Planetary Terrestrial Analogues Library Project: 2

Total Page:16

File Type:pdf, Size:1020Kb

Planetary Terrestrial Analogues Library Project: 2 Planetary and Space Science 193 (2020) 105087 Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss Planetary Terrestrial Analogues Library project: 2. building a laboratory facility for MicrOmega characterization Damien Loizeau a,*, Guillaume Lequertier a, François Poulet a, Vincent Hamm a,Cedric Pilorget a, Lionel Meslier-Lourit a, Cateline Lantz a, Stephanie C. Werner b, Fernando Rull c, Jean-Pierre Bibring a a Universite Paris-Saclay, CNRS, Institut D’astrophysique Spatiale, Batiment^ 121, 91405, Orsay, France b Centre for Earth Evolution and Dynamics, Department for Geosciences, University of Oslo, Oslo, Norway c Department of Condensed Matter Physics, Crystallography and Mineralogy, University of Valladolid, Ave. Francisco Valles, 8, Boecillo, 47151, Spain ARTICLE INFO ABSTRACT Keywords: Multiple spectroscopic techniques have been selected on previous, present and forthcoming missions to explore Planetary analogues planetary surfaces in the Solar System. In particular, forthcoming ESA/Roscosmos and NASA missions to the Spectral library surface of Mars will bring instruments capable of near-infrared (NIR), Raman and Laser Induced Breakdown Space instrument Spectroscopies to analyze the mineralogy and chemistry of rocks. The PTAL (Planetary Terrestrial Analogues Laboratory facility Library) project aims at building a multi-instrument spectral database of a large variety of natural Earth rock samples, including Mars analogues. The NIR hyperspectral microscope MicrOmega was selected to characterize the mineralogy of these analogues within the PTAL project. The instrument model used for the PTAL project is a spare flight model that requires specific care. For the safety of the instrument, and because of the large number of samples in the PTAL library and the requirement to optimize the observational conditions, a dedicated and semi- automated setup was built for the use of the MicrOmega instrument for this project. This paper presents the requirements specified for this setup, the technical solutions that have been selected, their implementation and the performances of the set-up. Sample preparation and operations during sample observations are explained, and a characterization example is presented to briefly illustrate the capabilities of MicrOmega in this set-up. The complete results from the MicrOmega characterizations of the PTAL rock analogues will be presented in a forthcoming paper (Loizeau et al. in prep). 1. Introduction and Raman spectroscopy, and Laser Induced Breakdown Spectroscopy (LIBS), on a large number of natural Earth samples characterized by X- Near InfraRed (NIR) hyperspectral imagers are among the major in- Ray Diffraction (Werner et al., 2018). Those samples have been selected struments of many recent and new payloads of planetary space missions. to represent a variety of geologic contexts with strong analogies to They have the strong advantage of providing mineral and organic in- multiple Martian past aqueous environments. The chosen analysis tech- formation of planetary surfaces with a relatively high speed/high spatial niques represent instruments that will be widely onboard future surface resolution in a non-destructive way. They can be integrated both on exploration missions as best exemplified by the forthcoming ESA/Ex- orbital missions and on surface platforms, to provide surface composi- oMars Rover and NASA/Mars2020 missions that will combine diverse tional information from global surveys to sample microanalyses (e.g. instruments capable of NIR spectroscopy (SuperCam/Mars 2020, ISE- Bibring et al., 2004; Murchie et al., 2007; Pilorget and Bibring, 2013). M/ExoMars, Ma-MISS/ExoMars, MicrOmega/ExoMars), Raman spec- During in situ exploration missions, mineralogical and organic ana- troscopy (SuperCam/Mars 2020, SHERLOC/Mars 2020, RLS/ExoMars), lyses are strongly strengthen by the combination of multiple spectro- and LIBS (SuperCam/Mars 2020) (Wiens et al., 2016; Beegle et al., 2015; scopic and chemical methods including NIR spectroscopy. In this context, Vago et al., 2018). the aim of the PTAL project is to build and exploit a multi-instrument Within the PTAL database, the NIR characterization of the samples is spectral database and joint spectral interpretation tools, including NIR made with both a laboratory point spectrometer of high spectral * Corresponding author. E-mail address: [email protected] (D. Loizeau). https://doi.org/10.1016/j.pss.2020.105087 Received 28 January 2020; Received in revised form 26 August 2020; Accepted 3 September 2020 Available online 10 September 2020 