Accessing Pds Data in Pipeline Processing and Web Sites Through Pds Geosciences Orbital Data Explorer’S Web-Based Api (Rest) Interface

Total Page:16

File Type:pdf, Size:1020Kb

Accessing Pds Data in Pipeline Processing and Web Sites Through Pds Geosciences Orbital Data Explorer’S Web-Based Api (Rest) Interface 45th Lunar and Planetary Science Conference (2014) 1026.pdf ACCESSING PDS DATA IN PIPELINE PROCESSING AND WEB SITES THROUGH PDS GEOSCIENCES ORBITAL DATA EXPLORER’S WEB-BASED API (REST) INTERFACE. K. J. Bennett, J. Wang, D. Scholes, Washington University in St. Louis, 1 Brookings Drive, Campus Box 1169, St. Louis, Missouri, 63130, {bennett, wang, sholes}@wunder.wustl.edu. Introduction: The Orbital Data Explorer (ODE) is tem (RSS). a web-based search tool (http://ode.rsl.wustl.edu) de- High Resolution Stereo Camera (HRSC), Mars Advanced Radar for Subsurface and Iono- veloped at NASA’s Planetary Data System’s (PDS) sphere Sounding (MARSIS), OMEGA Geosciences Node (http://pds-geosciences.wustl.edu/). Mars Express (Observatoire Mineralogie, Eau, Glaces, Through ODE, users can search, browse, and download Activite) Visible and Infrared Mineralogical a wide range of PDS Mars, Moon, Mercury, and Venus Mapping Spectrometer, and Planetary Fourier Spectrometer (PFS). data ([1,2,3,4]). Mars Orbiter Laser Altimeter (MOLA), and Mars Global In the fall of 2012, the Geosciences node intro- MOC Narrow Angle (NA) and Wide Angle Surveyor (MGS) duced a simple web-based API that allows non-PDS (WA) cameras. Gamma Ray Spectrometer (GRS) and Thermal web and processing tools to search for PDS products, Odyssey Emission Imaging System (THEMIS) obtain meta-data about those products, and download Viking Orbiter Visual Imaging Subsystem Camera A/B the products stored in ODE’s meta-data database. The Gamma Ray Spectrometer (GRS), Radio Sci- first version is now used by several teams in periodic MESSENGER ence Subsystem (RSS), Neutron Spectrometer processing and web sites. (Mercury Sur- (NS), X-Ray Spectrometer (XRS), face, Space MERCURY Atmospheric and Surface Com- ODE Overview: ODE provides a cross-mission, Environment, position Spectrometer (MASCS), Mercury cross-instrument searchable web tools for finding and Geochemistry Laser Altimeter (MLA), and Mercury Dual downloading single or multiple PDS compliant archive and Ranging) Imaging System (MDIS) Narrow Angle Cam- data products for Mars, Mercury, Venus, and the era (NAC) and Wide Angle Camera (WAC). Ultraviolet-Visual (UV-VIS) Camera, Long- Earth’s Moon. The basic structure of ODE is shown in wave Infrared (LWIR) Camera, High- Figure 1. It consists of a back-end processor named resolution (HiRes) Camera, Near-Infrared Clementine Bunter, a metadata database, a front-end web interface, (NIR) Camera, two Star Tracker Cameras, and and, as of 2012, a web-based REST (Representational Laser Image Detection and Ranging (LIDAR) system. State Transfer) interface. Gamma Ray Spectrometer (GRS), Neutron Lunar Spectrometer (NS), Alpha Particle Spectrome- Limited PDS PDS Mission Prospector ter (APS), Magnetometer (MAG), and Elec- Imaging Geosciences Data Instrument Node Node tron Reflectometer (ER). Instrument Spacecraft PDS HiRISE DIVINER Lunar Radiometer Experiment, Orbital Data Explorer (ODE) Instrument Data Node ODE REST External Lymap Alpha Mapping Project (LAMP), Instrument Interface Tools PDS Lunar Atmopheres Lunar Exploration Neutron Detector (LEND), Node Instrument ODE Backend Reconnaissance Spacecraft Processor ODE (Bunter) Metadata Lunar Orbiter Laser Altimeter (LOLA), Lunar Instrument PDS Database Orbiter (LRO) PPI ODE Web Reconnaissance Orbiter Camera (LROC), Instrument Node Interface Domain Spacecraft Scientist Mini-RF Instrument PDS THEMIS Data Node Moon Mineralogy Mapper (M3), Forerunner Instrument Chandrayaan-1 Instrument PDS (aka Mini-RF or Mini-SAR) Spacecraft LOLA Data Node 24-Inch Focal Length Camera, 80mm Focal