The Next Frontier for Planetary and Human Exploration
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Mars Express Orbiter Radio Science
MaRS: Mars Express Orbiter Radio Science M. Pätzold1, F.M. Neubauer1, L. Carone1, A. Hagermann1, C. Stanzel1, B. Häusler2, S. Remus2, J. Selle2, D. Hagl2, D.P. Hinson3, R.A. Simpson3, G.L. Tyler3, S.W. Asmar4, W.I. Axford5, T. Hagfors5, J.-P. Barriot6, J.-C. Cerisier7, T. Imamura8, K.-I. Oyama8, P. Janle9, G. Kirchengast10 & V. Dehant11 1Institut für Geophysik und Meteorologie, Universität zu Köln, D-50923 Köln, Germany Email: [email protected] 2Institut für Raumfahrttechnik, Universität der Bundeswehr München, D-85577 Neubiberg, Germany 3Space, Telecommunication and Radio Science Laboratory, Dept. of Electrical Engineering, Stanford University, Stanford, CA 95305, USA 4Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91009, USA 5Max-Planck-Instuitut für Aeronomie, D-37189 Katlenburg-Lindau, Germany 6Observatoire Midi Pyrenees, F-31401 Toulouse, France 7Centre d’etude des Environnements Terrestre et Planetaires (CETP), F-94107 Saint-Maur, France 8Institute of Space & Astronautical Science (ISAS), Sagamihara, Japan 9Institut für Geowissenschaften, Abteilung Geophysik, Universität zu Kiel, D-24118 Kiel, Germany 10Institut für Meteorologie und Geophysik, Karl-Franzens-Universität Graz, A-8010 Graz, Austria 11Observatoire Royal de Belgique, B-1180 Bruxelles, Belgium The Mars Express Orbiter Radio Science (MaRS) experiment will employ radio occultation to (i) sound the neutral martian atmosphere to derive vertical density, pressure and temperature profiles as functions of height to resolutions better than 100 m, (ii) sound -
JUICE Red Book
ESA/SRE(2014)1 September 2014 JUICE JUpiter ICy moons Explorer Exploring the emergence of habitable worlds around gas giants Definition Study Report European Space Agency 1 This page left intentionally blank 2 Mission Description Jupiter Icy Moons Explorer Key science goals The emergence of habitable worlds around gas giants Characterise Ganymede, Europa and Callisto as planetary objects and potential habitats Explore the Jupiter system as an archetype for gas giants Payload Ten instruments Laser Altimeter Radio Science Experiment Ice Penetrating Radar Visible-Infrared Hyperspectral Imaging Spectrometer Ultraviolet Imaging Spectrograph Imaging System Magnetometer Particle Package Submillimetre Wave Instrument Radio and Plasma Wave Instrument Overall mission profile 06/2022 - Launch by Ariane-5 ECA + EVEE Cruise 01/2030 - Jupiter orbit insertion Jupiter tour Transfer to Callisto (11 months) Europa phase: 2 Europa and 3 Callisto flybys (1 month) Jupiter High Latitude Phase: 9 Callisto flybys (9 months) Transfer to Ganymede (11 months) 09/2032 – Ganymede orbit insertion Ganymede tour Elliptical and high altitude circular phases (5 months) Low altitude (500 km) circular orbit (4 months) 06/2033 – End of nominal mission Spacecraft 3-axis stabilised Power: solar panels: ~900 W HGA: ~3 m, body fixed X and Ka bands Downlink ≥ 1.4 Gbit/day High Δv capability (2700 m/s) Radiation tolerance: 50 krad at equipment level Dry mass: ~1800 kg Ground TM stations ESTRAC network Key mission drivers Radiation tolerance and technology Power budget and solar arrays challenges Mass budget Responsibilities ESA: manufacturing, launch, operations of the spacecraft and data archiving PI Teams: science payload provision, operations, and data analysis 3 Foreword The JUICE (JUpiter ICy moon Explorer) mission, selected by ESA in May 2012 to be the first large mission within the Cosmic Vision Program 2015–2025, will provide the most comprehensive exploration to date of the Jovian system in all its complexity, with particular emphasis on Ganymede as a planetary body and potential habitat. -
Mars Subsurface Water Ice Mapping (Swim): Radar Subsurface Reflectors
