Neutral Winds in the Lower Thermosphere from Dynamics Explorer 2
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University of Iowa Instruments in Space
University of Iowa Instruments in Space A-D13-089-5 Wind Van Allen Probes Cluster Mercury Earth Venus Mars Express HaloSat MMS Geotail Mars Voyager 2 Neptune Uranus Juno Pluto Jupiter Saturn Voyager 1 Spaceflight instruments designed and built at the University of Iowa in the Department of Physics & Astronomy (1958-2019) Explorer 1 1958 Feb. 1 OGO 4 1967 July 28 Juno * 2011 Aug. 5 Launch Date Launch Date Launch Date Spacecraft Spacecraft Spacecraft Explorer 3 (U1T9)58 Mar. 26 Injun 5 1(U9T68) Aug. 8 (UT) ExpEloxrpelro r1e r 4 1915985 8F eJbu.l y1 26 OEGxOpl o4rer 41 (IMP-5) 19697 Juunlye 2 281 Juno * 2011 Aug. 5 Explorer 2 (launch failure) 1958 Mar. 5 OGO 5 1968 Mar. 4 Van Allen Probe A * 2012 Aug. 30 ExpPloiorenre 3er 1 1915985 8M Oarc. t2. 611 InEjuxnp lo5rer 45 (SSS) 197618 NAouvg.. 186 Van Allen Probe B * 2012 Aug. 30 ExpPloiorenre 4er 2 1915985 8Ju Nlyo 2v.6 8 EUxpKlo 4r e(rA 4ri1el -(4IM) P-5) 197619 DJuenc.e 1 211 Magnetospheric Multiscale Mission / 1 * 2015 Mar. 12 ExpPloiorenre 5e r 3 (launch failure) 1915985 8A uDge.c 2. 46 EPxpiolonreeerr 4130 (IMP- 6) 19721 Maarr.. 313 HMEaRgCnIe CtousbpeShaetr i(cF oMxu-1ltDis scaatelell itMe)i ssion / 2 * 2021081 J5a nM. a1r2. 12 PionPeioenr e1er 4 1915985 9O cMt.a 1r.1 3 EExpxlpolorerer r4 457 ( S(IMSSP)-7) 19721 SNeopvt.. 1263 HMaalogSnaett oCsupbhee Sriact eMlluitlet i*scale Mission / 3 * 2021081 M5a My a2r1. 12 Pioneer 2 1958 Nov. 8 UK 4 (Ariel-4) 1971 Dec. 11 Magnetospheric Multiscale Mission / 4 * 2015 Mar. -
A Comparison Study on Thermal Control Techniques for a Nanosatellite Carrying Infrared Science Instrument
ICES-2020-15 A comparison study on thermal control techniques for a nanosatellite carrying infrared science instrument Shanmugasundaram Selvadurai1, Amal Chandran2, Sunil C Joshi3 and Teo Hang Tong Edwin 4 Nanyang Technological University, Singapore, 639798 David Valentini5 Thales Alenia Space, Cannes, 06150, France Friedhelm Olschewski6 University of Wuppertal, 42119 Wuppertal, Germany Based on current technological advancements and forecasts, nanosatellites will be used for both scientific and defense applications leveraging advantages on both development cost and development lifecycle. As nanosatellites become more capable, there is an increase in demand for high power applications which makes the missions complex from implementing a proper thermal control system (TCS) to dissipate the huge waste heat generated. One of the applications for nanosatellites is advanced infrared imaging for both scientific and military applications. ARCADE (Atmospheric coupling and Dynamics Explorer), a 27U satellite is being developed by Satellite Research Centre (SaRC) at Nanyang Technological University (NTU) for scientific objectives. The main payload AtmoLITE needs a detector cool down at -30°C and to meet this requirement, an appropriate classical TCS is chosen and described in this paper. Nanosatellites carrying infrared, cryogenic or other scientific instruments that need active cooling, should be equipped with a proper TCS within the highly constrained available volume. Another objective of this study is to compare the existing TCS for nanosatellites and adopt a suitable and efficient TCS for a scientific nanosatellite mission carrying a generic science instrument that needs an active cooling of up to 95K. TCS using Heat pipes (HP), single-phase mechanically pumped fluid loop (SMPFL), and two-phase mechanically pumped fluid loop systems (2ΦMPFL) have been extensively used only by larger satellites. -
