Chemical Composition of Venus Atmosphere and Clouds: Some Unsolved Problems
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The Geology of the Rocky Bodies Inside Enceladus, Europa, Titan, and Ganymede
49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083) 2905.pdf THE GEOLOGY OF THE ROCKY BODIES INSIDE ENCELADUS, EUROPA, TITAN, AND GANYMEDE. Paul K. Byrne1, Paul V. Regensburger1, Christian Klimczak2, DelWayne R. Bohnenstiehl1, Steven A. Hauck, II3, Andrew J. Dombard4, and Douglas J. Hemingway5, 1Planetary Research Group, Department of Marine, Earth, and Atmospheric Sciences, North Carolina State University, Raleigh, NC 27695, USA ([email protected]), 2Department of Geology, University of Georgia, Athens, GA 30602, USA, 3Department of Earth, Environmental, and Planetary Sciences, Case Western Reserve University, Cleveland, OH 44106, USA, 4Department of Earth and Environmental Sciences, University of Illinois at Chicago, Chicago, IL 60607, USA, 5Department of Earth & Planetary Science, University of California Berkeley, Berkeley, CA 94720, USA. Introduction: The icy satellites of Jupiter and horizontal stresses, respectively, Pp is pore fluid Saturn have been the subjects of substantial geological pressure (found from (3)), and μ is the coefficient of study. Much of this work has focused on their outer friction [12]. Finally, because equations (4) and (5) shells [e.g., 1–3], because that is the part most readily assess failure in the brittle domain, we also considered amenable to analysis. Yet many of these satellites ductile deformation with the relation n –E/RT feature known or suspected subsurface oceans [e.g., 4– ε̇ = C1σ exp , (6) 6], likely situated atop rocky interiors [e.g., 7], and where ε̇ is strain rate, C1 is a constant, σ is deviatoric several are of considerable astrobiological significance. stress, n is the stress exponent, E is activation energy, R For example, chemical reactions at the rock–water is the universal gas constant, and T is temperature [13]. -
Astronomy 330 HW 2 Presentations Outline
Astronomy 330 HW 2 •! Stanley Swat This class (Lecture 12): http://www.ufohowto.com/ Life in the Solar System •! Lucas Guthrie Next Class: http://www.crystalinks.com/abduction.html Life in the Solar System HW 5 is due Wednesday Music: We Are All Made of Stars– Moby Presentations Outline •! Daniel Borup •! Life on Venus? Futurama •! Life on Mars? Life in the Solar System? Earth – Venus comparison •! We want to examine in more detail the backyard of humans. •! What we find may change our estimates of ne. Radius 0.95 Earth Surface gravity 0.91 Earth Venus is the hottest Mass 0.81 Earth planet, the closest in Distance from Sun 0.72 AU size to Earth, the closest Average Temp 475 C in distance to Earth, and Year 224.7 Earth days the planet with the Length of Day 116.8 Earth days longest day. Atmosphere 96% CO2 What We Used to Think Turns Out that Venus is Hell Venus must be hotter, as it is closer the Sun, but the cloud •! The surface is hot enough to melt lead cover must reflect back a large amount of the heat. •! There is a runaway greenhouse effect •! There is almost no water In 1918, a Swedish chemist and Nobel laureate concluded: •! There is sulfuric acid rain •! Everything on Venus is dripping wet. •! Most of the surface is no doubt covered with swamps. •! Not a place to visit for Spring Break. •! The constantly uniform climatic conditions result in an entire absence of adaptation to changing exterior conditions. •! Only low forms of life are therefore represented, mostly no doubt, belonging to the vegetable kingdom; and the organisms are nearly of the same kind all over the planet. -
Exomoon Habitability Constrained by Illumination and Tidal Heating
