Helios Spacecraft Data Revisited: Detection of Cometary Meteoroid
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
AE Newsletter 2020
Colonel Shorty Powers Composite Squadron July 25, 2020 AEROSPACE Aircraft | Spacecraft | Biography | Squadron Gen. Ira C. Eaker A New Eagle Boeing to build new F-15EXs for USAF The Department of the Air Force and Boeing recently signed a deal worth 1.2 billion dollars for the first lot of eight F-15EX jets that will be delivered to Eglin Air Force Base, Florida. The aircraft will replace the oldest F-15Cs and F-15Ds in the U.S. Air Force fleet. The first two already built F-15EX aircraft will be delivered during the second quarter of 2021, while the remaining aircraft will be delivered in 2023. The Air Force plans to buy 76 F-15EX aircraft. The new F-15EX was developed to meet needs identified by the National Defense Strategy review which directed the U.S. armed services to adapt to the new threats from China and Russia. The most burdensome requirement is the need for the Air Force to add 74 new squadrons to the existing 312 squadrons by 2030. The General Ira C. Eaker was one of the forefathers of an independent Air Force. With General (then major) Spaatz, in 1929 Eaker remained aloft aboard The Question Mark, a modified Atlantic-Fokker C-2A, for nearly a week, to demonstrate a newfound capability of aerial refueling. During WWII, Eaker rose to the grade of lieutenant general and commanded the Eighth Air Force, "The Mighty Eighth" force of strategic The first F-15EX being assembled at Boeing facilities. (Photo: Boeing) Aerospace Newsletter 1 Colonel Shorty Powers Composite Squadron July 25, 2020 Eaker (continued) Air Force also seeks to lower the average aircraft age of 28 years down to 15 years without losing any capacity. -
Ulysses Awardees
Ulysses Awardees Irish Higher Project Leader - Project Leader - French Higher Funding Education Disciplinary Area Project Title Ireland France Education Institution Institution Comparing Laws with Help from Humanities including Peter Arnds IRC / Embassy TCD Renaud Colson ENSCM, Montpellier the Humanities: Translation Theory languages, Law to the Rescue of Legal Studies Novel biomarkers of interplay between neuroglobin and George Barreto HRB / Embassy UL Karim Belarbi Université de Nantes Life Sciences neuroinflammation in Parkinson’s disease Geometric Constructions of Codes Eimear Byrne IRC / Embassy UCD Martino Borello University of Lille Mathematics for Secret Sharing Schemes BOUHÉREAU: EXILE, TOLERATION Didier Poton de Humanities including Derval Conroy IRC / Embassy UCD University Paris 8 - LAGA AND CARE IN THE EARLY MODERN Xaintrailles languages PERIOD Knotting peptides for DNA Fabian Cougnon IRC / Embassy NUIG Sebastian Ulrich La Rochelle University Chemistry recognition and gene delivery Automating Segmentation and Computer Science & Kathleen Curran HRB / Embassy UCD David Bendahan Muscle Architecture Analysis from Telecommunications Aix Marseille University Diffusion Tensor Imaging The Impact of Student Exchanges Social science and Ronald Davies IRC / Embassy UCD Farid Toubal on International Trade: The Role of University of Paris- economics Cultural Similarity Dauphine -- PSL Computer Science & Three dimensional audio and Gordon Delap IRC / Embassy MU Thibaud Keller Telecommunications musical experimentation CNRS – LaBRI Multi-scale, -
General Disclaimer One Or More of the Following Statements May Affect
