Persephone: a Pluto-System Orbiter & Kuiper Belt Explorer
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Tectonics of Charon Ross A. Beyer1,2, Francis Nimmo3, William B. Mckinnon4, Jeffrey Moore2, Paul Schenk5, Kelsi Singer6, John R
47th Lunar and Planetary Science Conference (2016) 2714.pdf Tectonics of Charon Ross A. Beyer1;2, Francis Nimmo3, William B. McKinnon4, Jeffrey Moore2, Paul Schenk5, Kelsi Singer6, John R. Spencer6, Hal Weaver7, Leslie Young6, Kimberly Ennico2, Cathy Olkin6, Alan Stern6, and the New Horizons Science Team. 1Carl Sagan Center at the SETI Institute, 2NASA Ames Research Center, Moffett Field, CA, USA ([email protected]), 3UCSC, 4WUStL, 5LPI, 6SwRI, 7JHU APL Charon, Pluto’s large companion, has a variety of (0.288 m s−2). Charon’s tectonic terrain is exception- terrains that exhibit tectonic features. The Pluto-facing ally rugged and and contains a network of fault-bounded hemisphere that New Horizons [1] observed at high res- troughs and scarps in the equatorial to middle latitudes. olution has two broad provinces: the relatively smooth This transitions northward and over the pole to the visi- plains of the informally named (as are all names in this ble limb into an irregular zone where the fault traces are abstract) Vulcan Planum to the south of the encounter neither so parallel nor so obvious, but which contains ir- hemisphere, and the zone north of Vulcan Planum. This regular depressions (one as deep as 10 km just outside of area is characterized by ridges, graben, and scarps, which Mordor Macula) and other large relief variations. are signs of extensional tectonism. The border between Chasmata: There are a number of chasmata that gen- these two provinces strikes diagonally across the en- erally parallel the strike of the northern margin of Vulcan counter hemisphere from as far south as −19◦ latitude ◦ Planum, and we will discuss the largest two here as they in the west to 25 in the east (Figure1). -
The Wsfa Journal Tb , ;,;T He W S F a J 0 U R N a L
THE WSFA JOURNAL TB , ;,;T HE W S F A J 0 U R N A L (The Official Organ of the Washington S. F. Association) Issue Number 76: April-May '71 1971 DISCLAVE SPECIAL n X Copyright \,c) 1971 by Donald-L. Miller. All rights reserved for contributors. The JOURNAL Staff Managing Editor & Publisher — Don Miller, 12315 Judson Rd., Wheaton, MD, USA, 20 906. Associate Editors — Art Editor: Alexis Gilliland, 2126 Penna. Ave., N.W., Washington, DC, 20037. Fiction Editors: Doll St Alexis Gilliland (address above). SOTWJ Editor: OPEN (Acting Editor: Don Miller). Overseas Agents — Australia: Michael O'Brien, 15>8 Liverpool St., Hobart, Tasmania, Australia, 7000 Benelux: Michel Feron, Grand-Place 7, B—I4.28O HANNUT, Belgium. Japan:. Takumi Shibano, I-II4-IO, 0-0kayama, Meguro-ku, Tokyo, Japan. Scandinavia: Per Insulander, Midsommarv.. 33> 126 35 HMgersten, Sweden. South Africa: A.B. Ackerman, POBox 25U5> Pretoria, Transvaal, Rep. of So.Africa. United Kingdom: Peter Singleton, 60W4, Broadmoor Hospital, Block I4, Crowthorne, Berks. RG11 7EG, England. Still needed for France, Germany, Italy, South Timerica, and Soain. Contributing Editors — Bibliographer: Mark Owings. Film Reviewer: Richard Delap. Book Reviewers: Al Gechter, Alexis Music Columnist: Harry Warner, Jr. Gilliland, Dave Halterman, James News Reporters: ALL OPEN (Club, Con R. Newton, Fred Patten, Ted Pauls, vention, Fan, Pro, Publishing). Mike Shoemaker. (More welcome.) Pollster: Mike Shoemaker. Book Review Indexer: Hal Hall. Prozine Reviewers: Richard Delap, Comics Reviewer: Kim Weston. Mike Shoemaker (serials only). Fanzine Reviewers: Doll Gilliland, Pulps: Bob Jones. Mike Shoemaker. Special mention to Jay Kay Klein and Feature Writer: Alexis Gilliland. -
Chemical Composition of Pluto's Aerosols Analogues
