caltech
Bethany L. Ehlmann California Institute of Technology [email protected] 1200 E. California Blvd. Caltech office: +1 626.395.6720 MC 150-21 JPL office: +1 818.354.2027 Pasadena, CA 91125 USA Fax: +1 626.568.0935 EDUCATION Ph.D., 2010; Sc. M., 2008, Brown University, Geological Sciences (advisor, J. Mustard) M.Sc. by research, 2007, University of Oxford, Geography (Geomorphology; advisor, H. Viles) M.Sc. with distinction, 2005, Univ. of Oxford, Environ. Change & Management (advisor, J. Boardman) A.B. summa cum laude, 2004, Washington University in St. Louis (advisor, R. Arvidson) Majors: Earth & Planetary Sciences, Environmental Studies; Minor: Mathematics International Baccalaureate Diploma, Rickards High School, Tallahassee, Florida, 2000 Additional Training: Nordic/NASA Summer School: Water, Ice and the Origin of Life in the Universe, Iceland, 2009 Vatican Observatory Summer School in Astronomy &Astrophysics, Castel Gandolfo, Italy, 2005 Rainforest to Reef Program: Marine Geology, Coastal Sedimentology, James Cook Univ., Australia, 2004 School for International Training, Development and Conservation Program, Panamá, Sept-Dec 2002 PROFESSIONAL EXPERIENCE Professor of Planetary Science, Division of Geological & Planetary Sciences, California Institute of Technology, Assistant Professor 2011-2017, Professor 2017-present; Associate Director, Keck Institute for Space Studies 2018-present Research Scientist, Jet Propulsion Laboratory, California Institute of Technology, 2011-2020 Lunar Trailblazer, Principal Investigator, 2019-present MaMISS -
The Population of Secondary Impact Craters on Mars
THE POPULATION OF SECONDARY IMPACT CRATERS ON MARS. S.J. Robbins1 and B.M. Hynek1,2, 1LASP, 3665 Discovery Dr., University of Colorado, Boulder, CO 80309, 2Geological Sciences Department, UCB 399, University of Colorado, Boulder, CO 80309. [email protected] Introduction: Impact craters are the most ubiqui- tor of the primary crater population because, like sec- tous exogenic feature on planetary surfaces in the solar ondaries, they form in a geologic instant and are tightly system. They have innumerable applications, but one clustered spatially. Ergo, their removal – or an esti- of their primary utilities is to model surface ages: if mate of what crater would have formed from an intact there are more craters per unit area on one surface, primary – would also be necessary for applications of then it is older than another with fewer craters. This primary craters such as age-modeling. very basic method requires the assumption that the Analysis: To determine a "global" value for the craters formed spatially randomly and stochastically dominance of secondaries, two incremental crater size- with time. Unfortunately, secondary impact craters frequency distributions (SFDs) were calculated – one belie both these assumptions: They form in a geologic for primaries and one for secondaries. If the secondar- instant from cohesive ejecta blocks launched by a pri- ies' SFD intersected and grew larger than the primaries' mary impact ("primary"), and while they may be spa- at any diameter, that would be considered the transition tially correlated with that primary, this is not always diameter. To calculate this on a more useful regional the case. -
Roving on Phobos: Challenges of the Mmx Rover for Space Robotics
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Institute of Transport Research:Publications ROVING ON PHOBOS: CHALLENGES OF THE MMX ROVER FOR SPACE ROBOTICS Jean Bertrand (1), Simon Tardivel (1), Frans IJpelaan (1), Emile Remetean (1), Alex Torres (1), Stéphane Mary (1), Maxime Chalon (2), Fabian Buse (2), Thomas Obermeier (2), Michal Smisek (2), Armin Wedler (2), Joseph Reill (2), Markus Grebenstein (2) (1) CNES, 18 avenue Edouard Belin 31401 Toulouse Cedex 9 (France), [email protected] (2) DLR, Münchener Straße 20 82234 Weßling (Germany), [email protected] ABSTRACT Once on the surface, the rover would deploy and upright itself from its stowed position and orientation, and carry This paper presents a small rover for exploration mission out several science objectives over the course of a few dedicated to the moons of Mars, Phobos and Deimos. months. In October 2018, CNES and DLR have This project is a collaboration between JAXA for the expressed their interest in partnering together on this mother spacecraft, and a cooperative contribution of project and the MMX rover is now a joint project of both CNES and DLR to provide a rover payload. organizations in tight cooperation. After a description of the MMX mission defined by JAXA, this paper presents This rover will be different in many aspects compared to the Phobos environment. Then, it details the mission the existing ones. It will have to drive in a very low constraints and the rover objectives. It outlines some gravity with only little power given by the solar arrays. -
Information to Users
