MULTI-SCALE ANALYSIS of ALLUVIAL SEDIMENTARY OUTCROPS in UTAH USING EXOMARS 2020 PANCAM, ISEM, and CLUPI EMULATORS
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Pancam: a Multispectral Imaging Investigation on the NASA 2003 Mars Exploration Rover Mission
Sixth International Conference on Mars (2003) 3029.pdf Pancam: A Multispectral Imaging Investigation on the NASA 2003 Mars Exploration Rover Mission. J.F. Bell III1, S.W. Squyres1, K.E. Herkenhoff2, J. Maki3, M. Schwochert3, A. Dingizian3, D. Brown3, R.V. Morris4, H.M. Arneson1, M.J. Johnson1, J. Joseph1, J.N. Sohl-Dickstein1, and the Athena Science Team. 1Cornell University, Dept. of Astronomy, Ithaca NY 14853-6801; [email protected] , 2USGS Branch of Astrogeology, Flagstaff AZ 86001, 3JPL/Caltech, Pasadena CA 91109, 4NASA/JSC, Code SR, Houston TX 77058. Introduction: One of the six science payload ele- both cameras consist of identical 3-element symmetri- ments carried on each of the NASA Mars Exploration cal lenses with an effective focal length of 42 mm and Rovers (MER; Figure 1) is the Panoramic Camera a focal ratio of f/20, yielding an IFOV of 0.28 System, or Pancam. Pancam consists of three major mrad/pixel or a rectangular Field of View (FOV) of components: a pair of digital CCD cameras, the Pan- 16°× 16° per eye (Figures 3,4). The two eyes are sepa- cam Mast Assembly (PMA), and a radiometric cali- rated by 30 cm horizontally and have a 1° toe-in to bration target [1]. The PMA provides the azimuth and provide adequate parallax for stereo imaging (Figure elevation actuation for the cameras as well as a 1.5 5). The camera FOVs have been determined relative to meter high vantage point from which to image. The the adjacent wide-field stereo Navigation Cameras, and calibration target provides a set of reference color and the Mini-TES FOV. -
Exploration of Mars by the European Space Agency 1
Exploration of Mars by the European Space Agency Alejandro Cardesín ESA Science Operations Mars Express, ExoMars 2016 IAC Winter School, November 20161 Credit: MEX/HRSC History of Missions to Mars Mars Exploration nowadays… 2000‐2010 2011 2013/14 2016 2018 2020 future … Mars Express MAVEN (ESA) TGO Future ESA (ESA- Studies… RUSSIA) Odyssey MRO Mars Phobos- Sample Grunt Return? (RUSSIA) MOM Schiaparelli ExoMars 2020 Phoenix (ESA-RUSSIA) Opportunity MSL Curiosity Mars Insight 2020 Spirit The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export‐controlled information. Mars Express 2003-2016 … First European Mission to orbit another Planet! First mission of the “Rosetta family” Up and running since 2003 Credit: MEX/HRSC First European Mission to orbit another Planet First European attempt to land on another Planet Original mission concept Credit: MEX/HRSC December 2003: Mars Express Lander Release and Orbit Insertion Collission trajectory Bye bye Beagle 2! Last picture Lander after release, release taken by VMC camera Insertion 19/12/2003 8:33 trajectory Credit: MEX/HRSC Beagle 2 was found in January 2015 ! Only 6km away from landing site OK Open petals indicate soft landing OK Antenna remained covered Lessons learned: comms at all time! Credit: MEX/HRSC Mars Express: so many missions at once Mars Mission Phobos Mission Relay Mission Credit: MEX/HRSC Mars Express science investigations Martian Moons: Phobos & Deimos: Ionosphere, surface, -
Page 1 E X O M a R S E X O M a R S
NOTE ADDED BY JPL WEBMASTER: This document was prepared by the European Space Agency. The content has not been approved or adopted by, NASA, JPL, or the California Institute of Technology. This document is being made available for information purposes only, and any views and opinions expressed herein do not necessarily state or reflect those of NASA, JPL, or the California Institute of Technology. EE XX OO MM AA RR SS ExoMars Status th J. L. Vago and the ExoMars Project Team 20 MEPAG Meeting 3–4 March 2009, Arlington, VA (USA) ExoMars Original Objectives Technology Demonstration Objectives : Entry, Descent, and Landing (EDL) of a large payload on the surface of Mars; Surface mobility with a rover having several kilometres range; Access to the subsurface with a drill to acquire samples down to 2 metres; Automatic sample preparation and distribution for analysis with scientific instruments. Scientific Objectives (in order of priority): To search for signs of past and present life on Mars; To characterise the water/geochemical environment as a function of depth in the shallow subsurface; To study the surface environment and identify hazards to future human missions; To investigate the planet’s subsurface and deep interior to better understand its evolution and habitability. What is ExoMars Now? KEY REQUIREMENTS FOR EXOMARS : (but also for all future ESA Mars exploration missions) Clear synergy of technology and science goals: ExoMars has to land; ExoMars has to rove; ExoMars has to drill; ExoMars has to perform novel organics -