Lunar Orbiter PDS Lunar Orbiter Planetary USGS LROC Digitized File Base Products UPC Data Length Camera Data Node Archive GRAIL LGRS (Lunar Gravity Ranging System) in- Figure 1. ODE Structure with REST Interface (Gravity Recov- cluding the Radio Science System ODE currently supports multiple mission data ery and Interior products for Mars, Moon, Venus and Mercury. The Laboratory) various datasets imported from different instruments Magellan Radar System, Radio Science Subsystem and missions are listed in Table 1. A detailed list of ODE Metadatabase: Behind the scenes, Bunter current ODE holdings can be found at scans the various PDS nodes, PDS data nodes, and http://wufs.wustl.edu/ode/odeholdings/index.html. other data sources to extract metadata about PDS prod- Table 1. ODE Data Holdings ucts. This metadata is stored in the ODE metadata da- Mission Instrument tabase. This database is the core of both the ODE web Shallow Radar (SHARAD), Compact Recon- site and ODE REST interface. Through this database, naissance Imaging Spectrometers for Mars Mars ODE also stores direct links to the PDS product files (CRISM), High Resolution Imaging Science Reconnaissance Experiment (HiRISE), Context Imager (CTX), allowing direct access to those product files as needed. Orbiter (MRO) Mars Color Imager (MARCI), Mars Climate Granular Data: In addition to PDS products, ODE Sounder (MCS), and Radio Science Subsys- also offers a set of “granular data” tools for extracting 45th Lunar and Planetary Science Conference (2014) 1026.pdf granular-level data from selected PDS products. These </QuerySummary> tools allow users to select granular-level observation <Count>353</Count> data from a range of PDS products that cover selected </ODEResults> areas and that meet specific criteria. REST Product Queries: The ODE REST inter- Currently, ODE supports granular-level search face allows external tools to query ODE for a wide tools for MGS MOLA PEDR (Precision Experiment range of data including product metadata. Product Data Record), LRO LOLA RDR (Reduced Data Rec- metadata, which varies depending on the data set, in- ord) and Diviner RDR. These data sets consist of or- cludes observation times, creation times, map resolu- bit-track oriented products where specific measure- tions/scales, observation angles, solar longitudes, solar ments were taken along orbit tracks in time-sequence distances, spacecraft clock times, version numbers, chunks. To facilitate granular-level searches, the indi- activity ids, producer information, and links to instru- vidual granular-level data records are extracted from ment web sites. Queries can be limited by instrument the products and stored in granular databases. Each hosts, instruments, product types, data set ids, location, granular database has global coverage of the data features, observation times, and creation times. Loca- products. The MOLA searchable database includes tion limits can be based on the “intersecting”, “con- approximately 595 million individual PEDR measure- tains”, or “contained by” geographic relationships be- ments. There are approximately 6 billion and 30 billion tween products intersecting a surface lat/lon bounding records for LOLA and Diviner data respectively. box or footprint. Using a series of queries can produce REST Interface Overview: The ODE Represen- a very sophisticated result that find spatial and tem- tational State Transfer (REST) interface is a simple poral relationships between various products. web-based interface allowing external users and tools REST Granluar Queries: In addition to the PDS to access the ODE metadata and products. product queries, the current ODE REST interface also REST query. The current ODE REST interface on- supports LOLA RDR granular-level queries. The re- ly supports read-only GET functions. The query format sults are the same as the current ODE web-based basically breaks down into several