Mars Atmospheric Chemistry Simulations with the GEM-Mars General Circulation Model
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Mars Express Orbiter Radio Science
MaRS: Mars Express Orbiter Radio Science M. Pätzold1, F.M. Neubauer1, L. Carone1, A. Hagermann1, C. Stanzel1, B. Häusler2, S. Remus2, J. Selle2, D. Hagl2, D.P. Hinson3, R.A. Simpson3, G.L. Tyler3, S.W. Asmar4, W.I. Axford5, T. Hagfors5, J.-P. Barriot6, J.-C. Cerisier7, T. Imamura8, K.-I. Oyama8, P. Janle9, G. Kirchengast10 & V. Dehant11 1Institut für Geophysik und Meteorologie, Universität zu Köln, D-50923 Köln, Germany Email: [email protected] 2Institut für Raumfahrttechnik, Universität der Bundeswehr München, D-85577 Neubiberg, Germany 3Space, Telecommunication and Radio Science Laboratory, Dept. of Electrical Engineering, Stanford University, Stanford, CA 95305, USA 4Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91009, USA 5Max-Planck-Instuitut für Aeronomie, D-37189 Katlenburg-Lindau, Germany 6Observatoire Midi Pyrenees, F-31401 Toulouse, France 7Centre d’etude des Environnements Terrestre et Planetaires (CETP), F-94107 Saint-Maur, France 8Institute of Space & Astronautical Science (ISAS), Sagamihara, Japan 9Institut für Geowissenschaften, Abteilung Geophysik, Universität zu Kiel, D-24118 Kiel, Germany 10Institut für Meteorologie und Geophysik, Karl-Franzens-Universität Graz, A-8010 Graz, Austria 11Observatoire Royal de Belgique, B-1180 Bruxelles, Belgium The Mars Express Orbiter Radio Science (MaRS) experiment will employ radio occultation to (i) sound the neutral martian atmosphere to derive vertical density, pressure and temperature profiles as functions of height to resolutions better than 100 m, (ii) sound -
Photophoretic Spectroscopy in Atmospheric Chemistry – High-Sensitivity Measurements of Light Absorption by a Single Particle
Atmos. Meas. Tech., 13, 3191–3203, 2020 https://doi.org/10.5194/amt-13-3191-2020 © Author(s) 2020. This work is distributed under the Creative Commons Attribution 4.0 License. Photophoretic spectroscopy in atmospheric chemistry – high-sensitivity measurements of light absorption by a single particle Nir Bluvshtein, Ulrich K. Krieger, and Thomas Peter Institute for Atmospheric and Climate Science, ETH Zurich, 8092, Switzerland Correspondence: Nir Bluvshtein ([email protected]) Received: 28 February 2020 – Discussion started: 4 March 2020 Revised: 30 April 2020 – Accepted: 16 May 2020 – Published: 18 June 2020 Abstract. Light-absorbing organic atmospheric particles, the UV–vis wavelength range, attributing them with a nega- termed brown carbon, undergo chemical and photochemi- tive (cooling) radiative effect. However, light-absorbing or- cal aging processes during their lifetime in the atmosphere. ganic aerosol, termed brown carbon (BrC), with wavelength- The role these particles play in the global radiative balance dependent light absorption (λ−2 − λ−6) in the UV–vis wave- and in the climate system is still uncertain. To better quan- length range (Chen and Bond, 2010; Hoffer et al., 2004; tify their radiative forcing due to aerosol–radiation interac- Kaskaoutis et al., 2007; Kirchstetter et al., 2004; Lack et al., tions, we need to improve process-level understanding of ag- 2012b; Moosmuller et al., 2011; Sun et al., 2007), may be the ing processes, which lead to either “browning” or “bleach- dominant light absorber downwind of urban and industrial- ing” of organic aerosols. Currently available laboratory tech- ized areas and in biomass burning plumes (Feng et al., 2013). -
+ 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 -
Mariner to Mercury, Venus and Mars
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mariner to Mercury, Venus and Mars Between 1962 and late 1973, NASA’s Jet carry a host of scientific instruments. Some of the Propulsion Laboratory designed and built 10 space- instruments, such as cameras, would need to be point- craft named Mariner to explore the inner solar system ed at the target body it was studying. Other instru- -- visiting the planets Venus, Mars and Mercury for ments were non-directional and studied phenomena the first time, and returning to Venus and Mars for such as magnetic fields and charged particles. JPL additional close observations. The final mission in the engineers proposed to make the Mariners “three-axis- series, Mariner 10, flew past Venus before going on to stabilized,” meaning that unlike other space probes encounter Mercury, after which it