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 2069.pdf MARS SUBSURFACE WATER ICE MAPPING (SWIM): RADAR SUBSURFACE REFLECTORS. A. M. Bramson1, E. I. Petersen1, Z. M. Bain2, N. E. Putzig2, G. A. Morgan2, M. Mastrogiuseppe3, M. R. Perry2, I. B. Smith2, H. G. Sizemore2, D. M. H. Baker4, R. H. Hoover5, B. A. Campbell6. 1Lunar and Planetary Laboratory, University of Arizona ([email protected]), 2Planetary Science Institute, 3California Institute of Technology, 4NASA Goddard Space Flight Center, 5Southwest Research Institute, 6Smithsonian Institution Introduction: The Subsurface Water Ice Mapping Consistency Mapping: To enable a quantitative as- (SWIM) in the Northern Hemisphere of Mars, supports sessment of how consistent (or inconsistent) the various an effort by NASA’s Mars Exploration Program to de- remote sensing datasets are with the presence of shallow termine in situ resource availability. We are performing (<5 m) and deep (>5 m) ice across these regions, we in- global reconnaissance mapping as well as focused troduce the SWIM Equation. Outlined in detail by Perry multi-dataset mapping from 0º to 60ºN in four longitude et al. [this LPSC], the SWIM Equation yields con- bands: “Arcadia” (150–225ºE, which also contains our sistency values ranging between +1 and -1, where +1 pilot study region), “Acidalia” (290–360ºE), “Onilus” means that the data are consistent with the presence of (0–70ºE, which covers Deuteronilus and Protonilus ice, 0 means that the data give no indications of the pres- Mensae), and “Utopia” (70–150ºE). Our maps are being ence or absence of ice, and -1 means that the data are made available to the community on the SWIM Project inconsistent with the presence of ice. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
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. -
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, -
Estimated Attenuation Rates Using GPR and TDR in Volcanic Depos
PUBLICATIONS Journal of Geophysical Research: Planets RESEARCH ARTICLE Electromagnetic signal penetration in a planetary soil 10.1002/2016JE005192 simulant: Estimated attenuation rates using GPR Key Points: and TDR in volcanic deposits on Mount Etna • GPR methodologies for evaluating the loss tangent of volcanic sediments S. E. Lauro1 , E. Mattei1 , B. Cosciotti1 , F. Di Paolo1 , S. A. Arcone2, M. Viccaro3,4 , • Characterization of electrical 1 properties of a planetary soil simulant and E. Pettinelli • Comparison between GPR and TDR 1 2 measurements Dipartimento di Matematica e Fisica, Università degli Studi Roma TRE, Rome, Italy, US Army ERDC-CRREL, Hanover, New Hampshire, USA, 3Dipartimento di Scienze Biologiche Geologiche e Ambientali, Università degli Studi di Catania, Catania, Italy, 4Osservatorio Etneo, Istituto Nazionale di Geofisica e Vulcanologia, Catania, Italy Correspondence to: S. E. Lauro, Abstract Ground-penetrating radar (GPR) is a well-established geophysical terrestrial exploration method [email protected] and has recently become one of the most promising for planetary subsurface exploration. Several future landing vehicles like EXOMARS, 2020 NASA ROVER, and Chang’e-4, to mention a few, will host GPR. A GPR Citation: survey has been conducted on volcanic deposits on Mount Etna (Italy), considered a good analogue for Lauro, S. E., E. Mattei, B. Cosciotti, F. Di Paolo, S. A. Arcone, M. Viccaro, and Martian and Lunar volcanic terrains, to test a novel methodology for subsoil dielectric properties estimation. E. Pettinelli (2017), Electromagnetic The stratigraphy of the volcanic deposits was investigated using 500 MHz and 1 GHz antennas in two different signal penetration in a planetary soil configurations: transverse electric and transverse magnetic. -
DSCOVR Magnetometer Observations Adam Szabo, Andriy Koval NASA Goddard Space Flight Center
DSCOVR Magnetometer Observations Adam Szabo, Andriy Koval NASA Goddard Space Flight Center 1 Locations of the Instruments Faraday Cup EPIC Omni Antenna Star Tracker Thruster Modules Digital Sun Sensor Electron Spectrometer +Z +X Magnetometer +Y 2 Goddard Fluxgate Magnetometer The Fluxgate Magnetometer measures the interplanetary vector magnetic field It is located at the tip of a 4.0 m boom to minimize the effect of spacecraft fields Requirement Value Method Performance Magnetometer Range 0.1-100 nT Test 0.004-65,500 nT Accuracy +/- 1 nT Measured +/- 0.2 nT Cadence 1 min Measured 50 vector/sec 3 Pre-flight Calibration • Determined