Expected Science Return of Spatially-Extended In-Situ Exploration at Small Solar System Bodies
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Russia's Posture in Space
Russia’s Posture in Space: Prospects for Europe Executive Summary Prepared by the European Space Policy Institute Marco ALIBERTI Ksenia LISITSYNA May 2018 Table of Contents Background and Research Objectives ........................................................................................ 1 Domestic Developments in Russia’s Space Programme ............................................................ 2 Russia’s International Space Posture ......................................................................................... 4 Prospects for Europe .................................................................................................................. 5 Background and Research Objectives For the 50th anniversary of the launch of Sputnik-1, in 2007, the rebirth of Russian space activities appeared well on its way. After the decade-long crisis of the 1990s, the country’s political leadership guided by President Putin gave new impetus to the development of national space activities and put the sector back among the top priorities of Moscow’s domestic and foreign policy agenda. Supported by the progressive recovery of Russia’s economy, renewed political stability, and an improving external environment, Russia re-asserted strong ambitions and the resolve to regain its original position on the international scene. Towards this, several major space programmes were adopted, including the Federal Space Programme 2006-2015, the Federal Target Programme on the development of Russian cosmodromes, and the Federal Target Programme on the redeployment of GLONASS. This renewed commitment to the development of space activities was duly reflected in a sharp increase in the country’s launch rate and space budget throughout the decade. Thanks to the funds made available by flourishing energy exports, Russia’s space expenditure continued to grow even in the midst of the global financial crisis. Besides new programmes and increased funding, the spectrum of activities was also widened to encompass a new focus on space applications and commercial products. -
Autonomous Onboard Science Data Analysis for Comet Missions
AUTONOMOUS ONBOARD SCIENCE DATA ANALYSIS FOR COMET MISSIONS David R. Thompson(1), Daniel Q. Tran(1), David McLaren(1), Steve A. Chien(1), Larry Bergman(1), Rebecca Castaño(1), Richard Doyle(1), Tara Estlin(1), Matthew Lenda(1), (1) Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr. Pasadena, CA 91109, USA Email: [email protected], all others [email protected] Figure 1. Plume detection by identifying the nucleus. Left: computational edge detection. Center: a convex hull of edge points. Right: bright areas outside the nucleus are plumes. Image credit: NASA/JPL/UMD. ABSTRACT active geologic processes including scarps and outflows [1]. Its surface undergoes continuous modification, Coming years will bring several comet rendezvous with visible change during the years between two missions. The Rosetta spacecraft arrives at Comet flybys. The EPOXI flyby of comet Hartley 2 shows 67P/Churyumov–Gerasimenko in 2014. Subsequent skyscraper-size spires, flat featureless plains that outgas rendezvous might include a mission such as the H O, regions of rough and mottled texture, bands of proposed Comet Hopper with multiple surface landings, 2 various shapes, and diverse surface albedo. Comets’ as well as Comet Nucleus Sample Return (CNSR) and active areas range from 10-90%, changing over time Coma Rendezvous and Sample Return (CRSR). These and distance to the sun. They manifest as both localized encounters will begin to shed light on a population that, jets and diffuse regions (Figure 1). Still more exotic, despite several previous flybys, remains mysterious and recently discovered “active asteroids” suggest that poorly understood. -
A Deeper Look at the Colors of the Saturnian Irregular Satellites Arxiv
A deeper look at the colors of the Saturnian irregular satellites Tommy Grav Harvard-Smithsonian Center for Astrophysics, MS51, 60 Garden St., Cambridge, MA02138 and Instiute for Astronomy, University of Hawaii, 2680 Woodlawn Dr., Honolulu, HI86822 [email protected] James Bauer Jet Propulsion Laboratory, California Institute of Technology 4800 Oak Grove Dr., MS183-501, Pasadena, CA91109 [email protected] September 13, 2018 arXiv:astro-ph/0611590v2 8 Mar 2007 Manuscript: 36 pages, with 11 figures and 5 tables. 