returned to Mercury they would not spin. for a total of three flybys. The next-to-last, Mariner Each of the Mariner projects was designed to have 9, became the first ever to orbit another planet when two spacecraft launched on separate rockets, in case it rached Mars for about a year of mapping and mea- of difficulties with the nearly untried launch vehicles. surement. Mariner 1, Mariner 3, and Mariner 8 were in fact lost The Mariners were all relatively small robotic during launch, but their backups were successful. No explorers, each launched on an Atlas rocket with Mariners were lost in later flight to their destination either an Agena or Centaur upper-stage booster, and planets or before completing their scientific missions. -
DSCOVR Magnetometer Observations Adam Szabo, Andriy Koval NASA Goddard Space Flight Center
DSCOVR Magnetometer Observations Adam Szabo, Andriy Koval NASA Goddard Space Flight Center 1 Locations of the Instruments Faraday Cup EPIC Omni Antenna Star Tracker Thruster Modules Digital Sun Sensor Electron Spectrometer +Z +X Magnetometer +Y 2 Goddard Fluxgate Magnetometer The Fluxgate Magnetometer measures the interplanetary vector magnetic field It is located at the tip of a 4.0 m boom to minimize the effect of spacecraft fields Requirement Value Method Performance Magnetometer Range 0.1-100 nT Test 0.004-65,500 nT Accuracy +/- 1 nT Measured +/- 0.2 nT Cadence 1 min Measured 50 vector/sec 3 Pre-flight Calibration • Determined the magnetometer zero levels, scale factors, and magnetometer orthogonalization matrix. • Determined the spacecraft generated magnetic fields – Subsystem level magnetic tests. Reaction wheels, major source of dynamic field, were shielded – Spacecraft unpowered magnetic test in the GSFC 40’ magnetic facility In-Flight Boom Deployment • Nominal deployment on 2/15/15, seen as 4.4 rotations in the magnetometer components Mostly spacecraft Boom deployment Interplanetary magnetic field induced fields 5 Alfven Waves in the Solar Wind • The solar wind contains magnetic field rotations that preserve the magnitude of the field, so called Alfven waves. • Alfven waves are ubiquitous and are possible to identify with automated routines. • Systematic deviations from a constant field magnitude during these waves are an indication of spacecraft induced offsets. • Minimizing the deviations with slowly changing offsets allows in-flight calibrations. 6 In-Flight Magnetometer Calibrations Z Magnetometer Zero Offsets X • X axis Roll and Z axis Slew data is Y consistent with ground calibration estimates X • Independent zero offset determination by rolls, slews and using solar wind Alfvenicity give consistent values Z • Time variation is consistent with yearly orbital change. -
An Approach to Magnetic Cleanliness for the Psyche Mission M
An Approach to Magnetic Cleanliness for the Psyche Mission M. de Soria-Santacruz J. Ream K. Ascrizzi ([email protected]), ([email protected]), ([email protected]) M. Soriano R. Oran University of Michigan Ann Arbor ([email protected]), ([email protected]), 500 S State St O. Quintero B. P. Weiss Ann Arbor, MI 48109 ([email protected]), ([email protected]) F. Wong Department of Earth, Atmospheric, ([email protected]), and Planetary Sciences S. Hart Massachusetts Institute of Technology ([email protected]), 77 Massachusetts Avenue M. Kokorowski Cambridge, MA 02139 ([email protected]) B. Bone ([email protected]), B. Solish ([email protected]), D. Trofimov ([email protected]), E. Bradford ([email protected]), C. Raymond ([email protected]), P. Narvaez ([email protected]) Jet Propulsion Laboratory, California Institute of Technology 4800 Oak Grove Drive Pasadena, CA 91109 C. Keys C. Russell L. Elkins-Tanton ([email protected]), ([email protected]), ([email protected]) P. Lord University of California Los Angeles Arizona State University ([email protected]) 405 Hilgard Avenue PO Box 871404 Maxar Technologies Inc. Los Angeles, CA 90095 Tempe, AZ 85287 3825 Fabian Avenue Palo Alto, CA 94303 Abstract— Psyche is a Discovery mission that will visit the fields. Limiting and characterizing spacecraft-generated asteroid (16) Psyche to determine if it is the metallic core of a magnetic fields is therefore essential to the mission. This is the once larger differentiated body or otherwise was formed from objective of the Psyche’s magnetics control program described accretion of unmelted metal-rich material. -
