Proceedings Symposium Art of Scientific Glassblowing

Total Page:16

File Type:pdf, Size:1020Kb

Proceedings Symposium Art of Scientific Glassblowing PROCEEDINGS THE SIXTY-THIRD ANNUAL SYMPOSIUM ON THE ART OF SCIENTIFIC GLASSBLOWING 2018 THE AMERICAN SCIENTIFIC GLASSBLOWERS SOCIETY i Proceedings The Sixty-third Annual Symposium on the Art of Scientific Glassblowing Sponsored by The American Scientific Glassblowers Society Colorado Springs, Colorado June 19-22, 2018 THE AMERICAN SCIENTIFIC GLASSBLOWERS SOCIETY Norman, OK i The American Scientific Glassblowers Society P.O. Box 1777 Norman, OK 73070 Phone: 716-353-8062 FAX: 866-880-3216 [email protected] Library of Congress #58-3756 Copyright 2018 ii OFFICERS AND DIRECTORS OF THE AMERICAN SCIENTIFIC GLASSBLOWERS SOCIETY 2017 – 2018 Officers President Philip Legge President-Elect Benjamin Revis Secretary Kathryn Jones Treasurer Victor Mathews Sectional Directors Elayne Ashley Jeff Haut Scott Bankroff Jack Korfhage Sabrina Bélanger Philip Sliwoski Katie Severance Jared Carver Blake Bortolin Dennis Wargo Andrew Gibbs Jerry Cloninger, Executive Secretary Jim and Laura Cornell, National Office Managers Marylin C. Brown, Ph.D., Fusion & Proceedings Editor PROCEEDINGS is an informational journal and assumes no responsibil- ity for the accuracy, validity, or originality of any contributed article or opinion expressed herein. iii Past Presidents † J. Allen Alexander Joseph Walas, Jr. † Karl H. Walther A. Ben Seal † Arthur Dolenga Robert J. Ponton † Alfred H. Walrod Ian B. Duncanson † Richard W. Poole † Allan B. Brown † William E. Barr Richard C. Smith † Charles J. Cassidy Richard P. Gerhart † Jonathan Seckman David G. Daenzer † William A. Gilhooley Barry W. Lafler M. Howe Smith Doni J. Hatz † Billie E. Pahl Gary S. Coyne Theodore W. Bolan Edwin A. Powell Earl R. Nagle Michael J. Souza † Werner H. Haak Scott Bankroff † Gordon Good Ronald A. Bihler Robert G. Campbell James R. Hodgson † Helmut E. Drechsel Robert B. Singer Lawrence W. Ryan, Jr. Jack Korfhage † Joseph W. Baum Gene Nelson Andre W. Spaan Curt Sexton Donald E. Lillie Patrick DeFlorio † Wilbur C. Mateyka Frank Meints Jerry A. Cloninger James C. Cornell † David Chandler Steven D. Moder † Owen J. Kingsbury, Jr. Raymond T. “Skip” Huckaby Raymond L. Carew Joseph S. Gregar James K. Merritt Joseph S. Gregar † Deceased iv 63rd Symposium Committees Symposium Co-Chairs Ron Bihler Precision Glassblowing of Colorado Joe Gregar Argonne National Labs Symposium Coordinator Bob Singer Technical Glass Products Allan B. Brown Regular Member Kevin Teaford Seminars Chair University of Utah Artistic Demonstrations / Jennifer Langill, Scripps Health Auction Chair Annalee Pickett, Elemental Scientific Exhibits Chair Dennis Wargo Wale Apparatus, Inc. Joseph S. Gregar Junior Member Christopher Bock Seminar Chair Sea Cube Co. Seminars Chair Jim Hodgson Kansas State University Technical Papers Chair Tracy Drier University of Wisconsin-Madison Technical Posters Chair Elayne Ashley Georgia Tech Technical Demonstrations Chair Blake Bortolin Precision Glassblowing of Colorado v Contents Papers From Object to Project – A Primer on the Procedural Approach to Scien- tific Glassblowing By Steven Sweat ...................................... Unavailable for publication ICEMAG: Constructing Magnometers for a Journey to Find Life on Europa By Michael J. Souza .......................................................................... 3 Imagination of the Electrics By Bryan Kekst Brown .................................................................... 12 A Look into Volcanology through the Glass Fluidization Cup By Elayne Ashley ............................................................................. 21 Point of Excellence: Machine Shop By Tracy O. Drier and Steve Myers ................................................ 