General Disclaimer One or more of the Following Statements may affect this Document This document has been reproduced from the best copy furnished by the organizational source. It is being released in the interest of making available as much information as possible. This document may contain data, which exceeds the sheet parameters. It was furnished in this condition by the organizational source and is the best copy available. This document may contain tone-on-tone or color graphs, charts and/or pictures, which have been reproduced in black and white. This document is paginated as submitted by the original source. Portions of this document are not fully legible due to the historical nature of some of the material. However, it is the best reproduction available from the original submission. Produced by the NASA Center for Aerospace Information (CASI) NASA Technical Memorandum 85094 SOLAR RADIO BURST AND IN SITU DETERMINATION OF INTERPLANETARY ELECTRON DENSITY (NASA-^'M-85094) SOLAR RADIO BUFST AND IN N83-35989 SITU DETERMINATION OF INTEFPIAKETARY ELECTRON DENSITY SNASA) 26 p EC A03/MF A01 CSCL 03B Unclas G3/9.3 492134 J. L. Bougeret, J. H. King and R. Schwenn OCT Y'183 RECEIVED NASA Sri FACIUTY ACCESS DEPT. September 1883 I 3 National Aeronautics and Space Administration Goddard Spne Flight Center Greenbelt, Maryland 20771 k it R ^ f A SOLAR RADIO BURST AND IN SITU DETERMINATION OF INTERPLANETARY ELECTRON DENSITY J.-L. Bou eret * J.H. Kinr ^i Laboratory for Extraterrestrial Physics, NASA/Goddard Space Flight. Center, Greenbelt, Maryland 20771, U.S.A. and R. Schwenn Max-Planck-Institut fOr Aeronomie, Postfach 20, D-3411 Katlenburg-Lindau, Federal Republic of Germany - 2 - °t i t: ABSTRACT i • We review and discuss a few interplanetary electron density scales which have been derived from the analysis of interplanetary solar radio bursts, and we compare them to a model derived from 1974-1980 Helioi 1 and 2 in situ i i density observations made in the 0.3-1.0 AU range. -
Let's Go to a Comet!
Mission Rosetta Let’s go to a comet! Elsa Montagnon European Space Agency 1 What is left to explore today? 15th century Credits: ESA/AOES Medialab 21st century 2 Back to the origins… 3 What has happened since the big bang? Big bang 13 billion years ago ejects hydrogen and helium From elements to dust From water to heavy elements From dust to gas From solar cloud to the solar system: planets, asteroids, comets 4 How do we see the solar system today? Galactic Tides Nearby Stars Large Clouds LPidCtLong Period Comets Short Period Comets Galactic Tides Inner Outer Oort Oort Pluto Cloud Cloud ? Stable Stable Kuiper Belt 10 Gy 1 Gy ? 10 50 100 Alpha I, e 1000 Centauri 10^4 Ejected AU 10^5 3.10^5 5 Where are we going? Comet 67P / Churyumow-Gerasimenko 3-D reconstruction of nucleus based on 12 March, 2003 Hubble Space Telescope observations Nucleus diameter: 4km Discovered in 1969 Orbital period: 6.6 years Pole End Side Nasa, Esa and Philippe Lamy (Laboratoire d’Astrobomie Spatiale) - STScl-PRC03-26 6 A picture of the comet… Credits: ESA and European Southern Observatory 7 The Mission Rendezvous with the comet shortly after aphelion Follow the comet up to perihelion and beyond Deploy a lander on the comet surface QuickTime™ and a YUV420 codec decompressor are needed to see this picture. 8 The Journey Launch: March 2004 Launcher: Ariane 5 Rendezvous with comet: August 2014 Distance: 6.5 billions km Cruise duration: 10 years Mission duration: 2 years 9 The Cruise The comet is very far away. -
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. -
Solar Orbiter Assessment Study and Model Payload
Solar Orbiter assessment study and model payload N.Rando(1), L.Gerlach(2), G.Janin(4), B.Johlander(1), A.Jeanes(1), A.Lyngvi(1), R.Marsden(3), A.Owens(1), U.Telljohann(1), D.Lumb(1) and T.Peacock(1). (1) Science Payload & Advanced Concepts Office, (2) Electrical Engineering Department, (3) Research and Scientific Support Department, European Space Agency, ESTEC, Postbus 299, NL-2200AG, Noordwijk, The Netherlands (4) Mission Analysis Office, European Space Agency, ESOC, Darmstadt, Germany ABSTRACT The Solar Orbiter mission is presently in assessment phase by the Science Payload and Advanced Concepts Office of