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 ......................................................... -
Atmospheric Chemistry
Atmospheric Chemistry John Lee Grenfell Technische Universität Berlin Atmospheres and Habitability (Earthlike) Atmospheres: -support complex life (respiration) -stabilise temperature -maintain liquid water -we can measure their spectra hence life-signs Modern Atmospheric Composition CO2 Modern Atmospheric Composition O2 CO2 N2 CO2 N2 CO2 Modern Atmospheric Composition O2 CO2 N2 CO2 N2 P 93bar 1bar 6mb 1.5bar surface CO2 Tsurface 735K 288K 220K 94K Early Earth Atmospheric Compositions Magma Hadean Archaean Proterozoic Snowball CO2 Early Earth Atmospheric Compositions Magma Hadean Archaean Proterozoic Snowball Silicate CO2 CO2 N2 N2 Steam H2ON2 O2 O2 CO2 Additional terrestrial-type atmospheres Jurassic Earth Early Mars Early Venus Jungleworld Desertworld Waterworld Superearth Modern Atmospheric Composition Today we will talk about these CO2 Reading List Yuk Yung (Caltech) and William DeMore “Photochemistry of Planetary Atmospheres” Richard P. Wayne (Oxford) “Chemistry of Atmospheres” T. Gredel and Paul Crutzen (Mainz) “Chemie der Atmosphäre” Processes influencing Photochemistry Photons Protection Delivery Escape Clouds Photochemistry Surface OCEAN Biology Volcanism Some fundamentals… ALKALI METALS The Periodic Table NOBLE GASES One outer electron Increasing atomic number 8 outer electrons: reactive Rows called PERIODS unreactive GROUPS: similar Halogens chemical C, Si etc. have 4 outer electrons properties SO CAN FORM STABLE CHAINS Chemical Structure and Reactivity s and p orbitals d orbitals The Aufbau Method works OK for the first 18 elements -
Chapter 1 – Introduction
1 Chapter 1 – Introduction 1.1 – Scientific Background Knowledge of gas phase compounds and their chemical reactions are pivotal to our understanding of chemistry. The conditions these molecules are in can vary dramatically, from temperatures as low as 10 K in the depths of the interstellar medium, to more than 1000 K in the combustion of hydrocarbons in engines. The chemistry in these systems is dominated by highly reactive, unstable compounds, leading to fast and complex chemistry occurring. In order to accurately understand these systems, we must be able to observe these unstable species and measure the kinetics of their formation and destruction. While molecular spectra and reaction rate constants of these reactive compounds can be computed with theoretical calculations, they must be benchmarked with experimental measurements to determine their accuracy. To that end, one major focus in experimental gas phase chemistry is to better understand these unstable molecules and their reactions in systems such as atmospheric chemistry and astrochemistry. 1.1a – Atmospheric Chemistry Understanding Earth’s atmosphere and the chemistry behind it has been a major topic in gas phase chemistry since the mid-20th century, when the impact of fossil fuel usage and air pollution resulting from the Industrial Revolution became apparent. The dominant molecule in Earth’s atmosphere is N2 (77% of the atmosphere) followed by O2 (21%) and argon (1%). The remaining components are largely stable molecules, such as CO2 and H2O. 2 Figure 1.1: The average temperature (left) and pressure (right) profiles of the Earth’s lower atmosphere, consisting of the troposphere and stratosphere. -
A Lunar Micro Rover System Overview for Aiding Science and ISRU Missions Virtual Conference 19–23 October 2020 R
i-SAIRAS2020-Papers (2020) 5051.pdf A lunar Micro Rover System Overview for Aiding Science and ISRU Missions Virtual Conference 19–23 October 2020 R. Smith1, S. George1, D. Jonckers1 1STFC RAL Space, R100 Harwell Campus, OX11 0DE, United Kingdom, E-mail: [email protected] ABSTRACT the form of rovers and landers of various size [4]. Due to the costly nature of these missions, and the pressure Current science missions to the surface of other plan- for a guaranteed science return, they have been de- etary bodies tend to be very large with upwards of ten signed to minimise risk by using redundant and high instruments on board. This is due to high reliability re- reliability systems. This further increases mission cost quirements, and the desire to get the maximum science as components and subsystems are expected to be ex- return per mission. Missions to the lunar surface in the tensively qualified. next few years are key in the journey to returning hu- mans to the lunar surface [1]. The introduction