27 A Repurposed Rotovap for Peptide Synthesis By James Hodgson ........................................................................... 40 Other Information 2018 Technical Posters ........................................................................... 46 2018 Technical Demonstrations ............................................................. 47 2018 Exhibitors ..................................................................................... 48 2018 Symposium Attendees ................................................................... 51 vi Papers 1 2 ICEMAG: (The Interior Characterization of Europa using Magnetometry) Constructing Magnetometers for a Journey to Find Life on Europa By Michael J. Souza* ABSTRACT ICEMAG: The Flight Ready Process of Constructing Magnetometers for a Journey to Europa. The Interior Characterization of Europa using Magnetometry (ICEMAG) is a multi-frequency helium magnetometer made of aluminosilicate glass that will be flown on board the Europa Clipper mission to Jupiter’s moon Europa. A glass cell filled with helium acts as a vector magnetometer that will be used for probing the subsurface and determining Europa’s ocean depth, salinity, and ice shell thickness, as well as detecting erupting plume activity. The paper will discuss the mission outline and detail the certifi- cation process used by NASA and JPL. INTRODUCTION Perhaps one of the primary questions mankind faces is: What other forms of life exist outside the confines of our planet? Given the near infinite possibilities of our universe, the theoretical answer is that life is inevitable. However, the vastness of space makes empiri- cal discovery difficult to prove. Nevertheless, scientists now have reason to believe that we may soon discover that life exists within our own Solar System. In an almost mystical coincidence, the source of this possible discovery comes from one of the Galilean moons of Jupiter. Four centuries ago, when Galileo used his telescope to gaze towards Jupiter and found four of the moons orbiting the giant planet, this incontrovertible evidence proved that the universe was not Earth centric and forever changed our civilization. Many histori- ans believe that this historic moment established a place for scientific reason and methodol- ogy on which modern science and technology now stands. WHY EUROPA? Europa is the 3rd moon closest to Jupiter and is about 3,160 kilometers (1,950 miles) in diameter, or about the size of Earth’s moon. In late 2012, NASA’s Hubble Space Telescope spotted what seemed to be 125-mile- high (200 kilometers) geysers of water vapor spew- ing from the poles of Europa.1 (see Image 1) This was later confirmed by NASA’s Galileo Jupiter probe. Could these geothermal vents provide heat and energy to sustain life? And what are those brown smudges? Image 1. Europa. This image or video was catalogued by Jet Propulsion Laboratory of the United States National Aeronautics and Space Administration (NASA) under Photo ID: PIA00502. *Department of Physics, Princeton University, Princeton, NJ 08544. Email: [email protected]. 1 https://www.jpl.nasa.gov/news/news.php?release=2013-363. Published December 12, 2013. 3 CLIPPER MISSION & ICEMAG On May 26, 2015, NASA announced the selection of ICEMAG and eight other investi- gations for the Europa mission’s science payload for scientific instruments to fly onboard its planned Clipper spacecraft which would orbit Jupiter and conduct repeated close flybys of the small moon during a three-year period. SCIENTIFIC PAYLOAD • Plasma Instrument for Magnetic Sounding (PIMS) - This instrument works in con- junction with a magnetometer and is key to determining Europa’s ice shell thickness, ocean depth, and salinity by correcting the magnetic induction signal for plasma cur- rents around Europa. • Interior Characterization of Europa using Magnetometry (ICEMAG) - This mag- netometer will measure the magnetic field near Europa and, in conjunction with the PIMS instrument, infer the location, thickness and salinity of Europa’s subsurface ocean. • Mapping Imaging Spectrometer for Europa (MISE) - This instrument will probe the composition of Europa, identifying and mapping the distributions of organics, salts, acid hydrates, water ice phases, and other materials to determine the habitability of Europa’s ocean. • Europa Imaging System (EIS) - The wide and narrow angle cameras on this instru- ment will map most of Europa at 50 meter (164 foot) resolution, and will provide im- ages of areas of Europa’s surface at up to 100 times higher resolutionn. • Radar for Europa Assessment and Sounding: Ocean to Near-surface (REASON) - This dual-frequency ice penetrating radar instrument is designed to characterize and sound Europa’s icy crust from the near-surface to the ocean, revealing the hidden structure of Europa’s ice shell and potential water within. • Europa Thermal Emission Imaging System (E-THEMIS) - This “heat detector” will provide high spatial resolution, multi-spectral thermal imaging of Europa to help detect active sites, such as potential vents erupting plumes of water into space. • MAss SPectrometer for Planetary EXploration/Europa (MASPEX) - This instru- ment will determine the composition of the surface and subsurface ocean by measuring Europa’s extremely tenuous atmosphere and any surface material ejected into space. • Ultraviolet Spectrograph/Europa (UVS) - This instrument will investigate the likely presence of water plumes erupting from Europa’s surface. UVS will be able to detect small plumes and will provide valuable data about the composition and dynamics of the moon’s rarefied atmosphere. • SUrface Dust Mass Analyzer (SUDA) - This instrument will measure the composi- tion of small, solid particles ejected from Europa, providing the opportunity to directly sample the surface and potential plumes on low-altitude
Recommended publications
  • An Impacting Descent Probe for Europa and the Other Galilean Moons of Jupiter
    An Impacting Descent Probe for Europa and the other Galilean Moons of Jupiter P. Wurz1,*, D. Lasi1, N. Thomas1, D. Piazza1, A. Galli1, M. Jutzi1, S. Barabash2, M. Wieser2, W. Magnes3, H. Lammer3, U. Auster4, L.I. Gurvits5,6, and W. Hajdas7 1) Physikalisches Institut, University of Bern, Bern, Switzerland, 2) Swedish Institute of Space Physics, Kiruna, Sweden, 3) Space Research Institute, Austrian Academy of Sciences, Graz, Austria, 4) Institut f. Geophysik u. Extraterrestrische Physik, Technische Universität, Braunschweig, Germany, 5) Joint Institute for VLBI ERIC, Dwingelo, The Netherlands, 6) Department of Astrodynamics and Space Missions, Delft University of Technology, The Netherlands 7) Paul Scherrer Institute, Villigen, Switzerland. *) Corresponding author, [email protected], Tel.: +41 31 631 44 26, FAX: +41 31 631 44 05 1 Abstract We present a study of an impacting descent probe that increases the science return of spacecraft orbiting or passing an atmosphere-less planetary bodies of the solar system, such as the Galilean moons of Jupiter. The descent probe is a carry-on small spacecraft (< 100 kg), to be deployed by the mother spacecraft, that brings itself onto a collisional trajectory with the targeted planetary body in a simple manner. A possible science payload includes instruments for surface imaging, characterisation of the neutral exosphere, and magnetic field and plasma measurement near the target body down to very low-altitudes (~1 km), during the probe’s fast (~km/s) descent to the surface until impact. The science goals and the concept of operation are discussed with particular reference to Europa, including options for flying through water plumes and after-impact retrieval of very-low altitude science data.
