5 Escape of Atmospheres to Space
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Modeling the Formation of the Earth's Atmosphere by Hydrodynamic
Origin of the Earth and Moon Conference 4102.pdf MODELING THE FORMATION OF THE EARTH’S ATMOSPHERE BY HYDRODYNAMIC ESCAPE AND PLANETARY OUTGASSING. R. O. Pepin, School of Physics and Astronomy, University of Minnesota, Minneapolis MN 55455, USA. Accretion of lunar- to Mars-sized terrestrial Models of this kind have had some success in planet embryos is believed to have occurred on accounting for the details of terrestrial noble gas timescales of »105 years in the presence of nebular mass distributions [3,6]. However, they are not with- gas [1,2]. Mechanisms for trapping nebular (“solar”) out problems. “Solar” isotopic distributions in the noble gases in these embryos include occlusion of initial terrestrial reservoirs are taken to be those ambient gases in the planetesimals accreted to form measured in the solar wind. Although current esti- them, and, probably more important, efficient ad- mates for the isotopic compositions of solar-wind Ne, sorption of gravitationally condensed nebular gases Ar, and Kr are compatible with those required in the on embryo surfaces once they had grown to modeling for Earth’s primordial noble gas invento- ~Mercury size [3]. During the following ~100–200 ries, this assumption that the wind correctly repre- m.y. of growth through the “giant-impact” stage sents the composition of the nebular source supply- [1,4] to a fully assembled planet, a coaccreting pri- ing these gases to the early Earth is not strictly valid mordial atmosphere is likely to develop by impact- for Xe. Generating the isotope ratios of terrestrial degassing of colliding embryos and inward-scattered nonradiogenic Xe by fractionation in hydrodynamic icy planetesimals, and by gravitational capture of escape requires an initial composition called U-Xe, nebular gases if the gas phase of the nebula had not which appears to be isotopically identical to meas- yet fully dissipated. -
Martian Crater Morphology
ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter. -
Water on Venus: Implications of Theearly Hydrodynamic Escape
EPSC Abstracts Vol. 5, EPSC2010-288, 2010 European Planetary Science Congress 2010 c Author(s) 2010 Water on Venus: Implications of theEarly Hydrodynamic Escape C. Gillmann (1), E. Chassefière (2) and P. Lognonné (1) (1) Institut de Physique du Globe (IPGP), Paris, France, ([email protected]) (2) CNRS/UPS UMR 8148 IDES Interactions et Dynamique des Environnements de Surface, Paris, France Abstract toward a common origin for those three atmospheres and a usual theory is that these atmospheres are In order to study the evolution of the primitive secondary, created by the degassing of volatiles from atmosphere of Venus, we developed a time the bodies that constituted the early planet. The dependent model of hydrogen hydrodynamic escape atmosphere of Venus could then represent a primitive state of the evolution of terrestrial. Moreover, Mars powered by solar EUV (Extreme UV) flux and solar and the Earth possess reservoirs of water at present- wind, and accounting for oxygen frictional escape day whereas Venus seems to be dry. The early We study specifically the isotopic fractionation of evolution of terrestrial planets and the effects of noble gases resulting from hydrodynamic escape. hydrodynamic escape might explain this observation The fractionation’s primary cause is the effect of by the removal of most of the initial water on Venus. diffusive/gravitational separation between the homopause and the base of the escape. Heavy noble 2. Results and Scenario gases such as Kr and Xe are not fractionated. Ar is only marginally fractionated whereas Ne is We study the evolution of the primitive atmosphere moderately fractionated. of Venus and investigate the possibility of an early We also take into account oxygen dragged off habitable Venus with a possible liquid water ocean on along with hydrogen by hydrodynamic process. -
