Ganymede–Induced Decametric Radio Emission: In-Situ

Total Page:16

File Type:pdf, Size:1020Kb

Ganymede–Induced Decametric Radio Emission: In-Situ manuscript submitted to Geophysical Research Letters 1 Ganymede{induced decametric radio emission: in-situ 2 observations and measurements by Juno 1 1 2;3 4 5 3 C. K. Louis , P. Louarn , F. Allegrini , W. S. Kurth , J. R. Szalay 1 4 IRAP, Universit´ede Toulouse, CNRS, CNES, UPS, (Toulouse), France 2 5 Southwest Research Institute, San Antonio, Texas, USA 3 6 Department of Physics and Astronomy, University of Texas at San Antonio, San Antonio, Texas, USA 4 7 Department of Physics and Astronomy, University of Iowa, Iowa City, Iowa, USA 5 8 Department of Astrophysical Sciences, Princeton University, Princeton, New Jersey, USA 9 Key Points: 10 • First detailed wave/particle investigation of a Ganymede-induced decametric ra- 11 dio source using Juno/Waves and Juno/JADE instruments 12 • Confirmation that the emission is produced by a loss-cone-driven Cyclotron Maser 13 Instability 14 • Ganymede-induced radio emission is produced by electrons of ∼ 4-15 keV, at a ◦ ◦ 15 beaming angle [76 -83 ], and a frequency 1:005 − 1:021 × fce Corresponding author: C. K. Louis, [email protected] {1{ manuscript submitted to Geophysical Research Letters 16 Abstract 17 At Jupiter, part of the auroral radio emissions are induced by the Galilean moons 18 Io, Europa and Ganymede. Until now, they have been remotely detected, using ground- 19 based radio-telescopes or electric antennas aboard spacecraft. The polar trajectory of 20 the Juno orbiter allows the spacecraft to cross the magnetic flux tubes connected to these 21 moons, or their tail, and gives a direct measure of the characteristics of these decamet- 22 ric moon{induced radio emissions. In this study, we focus on the detection of a radio emis- 23 sion during the crossing of magnetic field lines connected to Ganymede's tail. Us- 24 ing electromagnetic waves (Juno/Waves) and in-situ electron measurements (Juno/JADE- 25 E), we estimate the radio source size of ∼ 250 km, a radio emission growth rate −4 26 > 3 × 10 , an resonant electron population of energy E = 4 − 15 keV and an emis- ◦ ◦ 27 sion beaming angle of θ = 76 −83 , at a frequency ∼ 1:005−1:021×fce. We also con- 28 firmed that radio emission is associated with Ganymede's down-tail far-ultraviolet emis- 29 sion. 30 Plain Language Summary 31 The Juno spacecraft crossed magnetic field lines connected to Ganymede's auro- 32 ral signature in Jupiter's atmosphere. At the same time, Juno also crossed a decamet- 33 ric radio source. By measuring the electrons during this radio source crossing, we deter- 34 mine that this emission is produced by the cyclotron maser instability driven by upgo- 35 ing electrons, at a frequency 0:5 to 2:1% above the cyclotron electronic frequency with 36 electrons of energy 4-15 keV. 37 1 Introduction 38 With the arrival of Juno at Jupiter in July 2016, the probe passes above the poles 39 once per orbit, every 53 days, and acquires high-resolution measurements in the auro- 40 ral regions (Bagenal et al., 2017). In particular the instruments Waves (radio and plasma 41 waves, Kurth et al., 2017), JADE-E (Jovian Auroral Distributions Experiment - Elec- 42 trons, McComas et al., 2017) and MAG (Magnetometer , Connerney et al., 2017) offer 43 a unique opportunity to investigate in-situ the Jovian radio emissions produced in these 44 polar regions. These instruments enable constraints on the position of the sources (Louis 45 et al., 2019; Imai et al., 2017, 2019) and the mechanism producing these emissions (Louarn {2{ manuscript submitted to Geophysical Research Letters 46 et al., 2017, 2018), the Cyclotron Maser Instability (CMI), which is also responsible for 47 the production of the auroral kilometric radiation at Earth and Saturn (Treumann, 2006; 48 Wu, 1985; Wu & Lee, 1979; Le Queau et al., 1984b, 1984a; Pritchett, 1986a). 