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The Space Impact of the Euro Crisis 50 Years After Mariner 2: Exploration at a Crossroads
0827_SPN_DOM_00_019_00 (READ ONLY) 8/24/2012 11:39 AM Page 19 www.spacenews.com SPACENEWS 19 August27, 2012 TheSpaceImpact of the Euro Crisis < ROBBIN LAIRD and HARALD MALMGREN > he European sovereign debt crisis Europe will now be challenged in the ing to hide the reality of European bank of the savings of millions of European is not simply abump in historical form of rollbacks of the many inter- weaknesses. The main reason is that eu- citizens. Tprogress; it is the end of aperiod twined strands of integration, fraying rozone economies are far more bank- European leaders are also attempt- of historyand acritical point in Euro- what has been an intricate but incom- dependent than economies like those in ing to initiate amore comprehensive fis- pean and global transition in the 21st plete tapestry. It is questionable whether the United States or United Kingdom, cal union, with new decision-making century. Europe will be able to prevent stalling of where substantial nonbank financing al- mechanisms that transfer sovereignty in The confluence of several trend lines the integration process in the face of ternatives exist for the corporate sector. parallel with the new banking union. We — the unification of Germany,the end widening gaps among the interests of In the eurozone, banks are the fi- do not believe that any of the eurozone of the Soviet Union, the collapse of the each nation and even within each nation. nancial markets; in the U.S., banks are governments are ready for such apoliti- Berlin Wall, the expansion of NATO, Since the birth of the euro, the but one segment of amultifaceted fi- cal transition in which citizens in each the expansion of the European Union French and Germans were in the lead in nancial market. -
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. -
Investigating Mineral Stability Under Venus Conditions: a Focus on the Venus Radar Anomalies Erika Kohler University of Arkansas, Fayetteville
University of Arkansas, Fayetteville ScholarWorks@UARK Theses and Dissertations 5-2016 Investigating Mineral Stability under Venus Conditions: A Focus on the Venus Radar Anomalies Erika Kohler University of Arkansas, Fayetteville Follow this and additional works at: http://scholarworks.uark.edu/etd Part of the Geochemistry Commons, Mineral Physics Commons, and the The unS and the Solar System Commons Recommended Citation Kohler, Erika, "Investigating Mineral Stability under Venus Conditions: A Focus on the Venus Radar Anomalies" (2016). Theses and Dissertations. 1473. http://scholarworks.uark.edu/etd/1473 This Dissertation is brought to you for free and open access by ScholarWorks@UARK. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of ScholarWorks@UARK. For more information, please contact [email protected], [email protected]. Investigating Mineral Stability under Venus Conditions: A Focus on the Venus Radar Anomalies A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy in Space and Planetary Sciences by Erika Kohler University of Oklahoma Bachelors of Science in Meteorology, 2010 May 2016 University of Arkansas This dissertation is approved for recommendation to the Graduate Council. ____________________________ Dr. Claud H. Sandberg Lacy Dissertation Director Committee Co-Chair ____________________________ ___________________________ Dr. Vincent Chevrier Dr. Larry Roe Committee Co-chair Committee Member ____________________________ ___________________________ Dr. John Dixon Dr. Richard Ulrich Committee Member Committee Member Abstract Radar studies of the surface of Venus have identified regions with high radar reflectivity concentrated in the Venusian highlands: between 2.5 and 4.75 km above a planetary radius of 6051 km, though it varies with latitude. -
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. -
(50000) Quaoar, See Quaoar (90377) Sedna, See Sedna 1992 QB1 267