0032-0633/© 2020 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by- nc-nd/4.0/). D. Loizeau et al. Planetary and Space Science 193 (2020) 105087 Table 1 Table 2 MicrOmega FS specifications. Requirements for the set-up. MicrOmega instantaneous 20 μm  20 μm Quantified requirement Origin of the FOV (IFOV) requirement MicrOmega FOV 256  256 IFOV (5  5mm2) Controlled chamber characteristic Spectral range 0.99–3.6 μm þ 4 LEDs (LED1: 595 nm, LED2: 643 Operating MicrOmega À15 CtoÀ20 C Performance nm, LED3: 770 nm and LED4: 885 nm) FS temperature Spectral resolution 20 cm-1 Sample temperature < À5 C Performance Focal distance from the base 28.7 mm Atmosphere Dry atmosphere (no frost or Safety of the of MicrOmega condensation on the instrument or instrument Depth of focus Æ0.1 mm sample) Acquisition duration for one 15 min Operational requirements spectral cube Number of samples per 1-8 or more (depending on sample Automatization analysis size) fl Duration from ambient 1 Hour Duration resolution (detailed in Lantz et al., 2020), and a ight spare of the to optimal conditions MicrOmega ExoMars instrument. MicrOmega is a NIR hyperspectral Accuracy for the sample positioning microscope (Pilorget and Bibring, 2013). MicrOmega illuminates the Horizontally (X, Y) <60 μm  60 μm(3 MicrOmega Automatization field of view with monochromatic light at chosen wavelengths selected pixels) < through an Acousto-Optic Tunable Filter (AOTF) and acquires this way a Vertically (Z) 0.1 mm (MicrOmega depth of Performance focus) series of images at many different wavelengths. Earlier versions of MicrOmega have been selected to characterize Phobos on the Russian PhobosGrunt mission (Pilorget et al., 2011) and the surface of the better performances are achieved at cold temperatures. At these condi- near-Earth asteroid 162,173 Ryugu on the Mascot/Hayabusa-2 lander tions, the background thermal infrared emission of the instrument is mission (Bibring et al., 2017a). The model that is used for the PTAL lower, which increases the Signal to Noise Ratio (SNR) (Riu et al., 2018). project is the spare flight instrument of the MicrOmega model (hereafter In addition, operating the instrument at negative temperatures allows to named MicrOmega FS), whose flight model has been integrated on the simulate the observation conditions on the Martian surface. The thermal ExoMars rover Rosalind Franklin (Bibring et al., 2017b). regulation of the instrument within the PTAL set-up has been thus The use of MicrOmega FS to observe a large number of samples in safe considered as an important aspect of the setup. and efficient conditions required the design of a dedicated set-up. After a For the same reason, it was also chosen to cool-down the samples. short description of the MicrOmega instrument (section 2), the paper Although the systematic subtraction of the “dark” image enables to work describes in detail the choices that were made for the final design of a with samples at ambient temperature, the detector saturation is reached specific set-up for MicrOmega FS (section 3). The operational conditions more rapidly due to the higher thermal emission of the sample. Lowering that were defined for the characterization of the whole PTAL analogue the temperature, and hence the thermal emission of the sample, enables to rock collections are presented in sections 4 & 5. The characterization of acquire data with longer integration time, and hence to increase the SNR. one PTAL mineral sample is then exemplified (section 6), whereas the results of the characterization of the entire PTAL collection using this 2. Technical configuration of the PTAL MicrOmega set-up facility will be presented in a forthcoming paper (Loizeau et al. in prep). 2.1. Requirements 1.1. MicrOmega/ExoMars instrument In addition to the previous requirements related to the performances The MicrOmega instrument for ExoMars (Bibring et al., 2017b)isa of MicrOmega FS, the other major objective of the set-up was to ease and microscope acquiring images with pixels of ~20  20 μm2 over a 256  automatize the characterization of the PTAL samples. This leads to define 256 pixels field of view (~5  5mm2). An AOTF enables to illuminate the several environmental and operational requirements listed in Table 2. field of view (FOV) with monochromatic light in the NIR range from The operational and performance related requirements conduct to ~0.99 to ~3.6 μm with a spectral resolution of 20 cm-1 (equivalent in have both the instrument and the samples in a thermally controlled and wavelength to 2 nm at 1 μm and to 26 nm at 3.6 μm). The cooled detector dry atmosphere to avoid water frost and condensation. The desired ac- acquires the reflected light at each ~300 wavelengths and builds this curacy in the sample positioning implies the use of a precise electroni- way a hyperspectral cube. The NIR observations using the AOTF are cally controlled stage with motions in all three directions. completed with four images illuminated with LEDs (Light Emitting Di- To ensure protection from dust, in compliance with the nature of the odes) centered on wavelengths at about 595, 643, 770 and 885 nm flight model of MicrOmega FS, an additional requirement was made to (Bibring et al., 2017b). The main characteristics are listed in Table 1. set MicrOmega FS in a contained environment with respect to the The spectral range and sampling were selected to enable the identi- samples.