1 the Atmosphere of Pluto As Observed by New Horizons G
The Atmosphere of Pluto as Observed by New Horizons G. Randall Gladstone,1,2* S. Alan Stern,3 Kimberly Ennico,4 Catherine B. Olkin,3 Harold A. Weaver,5 Leslie A. Young,3 Michael E. Summers,6 Darrell F. Strobel,7 David P. Hinson,8 Joshua A. Kammer,3 Alex H. Parker,3 Andrew J. Steffl,3 Ivan R. Linscott,9 Joel Wm. Parker,3 Andrew F. Cheng,5 David C. Slater,1† Maarten H. Versteeg,1 Thomas K. Greathouse,1 Kurt D. Retherford,1,2 Henry Throop,7 Nathaniel J. Cunningham,10 William W. Woods,9 Kelsi N. Singer,3 Constantine C. C. Tsang,3 Rebecca Schindhelm,3 Carey M. Lisse,5 Michael L. Wong,11 Yuk L. Yung,11 Xun Zhu,5 Werner Curdt,12 Panayotis Lavvas,13 Eliot F. Young,3 G. Leonard Tyler,9 and the New Horizons Science Team 1Southwest Research Institute, San Antonio, TX 78238, USA 2University of Texas at San Antonio, San Antonio, TX 78249, USA 3Southwest Research Institute, Boulder, CO 80302, USA 4National Aeronautics and Space Administration, Ames Research Center, Space Science Division, Moffett Field, CA 94035, USA 5The Johns Hopkins University Applied Physics Laboratory, Laurel, MD 20723, USA 6George Mason University, Fairfax, VA 22030, USA 7The Johns Hopkins University, Baltimore, MD 21218, USA 8Search for Extraterrestrial Intelligence Institute, Mountain View, CA 94043, USA 9Stanford University, Stanford, CA 94305, USA 10Nebraska Wesleyan University, Lincoln, NE 68504 11California Institute of Technology, Pasadena, CA 91125, USA 12Max-Planck-Institut für Sonnensystemforschung, 37191 Katlenburg-Lindau, Germany 13Groupe de Spectroscopie Moléculaire et Atmosphérique, Université Reims Champagne-Ardenne, 51687 Reims, France *To whom correspondence should be addressed. -
Diffusion-Limited Escape/ the Atmospheric Hydrogen Budget/ Hydrodynamic Escape
41st Saas-Fee Course From Planets to Life 3-9 April 2011 Lecture 6--Hydrogen escape, Part 2 Diffusion-limited escape/ The atmospheric hydrogen budget/ Hydrodynamic escape J. F. Kasting Diffusion-limited escape • On Earth, hydrogen escape is limited by diffusion through the homopause • Escape rate is given by (Walker, 1977*) esc(H) bi ftot/Ha where bi = binary diffusion parameter for H (or H2) in air Ha = atmospheric (pressure) scale height ftot = total hydrogen mixing ratio in the stratosphere *J.C.G. Walker, Evolution of the Atmosphere (1977) • Numerically 19 -1 -1 b i 1.810 cm s (avg. of H and H2 in air) 5 Ha = kT/mg 6.410 cm so 13 -2 -1 esc (H) 2.510 ftot (H) (molecules cm s ) Total hydrogen mixing ratio • In the stratosphere, hydrogen interconverts between various chemical forms • Rate of upward diffusion of hydrogen is determined by the total hydrogen mixing ratio ftot(H) = f(H) + 2 f(H2) + 2 f(H2O) + 4 f(CH4) + … • ftot(H) is nearly constant from the tropopause up to the homopause (i.e., 10-100 km) Total hydrogen mixing ratio Homopause Tropopause Diffusion-limited escape • Let’s put in some numbers. In the lower stratosphere −6 f(H2O) 3-5 ppmv = (3-5)10 −6 f(CH4 ) = 1.6 ppmv = 1.6 10 • Thus −6 −6 ftot (H) = 2 (310 ) + 4 (1.6 10 ) 1.210−5 so the diffusion-limited escape rate is 13 −5 8 -2 -1 esc (H) 2.510 (1.210 ) = 310 cm s Hydrogen budget on the early Earth • For the early earth, we can estimate the atmospheric H2 mixing ratio by balancing volcanic outgassing of H2 (and other reduced gases) with the diffusion-limited escape -
Arxiv:2003.06799V2 [Astro-Ph.EP] 6 Feb 2021