EPSC Abstracts Vol. 13, EPSC-DPS2019-941-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Chemical composition of Pluto’s aerosols analogues Lora Jovanovic (1), Thomas Gautier (1), Nathalie Carrasco (1), Véronique Vuitton (2), Cédric Wolters (2), François-Régis Orthous-Daunay (2), Ludovic Vettier (1), Laurène Flandinet (2) ([email protected]) (1) Laboratoire Atmosphères, Milieux, Observations Spatiales (LATMOS), Guyancourt, France (2) Institut de Planétologie et d’Astrophysique de Grenoble (IPAG), Grenoble, France Abstract Table 1: Types of Pluto’s aerosols analogues produced with the PAMPRE experiment. The discovery of haze in Pluto’s atmosphere on July 14th, 2015, has raised lots of questions. To help Corresponding understand the data provided by the New Horizons Composition of the gas mixture altitude on spacecraft, Pluto’s aerosols analogues were Pluto [2] synthetized and their chemical composition was 99% N2 : 1% CH4 : 500 ppm CO 400 km determined by high-resolution mass spectrometry 95% N2 : 5% CH4 : 500 ppm CO 600 km (Orbitrap technique). 2.2. High-resolution mass spectrometry 1. Introduction (HRMS) study On July 14th, 2015, when Pluto was flown by the New Horizons spacecraft, aerosols were detected in its We analyzed the soluble fraction of Pluto’s aerosols atmosphere, mainly composed of molecular nitrogen analogues, dissolved in a 50:50 (v/v)% methanol:acetonitrile mixture. The analytical N2, methane CH4, with around 500 ppm of carbon monoxide CO [1,2,3]. These aerosols aggregate into instrument used was the LTQ Orbitrap XL several thin haze layers that extend at more than (ThermoFisher Scientific). -
A Deep Search for Additional Satellites Around the Dwarf Planet
Search for Additional Satellites around Haumea A Preprint typeset using LTEX style emulateapj v. 01/23/15 A DEEP SEARCH FOR ADDITIONAL SATELLITES AROUND THE DWARF PLANET HAUMEA Luke D. Burkhart1,2, Darin Ragozzine1,3,4, Michael E. Brown5 Search for Additional Satellites around Haumea ABSTRACT Haumea is a dwarf planet with two known satellites, an unusually high spin rate, and a large collisional family, making it one of the most interesting objects in the outer solar system. A fully self-consistent formation scenario responsible for the satellite and family formation is still elusive, but some processes predict the initial formation of many small moons, similar to the small moons recently discovered around Pluto. Deep searches for regular satellites around KBOs are difficult due to observational limitations, but Haumea is one of the few for which sufficient data exist. We analyze Hubble Space Telescope (HST) observations, focusing on a ten-consecutive-orbit sequence obtained in July 2010, to search for new very small satellites. To maximize the search depth, we implement and validate a non-linear shift-and-stack method. No additional satellites of Haumea are found, but by implanting and recovering artificial sources, we characterize our sensitivity. At distances between 10,000 km and 350,000 km from Haumea, satellites with radii as small as 10 km are ruled out, assuming∼ an albedo∼ (p 0.7) similar to Haumea. We also rule out satellites larger∼ than &40 km in most of the Hill sphere using≃ other HST data. This search method rules out objects similar in size to the small moons of Pluto. -
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. -
CHORUS: Let's Go Meet the Dwarf Planets There Are Five in Our Solar
Meet the Dwarf Planet Lyrics: CHORUS: Let’s go meet the dwarf planets There are five in our solar system Let’s go meet the dwarf planets Now I’ll go ahead and list them I’ll name them again in case you missed one There’s Pluto, Ceres, Eris, Makemake and Haumea They haven’t broken free from all the space debris There’s Pluto, Ceres, Eris, Makemake and Haumea They’re smaller than Earth’s moon and they like to roam free I’m the famous Pluto – as many of you know My orbit’s on a different path in the shape of an oval I used to be planet number 9, But I break the rules; I’m one of a kind I take my time orbiting the sun It’s a long, long trip, but I’m having fun! Five moons keep me company On our epic journey Charon’s the biggest, and then there’s Nix Kerberos, Hydra and the last one’s Styx 248 years we travel out Beyond the other planet’s regular rout We hang out in the Kuiper Belt Where the ice debris will never melt CHORUS My name is Ceres, and I’m closest to the sun They found me in the Asteroid Belt in 1801 I’m the only known dwarf planet between Jupiter and Mars They thought I was an asteroid, but I’m too round and large! I’m Eris the biggest dwarf planet, and the slowest one… It takes me 557 years to travel around the sun I have one moon, Dysnomia, to orbit along with me We go way out past the Kuiper Belt, there’s so much more to see! CHORUS My name is Makemake, and everyone thought I was alone But my tiny moon, MK2, has been with me all along It takes 310 years for us to orbit ‘round the sun But out here in the Kuiper Belt… our adventures just begun Hello my name’s Haumea, I’m not round shaped like my friends I rotate fast, every 4 hours, which stretched out both my ends! Namaka and Hi’iaka are my moons, I have just 2 And we live way out past Neptune in the Kuiper Belt it’s true! CHORUS Now you’ve met the dwarf planets, there are 5 of them it’s true But the Solar System is a great big place, with more exploring left to do Keep watching the skies above us with a telescope you look through Because the next person to discover one… could be me or you… . -