Recommended publications
  • 1 Cross-Calibration of Laser-Induced Breakdown Spectroscopy (LIBS)
    ISSI/ISSI-BJ Joint Call for Proposals 2018 International Teams in Space and Earth Sciences Cross-calibration of Laser-Induced Breakdown Spectroscopy (LIBS) instruments for planetary exploration. 1 Summary of the project : A revolutionary technique for planetary science: Laser-induced Breakdown Spectroscopy (LIBS) is an active analytical technique that makes use of a pulsed laser to ablate material of interest at a distance. The atoms in the high temperature plasma emit at specific wavelengths from the UV to near- IR and the light can be analyzed by spectrometry to determine the composition of the target [1]. Since 2012, LIBS has been successfully used under low atmospheric pressure for exploring the geology of Mars at Gale Crater with the Mars Science Laboratory rover’s ChemCam instrument [2-4]. LIBS can be used to analyze single regolith mineral particles and larger rocks, giving major and minor elements compositions. Moreover, LIBS is sensitive to volatile elements (H, Na, etc.) that are of intrinsic interest to understand key planetary processes. The generated shock wave can also ablate dust covering rocks to allow further analysis by other instruments on the mission platform (rover, lander). In order to quantify the elemental composition of various targets, large laboratory samples analyses are required for calibration, with ChemCam’s calibration database containing more than 400 standards [5-6]. LIBS is becoming international: Due to its ease of deployment and rapidity of analysis, LIBS has shown a great potential as a chemistry survey instrument for the next generation of in situ space missions to planets, satellites and small bodies. In the next couple of years, three more LIBS space instruments will be sent for planetary exploration by teams representing several different nationalities In 2018, the Indian space mission to the Moon Chandrayaan 2 will comprise a rover equipped with a small portable LIBS instrument for regolith reconnaissance around the landing site [7].
    [Show full text]
  • 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.
    [Show full text]
  • 18Th EANA Conference European Astrobiology Network Association
    18th EANA Conference European Astrobiology Network Association Abstract book 24-28 September 2018 Freie Universität Berlin, Germany Sponsors: Detectability of biosignatures in martian sedimentary systems A. H. Stevens1, A. McDonald2, and C. S. Cockell1 (1) UK Centre for Astrobiology, University of Edinburgh, UK ([email protected]) (2) Bioimaging Facility, School of Engineering, University of Edinburgh, UK Presentation: Tuesday 12:45-13:00 Session: Traces of life, biosignatures, life detection Abstract: Some of the most promising potential sampling sites for astrobiology are the numerous sedimentary areas on Mars such as those explored by MSL. As sedimentary systems have a high relative likelihood to have been habitable in the past and are known on Earth to preserve biosignatures well, the remains of martian sedimentary systems are an attractive target for exploration, for example by sample return caching rovers [1]. To learn how best to look for evidence of life in these environments, we must carefully understand their context. While recent measurements have raised the upper limit for organic carbon measured in martian sediments [2], our exploration to date shows no evidence for a terrestrial-like biosphere on Mars. We used an analogue of a martian mudstone (Y-Mars[3]) to investigate how best to look for biosignatures in martian sedimentary environments. The mudstone was inoculated with a relevant microbial community and cultured over several months under martian conditions to select for the most Mars-relevant microbes. We sequenced the microbial community over a number of transfers to try and understand what types microbes might be expected to exist in these environments and assess whether they might leave behind any specific biosignatures.