The Pancam Instrument for the Exomars Rover
ASTROBIOLOGY ExoMars Rover Mission Volume 17, Numbers 6 and 7, 2017 Mary Ann Liebert, Inc. DOI: 10.1089/ast.2016.1548 The PanCam Instrument for the ExoMars Rover A.J. Coates,1,2 R. Jaumann,3 A.D. Griffiths,1,2 C.E. Leff,1,2 N. Schmitz,3 J.-L. Josset,4 G. Paar,5 M. Gunn,6 E. Hauber,3 C.R. Cousins,7 R.E. Cross,6 P. Grindrod,2,8 J.C. Bridges,9 M. Balme,10 S. Gupta,11 I.A. Crawford,2,8 P. Irwin,12 R. Stabbins,1,2 D. Tirsch,3 J.L. Vago,13 T. Theodorou,1,2 M. Caballo-Perucha,5 G.R. Osinski,14 and the PanCam Team Abstract The scientific objectives of the ExoMars rover are designed to answer several key questions in the search for life on Mars. In particular, the unique subsurface drill will address some of these, such as the possible existence and stability of subsurface organics. PanCam will establish the surface geological and morphological context for the mission, working in collaboration with other context instruments. Here, we describe the PanCam scientific objectives in geology, atmospheric science, and 3-D vision. We discuss the design of PanCam, which includes a stereo pair of Wide Angle Cameras (WACs), each of which has an 11-position filter wheel and a High Resolution Camera (HRC) for high-resolution investigations of rock texture at a distance. The cameras and electronics are housed in an optical bench that provides the mechanical interface to the rover mast and a planetary protection barrier. -
Mars Surface Context Cameras Past, Present, and Future 10.1002/2016EA000166 M
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Aberystwyth Research Portal Aberystwyth University Mars surface context cameras past, present and future Gunn, Matthew; Cousins, Claire Published in: Earth and Space Science DOI: 10.1002/2016EA000166 Publication date: 2016 Citation for published version (APA): Gunn, M., & Cousins, C. (2016). Mars surface context cameras past, present and future. Earth and Space Science, 3(4), 144-162. https://doi.org/10.1002/2016EA000166 Document License CC BY-NC-ND General rights Copyright and moral rights for the publications made accessible in the Aberystwyth Research Portal (the Institutional Repository) are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. • Users may download and print one copy of any publication from the Aberystwyth Research Portal for the purpose of private study or research. • You may not further distribute the material or use it for any profit-making activity or commercial gain • You may freely distribute the URL identifying the publication in the Aberystwyth Research Portal Take down policy If you believe that this document breaches copyright please contact us providing details, and we will remove access to the work immediately and investigate your claim. tel: +44 1970 62 2400 email: [email protected] Download date: 09. Jul. 2020 PUBLICATIONS Earth and Space Science REVIEW Mars surface context cameras past, present, and future 10.1002/2016EA000166 M. D. Gunn1 and C. R. Cousins2 Key Points: 1Institute of Maths, Physics and Computer Science, Aberystwyth University, Aberystwyth, UK, 2Department of Earth and • Camera systems have been a core component of all instrument payloads Environmental Sciences, Irvine Building, University of St Andrews, St. -
Exomars Trace Gas Orbiter