RELATIVE AGES AND THE GEOLOGIC EVOLUTION OF MARTIAN TERRAIN UNITS (MARS, CRATERS). Item Type text; Dissertation-Reproduction (electronic) Authors BARLOW, NADINE GAIL. Publisher The University of Arizona. Rights Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author. Download date 06/10/2021 23:02:22 Link to Item http://hdl.handle.net/10150/184013 INFORMATION TO USERS While the most advanced technology has been used to photograph and reproduce this manuscript, the quality of the reproduction is heavily dependent upon the quality of the material submitted. For example: • Manuscript pages may have indistinct print. In such cases, the best available copy has been filmed. o Manuscripts may not always be complete. In such cases, a note will indicate that it is not possible to obtain missing pages. • Copyrighted material may have been removed from the manuscript. In such cases, a note will indicate the deletion. Oversize materials (e.g., maps, drawings, and charts) are photographed by sectioning the original, beginning at the upper left-hand corner and continuing from left to right in equal sections with small overlaps. Each oversize page is also filmed as one exposure and is available, for an additional charge, as a standard 35mm slide or as a 17"x 23" black and white photographic print. Most photographs reproduce acceptably on positive microfilm or microfiche but lack the clarity on xerographic copies made from the microfilm. -
Large Impact Crater Histories of Mars: the Effect of Different Model Crater Age Techniques ⇑ Stuart J
Icarus 225 (2013) 173–184 Contents lists available at SciVerse ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Large impact crater histories of Mars: The effect of different model crater age techniques ⇑ Stuart J. Robbins a, , Brian M. Hynek a,b, Robert J. Lillis c, William F. Bottke d a Laboratory for Atmospheric and Space Physics, 3665 Discovery Drive, University of Colorado, Boulder, CO 80309, United States b Department of Geological Sciences, 3665 Discovery Drive, University of Colorado, Boulder, CO 80309, United States c UC Berkeley Space Sciences Laboratory, 7 Gauss Way, Berkeley, CA 94720, United States d Southwest Research Institute and NASA Lunar Science Institute, 1050 Walnut Street, Suite 300, Boulder, CO 80302, United States article info abstract Article history: Impact events that produce large craters primarily occurred early in the Solar System’s history because Received 25 June 2012 the largest bolides were remnants from planet ary formation .Determi ning when large impacts occurred Revised 6 February 2013 on a planetary surface such as Mars can yield clues to the flux of material in the early inner Solar System Accepted 25 March 2013 which, in turn, can constrain other planet ary processes such as the timing and magnitude of resur facing Available online 3 April 2013 and the history of the martian core dynamo. We have used a large, global planetary databas ein conjunc- tion with geomorpholog icmapping to identify craters superposed on the rims of 78 larger craters with Keywords: diameters D P 150 km on Mars, 78% of which have not been previously dated in this manner. -
Final Report for a Robotic Exploration Mission to Mars and Phobos Argos
NASA-CR-197168 NASw-4435 /'/F/ 4 '_/e'7 t'/-q 1- Final Report for a Robotic Exploration Mission to Mars and Phobos PROJECT AENEAS Response to RFP Number ASE274L.0893 o r,4 u_ 4" submitted to: I ,-- ,0 U i'_ C_ e" 0 Z _ 0 Dr. George Botbyl The University of Texas at Austin Department of Aerospace Engineering and Engineering Mechanics Austin, Texas 78712 Z cn _. submitted by: 0 cO_ 0 Argos Space Endeavours 29 November 1993 zxI_f _rOos 8Face _.aea_ours _roJect Aeneas CDestBn _"eam Fall 1993 Chief Executive Officer Justin H. Kerr Chief Engineer Erin Defoss6 Chief Administrator Quang Ho Engineers Emisto Barriga Grant Davis Steve McCourt Matt Smith Aeneas Project Preliminary Design of a Robotic Exploration Mission to Mars and Phobos Approved: Justin H. Kerr CEO, Argos Space Endeavours Approved: Erin Defoss6 Chief Engineer, Argos Space Endeavours Approved: Quang Ho Administrative Officer, Argos Space Endeavours Argos 8pace q .aca ours University of Texas at Austin Department of Aerospace Engineering and Engineering Mechanics November 1993 Acknowledgments Argos Space Endeavours would like to thank all personnel at The University and in industry who made Project Aeneas possible. This project was conducted with the support of the NASA/USRA Advanced Design Program. Argos Space Endeavours wholeheartedly thanks the following faculty, staff, and students from the University of Texas at Austin: Dr. Wallace Fowler, Dr. Ronald Stearman, Dr. John Lundberg, Professor Richard Drury, Dr. David Dolling, Ms. Kelly Spears, Mr. Elfego Piton, Mr. Tony Economopoulos, and Mr. David Garza. The support of Project Aeneas from the aerospace industry was overwhelming.