49 This instability produces emissions very close to the electron cyclotron frequency 50 fce, and requires two primary conditions: (i) a magnetized plasma, where the electron 51 plasma frequency fpe (proportional to the square root of the electron plasma density ne) 52 is much lower than the electron cyclotron frequency fce (proportional to the magnetic 53 field amplitude B); and (ii) a weakly relativistic electron population previously accel- 54 erated along high-latitude magnetic field lines at typical energies of a few keV. The first 55 orbits of Jupiter allowed Louarn et al. (2017, 2018) to study in-situ the radio emission 56 during source crossings and determine that the auroral hectometric/decametric radio emis- 57 sions are driven by the CMI with a loss cone distribution function, i.e. triggered by a 58 lack in the up-going electron population. 59 The Jupiter auroral radio emission is split into three major components, depend- 60 ing on the emission wavelength, namely broadband kilometric, hectometric and deca- 61 metric. Part of the auroral radio emissions in the decametric range are induced by the 62 interaction between the jovian magnetosphere and the Galilean moons: the best known 63 case Io, discovered by Bigg (1964), Europa and Ganymede (Louis, Lamy, Zarka, Cec- 64 coni, & Hess, 2017; Zarka et al., 2018, 2017) and potentially Callisto (Menietti et 65 al., 2001; Higgins, 2007). These moons are also known to induce Far Ultraviolet (FUV) 66 aurora above Jupiter's atmosphere (Prang´eet al., 1996; Clarke, 1998; Clarke et 67 al., 2002; Bhattacharyya et al., 2018). 68 In the Io case, we know that FUV and radio auroral emission are produced by Alfv´enic 69 interactions, and that Io-induced radio emissions are produced on the magnetic field lines 70 connected to the main Alfv´enwing (MAW) and reflected Alfv´enwing (RAW) spots (Hess 71 et al., 2010). In the Europa and Ganymede case, FUV emissions have been observed 72 at the moon's footprint and along the moon's footprint tail (Bonfond, Gro- 73 dent, et al., 2017; Bonfond, Saur, et al., 2017), but no simultaneous observation 74 of FUV and radio emissions has yet been obtained. 75 In this study, we focus on Juno's crossing of field lines connected to Ganymede's 76 footprint tail, which took place on May 29, 2019, where simultaneous FUV (Szalay et 77 al., 2020a) and radio emission were observed (see Section 2). In Section 3 we present the {3{ manuscript submitted to Geophysical Research Letters 78 instability leading to radio emission and the calculation to determine the different pa- 79 rameters of the radio emission (growth rate, electron distribution function and energy, 80 opening of the emission cone). Finally in Section 4 we summarize and discuss the results. 81 2 Observations th th 82 On May 29 , 2019 between 07:37:14 and 07:37:32 (20 perijove) Juno crossed ◦ 83 the magnetic field lines connected to Ganymede's tail (∼ 8 downtail from Ganymede's 84 main auroral spot). The in-situ measurements of Juno/MAG and Juno/JADE for the 85 down-going electrons and the Juno/UVS images were used by Szalay et al. (2020a) to 86 show the presence of Alfv´enwave activity capable of accelerating electrons into the at- 87 mosphere and producing FUV emissions, observed at the footprint of the crossed mag- 88 netic field lines. Here we focus on the study of Juno/JADE for the up-going electrons 89 and the radio measurements of Juno/Waves. 