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Infrared Experiments for Spaceborne Planetary Atmospheres Research Full Report
NASA Technical Memorandum 84414 Infrared Experiments for Spaceborne Planetary Atmospheres Research Full Report Infrared Experiments Working Group NOVEMBER 1981 NASA NASA Technical Memorandum 84414 Infrared Experiments for Spaceborne Planetary Atmospheres Research Full Report Infrared Experiments Working Group Jet Propulsion Laboratory Pasadena, California NASA National Aeronautics and Space Administration Scientific and Technical Information Branch 1981 TABLE OF CONTENTS Preface Summary of Principal Conclusions and Recommendations Chapter I The Role of Infrared Sensing in Atmospheric Science Chapter II Review of Existing Infrared Measurement Techniques Chapter III Critical Comparison of Proposed Measurement Techniques Chapter IV Conclusions and Recommended Instrument Developments Appendices: A Critical Technologies B Applicability of Atmospheric Infrared Instrumentation to Surface Science C Supporting Studies in Data Analysis and Numerical Modeling D Description of Planned Earth Orbital Platforms ii PREFACE Experiments conducted in the infrared spectral region provide a powerful tool for the study of the composition, structure and dynamics of planetary atmospheres. However, the field has become highly complex, especially that part associated with spacecraft sensing, and the range of technologies used so diverse that it is difficult to determine which of the available methods for making a particular measurement is to be preferred, even for those deeply involved in the field. Unfortunately, the realities of the age demand that some selectivity be employed; not all approaches can be supported. Furthermore, the chosen methods are generally sufficiently untried that long pre-flight developments are neces- sary if viable proposals are to be written for future flight opportunities. These considerations clearly lead to a program of developments which must be coordinated on a national scale. -
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. -
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 -
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. -
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. -
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. -
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, -
Alluvial Fans As Potential Sites for Preservation of Biosignatures on Mars
Alluvial Fans as Potential Sites for Preservation of Biosignatures on Mars Phylindia Gant August 15, 2016 Candidate, Masters of Environmental Science Committee Chair: Dr. Deborah Lawrence Committee Member: Dr. Manuel Lerdau, Dr. Michael Pace 2 I. Introduction Understanding the origin of life Life on Earth began 3.5 million years ago as the temperatures in the atmosphere were cool enough for molten rocks to solidify (Mojzsis et al 1996). Water was then able to condense and fall to the Earth’s surface from the water vapor that collected in the atmosphere from volcanoes. Additionally, atmospheric gases from the volcanoes supplied Earth with carbon, hydrogen, nitrogen, and oxygen. Even though the oxygen was not free oxygen, it was possible for life to begin from the primordial ooze. The environment was ripe for life to begin, but how would it begin? This question has intrigued humanity since the dawn of civilization. Why search for life on Mars There are several different scientific ways to answer the question of how life began. Some scientists believe that life started out here on Earth, evolving from a single celled organism called Archaea. Archaea are a likely choice because they presently live in harsh environments similar to the early Earth environment such as hot springs, deep sea vents, and saline water (Wachtershauser 2006). Another possibility for the beginning of evolution is that life traveled to Earth on a meteorite from Mars (Whitted 1997). Even though Mars is anaerobic, carbonate-poor and sulfur rich, it was warm and wet when Earth first had organisms evolving (Lui et al. -
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. -
Complete List of Contents
Complete List of Contents Volume 1 Cape Canaveral and the Kennedy Space Center ......213 Publisher’s Note ......................................................... vii Chandra X-Ray Observatory ....................................223 Introduction ................................................................. ix Clementine Mission to the Moon .............................229 Preface to the Third Edition ..................................... xiii Commercial Crewed vehicles ..................................235 Contributors ............................................................. xvii Compton Gamma Ray Observatory .........................240 List of Abbreviations ................................................. xxi Cooperation in Space: U.S. and Russian .................247 Complete List of Contents .................................... xxxiii Dawn Mission ..........................................................254 Deep Impact .............................................................259 Air Traffic Control Satellites ........................................1 Deep Space Network ................................................264 Amateur Radio Satellites .............................................6 Delta Launch Vehicles .............................................271 Ames Research Center ...............................................12 Dynamics Explorers .................................................279 Ansari X Prize ............................................................19 Early-Warning Satellites ..........................................284 -
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. -
Galileo in 1610
Module 3 – Nautical Science Unit 4 – Astronomy Chapter 15 - The Planets Section 2 – Mars & Jupiter What You Will Learn to Do Demonstrate understanding of astronomy and how it pertains to our solar system and its related bodies: Moon, Sun, stars and planets Objectives 1. Describe the major features of Mars 2. Identify the principal characteristics of Jupiter Key Terms CPS Key Term Questions 1 - 5 Key Terms Nix Olympica - Snow of Olympus Galilean satellites - The four largest and brightest moons of Jupiter: Io, Europa, Ganymede and Callisto; discovered by Galileo in 1610 Prograde The counter-clockwise direction of motion - celestial bodies around the Sun as seen from above the north pole of the Sun; in the sky it is from west to east Key Terms Retrograde The clockwise direction of celestial motion - bodies around the Sun; in the sky it is from east to west Rotational axis - The straight line through all fixed points of a rotating rigid body around which all other points of the body move in circles Opening Question Discuss what types of exploration missions have occurred on Mars. (Use CPS “Pick a Student” for this question.) Mars Fourth from Mars the Sun and the next planet beyond Earth, Mars has aroused the greatest interest. Mars Mars Ares (Roman Mars) Mars Named for the Roman god of war, it is often called the “red planet.” Mars Mars’ red color and its rapid movement from west to east among the stars make it stand out in the sky. Mars Earth The best time to see Mars is when it is nearest to Earth in August and September, when the Earth is Sun between the Sun and Mars.