    [Show full text]
  • PDS Mission Interface for Europa Mission Status of Planning for Data Archiving
    PDS Mission Interface for Europa Mission Status of Planning for Data Archiving CARTOGRAPHY AND IMAGING SCIENCES (“Imaging”) NODE PDS Lead Node Lisa Gaddis (USGS, Astrogeology) August 2016 Overview Common goals PDS4 Archiving roles, responsibilities EM archiving deliverables Data and Archive Working Group (DAWG) Archiving assignments Archiving activities to date Archiving schedule Current archiving activities Where we are now August 2016 2 Common Goals The PDS and Europa Mission (EM) will work together to ensure that we Organize, document and format EM digital planetary data in a standardized manner Collect complete, well-documented, peer-reviewed planetary data into archives Make planetary data available and useful to the science community ○ Provide online data delivery tools & services Ensure the long-term preservation and usability of the data August 2016 3 PDS4 The new PDS, an integrated data system to improve access ○ Required for all missions (e.g., used by LADEE, MAVEN) A re-architected, modern, online data system ○ Data are organized into bundles Includes all data for a particular instrument (e.g., PDF/A documents) ○ Bundles have collections Grouped files with a similar origin (e.g., Document Collection) Improves efficiency of ingestion and distribution of data ○ Uses Extensible Markup Language (XML) and standard data format templates ○ Self-consistent information model & software system ○ Information for Data Providers https://pds.nasa.gov/pds4/about ○ PDS4 Concepts Document https://pds.nasa.gov/pds4/doc/concepts/Concepts_150909.pdf
    [Show full text]
  • Using the Galileo Solid-State Imaging Instrument As a Sensor of Jovian
    Using the Galileo Solid-State Imaging Instrument as a Sensor of Jovian Energetic Electrons Ashley Carlton1, Maria de Soria-Santacruz Pich2, Insoo Jun2, Wousik Kim2, and Kerri Cahoy1 1Massachusetts Institute of Technology, Cambridge, 02139, USA (e-mail: [email protected]) 2Jet Propulsion Laboratory, California Institute of Technology, Pasadena, 91109, USA respectively. For the most part, information about the Jovian I. INTRODUCTION environment comes from the Galileo spacecraft Energetic Harsh radiation in the form of ionized, highly energetic Particle Detector (EPD) [Williams et al., 1992] (in Jovian particles is part of the space environment and can affect orbit from December 1995 to September 2003), which had a spacecraft. These particles not only sweep through the solar nearly equatorial orbit. Juno, a NASA spacecraft that entered system in the solar wind and flares and are ejected from Jovian orbit in July 2016, and Europa Clipper, a NASA galactic and extra-galactic supernovae, but also are trapped as mission planned for the 2020s, do not carry instruments belts in planetary magnetic fields. Jupiter’s magnetosphere is capable of measuring high-energy (>1 MeV) electrons. Juno is the largest and strongest of a planet in the solar system. in a polar orbit; Europa Clipper is planned to be in a highly Similar to Earth, Jupiter is roughly a magnetic dipole with a elliptical Jovian orbit, flying-by Jupiter’s moon, Europa, in tilt of ~11° [Khurana et al., 2004]. Jupiter’s magnetic field each orbit. strength is an order of magnitude larger than Earth, and its We develop a technique to extract the high-energy magnetic moment is roughly 18,000 times larger [Bagenal et electron environment using scientific imager data.
    [Show full text]
  • Europa Clipper Mission: Preliminary Design Report
    Europa Clipper Mission: Preliminary Design Report Todd Bayer, Molly Bittner, Brent Buffington, Karen Kirby, Nori Laslo Gregory Dubos, Eric Ferguson, Ian Harris, Johns Hopkins University Applied Physics Maddalena Jackson, Gene Lee, Kari Lewis, Jason Laboratory 11100 Johns Hopkins Road Laurel, Kastner, Ron Morillo, Ramiro Perez, Mana MD 20723-6099 Salami, Joel Signorelli, Oleg Sindiy, Brett Smith, [email protected] Melissa Soriano Jet Propulsion Laboratory California Institute of Technology 4800 Oak Grove Dr. Pasadena, CA 91109 818-354-4605 [email protected] Abstract—Europa, the fourth largest moon of Jupiter, is 1. INTRODUCTION believed to be one of the best places in the solar system to look for extant life beyond Earth. Exploring Europa to investigate its Europa’s subsurface ocean is a particularly intriguing target habitability is the goal of the Europa Clipper mission. for scientific exploration and the hunt for life beyond Earth. The 2011 Planetary Decadal Survey, Vision and Voyages, The Europa Clipper mission envisions sending a flight system, states: “Because of this ocean’s potential suitability for life, consisting of a spacecraft equipped with a payload of NASA- Europa is one of the most important targets in all of planetary selected scientific instruments, to execute numerous flybys of Europa while in Jupiter orbit. A key challenge is that the flight science” [1]. Investigation of Europa’s habitability is system must survive and operate in the intense Jovian radiation intimately tied to understanding the three “ingredients” for environment, which is especially harsh at Europa. life: liquid water, chemistry, and energy. The Europa Clipper mission would investigate these ingredients by The spacecraft is planned for launch no earlier than June 2023, comprehensively exploring Europa’s ice shell and liquid from Kennedy Space Center, Florida, USA, on a NASA supplied ocean interface, surface geology and surface composition to launch vehicle.
