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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. -
Chemical Variations in Yellowknife Bay Formation Sedimentary Rocks
PUBLICATIONS Journal of Geophysical Research: Planets RESEARCH ARTICLE Chemical variations in Yellowknife Bay formation 10.1002/2014JE004681 sedimentary rocks analyzed by ChemCam Special Section: on board the Curiosity rover on Mars Results from the first 360 Sols of the Mars Science Laboratory N. Mangold1, O. Forni2, G. Dromart3, K. Stack4, R. C. Wiens5, O. Gasnault2, D. Y. Sumner6, M. Nachon1, Mission: Bradbury Landing P.-Y. Meslin2, R. B. Anderson7, B. Barraclough4, J. F. Bell III8, G. Berger2, D. L. Blaney9, J. C. Bridges10, through Yellowknife Bay F. Calef9, B. Clark11, S. M. Clegg5, A. Cousin5, L. Edgar8, K. Edgett12, B. Ehlmann4, C. Fabre13, M. Fisk14, J. Grotzinger4, S. Gupta15, K. E. Herkenhoff7, J. Hurowitz16, J. R. Johnson17, L. C. Kah18, N. Lanza19, Key Points: 2 1 20 21 12 16 2 • J. Lasue , S. Le Mouélic , R. Léveillé , E. Lewin , M. Malin , S. McLennan , S. Maurice , Fluvial sandstones analyzed by 22 22 23 19 19 24 25 ChemCam display subtle chemical N. Melikechi , A. Mezzacappa , R. Milliken , H. Newsom , A. Ollila , S. K. Rowland , V. Sautter , variations M. Schmidt26, S. Schröder2,C.d’Uston2, D. Vaniman27, and R. Williams27 • Combined analysis of chemistry and texture highlights the role of 1Laboratoire de Planétologie et Géodynamique de Nantes, CNRS, Université de Nantes, Nantes, France, 2Institut de Recherche diagenesis en Astrophysique et Planétologie, CNRS/Université de Toulouse, UPS-OMP, Toulouse, France, 3Laboratoire de Géologie de • Distinct chemistry in upper layers 4 5 suggests distinct setting and/or Lyon, Université de Lyon, Lyon, France, California Institute of Technology, Pasadena, California, USA, Los Alamos National 6 source Laboratory, Los Alamos, New Mexico, USA, Earth and Planetary Sciences, University of California, Davis, California, USA, 7Astrogeology Science Center, U.S. -
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. -
ROVING ACROSS MARS: SEARCHING for EVIDENCE of FORMER HABITABLE ENVIRONMENTS Michael H
PERSPECTIVE ROVING ACROSS MARS: SEARCHING FOR EVIDENCE OF FORMER HABITABLE ENVIRONMENTS Michael H. Carr* My love affair with Mars started in the late 1960s when I was appointed a member of the Mariner 9 and Viking Orbiter imaging teams. The global surveys of these two missions revealed a geological wonderland in which many of the geological processes that operate here on Earth operate also on Mars, but on a grander scale. I was subsequently involved in almost every Mars mission, both US and non- US, through the early 2000s, and wrote several books on Mars, most recently The Surface of Mars (Carr 2006). I also participated extensively in NASA’s long-range strategic planning for Mars exploration, including assessment of the merits of various techniques, such as penetrators, Mars rovers showing their evolution from 1996 to the present day. FIGURE 1 balloons, airplanes, and rovers. I am, therefore, following the results In the foreground is the tethered rover, Sojourner, launched in 1996. On the left is a model of the rovers Spirit and Opportunity, launched in 2004. from Curiosity with considerable interest. On the right is Curiosity, launched in 2011. IMAGE CREDIT: NASA/JPL-CALTECH The six papers in this issue outline some of the fi ndings of the Mars rover Curiosity, which has spent the last two years on the Martian surface looking for evidence of past habitable conditions. It is not the fi rst rover to explore Mars, but it is by far the most capable (FIG. 1). modest-sized landed vehicles. Advances in guidance enabled landing Included on the vehicle are a number of cameras, an alpha particle at more interesting and promising places, and advances in robotics led X-ray spectrometer (APXS) for contact elemental composition, a spec- to vehicles with more independent capabilities. -