Cubesat-Based Science Missions for Geospace and Atmospheric Research
National Aeronautics and Space Administration NATIONAL SCIENCE FOUNDATION (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH annual report October 2013 www.nasa.gov www.nsf.gov LETTERS OF SUPPORT 3 CONTACTS 5 NSF PROGRAM OBJECTIVES 6 GSFC WFF OBJECTIVES 8 2013 AND PRIOR PROJECTS 11 Radio Aurora Explorer (RAX) 12 Project Description 12 Scientific Accomplishments 14 Technology 14 Education 14 Publications 15 Contents Colorado Student Space Weather Experiment (CSSWE) 17 Project Description 17 Scientific Accomplishments 17 Technology 18 Education 18 Publications 19 Data Archive 19 Dynamic Ionosphere CubeSat Experiment (DICE) 20 Project Description 20 Scientific Accomplishments 20 Technology 21 Education 22 Publications 23 Data Archive 24 Firefly and FireStation 26 Project Description 26 Scientific Accomplishments 26 Technology 27 Education 28 Student Profiles 30 Publications 31 Cubesat for Ions, Neutrals, Electrons and MAgnetic fields (CINEMA) 32 Project Description 32 Scientific Accomplishments 32 Technology 33 Education 33 Focused Investigations of Relativistic Electron Burst, Intensity, Range, and Dynamics (FIREBIRD) 34 Project Description 34 Scientific Accomplishments 34 Education 34 2014 PROJECTS 35 Oxygen Photometry of the Atmospheric Limb (OPAL) 36 Project Description 36 Planned Scientific Accomplishments 36 Planned Technology 36 Planned Education 37 (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH [ 1 QB50/QBUS 38 Project Description 38 Planned Scientific Accomplishments 38 Planned -
Chandra-Hetgs Characterization of an Outflowing Wind in the Accreting Millisecond Pulsar Igr J17591−2342
Draft version February 27, 2019 Typeset using LATEX twocolumn style in AASTeX61 CHANDRA-HETGS CHARACTERIZATION OF AN OUTFLOWING WIND IN THE ACCRETING MILLISECOND PULSAR IGR J17591−2342 Michael A. Nowak,1 Adamantia Paizis,2 Gaurava Kumar Jaisawal,3 Jer´ ome^ Chenevez,3 Sylvain Chaty,4 Francis Fortin,4 Jer´ ome^ Rodriguez,4 andJ orn¨ Wilms5 1Physics Dept., CB 1105, Washington University, One Brookings Drive, St. Louis, MO 63130-4899 2Istituto Nazionale di Astrofisica, INAF-IASF, Via Alfonso Corti 12, I-20133 Milano, Italy 3National Space Institute, Technical University of Denmark, Elektrovej 327-328, DK-2800 Lyngby, Denmark 4AIM, CEA, CNRS, Universit´eParis-Saclay, Universit´eParis-Diderot, Sorbonne Paris Cit´e,F-91191 Gif sur Yvette, France 5Dr. Karl Remeis-Observatory & ECAP, University of Erlangen-Nuremberg, Sternwartstr. 7, 96049 Bamberg, Germany (Received 2019 January; Accepted 2019 February) Submitted to ApJ ABSTRACT IGR J17591−2342 is an accreting millisecond X-ray pulsar discovered in 2018 August in scans of the Galactic bulge and center by the INTEGRAL X-ray and gamma-ray observatory. It exhibited an unusual outburst profile with multiple peaks in the X-ray, as observed by several X-ray satellites over three months. Here we present observations of this source performed in the X-ray/gamma-ray and near infrared domains, and focus on a simultaneous observation performed with the Chandra-High Energy Transmission Gratings Spectrometer (HETGS) and the Neutron Star Interior Composition Explorer (NICER). HETGS provides high resolution spectra of the Si-edge region, which yield clues as to the source's distance and reveal evidence (at 99.999% significance) of an outflow with a velocity of 2 800 km s−1. -