submitted to Astrobiology: April 6, 2012 accepted by Astrobiology: September 8, 2012 published in Astrobiology: January 24, 2013 this updated draft: October 30, 2013 doi:10.1089/ast.2012.0859 Exomoon habitability constrained by illumination and tidal heating René HellerI , Rory BarnesII,III I Leibniz-Institute for Astrophysics Potsdam (AIP), An der Sternwarte 16, 14482 Potsdam, Germany, [email protected] II Astronomy Department, University of Washington, Box 951580, Seattle, WA 98195, [email protected] III NASA Astrobiology Institute – Virtual Planetary Laboratory Lead Team, USA Abstract The detection of moons orbiting extrasolar planets (“exomoons”) has now become feasible. Once they are discovered in the circumstellar habitable zone, questions about their habitability will emerge. Exomoons are likely to be tidally locked to their planet and hence experience days much shorter than their orbital period around the star and have seasons, all of which works in favor of habitability. These satellites can receive more illumination per area than their host planets, as the planet reflects stellar light and emits thermal photons. On the contrary, eclipses can significantly alter local climates on exomoons by reducing stellar illumination. In addition to radiative heating, tidal heating can be very large on exomoons, possibly even large enough for sterilization. We identify combinations of physical and orbital parameters for which radiative and tidal heating are strong enough to trigger a runaway greenhouse. By analogy with the circumstellar habitable zone, these constraints define a circumplanetary “habitable edge”. We apply our model to hypothetical moons around the recently discovered exoplanet Kepler-22b and the giant planet candidate KOI211.01 and describe, for the first time, the orbits of habitable exomoons. -
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. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
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. -
Projection of Meteosat Images Into World Geodetic System WGS-84 Matching Spot/Vegetation Grid
Projection of Meteosat images into World Geodetic system WGS-84 matching Spot/Vegetation grid Bruno COMBAL, Josué NOEL EUR 23945 EN - 2009 The mission of the JRC-IES is to provide scientific-technical support to the European Union’s policies for the protection and sustainable development of the European and global environ- ment. European Commission Joint Research Centre Institute for Environment and Sustainability Contact information Address: Global Environment Monitoring Unit, Institute for Environment and Sustainability, Joint Research Centre, via E. Fermi, 2749, I-21027 Ispra (VA), Italy E-mail: [email protected] Tel.: +39 03 32 78 93 78 Fax: +39 03 32 78 90 73 http://ies.jrc.ec.europa.eu/ http://www.jrc.ec.europa.eu/ Legal Notice Neither the European Commission nor any person acting on behalf of the Commission is re- sponsible for the use which might be made of this publication. Europe Direct is a service to help you find answers to your questions about the European Union Freephone number (*): 00 800 6 7 8 9 10 11 (*) Certain mobile telephone operators do not allow access to 00 800 numbers or these calls may be billed. A great deal of additional information on the European Union is available on the Internet. It can be accessed through the Europa server http://europa.eu/ JRC 52438 EUR 23945 EN ISBN 978-92-79-12953-7 ISSN 1018-5593 DOI 10.2788/2452 Luxembourg: Office for Official Publications of the European Communities © European Communities, 2009 Reproduction is authorised provided the source is acknowledged Printed in Italy Table of contents 1 Introduction......................................................................................... -
Outer Planets Flagship Mission Studies