1 Proposed running head: Colors of Saturnian irregular satellites Corresponding author: Tommy Grav MS51, 60 Garden St. Cambridge, MA02138 USA Phone: (617) 384-7689 Fax: (617) 495-7093 Email: [email protected] 2 Abstract We have performed broadband color photometry of the twelve brightest irregular satellites of Saturn with the goal of understanding their surface composition, as well as their physical relationship. We find that the satellites have a wide variety of different surface colors, from the negative spectral slopes of the two retrograde satellites S IX Phoebe (S0 = −2:5 ± 0:4) and S XXV Mundilfari (S0 = −5:0 ± 1:9) to the fairly red slope of S XXII Ijiraq (S0 = 19:5 ± 0:9). We further find that there exist a correlation between dynamical families and spectral slope, with the prograde clusters, the Gallic and Inuit, showing tight clustering in colors among most of their members. The retrograde objects are dynamically and physically more dispersed, but some internal structure is apparent. Keywords: Irregular satellites; Photometry, Satellites, Surfaces; Saturn, Satellites. 3 1 Introduction The satellites of Saturn can be divided into two distinct groups, the regular and irregular, based on their orbital characteristics. -
NASA's Curiosity Rover Maximizes Data Sent to Earth by Using International Space Data Communication Standards
Press Release For immediate release NASA's Curiosity Rover Maximizes Data Sent to Earth by Using International Space Data Communication Standards WASHINGTON, 22 August 2012 (CCSDS) – NASA’s Mars Science Laboratory (MSL) mission began its planned 2-year Mars surface exploration mission on August 6 after landing its large, mobile laboratory called Curiosity. The goal of the mission is to assess whether Mars has ever had, or still has, environmental conditions favorable to microbial life. Curiosity, with its one-ton payload carrying capacity carries 10 science instruments that will gather samples of rocks and soil, and process and distribute them to onboard test chambers inside analytical instruments. Some of the rover’s scientific data, including images of the surface of Mars collected by Curiosity’s 17 onboard cameras, are sent directly to and from Earth via NASA’s Deep Space Network (DSN) of large ground antennas. However, once Curiosity becomes fully operational most of the scientific and engineering data will be transferred via relay satellites that are in orbit around Mars. These are primarily the Mars Reconnaissance Orbiter (MRO) and the Mars Odyssey (ODY) spacecraft. The MSL Mars-Earth communications systems are using internationally-agreed space data communications standards to enable reliable transmission of the expected rich data sets to be gathered by Curiosity. These standards were developed by a team of international space data communication specialists collaborating within the Consultative Committee for Space Data Systems (CCSDS). Use of internationally-agreed upon standards reduce cost and risk to space missions, and also offer rich “cross-support” capabilities to collaborate since key data interfaces are inherently interoperable. -
Mars Reconnaissance Orbiter
Chapter 6 Mars Reconnaissance Orbiter Jim Taylor, Dennis K. Lee, and Shervin Shambayati 6.1 Mission Overview The Mars Reconnaissance Orbiter (MRO) [1, 2] has a suite of instruments making observations at Mars, and it provides data-relay services for Mars landers and rovers. MRO was launched on August 12, 2005. The orbiter successfully went into orbit around Mars on March 10, 2006 and began reducing its orbit altitude and circularizing the orbit in preparation for the science mission. The orbit changing was accomplished through a process called aerobraking, in preparation for the “science mission” starting in November 2006, followed by the “relay mission” starting in November 2008. MRO participated in the Mars Science Laboratory touchdown and surface mission that began in August 2012 (Chapter 7). MRO communications has operated in three different frequency bands: 1) Most telecom in both directions has been with the Deep Space Network (DSN) at X-band (~8 GHz), and this band will continue to provide operational commanding, telemetry transmission, and radiometric tracking. 2) During cruise, the functional characteristics of a separate Ka-band (~32 GHz) downlink system were verified in preparation for an operational demonstration during orbit operations. After a Ka-band hardware anomaly in cruise, the project has elected not to initiate the originally planned operational demonstration (with yet-to-be used redundant Ka-band hardware). 201 202 Chapter 6 3) A new-generation ultra-high frequency (UHF) (~400 MHz) system was verified with the Mars Exploration Rovers in preparation for the successful relay communications with the Phoenix lander in 2008 and the later Mars Science Laboratory relay operations. -
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. -
Agile Science Operations David R