Final Release from the Extended Baryon
Draft version August 19, 2019 Preprint typeset using LATEX style emulateapj v. 12/16/11 THE SIXTEENTH DATA RELEASE OF THE SLOAN DIGITAL SKY SURVEYS: FINAL RELEASE FROM THE EXTENDED BARYON OSCILLATION SPECTROSCOPIC SURVEY, AND FIRST RELEASE FROM APOGEE-2S V´ıctor Silva Aguirre1, Romina Ahumada2, Carlos Allende Prieto3,4, Andres´ Almeida5, Friedrich Anders6,7, Scott F. Anderson8, Brett H. Andrews9, Borja Anguiano10, Riccardo Arcodia11, Marie Aubert12, Santiago Avila13,14, Vladimir Avila-Reese15, Christophe Balland16, Kat Barger17, Sarbani Basu18, Julian Bautista19, Rachael L. Beaton20, Timothy C. Beers21, Chad F. Bender22, Mariangela Bernardi23, Matthew Bershady24,25, Florian Beutler19, Dmitry Bizyaev26, Michael R. Blanton27,Med´ eric´ Boquien28, Jura Borissova29,30, Jo Bovy31,32, W.N. Brandt33,34,35, Jonathan Brinkmann26, Joel R. Brownstein36, Kevin Bundy37, Martin Bureau38, Adam Burgasser39, Mariana Cano-D´ıaz15, Raffaella Capasso40,41,42, Ricardo Carrera43, Solene` Chabanier44, Brian Cherinka45, Cristina Chiappini6, Peter Doohyun Choi46, Haeun Chung47, Nicolas Clerc48, Damien Coffey11, Julia M. Comerford49, Johan Comparat11, Luiz da Costa50,51, Marie-Claude Cousinou12, Kevin Covey52, Jeffrey D. Crane20, Katia Cunha51,22, Gabriele da Silva Ilha53,50, Yu Sophia Dai54, Sanna B. Damsted55, Danny Horta Darrington56, James W. Davidson Jr.10, Kyle Dawson36, Nikhil De57,17, Axel de la Macorra58, Nathan De Lee59, Alice Deconto Machado53,50, Sylvain de la Torre60, Flavia Dell'Agli3,4, Helion´ du Mas des Bourboux36, Aleksandar M. Diamond-Stanic61, Sean Dillon62,63, John Donor17, Niv Drory64, Chris Duckworth65, Tom Dwelly11, Garrett Ebelke10, Arthur Davis Eigenbrot24, Yvonne P. Elsworth66, Mike Eracleous33,34, Ghazaleh Erfanianfar11, Stephanie Escoffier12, Xiaohui Fan22, Emily Farr8, Jose´ G. Fernandez-Trincado´ 67,68, Diane Feuillet69, Alexis Finoguenov55, Patricia Fofie62,70, Amelia Fraser-McKelvie71, Peter M. -
THEMIS ESA First Science Results and Performance Issues
Space Sci Rev DOI 10.1007/s11214-008-9433-1 THEMIS ESA First Science Results and Performance Issues J.P. McFadden · C.W. Carlson · D. Larson · J. Bonnell · F. Mozer · V. Angelopoulos · K.-H. Glassmeier · U. Auster Received: 5 April 2008 / Accepted: 25 August 2008 © Springer Science+Business Media B.V. 2008 Abstract Early observations by the THEMIS ESA plasma instrument have revealed new details of the dayside magnetosphere. As an introduction to THEMIS plasma data, this pa- per presents observations of plasmaspheric plumes, ionospheric ion outflows, field line reso- nances, structure at the low latitude boundary layer, flux transfer events at the magnetopause, and wave and particle interactions at the bow shock. These observations demonstrate the ca- pabilities of the plasma sensors and the synergy of its measurements with the other THEMIS experiments. In addition, the paper includes discussions of various performance issues with the ESA instrument such as sources of sensor background, measurement limitations, and data formatting problems. These initial results demonstrate successful achievement of all measurement objectives for the plasma instrument. Keywords THEMIS · Magnetosphere · Magnetopause · Bow shock · Instrument performance PACS 94.80.+g · 06.20.Fb · 94.30.C- · 94.05.-a · 07.87.+v 1 Introduction The THEMIS mission provides the first multi-satellite measurements of the dayside mag- netosphere, magnetopause and bow shock utilizing a string of pearls orbit near the ecliptic plane (Angelopoulos 2008). During a 7 month coast phase, the instruments were commis- sioned and cross-calibrated while spacecraft separations were adjusted from a few hundred J.P. McFadden () · C.W. Carlson · D. -