90 Figure 1 displays Juno measurements around the Ganymede's tail flux tube en- 91 counter. Panel (a) presents the Juno/Waves measurements (low resolution mode) around 92 the twentieth perijove (∼ −2=+1 h). Panel (b) is a 5-minute zoom-in of panel (a) us- 93 ing the Juno/Waves high-resolution mode. The solid-white line represents fce while the 94 dashed-white line (panel b) represents 1:01×fce (typical frequency for a loss-cone-CMI- 95 driven emission with electron energy of ∼ 5 keV, see Louarn et al., 2017). Panels (c{ 96 f) display Juno/JADE-E (electrons) measurements: panel (c) presents the electron dif- 97 ferential energy flux; panels (d-e) display the electron distribution functions for energy 98 in range [2-21] keV for different pitch angle ranges, panel (e) showing a subset for 99 pitch angle corresponding to up-going electrons; panel (f) presents the par- 100 tial electron density, where all the low energy population (here < 0:050 keV) 101 is not accounted for. 102 Figure 1b displays an emission very close to fce, tangent to the 1:01×fce line, be- 103 tween ∼ 07:37:00 and ∼ 07:38:10. During this time interval, and more precisely between 104 ∼ 07:37:14 and ∼07:37:32 (during Ganymede's tail magnetic field lines crossing), we 105 observe an enhancement in the electron energy flux (panel c) at a few keV, a strong in- 106 tensification in the distribution function (panel d) and an increase of the electron den- 107 sity (panel f). {4{ manuscript submitted to Geophysical Research Letters 20 a Waves 3 5 dB above bacakgroun ) 3 0 15 2 5 2 0 Freq. (MHz 10 1 5 1 0 d 5 5 0 06:00 06:20 06:40 07:00 07:20 07:40 08:00 08:20 08:40 09:00 Waves 7.0 b 3 0 dB above bacakgroun 6.8 ) 2 5 6.6 2 0 Freq. (MHz 6.4 1 5 d 6.2 1 0 6.0 5 (sec 10 c -1 .cm (keV) 1 -2 .sr -1 Electron energy 0.1 ) d (deg) Pitch angle (s 3 .km e -6 ) (deg) Pitch angle f ) -3 (cm Electron density 07:35 07:36 07:37 07:38 07:39 07:40 RJ 1.53 1.51 1.49 1.47 1.45 1.43 LonIII 284.30 290.60 296.50 302.00 307.10 311.70 Lat 78.29 77.78 77.14 76.39 75.53 74.56 MLatJRM09 74.75 73.52 72.24 70.92 69.55 68.14 MLT 14.55 14.43 14.33 14.23 14.15 14.08 L 22.19 18.81 16.04 13.77 11.89 10.32 2019-05-29 (149) 7:35 to 7:40 Figure 1.
Recommended publications
  • Lessons Learned from the Juno Project
    Lessons Learned from the Juno Project Presented by: William McAlpine Insoo Jun EJSM Instrument Workshop January 18‐20, 2010 © 2010 All rights reserved. Pre‐decisional, For Planning and Discussion Purposes Only Y‐1 Topics Covered • Radiation environment • Radiation control program • Radiation control program lessons learned Pre‐decisional, For Planning and Discussion Purposes Only Y‐2 Juno Radiation Environments Pre‐decisional, For Planning and Discussion Purposes Only Y‐3 Radiation Environment Comparison • Juno TID environment is about a factor of 5 less than JEO • Juno peak flux rate is about a factor of 3 above JEO Pre‐decisional, For Planning and Discussion Purposes Only Y‐4 Approach for Mitigating Radiation (1) • Assign a radiation control manager to act as a focal point for radiation related activities and issues across the Project early in the lifecycle – Requirements, EEE parts, materials, environments, and verification • Establish a radiation advisory board to address challenging radiation control issues • Hold external reviews for challenging radiation control issues • Establish a radiation control process that defines environments, defines requirements, and radiation requirements verification documentation • Design the mission trajectory to minimize the radiation exposure Pre‐decisional, For Planning and Discussion Purposes Only Y‐5 Approach for Mitigating Radiation (2) • Optimize shielding design to accommodate cumulative total ionizing dose and displacement damage dose and instantaneous charged particle fluxes near Perijove
    [Show full text]
  • 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.
