Examinando por Autor "Lasue, J."

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Acceso Abierto
First detection of visible-wavelength aurora on Mars
(Europlanet, 2024-07-03) Wright Knutsen, Elise; McConnochie, Tim H.; Lemmon, M. T.; Tamppari, L. K.; Viet, Shayla; Cousin, Agnes; Wiens, Roger C.; Francis, R.; Donaldson, Chris; Lasue, J.; Forni, O.; Patel, P.; Schneider, Nick; Toledo, D.; Apéstigue, V.
Auroras are hallmarks of the interaction between solar particles and the atmosphere of planets. Martian aurora was first discovered in 2005, since then, four different types have been identified: localized discreet aurora (Bertaux et al., 2005), global diffuse aurora (Schneider et al., 2015), dayside proton aurora (Deighan et al., 2018), and large-scale sinuous aurora (Lillis et al., 2022). All previous detections have been made in the UV from orbit. Here we present, from observations with the SuperCam and MastCam-Z instruments on the Mars 2020 Perseverance rover, the first detection of aurora from the Martian surface and the first detection of the green 557.7 nm atomic oxygen auroral emission on Mars. This is the same emission line that is familiar from terrestrial aurora. Charged particles accelerated by interplanetary coronal mass ejections (ICMEs) or solar flares are referred to as solar energetic particles (SEPs) (Reames, 1999). Diffuse aurora is strongly correlated with SEP events. ICME-accelerated SEPs travel nearly radially, as opposed to flare-accelerated SEPs which follow the Parker spiral. If the solar source region is identified, ICME-accelerated SEP events at Mars, and thus diffuse aurora, can be forecasted. The dynamic nature of rover planning and operations allows for a reactive observation strategy that takes advantage of such forecasts. We made several attempts, starting in May 2023, to react to SEP events and observe with the M2020 rover (Farley et al., 2020) instruments at times when we believed the likelihood of emission to be highest. Our fourth attempt, in March 2024, yielded the positive detection reported here.
Restringido
Joint Europa Mission (JEM): a multi-scale study of Europa to characterize its habitability and search for extant life
(Elsevier BV, 2020-11-15) Blanc, M.; Prieto-Ballesteros, Olga; André, N.; Gómez Elvira, J.; Jones, G.; Sterken, V.; Desprats, W.; Gurvits, L. I.; Khurana, K.; Balmino, G.; Blöcker, A.; Broquet, R.; Bunce, E.; Cavel, C.; Choblet, G.; Colins, G.; Coradini, M.; Cooper, J.; Dirkx, D.; Fontaine, D.; Garnier, P.; Gaudin, D.; Hartogh, P.; Hussmann, H.; Genova, A.; Less, L.; Jäggi, A.; Kempf, S.; Krupp, N.; Lara, L.; Lasue, J.; Lainey, V.; Leblanc, F.; Lebreton, J. P.; Longobardo, A.; Lorenz, R.; Martins, P.; Martins, Z.; Marty, J. C.; Masters, A.; Mimoun, D.; Palumba, E.; Parro García, V.; Regnier, P.; Saur, J.; Schutte, A.; Sittler, E. C.; Spohn, T.; Srama, R.; Stephan, K.; Szego, K.; Tosi, F.; Vance, S.; Wagner, R.; Van Hoolst, T.; Volwerk, M.; Wahlund, J. E.; Westall, Frances; Wurz, P.; Ministerio de Economía y Competitividad (MINECO); Agencia Estatal de Investigación (AEI); 0000-0003-4002-2434; 0000-0002-2278-1210; 0000-0002-1797-2741; 0000-0002-9820-8584; Unidad de Excelencia Científica María de Maeztu Centro de Astrobiología del Instituto Nacional de Técnica Aeroespacial y CSIC, MDM-2017-0737
Europa is the closest and probably the most promising target to search for extant life in the Solar System, based on complementary evidence that it may fulfil the key criteria for habitability: the Galileo discovery of a sub-surface ocean; the many indications that the ice shell is active and may be partly permeable to transfer of chemical species, biomolecules and elementary forms of life; the identification of candidate thermal and chemical energy sources necessary to drive a metabolic activity near the ocean floor. In this article we are proposing that ESA collaborates with NASA to design and fly jointly an ambitious and exciting planetary mission, which we call the Joint Europa Mission (JEM), to reach two objectives: perform a full characterization