components includ- LOLA RDR granular query including Comma- ing target, query type, output format, and query param- Separated Value (CSV) text files, shapefiles, and eters. A simple query will return a variety of data such binned images. as a list of products, product metadata, product foot- REST Access: The REST interface is accessable at prints, product browse images, or even the products http://oderest.rsl.wustl.edu/live/. Interested users themselves. Results are typically in XML or JSON should contact the author for more information at ben- format except in cases where the return is an image. [email protected]. Product file requests return one or more web-addresses Future Developments: The Geosciences node is for directly downloading the file(s). working on Version 2.0 of the ODE REST interface. Example. A simple example of using the REST in- This version will include additional product query lim- terface to find how many HiRISE Version 1.1 RDR its (example: emission, incidence, and phase angles) as products exist within a latitudes 0 to 10 and longitudes well as expanding the granular queries to include 0 to 10: MOLA PEDR and Diviner RDR queries similar to the http://oderest.rsl.wustl.edu/live?target=mars&query=pr current web-based tools. In addition, the granular-level oducts&results=c&iid=HIRISE&pt=RDRV11&maxlat queries will be accessable through a standard Open =10.0&minlat=0.0&westernlon=0.0&easternlon=10.0 Geospatial Consortium (OGC) Web-Feature Service Returns (formatted for readability): (WFS) interface. <ODERsults> Contact Information: The Geosciences Node <Status>Success</Status> welcomes questions and comments from the user <QuerySummary> community. Please send email to <Date>2013-12-18T09:07:08.197</Date> [email protected]. Comments on ODE and <target>MARS</target> questions on REST access can be sent to ben- <query>PRODUCT</query> [email protected]. <results>C</results> References: [1] Bennett, K. et al. (2008), LPS <iid>HIRISE</iid> XXXIX, Abstract #1379. [2] Wang, J. et al. (2009), <pt>RDRV11</pt> LPS XL, Abstract #1193. [3] Wang, J. et al. (2010), <westernlon>0</westernlon> LPS XLI, Abstract #2251. [4] Bennett, K. et al. (2013), <easternlon>10</easternlon> 44th LPS, Abstract #1310. <minlat>0</minlat> <maxlat>10</maxlat> .
Recommended publications
  • 2018: Aiaa-Space-Report
    AIAA TEAM SPACE TRANSPORTATION DESIGN COMPETITION TEAM PERSEPHONE Submitted By: Chelsea Dalton Ashley Miller Ryan Decker Sahil Pathan Layne Droppers Joshua Prentice Zach Harmon Andrew Townsend Nicholas Malone Nicholas Wijaya Iowa State University Department of Aerospace Engineering May 10, 2018 TEAM PERSEPHONE Page I Iowa State University: Persephone Design Team Chelsea Dalton Ryan Decker Layne Droppers Zachary Harmon Trajectory & Propulsion Communications & Power Team Lead Thermal Systems AIAA ID #908154 AIAA ID #906791 AIAA ID #532184 AIAA ID #921129 Nicholas Malone Ashley Miller Sahil Pathan Joshua Prentice Orbit Design Science Science Science AIAA ID #921128 AIAA ID #922108 AIAA ID #761247 AIAA ID #922104 Andrew Townsend Nicholas Wijaya Structures & CAD Trajectory & Propulsion AIAA ID #820259 AIAA ID #644893 TEAM PERSEPHONE Page II Contents 1 Introduction & Problem Background2 1.1 Motivation & Background......................................2 1.2 Mission Definition..........................................3 2 Mission Overview 5 2.1 Trade Study Tools..........................................5 2.2 Mission Architecture.........................................6 2.3 Planetary Protection.........................................6 3 Science 8 3.1 Observations of Interest.......................................8 3.2 Goals.................................................9 3.3 Instrumentation............................................ 10 3.3.1 Visible and Infrared Imaging|Ralph............................ 11 3.3.2 Radio Science Subsystem.................................
