ROVING ACROSS MARS: SEARCHING for EVIDENCE of FORMER HABITABLE ENVIRONMENTS Michael H
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Chemical Variations in Yellowknife Bay Formation Sedimentary Rocks
PUBLICATIONS Journal of Geophysical Research: Planets RESEARCH ARTICLE Chemical variations in Yellowknife Bay formation 10.1002/2014JE004681 sedimentary rocks analyzed by ChemCam Special Section: on board the Curiosity rover on Mars Results from the first 360 Sols of the Mars Science Laboratory N. Mangold1, O. Forni2, G. Dromart3, K. Stack4, R. C. Wiens5, O. Gasnault2, D. Y. Sumner6, M. Nachon1, Mission: Bradbury Landing P.-Y. Meslin2, R. B. Anderson7, B. Barraclough4, J. F. Bell III8, G. Berger2, D. L. Blaney9, J. C. Bridges10, through Yellowknife Bay F. Calef9, B. Clark11, S. M. Clegg5, A. Cousin5, L. Edgar8, K. Edgett12, B. Ehlmann4, C. Fabre13, M. Fisk14, J. Grotzinger4, S. Gupta15, K. E. Herkenhoff7, J. Hurowitz16, J. R. Johnson17, L. C. Kah18, N. Lanza19, Key Points: 2 1 20 21 12 16 2 • J. Lasue , S. Le Mouélic , R. Léveillé , E. Lewin , M. Malin , S. McLennan , S. Maurice , Fluvial sandstones analyzed by 22 22 23 19 19 24 25 ChemCam display subtle chemical N. Melikechi , A. Mezzacappa , R. Milliken , H. Newsom , A. Ollila , S. K. Rowland , V. Sautter , variations M. Schmidt26, S. Schröder2,C.d’Uston2, D. Vaniman27, and R. Williams27 • Combined analysis of chemistry and texture highlights the role of 1Laboratoire de Planétologie et Géodynamique de Nantes, CNRS, Université de Nantes, Nantes, France, 2Institut de Recherche diagenesis en Astrophysique et Planétologie, CNRS/Université de Toulouse, UPS-OMP, Toulouse, France, 3Laboratoire de Géologie de • Distinct chemistry in upper layers 4 5 suggests distinct setting and/or Lyon, Université de Lyon, Lyon, France, California Institute of Technology, Pasadena, California, USA, Los Alamos National 6 source Laboratory, Los Alamos, New Mexico, USA, Earth and Planetary Sciences, University of California, Davis, California, USA, 7Astrogeology Science Center, U.S. -
Mariner to Mercury, Venus and Mars
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mariner to Mercury, Venus and Mars Between 1962 and late 1973, NASA’s Jet carry a host of scientific instruments. Some of the Propulsion Laboratory designed and built 10 space- instruments, such as cameras, would need to be point- craft named Mariner to explore the inner solar system ed at the target body it was studying. Other instru- -- visiting the planets Venus, Mars and Mercury for ments were non-directional and studied phenomena the first time, and returning to Venus and Mars for such as magnetic fields and charged particles. JPL additional close observations. The final mission in the engineers proposed to make the Mariners “three-axis- series, Mariner 10, flew past Venus before going on to stabilized,” meaning that unlike other space probes encounter Mercury, after which it returned to Mercury they would not spin. for a total of three flybys. The next-to-last, Mariner Each of the Mariner projects was designed to have 9, became the first ever to orbit another planet when two spacecraft launched on separate rockets, in case it rached Mars for about a year of mapping and mea- of difficulties with the nearly untried launch vehicles. surement. Mariner 1, Mariner 3, and Mariner 8 were in fact lost The Mariners were all relatively small robotic during launch, but their backups were successful. No explorers, each launched on an Atlas rocket with Mariners were lost in later flight to their destination either an Agena or Centaur upper-stage booster, and planets or before completing their scientific missions. -
JSC-Rocknest: a Large-Scale Mojave Mars Simulant (MMS) Based Soil Simulant for In-Situ
