The Structure and Variability of Mars Dayside Thermosphere from MAVEN
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Financial Support for the Development of These Album Pages Provided by Mystic Stamp Company America's Leading Stamp Dealer
SPACE ON STAMPS Created for free use in the public domain American Philatelic Society ©2010 • www.stamps.org Financial support for the development of these album pages provided by Mystic Stamp Company America’s Leading Stamp Dealer and proud of its support of the American Philatelic Society www.MysticStamp.com, 800-433-7811 Space on Stamps ou might say, it all started with the dream of flight and a desire to see the world as the birds do. For tens of thousands of years mankind has watched the stars Yand wondered what they might represent. Possibly the oldest constellation identified by humans as a permanent fixture in the night sky is Ursa Major, the Great Bear, the third largest of the constellations, and best known for the seven stars that make up its rump and tail: the Big Dipper (also known as the Plough or the Wagon). The most helpful of the sky maps, a line drawn though the two outside stars on the bowl of the “dipper” points directly to the North Star. Nothing successfully got human beings above the earth on a repeatable basis, however, until the age of ballooning. The first human to go aloft was a scientist, Pilatre de Rozier, who rose 250 feet into the sky in a hot air balloon and remained suspended above the French countryside for fifteen minutes in October 1783. A month later he and the Marquis d’Arlandes traveled about 5½ miles in the first free flight, using a balloon designed by the Montgolfier brothers. The first North American flight was made January 9, 1793, from Philadelphia to Gloucester County, New Jersey. -
Electron Energetics in the Martian Dayside Ionosphere: Model Comparisons with MAVEN Data Shotaro Sakai1, Laila Andersson2, Thomas E
Electron energetics in the Martian dayside ionosphere: Model comparisons with MAVEN data Shotaro Sakai1, Laila Andersson2, Thomas E. Cravens1, David L. Mitchell3, Christian Mazelle4,5, Ali Rahmati1,3, Christopher M. Fowler2, Stephen W. Bougher6, Edward M. B. Thiemann2, Francis G. Eparvier2, Juan M. Fontenla7, Paul R. Mahaffy8, John E. P. Connerney8, and Bruce M. Jakosky2 1Department of Physics and Astronomy, University of Kansas, Malott Hall, 1251 Wescoe Hall Drive, Lawrence, Kansas 66045, USA 2Laboratory for Atmospheric and Space Physics, University of Colorado Boulder, 1234 Innovation Drive, Boulder, Colorado 80303, USA 3Space Science Laboratory, University of California, 7 Gauss Way, Berkeley, California 94720, USA 4Université de Toulouse, UPS-OMP, IRAP, Toulouse, France 5CNRS, IRAP, 9 Av. Colonel Roche, BP 44346-31028 Toulouse Cedex 4, France 6Department of Atmospheric, Oceanic and Space Sciences, University of Michigan, 2455 Hayward Street, Ann Arbor, Michigan 48109, USA 7NorthWest Research Associates, 3380 Mitchell Ln, Boulder, Colorado 80301, USA 8NASA Goddard Space Flight Center, 8800 Greenbelt Rd, Greenbelt, Maryland 20771, USA Corresponding Author: Thomas E. Cravens, Department of Physics and Astronomy, University of Kansas, Malott Hall, 1251 Wescoe Hall Drive, Lawrence, KS 66045, USA ([email protected]) Main points * High electron temperatures (e.g., 3000 K) can be obtained in the Martian topside ionosphere without invoking solar wind heating. * The magnetic topology is a key factor in determining electron temperatures and photoelectron fluxes at Mars. This is the author manuscript accepted for publication and has undergone full peer review but has not been through the copyediting, typesetting, pagination and proofreading process, which may lead to differences between this version and the Version of Record. -
Infrared Experiments for Spaceborne Planetary Atmospheres Research Full Report
NASA Technical Memorandum 84414 Infrared Experiments for Spaceborne Planetary Atmospheres Research Full Report Infrared Experiments Working Group NOVEMBER 1981 NASA NASA Technical Memorandum 84414 Infrared Experiments for Spaceborne Planetary Atmospheres Research Full Report Infrared Experiments Working Group Jet Propulsion Laboratory Pasadena, California NASA National Aeronautics and Space Administration Scientific and Technical Information Branch 1981 TABLE OF CONTENTS Preface Summary of Principal Conclusions and Recommendations Chapter I The Role of Infrared Sensing in Atmospheric Science Chapter II Review of Existing Infrared Measurement Techniques Chapter III Critical Comparison of Proposed Measurement Techniques Chapter IV Conclusions and Recommended Instrument Developments Appendices: A Critical Technologies B Applicability of Atmospheric Infrared Instrumentation to Surface Science C Supporting Studies in Data Analysis and Numerical Modeling D Description of Planned Earth Orbital Platforms ii