    [Show full text]
  • Abstracts of the 50Th DDA Meeting (Boulder, CO)
    Abstracts of the 50th DDA Meeting (Boulder, CO) American Astronomical Society June, 2019 100 — Dynamics on Asteroids break-up event around a Lagrange point. 100.01 — Simulations of a Synthetic Eurybates 100.02 — High-Fidelity Testing of Binary Asteroid Collisional Family Formation with Applications to 1999 KW4 Timothy Holt1; David Nesvorny2; Jonathan Horner1; Alex B. Davis1; Daniel Scheeres1 Rachel King1; Brad Carter1; Leigh Brookshaw1 1 Aerospace Engineering Sciences, University of Colorado Boulder 1 Centre for Astrophysics, University of Southern Queensland (Boulder, Colorado, United States) (Longmont, Colorado, United States) 2 Southwest Research Institute (Boulder, Connecticut, United The commonly accepted formation process for asym- States) metric binary asteroids is the spin up and eventual fission of rubble pile asteroids as proposed by Walsh, Of the six recognized collisional families in the Jo- Richardson and Michel (Walsh et al., Nature 2008) vian Trojan swarms, the Eurybates family is the and Scheeres (Scheeres, Icarus 2007). In this theory largest, with over 200 recognized members. Located a rubble pile asteroid is spun up by YORP until it around the Jovian L4 Lagrange point, librations of reaches a critical spin rate and experiences a mass the members make this family an interesting study shedding event forming a close, low-eccentricity in orbital dynamics. The Jovian Trojans are thought satellite. Further work by Jacobson and Scheeres to have been captured during an early period of in- used a planar, two-ellipsoid model to analyze the stability in the Solar system. The parent body of the evolutionary pathways of such a formation event family, 3548 Eurybates is one of the targets for the from the moment the bodies initially fission (Jacob- LUCY spacecraft, and our work will provide a dy- son and Scheeres, Icarus 2011).
    [Show full text]
  • The Cassini Ion and Neutral Mass Spectrometer (Inms) Investigation
    THE CASSINI ION AND NEUTRAL MASS SPECTROMETER (INMS) INVESTIGATION 1, 2 3 4 J. H. WAITE ∗, JR., W. S. LEWIS ,W.T. KASPRZAK ,V.G. ANICICH , B. P. BLOCK1,T.E. CRAVENS5,G.G. FLETCHER1,W.-H. IP6,J.G. LUHMANN7, R. L. MCNUTT8,H.B. NIEMANN3,J.K.PAREJKO1,J.E. RICHARDS3, R. L. THORPE2, E. M. WALTER1 and R. V. YELLE9 1University of Michigan, Ann Arbor, MI, U.S.A. 2Southwest Research Institute, San Antonio, TX, U.S.A. 3NASA Goddard Space Flight Center, Greenbelt, MD, U.S.A. 4NASA Jet Propulsion Laboratory, Pasadena, CA, U.S.A. 5University of Kansas, Lawrence, KS, U.S.A. 6National Central University, Chung-Li, Taiwan 7University of California, Berkeley, CA, U.S.A. 8Johns Hopkins University Applied Physics Laboratory, Laurel, MD, U.S.A. 9University of Arizona, Flagstaff, AZ, U.S.A. (∗Author for correspondence, E-mail: [email protected]) (Received 13 August 1998; Accepted in final form 17 February 2004) Abstract. The Cassini Ion and Neutral Mass Spectrometer (INMS) investigation will determine the mass composition and number densities of neutral species and low-energy ions in key regions of the Saturn system. The primary focus of the INMS investigation is on the composition and structure of Titan’s upper atmosphere and its interaction with Saturn’s magnetospheric plasma. Of particular interest is the high-altitude region, between 900 and 1000 km, where the methane and nitrogen photochemistry is initiated that leads to the creation of complex hydrocarbons and nitriles that may eventually precipitate onto the moon’s surface to form hydrocarbon–nitrile lakes or oceans.