1 JSC-Rocknest: A large-scale Mojave Mars Simulant (MMS) based soil simulant for in-situ 2 resource utilization water-extraction studies 3 Clark, J.V.a*, Archer, P.D.b, Gruener, J.E.c, Ming, D.W.c, Tu, V.M.b, Niles, P.B.c, Mertzman, 4 S.A.d 5 a GeoControls Systems, Inc – Jacobs JETS Contract at NASA Johnson Space Center, 2101 6 NASA Pkwy, Houston, TX 77058, USA. [email protected], 281-244-7442 7 b Jacobs JETS Contract at NASA Johnson Space Center, 2101 NASA Pkwy, Houston, TX 8 77058, USA. 9 c NASA Johnson Space Center, 2101 NASA Pkwy, Houston, TX 77058, USA. 10 d Department of Earth and Environmental, Franklin & Marshall College, Lancaster, PA 17604, 11 USA. 12 *Corresponding author 13 14 15 16 17 18 19 Keywords: Simulant, Mars, In-situ resource utilization, evolved gas analysis, Rocknest 1 20 Abstract 21 The Johnson Space Center-Rocknest (JSC-RN) simulant was developed in response to a 22 need by NASA's Advanced Exploration Systems (AES) In-Situ Resource Utilization (ISRU) 23 project for a simulant to be used in component and system testing for water extraction from Mars 24 regolith. JSC-RN was designed to be chemically and mineralogically similar to material from the 25 aeolian sand shadow named Rocknest in Gale Crater, particularly the 1-3 wt.% low temperature 26 (<450 ºC) water release as measured by the Sample Analysis at Mars (SAM) instrument on the 27 Curiosity rover. Sodium perchlorate, goethite, pyrite, ferric sulfate, regular and high capacity 28 granular ferric oxide, and forsterite were added to a Mojave Mars Simulant (MMS) base in order 29 to match the mineralogy, evolved gases, and elemental chemistry of Rocknest. -
Combinatorics in Space
Combinatorics in Space The Mariner 9 Telemetry System Mariner 9 Mission Launched: May 30, 1971 Arrived: Nov. 14, 1971 Turned Off: Oct. 27, 1972 Mission Objectives: (Mariner 8): Map 70% of Martian surface. (Mariner 9): Study temporal changes in Martian atmosphere and surface features. Live TV A black and white TV camera was used to broadcast “live” pictures of the Martian surface. Each photo-receptor in the camera measures the brightness of a section of the Martian surface about 4-5 km square, and outputs a grayness value in the range 0-63. This value is represented as a binary 6-tuple. The TV image is thus digitalized by the photo-receptor bank and is output as a stream of thousands of binary 6-tuples. Coding Needed Without coding and a failure probability p = 0.05, 26% of the image would be in error ... unacceptably poor quality for the nature of the mission. Any coding will increase the length of the transmitted message. Due to power constraints on board the probe and equipment constraints at the receiving stations on Earth, the coded message could not be much more than 5 times as long as the data. Thus, a 6-tuple of data could be coded as a codeword of about 30 bits in length. Other concerns A second concern involves the coding procedure. Storage of data requires shielding of the storage media – this is dead weight aboard the probe and economics require that there be little dead weight. Coding should therefore be done “on the fly”, without permanent memory requirements. -
Seasonal and Interannual Variability of Solar Radiation at Spirit, Opportunity and Curiosity Landing Sites
Seasonal and interannual variability of solar radiation at Spirit, Opportunity and Curiosity landing sites Álvaro VICENTE-RETORTILLO1, Mark T. LEMMON2, Germán M. MARTÍNEZ3, Francisco VALERO4, Luis VÁZQUEZ5, Mª Luisa MARTÍN6 1Departamento de Física de la Tierra, Astronomía y Astrofísica II, Universidad Complutense de Madrid, Madrid, Spain, [email protected]. 2Department of Atmospheric Sciences, Texas A&M University, College Station, TX, USA, [email protected]. 3Department of Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, MI, USA, [email protected]. 4Departamento de Física de la Tierra, Astronomía y Astrofísica II, Universidad Complutense de Madrid, Madrid, Spain, [email protected]. 5Departamento de Matemática Aplicada, Universidad Complutense de Madrid, Madrid, Spain, [email protected]. 6Departamento de Matemática Aplicada, Universidad de Valladolid, Segovia, Spain, [email protected]. Received: 14/04/2016 Accepted: 22/09/2016 Abstract In this article we characterize the radiative environment at the landing sites of NASA's Mars Exploration Rover (MER) and Mars Science Laboratory (MSL) missions. We use opacity values obtained at the surface from direct imaging of the Sun and our radiative transfer model COMIMART to analyze the seasonal and interannual variability of the daily irradiation at the MER and MSL landing sites. In addition, we analyze the behavior of the direct and diffuse components of the solar radiation at these landing sites. Key words: Solar radiation; Mars Exploration Rovers; Mars Science Laboratory; opacity, dust; radiative transfer model; Mars exploration. Variabilidad estacional e interanual de la radiación solar en las coordenadas de aterrizaje de Spirit, Opportunity y Curiosity Resumen El presente artículo está dedicado a la caracterización del entorno radiativo en los lugares de aterrizaje de las misiones de la NASA de Mars Exploration Rover (MER) y de Mars Science Laboratory (MSL). -