Index (50000) Quaoar, see Quaoar Apollo Mission Science Reports 114 (90377) Sedna, see Sedna Apollo samples 114, 115, 122, 1992 QB1 267, 268 ap-value, 3-hour, conversion from Kp 10 1996 TL66 268 arcade, post-eruptive 24–26 1998 WW31 274 Archimedian spiral 11 2000 CR105 269 Arecibo observatory 63 2000 OO67 277 Ariel, carbon dioxide ice 256–257 2003 EL61 270, 271, 273, 274, 275, 286, astrometric detection, of extrasolar planets – mass 273 190 – satellites 273 Atlas 230, 242, 244 – water ice 273 Bartels, Julius 4, 8 2003 UB313 269, 270, 271–272, 274, 286 – methane 271–272 Becquerel, Antoine Henry 3 – orbital parameters 271 Biermann, Ludwig 5 – satellite 272 biomass, from chemolithoautotrophs, on Earth 169 – spectroscopic studies 271 –, – on Mars 169 2005 FY 269, 270, 272–273, 286 9 bombardment, late heavy 68, 70, 71, 77, 78 – atmosphere 273 Borealis basin 68, 71, 72 – methane 272–273 ‘Brown Dwarf Desert’ 181, 188 – orbital parameters 272 brown dwarfs, deuterium-burning limit 181 51 Pegasi b 179, 185 – formation 181 Alfvén, Hannes 11 Callisto 197, 198, 199, 200, 204, 205, 206, ALH84001 (martian meteorite) 160 207, 211, 213 Amalthea 198, 199, 200, 204–205, 206, 207 – accretion 206, 207 – bright crater 199 – compared with Ganymede 204, 207 – density 205 – composition 204 – discovery by Barnard 205 – geology 213 – discovery of icy nature 200 – ice thickness 204 – evidence for icy composition 205 – internal structure 197, 198, 204 – internal structure 198 – multi-ringed impact basins 205, 211 – orbit 205 – partial differentiation 200, 204, 206, -
Styles of Deformation in Ishtar Terra and Their Implications
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 97, NO. El0, PAGES 16,085-16,120, OCTOBER 25, 1992 Stylesof Deformationin IshtarTerra and Their Implications Wn.T.TAMM. KAU•A,• DOAN•L. BINDSCHAD•-R,l ROBERT E. GPaM•,2'3 VICKIL. HANSEN,2KARl M. ROBERTS,4AND SUZANNE E. SMREr,AR s IshtarTerra, the highest region on Venus, appears to havecharacteristics of both plume uplifts and convergent belts.Magellan imagery over longitudes 330ø-30øE indicates a great variety of tectonicand volcanic activity, with largevariations within distances of onlya few 100km. Themost prominent terrain types are the volcanic plains of Lakshmiand the mountain belts of Maxwell,Freyja, and Danu. Thebelts appear to havemarked variations in age. Thereare also extensive regions of tesserain boththe upland and outboard plateaus, some rather featureless smoothscarps, flanking basins of complexextensional tectonics, and regions of gravitationalor impactmodifica- tion.Parts of Ishtarare the locations of contemporaryvigorous tectonics and past extensive volcanism. Ishtar appearsto be the consequence of a history of several100 m.y., in whichthere have been marked changes in kinematic patternsand in whichactivity at any stage has been strongly influenced by the past. Ishtar demonstrates three general propertiesof Venus:(1) erosionaldegradation is absent,leading to preservationof patternsresulting from past activity;(2) manysurface features are the responses ofa competentlayer less than 10 km thick to flowsof 100km orbroaderscale; and (3) thesebroader scale flows are controlled mainly by heterogeneities inthe mantle. Ishtar Terra doesnot appear to bethe result of a compressionconveyed by anEarthlike lithosphere. But there is stilldoubt as to whetherIshtar is predominantlythe consequence of a mantleupflow or downflow.Upflow is favoredby the extensivevolcanic plain of Lakshmiand the high geoid: topography ratio; downflow is favoredby the intense deformationof themountain belts and the absence of majorrifts. -
Jupitor's Great Red Spot
GREAT RED SPOT appears somewhat orange in this remarkably ly ranged from '.'full gray" and "pinkish" to "brick red" and "car· detailed photograph made at the Lunar and Planetary Laboratory mine." The photograph was made on December 23, 1966, by Alika of the University of Arizona. During the century or so that Jupiter's Herring and John Fountain, who used a 61·inch reflecting tele· great red spot bas been closely observed its color has reported. scope. The exposure was one second on High Speed Ektachrome. © 1968 SCIENTIFIC AMERICAN, INC JUPITER'S GREAT RED SPOT There is evidence to suggest that this peculiar Inarking is the top of a "Taylor cohunn": a stagnant region above a bll111p 01' depression at the botton1 of a circulating fluid by Haymond Hide he surface markings of the plan To explain the fluctuations in the red tals suspended in an atmosphere that is Tets have always had a special fas spot's period of rotation one must assume mainly hydrogen admixed with water cination, and no single marking that there are forces acting on the solid and perhaps methane and helium. Other has been more fascinating and puzzling planet capable of causing an equivalent lines of evidence, particularly the fact than the great red spot of Jupiter. Un change in its rotation period. In other that Jupiter's density is only 1.3 times like the elusive "canals" of Mars, the red words, the fluctuations in the rotation the density of water, suggest that the spot unmistakably exists. Although it has period of the red spot are to be regarded main constituents of the planet are hy been known to fade and change color, it as a true reflection of the rotation period drogen and helium. -