    [Show full text]
  • Juno Magnetometer (MAG) Standard Product Data Record and Archive Volume Software Interface Specification
    Juno Magnetometer Juno Magnetometer (MAG) Standard Product Data Record and Archive Volume Software Interface Specification Preliminary March 6, 2018 Prepared by: Jack Connerney and Patricia Lawton Juno Magnetometer MAG Standard Product Data Record and Archive Volume Software Interface Specification Preliminary March 6, 2018 Approved: John E. P. Connerney Date MAG Principal Investigator Raymond J. Walker Date PDS PPI Node Manager Concurrence: Patricia J. Lawton Date MAG Ground Data System Staff 2 Table of Contents 1 Introduction ............................................................................................................................. 1 1.1 Distribution list ................................................................................................................... 1 1.2 Document change log ......................................................................................................... 2 1.3 TBD items ........................................................................................................................... 3 1.4 Abbreviations ...................................................................................................................... 4 1.5 Glossary .............................................................................................................................. 6 1.6 Juno Mission Overview ...................................................................................................... 7 1.7 Software Interface Specification Content Overview .........................................................
    [Show full text]
  • Dynamics of the J Avian Magnetosphere
    25 Dynamics of the J avian Magnetosphere N. Krupp, V. M. Vasyliunas, J. Woch, A. Lagg Max-Planck-Institut fur Sonnensystemforschung, Katlenburg-Lindau K. K. Khurana, M. G. Kivelson IGPP and Dept. Earth & Space Sciences, University of California, Los Angeles B. H. Mauk, E. C. Roelof, D. J. Williams, S. M. Krimigis The Johns Hopkins University Applied Physics Laboratory W. S. Kurth, L. A. Frank, W. R. Paterson Dept. of Physics & As.tronomy, University of Iowa 25.1 INTRODUCTION around Jupiter for almost 8 years (1995-2003), Galileo has collected in situ data of the jovian system over an extended Understanding the dynamic processes in the largest magne­ duration and has for the first time made possible the study tosphere of our solar system is one of the outstanding goals of Jupiter on timescales of weeks, months, and even years, of magnetospheric physics. These processes are associated using the same instrumentation. New regions of the jovian with temporal and/ or spatial variations of the global config­ magnetosphere have been explored, especially the jovian uration. Their timescales range from several tens of minutes magnetotail which was not visited by any of the previous to sizeable fractions of the planetary rotation period to long­ spacecraft (except, to a very minor extent, by Voyager 2). term variations which take several days to develop. They oc­ Additional inputs have become available from ground-based cur on both local and global spatial scales, out to dimensions and Earth-orbit-based measurements and from advanced representing a large fraction of the magnetosphere. global magneto hydrodynamic (MHD) simulations of the jo­ Early indications of a "living", varying jovian magneto­ vian magnetosphere.
    [Show full text]
  • Juno Observations of Large-Scale Compressions of Jupiter's Dawnside
    PUBLICATIONS Geophysical Research Letters RESEARCH LETTER Juno observations of large-scale compressions 10.1002/2017GL073132 of Jupiter’s dawnside magnetopause Special Section: Daniel J. Gershman1,2 , Gina A. DiBraccio2,3 , John E. P. Connerney2,4 , George Hospodarsky5 , Early Results: Juno at Jupiter William S. Kurth5 , Robert W. Ebert6 , Jamey R. Szalay6 , Robert J. Wilson7 , Frederic Allegrini6,7 , Phil Valek6,7 , David J. McComas6,8,9 , Fran Bagenal10 , Key Points: Steve Levin11 , and Scott J. Bolton6 • Jupiter’s dawnside magnetosphere is highly compressible and subject to 1Department of Astronomy, University of Maryland, College Park, College Park, Maryland, USA, 2NASA Goddard Spaceflight strong Alfvén-magnetosonic mode Center, Greenbelt, Maryland, USA, 3Universities Space Research Association, Columbia, Maryland, USA, 4Space Research coupling 5 • Magnetospheric compressions may Corporation, Annapolis, Maryland, USA, Department of Physics and Astronomy, University of Iowa, Iowa City, Iowa, USA, 6 7 enhance reconnection rates and Southwest Research Institute, San Antonio, Texas, USA, Department of Physics and Astronomy, University of Texas at San increase mass transport across the Antonio, San Antonio, Texas, USA, 8Department of Astrophysical Sciences, Princeton University, Princeton, New Jersey, USA, magnetopause 9Office of the VP for the Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jersey, USA, • Total pressure increases inside the 10Laboratory for Atmospheric and Space Physics, University of Colorado
    [Show full text]