    [Show full text]
  • March 21–25, 2016
    FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk,
    [Show full text]
  • IAC-17-F1.2.3 Page 1 of 23 IAC-17-C1.7.8 EVOLUTION OF
    68th International Astronautical Congress (IAC), Adelaide, Australia, 25-29 September 2017. Copyright © 2017 California Institute of Technology. Government sponsorship acknowledged. IAC-17-C1.7.8 EVOLUTION OF TRAJECTORY DESIGN REQUIREMENTS ON NASA’S PLANNED EUROPA CLIPPER MISSION Brent Buffingtona*, Try Lamb, Stefano Campagnolab, Jan Ludwinskic, Eric Fergusonc, Ben Bradleyc a Europa Clipper Mission Design Manager, Jet Propulsion Laboratory / California Institute of Technology 4800 Oak Grove Drive, Pasadena, CA, 91109-8099, [email protected] b Mission Design Engineer, Jet Propulsion Laboratory / California Institute of Technology 4800 Oak Grove Drive, Pasadena, CA, 91109-8099 c Mission Planning Engineer, Jet Propulsion Laboratory / California Institute of Technology 4800 Oak Grove Drive, Pasadena, CA, 91109-8099 * Corresponding Author Abstract Europa is one of the most scientifically intriguing targets in planetary science due to its potential suitability for extant life. As such, NASA has funded the California Institute of Technology Jet Propulsion Laboratory and the Johns Hopkins University Applied Physics Laboratory to jointly develop the planned Europa Clipper mission—a multiple Europa flyby mission architecture aimed to thoroughly investigate the habitability of Europa and provide reconnaissance data to determine a landing site that maximizes the probability of both a safe landing and high scientific value for a potential future Europa lander. The trajectory design—a major enabling component for this Europa Clipper mission concept—was developed to maximize science from a set of eight model payload instruments determined by a NASA-appointed Europa Science Definition Team (SDT) between 2011-2015. On May 26, 2015, NASA officially selected 10 instruments from 6 different U.S.
    [Show full text]
  • Power Subsystem Approach for the Europa Mission
    E3S Web of Conferences 16, 13004 (2017) DOI: 10.1051/ e3sconf/20171613004 ESPC 2016 POWER SUBSYSTEM APPROACH FOR THE EUROPA MISSION Antonio Ulloa-Severino(1), Gregory A. Carr(1), Douglas J. Clark(1), Sonny M. Orellana(1), Roxanne Arellano(1), Marshall C. Smart(1), Ratnakumar V. Bugga(1), Andreea Boca(1), and Stephen F. Dawson(1) (1)Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109 USA, Email: [email protected] ABSTRACT implementation of the spacecraft and instrument hardware. The mission design team is expending great NASA is planning to launch a spacecraft on a mission to efforts to minimize the amount of total dose radiation the Jovian moon Europa, in order to conduct a detailed the flight system would accumulate and maximize reconnaissance and investigation of its habitability. The science data return. spacecraft would orbit Jupiter and perform a detailed science investigation of Europa, utilizing a number of The NASA-selected instruments intend to characterize science instruments including an ice-penetrating radar to Europa by producing high-resolution images and determine the icy shell thickness and presence of surface composition maps. An ice-penetrating radar subsurface oceans. The spacecraft would be exposed to intends to determine the crust thickness, and a harsh radiation and extreme temperature environments. magnetometer would measure the magnetic field To meet mission objectives, the spacecraft power strength and direction to further help scientists subsystem is being architected and designed to operate determine ocean depth and salinity. A thermal efficiently, and with a high degree of reliability. instrument would be used to identify warmer water that could have erupted through the crust, while other 1.