User Guide to the Magellan Synthetic Aperture Radar Images
https://ntrs.nasa.gov/search.jsp?R=19950018567 2020-06-16T07:22:10+00:00Z User Guide to the Magellan Synthetic Aperture Radar Images Stephen D. Wall Shannon L. McConnell Craig E. Left Richard S. Austin Kathi K. Beratan Mark J. Rokey National Aeronautics and Jet Propulsion Laboratory Space Administration California Institute of Technology Scientific and Technical Pasadena, California Information Branch NASA Reference Publication 1356 March 1995 This publication was prepared at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. Contents Iri Introduction .................................................................................................................................................................... 1 I_1 The Spacecraft ................................................................................................................................................................ 2 IB Mission Design ................................................................................................................................................................ 4 D Experiment Description ................................................................................................................................................ 15 B Mission Operations ....................................................................................................................................................... 17 [] Notable Events and Problems ..................................................................................................................................... -
Phil Liebrecht Assistant Deputy Associate Administrator and Deputy Program Manager Space Communications and Navigation NASA HQ
Phil Liebrecht Assistant Deputy Associate Administrator and Deputy Program Manager Space Communications and Navigation NASA HQ Meeting the Communications and Navigation Needs of Space missions since 1957 “Keeping the Universe Connected” Public University of Navarra, 2010 [email protected] 1 Operations and Communications Customers 2 Space Operations 101 Relation Between Space Segment, Ground System, and Data Users* Ground System Command Commands Requests Spacecraft and Payload Support • Mission Planning Telemetry • Flight Operations • Flight Dynamics • Perf. Assess., Trending & Archiving Space Data Users • Anomaly Support Segment Data Relay and Level (S/C) Mission Zero Data Processing Mission Data Data • Space-to-ground Comm. • Data Capture • Data Processing • Network Management • Data Distribution • Quick Look * Based on Wertz and Wiley; Space Mission Analysis and Design 3 Communications Theory- Basic Concepts Transmitter and Receiver must use the same language Noise causes interference a) Figures it – no errors (Identify and quantify) b) Figures it – corrects Must be loud enough ENERGY! c) Figures it – incorrectly (message in error) d) Cannot figure- recognizes E L an error T M E XP AIN L E e) Cannot figure- ? TRANSMITTER Distance weakens the sound RECEIVER (calculate the loss) CHANNEL Has to correctly interpret the message - the most difficult job The fundamental problem of communications is that of reproducing at one point either exactly or approximately a message selected at another point. 4 Functional - End to End Process -
Volcanism and Tectonism in Rusalka Planitia and Atla Regio, Venus; M