Thomas Ruedas1,2 Doris Breuer2 Electrical and seismological structure of the martian mantle and the detectability of impact-generated anomalies final version 18 September 2020 published: Icarus 358, 114176 (2021) 1Museum für Naturkunde Berlin, Germany 2Institute of Planetary Research, German Aerospace Center (DLR), Berlin, Germany arXiv:2003.06799v2 [astro-ph.EP] 6 Feb 2021 The version of record is available at http://dx.doi.org/10.1016/j.icarus.2020.114176. This author pre-print version is shared under the Creative Commons Attribution Non-Commercial No Derivatives License (CC BY-NC-ND 4.0). Electrical and seismological structure of the martian mantle and the detectability of impact-generated anomalies Thomas Ruedas∗ Museum für Naturkunde Berlin, Germany Institute of Planetary Research, German Aerospace Center (DLR), Berlin, Germany Doris Breuer Institute of Planetary Research, German Aerospace Center (DLR), Berlin, Germany Highlights • Geophysical subsurface impact signatures are detectable under favorable conditions. • A combination of several methods will be necessary for basin identification. • Electromagnetic methods are most promising for investigating water concentrations. • Signatures hold information about impact melt dynamics. Mars, interior; Impact processes Abstract We derive synthetic electrical conductivity, seismic velocity, and density distributions from the results of martian mantle convection models affected by basin-forming meteorite impacts. The electrical conductivity features an intermediate minimum in the strongly depleted topmost mantle, sandwiched between higher conductivities in the lower crust and a smooth increase toward almost constant high values at depths greater than 400 km. The bulk sound speed increases mostly smoothly throughout the mantle, with only one marked change at the appearance of β-olivine near 1100 km depth. -
THE CHANTICLEER Jacksonville State University Jacksonville
Jacksonville State University JSU Digital Commons Chanticleer Historical Newspapers 1985-01-11 Chanticleer | Vol 32, Issue 15 Jacksonville State University Follow this and additional works at: https://digitalcommons.jsu.edu/lib_ac_chanty Recommended Citation Jacksonville State University, "Chanticleer | Vol 32, Issue 15" (1985). Chanticleer. 871. https://digitalcommons.jsu.edu/lib_ac_chanty/871 This Book is brought to you for free and open access by the Historical Newspapers at JSU Digital Commons. It has been accepted for inclusion in Chanticleer by an authorized administrator of JSU Digital Commons. For more information, please contact [email protected]. C Entertainment THE CHANTICLEER Jacksonville State university Jacksonville. Alabama Vol. &No. W January 11, 1985 Mild controversy erupts over - senate resolution By JAN DICKINSON A resolution calling for a faculty-wide vote of "no confidence" in Resident Theron Montgomery was presented to the Faculty Senate at its December 10 meeting, two days before Montgomery anriounced his resignation to the Board of Trustees. Now the sponsor of the resolution, Dr. Gene Blanton, of the English Department, says that he intends to withdraw the resolution at the January 14 meeting of the senate. 13lanton stated in the January 6 edition of the Anniston Star that, because of comments made by several members of the Board of bstees, the wssibility of dropping the resolution was strong. According to that article, trustee Paul Carpenter said, "It (the vote) wouid make absolutely no difference in my opinion. We have studied the entire situation, and we are satisfied with the decision." Another board member, Dwaine Luce, stated, "....the bard is responsible for running the school, and the faculty is responsible for iristructing the students." Echoing the sentiments of Carpenter, he added, "'I'he board has inade its decision and the board, in my pinion, will stand by its decision." According to Dr. -
The Longevity of Water Ice on Ganymedes and Europas Around Migrated Giant Planets