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 -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
Mass of the Kuiper Belt · 9Th Planet PACS 95.10.Ce · 96.12.De · 96.12.Fe · 96.20.-N · 96.30.-T
Celestial Mechanics and Dynamical Astronomy manuscript No. (will be inserted by the editor) Mass of the Kuiper Belt E. V. Pitjeva · N. P. Pitjev Received: 13 December 2017 / Accepted: 24 August 2018 The final publication ia available at Springer via http://doi.org/10.1007/s10569-018-9853-5 Abstract The Kuiper belt includes tens of thousands of large bodies and millions of smaller objects. The main part of the belt objects is located in the annular zone between 39.4 au and 47.8 au from the Sun, the boundaries correspond to the average distances for orbital resonances 3:2 and 2:1 with the motion of Neptune. One-dimensional, two-dimensional, and discrete rings to model the total gravitational attraction of numerous belt objects are consid- ered. The discrete rotating model most correctly reflects the real interaction of bodies in the Solar system. The masses of the model rings were determined within EPM2017—the new version of ephemerides of planets and the Moon at IAA RAS—by fitting spacecraft ranging observations. The total mass of the Kuiper belt was calculated as the sum of the masses of the 31 largest trans-neptunian objects directly included in the simultaneous integration and the estimated mass of the model of the discrete ring of TNO. The total mass −2 is (1.97 ± 0.30) · 10 m⊕. The gravitational influence of the Kuiper belt on Jupiter, Saturn, Uranus and Neptune exceeds at times the attraction of the hypothetical 9th planet with a mass of ∼ 10 m⊕ at the distances assumed for it. -
Solar Orbiter Assessment Study and Model Payload
Solar Orbiter assessment study and model payload N.Rando(1), L.Gerlach(2), G.Janin(4), B.Johlander(1), A.Jeanes(1), A.Lyngvi(1), R.Marsden(3), A.Owens(1), U.Telljohann(1), D.Lumb(1) and T.Peacock(1). (1) Science Payload & Advanced Concepts Office, (2) Electrical Engineering Department, (3) Research and Scientific Support Department, European Space Agency, ESTEC, Postbus 299, NL-2200AG, Noordwijk, The Netherlands (4) Mission Analysis Office, European Space Agency, ESOC, Darmstadt, Germany ABSTRACT The Solar Orbiter mission is presently in assessment phase by the Science Payload and Advanced Concepts Office of the European Space Agency. The mission is confirmed in the Cosmic Vision programme, with the objective of a launch in October 2013 and no later than May 2015. The Solar Orbiter mission incorporates both a near-Sun (~0.22 AU) and a high-latitude (~ 35 deg) phase, posing new challenges in terms of protection from the intense solar radiation and related spacecraft thermal control, to remain compatible with the programmatic constraints of a medium class mission. This paper provides an overview of the assessment study activities, with specific emphasis on the definition of the model payload and its accommodation in the spacecraft. The main results of the industrial activities conducted with Alcatel Space and EADS-Astrium are summarized. Keywords: Solar physics, space weather, instrumentation, mission assessment, Solar Orbiter 1. INTRODUCTION The Solar Orbiter mission was first discussed at the Tenerife “Crossroads” workshop in 1998, in the framework of the ESA Solar Physics Planning Group. The mission was submitted to ESA in 2000 and then selected by ESA’s Science Programme Committee in October 2000 to be implemented as a flexi-mission, with a launch envisaged in the 2008- 2013 timeframe (after the BepiColombo mission to Mercury) [1]. -
Elevation-Dependant CH4 Condensation on Pluto: What Are the Origins of the Observed CH4 Snow-Capped Mountains?