    [Show full text]
  • ODE Overview Web-Based
    Checkout Version 2.0 K. J. Bennett, J. Wang, and D. Scholes, Washington University in St. Louis, 1 Brookings Drive, Campus Box 1169, St. Louis, Missouri, 63130, {bennett, wang , scholes}@wunder.wustl.edu Beta! ODE Overview http://ode.rsl.wustl.edu/ Planet Mission Instrument Shallow Radar (SHARAD), Compact Reconnaissance Imaging Spectrometer for Mars (CRISM), High Resolution Imaging Science Experiment (HiRISE), Context MRO Orbital Data Explorer Imager (CTX), Mars Color Imager (MARCI), Mars Climate Sounder (MCS), and Radio Science Subsystem (RSS). (ODE) was developed by RETRIEVE and High Resolution Stereo Camera (HRSC), Mars Advanced Radar for Subsurface and NASA’s Planetary Data View Products ESA’s Mars Ionosphere Sounding (MARSIS), OMEGA (Observatoire Mineralogie, Eau, Glaces, System (PDS)’s Mars Express Activite) Visible and Infrared Mineralogical Mapping Spectrometer, and Planetary Fourier Spectrometer (PFS). Geosciences Node. ODE Mars Orbiter Laser Altimeter (MOLA), and Mars Orbiter Camera (MOC) Narrow MGS provides web-based Angle and Wide Angle cameras. functions to search, Odyssey Thermal Emission Imaging System (THEMIS), Gamma Ray Spectrometer (GRS). retrieve, and download SEARCH for Viking Orbiter 1/2 Visual Imaging Subsystem Camera A/B Products data from multiple GRS, RSS, Neutron Spectrometer (NS), X-Ray Spectrometer (XRS), Mercury Atmospheric and Surface Composition Spectrometer (MASCS), Mercury Laser Mercury MESSENGER missions and instruments Altimeter (MLA), and Mercury Dual Imaging System (MDIS) Narrow Angle in the rapidly
    [Show full text]
  • Saturn Satellites As Seen by Cassini Mission
    Saturn satellites as seen by Cassini Mission A. Coradini (1), F. Capaccioni (2), P. Cerroni(2), G. Filacchione(2), G. Magni,(2) R. Orosei(1), F. Tosi(1) and D. Turrini (1) (1)IFSI- Istituto di Fisica dello Spazio Interplanetario INAF Via fosso del Cavaliere 100- 00133 Roma (2)IASF- Istituto di Astrofisica Spaziale e Fisica Cosmica INAF Via fosso del Cavaliere 100- 00133 Roma Paper to be included in the special issue for Elba workshop Table of content SATURN SATELLITES AS SEEN BY CASSINI MISSION ....................................................................... 1 TABLE OF CONTENT .................................................................................................................................. 2 Abstract ....................................................................................................................................................................... 3 Introduction ................................................................................................................................................................ 3 The Cassini Mission payload and data ......................................................................................................................... 4 Satellites origin and bulk characteristics ...................................................................................................................... 6 Phoebe ...............................................................................................................................................................................