List of Missions Using SPICE (PDF)
1/7/20 Data Restorations Selected Past Users Current/Pending Users Examples of Possible Future Users Apollo 15, 16 [L] Magellan [L] Cassini Orbiter NASA Discovery Program Mariner 2 [L] Clementine (NRL) Mars Odyssey NASA New Frontiers Program Mariner 9 [L] Mars 96 (RSA) Mars Exploration Rover Lunar IceCube (Moorehead State) Mariner 10 [L] Mars Pathfinder Mars Reconnaissance Orbiter LunaH-Map (Arizona State) Viking Orbiters [L] NEAR Mars Science Laboratory Luna-Glob (RSA) Viking Landers [L] Deep Space 1 Juno Aditya-L1 (ISRO) Pioneer 10/11/12 [L] Galileo MAVEN Examples of Users not Requesting NAIF Help Haley armada [L] Genesis SMAP (Earth Science) GOLD (LASP, UCF) (Earth Science) [L] Phobos 2 [L] (RSA) Deep Impact OSIRIS REx Hera (ESA) Ulysses [L] Huygens Probe (ESA) [L] InSight ExoMars RSP (ESA, RSA) Voyagers [L] Stardust/NExT Mars 2020 Emmirates Mars Mission (UAE via LASP) Lunar Orbiter [L] Mars Global Surveyor Europa Clipper Hayabusa-2 (JAXA) Helios 1,2 [L] Phoenix NISAR (NASA and ISRO) Proba-3 (ESA) EPOXI Psyche Parker Solar Probe GRAIL Lucy EUMETSAT GEO satellites [L] DAWN Lunar Reconnaissance Orbiter MOM (ISRO) Messenger Mars Express (ESA) Chandrayan-2 (ISRO) Phobos Sample Return (RSA) ExoMars 2016 (ESA, RSA) Solar Orbiter (ESA) Venus Express (ESA) Akatsuki (JAXA) STEREO [L] Rosetta (ESA) Korean Pathfinder Lunar Orbiter (KARI) Spitzer Space Telescope [L] [L] = limited use Chandrayaan-1 (ISRO) New Horizons Kepler [L] [S] = special services Hayabusa (JAXA) JUICE (ESA) Hubble Space Telescope [S][L] Kaguya (JAXA) Bepicolombo (ESA, JAXA) James Webb Space Telescope [S][L] LADEE Altius (Belgian earth science satellite) ISO [S] (ESA) Armadillo (CubeSat, by UT at Austin) Last updated: 1/7/20 Smart-1 (ESA) Deep Space Network Spectrum-RG (RSA) NAIF has or had project-supplied funding to support mission operations, consultation for flight team members, and SPICE data archive preparation. -
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, -
JSC-Rocknest: a Large-Scale Mojave Mars Simulant (MMS) Based Soil Simulant for In-Situ
1 JSC-Rocknest: A large-scale Mojave Mars Simulant (MMS) based soil simulant for in-situ 2 resource utilization water-extraction studies 3 Clark, J.V.a*, Archer, P.D.b, Gruener, J.E.c, Ming, D.W.c, Tu, V.M.b, Niles, P.B.c, Mertzman, 4 S.A.d 5 a GeoControls Systems, Inc – Jacobs JETS Contract at NASA Johnson Space Center, 2101 6 NASA Pkwy, Houston, TX 77058, USA. [email protected], 281-244-7442 7 b Jacobs JETS Contract at NASA Johnson Space Center, 2101 NASA Pkwy, Houston, TX 8 77058, USA. 9 c NASA Johnson Space Center, 2101 NASA Pkwy, Houston, TX 77058, USA. 10 d Department of Earth and Environmental, Franklin & Marshall College, Lancaster, PA 17604, 11 USA. 12 *Corresponding author 13 14 15 16 17 18 19 Keywords: Simulant, Mars, In-situ resource utilization, evolved gas analysis, Rocknest 1 20 Abstract 21 The Johnson Space Center-Rocknest (JSC-RN) simulant was developed in response to a 22 need by NASA's Advanced Exploration Systems (AES) In-Situ Resource Utilization (ISRU) 23 project for a simulant to be used in component and system testing for water extraction from Mars 24 regolith. JSC-RN was designed to be chemically and mineralogically similar to material from the 25 aeolian sand shadow named Rocknest in Gale Crater, particularly the 1-3 wt.% low temperature 26 (<450 ºC) water release as measured by the Sample Analysis at Mars (SAM) instrument on the 27 Curiosity rover. Sodium perchlorate, goethite, pyrite, ferric sulfate, regular and high capacity 28 granular ferric oxide, and forsterite were added to a Mojave Mars Simulant (MMS) base in order 29 to match the mineralogy, evolved gases, and elemental chemistry of Rocknest. -