Pre-Mission Insights on the Interior of Mars Suzanne E
Pre-mission InSights on the Interior of Mars Suzanne E. Smrekar, Philippe Lognonné, Tilman Spohn, W. Bruce Banerdt, Doris Breuer, Ulrich Christensen, Véronique Dehant, Mélanie Drilleau, William Folkner, Nobuaki Fuji, et al. To cite this version: Suzanne E. Smrekar, Philippe Lognonné, Tilman Spohn, W. Bruce Banerdt, Doris Breuer, et al.. Pre-mission InSights on the Interior of Mars. Space Science Reviews, Springer Verlag, 2019, 215 (1), pp.1-72. 10.1007/s11214-018-0563-9. hal-01990798 HAL Id: hal-01990798 https://hal.archives-ouvertes.fr/hal-01990798 Submitted on 23 Jan 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. Open Archive Toulouse Archive Ouverte (OATAO ) OATAO is an open access repository that collects the wor of some Toulouse researchers and ma es it freely available over the web where possible. This is an author's version published in: https://oatao.univ-toulouse.fr/21690 Official URL : https://doi.org/10.1007/s11214-018-0563-9 To cite this version : Smrekar, Suzanne E. and Lognonné, Philippe and Spohn, Tilman ,... [et al.]. Pre-mission InSights on the Interior of Mars. (2019) Space Science Reviews, 215 (1). -
A Miniaturized Chemin Xrd/Xrf for Future Mars Exploration
Ninth International Conference on Mars 2019 (LPI Contrib. No. 2089) 6230.pdf A MINIATURIZED CHEMIN XRD/XRF FOR FUTURE MARS EXPLORATION. B. Lafuente1, P. Sarrazin1, T. F. Bristow2, D. F. Blake2, M. Gailhanou3, J. Chen4, K. Thompson1, R. Walroth2, K. Zacny5, R. T. Downs6, and A. Yen7, 1SETI Institute, Mountain View, CA ([email protected]), 2Exobiology, NASA ARC, Moffett Field, CA, 3CNRS, IM2NP UMR, Marseille, France, 4Baja Technology, Tempe, AZ, 5Honeybee Robotics Spacecraft Mecha- nisms Corp., Pasadena, CA, 6Geosciences, Univ. Arizona, Tucson AZ, 7JPL, Pasadena, CA. Introduction: X-ray Diffraction (XRD) and X-ray ergy-selective detection of XRD photons in Mars’ ra- Fluorescence (XRF) analyses provide the most diag- diative environment. The CheMinX XRD geometry is nostic and complete characterization of rocks and soil based on an architecture demonstrated by hundreds of by any spacecraft-capable technique, improved upon commercial XRD instruments (Terra, commercial spin- only by sample return and analysis in terrestrial labora- off of CheMin, Fig. 1). This design resulted from a tories. In a complex sample such as a basalt, XRD can ray-tracing study of XRD geometries based on high as- definitively identify and quantify all minerals, establish pect-ratio detectors. It was found that reduced surface their individual elemental compositions and quantify area detectors can be used with no loss in throughput, the amount of the amorphous component. When cou- angular resolution or angular range, the loss in detector pled with XRF, the composition of the amorphous coverage being fully compensated for by an optimized component can be determined as well. collimator design. The MSL CheMin instrument, the first XRD instru- In its basic implementation CheMinX will provide ment flown in space, established the quantitative min- a resolution of 0.3° 2θ FWHM, slightly improved over eralogy of the Mars soil [1], characterized the first hab- CheMin’s 0.35°. -
Phil Liebrecht Assistant Deputy Associate Administrator and Deputy Program Manager Space Communications and Navigation NASA HQ