    [Show full text]
  • Gao-21-306, Nasa
    United States Government Accountability Office Report to Congressional Committees May 2021 NASA Assessments of Major Projects GAO-21-306 May 2021 NASA Assessments of Major Projects Highlights of GAO-21-306, a report to congressional committees Why GAO Did This Study What GAO Found This report provides a snapshot of how The National Aeronautics and Space Administration’s (NASA) portfolio of major well NASA is planning and executing projects in the development stage of the acquisition process continues to its major projects, which are those with experience cost increases and schedule delays. This marks the fifth year in a row costs of over $250 million. NASA plans that cumulative cost and schedule performance deteriorated (see figure). The to invest at least $69 billion in its major cumulative cost growth is currently $9.6 billion, driven by nine projects; however, projects to continue exploring Earth $7.1 billion of this cost growth stems from two projects—the James Webb Space and the solar system. Telescope and the Space Launch System. These two projects account for about Congressional conferees included a half of the cumulative schedule delays. The portfolio also continues to grow, with provision for GAO to prepare status more projects expected to reach development in the next year. reports on selected large-scale NASA programs, projects, and activities. This Cumulative Cost and Schedule Performance for NASA’s Major Projects in Development is GAO’s 13th annual assessment. This report assesses (1) the cost and schedule performance of NASA’s major projects, including the effects of COVID-19; and (2) the development and maturity of technologies and progress in achieving design stability.
    [Show full text]
  • Europa Mission Update: Beyond Payload Selection
    Europa Mission Update: Beyond Payload Selection Todd Bayer, Brent Buffington, Jean- Karen Kirby Francois Castet, Maddalena Jackson, Johns Hopkins University Gene Lee, Kari Lewis, Jason Applied Physics Laboratory Kastner, Kathy Schimmels 11100 Johns Hopkins Road Jet Propulsion Laboratory Laurel, MD 20723-6099 California Institute of Technology [email protected] 4800 Oak Grove Dr. Pasadena, CA 91109 818-354-4605 [email protected] Abstract—Europa, the fourth largest moon of Jupiter, is believed 2. MISSION OVERVIEW ................................2 to be one of the best places in the solar system to look for 3. FLIGHT SYSTEM OVERVIEW ..................7 extant life beyond Earth. The 2011 Planetary Decadal Survey, Vision and Voyages, states: “Because of this ocean’s potential 4. FUTURE WORK .................................... 11 suitability for life, Europa is one of the most important targets 5. SUMMARY AND CONCLUSIONS .................... 11 in all of planetary science.” Exploring Europa to investigate its habitability is the goal of the planned Europa Mission. This ACKNOWLEDGMENTS ................................ 11 exploration is intimately tied to understanding the three “ingre- REFERENCES ......................................... 11 dients” for life: liquid water, chemistry, and energy. The Europa BIOGRAPHY .......................................... 11 Mission would investigate these ingredients by comprehensively exploring Europa’s ice shell and liquid ocean interface, surface geology and surface composition to glean insight into the inner workings of this fascinating moon. In addition, a lander mission 1. INTRODUCTION is seen as a possible future step, but current data about the Jo- vian radiation environment and about potential landing site haz- Scientific motivation for studying the habitability of Europa ards and potential safe landing zones is insufficient.
