Aberystwyth University Infrared Spectrometer for Exomars
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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. -
Cumulated Bibliography of Biographies of Ocean Scientists Deborah Day, Scripps Institution of Oceanography Archives Revised December 3, 2001
Cumulated Bibliography of Biographies of Ocean Scientists Deborah Day, Scripps Institution of Oceanography Archives Revised December 3, 2001. Preface This bibliography attempts to list all substantial autobiographies, biographies, festschrifts and obituaries of prominent oceanographers, marine biologists, fisheries scientists, and other scientists who worked in the marine environment published in journals and books after 1922, the publication date of Herdman’s Founders of Oceanography. The bibliography does not include newspaper obituaries, government documents, or citations to brief entries in general biographical sources. Items are listed alphabetically by author, and then chronologically by date of publication under a legend that includes the full name of the individual, his/her date of birth in European style(day, month in roman numeral, year), followed by his/her place of birth, then his date of death and place of death. Entries are in author-editor style following the Chicago Manual of Style (Chicago and London: University of Chicago Press, 14th ed., 1993). Citations are annotated to list the language if it is not obvious from the text. Annotations will also indicate if the citation includes a list of the scientist’s papers, if there is a relationship between the author of the citation and the scientist, or if the citation is written for a particular audience. This bibliography of biographies of scientists of the sea is based on Jacqueline Carpine-Lancre’s bibliography of biographies first published annually beginning with issue 4 of the History of Oceanography Newsletter (September 1992). It was supplemented by a bibliography maintained by Eric L. Mills and citations in the biographical files of the Archives of the Scripps Institution of Oceanography, UCSD. -
Characterization of the Stray Light in a Space Borne Atmospheric AOTF Spectrometer
Characterization of the stray light in a space borne atmospheric AOTF spectrometer Korablev Oleg 1, Fedorova Anna 1, Eric Villard 2,3, Lilian Joly 4, Alexander Kiselev 1, Denis Belyaev 1, Jean-Loup Bertaux 2 1Space Research Institute (IKI), 84/32 Profsoyuznaya, 117997 Moscow, Russia; Moscow Institute of Physics and Technology, Institutsky dr. 9, 141700 Dolgoprudnyi, Russia 2LATMOS/CNRS, 78280 Guyancourt , France. 3ALMA/European Southern Observatory, Santiago, Chile 4GSMA/CNRS Univ. de Reims, Moulin de la Housse, BP 1039, 51687 Reims, France. [email protected] Abstract : Acousto-optic tunable filter (AOTF) spectrometers are being criticized for spectral leakage, distant side lobes of their spectral response (SRF) function, or the stray light. SPICAM-IR is the AOTF spectrometer in the range 1000-1700 nm with a resolving power of 1800-2200 operating on the Mars Express interplanetary probe. It is primarily dedicated to measurements of water vapor in the Martian atmosphere. SPICAM H2O retrievals are generally lower than simultaneous measurements with other instruments, the stray light suggested as a likely explanation. We report the results of laboratory measurements of water vapor in quantity characteristic for the Mars atmosphere with the Flight Spare model of SPICAM-IR. The level of the stray light is below 1.3·10 -4, and the accuracy to measure water vapor is ~0.2 pr. µm, mostly determined by measurement uncertainties and the accuracy of the synthetic modeling. We demonstrate that the AOTF spectrometer dependably measures the water abundance and can be employed as an atmospheric spectrometer. References and links 1. N. J. Chanover, D. A. -
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]. -
Status After the Venus Flybys
Acta Astronautica 63 (2008) 68–73 www.elsevier.com/locate/actaastro The MESSENGER mission to Mercury: Status after the Venusflybys Ralph L. McNutt Jr.a,∗, Sean C. Solomonb, David G. Granta, Eric J. Finnegana, Peter D. Bedinia, the MESSENGER Team aThe Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723, USA bDepartment of Terrestrial Magnetism, Carnegie Institution of Washington, 5241 Broad Branch Road, N.W., Washington, DC 20015, USA Available online 21 April 2008 Abstract NASA’s MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) spacecraft, launched on 3 August 2004, is well into its voyage to initiate a new era in our understanding of the terrestrial planets. The mission, spacecraft, and payload are designed to answer six fundamental questions regarding the innermost planet during three flybys and a one-year-long, near-polar-orbital observational campaign. The cruise phase to date has been used to commission the spacecraft and instruments and begin the transition to automated use of the instruments with on-board, time-tagged commands. An Earth flyby one year after launch, a large propulsive maneuver in December 2005, and Venus flybys in October 2006 and June 2007 began the process of changing MESSENGER’s heliocentric motion. The second Venus flyby was also used to complete final rehearsals for Mercury flyby operations in January 2008 while coordinating observations with the European Space Agency’s Venus Express mission. The upcoming Mercury flyby will be the first since that of Mariner 10 in 1975. Along with the second and third MESSENGER flybys in October 2008 and September 2009, that flyby will provide images of the hemisphere of Mercury never seen before by spacecraft as well as the first high-resolution information on Mercury’s surface mineralogy. -