the European Space Agency. The mission is confirmed in the Cosmic Vision programme, with the objective of a launch in October 2013 and no later than May 2015. The Solar Orbiter mission incorporates both a near-Sun (~0.22 AU) and a high-latitude (~ 35 deg) phase, posing new challenges in terms of protection from the intense solar radiation and related spacecraft thermal control, to remain compatible with the programmatic constraints of a medium class mission. This paper provides an overview of the assessment study activities, with specific emphasis on the definition of the model payload and its accommodation in the spacecraft. The main results of the industrial activities conducted with Alcatel Space and EADS-Astrium are summarized. Keywords: Solar physics, space weather, instrumentation, mission assessment, Solar Orbiter 1. INTRODUCTION The Solar Orbiter mission was first discussed at the Tenerife “Crossroads” workshop in 1998, in the framework of the ESA Solar Physics Planning Group. The mission was submitted to ESA in 2000 and then selected by ESA’s Science Programme Committee in October 2000 to be implemented as a flexi-mission, with a launch envisaged in the 2008- 2013 timeframe (after the BepiColombo mission to Mercury) [1]. -
ESA & ESOC Overview
NASA PM Challenge 2010 Developing the International Program/Project Management Community 9/10 February 2010 Dr. Bettina Böhm Program & Project Manager Career at ESA | Bettina Böhm | ESA/HQ | 23/11/09 | Page 1 Used with Permission PURPOSE OF ESA / ACTIVITIES “To provide for and promote, for exclusively Space science peaceful purposes, cooperation among Human spaceflight European states in space research and Exploration technology and their space applications.” Earth observation Launchers [Article 2 of ESA Convention] Navigation ESA is one of the few space agencies Telecommunications in the world to combine responsibility Technology in all areas of space activity. Operations Program & Project Manager Career at ESA | Bettina Böhm | ESA/HQ | 23/11/09 | Page 2 ESA FACTS AND FIGURES Over 30 years of experience 18 Member States 2080 staff, thereof 880 in Program Directorates, 790 in Operations and Technical Support and 410 in other Support Directorates 3 500 million Euros budget Over 60 satellites designed and tested Over 60 satellites operated in-flight and 8 missions rescued 16 scientific satellites in operation Five types of launcher developed More than 180 launches made Program & Project Manager Career at ESA | Bettina Böhm | ESA/HQ | 23/11/09 | Page 3 ESA Locations EAC (Cologne) Salmijaervi ESTEC Astronaut training (Noordwijk) Satellite technology development and testing Harwell ESOC ESA HQ (Darmstadt) (Paris) Brussels Satellite operations and ground system technology development ESAC (Villanueva de la Cañada Oberpfaffenhofen -
Radial Variation of the Interplanetary Magnetic Field Between 0.3 AU and 1.0 AU
|00000575|| J. Geophys. 42, 591 - 598, 1977 Journal of Geophysics Radial Variation of the Interplanetary Magnetic Field between 0.3 AU and 1.0 AU Observations by the Helios-I Spacecraft G. Musmann, F.M. Neubauer and E. Lammers Institut for Geophysik and Meteorologie, Technische Universitiit Braunschweig, Mendelssohnstr. lA, D-3300 Braunschweig, Federal Republic of Germany Abstract. We have investigated the radial dependence of the radial and azimuthal components and the magnitude of the interplanetary magnetic field obtained by the Technical University of Braunschweig magnetometer experiment on-board of Helios-1 from December 10, 1974 to first perihelion on March 15, 1975. Absolute values of daily averages of each quantity have been employed. The regression analysis based on power laws leads to 2.55 y x r- 2 · 0 , 2.26 y x r- i.o and F = 5.53 y x r- i. 6 with standard deviations of 2.5 y, 2.0 y and 3.2 y for the radial and azimuthal