of Europa's habitability with the capabilities of a Europa orbiter, and search for bio-signatures in the environment of Europa (surface, subsurface and exosphere) by the combination of an orbiter and a lander. JEM can build on the advanced understanding of this system which the missions preceding JEM will provide: Juno, JUICE and Europa Clipper, and on the Europa lander concept currently designed by NASA (Maize, report to OPAG, 2019). We propose the following overarching goals for our Joint Europa Mission (JEM): Understand Europa as a complex system responding to Jupiter system forcing, characterize the habitability of its potential biosphere, and search for life at its surface and in its sub-surface and exosphere. We address these goals by a combination of five Priority Scientific Objectives, each with focused measurement objectives providing detailed constraints on the science payloads and on the platforms used by the mission. The JEM observation strategy will combine three types of scientific measurement sequences: measurements on a high-latitude, low-altitude Europan orbit; in-situ measurements to be performed at the surface, using a soft lander; and measurements during the final descent to Europa's surface. The implementation of these three observation sequences will rest on the combination of two science platforms: a soft lander to perform all scientific measurements at the surface and sub-surface at a selected landing site, and an orbiter to perform the orbital survey and descent sequences. We describe a science payload for the lander and orbiter that will meet our science objectives. We propose an innovative distribution of roles for NASA and ESA; while NASA would provide an SLS launcher, the lander stack and most of the mission operations, ESA would provide the carrier-orbiter-relay platform and a stand-alone astrobiology module for the characterization of life at Europa's surface: the Astrobiology We Laboratory (AWL). Following this approach, JEM will be a major exciting joint venture to the outer Solar System of NASA and ESA, working together toward one of the most exciting scientific endeavours of the 21st century: to search for life beyond our own planet.
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Photogeologic Map of the Perseverance Rover Field Site in Jezero Crater Constructed by the Mars 2020 Science Team
(Springer Link, 2020-11-03) Stack, K. M.; Williams, N. R.; Calef, F. J.; Sun, V. Z.; Williford, K. H.; Farley, K. A.; Eide, S.; Flannery, D.; Hughes, C.; Jacob, S. R.; Kah, L. C.; Meyen, F.; Molina, A.; Quantin Nataf, C.; Rice, M.; Russel, P.; Scheller, E.; Seeger, C. H.; Abbey, W. J.; Adler, J. B.; Amudsen, H.; Anderson, R. B.; Ángel, S. M.; Arana, G.; Atkins, J.; Barrington, M.; Berger, T.; Borden, R.; Boring, B.; Brown, A.; Carrier, B. L.; Conrad, Pamela G.; Dypvik, H.; Fagents, S. A.; Gallegos, Z. E.; Garczynski, B.; Golder, K.; Gómez, Felipe; Goreva, Y.; Gupta, S.; Hamran, S. E.; Hicks, T.; Hinterman, E. D.; Horgan, B. N.; Hurowitz, J.; Johnson, J. R.; Lasue, J.; Kronyak, R. E.; Liu, Y.; Madariaga, J. M.; Mangold, N.; McClean, John; Miklusicak, N.; Nunes, D.; Rojas, C.; Runyon, Kirby; Schmitz, N.; Scudder, N.; Shaver, E.; SooHoo, J.; Spaulding, R.; Stanish, E.; Tamppari, L. K.; Tice, M. M.; Turenne, N.; Willis, P. A.; Aileen Yingst, R.; European Research Council (ERC); National Aeronautics and Space Administration (NASA); Molina, A. [0000-0002-5038-2022]; Hughes, C. [0000-0002-7061-1443]; Jacob, S. [0000-0001-9950-1486]; Arana, Gorka [0000-0001-7854-855X]; Sun, V. Z. [0000-0003-1480-7369]; Stack, K. [0000-0003-3444-6695]; Williford, K. [0000-0003-0633-408X]; Flannery, D. [0000-0001-8982-496X]; Gupta, S. [0000-0001-6415-1332]; Williams, N. [0000-0003-0602-484X]; Unidad de Excelencia Científica Centro de Astrobiología María de Maeztu del Instituto Nacional de Técnica Aeroespacial y CSIC, MDM-2017-0737