Agile Science Operations David R. Thompson Machine Learning and Instrument Autonomy Jet Propulsion Laboratory, California Institute of Technology Engineering Resilient Space Systems Keck Institute Study, July 31 2012. A portion of this research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under contract with the National Aeronautics and Space Administration. Copyright 2012 California Institute of Technology. All Rights Reserved; U. S. Government Support Acknowledged. Image: Hartley 2 (EPOXI), NASA/JPL/UMD Jet Propulsion Laboratory / California Institute of Technology / Solar System Exploration Directorate 1 Agenda Motivation: science at primitive bodies Critical Path Analysis and reaction time A survey of onboard science data analysis Case study – how could onboard data analysis impact missions? Image: Hartley 2 (EPOXI), NASA/JPL/UMD Jet Propulsion Laboratory / California Institute of Technology / Solar System Exploration Directorate 2 Primitive bodies Jet Propulsion Laboratory / California Institute of Technology / Solar System Exploration Directorate 3 Typical encounter (Lutetia 21, Rosetta) Jet Propulsion Laboratory / California Institute of Technology / Solar System Exploration Directorate 4 Primitive bodies: key measurements Reproduced from Castillo-Rogez, Pavone, Nesnas, Hoffman, “Expected Science Return of Spatially-Extended In-Situ Exploration at Small Solar System Bodies,” IEEE Aerospace 2012. Jet Propulsion Laboratory / California Institute of Technology / Solar System Exploration Directorate -
Asteroid Retrieval Mission
Where you can put your asteroid Nathan Strange, Damon Landau, and ARRM team NASA/JPL-CalTech © 2014 California Institute of Technology. Government sponsorship acknowledged. Distant Retrograde Orbits Works for Earth, Moon, Mars, Phobos, Deimos etc… very stable orbits Other Lunar Storage Orbit Options • Lagrange Points – Earth-Moon L1/L2 • Unstable; this instability enables many interesting low-energy transfers but vehicles require active station keeping to stay in vicinity of L1/L2 – Earth-Moon L4/L5 • Some orbits in this region is may be stable, but are difficult for MPCV to reach • Lunar Weakly Captured Orbits – These are the transition from high lunar orbits to Lagrange point orbits – They are a new and less well understood class of orbits that could be long term stable and could be easier for the MPCV to reach than DROs – More study is needed to determine if these are good options • Intermittent Capture – Weakly captured Earth orbit, escapes and is then recaptured a year later • Earth Orbit with Lunar Gravity Assists – Many options with Earth-Moon gravity assist tours Backflip Orbits • A backflip orbit is two flybys half a rev apart • Could be done with the Moon, Earth or Mars. Backflip orbit • Lunar backflips are nice plane because they could be used to “catch and release” asteroids • Earth backflips are nice orbits in which to construct things out of asteroids before sending them on to places like Earth- Earth or Moon orbit plane Mars cyclers 4 Example Mars Cyclers Two-Synodic-Period Cycler Three-Synodic-Period Cycler Possibly Ballistic Chen, et al., “Powered Earth-Mars Cycler with Three Synodic-Period Repeat Time,” Journal of Spacecraft and Rockets, Sept.-Oct. -
The Orbits of Saturn's Small Satellites Derived From
The Astronomical Journal, 132:692–710, 2006 August A # 2006. The American Astronomical Society. All rights reserved. Printed in U.S.A. THE ORBITS OF SATURN’S SMALL SATELLITES DERIVED FROM COMBINED HISTORIC AND CASSINI IMAGING OBSERVATIONS J. N. Spitale CICLOPS, Space Science Institute, 4750 Walnut Street, Suite 205, Boulder, CO 80301; [email protected] R. A. Jacobson Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099 C. C. Porco CICLOPS, Space Science Institute, 4750 Walnut Street, Suite 205, Boulder, CO 80301 and W. M. Owen, Jr. Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099 Received 2006 February 28; accepted 2006 April 12 ABSTRACT We report on the orbits of the small, inner Saturnian satellites, either recovered or newly discovered in recent Cassini imaging observations. The orbits presented here reflect improvements over our previously published values in that the time base of Cassini observations has been extended, and numerical orbital integrations have been performed in those cases in which simple precessing elliptical, inclined orbit solutions were found to be inadequate. Using combined Cassini and Voyager observations, we obtain an eccentricity for Pan 7 times smaller than previously reported because of the predominance of higher quality Cassini data in the fit. The orbit of the small satellite (S/2005 S1 [Daphnis]) discovered by Cassini in the Keeler gap in the outer A ring appears to be circular and coplanar; no external perturbations are appar- ent. Refined orbits of Atlas, Prometheus, Pandora, Janus, and Epimetheus are based on Cassini , Voyager, Hubble Space Telescope, and Earth-based data and a numerical integration perturbed by all the massive satellites and each other. -