OuterOuterOuter PlanetsPlanetsPlanets FlagshipFlagshipFlagship MissionMissionMission StudiesStudiesStudies Curt Niebur OPF Program Scientist NASA Headquarters Planetary Science Subcommittee June 23, 2008 Overview ¾ NASA is currently mid way through a six month long Phase II study of the remaining two candidate Outer Planet Flagship Missions ¾Europa Jupiter System Mission (EJSM) ¾Titan Saturn System Mission (TSSM) ¾ NASA plans to select a single Outer Planet Flagship mission to be pursued jointly with ESA and other international partners. ¾ The study plan includes a NASA only option in addition to the collaborative options. According to Phase II study ground rules the funding cap is $2.1B FY07 2 Outer Planet Flagship Mission Study Process Submitted 8/07 Downselected 12/07 Titan Saturn System Mission Downselect 11/08 Review 8-11/07 Started 2/08 Titan Saturn System Mission TMC and Phase II or Science Europa Study Europa Jupiter Panel Jupiter System Mission System Mission 3 NASA Phase II Study – Key Milestones • Joint SDT members selected…………………………………….Feb 1, 2008 • Study Kickoff……………………………………………………..Feb 9, 2008 • First Interim Review…………………………………………….April 9, 2008 • ESA Concurrent Design Facility Studies –kickoff…………….May 21, 2008 • Science Instrument Workshop………………………………….June 3-5, 2008 • Second Interim Review………………………………………….June 19-20, 2008 • ESA Concurrence Design Facility Studies – Outbrief…………July 27, 2008 • Phase II Initial Report…………………………………………..Aug 4, 2008 • Science and TMC Panels reviews ……………………………...Sep 9-11, 2008 – Europa Jupiter -
Technologies for Future Venus Exploration
September 9, 2009 WHITE PAPER TO THE NRC DECADAL SURVEY INNER PLANETS SUB–PANEL ON TECHNOLOGIES FOR FUTURE VENUS EXPLORATION by Tibor Balint1 & James Cutts1 (818) 354-1105 & (818) 354-4120 [email protected] & [email protected] and Mark Bullock2, James Garvin3, Stephen Gorevan4, Jeffery Hall1, Peter Hughes3, Gary Hunter4, Satish Khanna1, Elizabeth Kolawa1, Viktor Kerzhanovich1, Ethiraj Venkatapathy5 1Jet Propulsion Laboratory, California Institute of Technology; 2Southwest Research Institute; 3NASA–Goddard Space Flight Center; 3Honeybee Robotics; 4NASA–Glenn Research Center; 5NASA–Ames Research Center ABSTRACT The purpose of this white paper is to provide an overview to the NRC Decadal Survey Inner Planets Sub–Panel on key technologies required for future Venus exploration missions. It covers both heritage technologies and identifies new technologies to enable future missions in all three mission classes. The technologies will focus on mission enabling and enhancing capabilities for in situ missions, because most orbiter related sub–systems are considered heritage technologies. This white paper draws heavily on the recently completed Venus Flagship Mission study that identified key technologies required to implement its Design Reference Mission and other important mission options. The highest priority technologies and capabilities for the Venus Flagship Design Reference mission consist of: surface sample acquisition and handling; mechanical implementation of a rotating pressure vessel; a rugged–terrain landing system; and a large scale environmental test chamber to test these technologies under relevant Venus–like conditions. Other longer–term Venus Flagship Mission options will require additional new capabilities, namely a Venus–specific Radioisotope Power System; active refrigeration, high temperature electronics and advanced thermal insulation. -
Chemistry of Small Components of Upper Shells of Venus
Lunar and Planetary Science XXIX 1003.pdf CHEMISTRY OF SMALL COMPONENTS OF UPPER SHELLS OF VENUS. B.M. Andreichikov, Space Research Institute, Russian Academy of Sciences, 117810, Profsojuznaja st. 84/32,Moscow, Russia. Received by means of the VEGA 1, VEGA 2, a water mass (~ 4,5 ´ 1022 g, in the manner of GALILEO spacecrafts, information on Venus [1– hydro-xylgroups). 9] has vastly increased our knowledge about this (5) The possibility of presence in atmosphere of planet, but has introduced new questions connected planet of oxidizes of phosphorus is shown. (6) It with the chemistry of the atmosphere, the surface, had been revealed that they form of the atmos- and interaction processes. Additionally last publi- pheric components mixing ratio vertical profiles cations of the data of the optical spectroscopy [9– participating actively in reactions of the oxidation- 13] have revealed else greater divergence of them reduction. (7) The possibility of formation at a rate with results of the gas chromatography [14–17], of of 11–12 km of traces of aerosol of the layered the mass- spectrometers [18] and of the others of polymers (P2O5)n is shown. (8) It was revealed, that the contact measurements methods [6]. It had been seeming discord of results of direct measurements reported in works [7,8] about finding in the Ve- in the atmosphere of Venus is connected with the nusian night clouds of aerosol which contain a difference of chemical processes daytime and in the phosphor. The nephelometeric measurements [19] night, stipulated by the influence (of deeper at a have shown also that lower, the most dense clouds day time) of photochemical reactions products in layer an (47,5–50,5 km) is formed in the night and the upper troposphere. -
The High Priority and Relevance of Europa Exploration Galileo Galilei's
The High Priority and Relevance of Europa Exploration Galileo Galilei's discovery of moons of to that of Mars exploration6. In 2003, the Jupiter in 1610 advanced the Copernican decadal Solar System Exploration Survey7 of Revolution. Now nearly 400 years later, one the NRC called for a Europa orbiting space- of these moons–Europa–has the potential for craft as the single highest priority large "flag- discoveries just as profound. Europa's icy sur- ship class" exploration mission for the decade face is believed to hide a global subsurface 2003-2013. Such a spacecraft mission would ocean with volume nearly three times that of confirm the existence of Europa's subsurface Earth's oceans1. The moon's surface is young, ocean, characterize in detail the moon's sur- with a nominal age of 50 million years, imply- face and icy shell, and conduct reconnaissance ing that it is most likely geologically active vital for future landed exploration. 2 today . The primitive materials that nourish Much of NASA's current planetary explo- life have rained onto Europa throughout solar ration focus, and that planned for the future in system history, are created by radiation chem- NASA's exploration vision8, is placed on the istry at its surface, and may pour from vents at 3 astrobiological potential of Mars, which likely the ocean's deep bottom . On Earth, microbial once had liquid water on its surface and may extremophiles take advantage of environ- have water underground today. Given that Eu- mental niches arguably as harsh as within Eu- 4 ropa appears to currently possess the three ropa's subsurface ocean . -
On the Detection of Exomoons in Photometric Time Series
On the Detection of Exomoons in Photometric Time Series Dissertation zur Erlangung des mathematisch-naturwissenschaftlichen Doktorgrades “Doctor rerum naturalium” der Georg-August-Universität Göttingen im Promotionsprogramm PROPHYS der Georg-August University School of Science (GAUSS) vorgelegt von Kai Oliver Rodenbeck aus Göttingen, Deutschland Göttingen, 2019 Betreuungsausschuss Prof. Dr. Laurent Gizon Max-Planck-Institut für Sonnensystemforschung, Göttingen, Deutschland und Institut für Astrophysik, Georg-August-Universität, Göttingen, Deutschland Prof. Dr. Stefan Dreizler Institut für Astrophysik, Georg-August-Universität, Göttingen, Deutschland Dr. Warrick H. Ball School of Physics and Astronomy, University of Birmingham, UK vormals Institut für Astrophysik, Georg-August-Universität, Göttingen, Deutschland Mitglieder der Prüfungskommision Referent: Prof. Dr. Laurent Gizon Max-Planck-Institut für Sonnensystemforschung, Göttingen, Deutschland und Institut für Astrophysik, Georg-August-Universität, Göttingen, Deutschland Korreferent: Prof. Dr. Stefan Dreizler Institut für Astrophysik, Georg-August-Universität, Göttingen, Deutschland Weitere Mitglieder der Prüfungskommission: Prof. Dr. Ulrich Christensen Max-Planck-Institut für Sonnensystemforschung, Göttingen, Deutschland Dr.ir. Saskia Hekker Max-Planck-Institut für Sonnensystemforschung, Göttingen, Deutschland Dr. René Heller Max-Planck-Institut für Sonnensystemforschung, Göttingen, Deutschland Prof. Dr. Wolfram Kollatschny Institut für Astrophysik, Georg-August-Universität, Göttingen,