    [Show full text]
  • Team Develops Optocoupler for Spaceflight Applications 6 February 2019
    Team develops optocoupler for spaceflight applications 6 February 2019 "Operating in conditions from -40° to 100° Celsius, our power converter is ruggedized to withstand the rigors of launch and adverse radiation conditions in space," said Carlos Urdiales, a senior program manager in SwRI's Space Science and Engineering Division. "In addition to being able to withstand the radiation environment around Jupiter, our optocoupler is fast, stepping from 0 to 10 kilovolts in 23.4 microseconds. The half-inch package weighs less than 4 grams and has a radiation tolerance in excess of 100 kilorads." The high-quality device offers high reliability and long life in a relatively small footprint, which is critical for space applications. The optocoupler is being integrated into the MAss SPectrometer for Planetary EXploration (MASPEX), the Plasma Instrument for Magnetic Sounding (PIMS) and the SwRI is integrating its optocoupler power conversion SUrface Dust Analyser (SUDA) instruments for the technology into three instruments bound for Jupiter’s Europa Clipper mission. SwRI's optocoupler will moon Europa. The radiation-hardened, high-reliability help power astrobiology examinations to device, developed with internal funding, overcomes understand the moon's subsurface sea and problems similar systems have had operating in space. potential habitability as well as characterization of Credit: Southwest Research Institute its atmosphere, ionosphere and magnetosphere. "SwRI can configure the device to suit a range of applications," Urdiales said. "We deliver increased Southwest Research Institute has developed a reliability through redundancy in the high-current 2 high-reliability, high-voltage optocoupler for Amp LED array, which provides a lightning fast spaceflight applications.
    [Show full text]
  • A Lunar Micro Rover System Overview for Aiding Science and ISRU Missions Virtual Conference 19–23 October 2020 R
    i-SAIRAS2020-Papers (2020) 5051.pdf A lunar Micro Rover System Overview for Aiding Science and ISRU Missions Virtual Conference 19–23 October 2020 R. Smith1, S. George1, D. Jonckers1 1STFC RAL Space, R100 Harwell Campus, OX11 0DE, United Kingdom, E-mail: [email protected] ABSTRACT the form of rovers and landers of various size [4]. Due to the costly nature of these missions, and the pressure Current science missions to the surface of other plan- for a guaranteed science return, they have been de- etary bodies tend to be very large with upwards of ten signed to minimise risk by using redundant and high instruments on board. This is due to high reliability re- reliability systems. This further increases mission cost quirements, and the desire to get the maximum science as components and subsystems are expected to be ex- return per mission. Missions to the lunar surface in the tensively qualified. next few years are key in the journey to returning hu- mans to the lunar surface [1]. The introduction of the As an example, the Mars Science Laboratory, nick- Commercial lunar Payload Services (CLPS) delivery named the Curiosity rover, one of the most successful architecture for science instruments and technology interplanetary rovers to date, has 10 main scientific in- demonstrators has lowered the barrier to entry of get- struments, requires a large team of people to control ting science to the surface [2]. Many instruments, and and cost over $2.5 billion to build and fly [5]. Curios- In Situ Surface Utilisation (ISRU) experiments have ity had 4 main science goals, with the instruments and been funded, and are being built with the intention of the design of the rover specifically tailored to those flying on already awarded CLPS missions.