    [Show full text]
  • ESA Space Weather STUDY Alcatel Consortium
    ESA Space Weather STUDY Alcatel Consortium SPACE Weather Parameters WP 2100 Version V2.2 1 Aout 2001 C. Lathuillere, J. Lilensten, M. Menvielle With the contributions of T. Amari, A. Aylward, D. Boscher, P. Cargill and S.M. Radicella 1 2 1 INTRODUCTION........................................................................................................................................ 5 2 THE MODELS............................................................................................................................................. 6 2.1 THE SUN 6 2.1.1 Reconstruction and study of the active region static structures 7 2.1.2 Evolution of the magnetic configurations 9 2.2 THE INTERPLANETARY MEDIUM 11 2.3 THE MAGNETOSPHERE 13 2.3.1 Global magnetosphere modelling 14 2.3.2 Specific models 16 2.4 THE IONOSPHERE-THERMOSPHERE SYSTEM 20 2.4.1 Empirical and semi-empirical Models 21 2.4.2 Physics-based models 23 2.4.3 Ionospheric profilers 23 2.4.4 Convection electric field and auroral precipitation models 25 2.4.5 EUV/UV models for aeronomy 26 2.5 METEOROIDS AND SPACE DEBRIS 27 2.5.1 Space debris models 27 2.5.2 Meteoroids models 29 3 THE PARAMETERS ................................................................................................................................ 31 3.1 THE SUN 35 3.2 THE INTERPLANETARY MEDIUM 35 3.3 THE MAGNETOSPHERE 35 3.3.1 The radiation belts 36 3.4 THE IONOSPHERE-THERMOSPHERE SYSTEM 36 4 THE OBSERVATIONS ...........................................................................................................................
    [Show full text]
  • Cassini-Huygens
    High Ambitions for an Outstanding Planetary Mission: Cassini-Huygens Composite image of Titan in ultraviolet and infrared wavelengths taken by Cassini’s imaging science subsystem on 26 October. Red and green colours show areas where atmospheric methane absorbs light and reveal a brighter (redder) northern hemisphere. Blue colours show the high atmosphere and detached hazes (Courtesy of JPL /Univ. of Arizona) Cassini-Huygens Jean-Pierre Lebreton1, Claudio Sollazzo2, Thierry Blancquaert13, Olivier Witasse1 and the Huygens Mission Team 1 ESA Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands 2 ESA Directorate of Operations and Infrastructure, ESOC, Darmstadt, Germany 3 ESA Directorate of Technical and Quality Management, ESTEC, Noordwijk, The Netherlands Earl Maize, Dennis Matson, Robert Mitchell, Linda Spilker Jet Propulsion Laboratory (NASA/JPL), Pasadena, California Enrico Flamini Italian Space Agency (ASI), Rome, Italy Monica Talevi Science Programme Communication Service, ESA Directorate of Scientific Programmes, ESTEC, Noordwijk, The Netherlands assini-Huygens, named after the two celebrated scientists, is the joint NASA/ESA/ASI mission to Saturn Cand its giant moon Titan. It is designed to shed light on many of the unsolved mysteries arising from previous observations and to pursue the detailed exploration of the gas giants after Galileo’s successful mission at Jupiter. The exploration of the Saturnian planetary system, the most complex in our Solar System, will help us to make significant progress in our understanding
    [Show full text]
  • Determining the Small-Scale Structure and Particle Properties in Saturn's Rings from Stellar and Radio Occultations
    University of Central Florida STARS Electronic Theses and Dissertations, 2004-2019 2018 Determining the Small-scale Structure and Particle Properties in Saturn's Rings from Stellar and Radio Occultations Richard Jerousek University of Central Florida Part of the The Sun and the Solar System Commons Find similar works at: https://stars.library.ucf.edu/etd University of Central Florida Libraries http://library.ucf.edu This Doctoral Dissertation (Open Access) is brought to you for free and open access by STARS. It has been accepted for inclusion in Electronic Theses and Dissertations, 2004-2019 by an authorized administrator of STARS. For more information, please contact [email protected]. STARS Citation Jerousek, Richard, "Determining the Small-scale Structure and Particle Properties in Saturn's Rings from Stellar and Radio Occultations" (2018). Electronic Theses and Dissertations, 2004-2019. 5840. https://stars.library.ucf.edu/etd/5840 DETERMINING THE SMALL-SCALE STRUCTURE AND PARTICLE PROPERTIES IN SATURN’S RINGS FROM STELLAR AND RADIO OCCULTATIONS by RICHARD GREGORY JEROUSEK M.S. University of Central Florida, 2009 A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy in the Department of Physics in the College of Sciences at the University of Central Florida Orlando, Florida Spring Term 2018 Major Professor: Joshua E. Colwell © 2018 Richard G. Jerousek ii ABSTRACT Saturn’s rings consist of icy particles of various sizes ranging from millimeters to several meters. Particles may aggregate into ephemeral elongated clumps known as self-gravity wakes in regions where the surface mass density and epicyclic frequency give a Toomre critical wavelength which is much larger than the largest individual particles (Julian and Toomre 1966).