components and magnitude, respectively. Here r is the radial distance from the sun in astronomical units. The results are compared with results obtained for Mariners 4, 5 and 10 and Pioneers 6 and 10. The differences are probably due to different epochs in the solar cycle and the different statistical techniques used. Key words: Interplanetary magnetic field - Helios-1 results. Introduction The study of the vanat10n of the components and magnitude of the in terplanetary magnetic field with heliocentric distance is very intersting at the present time. The mission of Mariner 10 to the inner solar system to a heliocentric distance of 0.46 AU and the missions of Pioneer 10 and Pioneer 11 to the outer solar system to heliocentric distances beyond 5 AU have provided new data over a wide range of heliocentric distance. -
(IES) Measurement of the Development of Pickup Ions from Comet 67P/Churyumov-Gerasimenko
PUBLICATIONS Geophysical Research Letters RESEARCH LETTER The Rosetta Ion and Electron Sensor (IES) measurement 10.1002/2015GL063939 of the development of pickup ions from comet Key Point: 67P/Churyumov-Gerasimenko • IES observed low-energy ions in August 2014, at an 80 km distance R. Goldstein1, J. L. Burch1, P. Mokashi1, T. Broiles1, K. Mandt1, J. Hanley1, T. Cravens2, A. Rahmati2, from the comet M. Samara3, G. Clark3, M. Hässig1,4, and J. M. Webster1 1Southwest Research Institute, San Antonio, Texas, USA, 2Physics and Astronomy, University of Kansas, Lawrence, Kansas, USA, 3 4 Correspondence to: NASA Goddard Space Flight Center, Greenbelt, Maryland, USA, Physikalisches Institut, University of Bern, Bern, Switzerland R. Goldstein, [email protected] Abstract The Rosetta Ion and Electron Sensor (IES) has been measuring solar wind ions intermittently since exiting from hibernation in May 2014. On 19 August, when Rosetta was ~80 km from the comet Citation: Goldstein, R., et al. (2015), The Rosetta Ion 67P/Churyumov-Gerasimenko, which was ~3.5 AU from the Sun, IES began to see ions at its lowest energy and Electron Sensor (IES) measurement range, ~4–10 eV. We identify these as ions created from neutral species emitted by the comet nucleus, of the development of pickup ions from photoionized by solar UV radiation in the neighborhood of the Rosetta spacecraft (S/C), and attracted by the comet 67P/Churyumov-Gerasimenko, Geophys. Res. Lett., 42,3093–3099, small negative potential of the S/C resulting from the population of thermal electrons. Later, IES began to doi:10.1002/2015GL063939. see higher-energy ions that we identify as having been picked up and accelerated by the solar wind. -
Exploring the Solar Poles and the Heliosphere from High Helio-Latitude
A white paper submitted to ESA for the Voyage 2050 long- term plan ? A journey to the polar regions of a star: Exploring the solar poles and the heliosphere from high helio-latitude Louise Harra ([email protected]) and the solar polar team PMOC/WRC, Dorfstrasse 33, CH-7260 Davos Dorf & ETH-Zürich, Switzerland [Image: Polar regions of major Solar System bodies. Top left, clockwise - Near-surface zonal flows around the solar north pole Bogart et al. (2015); Earth’s changing magnetic field from ESA’s Swarm constellation; Southern polar cap of Mars from ESA’s ExoMars; Jupiter’s poles from the NASA Juno mission; Saturn’s poles from the NASA Cassini mission.] Overview We aim to embark on one of humankind’s great journeys – to travel over the poles of our star, with a spacecraft unprecedented in its technology and instrumentation – to explore the polar regions of the Sun and their effect on the inner heliosphere in which we live. The polar vantage point provides a unique opportunity for major scientific advances in the field of heliophysics, and thus also provides the scientific underpinning for space weather applications. It has long been a scientific goal to study the poles of the Sun, illustrated by the NASA/ESA International Solar Polar Mission that was proposed over four decades ago, which led to the flight of ESA’s Ulysses spacecraft (1990 to 2009). Indeed, with regard to the Earth, we took the first tentative steps to explore the Earth’s polar regions only in the 1800s. Today, with the aid of space missions, key measurements relating to the nature and evolution of Earth’s polar regions are being made, providing vital input to climate-change models. -