  • EGU2018-10209, 2018 EGU General Assembly 2018 © Author(S) 2018
    Geophysical Research Abstracts Vol. 20, EGU2018-10209, 2018 EGU General Assembly 2018 © Author(s) 2018. CC Attribution 4.0 license. Jupiter’s auroras in radio and ultraviolet wavelengths as seen from Juno Masafumi Imai (1), G. Randall Gladstone (2), William S. Kurth (1), Thomas K. Greathouse (2), George B. Hospodarsky (1), Scott J. Bolton (2), John E. P. Connerney (3), and Steven M. Levin (4) (1) University of Iowa, Iowa City, Iowa, United States ([email protected]), (2) Southwest Research Institute, San Antonio, Texas, United States, (3) NASA Goddard Space Flight Center, Greenbelt, Maryland, United States, (4) Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, United States Jupiter is the strongest auroral radio source in our solar system, producing low-frequency radio emissions in a broad frequency range from 10 kHz to 40 MHz from both north and south polar regions of the planet. These sporadic nonthermal bursts and ultraviolet (UV) auroras have been monitored with the radio and plasma wave instrument (Waves) and the ultraviolet spectrograph instrument (Juno-UVS) aboard the spinning Juno spacecraft in polar orbit about Jupiter since July 5, 2016. Waves is capable of recording the electric fields of waves from 50 Hz to 41 MHz with one electric dipole antenna and the magnetic fields of waves from 50 Hz to 20 kHz with one magnetic search coil sensor. Juno-UVS is designed to image and obtain spectra in a wavelength range from 70 to 205 nm with a 4 cm by 4 cm aperture. The Juno spacecraft rotates with a period of 30 s, which modulates the Waves spectral intensity sensed with the dipole antenna.
    [Show full text]
  • Radiation: Lessons Learned
    Radiation:Radiation: LessonsLessons LearnedLearned Scott Bolton Southwest Research Institute Insoo Jun Jet Propulsion Laboratory This document has been reviewed for export control and it does NOT contain controlled technical data. Juno Science Objectives • Origin – Determine O/H ratio (water abundance) and constrain core mass to decide among alternative theories of origin. • Interior – Understand Jupiter's interior structure and dynamical properties by mapping its gravitational and magnetic fields. • Atmosphere – Map variations in atmospheric composition, temperature, cloud opacity and dynamics to depths greater than 100 bars. • Polar Magnetosphere – Explore the three-dimensional structure of Jupiter's polar magnetosphere and aurorae. Juno Juno Payload Gravity Science (JPL/Italy) Magnetometer— MAG (GSFC) Microwave Radiometer— MWR (JPL) Energetic Particles —JEDI (APL) Plasma ions and electrons — JADE (SwRI) Plasma waves/radio — Waves (U of Iowa) Ultra Violet Imager — UVS (SwRI) Visible Camera – Juno Cam (Malin) InfraRed Imager – JIRAM (Italy) Radiation Lessons Learned 3 Juno Juno Mission Design Launch: August 2011 5 year cruise Baseline mission: 32 polar orbits Perijove ~5000 km 11 day period Spinner Solar-powered Orbit is designed to avoid radiation from the inner belts of Jupiter. Dips inside inner belt at perijove and goes above belts (Juno is in polar orbit). Radiation Lessons Learned 4 Juno Orbit 4: Juno Gravity Science 5 days 4 days 6-hour Jupiter science pass 3 days 2 days 1 day Opportunities for 0 communication 11 with Earth 10
    [Show full text]
  • The Pulsating Magnetosphere at Jupiter
    EGU2020-3651 https://doi.org/10.5194/egusphere-egu2020-3651 EGU General Assembly 2020 © Author(s) 2021. This work is distributed under the Creative Commons Attribution 4.0 License. The Pulsating Magnetosphere at Jupiter Harry Manners and Adam Masters Space and Atmospheric Physics Group, Blackett Laboratory, Imperial College London, London, UK ([email protected]) The magnetosphere of Jupiter is the largest planetary magnetosphere in the solar system, and plays host to internal dynamics that remain, in many ways, mysterious. Prominent among these mysteries are the ultra-low-frequency (ULF) pulses ubiquitous in this system. Pulsations in the electromagnetic emissions, magnetic field and flux of energetic particles have been observed for decades, with little to indicate the source mechanism. While ULF waves have been observed in the magnetospheres of all the magnetized planets, the magnetospheric environment at Jupiter seems particularly conducive to the emergence of ULF waves over a wide range of periods (1-100+ minutes). This is mainly due to the high variability of the system on a global scale: internal plasma sources and a powerful intrinsic magnetic field produce a highly-compressible magnetospheric cavity, which can be reduced to a size significantly smaller than its nominal expanded state by variations in the dynamic pressure of the solar wind. Compressive fronts in the solar wind, turbulent surface interactions on the magnetopause and internal plasma processes can also all lead to ULF wave activity inside the magnetosphere. To gain the first comprehensive view of ULF waves in the Jovian system, we have performed a heritage survey of magnetic field data measured by six spacecraft that visited the magnetosphere (Galileo, Ulysses, Voyager 1 & 2 and Pioneer 10 & 11).