Navigation Challenges During Exomars Trace Gas Orbiter Aerobraking Campaign
NON-PEER REVIEW Please select category below: Normal Paper Student Paper Young Engineer Paper Navigation Challenges during ExoMars Trace Gas Orbiter Aerobraking Campaign Gabriele Bellei 1, Francesco Castellini 2, Frank Budnik 3 and Robert Guilanyà Jané 4 1 DEIMOS Space located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 2 Telespazio VEGA located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 3 ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 4 GMV INSYEN located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany Abstract The ExoMars Trace Gas Orbiter satellite spent one year in aerobraking operations at Mars, lowering its orbit period from one sol to about two hours. This delicate phase challenged the operations team and in particular the navigation system due to the highly unpredictable Mars atmosphere, which imposed almost continuous monitoring, navigation and re-planning activities. An aerobraking navigation concept was, for the first time at ESA, designed, implemented and validated on-ground and in-flight, based on radiometric tracking data and complemented by information extracted from spacecraft telemetry. The aerobraking operations were successfully completed, on time and without major difficulties, thanks to the simplicity and robustness of the selected approach. This paper describes the navigation concept, presents a recollection of the main in-flight results and gives a retrospective of the main lessons learnt during this activity. Keywords: ExoMars, Trace Gas Orbiter, aerobraking, navigation, orbit determination, Mars atmosphere, accelerometer Introduction The ExoMars program is a cooperation between the European Space Agency (ESA) and Roscosmos for the robotic exploration of the red planet. -
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. -
Appendix I Lunar and Martian Nomenclature
APPENDIX I LUNAR AND MARTIAN NOMENCLATURE LUNAR AND MARTIAN NOMENCLATURE A large number of names of craters and other features on the Moon and Mars, were accepted by the IAU General Assemblies X (Moscow, 1958), XI (Berkeley, 1961), XII (Hamburg, 1964), XIV (Brighton, 1970), and XV (Sydney, 1973). The names were suggested by the appropriate IAU Commissions (16 and 17). In particular the Lunar names accepted at the XIVth and XVth General Assemblies were recommended by the 'Working Group on Lunar Nomenclature' under the Chairmanship of Dr D. H. Menzel. The Martian names were suggested by the 'Working Group on Martian Nomenclature' under the Chairmanship of Dr G. de Vaucouleurs. At the XVth General Assembly a new 'Working Group on Planetary System Nomenclature' was formed (Chairman: Dr P. M. Millman) comprising various Task Groups, one for each particular subject. For further references see: [AU Trans. X, 259-263, 1960; XIB, 236-238, 1962; Xlffi, 203-204, 1966; xnffi, 99-105, 1968; XIVB, 63, 129, 139, 1971; Space Sci. Rev. 12, 136-186, 1971. Because at the recent General Assemblies some small changes, or corrections, were made, the complete list of Lunar and Martian Topographic Features is published here. Table 1 Lunar Craters Abbe 58S,174E Balboa 19N,83W Abbot 6N,55E Baldet 54S, 151W Abel 34S,85E Balmer 20S,70E Abul Wafa 2N,ll7E Banachiewicz 5N,80E Adams 32S,69E Banting 26N,16E Aitken 17S,173E Barbier 248, 158E AI-Biruni 18N,93E Barnard 30S,86E Alden 24S, lllE Barringer 29S,151W Aldrin I.4N,22.1E Bartels 24N,90W Alekhin 68S,131W Becquerei -
The Very Forward CASTOR Calorimeter of the CMS Experiment
EUROPEAN ORGANIZATION FOR NUCLEAR RESEARCH (CERN) CERN-EP-2020-180 2021/02/11 CMS-PRF-18-002 The very forward CASTOR calorimeter of the CMS experiment The CMS Collaboration* Abstract The physics motivation, detector design, triggers, calibration, alignment, simulation, and overall performance of the very forward CASTOR calorimeter of the CMS exper- iment are reviewed. The CASTOR Cherenkov sampling calorimeter is located very close to the LHC beam line, at a radial distance of about 1 cm from the beam pipe, and at 14.4 m from the CMS interaction point, covering the pseudorapidity range of −6.6 < h < −5.2. It was designed to withstand high ambient radiation and strong magnetic fields. The performance of the detector in measurements of forward energy density, jets, and processes characterized by rapidity gaps, is reviewed using data collected in proton and nuclear collisions at the LHC. ”Published in the Journal of Instrumentation as doi:10.1088/1748-0221/16/02/P02010.” arXiv:2011.01185v2 [physics.ins-det] 10 Feb 2021 © 2021 CERN for the benefit of the CMS Collaboration. CC-BY-4.0 license *See Appendix A for the list of collaboration members Contents 1 Contents 1 Introduction . .1 2 Physics motivation . .3 2.1 Forward physics in proton-proton collisions . .3 2.2 Ultrahigh-energy cosmic ray air showers . .5 2.3 Proton-nucleus and nucleus-nucleus collisions . .5 3 Detector design . .6 4 Triggers and operation . .9 5 Event reconstruction and calibration . 12 5.1 Noise and baseline . 13 5.2 Gain correction factors . 15 5.3 Channel-by-channel intercalibration . -
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.