Dust Environment and Dynamical History of a Sample of Short-Period Comets II
A&A 571, A64 (2014) Astronomy DOI: 10.1051/0004-6361/201424331 & c ESO 2014 Astrophysics Dust environment and dynamical history of a sample of short-period comets II. 81P/Wild 2 and 103P/Hartley 2 F. J. Pozuelos1;3, F. Moreno1, F. Aceituno1, V. Casanova1, A. Sota1, J. J. López-Moreno1, J. Castellano2, E. Reina2, A. Climent2, A. Fernández2, A. San Segundo2, B. Häusler2, C. González2, D. Rodriguez2, E. Bryssinck2, E. Cortés2, F. A. Rodriguez2, F. Baldris2, F. García2, F. Gómez2, F. Limón2, F. Tifner2, G. Muler2, I. Almendros2, J. A. de los Reyes2, J. A. Henríquez2, J. A. Moreno2, J. Báez2, J. Bel2, J. Camarasa2, J. Curto2, J. F. Hernández2, J. J. González2, J. J. Martín2, J. L. Salto2, J. Lopesino2, J. M. Bosch2, J. M. Ruiz2, J. R. Vidal2, J. Ruiz2, J. Sánchez2, J. Temprano2, J. M. Aymamí2, L. Lahuerta2, L. Montoro2, M. Campas2, M. A. García2, O. Canales2, R. Benavides2, R. Dymock2, R. García2, R. Ligustri2, R. Naves2, S. Lahuerta2, and S. Pastor2 1 Instituto de Astrofísica de Andalucía (CSIC), Glorieta de la Astronomía s/n, 18008 Granada, Spain e-mail: [email protected] 2 Amateur Association Cometas-Obs, Spain 3 Universidad de Granada-Phd Program in Physics and Mathematics (FisyMat), 18071 Granada, Spain Received 3 June 2014 / Accepted 5 August 2014 ABSTRACT Aims. This paper is a continuation of the first paper in this series, where we presented an extended study of the dust environment of a sample of short-period comets and their dynamical history. On this occasion, we focus on comets 81P/Wild 2 and 103P/Hartley 2, which are of special interest as targets of the spacecraft missions Stardust and EPOXI. -
LAST CALL for the DAS Dinner Meeting Tuesday, May17th
Vol. 56, No. 5, May, 2011 Next Meeting – May 17th, 2011 at 6:00 PM ~ Annual Dinner Meeting at the Hilton Wilmington/Christiana ~ See Pages 4 & 5 for full Details on this Event Celebrating the DAS Amateur Astronomer of the Year FROM THE PRESIDENT ! Bill Hanagan To start off, I’d like to thank Bill McKibben for his LAST CALL for the presentation at the April meeting on the Ancient Astronomy of Machu Picchu and Greg Lee for his presentation on DAS Dinner Meeting “What’s Up in the Sky”. If you missed the April meeting, you also missed my presentation on the sizing, positioning, and th surface quality of Newtonian secondary mirrors. Tuesday, May 17 Our May meeting is the annual “dinner” meeting of the DAS and it will be held on Tuesday, May 17 at the Christiana You’ll need to call Treasurer McKibben Hilton, the same location as last year. Social hour begins at at this late hour for Reservations. 6:00 P.M. followed by dinner at 7:00 P.M. After dinner, we’ll view a short video of time lapse astrophotos followed by the Andrew K. Johnston presentation of the Amateur Astronomer of the Year Award. We’ll conclude the evening with a talk titled “Navigating across from the the Solar System” by Mr. Andrew K. Johnston from the National Smithsonian Air and Space Museum. Mr. Johnston is the co-author of the “Smithsonian Atlas of Space Exploration” and his talk will give National Air & us a look at the history and technology of solar system explora- tion. -
Search for Rings and Satellites Around the Exoplanet Corot-9B Using Spitzer Photometry A
Search for rings and satellites around the exoplanet CoRoT-9b using Spitzer photometry A. Lecavelier Etangs, G. Hebrard, S. Blandin, J. Cassier, H. J. Deeg, A. S. Bonomo, F. Bouchy, J. -m. Desert, D. Ehrenreich, M. Deleuil, et al. To cite this version: A. Lecavelier Etangs, G. Hebrard, S. Blandin, J. Cassier, H. J. Deeg, et al.. Search for rings and satellites around the exoplanet CoRoT-9b using Spitzer photometry. Astronomy and Astrophysics - A&A, EDP Sciences, 2017, 603, pp.A115. 10.1051/0004-6361/201730554. hal-01678524 HAL Id: hal-01678524 https://hal.archives-ouvertes.fr/hal-01678524 Submitted on 16 Jan 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. A&A 603, A115 (2017) Astronomy DOI: 10.1051/0004-6361/201730554 & c ESO 2017 Astrophysics Search for rings and satellites around the exoplanet CoRoT-9b using Spitzer photometry A. Lecavelier des Etangs1, G. Hébrard1; 2, S. Blandin1, J. Cassier1, H. J. Deeg3; 4, A. S. Bonomo5, F. Bouchy6, J.-M. Désert7, D. Ehrenreich6, M. Deleuil8, R. F. Díaz9; 10, C. Moutou11, and A. Vidal-Madjar1 1 Institut d’astrophysique de Paris, CNRS, UMR 7095 & Sorbonne Universités, UPMC Paris 6, 98bis Bd Arago, 75014 Paris, France e-mail: [email protected] 2 Observatoire de Haute-Provence, CNRS/OAMP, 04870 Saint-Michel-l’Observatoire, France 3 Instituto de Astrofísica de Canarias, 38205 La Laguna, Tenerife, Spain 4 Universidad de La Laguna, Dept.