Phil Liebrecht Assistant Deputy Associate Administrator and Deputy Program Manager Space Communications and Navigation NASA HQ Meeting the Communications and Navigation Needs of Space missions since 1957 “Keeping the Universe Connected” Public University of Navarra, 2010 [email protected] 1 Operations and Communications Customers 2 Space Operations 101 Relation Between Space Segment, Ground System, and Data Users* Ground System Command Commands Requests Spacecraft and Payload Support • Mission Planning Telemetry • Flight Operations • Flight Dynamics • Perf. Assess., Trending & Archiving Space Data Users • Anomaly Support Segment Data Relay and Level (S/C) Mission Zero Data Processing Mission Data Data • Space-to-ground Comm. • Data Capture • Data Processing • Network Management • Data Distribution • Quick Look * Based on Wertz and Wiley; Space Mission Analysis and Design 3 Communications Theory- Basic Concepts Transmitter and Receiver must use the same language Noise causes interference a) Figures it – no errors (Identify and quantify) b) Figures it – corrects Must be loud enough ENERGY! c) Figures it – incorrectly (message in error) d) Cannot figure- recognizes E L an error T M E XP AIN L E e) Cannot figure- ? TRANSMITTER Distance weakens the sound RECEIVER (calculate the loss) CHANNEL Has to correctly interpret the message - the most difficult job The fundamental problem of communications is that of reproducing at one point either exactly or approximately a message selected at another point. 4 Functional - End to End Process -
Determining Mineralogy on Mars with the Chemin X-Ray Diffractometer the Chemin Team Logo Illustrating the Diffraction of Minerals on Mars
Determining Mineralogy on Mars with the CheMin X-Ray Diffractometer The CheMin team logo illustrating the diffraction of minerals on Mars. Robert T. Downs1 and the MSL Science Team 1811-5209/15/0011-0045$2.50 DOI: 10.2113/gselements.11.1.45 he rover Curiosity is conducting X-ray diffraction experiments on the The mineralogy of the Martian surface of Mars using the CheMin instrument. The analyses enable surface is dominated by the phases found in basalt and its ubiquitous Tidentifi cation of the major and minor minerals, providing insight into weathering products. To date, the the conditions under which the samples were formed or altered and, in turn, major basaltic minerals identi- into past habitable environments on Mars. The CheMin instrument was devel- fied by CheMin include Mg– Fe-olivines, Mg–Fe–Ca-pyroxenes, oped over a twenty-year period, mainly through the efforts of scientists and and Na–Ca–K-feldspars, while engineers from NASA and DOE. Results from the fi rst four experiments, at the minor primary minerals include Rocknest, John Klein, Cumberland, and Windjana sites, have been received magnetite and ilmenite. CheMin and interpreted. The observed mineral assemblages are consistent with an also identifi ed secondary minerals formed during alteration of the environment hospitable to Earth-like life, if it existed on Mars. basalts, such as calcium sulfates KEYWORDS: X-ray diffraction, Mars, Gale Crater, habitable environment, CheMin, (anhydrite and bassanite), iron Curiosity rover oxides (hematite and akaganeite), pyrrhotite, clays, and quartz. These secondary minerals form and INTRODUCTION persist only in limited ranges of temperature, pressure, and The Mars rover Curiosity landed in Gale Crater on August ambient chemical conditions (i.e. -
Chemin: a Definitive Mineralogy Instrument on the Mars Science Laboratory (Msl ’09) Rover
Seventh International Conference on Mars 3220.pdf CHEMIN: A DEFINITIVE MINERALOGY INSTRUMENT ON THE MARS SCIENCE LABORATORY (MSL ’09) ROVER. D.F. Blake1, P. Sarrazin2, D. L. Bish3, S. J. Chipera4, D. T. Vaniman4, D. Ming5, D. Morris5 and Albert Yen6. 1NASA ARC, MS 239-4, Moffett Field, CA 94035 ([email protected]), 2 In-Xitu, Inc., 2551 Casey Ave. Ste A, Mountain View, CA 94042, 3Dept. Geological Sciences, Indiana University, Bloomington, IN 47405, 4Hydrology, Geochemistry, and Geology, Los Alamos National Laboratory, MS D469, Los Alamos, NM 87545, 5NASA Johnson Space Center, Houston, TX 77058, MS 300-315L, Pasadena, CA 91109, 6MS 183-501, Jet Propulsion Laboratory, Pasadena, CA 91109 Introduction: An important goal of the Mars Sci- a 600X600 front-illuminated frame transfer device ence Laboratory (MSL ’09) mission is the determina- having 40 !m square pixels, a deep depletion zone for tion of definitive mineralogy and chemical composi- high quantum efficiency of 7 KeV X-rays (CoK"), tion of Mars soil and rocks. CheMin is a miniature and a thin polygate structure for enhanced sensitivity X-ray diffraction (XRD) instrument that has been cho- to lower atomic number elements such as Mg. sen for the analytical laboratory of MSL [1]. CheMin uses a microfocus-source Co X-ray tube, a transmis- Table 1: Critical source and detector requirements. sion sample cell, and an energy-discriminating X-ray sensitive CCD to produce simultaneous 2-D XRD pat- Parameter Value terns and energy-dispersive X-ray histograms from powdered samples. A diagram of the instrument ge- 2! range 5-50° 2! ometry is shown in Figure 1. -