the magnetometer zero levels, scale factors, and magnetometer orthogonalization matrix. • Determined the spacecraft generated magnetic fields – Subsystem level magnetic tests. Reaction wheels, major source of dynamic field, were shielded – Spacecraft unpowered magnetic test in the GSFC 40’ magnetic facility In-Flight Boom Deployment • Nominal deployment on 2/15/15, seen as 4.4 rotations in the magnetometer components Mostly spacecraft Boom deployment Interplanetary magnetic field induced fields 5 Alfven Waves in the Solar Wind • The solar wind contains magnetic field rotations that preserve the magnitude of the field, so called Alfven waves. • Alfven waves are ubiquitous and are possible to identify with automated routines. • Systematic deviations from a constant field magnitude during these waves are an indication of spacecraft induced offsets. • Minimizing the deviations with slowly changing offsets allows in-flight calibrations. 6 In-Flight Magnetometer Calibrations Z Magnetometer Zero Offsets X • X axis Roll and Z axis Slew data is Y consistent with ground calibration estimates X • Independent zero offset determination by rolls, slews and using solar wind Alfvenicity give consistent values Z • Time variation is consistent with yearly orbital change. -
Range Resolution Enhancement of WISDOM/Exomars
Range resolution enhancement of WISDOM/ExoMars radar soundings by the Bandwidth Extrapolation technique: Validation and application to field campaign measurements Nicolas Oudart, Valérie Ciarletti, Alice Le Gall, Marco Mastrogiuseppe, Yann Herve, Wolf-Stefan Benedix, Dirk Plettemeier, Vivien Tranier, Rafik Hassen-Khodja, Christoph Statz, et al. To cite this version: Nicolas Oudart, Valérie Ciarletti, Alice Le Gall, Marco Mastrogiuseppe, Yann Herve, et al.. Range resolution enhancement of WISDOM/ExoMars radar soundings by the Bandwidth Extrapolation tech- nique: Validation and application to field campaign measurements. Planetary and Space Science, Elsevier, 2021, 197 (March), pp.105173. 10.1016/j.pss.2021.105173. insu-03114236v2 HAL Id: insu-03114236 https://hal-insu.archives-ouvertes.fr/insu-03114236v2 Submitted on 28 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. Distributed under a Creative Commons Attribution| 4.0 International License Planetary and Space Science 197 (2021) 105173 Contents lists available at ScienceDirect Planetary -
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. -
An Approach to Magnetic Cleanliness for the Psyche Mission M
An Approach to Magnetic Cleanliness for the Psyche Mission M. de Soria-Santacruz J. Ream K. Ascrizzi ([email protected]), ([email protected]), ([email protected]) M. Soriano R. Oran University of Michigan Ann Arbor ([email protected]), ([email protected]), 500 S State St O. Quintero B. P. Weiss Ann Arbor, MI 48109 ([email protected]), ([email protected]) F. Wong Department of Earth, Atmospheric, ([email protected]), and Planetary Sciences S. Hart Massachusetts Institute of Technology ([email protected]), 77 Massachusetts Avenue M. Kokorowski Cambridge, MA 02139 ([email protected]) B. Bone ([email protected]), B. Solish ([email protected]), D. Trofimov ([email protected]), E. Bradford ([email protected]), C. Raymond ([email protected]), P. Narvaez ([email protected]) Jet Propulsion Laboratory, California Institute of Technology 4800 Oak Grove Drive Pasadena, CA 91109 C. Keys C. Russell L. Elkins-Tanton ([email protected]), ([email protected]), ([email protected]) P. Lord University of California Los Angeles Arizona State University ([email protected]) 405 Hilgard Avenue PO Box 871404 Maxar Technologies Inc. Los Angeles, CA 90095 Tempe, AZ 85287 3825 Fabian Avenue Palo Alto, CA 94303 Abstract— Psyche is a Discovery mission that will visit the fields. Limiting and characterizing spacecraft-generated asteroid (16) Psyche to determine if it is the metallic core of a magnetic fields is therefore essential to the mission. This is the once larger differentiated body or otherwise was formed from objective of the Psyche’s magnetics control program described accretion of unmelted metal-rich material. -
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.