The Astrophysical Journal, 839:32 (9pp), 2017 April 10 https://doi.org/10.3847/1538-4357/aa67ea © 2017. The American Astronomical Society. All rights reserved. The Longevity of Water Ice on Ganymedes and Europas around Migrated Giant Planets Owen R. Lehmer1, David C. Catling1, and Kevin J. Zahnle2 1 Dept. of Earth and Space Sciences/Astrobiology Program, University of Washington, Seattle, WA, USA; [email protected] 2 NASA Ames Research Center, Moffett Field, CA, USA Received 2017 February 17; revised 2017 March 14; accepted 2017 March 18; published 2017 April 11 Abstract The gas giant planets in the Solar System have a retinue of icy moons, and we expect giant exoplanets to have similar satellite systems. If a Jupiter-like planet were to migrate toward its parent star the icy moons orbiting it would evaporate, creating atmospheres and possible habitable surface oceans. Here, we examine how long the surface ice and possible oceans would last before being hydrodynamically lost to space. The hydrodynamic loss rate from the moons is determined, in large part, by the stellar flux available for absorption, which increases as the giant planet and icy moons migrate closer to the star. At some planet–star distance the stellar flux incident on the icy moons becomes so great that they enter a runaway greenhouse state. This runaway greenhouse state rapidly transfers all available surface water to the atmosphere as vapor, where it is easily lost from the small moons. However, for icy moons of Ganymede’s size around a Sun-like star we found that surface water (either ice or liquid) can persist indefinitely outside the runaway greenhouse orbital distance. -
Atmospheric Escape and the Evolution of Close-In Exoplanets
Atmospheric Escape and the Evolution of Close-in Exoplanets James E. Owen Astrophysics Group, Imperial College London, Blackett Laboratory, Prince Consort Road, London SW7 2AZ, UK; email: [email protected] Xxxx. Xxx. Xxx. Xxx. YYYY. AA:1{26 Keywords https://doi.org/10.1146/((please add atmospheric evolution, exoplanets, exoplanet composition article doi)) Copyright c YYYY by Annual Reviews. Abstract All rights reserved Exoplanets with substantial Hydrogen/Helium atmospheres have been discovered in abundance, many residing extremely close to their par- ent stars. The extreme irradiation levels these atmospheres experience causes them to undergo hydrodynamic atmospheric escape. Ongoing atmospheric escape has been observed to be occurring in a few nearby exoplanet systems through transit spectroscopy both for hot Jupiters and lower-mass super-Earths/mini-Neptunes. Detailed hydrodynamic calculations that incorporate radiative transfer and ionization chemistry are now common in one-dimensional models, and multi-dimensional calculations that incorporate magnetic-fields and interactions with the arXiv:1807.07609v3 [astro-ph.EP] 6 Jun 2019 interstellar environment are cutting edge. However, there remains very limited comparison between simulations and observations. While hot Jupiters experience atmospheric escape, the mass-loss rates are not high enough to affect their evolution. However, for lower mass planets at- mospheric escape drives and controls their evolution, sculpting the ex- oplanet population we observe today. 1 Contents 1. -
The Loss of Nitrogen-Rich Atmospheres from Earth-Like Exoplanets Within M-Star Habitable Zones
**FULL TITLE** ASP Conference Series, Vol. **VOLUME**, **YEAR OF PUBLICATION** **NAMES OF EDITORS** The loss of nitrogen-rich atmospheres from Earth-like exoplanets within M-star habitable zones H. Lammer Space Research Institute, Austrian Academy of Sciences, Schmiedlstr. 6, A-8042 Graz, Austria H. I. M. Lichtenegger Space Research Institute, Austrian Academy of Sciences, Schmiedlstr. 6, A-8042 Graz, Austria M. L. Khodachenko Space Research Institute, Austrian Academy of Sciences, Schmiedlstr. 6, A-8042 Graz, Austria Yu. N. Kulikov Polar Geophysical Institute (PGI), Russian Academy of Sciences, Khalturina Str. 15, Murmansk, 183010, Russian Federation J.