ESA Space Weather STUDY Alcatel Consortium
ESA Space Weather STUDY Alcatel Consortium SPACE Weather Parameters WP 2100 Version V2.2 1 Aout 2001 C. Lathuillere, J. Lilensten, M. Menvielle With the contributions of T. Amari, A. Aylward, D. Boscher, P. Cargill and S.M. Radicella 1 2 1 INTRODUCTION........................................................................................................................................ 5 2 THE MODELS............................................................................................................................................. 6 2.1 THE SUN 6 2.1.1 Reconstruction and study of the active region static structures 7 2.1.2 Evolution of the magnetic configurations 9 2.2 THE INTERPLANETARY MEDIUM 11 2.3 THE MAGNETOSPHERE 13 2.3.1 Global magnetosphere modelling 14 2.3.2 Specific models 16 2.4 THE IONOSPHERE-THERMOSPHERE SYSTEM 20 2.4.1 Empirical and semi-empirical Models 21 2.4.2 Physics-based models 23 2.4.3 Ionospheric profilers 23 2.4.4 Convection electric field and auroral precipitation models 25 2.4.5 EUV/UV models for aeronomy 26 2.5 METEOROIDS AND SPACE DEBRIS 27 2.5.1 Space debris models 27 2.5.2 Meteoroids models 29 3 THE PARAMETERS ................................................................................................................................ 31 3.1 THE SUN 35 3.2 THE INTERPLANETARY MEDIUM 35 3.3 THE MAGNETOSPHERE 35 3.3.1 The radiation belts 36 3.4 THE IONOSPHERE-THERMOSPHERE SYSTEM 36 4 THE OBSERVATIONS ........................................................................................................................... -
The Swift Ultra-Violet/Optical Telescope
The Swift Ultra-Violet/Optical Telescope Peter W. A. Roming*a, Thomas E. Kennedyb, Keith O. Masonb, John A. Nouseka, Lindy Ahrc, Richard E. Binghamd, Patrick S. Broosa, Mary J. Carterb, Barry K. Hancockb, Howard E. Huckleb, S. D. Hunsbergera, Hajime Kawakamib, Ronnie Killoughc, T. Scott Kocha, Michael K. McLellandc, Kelly Smithc, Philip J. Smithb, Juan Carlos Soto†e, Patricia T. Boydf, Alice A. Breeveldb, Stephen T. Hollandf, Mariya Ivanushkinaa, Michael S. Pryzbyg, Martin D. Stillf, Joseph Stockg aDepartment of Astronomy & Astrophysics, Pennsylvania State University, 525 Davey Lab, University Park, PA 16802, USA bMullard Space Sciences Laboratory, University College London, Holmbury St. Mary, Dorking, Surrey RH5 6NT, UK cSouthwest Research Institute, 6220 Culebra Rd, San Antonio, TX 78228, USA dOptical Science Laboratory, University College London, Gower St, London WC1E 6BT, UK eStarsys Research Corporation, 4909 Nautilus Court N., Boulder, CO 80301, USA fNASA/Goddard Space Flight Center, Code 660.1, Greenbelt, MD 20771, USA gSwales Aerospace, 5050 Powder Mill Rd, Beltsville, MD 20705, USA ABSTRACT The UV/Optical Telescope (UVOT) is one of three instruments flying aboard the Swift Gamma-ray Observatory. It is designed to capture the early (~1 minute) UV and optical photons from the afterglow of gamma-ray bursts in the 170-600 nm band as well as long term observations of these afterglows. This is accomplished through the use of UV and optical broadband filters and grisms. The UVOT has a modified Ritchey-Chrétien design with micro-channel plate intensified charged-coupled device detectors that record the arrival time of individual photons and provide sub- arcsecond positioning of sources. -