    [Show full text]
  • First Observations Near Jupiter by the Juno Waves Investigation
    FIRST OBSERVATIONS NEAR JUPITER BY THE JUNO WAVES INVESTIGATION W. S. Kurth∗,M.Imai∗, G. B. Hospodarsky∗, D. A. Gurnett∗, S. S. Tetrick∗, S.–Y. Ye∗, S. J. Bolton†,J.E.P.Connerney‡, andS.M.Levin§ Abstract The Juno spacecraft successfully entered Jupiter orbit on 5 July 2016. One of Juno’s primary objectives is to explore Jupiter’s polar magnetosphere for the first time. An obvious major aspect of this exploration includes remote and in-situ observations of Jupiter’s auroras and the processes responsible for them. To this end, Juno carries a suite of particle, field, and remote sensing instruments. One of these instruments is a radio and plasma wave instrument called Waves, designed to detect one electric field component of waves in the frequency range of 50 Hz to 41 MHz and one magnetic field component of waves in the range of 50 Hz to 20 kHz. Juno’s first perijove pass with science observations occurred on 27 August 2016. This paper presents some of the first observations of the Juno Waves instrument made during that first perijove. Among radio emissions, kilometric, hectometric, and decametric emissions were observed. From a vantage point at high latitudes, many of Jupiter’s auroral radio emissions appear as V-shaped emissions in frequency–time space with vertices near the electron cyclotron frequency where the emissions intensify. In fact, we present observations suggesting Juno flew through or close to as many as five or six sources of auroral radio emissions during its first perijove. Waves made in-situ observations of plasma waves on auroral field lines such as whistler–mode hiss, a common feature of terrestrial auroral regions.
    [Show full text]
  • Plasma Waves in Jupiter's High Latitude Regions
    PLASMA WAVES IN JUPITER’S HIGH LATITUDE REGIONS: OBSERVATIONS FROM THE JUNO SPACECRAFT by Sadie Suzanne Tetrick A thesis submitted in partial fulfillment of the requirements for the Master of Science degree in Physics in the Graduate College of The University of Iowa December 2017 Thesis Supervisor: Professor Donald A. Gurnett Copyright by SADIE SUZANNE TETRICK 2017 All Rights Reserved Graduate College The University of Iowa Iowa City, Iowa CERTIFICATE OF APPROVAL ____________________________ MASTER'S THESIS _________________ This is to certify that the Master's thesis of Sadie Suzanne Tetrick has been approved by the Examining Committee for the thesis requirement for the Master of Science degree in Physics at the December 2017 graduation. Thesis Committee: Donald A. Gurnett, Thesis Supervisor Jasper S. Halekas, Committee Member Vincent G. J. Rodgers, Committee Member ACKNOWLEDGEMENTS A special thanks to Dr. Donald Gurnett and Dr. Bill Kurth for providing me the opportunity to work on Juno research and for their continued support during the completion of my Master of Science degree. I would also like to thank Masafumi Imai, Jeremy Faden, and Terry Averkamp for their help, feedback, and encouragement that has allowed me to successfully complete this research. A final thank you to my parents, Kelly and Paul Tetrick, my soon-to-be parents-in-law, Rose and Scott Elliott, and fiancé, Josh Elliott for their continued support throughout my educational journey. ii ABSTRACT The Juno Waves instrument detected new broadband plasma wave emissions on the first three successful passes over the low altitude polar regions of Jupiter on Days 240 and 346 of 2016 and Day 033 of 2017.