EE XX OO MM AA RR SS POCKOCMOC The ExoMars Programme NASA PPS G. Kminek, J. L. Vago, O. Witasse, and the ExoMars Team 12–13 November 2013, GSFC 1 (USA) Cooperation EE XX OO MM AA RR SS POCKOCMOC ExoMars Programme • Consists of two missions, in 2016 and 2018. • A cooperation between ESA and Roscosmos (agreement signed in Mar 2013). • The programme includes some important contributions from NASA. • ExoMars constitutes ESA’s highest priority in robotic exploration. Credit: MEX/HRSC 2 2016 Mission Objectives EE XX OO MM AA RR SS TECHNOLOGY OBJECTIVE ‣ Entry, Descent, and Landing (EDL) of a payload on the surface of Mars. 2016 SCIENTIFIC OBJECTIVES ‣ To study Martian atmospheric trace gases and their sources; ‣ To conduct surface environment measurements. ➔ ‣ Data relay services for landed missions until 2022. Credit: MEX/HRSC 3 Trace Gas Orbiter EE XX OO MM AA RR SS NOMAD Atmospheric composition High-resolution occultation (CH4, O3, trace species, isotopes) dust, clouds, P&T profiles and nadir spectrometers 0.2 0.5 1 2 5 10 20 UVIS (0.20 – 0.65 μm) λ/Δλ 250 SO Limb Nadir Wavelength (μm) ∼ IR (2.3 – 3.8 μm) λ/Δλ 10,000 SO Limb Nadir ∼ NOMAD nadir Date 4 Apr 2008 13:33:04 Ls=154 IR (2.3 – 4.3 μm) λ/Δλ 20,000 SO spatial resolution 60°N ∼ CaSSIS Mapping of sources High-resolution, stereo camera Landing site selection 30°N ACS Atmospheric chemistry, aerosols, 0°N Suite of 3 high-resolution surface T, structure spectrometers Background CH4 map, 30°S Mumma et al. -
Russian Part Exomars Is a Joint Project of Mars Exploration Implemented
25/09/2014 Press Center, Space Research Institute (IKI) Russian Academy of Sciences ExoMars: Russian part ExoMars is a joint project of Mars exploration implemented under bilateral Agreement between European Space Agency (ESA) and Federal Space Agency (Roscosmos). The scope of cooperation is unprecedented in the history of both agencies. One of the crucial elements is joint Earth-based interplanetary mission operation and data control complex, which is planned to be built within the program. Russian and European experts are striving to consolidate their experience to develop new technologies for interplanetary missions. ExoMars is also one of the steps toward manned exploration of Mars. Two missions are foreseen within the ExoMars programme: one consisting of an Orbiter plus an Entry, Descent and Landing Demonstrator Module, to be launched in 2016, and the other, featuring a rover, with a launch date of 2018. Both missions will be carried out in cooperation with Roscosmos. Bilateral cooperation started in 2012, when Roscosmos became the main partner of ESA on the project (Declaration of Intent was signed by ESA and Roscosmos for cooperation on the ExoMars programme in April 2012) under the condition that Russia is a full participant of the mission's second stage. Russian part includes: - launchers for both stages of the mission; - scientific instruments for both stages of the mission; - lander module for the second stage of the mission (2018), to be built by Lavochkin Space Association (Khimki, Moscow Region), part of the United Rocket and Space Corporation. Space Research Institute of the Russian Academy of Sciences (IKI for short) is a head organisation for scientific payload of ExoMars project. -
Stratigraphic Correlation Via Opportunity's Pancam of the Burns Formation, Meridiani Planum, Mars
Seventh International Conference on Mars 3389.pdf Stratigraphic Correlation via Opportunity's Pancam of the Burns Formation, Meridiani Planum, Mars. S. D. Thompson1, W. M. Calvin1, and the Athena Science Team, 1Dept. of Geological Sciences MS-172, University of Nevada, Reno, Reno NV 89557-0180 ([email protected]). Introduction: For over three Earth years the deposits are volcanic air fall ash layers even though Mars Exploration Rover, Opportunity, has no recognizable construct is visible in the region. investigated, via remote sensing and in situ The site occurrence of the Meridiani Planum observations, an extensive occurrence of hematite sediments being basaltic-andesitic in composition and sulfate-salt rich sedimentary bedrock exposures with ~10-15% hematite are consistent with a volcanic in crater walls and plains surfaces [1]. These origin, however there are no sizeable volcanic observations have occurred over ~10 kilometers of constructs in the region [8]. It is possible that the traverse odometry from the landing site to Victoria crater (Figure 1). The sedimentary bedrock has been named the Burns formation in honor of Roger Burns, who predicted sulfate deposits on Mars, particularly in the form of jarosite. Farrand et al. [2] have described the major spectral properties of the Burns formation in the craters Eagle and Endurance as observed by Pancam. Grotzinger et al. [3] and McLennan et al. [4] have described the stratigraphic record based on primary and secondary structures. This analysis looks at Pancam multispectral data acquired during Opportunity’s mission from landing to sol 1037. We analyzed nearby (<~10 m) rock targets with Pancam where sufficient spatial resolution (<10 mm) is achieved to obtain spectral parameters of individual sedimentary structures as well as erosional and possible secondary diagenetic features (i.e., fracture fill and rind materials). -