The Mars 2020 Perseverance rover landing site is located within Jezero crater, a similar to 50 km diameter impact crater interpreted to be a Noachian-aged lake basin inside the western edge of the Isidis impact structure. Jezero hosts remnants of a fluvial delta, inlet and outlet valleys, and infill deposits containing diverse carbonate, mafic, and hydrated minerals. Prior to the launch of the Mars 2020 mission, members of the Science Team collaborated to produce a photogeologic map of the Perseverance landing site in Jezero crater. Mapping was performed at a 1:5000 digital map scale using a 25 cm/pixel High Resolution Imaging Science Experiment (HiRISE) orthoimage mosaic base map and a 1 m/pixel HiRISE stereo digital terrain model. Mapped bedrock and surficial units were distinguished by differences in relative brightness, tone, topography, surface texture, and apparent roughness. Mapped bedrock units are generally consistent with those identified in previously published mapping efforts, but this study's map includes the distribution of surficial deposits and sub-units of the Jezero delta at a higher level of detail than previous studies. This study considers four possible unit correlations to explain the relative age relationships of major units within the map area. Unit correlations include previously published interpretations as well as those that consider more complex interfingering relationships and alternative relative age relationships. The photogeologic map presented here is the foundation for scientific hypothesis development and strategic planning for Perseverance's exploration of Jezero crater.
Acceso Abierto
SuperCam Calibration Targets: Design and Development
(Springer Link, 2020-11-26) Manrique, J. A.; López Reyes, G.; Cousin, Agnes; Rull, F.; Maurice, S.; Wiens, R. C.; Madariaga, M. B.; Gasnault, O.; Aramendia, J.; Arana, G.; Beck, P.; Bernard, S.; Bernardi, P.; Bernt, M. H.; Berrocal, A.; Beyssac, O.; Caïs, P.; Castro, K.; Clegg, S. M.; Cloutis, E.; Dromart, G.; Drouet, C.; Dubois, B.; Escribano, D.; Fabre, C.; Fernández, A.; Forni, O.; García Baonza, V.; Gontijo, I.; Johnson, J. R.; Laserna, Javier; Lasue, J.; Madsen, Soren N.; Mateo Marti, Eva; Medina García, J.; Meslin, P.; Montagnac, G.; Moros, J.; Ollila, A. M.; Ortega, Cristina; Prieto-Ballesteros, Olga; Reess, J. M.; Robinson, S.; Rodríguez, Joseph; Saiz, J.; Sanz Arranz, Aurelio; Sard, I.; Sautter, V.; Sobron, P.; Toplis, M.; Veneranda, M.; Agencia Estatal de Investigación (AEI)
SuperCam is a highly integrated remote-sensing instrumental suite for NASA’s Mars 2020 mission. It consists of a co-aligned combination of Laser-Induced Breakdown Spectroscopy (LIBS), Time-Resolved Raman and Luminescence (TRR/L), Visible and Infrared Spectroscopy (VISIR), together with sound recording (MIC) and high-magnification imaging techniques (RMI). They provide information on the mineralogy, geochemistry and mineral context around the Perseverance Rover. The calibration of this complex suite is a major challenge. Not only does each technique require its own standards or references, their combination also introduces new requirements to obtain optimal scientific output. Elemental composition, molecular vibrational features, fluorescence, morphology and texture provide a full picture of the sample with spectral information that needs to be co-aligned, correlated, and individually calibrated. The resulting hardware includes different kinds of targets, each one covering different needs of the instrument. Standards for imaging calibration, geological samples for mineral identification and chemometric calculations or spectral references to calibrate and evaluate the health of the instrument, are all included in the SuperCam Calibration Target (SCCT). The system also includes a specifically designed assembly in which the samples are mounted. This hardware allows the targets to survive the harsh environmental conditions of the launch, cruise, landing and operation on Mars during the whole mission. Here we summarize the design, development, integration, verification and functional testing of the SCCT. This work includes some key results obtained to verify the scientific outcome of the SuperCam system.