For Low Earth Orbit Missions N
A Wide Field Auroral Imager (WFAI) for low Earth orbit missions N. P. Bannister, E. J. Bunce, S. W. H. Cowley, R. Fairbend, G. W. Fraser, F. J. Hamilton, J. S. Lapington, J. E. Lees, M. Lester, S. E. Milan, et al. To cite this version: N. P. Bannister, E. J. Bunce, S. W. H. Cowley, R. Fairbend, G. W. Fraser, et al.. A Wide Field Auroral Imager (WFAI) for low Earth orbit missions. Annales Geophysicae, European Geosciences Union, 2007, 25 (2), pp.519-532. hal-00330118 HAL Id: hal-00330118 https://hal.archives-ouvertes.fr/hal-00330118 Submitted on 8 Mar 2007 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Ann. Geophys., 25, 519–532, 2007 www.ann-geophys.net/25/519/2007/ Annales © European Geosciences Union 2007 Geophysicae A Wide Field Auroral Imager (WFAI) for low Earth orbit missions N. P. Bannister1, E. J. Bunce1, S. W. H. Cowley1, R. Fairbend2, G. W. Fraser1, F. J. Hamilton1, J. S. Lapington1, J. E. Lees1, M. Lester1, S. E. Milan1, J. F. Pearson1, G. J. Price1, and R. Willingale1 1Department of Physics & Astronomy, University of Leicester, University Road, Leicester, LE1 7RH, UK 2Photonis SAS, Avenue Roger Roncier, Brive, 19410 Cedex, France Received: 6 January 2006 – Revised: 12 December 2006 – Accepted: 22 January 2007 – Published: 8 March 2007 Abstract. -
Ionospheric Simulation Compared with Dynamics Explorer Obselvations for November 22, 1981
JOUR NAL OF GEOPHYSICAL RESEARCH . VOL. 97, NO. A2 PAGES 1245- 1256 FEBRUARY 1, 1992 Ionospheric Simulation Compared With Dynamics Explorer ObselVations for November 22, 1981 J. I. SOJKA,) M. BOWLINE,) R. W. SCHUNK,) J. D. CRAVEN,2 L. A. FRANK,2 J. R. SHARBER/ J. D. WINNINGHAM,l AND L. H. BRACE· Dynamics Explorer (DE) 2 electric field and particle data have been used to constrain the inputs of a tirne dependent ionospheric model (TDIM) for a simulation of the ionosphere on November 22, 1981. The simulated densities have then been critically compared with the DE 2 electron density observations. This comparison uncovers a model-data disagreement in the morning sector trough, generally good agreement of the background density in the polar cap and evening sector trough, and a difficulty in modelling the observed polar F layer patches. From this comparison, the consequences of structure in the electric field and precipitation inputs can be seen. This is further highlighted during a substonn period for which DE 1 auroral images were available. Using these images, a revised dynamic particle precipitation pattem was used in the ionospheric model; the resulting densities were different from the original simulation. With this revised dynamic precipitation model. improved density agreement is obtained in the auroral/polar regions where the plasma convection is not stagnanL However, the dynamic study also reveals a difficulty of matching dynamic auroral patterns with static empirical convection patterns. In this case, the matching of the models produced intense auroral precipitation in a stagnation region, which, in tum,led to exceedingly large '!DIM densities. -
Neutral Atom Imaging of the Solar Wind‐Magnetosphere‐Exosphere