EPSC Abstracts Vol. 13, EPSC-DPS2019-375-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Elevation-dependant CH4 condensation on Pluto: what are the origins of the observed CH4 snow-capped mountains? Tanguy Bertrand (1) and François Forget (2) (1) NASA Ames Research Center, Moffett Field, CA 94035, USA (2) Laboratoire de Météorologie Dynamique, IPSL, Sorbonne Universités, UPMC Univ Paris 06, CNRS, 4 place Jussieu, 75005 Paris, ([email protected]). Abstract Pluto is covered by numerous deposits of methane ice (CH4), with a rich diversity of textures and colors. However, within the dark tholins-covered equatorial regions, CH4 ice mostly shows up on high-elevated terrains. What could trigger CH4 condensation at high altitude? Here we present high-resolution numerical simulations of Pluto's climate performed with a Global Climate Model (GCM) designed to Figure 1: (A) the ~100-km long CH4 snow-capped simulate the present-day CH4 cycle. ridges of Enrique Montes within Cthulhu Macula (147.0°E, 7.0°S), seen in an enhanced Ralph/MVIC 1. Introduction color image (680 m/pixel). The location of the bright ice on the mountain peaks correlates with the The exploration of Pluto by the New Horizons distribution of CH4 ice, as shown by (B) the MVIC spacecraft in July 2015 revealed a surface covered by CH4 spectral index map of the same scene, with numerous deposits of methane-rich ice (CH4), with a purple indicating CH4 absorption. (C) Terrestrial rich diversity of textures and colors [1-2]. At high water-ice capped mountain chains. -
A Free Spacecraft Simulation Tool
Orbiter: AFreeSpacecraftSimulationTool MartinSchweiger DepartmentofComputerScience UniversityCollegeLondon www.orbitersim.com 2nd ESAWorkshoponAstrodynamics ToolsandTechniques ESTEC,Noordwijk 13-15September2004 Contents • Overview • Scope • Limitations • SomeOrbiterfeatures: • Timepropagation • Gravitycalculation • Rigid-bodymodelandsuperstructures • OrbiterApplicationProgrammingInterface: • Concept • Orbiterinstrumentation • TheVESSELinterfaceclass • Newfeatures: • Air-breatingengines:scramjetdesign • Virtualcockpits • Newvisualeffects • Orbiterasateachingtool • Summaryandfutureplans • Demonstration Overview · Orbiterisareal-timespaceflightsimulationforWindowsPC platforms. · Modellingofatmosphericflight(launchandreentry), suborbital,orbitalandinterplanetarymissions(rendezvous, docking,transfer,swing-byetc.) · Newtonianmechanics,rigidbodymodelofrotation,basic atmosphericflightmodel. · Planetpositionsfrompublicperturbationsolutions.Time integrationofstatevectorsorosculatingelements. · Developedsince2000asaneducationalandrecreational applicationfororbitalmechanicssimulation. · WritteninC++,usingDirectXfor3-Drendering.Public programminginterfacefordevelopmentofexternalmodule plugins. · WithanincreasinglyversatileAPI,developmentfocusis beginningtoshiftfromtheOrbitercoreto3rd partyaddons. Scope · Launchsequencefromsurfacetoorbitalinsertion(including atmosphericeffects:drag,pressure-dependentengineISP...) · Orbitalmanoeuvres(alignmentoforbitalplane,orbit-to-orbit transfers,rendezvous) · Vessel-to-vesselapproachanddocking.Buildingof superstructuresfromvesselmodules(includingsimplerules