    [Show full text]
  • Radar Imager for Mars' Subsurface Experiment—RIMFAX
    Space Sci Rev (2020) 216:128 https://doi.org/10.1007/s11214-020-00740-4 Radar Imager for Mars’ Subsurface Experiment—RIMFAX Svein-Erik Hamran1 · David A. Paige2 · Hans E.F. Amundsen3 · Tor Berger 4 · Sverre Brovoll4 · Lynn Carter5 · Leif Damsgård4 · Henning Dypvik1 · Jo Eide6 · Sigurd Eide1 · Rebecca Ghent7 · Øystein Helleren4 · Jack Kohler8 · Mike Mellon9 · Daniel C. Nunes10 · Dirk Plettemeier11 · Kathryn Rowe2 · Patrick Russell2 · Mats Jørgen Øyan4 Received: 15 May 2020 / Accepted: 25 September 2020 © The Author(s) 2020 Abstract The Radar Imager for Mars’ Subsurface Experiment (RIMFAX) is a Ground Pen- etrating Radar on the Mars 2020 mission’s Perseverance rover, which is planned to land near a deltaic landform in Jezero crater. RIMFAX will add a new dimension to rover investiga- tions of Mars by providing the capability to image the shallow subsurface beneath the rover. The principal goals of the RIMFAX investigation are to image subsurface structure, and to provide information regarding subsurface composition. Data provided by RIMFAX will aid Perseverance’s mission to explore the ancient habitability of its field area and to select a set of promising geologic samples for analysis, caching, and eventual return to Earth. RIM- FAX is a Frequency Modulated Continuous Wave (FMCW) radar, which transmits a signal swept through a range of frequencies, rather than a single wide-band pulse. The operating frequency range of 150–1200 MHz covers the typical frequencies of GPR used in geology. In general, the full bandwidth (with effective center frequency of 675 MHz) will be used for The Mars 2020 Mission Edited by Kenneth A.
    [Show full text]
  • Neptune's Atmospheric Composition
    Poseidon - Trident Flying by Neptune TEAM BLUE Alpbach, 2 August 2012 Outline ● Science Case ● Objectives & Requirements ● Payload ● Mission trade study & design ● System design ● Ground Segment Mission statement ● To explore the Neptunian system as an archetype for ice giants ● To investigate the nature of the moon Triton ESA Cosmic Vision 2015-2025 Call Themes addressed ● 1.3 Life and habitability in the Solar System ● 2.1 From the Sun to the edge of the Solar System ● 2.2 The giant planets and their environments 1 Mission Profile ● Neptune and Triton Flyby ● Neptune Atmosphere Probe ● Launch date - June 2028 ● Arrival at Neptunian system - Jan 2041 ● Transit time 13.4 years ● Nominal mission duration: 15.4 years Neptunian System Rationale ● Limited knowledge about icy giants ● Planet formation process ● Link to Exoplanets ● Triton - possible KBO The Neptunian System ● Only visited by Voyager 2 (August 1989) ● Additional data taken from ground-based measurements and HST ● Icy giant (30 AU) ● 13 satellites (discovered so far) in the Neptunian system ● Ring Structure ● Very dynamic storm events (Suomi et al., 1991) Neptune's Atmospheric Composition ● Main species : H2 (~80 %), He (~18 %), CH4 (~2 %) ● We expect heavy elements (Z>3) O, C, N, S in the form: ○ S in H2S Troposphere ○ O in H2O ○ N in NH3 ○ C in CH4 ● Hydrocarbons, CO and HCN Stratosphere Atmospheric Structure PRESSURE The locations and densities of the various cloud layers in the atmosphere of Neptune. de Pater et al. (1991) Atmospheric Dynamics Sromovsky et al., 2001 ● Large
    [Show full text]
  • Download the Acquired Data Or to Fix Possible Problem