PREFACE Experiments conducted in the infrared spectral region provide a powerful tool for the study of the composition, structure and dynamics of planetary atmospheres. However, the field has become highly complex, especially that part associated with spacecraft sensing, and the range of technologies used so diverse that it is difficult to determine which of the available methods for making a particular measurement is to be preferred, even for those deeply involved in the field. Unfortunately, the realities of the age demand that some selectivity be employed; not all approaches can be supported. Furthermore, the chosen methods are generally sufficiently untried that long pre-flight developments are neces- sary if viable proposals are to be written for future flight opportunities. These considerations clearly lead to a program of developments which must be coordinated on a national scale. -
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. -
A Tracer of CO2 Density Variations in the Martian Lower CO2 Density Provided by the Mars Climate Database Is Scaled Down by a Factor Between 0.50 and 0.66
Journal of Geophysical Research: Planets 1 RESEARCH ARTICLE The O( S) 297.2-nm Dayglow Emission: A Tracer of CO2 Density 10.1029/2018JE005709 Variations in the Martian Lower Thermosphere Key Points: L. Gkouvelis1 , J.-C. Gérard1 , B. Ritter1,2 , B. Hubert1 , N. M. Schneider3 , and S. K. Jain3 • Limb observations of the O(1S-3P) fi dayglow by MAVEN con rm 1LPAP, STAR Institute, Université de Liège, Liege, Belgium, 2Royal Observatory of Belgium, Brussels, Belgium, 3LASP, existence of previously predicted emission peak near 80 km University of Colorado Boulder, Boulder, CO, USA • We successfully model the lower peak emission profile and show that 1 it only depends on the vertical CO2 Abstract The O( S) metastable atoms can radiatively relax by emitting airglow at 557.7 and 297.2 nm. The distribution and solar Ly-alpha latter one has been observed with the Imaging Ultraviolet Spectrograph onboard the Mars Atmosphere • Combination of model and fi observations enable to constrain the and Volatile Evolution Mars orbiter since 2014. Limb pro les of the 297.2-nm dayglow have been collected slant CO2 column over the peak and near periapsis with a spatial resolution of 5 km or less. They show a double-peak structure that was previously the corresponding atmospheric predicted but never observed during earlier Mars missions. The production of both 297.2-nm layers is pressure dominated by photodissociation of CO2. Their altitude and brightness is variable with season and latitude, reflecting changes in the total column of CO2 present in the lower thermosphere. Since the lower emission peak near 85 km is solely produced by photodissociation, its peak is an indicator of the unit optical depth Correspondence to: pressure level and the overlying CO2 column density. -
Space Sector Brochure
SPACE SPACE REVOLUTIONIZING THE WAY TO SPACE SPACECRAFT TECHNOLOGIES PROPULSION Moog provides components and subsystems for cold gas, chemical, and electric Moog is a proven leader in components, subsystems, and systems propulsion and designs, develops, and manufactures complete chemical propulsion for spacecraft of all sizes, from smallsats to GEO spacecraft. systems, including tanks, to accelerate the spacecraft for orbit-insertion, station Moog has been successfully providing spacecraft controls, in- keeping, or attitude control. Moog makes thrusters from <1N to 500N to support the space propulsion, and major subsystems for science, military, propulsion requirements for small to large spacecraft. and commercial operations for more than 60 years. AVIONICS Moog is a proven provider of high performance and reliable space-rated avionics hardware and software for command and data handling, power distribution, payload processing, memory, GPS receivers, motor controllers, and onboard computing. POWER SYSTEMS Moog leverages its proven spacecraft avionics and high-power control systems to supply hardware for telemetry, as well as solar array and battery power management and switching. Applications include bus line power to valves, motors, torque rods, and other end effectors. Moog has developed products for Power Management and Distribution (PMAD) Systems, such as high power DC converters, switching, and power stabilization. MECHANISMS Moog has produced spacecraft motion control products for more than 50 years, dating back to the historic Apollo and Pioneer programs. Today, we offer rotary, linear, and specialized mechanisms for spacecraft motion control needs. Moog is a world-class manufacturer of solar array drives, propulsion positioning gimbals, electric propulsion gimbals, antenna positioner mechanisms, docking and release mechanisms, and specialty payload positioners. -
Mars Core Structure—Concise Review and Anticipated Insights from Insight George Helffrich