Alejandro Cardesín Moinelo ESA Science Operations Center Mars Express & Exomars 2016 (Slides Courtesy of Christian Erd & Peter Falkner, ESA-ESTEC)
Alejandro Cardesín Moinelo ESA Science Operations Center Mars Express & ExoMars 2016 (slides courtesy of Christian Erd & Peter Falkner, ESA-ESTEC) ESAC, 7th February 2017 Mission Flow Diagram Slide 2 Space Mission Timeline: Phases Slide 3 Science Mission Design Process Slide 4 Science Objectives – Requirements - Solutions Science Objective is the high level motivation • Which scientific question/application purpose shall the WHY? project address and what answer is sought Requirement is the translation of this objective into verifiable statements of what is needed to achieve the objective With detailed quantities (unambiguous) • WHAT? • Several levels of detail • Traceable, all the way back to the top level • Careful with conflicting requirements Solution is the response to the all requirements • There can be several solutions meeting requirements HOW? • Non-compliance needs to be negotiated Slide 5 Conflicting Requirements Farm “Optimal” Animal : Eierlegende Wollmilchsau (famous Austrian animal) Slide 6 Trade-off Trade-off allows exploring alternative solutions to a baseline Most common criteria: mass, cost budget; several System Performance system properties can be translated into them Power consumption generation of more power solar array size mass Higher telemetry volume larger HGA, more power for TM&C mass High performance complex solutions Cost more effort for verification Mass longer integration time cost Slide 7 Mission Segments, Systems & Subsystems Slide 8 Mission Analysis Launch Transfer trajectory Insertion into -
Abundances 164 ACE (Advanced Composition Explorer) 1, 21, 60, 71
Index abundances 164 CIR (corotating interaction region) 3, ACE (Advanced Composition Explorer) 1, 14À15, 32, 36À37, 47, 62, 108, 151, 21, 60, 71, 170À171, 173, 175, 177, 254À255 200, 251 energetic particles 63, 154 SWICS 43, 86 Climax neutron monitor 197 ACRs (anomalous cosmic rays) 10, 12, 197, CME (coronal mass ejection) 3, 14À15, 56, 258À259 64, 86, 93, 95, 123, 256, 268 CIRs 159 composition 268 pickup ions 197 open flux 138 termination shock 197, 211 comets 2À4, 11 active longitude 25 ComptonÀGetting effect 156 active region 25 convection equation tilt 25 diffusion 204 activity cycle (see also solar cycle) 1À2, corona 1À2 11À12 streamers 48, 63, 105, 254 Advanced Composition Explorer see ACE temperature 42 Alfve´n waves 116, 140, 266 coronal hole 30, 42, 104, 254, 265 AMPTE (Active Magnetospheric Particle PCH (polar coronal hole) 104, 126, 128 Tracer Explorer) mission 43, 197, coronal mass ejections see CME 259 corotating interaction regions see CIR anisotropy telescopes (AT) 158 corotating rarefaction region see CRR Cosmic Ray and Solar Particle Bastille Day see flares Investigation (COSPIN) 152 bow shock 10 cosmic ray nuclear composition (CRNC) butterfly diagram 24À25 172 cosmic rays 2, 16, 22, 29, 34, 37, 195, 259 Cassini mission 181 anomalous 195 CELIAS see SOHO charge state 217 CH see coronal hole composition 196, 217 CHEM 43 convection–diffusion model 213 282 Index cosmic rays (cont.) Energetic Particle Composition Experiment drift 101, 225 (EPAC) 152 force-free approximation 213 energetic particle 268 galactic 195 anisotropy 156,