    Università degli Studi di Napoli Federico II DOTTORATO DI RICERCA IN FISICA Ciclo 30° Coordinatore: Prof. Salvatore Capozziello Settore Scientifico Disciplinare FIS/05 Characterisation of dust events on Earth and Mars the ExoMars/DREAMS experiment and the field campaigns in the Sahara desert Dottorando Tutore Gabriele Franzese dr. Francesca Esposito Anni 2014/2018 A birbetta e giggione che sono andati troppo veloci e a patata che invece adesso va piano piano Summary Introduction ......................................................................................................................... 6 Chapter 1 Atmospheric dust on Earth and Mars............................................................ 9 1.1 Mineral Dust ....................................................................................................... 9 1.1.1 Impact on the Terrestrial land-atmosphere-ocean system .......................... 10 1.1.1.1 Direct effect ......................................................................................... 10 1.1.1.2 Semi-direct and indirect effects on the cloud physics ......................... 10 1.1.1.3 Indirect effects on the biogeochemical system .................................... 11 1.1.1.4 Estimation of the total effect ............................................................... 11 1.2 Mars .................................................................................................................. 12 1.2.1 Impact on the Martian land-atmosphere system ......................................... 13 1.3
    [Show full text]
  • The Supercam Remote Raman Spectrometer for Mars 2020 R.C
    Lunar and Planetary Science XLVIII (2017) 2600.pdf THE SUPERCAM REMOTE RAMAN SPECTROMETER FOR MARS 2020 R.C. Wiens1, R. Newell1, S. Clegg1, S.K. Sharma2, A. Misra2, P. Bernardi3, S. Maurice4, K. McCabe1, P. Cais5, and the SuperCam Science Team (1LANL, Los Alamos, NM; [email protected], 2U. Hawaii; 3LESIA; 4IRAP; 5LAB) Overview: The Mars 2020 Science Definition length calibration as well as to have reasonable Team developed criteria for advanced instrumen- resolution; b) to identify a mineral by resolving tation for the next NASA rover. One important two of its closely-spaced peaks. Examples of this criterion is to provide mineral compositions at are olivine or albite whose twin peaks are gener- remote distances [1]. Hence, the SuperCam in- ally characteristic of their spectra; and c) to iden- strument that was selected provides two remote tify the presence of two or more minerals in the mineralogy techniques: passive visible and infra- same spectrum by resolving their respective red (VISIR) reflectance spectroscopy and remote peaks. An example is quartz and albite, which Raman spectroscopy. These are in addition to often occur together. A FWHM of 12 cm-1 vali- providing co-bore-sighted remote elemental com- dated on a naturally narrow emission line meets positions, color images, and acoustic spectra all of the above needs. There are other ways of (sounds) [2]. SuperCam’s remote Raman spec- specifying resolution, such as the pixel spread or troscopy complements the rover’s in-situ Raman the theoretical resolution of a system. For exam- experiment, SHERLOC (see below; [3]), and ple, the 12 cm-1 FWHM criterion is better than RLS on ExoMars, as the first Raman spectrome- examples labeled in [4] as “4 cm-1”, the highest ters to be built for another planet.
    [Show full text]
  • Supercam Calibration Targets: Design and Development J
    SuperCam Calibration Targets: Design and Development J. Manrique, G. Lopez-Reyes, A. Cousin, F. Rull, S. Maurice, R. Wiens, M. Madsen, J. Madariaga, O. Gasnault, J. Aramendia, et al. To cite this version: J. Manrique, G. Lopez-Reyes, A. Cousin, F. Rull, S. Maurice, et al.. SuperCam Calibration Tar- gets: Design and Development. Space Science Reviews, Springer Verlag, 2020, 216 (8), pp.138. 10.1007/s11214-020-00764-w. hal-03048873 HAL Id: hal-03048873 https://hal.archives-ouvertes.fr/hal-03048873 Submitted on 3 Jan 2021 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) 216:138 https://doi.org/10.1007/s11214-020-00764-w SuperCam Calibration Targets: Design and Development J.A. Manrique1 · G. Lopez-Reyes1 · A. Cousin2 · F. Rull 1 · S. Maurice2 · R.C. Wiens3 · M.B. Madsen4 · J.M. Madariaga5 · O. Gasnault2 · J. Aramendia5 · G. Arana5 · P. Beck6 · S. Bernard7 · P. Bernardi 8 · M.H. Bernt4 · A. Berrocal9 · O. Beyssac7 · P. Caïs 10 · C. Castro11 · K. Castro5 · S.M. Clegg3 · E. Cloutis12 · G. Dromart13 · C. Drouet14 · B. Dubois15 · D. Escribano16 · C. Fabre17 · A. Fernandez11 · O. Forni2 · V.