    [Show full text]
  • Europa Mission
    Europa Mission Lisa Gaddis (USGS, Astrogeology) PDS Cartography and Imaging Sciences Node (You can still call us “Imaging” or PDS-IMG or IMG) Feb 5, 2016 Europa Mission Interface Mission Status Instruments PDS Current Status: Node Assignments ○ Identify Lead Node, Instrument Support Nodes Feb 5, 2016 Europa Mission Now called “Europa Multiple Flyby Mission” Europa Clipper Orbiter and a Lander Explores potential for subsurface ocean & habitability on Jupiter’s moon Europa Ice shell and ocean, composition, geology Performs 45 close flybys of Europa from orbit around Jupiter Topographic survey, ice thickness, plumes? 7 to 10 days to transmit data between flybys Solar powered Joint investigation between JPL & APL Nine instruments on orbiter Nanosatellites for plume samples? Lander configuration is TBD Feb 5, 2016 Europa Clipper Orbital Instruments PIMS: Plasma Instrument for Magnetic Sounding PI: Joseph Westlake, APL ICEMAG: Interior Characterization of Europa using Magnetometry PI: Carol Raymond, JPL MISE: Mapping Imaging Spectrometer for Europa PI: Diana Blaney, JPL EIS: Europa Imaging System PI: Elizabeth Turtle, APL REASON: Radar for Europa Assessment and Sounding: Ocean to Near- Surface PI: Donald Blankenship, Univ. Texas E-THEMIS: Europa Thermal Emission Imaging System PI: Philip Christensen, Arizona State Univ. MASPEX: Mass Spectrometer for Planetary Exploration/Europa PI: Jack Waite, Southwest Research Institute UVS: Ultraviolet Spectrograph/Europa PI: Kurt Retherford, SWRI SUDA: Surface Dust Mass
    [Show full text]
  • Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave
    PROCEEDINGS OF SPIE Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave Makenzie Lystrup Howard A. MacEwen Giovanni G. Fazio Editors 10–15 June 2018 Austin, Texas, United States Sponsored by 4D Technology (United States) • Andor Technology, Ltd. (United Kingdom) • Astronomical Consultants & Equipment, Inc. (United States) • Giant Magellan Telescope (Chile) • GPixel, Inc. (China) • Harris Corporation (United States) • Materion Corporation (United States) • Optimax Systems, Inc. (United States) • Princeton Infrared Technologies (United States) • Symétrie (France) Teledyne Technologies, Inc. (United States) • Thirty Meter Telescope (United States) •SPIE Cooperating Organizations European Space Organisation • National Radio Astronomy Observatory (United States) • Science & Technology Facilities Council (United Kingdom) • Canadian Astronomical Society (Canada) Canadian Space Association ASC (Canada) • Royal Astronomical Society (United Kingdom) Association of Universities for Research in Astronomy (United States) • American Astronomical Society (United States) • Australian Astronomical Observatory (Australia) • European Astronomical Society (Switzerland) Published by SPIE Volume 10698 Part One of Three Parts Proceedings of SPIE 0277-786X, V. 10698 SPIE is an international society advancing an interdisciplinary approach to the science and application of light. The papers in this volume were part of the technical conference cited on the cover and title page. Papers were selected and subject to review by the editors and conference program committee. Some conference presentations may not be available for publication. Additional papers and presentation recordings may be available online in the SPIE Digital Library at SPIEDigitalLibrary.org. The papers reflect the work and thoughts of the authors and are published herein as submitted. The publisher is not responsible for the validity of the information or for any outcomes resulting from reliance thereon.
    [Show full text]
  • Blocks Size Frequency Distribution in the Enceladus Tiger Stripes Area: Implications on Their Formative Processes
    universe Article Blocks Size Frequency Distribution in the Enceladus Tiger Stripes Area: Implications on Their Formative Processes Maurizio Pajola 1,* , Alice Lucchetti 1 , Lara Senter 2 and Gabriele Cremonese 1 1 INAF-Astronomical Observatory of Padova, Vicolo dell’Osservatorio 5, 35122 Padova, Italy; [email protected] (A.L.); [email protected] (G.C.) 2 Department of Physics and Astronomy “G. Galilei”, Università di Padova, 35122 Padova, Italy; [email protected] * Correspondence: [email protected] Abstract: We study the size frequency distribution of the blocks located in the deeply fractured, geologically active Enceladus South Polar Terrain with the aim to suggest their formative mechanisms. Through the Cassini ISS images, we identify ~17,000 blocks with sizes ranging from ~25 m to 366 m, and located at different distances from the Damascus, Baghdad and Cairo Sulci. On all counts and for both Damascus and Baghdad cases, the power-law fitting curve has an index that is similar to the one obtained on the deeply fractured, actively sublimating Hathor cliff on comet 67P/Churyumov- Gerasimenko, where several non-dislodged blocks are observed. This suggests that as for 67P, sublimation and surface stresses favor similar fractures development in the Enceladus icy matrix, hence resulting in comparable block disaggregation. A steeper power-law index for Cairo counts may suggest a higher degree of fragmentation, which could be the result of localized, stronger tectonic disruption of lithospheric ice. Eventually, we show that the smallest blocks identified are located Citation: Pajola, M.; Lucchetti, A.; from tens of m to 20–25 km from the Sulci fissures, while the largest blocks are found closer to the Senter, L.; Cremonese, G.
    [Show full text]