RESEARCH LETTER Neutral Atom Imaging of the Solar Wind‐Magnetosphere‐ 10.1029/2020GL089362 Exosphere Interaction Near the Subsolar Magnetopause Key Points: S. A. Fuselier1,2 , M. A. Dayeh1,2 , A. Galli3 , H. O. Funsten4 , N. A. Schwadron5 , • ENA cameras image both 6 7 8 1 9,10 magnetosheath and magnetospheric S. M. Petrinec , K. J. Trattner , D. J. McComas , J. L. Burch , S. Toledo‐Redondo , plasmas in the vicinity of the J. R. Szalay8 , and R. J. Strangeway11 subsolar magnetopause • Magnetospheric plasma is not 1Southwest Research Institute, San Antonio, TX, USA, 2Department of Physics and Astronomy, University of Texas at San distributed evenly across the dayside Antonio, San Antonio, TX, USA, 3Physics Institute, University of Bern, Bern, Switzerland, 4Los Alamos National near the magnetopause 5 6 • The exospheric hydrogen density Laboratory, Los Alamos, NM, USA, Space Science Center, University of New Hampshire, Durham, NH, USA, Lockheed 7 near the magnetopause may have a Martin Advanced Technology Center, Palo Alto, CA, USA, Laboratory for Atmospheric and Space Physics, University of weak dependence on solar F10.7 Colorado Boulder, Boulder, CO, USA, 8Department of Astrophysical Sciences, Princeton University, Princeton, NJ, USA, 9Institut de Recherche en Astrophysique et Planétologie, Université de Toulouse, Toulouse, France, 10Department of Supporting Information: Electromagnetism and Electronics, University of Murcia, Murcia, Spain, 11Earth and Space Sciences, University of • Supporting Information S1 California, Los Angeles, CA, USA Correspondence to: Abstract Energetic neutral atoms (ENAs) created by charge‐exchange of ions with the Earth's hydrogen S. A. Fuselier, exosphere near the subsolar magnetopause yield information on the distribution of plasma in the outer [email protected] magnetosphere and magnetosheath. -
Chronology of NASA Expendable Vehicle Missions Since 1990
Chronology of NASA Expendable Vehicle Missions Since 1990 Launch Launch Date Payload Vehicle Site1 June 1, 1990 ROSAT (Roentgen Satellite) Delta II ETR, 5:48 p.m. EDT An X-ray observatory developed through a cooperative program between Germany, the U.S., and (Delta 195) LC 17A the United Kingdom. Originally proposed by the Max-Planck-Institut für extraterrestrische Physik (MPE) and designed, built and operated in Germany. Launched into Earth orbit on a U.S. Air Force vehicle. Mission ended after almost nine years, on Feb. 12, 1999. July 25, 1990 CRRES (Combined Radiation and Release Effects Satellite) Atlas I ETR, 3:21 p.m. EDT NASA payload. Launched into a geosynchronous transfer orbit for a nominal three-year mission to (AC-69) LC 36B investigate fields, plasmas, and energetic particles inside the Earth's magnetosphere. Due to onboard battery failure, contact with the spacecraft was lost on Oct. 12, 1991. May 14, 1991 NOAA-D (TIROS) (National Oceanic and Atmospheric Administration-D) Atlas-E WTR, 11:52 a.m. EDT A Television Infrared Observing System (TIROS) satellite. NASA-developed payload; USAF (Atlas 50-E) SLC 4 vehicle. Launched into sun-synchronous polar orbit to allow the satellite to view the Earth's entire surface and cloud cover every 12 hours. Redesignated NOAA-12 once in orbit. June 29, 1991 REX (Radiation Experiment) Scout 216 WTR, 10:00 a.m. EDT USAF payload; NASA vehicle. Launched into 450 nm polar orbit. Designed to study scintillation SLC 5 effects of the Earth's atmosphere on RF transmissions. 114th launch of Scout vehicle.