AN OVERVIEW of the JUNO MISSION to JUPITER Abstract Contents 1 Overview
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The 4 Major Asteroids and Chiron Report For
The 4 Major Asteroids and Chiron Report for Brad Roberts 10 January 1964 6:33 AM Winnipeg, Manitoba,Canada Calculated for: Standard time, Time Zone 6 hours West Latitude: 49 N 53 Longitude: 97 W 09 Positions of Planets at Birth: Sun 19 Cap 18 Asc. 20 Sag 35 Moon 1 Sag 21 MC 21 Lib 49 Mercury 6 Cap 24 2nd cusp 0 Aqu 56 Venus 21 Aqu 54 3rd cusp 17 Pis 07 Mars 27 Cap 52 5th cusp 15 Tau 45 Jupiter 11 Ari 42 6th cusp 4 Gem 07 Saturn 21 Aqu 25 Ceres 9 Sag 44 Uranus 9 Vir 47 Pallas 20 Sco 12 Neptune 17 Sco 47 Juno 23 Sco 36 Pluto 14 Vir 47 Vesta 4 Cap 54 True Node11 Can 47 Chiron 11 Pis 23 Aspects and orbs: Conjunction : 7 Deg 00 Min Trine : 5 Deg 00 Min Opposition : 6 Deg 00 Min Sextile : 3 Deg 00 Min Square : 4 Deg 00 Min Interpretations by astrologer Dave Campbell Report and Text Copyright By Cosmic Patterns Software, Inc. The contents of this report are protected by Copyright law. By purchasing this report you agree to comply with this Copyright. Libra Moon, Inc www.libramoonastrology.com www.zodiac-reports.com Chapter 1: Ceres Ceres in Sagittarius: You nurture people with your generosity cheerfulness and encouragement. Giving them the optimism and openness they need. You aim to inspire them and make them feel like they are it. Your honest disposition and behavior is also a gift for them to know your devotion to them. All of these things are exactly what you need in order to feel cared for. -
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. -
Occultation Newsletter Volume 8, Number 4
Volume 12, Number 1 January 2005 $5.00 North Am./$6.25 Other International Occultation Timing Association, Inc. (IOTA) In this Issue Article Page The Largest Members Of Our Solar System – 2005 . 4 Resources Page What to Send to Whom . 3 Membership and Subscription Information . 3 IOTA Publications. 3 The Offices and Officers of IOTA . .11 IOTA European Section (IOTA/ES) . .11 IOTA on the World Wide Web. Back Cover ON THE COVER: Steve Preston posted a prediction for the occultation of a 10.8-magnitude star in Orion, about 3° from Betelgeuse, by the asteroid (238) Hypatia, which had an expected diameter of 148 km. The predicted path passed over the San Francisco Bay area, and that turned out to be quite accurate, with only a small shift towards the north, enough to leave Richard Nolthenius, observing visually from the coast northwest of Santa Cruz, to have a miss. But farther north, three other observers video recorded the occultation from their homes, and they were fortuitously located to define three well- spaced chords across the asteroid to accurately measure its shape and location relative to the star, as shown in the figure. The dashed lines show the axes of the fitted ellipse, produced by Dave Herald’s WinOccult program. This demonstrates the good results that can be obtained by a few dedicated observers with a relatively faint star; a bright star and/or many observers are not always necessary to obtain solid useful observations. – David Dunham Publication Date for this issue: July 2005 Please note: The date shown on the cover is for subscription purposes only and does not reflect the actual publication date. -
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 ......................................................... -
Planetary Science
Mission Directorate: Science Theme: Planetary Science Theme Overview Planetary Science is a grand human enterprise that seeks to discover the nature and origin of the celestial bodies among which we live, and to explore whether life exists beyond Earth. The scientific imperative for Planetary Science, the quest to understand our origins, is universal. How did we get here? Are we alone? What does the future hold? These overarching questions lead to more focused, fundamental science questions about our solar system: How did the Sun's family of planets, satellites, and minor bodies originate and evolve? What are the characteristics of the solar system that lead to habitable environments? How and where could life begin and evolve in the solar system? What are the characteristics of small bodies and planetary environments and what potential hazards or resources do they hold? To address these science questions, NASA relies on various flight missions, research and analysis (R&A) and technology development. There are seven