LPSC xn/ 767 VOLCANISM AND TECTONISM IN RUSALKA PLANITIA AND ATLA REGIO, VENUS; M. G. Lancaster and J. E. Guest (University of London Observatory, University College London, London, NW7 2QS, U. K.). In order to investigate the relationships between volcanism and tectonism in Rusalka Planitia and Atla Regio, the geology of four adjacent Cycle 1 Magellan ClMIDRs has been mapped (C100N180, C115N180, C115N197, and C100N197). These cover nearly 12 x 106 km2 between latitudes 7.6 S and 22.6 N, and longitudes 171.4 to 206.2 E. This region was chosen because it contains nearly all the types of volcanic and tectonic features observed on Venus, and covers plains as well as highlands. The western half of the region comprises most of the volcanic plains of Rusalka Planitia, which are characterized by a large-scale pervasive fabric of NW-SE trending sinuous ridges that resemble lunar and martian wrinkle ridges [I]. A NW-SE to N-S trending deformation belt occupies the SW comer of C100N180, and contains several coronae including Eigin Corona (5.0 S, 175.0 E). The belt is the source for large, radar-bright, plains forming, flood lava flow fields. A similar collection of corona-like centers and deformation belts composed largely of ridges, is found in the NE comer of C115N197, where an extensive collection of lava flow fields is also present. Other smaller regions of radar-bright lava lie scattered across the plains. A number of N-S to NNW-SSE trending ridge belts occupy the north-central part of these plains. -
SPITZER SPACE TELESCOPE MID-IR LIGHT CURVES of NEPTUNE John Stauffer1, Mark S
The Astronomical Journal, 152:142 (8pp), 2016 November doi:10.3847/0004-6256/152/5/142 © 2016. The American Astronomical Society. All rights reserved. SPITZER SPACE TELESCOPE MID-IR LIGHT CURVES OF NEPTUNE John Stauffer1, Mark S. Marley2, John E. Gizis3, Luisa Rebull1,4, Sean J. Carey1, Jessica Krick1, James G. Ingalls1, Patrick Lowrance1, William Glaccum1, J. Davy Kirkpatrick5, Amy A. Simon6, and Michael H. Wong7 1 Spitzer Science Center (SSC), California Institute of Technology, Pasadena, CA 91125, USA 2 NASA Ames Research Center, Space Sciences and Astrobiology Division, MS245-3, Moffett Field, CA 94035, USA 3 Department of Physics and Astronomy, University of Delaware, Newark, DE 19716, USA 4 Infrared Science Archive (IRSA), 1200 E. California Boulevard, MS 314-6, California Institute of Technology, Pasadena, CA 91125, USA 5 Infrared Processing and Analysis Center, MS 100-22, California Institute of Technology, Pasadena, CA 91125, USA 6 NASA Goddard Space Flight Center, Solar System Exploration Division (690.0), 8800 Greenbelt Road, Greenbelt, MD 20771, USA 7 University of California, Department of Astronomy, Berkeley CA 94720-3411, USA Received 2016 July 13; revised 2016 August 12; accepted 2016 August 15; published 2016 October 27 ABSTRACT We have used the Spitzer Space Telescope in 2016 February to obtain high cadence, high signal-to-noise, 17 hr duration light curves of Neptune at 3.6 and 4.5 μm. The light curve duration was chosen to correspond to the rotation period of Neptune. Both light curves are slowly varying with time, with full amplitudes of 1.1 mag at 3.6 μm and 0.6 mag at 4.5 μm. -
Mercury Friday, February 23
ASTRONOMY 161 Introduction to Solar System Astronomy Class 18 Mercury Friday, February 23 Mercury: Basic characteristics Mass = 3.302×1023 kg (0.055 Earth) Radius = 2,440 km (0.383 Earth) Density = 5,427 kg/m³ Sidereal rotation period = 58.6462 d Albedo = 0.11 (Earth = 0.39) Average distance from Sun = 0.387 A.U. Mercury: Key Concepts (1) Mercury has a 3-to-2 spin-orbit coupling (not synchronous rotation). (2) Mercury has no permanent atmosphere because it is too hot. (3) Like the Moon, Mercury has cratered highlands and smooth plains. (4) Mercury has an extremely large iron-rich core. (1) Mercury has a 3-to-2 spin-orbit coupling (not synchronous rotation). Mercury is hard to observe from the Earth (because it is so close to the Sun). Its rotation speed can be found from Doppler shift of radar signals. Mercury’s unusual orbit Orbital period = 87.969 days Rotation period = 58.646 days = (2/3) x 87.969 days Mercury is NOT in synchronous rotation (1 rotation per orbit). Instead, it has 3-to-2 spin-orbit coupling (3 rotations for 2 orbits). Synchronous rotation (WRONG!) 3-to-2 spin-orbit coupling (RIGHT!) Time between one noon and the next is 176 days. Sun is above the horizon for 88 days at the time. Daytime temperatures reach as high as: 700 Kelvin (800 degrees F). Nighttime temperatures drops as low as: 100 Kelvin (-270 degrees F). (2) Mercury has no permanent atmosphere because it is too hot (and has low escape speed). Temperature is a measure of the 3kT v = random speed of m atoms (or v typical speed of atom molecules).