    [Show full text]
  • A Survey of Small-Scale Waves and Wave-Like Phenomena in Jupiter's Atmosphere Detected by Junocam
    1 A Survey of Small-Scale Waves and Wave-Like Phenomena in 2 Jupiter’s Atmosphere Detected by JunoCam 3 4 Glenn S. Orton1, Fachreddin Tabataba-Vakili1, Gerald Eichstädt2, John Rogers3, 5 Candice J. Hansen4, Thomas W. Momary1, Andrew P. Ingersoll5, Shawn Brueshaber 6, Michael 6 H. Wong7, Amy A. Simon8, Leigh N. Fletcher9, Michael Ravine10, Michael Caplinger10, Dakota 7 Smith11, Scott J. Bolton12, Stephen M. Levin1, James A. Sinclair1, Chloe Thepenier13, Hamish 8 Nicholson14, Abigail Anthony15 9 10 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA 11 2Independent scholar, Stuttgart, Germany 12 3British Astronomical Association, London, UK 13 4Planetary Science Institute, Tucson, Arizona, USA 14 5California Institute of Technology, Pasadena, California, USA 15 6Western Michigan University, Kalamazoo, Michigan, USA 16 7University of California, Berkeley, California, USA; SETI Institute, Mountain View, California, 17 USA 18 8NASA Goddard Space Flight Center, Greenbelt, Maryland, USA 19 9University of Leicester, Leicester, UK 20 10Malin Space Science Systems, San Diego, California, USA 21 11 National Center for Atmospheric Research, Boulder, Colorado, USA 22 12Southwest Research Institute, San Antonio, Texas, USA 23 13Glendale Community College, Glendale, California, USA† 24 14Harvard College, Cambridge, Massachusetts, USA 25 15Golden West College, Huntington Beach, California, USA†† 26 27 28 Corresponding author: Glenn Orton ([email protected]) 29 30 31 †currently at the University of California, Davis 32 ††currently at the University of California, Berkeley 33 34 Key Points: 35 -In the first 20 orbits of the Juno mission, over 150 waves and wave-like features have been 36 detected by the JunoCam public-outreach camera.
    [Show full text]
  • A Look Inside the Juno Mission to Jupiter12 Richard S
    A Look Inside the Juno Mission to Jupiter12 Richard S. Grammier Jet Propulsion Laboratory, California Institute of Technology 4800 Oak Grove Drive, M/S 301-320 Pasadena, CA 91109 818-354-0596 [email protected] Abstract—Juno, the second mission within the New deep-space maneuvers approximately one year after launch, Frontiers Program, is a Jupiter polar orbiter mission perform an Earth-gravity assist approximately 26 months designed to return high-priority science data that spans after launch, and achieve Jupiter orbit insertion in 2016 after across multiple divisions within NASA’s Science Mission a five-year journey. Juno will investigate the gas giant for Directorate. Juno’s science objectives, coupled with the one year, operating a suite of eight instruments to meet its natural constraints of a cost-capped, PI-led mission and the scientific objectives. After completing one year of orbital harsh environment of Jupiter, have led to a very unique science, the spacecraft will de-orbit into Jupiter for the mission and spacecraft design. purpose of planetary protection. The mission and spacecraft design accommodates the required payload suite of instruments in a way that maximizes science data collection and return, maintains a simplified orbital operations approach, and meets the many challenges associated with operating a spin-stabilized, solar- powered spacecraft in Jupiter’s high radiation and magnetic environment. The project’s efforts during the preliminary design phase have resulted in an integrated design and operations approach that meets all science objectives, retains significant technical, schedule and cost margins, and has retired key risks and challenges.
    [Show full text]