    [Show full text]
  • Martian Mysteries
    Mission Objectives Don't chute the messenger! Martian Included within the pattern on the inside of Looking for Habitability the rover's parachute was a hidden message. Exploring the Martian landscape to Binary code was used to spell out the phrase discover environments that could Dare Mighty Things, a motto used by NASA’s have once supported microbial life. Mysteries Jet Propulsion Laboratory, along with GPS coordinates for the lab's location in California. Seeking Biosignatures Perseverance and the Studying suitable environments Search for Life on Mars in search of evidence of ancient Martian lifeforms. Caching Samples ars has always been a source of marvel. Collecting rock and soil, to be M It captivated ancient civilizations, it's red hue stored until a future mission can setting it apart from other points of light in the night collect them for analysis on Earth. sky. Even in recent history, some suggested it was home to alien life, until Mariner 4 got close enough ONE Preparing for Humans to reveal a lifeless and barren planet. However, in Atmospheric Entry Testing oxygen production in the last few decades the true nature of Mars has and Deceleration Mars' hostile atmosphere, to help begun to emerge. We’ve discovered a place that has TOUCHDOWN IN... inform future human missions. substantially changed over time. An environment Approx. 7 mins where water once shaped the landscape and still sits ALTITUDE VELOCITY within icy polar regions and deep underground. And 131 km <5000 m/s Mission Technology a planet where microbial life may have once existed, TWO and perhaps against all odds still does.
    [Show full text]
  • Ocean Worlds : May 21–23, 2018, Houston, Texas
    Program Ocean Worlds May 21–23, 2018 • Houston, Texas Organizers Lunar and Planetary Institute Universities Space Research Association Convener Louise Prockter Lunar and Planetary Institute Science Organizing Committee Julie Castillo NASA Jet Propulsion Laboratory Christopher German Wood Hole Oceanographic Institution Jonathan Kay Lunar and Planetary Institute Marc Neveu NASA Headquarters Beth Orcutt Bigelow Laboratory for Ocean Sciences Paul Schenk Lunar and Planetary Institute Christophe Sotin NASA Jet Propulsion Laboratory Hajime Yano Japan Aerospace Exploration Agency Lunar and Planetary Institute 3600 Bay Area Boulevard Houston TX 77058-1113 Abstracts for this meeting are available via the meeting website at www.hou.usra.edu/meetings/oceanworlds2018/ Abstracts can be cited as Author A. B. and Author C. D. (2018) Title of abstract. In Ocean Worlds, Abstract #XXXX. LPI Contribution No. 2085, Lunar and Planetary Institute, Houston. Guide to Sessions Monday, May 21, 2018 1:00 p.m. Lecture Hall Opening Session: Setting the Framework 5:30 p.m. Great Room Poster Session Tuesday, May 22, 2018 8:30 a.m. Lecture Hall Session I 12:45p.m. Great Room Poster Viewing Tuesday, May 22, 2018 1:30 p.m. Lecture Hall Session II Wednesday, May 23, 2018 8:30 a.m. Lecture Hall Session III 1:00 p.m. Lecture Hall Session IV Program Monday, May 21, 2018 OPENING SESSION: SETTING THE FRAMEWORK 1:00 p.m. Lecture Hall Chair: Christopher German 1:00 p.m. German C. R. * Prockter L. * Opening Remarks 1:15 p.m. Hand K. P. * Ocean Worlds of the Outer Solar System [#6042] I will provide an overview of why we think we know ocean worlds exist, what we know about the physical and chemical conditions that likely persist on these worlds, and how we may proceed in our search for biosignatures on these worlds.
    [Show full text]