David Vaniman, Steve Chipera, Patricia Craig Calendar Year 2018 I
David Vaniman, Steve Chipera, Patricia Craig Calendar Year 2018 I. Report on research For calendar year 2018, focus remained on the Mars Science Laboratory (MSL) mission. Vaniman’s involvement with MSL continued in roles with two instruments, the CheMin X-ray diffraction (XRD) and X-ray florescence (XRF) instrument and, to lesser extent, the ChemCam laser-induced breakdown spectroscopy (LIBS) and remote micro-imager (RMI) instrument. Chipera and Craig are involved with the CheMin instrument. (1) Research at the MSL Gale Crater Field Site on Mars (1a) CheMin Instrument on MSL. David Vaniman is a Co-I on the CheMin instrument for Mars Science Laboratory (MSL); the PI is Tom Bristow of NASA Ames. This report also covers Steve Chipera, who is a Co-I for the CheMin instrument, and Patricia Craig, who is a Postdoctoral Research Scientist for the CheMin team. Steve Chipera works through PSI as a Senior Research Associate for the MSL mission and reports to Dave Vaniman. Patricia Craig, who is a Postdoctoral Research Scientist at PSI, also reports to Dave Vaniman. Vaniman has tactical, data analysis, and Planetary data System (PDS) reporting roles for MSL. Steve Chipera has a data analysis role and Patricia Craig has both tactical and data analysis roles for MSL. As members of the CheMin Science Team tasked with operations, Vaniman’s and Craig’s tactical participation included operations in the role of combined Payload Uplink Lead and Payload Downlink Lead (PUDL). With Dick Morris (NASA-JSC) and Mike Wilson (NASA-Ames), Vaniman completed three additional rounds of data delivery for the Planetary Data System (PDS), one on February 16, 2018 (PDS release #17), one on June 29, 2018 (PDS release #18), and one on November 2, 2018 (PDS release #19). -
A Review of Sample Analysis at Mars-Evolved Gas Analysis Laboratory Analog Work Supporting the Presence of Perchlorates and Chlorates in Gale Crater, Mars
minerals Review A Review of Sample Analysis at Mars-Evolved Gas Analysis Laboratory Analog Work Supporting the Presence of Perchlorates and Chlorates in Gale Crater, Mars Joanna Clark 1,* , Brad Sutter 2, P. Douglas Archer Jr. 2, Douglas Ming 3, Elizabeth Rampe 3, Amy McAdam 4, Rafael Navarro-González 5,† , Jennifer Eigenbrode 4 , Daniel Glavin 4 , Maria-Paz Zorzano 6,7 , Javier Martin-Torres 7,8, Richard Morris 3, Valerie Tu 2, S. J. Ralston 2 and Paul Mahaffy 4 1 GeoControls Systems Inc—Jacobs JETS Contract at NASA Johnson Space Center, Houston, TX 77058, USA 2 Jacobs JETS Contract at NASA Johnson Space Center, Houston, TX 77058, USA; [email protected] (B.S.); [email protected] (P.D.A.J.); [email protected] (V.T.); [email protected] (S.J.R.) 3 NASA Johnson Space Center, Houston, TX 77058, USA; [email protected] (D.M.); [email protected] (E.R.); [email protected] (R.M.) 4 NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA; [email protected] (A.M.); [email protected] (J.E.); [email protected] (D.G.); [email protected] (P.M.) 5 Institito de Ciencias Nucleares, Universidad Nacional Autonoma de Mexico, Mexico City 04510, Mexico; [email protected] 6 Centro de Astrobiología (INTA-CSIC), Torrejon de Ardoz, 28850 Madrid, Spain; [email protected] 7 Department of Planetary Sciences, School of Geosciences, University of Aberdeen, Aberdeen AB24 3FX, UK; [email protected] 8 Instituto Andaluz de Ciencias de la Tierra (CSIC-UGR), Armilla, 18100 Granada, Spain Citation: Clark, J.; Sutter, B.; Archer, * Correspondence: [email protected] P.D., Jr.; Ming, D.; Rampe, E.; † Deceased 28 January 2021.