    [Show full text]
  • Mapping of Earth's Magnetic Field with the Ãÿrsted Satellite
    I I I MAPPING OF EARTH'S MAGNETIC FIELD WITH THE BRSTED SATELLITE W.R.Baron, K. Lescbly and P.L.Thomsen Computer Resources International A/S I Space Division, Bregneredvej 144 P.O.Box 173 DK-3460 Birkered, Denmark I 1. Abstract 3. Science Overview The Danish 0rsted satellite will carry three science The purpose of the 0rsted satellite mission is to conduct experiments with the objectives of mapping the Earth's a research program in the field of solar-terrestrial physics I magnetic field and measuring the charged particle comprising magnetospheric, ionospheric, and atmospheric environmentfrom a 7801an altitude sun-synchronous polar physics in combination with research in the magnetic orbit. The science data generated during the planned one­ field of the Earth. A wider scope is to create a research year mission will be used to improve geomagnetic models environment called the Solar-Terrestrial Physics I and study the auroral phenomena. Comprehensive and Laboratory that links together a number of existing accurate mapping of the geomagnetic field every 5 to 10 research activities, which traditionally have been carried years is of particular interest to geophysical studies. As out with only limited coordination at the individual I such, the 0rsted science data return will complement the scientist level in Denmark and abroad. Magsat (1979-80) and Aristoteles (... 2(00) mission objectives. 1Wo magnetometers will be mounted on an 8 Solar-terrestrial science has attracted much attention meter long deployable boom together with a star imagerfor during recent years, among scientists as well as in the I detennining the absolute pointing vector for the CSC public.
    [Show full text]
  • UVIS) Measured Ultraviolet Light (From 55.8 to 190 Nanometers) Invisible to the Human Eye from the Saturn System’S Atmospheres, Rings, and Surfaces
    CASSINI FINAL MISSION REPORT 2019 1 ULTRAVIOLET IMAGING SPECTROGRAPH The Ultraviolet Imaging Spectrograph (UVIS) measured ultraviolet light (from 55.8 to 190 nanometers) invisible to the human eye from the Saturn system’s atmospheres, rings, and surfaces. The science objectives of UVIS were to produce ultraviolet maps of Saturn’s rings and many moons, to study the composition of atmospheres of the planet and its moon Titan, and also to look at how light from the Sun and the stars passed through atmospheres and rings in the Saturn system to determine their size characteristics and composition. UVIS had two spectrographic channels: the extreme ultraviolet channel (EUV) and the far ultraviolet (FUV) channel, and also included a high-speed photometer (HSP) to perform stellar occultations, and a hydrogen-deuterium absorption cell (HDAC). The spectrograph could determine the atomic composition of those gases by splitting the light into its component wavelengths. 2 VOLUME 1: MISSION OVERVIEW & SCIENCE OBJECTIVES AND RESULTS CONTENTS ULTRAVIOLET IMAGING SPECTROGRAPH .................................................................................................................. 1 Mission Objectives and Science Objectives and Results ....................................................................................... 3 Key Objectives........................................................................................................................................................ 4 Science Assessment, with tables ..........................................................................................................................