-M. Grie¼meier ASTRON, Dwingeloo, The Netherlands Abstract. After the ¯rst discovery of massive Earth-like exoplanets around M-type dwarf stars, the search for exoplanets which resemble more an Earth analogue continues. The discoveries of super-Earth planets pose questions on habitability and the possible origin of life on such planets. Future exoplanet space projects designed to characterize the atmospheres of terrestrial exoplanets will also search for atmospheric species which are considered as bio-markers (e.g. O3,H2O, CH4, etc.). By using the Earth with its atmosphere as a proxy and in agreement with the classical habitable zone concept, one should expect that Earth-like exoplanets suitable for life as we know it should have a nitrogen atmo- sphere and a very low CO2 content. Whether a water bearing terrestrial planet within its habitable zone can evolve into a habitable world similar than the Earth, depends on the capability of its water-inventory and atmosphere to sur- vive the period of high radiation of the young and/or active host star. -
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T. Crofton Department of Aerospace & Ocean Engineering TEAM LEAD Allison Quinn STUDENT MEMBERS Ethan LeBoeuf Brian McLemore Peter Bradley Smith Amanda Swanson Michael Valosin III Vidya Vishwanathan FACULTY SUPERVISOR AIAA 2018 Undergraduate Spacecraft Design Dr. Kevin Shinpaugh Competition Submission i AIAA Member Numbers and Signatures Ethan LeBoeuf Brian McLemore Member Number: 918782 Member Number: 908372 Allison Quinn Peter Bradley Smith Member Number: 920552 Member Number: 530342 Amanda Swanson Michael Valosin III Member Number: 920793 Member Number: 908465 Vidya Vishwanathan Dr. Kevin Shinpaugh Member Number: 608701 Member Number: 25807 ii Table of Contents List of Figures ................................................................................................................................................................ v List of Tables ................................................................................................................................................................vi List of Symbols ........................................................................................................................................................... vii I. Team Structure ........................................................................................................................................................... 1 II. Introduction .............................................................................................................................................................. -
Appendix I Lunar and Martian Nomenclature
APPENDIX I LUNAR AND MARTIAN NOMENCLATURE LUNAR AND MARTIAN NOMENCLATURE A large number of names of craters and other features on the Moon and Mars, were accepted by the IAU General Assemblies X (Moscow, 1958), XI (Berkeley, 1961), XII (Hamburg, 1964), XIV (Brighton, 1970), and XV (Sydney, 1973). The names were suggested by the appropriate IAU Commissions (16 and 17). In particular the Lunar names accepted at the XIVth and XVth General Assemblies were recommended by the 'Working Group on Lunar Nomenclature' under the Chairmanship of Dr D. H. Menzel. The Martian names were suggested by the 'Working Group on Martian Nomenclature' under the Chairmanship of Dr G. de Vaucouleurs. At the XVth General Assembly a new 'Working Group on Planetary System Nomenclature' was formed (Chairman: Dr P. M. Millman) comprising various Task Groups, one for each particular subject. For further references see: [AU Trans. X, 259-263, 1960; XIB, 236-238, 1962; Xlffi, 203-204, 1966; xnffi, 99-105, 1968; XIVB, 63, 129, 139, 1971; Space Sci. Rev. 12, 136-186, 1971. Because at the recent General Assemblies some small changes, or corrections, were made, the complete list of Lunar and Martian Topographic Features is published here. Table 1 Lunar Craters Abbe 58S,174E Balboa 19N,83W Abbot 6N,55E Baldet 54S, 151W Abel 34S,85E Balmer 20S,70E Abul Wafa 2N,ll7E Banachiewicz 5N,80E Adams 32S,69E Banting 26N,16E Aitken 17S,173E Barbier 248, 158E AI-Biruni 18N,93E Barnard 30S,86E Alden 24S, lllE Barringer 29S,151W Aldrin I.4N,22.1E Bartels 24N,90W Alekhin 68S,131W Becquerei