The WISDOM Radar: Unveiling the Subsurface Beneath the Exomars Rover and Identifying the Best Locations for Drilling
Open Research Online The Open University’s repository of research publications and other research outputs The WISDOM Radar: Unveiling the Subsurface Beneath the ExoMars Rover and Identifying the Best Locations for Drilling Journal Item How to cite: Ciarletti, Valérie; Clifford, Stephen; Plettemeyer, Dirk; LeGall, Alice; Hervé, Yann; Dorizon, Sophie; Quantin- Nataf, Cathy; Benedix, Wolf-Stefan; Schwenzer, Susanne; Pettinelli, Elena; Heggy, Essam; Herique, Alain; Berthellier, Jean-Jacques; Kofman, Wlodek; Vago, Jorge L.; Hamran, Svein-Erik and WISDOM team, . (2017). The WISDOM Radar: Unveiling the Subsurface Beneath the ExoMars Rover and Identifying the Best Locations for Drilling. Astrobiology, 17(6-7) pp. 565–584. For guidance on citations see FAQs. c 2017 The Authors https://creativecommons.org/licenses/by-nc-nd/4.0/ Version: Version of Record Link(s) to article on publisher’s website: http://dx.doi.org/doi:10.1089/ast.2016.1532 Copyright and Moral Rights for the articles on this site are retained by the individual authors and/or other copyright owners. For more information on Open Research Online’s data policy on reuse of materials please consult the policies page. oro.open.ac.uk ASTROBIOLOGY ExoMars Rover Mission Volume 17, Numbers 6 and 7, 2017 Mary Ann Liebert, Inc. DOI: 10.1089/ast.2016.1532 The WISDOM Radar: Unveiling the Subsurface Beneath the ExoMars Rover and Identifying the Best Locations for Drilling Vale´rie Ciarletti,1 Stephen Clifford,2 Dirk Plettemeier,3 Alice Le Gall,1 Yann Herve´,1 Sophie Dorizon,1 Cathy Quantin-Nataf,4 Wolf-Stefan Benedix,3 Susanne Schwenzer,5 Elena Pettinelli,6 Essam Heggy,7 Alain Herique,8 Jean-Jacques Berthelier,1 Wlodek Kofman,8,11 Jorge L. -
Embedding Sensor Visualization in Martian Terrain Reconstructions
EMBEDDING SENSOR VISUALIZATION IN MARTIAN TERRAIN RECONSTRUCTIONS Gerhard Paar (1), Gerd Hesina (2), Christoph Traxler (2), Valérie Ciarletti (3), Dirk Plettemeier (4), Christoph Statz (4), Kathrin Sander (1), Bernhard Nauschnegg (1) (1) JOANNEUM RESEARCH, Austria, Email: (gerhard.paar|kathrin.sander|bernhard.nauschnegg)@joanneum.at (2) VRVis Forschungs GmbH, Austria, Email: (hesina|traxler)@vrvis.at (3) UVSQ (UPSay); UPMC (Sorbonne Univ.); CNRS/INSU; LATMOS-IPSL, France , Email: [email protected] (4) Technische Universität Dresden, Germany, Email: (christoph.statz|dirk.plettemeier)@tu-dresden.de ABSTRACT terrain reconstructed from PanCam stereo imagery: PanCam is a part of the ExoMars on-board scientific The PASTEUR payload on the ESA ExoMars Rover sensors’ suite PASTEUR [2]. Based on PanCam- 2018 contains a panoramic imaging system (PanCam) provided 3D models in the context of the PASTEUR specifically designed for visual characterization of the data exploitation it is possible / necessary to Rover’s surroundings and remote detection of potential simultaneously visualize different sensors’ data within sample sites. PanCam with its wide angle stereo camera the 3D scene in joint consistent geometry. This pair WAC (Wide Angle Camera) and the narrow angle preserves the geospatial context and enables a combined HRC (High Resolution Camera) provides data for 3D perception of topographic and physical properties, reconstruction of the Rover’s environment which is fed thereby providing a valuable additional tool for in-depth into a real-time rendering suite to allow virtual scientific analysis. representations for scientific investigations and planning. One of the other PASTEUR sensors is In particular, data from the WISDOM (Water Ice WISDOM (Water Ice and Subsurface Deposit Subsurface Deposit Observation on Mars, [10]) ground Observation On Mars), a ground penetrating radar that penetrating radar (GPR) was considered for this kind of will allow the definition and representation of suitable embedded visualization. -