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 -
A Miniaturized Chemin Xrd/Xrf for Future Mars Exploration
Ninth International Conference on Mars 2019 (LPI Contrib. No. 2089) 6230.pdf A MINIATURIZED CHEMIN XRD/XRF FOR FUTURE MARS EXPLORATION. B. Lafuente1, P. Sarrazin1, T. F. Bristow2, D. F. Blake2, M. Gailhanou3, J. Chen4, K. Thompson1, R. Walroth2, K. Zacny5, R. T. Downs6, and A. Yen7, 1SETI Institute, Mountain View, CA ([email protected]), 2Exobiology, NASA ARC, Moffett Field, CA, 3CNRS, IM2NP UMR, Marseille, France, 4Baja Technology, Tempe, AZ, 5Honeybee Robotics Spacecraft Mecha- nisms Corp., Pasadena, CA, 6Geosciences, Univ. Arizona, Tucson AZ, 7JPL, Pasadena, CA. Introduction: X-ray Diffraction (XRD) and X-ray ergy-selective detection of XRD photons in Mars’ ra- Fluorescence (XRF) analyses provide the most diag- diative environment. The CheMinX XRD geometry is nostic and complete characterization of rocks and soil based on an architecture demonstrated by hundreds of by any spacecraft-capable technique, improved upon commercial XRD instruments (Terra, commercial spin- only by sample return and analysis in terrestrial labora- off of CheMin, Fig. 1). This design resulted from a tories. In a complex sample such as a basalt, XRD can ray-tracing study of XRD geometries based on high as- definitively identify and quantify all minerals, establish pect-ratio detectors. It was found that reduced surface their individual elemental compositions and quantify area detectors can be used with no loss in throughput, the amount of the amorphous component. When cou- angular resolution or angular range, the loss in detector pled with XRF, the composition of the amorphous coverage being fully compensated for by an optimized component can be determined as well. collimator design. The MSL CheMin instrument, the first XRD instru- In its basic implementation CheMinX will provide ment flown in space, established the quantitative min- a resolution of 0.3° 2θ FWHM, slightly improved over eralogy of the Mars soil [1], characterized the first hab- CheMin’s 0.35°. -
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 -
Managing Software Development – the Hidden Risk * Dr
Managing Software Development – The Hidden Risk * Dr. Steve Jolly Sensing & Exploration Systems Lockheed Martin Space Systems Company *Based largely on the work: “Is Software Broken?” by Steve Jolly, NASA ASK Magazine, Spring 2009; and the IEEE Fourth International Conference of System of Systems Engineering as “System of Systems in Space 1 Exploration: Is Software Broken?”, Steve Jolly, Albuquerque, New Mexico June 1, 2009 Brief history of spacecraft development • Example of the Mars Exploration Program – Danger – Real-time embedded systems challenge – Fault protection 2 Robotic Mars Exploration 2011 Mars Exploration Program Search: Search: Search: Determine: Characterize: Determine: Aqueous Subsurface Evidence for water Global Extent Subsurface Bio Potential Minerals Ice Found Found of Habitable Ice of Site 3 Found Environments Found In Work Image Credits: NASA/JPL Mars: Easy to Become Infamous … 1. [Unnamed], USSR, 10/10/60, Mars flyby, did not reach Earth orbit 2. [Unnamed], USSR, 10/14/60, Mars flyby, did not reach Earth orbit 3. [Unnamed], USSR, 10/24/62, Mars flyby, achieved Earth orbit only 4. Mars 1, USSR, 11/1/62, Mars flyby, radio failed 5. [Unnamed], USSR, 11/4/62, Mars flyby, achieved Earth orbit only 6. Mariner 3, U.S., 11/5/64, Mars flyby, shroud failed to jettison 7. Mariner 4, U.S. 11/28/64, first successful Mars flyby 7/14/65 8. Zond 2, USSR, 11/30/64, Mars flyby, passed Mars radio failed, no data 9. Mariner 6, U.S., 2/24/69, Mars flyby 7/31/69, returned 75 photos 10. Mariner 7, U.S., 3/27/69, Mars flyby 8/5/69, returned 126 photos 11.