programs within the Planetary Science Theme: R&A, Lunar Quest, Discovery, New Frontiers, Mars Exploration, Outer Planets, and Technology. R&A supports two operating missions with international partners (Rosetta and Hayabusa), as well as sample curation, data archiving, dissemination and analysis, and Near Earth Object Observations. The Lunar Quest Program consists of small robotic spacecraft missions, Missions of Opportunity, Lunar Science Institute, and R&A. Discovery has two spacecraft in prime mission operations (MESSENGER and Dawn), an instrument operating on an ESA Mars Express mission (ASPERA-3), a mission in its development phase (GRAIL), three Missions of Opportunities (M3, Strofio, and LaRa), and three investigations using re-purposed spacecraft: EPOCh and DIXI hosted on the Deep Impact spacecraft and NExT hosted on the Stardust spacecraft. -
Phase Integral of Asteroids Vasilij G
A&A 626, A87 (2019) Astronomy https://doi.org/10.1051/0004-6361/201935588 & © ESO 2019 Astrophysics Phase integral of asteroids Vasilij G. Shevchenko1,2, Irina N. Belskaya2, Olga I. Mikhalchenko1,2, Karri Muinonen3,4, Antti Penttilä3, Maria Gritsevich3,5, Yuriy G. Shkuratov2, Ivan G. Slyusarev1,2, and Gorden Videen6 1 Department of Astronomy and Space Informatics, V.N. Karazin Kharkiv National University, 4 Svobody Sq., Kharkiv 61022, Ukraine e-mail: [email protected] 2 Institute of Astronomy, V.N. Karazin Kharkiv National University, 4 Svobody Sq., Kharkiv 61022, Ukraine 3 Department of Physics, University of Helsinki, Gustaf Hällströmin katu 2, 00560 Helsinki, Finland 4 Finnish Geospatial Research Institute FGI, Geodeetinrinne 2, 02430 Masala, Finland 5 Institute of Physics and Technology, Ural Federal University, Mira str. 19, 620002 Ekaterinburg, Russia 6 Space Science Institute, 4750 Walnut St. Suite 205, Boulder CO 80301, USA Received 31 March 2019 / Accepted 20 May 2019 ABSTRACT The values of the phase integral q were determined for asteroids using a numerical integration of the brightness phase functions over a wide phase-angle range and the relations between q and the G parameter of the HG function and q and the G1, G2 parameters of the HG1G2 function. The phase-integral values for asteroids of different geometric albedo range from 0.34 to 0.54 with an average value of 0.44. These values can be used for the determination of the Bond albedo of asteroids. Estimates for the phase-integral values using the G1 and G2 parameters are in very good agreement with the available observational data. -
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 -
Iso and Asteroids
r bulletin 108 Figure 1. Asteroid Ida and its moon Dactyl in enhanced colour. This colour picture is made from images taken by the Galileo spacecraft just before its closest approach to asteroid 243 Ida on 28 August 1993. The moon Dactyl is visible to the right of the asteroid. The colour is ‘enhanced’ in the sense that the CCD camera is sensitive to near-infrared wavelengths of light beyond human vision; a ‘natural’ colour picture of this asteroid would appear mostly grey. Shadings in the image indicate changes in illumination angle on the many steep slopes of this irregular body, as well as subtle colour variations due to differences in the physical state and composition of the soil (regolith). There are brighter areas, appearing bluish in the picture, around craters on the upper left end of Ida, around the small bright crater near the centre of the asteroid, and near the upper right-hand edge (the limb). This is a combination of more reflected blue light and greater absorption of near-infrared light, suggesting a difference Figure 2. This image mosaic of asteroid 253 Mathilde is in the abundance or constructed from four images acquired by the NEAR spacecraft composition of iron-bearing on 27 June 1997. The part of the asteroid shown is about 59 km minerals in these areas. Ida’s by 47 km. Details as small as 380 m can be discerned. The moon also has a deeper near- surface exhibits many large craters, including the deeply infrared absorption and a shadowed one at the centre, which is estimated to be more than different colour in the violet than any 10 km deep. -
Appendix 1 1311 Discoverers in Alphabetical Order