of the As an example, the Mars Science Laboratory, nick- Commercial lunar Payload Services (CLPS) delivery named the Curiosity rover, one of the most successful architecture for science instruments and technology interplanetary rovers to date, has 10 main scientific in- demonstrators has lowered the barrier to entry of get- struments, requires a large team of people to control ting science to the surface [2]. Many instruments, and and cost over $2.5 billion to build and fly [5]. Curios- In Situ Surface Utilisation (ISRU) experiments have ity had 4 main science goals, with the instruments and been funded, and are being built with the intention of the design of the rover specifically tailored to those flying on already awarded CLPS missions. -
Mars Science Is Expanding Internationally Astrobiology
International Journal of Mars science is expanding internationally Astrobiology Rocco L. Mancinelli Ph.D cambridge.org/ija Editor-in-Chief, the International Journal of Astrobiology July 2020 marked the beginning of a busy year of Mars Exploration, that will culminate with Editorial the arrival of three spacecraft at Mars in February 2021. The three spacecraft, from the United Cite this article: Mancinelli RL (2021). Mars Arab Emirates, China and the United States are all primarily robotic missions that will join a science is expanding internationally. busy group of exploration spacecraft either in orbit or on the planet’s surface. International Journal of Astrobiology 20, The Emirati Hope orbiter, the first deep space explorer of the UAE, will be the first to arrive – 109 110. https://doi.org/10.1017/ on February 9th. The orbiter was developed through a partnership between Mohamed bin S1473550421000045 Rashid Space Centre (MBRSC), Laboratory for Atmospheric and Space Physics at the First published online: 16 February 2021 University of Colorado-Boulder, and Arizona State University (ASU). Hope has three instru- ments, two spectrometers and one exploration imager (high-resolution camera). One spec- trometer will determine the temperature of the planet through the Martian year, the other will measure the oxygen and hydrogen levels at ∼40,000 kilometers from the surface of Mars. The imager will also provide information on the ozone levels on the Red Planet. The orbiter will be active through one Martian year (two Earth years). Next will be China’s Tianwen-1 mission scheduled to arrive at Mars on February 10th. After orbiting the planet, it will send a lander containing a rover to the surface in May. -
MEASURING MAGNETIC FIELDS at OCEAN WORLDS. J. R. Espley1, G.A. Dibraccio1, and J. R. Gruesbeck1 1NASA's Goddard Space Flight C
52nd Lunar and Planetary Science Conference 2021 (LPI Contrib. No. 2548) 1746.pdf MEASURING MAGNETIC FIELDS AT OCEAN WORLDS. J. R. Espley1, G.A. DiBraccio1, and J. R. Gruesbeck1 1NASA’s Goddard Space Flight Center (Code 695, Goddard Space Flight Center, Greenbelt, MD 20771, [email protected]) Summary: Magnetic field measurements have selective way. Collaborative approaches between the been a vital part of Solar System exploration for spacecraft team and experienced magnetometer decades. Measuring magnetic fields at ocean worlds instrument teams can often allow for relatively easy will yield important science results. Magnetometers are magnetic cleanliness programs. Often times, the easiest very low resource instruments (even with magnetic approach is simply a relatively long boom to keep the cleanliness). We welcome interest in collaborations for sensor away from the spacecraft. Such booms do cost future missions. spacecraft resources (mass, volume, and budget) but Ocean World Magnetometer Science Topics: often these costs are very modest and allow Magnetic fields tell us about a world’s: comparatively lax magnetic cleanliness programs. In all plasma environment (magnetosphere, ionosphere) cases, the most appropriate solution will depend on the volatile escape (e.g. plumes, atmospheric erosion), science requirements. An experienced magnetometer distribution of conducting materials (e.g. water, instrumentation team can easily help craft this metal) appropriate approach and keep the overall impact of the Example Ocean Worlds Destinations: The magnetic investigation modest compared to the very potential future targets for magnetic field investigations significant science results. are abundant (figures 1a-d). As examples, we could detect and characterize subsurface water or magma oceans (e.g.