Helffrich Progress in Earth and Planetary Science (2017) 4:24 Progress in Earth and DOI 10.1186/s40645-017-0139-4 Planetary Science REVIEW Open Access Mars core structure—concise review and anticipated insights from InSight George Helffrich Abstract This review summarizes the knowledge of Mars’ interior structure, its inferred composition, and the anticipated seismological properties arising from its composition with particular focus on Mars’ core. The emphasis on the core stems from the unusual morphology of the liquidus diagram of iron at moderate pressures when enriched in sulfur. From a fairly detailed liquidus diagram constructed from experimental studies, I identify a set of processes that could act within Mars’ core: an iron “snow” from the core-mantle boundary’s surface and a Fe3−xS2 “ground fog” forming at the base of the core. Depending on temperature and bulk sulfur composition, these could form an inner core or could stratify the outer core by enriching it in sulfur, or both. Core stratification could be one explanation for the extinction of Mars’ magnetic field early in the planet’s history, and I demonstrate the feasibility of this mechanism. The crystallization processes in the core could be observable in the seismic data that the future Mars geophysical mission, InSight, is planned to provide. The core size, the presence of an inner core, and the wavespeed profile of the outer core, whose radial derivative provides a proxy for changes in composition, are key observables to seek. Keywords: Mars, InSight, Dynamo, Core, Fe-FeS phase relations, Stratification Introduction Consequently, physical parameters provided by astro- The Earth’s density distribution is known principally nomical and orbital measurements yield the only con- through the eigenfrequencies of its whole-body oscil- straints on Mars’ internal structure. -
Complete List of Contents
Complete List of Contents Volume 1 Cape Canaveral and the Kennedy Space Center ......213 Publisher’s Note ......................................................... vii Chandra X-Ray Observatory ....................................223 Introduction ................................................................. ix Clementine Mission to the Moon .............................229 Preface to the Third Edition ..................................... xiii Commercial Crewed vehicles ..................................235 Contributors ............................................................. xvii Compton Gamma Ray Observatory .........................240 List of Abbreviations ................................................. xxi Cooperation in Space: U.S. and Russian .................247 Complete List of Contents .................................... xxxiii Dawn Mission ..........................................................254 Deep Impact .............................................................259 Air Traffic Control Satellites ........................................1 Deep Space Network ................................................264 Amateur Radio Satellites .............................................6 Delta Launch Vehicles .............................................271 Ames Research Center ...............................................12 Dynamics Explorers .................................................279 Ansari X Prize ............................................................19 Early-Warning Satellites ..........................................284 -
Insight Spacecraft Launch for Mission to Interior of Mars
InSight Spacecraft Launch for Mission to Interior of Mars InSight is a robotic scientific explorer to investigate the deep interior of Mars set to launch May 5, 2018. It is scheduled to land on Mars November 26, 2018. It will allow us to better understand the origin of Mars. First Launch of Project Orion Project Orion took its first unmanned mission Exploration flight Test-1 (EFT-1) on December 5, 2014. It made two orbits in four hours before splashing down in the Pacific. The flight tested many subsystems, including its heat shield, electronics and parachutes. Orion will play an important role in NASA's journey to Mars. Orion will eventually carry astronauts to an asteroid and to Mars on the Space Launch System. Mars Rover Curiosity Lands After a nine month trip, Curiosity landed on August 6, 2012. The rover carries the biggest, most advanced suite of instruments for scientific studies ever sent to the martian surface. Curiosity analyzes samples scooped from the soil and drilled from rocks to record of the planet's climate and geology. Mars Reconnaissance Orbiter Begins Mission at Mars NASA's Mars Reconnaissance Orbiter launched from Cape Canaveral August 12. 2005, to find evidence that water persisted on the surface of Mars. The instruments zoom in for photography of the Martian surface, analyze minerals, look for subsurface water, trace how much dust and water are distributed in the atmosphere, and monitor daily global weather. Spirit and Opportunity Land on Mars January 2004, NASA landed two Mars Exploration Rovers, Spirit and Opportunity, on opposite sides of Mars. -