    [Show full text]
  • Team Persephone
    AIAA TEAM SPACE TRANSPORTATION DESIGN COMPETITION TEAM PERSEPHONE Submitted By: Chelsea Dalton Ashley Miller Ryan Decker Sahil Pathan Layne Droppers Joshua Prentice Zach Harmon Andrew Townsend Nicholas Malone Nicholas Wijaya Iowa State University Department of Aerospace Engineering May 10, 2018 TEAM PERSEPHONE Page I Iowa State University: Persephone Design Team Chelsea Dalton Ryan Decker Layne Droppers Zachary Harmon Trajectory & Propulsion Communications & Power Team Lead Thermal Systems AIAA ID #908154 AIAA ID #906791 AIAA ID #532184 AIAA ID #921129 Nicholas Malone Ashley Miller Sahil Pathan Joshua Prentice Orbit Design Science Science Science AIAA ID #921128 AIAA ID #922108 AIAA ID #761247 AIAA ID #922104 Andrew Townsend Nicholas Wijaya Structures & CAD Trajectory & Propulsion AIAA ID #820259 AIAA ID #644893 TEAM PERSEPHONE Page II Contents 1 Introduction & Problem Background 2 1.1 Motivation & Background . 2 1.2 Mission Definition . 3 2 Mission Overview 5 2.1 Trade Study Tools . 5 2.2 Mission Architecture . 6 2.3 Planetary Protection . 6 3 Science 8 3.1 Observations of Interest . 8 3.2 Goals . 9 3.3 Instrumentation . 10 3.3.1 Visible and Infrared Imaging|Ralph . 11 3.3.2 Radio Science Subsystem . 12 3.3.3 Atmosphere . 14 3.3.4 Solar Wind Around Pluto . 14 3.3.5 Descent Probes . 16 4 Trajectory 19 4.1 Interplanetary Trajectory Design . 19 4.2 Earth Launch . 19 4.2.1 Launch Vehicle Selection . 19 4.2.2 Launch Vehicle Integration . 22 4.2.3 Launch Characteristics . 23 4.3 Interplanetary Cruise . 25 4.4 Jupiter Gravity Assist . 26 4.5 Pluto Orbit Insertion . 28 5 Primary Mission 30 5.1 Design Methodology .
    [Show full text]
  • Subsidence-Induced Methane Clouds in Titan's Winter Polar Stratosphere
    Icarus 243 (2014) 129–138 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Subsidence-induced methane clouds in Titan’s winter polar stratosphere and upper troposphere ⇑ C.M. Anderson a, , R.E. Samuelson b, R.K. Achterberg b, J.W. Barnes c, F.M. Flasar a a Planetary Systems Laboratory, NASA Goddard Space Flight Center, Greenbelt, MD 20771-0001, USA b Department of Astronomy, University of Maryland, College Park, MD 20742-2421, USA c Department of Physics, University of Idaho, Moscow, ID 83844-0903, USA article info abstract Article history: Titan’s atmospheric methane most likely originates from lakes at the surface and subsurface reservoirs. Received 30 July 2013 Accordingly, it has been commonly assumed that Titan’s tropopause region, where the vertical temper- Revised 4 September 2014 ature profile is a minimum, acts as a cold trap for convecting methane, leading to the expectation that the Accepted 4 September 2014 formation of methane clouds in Titan’s stratosphere would be rare. The additional assumption that Available online 16 September 2014 Titan’s tropopause temperatures are independent of latitude is also required. However, Cassini Composite InfraRed Spectrometer (CIRS) and Radio Science Subsystem (RSS) data sets reveal colder temperatures in Keywords: Titan’s tropopause region near the winter pole than those at low latitudes and in the summer hemi- Titan, clouds sphere. This, combined with the presence of a cross-equatorial meridional circulation with winter polar Atmosphere Radiative transfer subsidence, as suggested by current general circulation models, implies the inevitable formation of Ices, IR spectroscopy Subsidence-Induced Methane Clouds (SIMCs) over Titan’s winter pole.
    [Show full text]