Science of the Europa Clipper Mission: Comprehensive Remote Sensing to Investigate the Ice Shell
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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. -
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. -
Europa Clipper Mission
Europa Clipper Mission Send a highly capable, radiation-tolerant spacecraft in a long, looping orbit around Jupiter to perform repeated close flybys of the icy moon. This document has been reviewed and determined not to contain export controlled technical data. 1 Exploring Europa’s Habitability: ! Ingredients for Life" Mission Goal: Explore Europa to Investigate its Habitability e-, O+, S+, … Water: • Probable saltwater ocean, implied by surface geology and magnetic field radiation-produced oxidants: • Possible lakes within the ice shell, produced by local melting O2, H2O2, CH2O ~ 100 K Chemistry: • Ocean in direct contact with mantle rock, promoting chemical leaching • Dark red surface materials contain salts, probably from the ocean Energy: • Chemical energy might sustain life • Surface irradiation creates oxidants • Mantle rock-water reactions could create reductants (hydrothermal or serpentinization) ? Habitability Activity: • Geological activity “stirs the pot” hydrothermally produced reductants: H S, H , CH , Fe • Activity could be cyclical, as tied to Io 2 2 4 ? This document has been reviewed and determined not to contain export controlled technical data. 2 Workshop Overview" Project manager, Barry Goldstein, and Planetary Protection Officer, Lisa Pratt, collaborated on setting objectives for the three-day workshop: • Validate the modeling framework for Europa Clipper Planetary Protection. • Agree on model input values, or on a plan to derive/ identify appropriate model inputs. • Develop workshop concurrence regarding future research plans and their priority. Spoiler Alert The three objectives were accomplished. This document has been reviewed and determined not to contain export controlled technical data. 3 Outside Subject-Matter Experts" A panel of multidisciplinary experts were assembled to provide consultation and guidance at the workshop." This document has been reviewed and determined not to contain export controlled technical data. -
Juno Spacecraft Description
Juno Spacecraft Description By Bill Kurth 2012-06-01 Juno Spacecraft (ID=JNO) Description The majority of the text in this file was extracted from the Juno Mission Plan Document, S. Stephens, 29 March 2012. [JPL D-35556] Overview For most Juno experiments, data were collected by instruments on the spacecraft then relayed via the orbiter telemetry system to stations of the NASA Deep Space Network (DSN). Radio Science required the DSN for its data acquisition on the ground. The following sections provide an overview, first of the orbiter, then the science instruments, and finally the DSN ground system. Juno launched on 5 August 2011. The spacecraft uses a deltaV-EGA trajectory consisting of a two-part deep space maneuver on 30 August and 14 September 2012 followed by an Earth gravity assist on 9 October 2013 at an altitude of 559 km. Jupiter arrival is on 5 July 2016 using two 53.5-day capture orbits prior to commencing operations for a 1.3-(Earth) year-long prime mission comprising 32 high inclination, high eccentricity orbits of Jupiter. The orbit is polar (90 degree inclination) with a periapsis altitude of 4200-8000 km and a semi-major axis of 23.4 RJ (Jovian radius) giving an orbital period of 13.965 days. The primary science is acquired for approximately 6 hours centered on each periapsis although fields and particles data are acquired at low rates for the remaining apoapsis portion of each orbit. Juno is a spin-stabilized spacecraft equipped for 8 diverse science investigations plus a camera included for education and public outreach. -
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. -
Magnetometer Power Supplies
bartington.com DS2520/5 Magnetometer Power Supplies The specifications of the products described in this brochure are subject to change without prior notice. Bartington Instruments Ltd 5, 8, 10, 11 & 12 Thorney Leys Business Park Witney, Oxford OX28 4GE. England Telephone: +44 (0)1993 706565 bartington.com Email: [email protected] Magnetometer Power Supplies bartington.com Magnetometer Power Supply Units A wide range of power supply units are available for our range of single and three-axis magnetic field sensors. All units accept analogue inputs from our sensors and output the signal to an analogue-to-digital converter or other separate device. The range includes: • PSU1 • Magmeter-2 Power Supply and Display Unit • DecaPSU Bartington® is a registered trademark of Bartington Holdings Limited, used under licence in the following countries: Australia, Canada, China, European Union, Hong Kong, Israel, Japan, Mexico, New Zealand, Norway, Russian Federation, Singapore, South Korea, Switzerland, Turkey, United Kingdom, United States of America, and Vietnam. Magnetometer Power Supplies bartington.com Product Function PSU1 Power Supply Unit Battery powered portable power supply for a single or three-axis magnetic field sensor and AC filtering of the sensor’s outputs. Magmeter-2 Power Supply and Display Unit A PSU1 with three displays for magnetic field value readings. DecaPSU Power supply unit and low-noise connection for up to 10 magnetometers at the end of long sensor cables. Product Compatibility PSU1 Magmeter-2 DecaPSU Mag-13 • • • Mag-03 • • •† Mag690 • • •† Mag648/649 •* •* •* Mag650 •* •* •* Mag651 •* •* •* Mag612 • • • Mag619 • • • Mag585/592 • • •† Mag670/646 • • •† Mag678/679 •* •* •* * The filtering function will be less effective at removing breakthrough from these sensors † Adaptor cable required Magnetometer Power Supplies bartington.com PSU1 Power Supply Unit The PSU1 is a self-contained, portable power supply for most Bartington Instruments magnetic field sensors, for use in any situation requiring the simple measurement of a magnetic field. -
(Preprint) AAS 18-416 PRELIMINARY INTERPLANETARY MISSION
(Preprint) AAS 18-416 PRELIMINARY INTERPLANETARY MISSION DESIGN AND NAVIGATION FOR THE DRAGONFLY NEW FRONTIERS MISSION CONCEPT Christopher J. Scott,∗ Martin T. Ozimek,∗ Douglas S. Adams,y Ralph D. Lorenz,z Shyam Bhaskaran,x Rodica Ionasescu,{ Mark Jesick,{ and Frank E. Laipert{ Dragonfly is one of two mission concepts selected in December 2017 to advance into Phase A of NASA’s New Frontiers competition. Dragonfly would address the Ocean Worlds mis- sion theme by investigating Titan’s habitability and prebiotic chemistry and searching for evidence of chemical biosignatures of past (or extant) life. A rotorcraft lander, Dragonfly would capitalize on Titan’s dense atmosphere to enable mobility and sample materials from a variety of geologic settings. This paper describes Dragonfly’s baseline mission design giv- ing a complete picture of the inherent tradespace and outlines the design process from launch to atmospheric entry. INTRODUCTION Hosting the moons Titan and Enceladus, the Saturnian system contains at least two unique destinations that have been classified as ocean worlds. Titan, the second largest moon in the solar system behind Ganymede and the only planetary satellite with a significant atmosphere, is larger than the planet Mercury at 5,150 km (3,200 miles) in diameter. Its atmosphere, approximately 10 times the column mass of Earth’s, is composed of 95% nitrogen, 5% methane, 0.1% hydrogen along with trace amounts of organics.1 Titan’s atmosphere may resemble that of the Earth before biological processes began modifying its composition. Similar to the hydrological cycle on Earth, Titan’s methane evaporates into clouds, rains, and flows over the surface to fill lakes and seas, and subsequently evaporates back into the atmosphere. -