Galileo in 1610
Module 3 – Nautical Science Unit 4 – Astronomy Chapter 15 - The Planets Section 2 – Mars & Jupiter What You Will Learn to Do Demonstrate understanding of astronomy and how it pertains to our solar system and its related bodies: Moon, Sun, stars and planets Objectives 1. Describe the major features of Mars 2. Identify the principal characteristics of Jupiter Key Terms CPS Key Term Questions 1 - 5 Key Terms Nix Olympica - Snow of Olympus Galilean satellites - The four largest and brightest moons of Jupiter: Io, Europa, Ganymede and Callisto; discovered by Galileo in 1610 Prograde The counter-clockwise direction of motion - celestial bodies around the Sun as seen from above the north pole of the Sun; in the sky it is from west to east Key Terms Retrograde The clockwise direction of celestial motion - bodies around the Sun; in the sky it is from east to west Rotational axis - The straight line through all fixed points of a rotating rigid body around which all other points of the body move in circles Opening Question Discuss what types of exploration missions have occurred on Mars. (Use CPS “Pick a Student” for this question.) Mars Fourth from Mars the Sun and the next planet beyond Earth, Mars has aroused the greatest interest. Mars Mars Ares (Roman Mars) Mars Named for the Roman god of war, it is often called the “red planet.” Mars Mars’ red color and its rapid movement from west to east among the stars make it stand out in the sky. Mars Earth The best time to see Mars is when it is nearest to Earth in August and September, when the Earth is Sun between the Sun and Mars. -
Getting to Mars How Close Is Mars?
Getting to Mars How close is Mars? Exploring Mars 1960-2004 Of 42 probes launched: 9 crashed on launch or failed to leave Earth orbit 4 failed en route to Mars 4 failed to stop at Mars 1 failed on entering Mars orbit 1 orbiter crashed on Mars 6 landers crashed on Mars 3 flyby missions succeeded 9 orbiters succeeded 4 landers succeeded 1 lander en route Score so far: Earthlings 16, Martians 25, 1 in play Mars Express Mars Exploration Rover Mars Exploration Rover Mars Exploration Rover 1: Meridiani (Opportunity) 2: Gusev (Spirit) 3: Isidis (Beagle-2) 4: Mars Polar Lander Launch Window 21: Jun-Jul 2003 Mars Express 2003 Jun 2 In Mars orbit Dec 25 Beagle 2 Lander 2003 Jun 2 Crashed at Isidis Dec 25 Spirit/ Rover A 2003 Jun 10 Landed at Gusev Jan 4 Opportunity/ Rover B 2003 Jul 8 Heading to Meridiani on Sunday Launch Window 1: Oct 1960 1M No. 1 1960 Oct 10 Rocket crashed in Siberia 1M No. 2 1960 Oct 14 Rocket crashed in Kazakhstan Launch Window 2: October-November 1962 2MV-4 No. 1 1962 Oct 24 Rocket blew up in parking orbit during Cuban Missile Crisis 2MV-4 No. 2 "Mars-1" 1962 Nov 1 Lost attitude control - Missed Mars by 200000 km 2MV-3 No. 1 1962 Nov 4 Rocket failed to restart in parking orbit The Mars-1 probe Launch Window 3: November 1964 Mariner 3 1964 Nov 5 Failed after launch, nose cone failed to separate Mariner 4 1964 Nov 28 SUCCESS, flyby in Jul 1965 3MV-4 No. -
Mars Pathfinder
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mars Pathfinder Mars Pathfinder was the first completed mission events, ending in a touchdown which left all systems in NASAs Discovery Program of low-cost, rapidly intact. developed planetary missions with highly focused sci- The landing site, an ancient flood plain in Mars ence goals. With a development time of only three northern hemisphere known as Ares Vallis, is among years and a total cost of $265 million, Pathfinder was the rockiest parts of Mars. It was chosen because sci- originally designed entists believed it to as a technology be a relatively safe demonstration of a surface to land on way to deliver an and one which con- instrumented lander tained a wide vari- and a free-ranging ety of rocks robotic rover to the deposited during a surface of the red catastrophic flood. planet. Pathfinder In the event early in not only accom- Mars history, sci- plished this goal but entists believe that also returned an the flood plain was unprecedented cut by a volume of amount of data and water the size of outlived its primary North Americas design life. Great Lakes in Pathfinder used about two weeks. an innovative The lander, for- method of directly mally named the entering the Carl Sagan Martian atmos- Memorial Station phere, assisted by a following its suc- parachute to slow cessful touchdown, its descent through and the rover, the thin Martian atmosphere and a giant system of named Sojourner after American civil rights crusader airbags to cushion the impact.