Appendix 1 1311 Discoverers in Alphabetical Order Abe, H. 28 (8) 1993-1999 Bernstein, G. 1 1998 Abe, M. 1 (1) 1994 Bettelheim, E. 1 (1) 2000 Abraham, M. 3 (3) 1999 Bickel, W. 443 1995-2010 Aikman, G. C. L. 4 1994-1998 Biggs, J. 1 2001 Akiyama, M. 16 (10) 1989-1999 Bigourdan, G. 1 1894 Albitskij, V. A. 10 1923-1925 Billings, G. W. 6 1999 Aldering, G. 4 1982 Binzel, R. P. 3 1987-1990 Alikoski, H. 13 1938-1953 Birkle, K. 8 (8) 1989-1993 Allen, E. J. 1 2004 Birtwhistle, P. 56 2003-2009 Allen, L. 2 2004 Blasco, M. 5 (1) 1996-2000 Alu, J. 24 (13) 1987-1993 Block, A. 1 2000 Amburgey, L. L. 2 1997-2000 Boattini, A. 237 (224) 1977-2006 Andrews, A. D. 1 1965 Boehnhardt, H. 1 (1) 1993 Antal, M. 17 1971-1988 Boeker, A. 1 (1) 2002 Antolini, P. 4 (3) 1994-1996 Boeuf, M. 12 1998-2000 Antonini, P. 35 1997-1999 Boffin, H. M. J. 10 (2) 1999-2001 Aoki, M. 2 1996-1997 Bohrmann, A. 9 1936-1938 Apitzsch, R. 43 2004-2009 Boles, T. 1 2002 Arai, M. 45 (45) 1988-1991 Bonomi, R. 1 (1) 1995 Araki, H. 2 (2) 1994 Borgman, D. 1 (1) 2004 Arend, S. 51 1929-1961 B¨orngen, F. 535 (231) 1961-1995 Armstrong, C. 1 (1) 1997 Borrelly, A. 19 1866-1894 Armstrong, M. 2 (1) 1997-1998 Bourban, G. 1 (1) 2005 Asami, A. 7 1997-1999 Bourgeois, P. 1 1929 Asher, D. -
Juno Mission to Jupiter
National Aeronautics and Space Administration Juno Mission to Jupiter unknown how deeply rooted Jupiter’s colorful, banded clouds and planet-sized spots are. And scientists yearn to understand what powers the auroras — Jupiter’s northern and southern lights. These mysteries make it clear that although Jupiter’s colorful clouds get most of the attention, some of the most enticing mysteries are hiding deep inside the planet. A Five-Year Journey Juno’s trip to Jupiter will take about five years. Though the journey may seem long, this flight plan allows the mission to use Earth’s gravity to speed the craft on its way. The spacecraft first loops around the inner solar system and then swings past Earth two years after launch to get a boost that will propel it onward to its With the exception of the sun, Jupiter is the most destination. dominant object in the solar system. Because of its enormous size and the fact that it was likely the first In July 2016, Juno will fire its main engine and slip of the planets to form, it has profoundly influenced the into orbit around the giant planet to begin its scientific formation and evolution of the other bodies that orbit mission. our star. NASA’s Juno mission will allow us to examine this gas giant planet from its innermost core to the outer A Solar-Powered, Spinning Spacecraft reaches of its enormous magnetic force field. Jupiter’s orbit is five times farther from the sun than Earth’s location, so the giant planet receives about During its mission, Juno will map Jupiter’s gravity 25 times less sunlight than Earth. -
Nasa Technical Memorandum .1
NASA TECHNICAL MEMORANDUM NASA TM X-64677 COMETS AND ASTEROIDS: A Strategy for Exploration REPORT OF THE COMET AND ASTEROID MISSION STUDY PANEL May 1972 .1!vP -V (NASA-TE-X- 6 q767 ) COMETS AND ASTEROIDS: A RR EXPLORATION (NASA) May 1972 CSCL 03A NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Reproduced by ' NATIONAL "TECHINICAL INFORMATION: SERVICE US Depdrtmett ofCommerce :. Springfield VA 22151 TECHNICAL REPORT STANDARD TITLE PAGE · REPORT NO. 2. GOVERNMENT ACCESSION NO. 3, RECIPIENT'S CATALOG NO. NASA TM X-64677 . TITLE AND SUBTITLE 5. REPORT aE COMETS AND ASTEROIDS ___1_ A Strategy for Exploration 6. PERFORMING ORGANIZATION CODE AUTHOR(S) 8. PERFORMING ORGANIZATION REPORT # Comet and Asteroid Mission Study Panel PERFORMING ORGANIZATION NAME AND ADDRESS 10. WORK UNIT NO. 11. CONTRACT OR GRANT NO. 13. TYPE OF REPORT & PERIOD COVERED 2. SPONSORING AGENCY NAME AND ADDRESS National Aeronautics and Space Administration Technical Memorandum Washington, D. C. 20546 14. SPONSORING AGENCY CODE 5. SUPPLEMENTARY NOTES ABSTRACT Many of the asteroids probably formed near the orbits where they are found today. They accreted from gases and particles that represented the primordial solar system cloud at that location. Comets, in contrast to asteroids, probably formed far out in the solar system, and at very low temperatures; since they have retained their volatile components they are probably the most primordial matter that presently can be found anywhere in the solar system. Exploration and detailed study of comets and asteroids, therefore, should be a significant part of NASA's efforts to understand the solar system. A comet and asteroid program should consist of six major types of projects: ground-based observations;Earth-orbital observations; flybys; rendezvous; landings; and sample returns. -
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.