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Open Research Online The Open University’s repository of research publications and other research outputs The Aeolian Environment of the Landing Site for the ExoMars Rosalind Franklin Rover in Oxia Planum, Mars Journal Item How to cite: Favaro, E.A.; Balme, M.R.; Davis, J.; Grindrod, P.M; Fawdon, P.; Barrett, A.M. and Lewis, S.R. (2021). The Aeolian Environment of the Landing Site for the ExoMars Rosalind Franklin Rover in Oxia Planum, Mars. Journal of Geophysical Research: Planets, 126(4), article no. e2020JE006723. For guidance on citations see FAQs. c 2021 E. A. Favaro et al https://creativecommons.org/licenses/by/4.0/ Version: Version of Record Link(s) to article on publisher’s website: http://dx.doi.org/doi:10.1029/2020je006723 Copyright and Moral Rights for the articles on this site are retained by the individual authors and/or other copyright owners. For more information on Open Research Online’s data policy on reuse of materials please consult the policies page. oro.open.ac.uk RESEARCH ARTICLE The Aeolian Environment of the Landing Site for the 10.1029/2020JE006723 ExoMars Rosalind Franklin Rover in Oxia Planum, Mars Key Points: E. A. Favaro1 , M. R. Balme1 , J. M. Davis2 , P. M. Grindrod2 , P. Fawdon1 , • Multiple wind regimes have A. M. Barrett1 , and S. R. Lewis1 influenced the surficial expression of Oxia Planum 1School of Physical Sciences, Open University, Milton Keynes, UK, 2Department of Earth Sciences, Natural History • Transverse aeolian ridges (TARs), periodic bedrock ridges, dust devils, Museum, London, UK and windstreaks were used to determine formative wind directions • Landscape evidence and climate Abstract Aeolian features at Oxia Planum—the 2023 landing site for the ExoMars Rosalind Franklin modeling suggest contemporary Rover (ERFR)—are important for Mars exploration because they record information about past and winds lack the necessary strength to mobilize TAR-forming materials current wind regimes, sand transport vectors, and lend insight to the abrasion, deposition, and transport of granular material. -
The Exomars Programme
EE XX OO MM AA RR SS POCKOCMOC The ExoMars Programme O. Witasse, J. L. Vago, and D. Rodionov 1 June 2014 ESTEC, NOORDWIJK, THE NETHERLANDS 2000-2010 2011 2013 2016 2018 2020 + Mars Sample Odyssey Return TGO MRO (ESA-NASA) MAVEN Mars Express (ESA) MOM India Phobos-Grunt ExoMars MER Phoenix Mars Science Lab MSL2010 Insight MER The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export-controlled information. 4 Cooperation EE XX OO MM AA RR SS POCKOCMOC 5 ExoMars Programme Objectives 1. Technology Demonstration 2. Science 3. Relay orbiter ESA UNCLASSIFIED – For Official Use 6 ExoMars Programme Objectives Technology Demonstration Objectives Entry, Descent and Landing (EDL) on the Mars’ surface Mobility on Mars surface (several kilometres) Access to Mars sub-surface (2 metres) Scientific Objectives To search for signs of past and present life on Mars To characterise the water/geochemical environment as a function of depth in the shallow subsurface To study the surface environment and identify hazards to future human missions Atmosphere characterisation – Trace Gas detection Programmatic Objective Provide link communication to Mars landed surface assets ESA UNCLASSIFIED – For Official Use 7 Programme Overview Two missions launched in 2016 and 2018, respectively The 2016 flight segment consists of a Trace Gas Orbiter (TGO) and an EDL Demonstrator Module (EDM) The 2018 flight segment consists of a Carrier Module (CM) and a Descent Module (DM) with a Rover and a stationary Landing Platform 2016 Mission & 2018 Mission Trace Gas Orbiter (TGO) Carrier Module Descent Module (CM) (DM) ESA ESTRACK Roscosmos Ground Segment Antennas Landing EDL Demonstrator Module Platform Rover (EDM) ESA UNCLASSIFIED – For Official Use NASA DSN 8 Proton M/Breeze M Proton M/Breeze M ESA UNCLASSIFIED – For Official Use 9 2016 Mission Objectives EE XX OO MM AA RR SS TECHNOLOGY OBJECTIVE ‣Entry, Descent, and Landing (EDL) of a payload on the surface of Mars.