Brief Curriculum Vitae and Publications)
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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. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Fiscal Year 1973, and Are the EROS Program Also Supports the ERTS Data Proiected at Almost $1 Million for Fiscal Year 1974
Aeronautics and Space Report of the President r973 Activities NOTE TO READERS: ALL PRINTED PAGES ARE INCLUDED, UNNUMBERED BLANK PAGES DURING SCANNING AND QUALITY CONTROL CHECK HAVE BEEN DELETED Aeronautics and Space Report of the President 1973 A c tivities National Aeronautics and Space Administration Washington, D.C. 20546 President’s Message of Transmittal To the Congress of the United States: the European Space Conference has agreed to con- struct a space laboratory-Spacelab-for use with the I am pleased to transmit this report on our Nation’s Shuttle. progress in aeronautics and space activities during Notable progress has also been made with the Soviet 1973. Union in preparing the Apollo-Soyuz Test Project This year has been particularly significant in that scheduled for 1975. We are continuing to cooperate many past efforts to apply the benefits of space tech- with other nations in space activities and sharing of nology and information to the solution of problems on scientific information. These efforts contribute to global Earth are now coming to fruition. Experimental data peace and prosperity. from the manned Skylab station and the unmanned While we stress the use of current technology to solve Earth Resources Technology Satellite are already being current problems, we are employing unmanned space- used operationally for resource discovery and manage- craft to stimulate further advances in technology and ment, environmental information, land use planning, to obtain knowledge that can aid us in solving future and other applications. problems. Pioneer 10 gave us our first closeup glimpse Communications satellites have become one of the of Jupiter and transmitted data which will enhance principal methods of international communication our knowledge of Jupiter, the solar system, and ulti- and are an important factor in meeting national de- mately our own planet. -
Solar Parameters for Modeling Interplanetary Background
— 2 — Solar parameters for modeling interplanetary background M. Bzowski, J.M. Sokoł´ Space Research Center Polish Academy of Sciences, Warsaw, Poland M. Tokumaru,K.Fujiki Solar-Terrestrial Environment Laboratory, Nagoya University, Nagoya, Japan E. Quemerais,R.Lallement LATMOS-IPSL, Universite Versailles Saint-Quentin, Guyancourt, France S. Ferron ACRI-ST, Sophia Antipolis, France P. Bochsler Space Science Center & Department of Physics, University of New Hampshire, Durham NH Physikalisches Institut, University of Bern, Bern, Switzerland D.J. McComas Southwest Research Institute, San Antonio TX University of Texas at San Antonio, San Antonio, TX 78249, USA Abstract The goal of the Fully Online Datacenter of Ultraviolet Emissions (FONDUE) Work- ing Team of the International Space Science Institute (ISSI) in Bern, Switzerland, was to establish a common calibration of various UV and EUV heliospheric observations, both spectroscopic and photometric. Realization of this goal required a credible and up-to-date model of spatial distribution of neutral interstellar hydrogen in the heliosphere, and to that end, a credible model of the radiation pressure and ionization processes was needed. This chapter describes the latter part of the project: the solar factors responsible for shap- arXiv:1112.2967v1 [astro-ph.SR] 13 Dec 2011 ing the distribution of neutral interstellar H in the heliosphere. Presented are the solar Lyman-alpha flux and the question of solar Lyman-alpha resonant radiation pressure force acting on neutral H atoms in the heliosphere, solar EUV radiation and the process of pho- toionization of heliospheric hydrogen, and their evolution in time and the still hypothetical variation with heliolatitude. Further, solar wind and its evolution with solar activity is 1 2 2. -
Deep Space Chronicle Deep Space Chronicle: a Chronology of Deep Space and Planetary Probes, 1958–2000 | Asifa
dsc_cover (Converted)-1 8/6/02 10:33 AM Page 1 Deep Space Chronicle Deep Space Chronicle: A Chronology ofDeep Space and Planetary Probes, 1958–2000 |Asif A.Siddiqi National Aeronautics and Space Administration NASA SP-2002-4524 A Chronology of Deep Space and Planetary Probes 1958–2000 Asif A. Siddiqi NASA SP-2002-4524 Monographs in Aerospace History Number 24 dsc_cover (Converted)-1 8/6/02 10:33 AM Page 2 Cover photo: A montage of planetary images taken by Mariner 10, the Mars Global Surveyor Orbiter, Voyager 1, and Voyager 2, all managed by the Jet Propulsion Laboratory in Pasadena, California. Included (from top to bottom) are images of Mercury, Venus, Earth (and Moon), Mars, Jupiter, Saturn, Uranus, and Neptune. The inner planets (Mercury, Venus, Earth and its Moon, and Mars) and the outer planets (Jupiter, Saturn, Uranus, and Neptune) are roughly to scale to each other. NASA SP-2002-4524 Deep Space Chronicle A Chronology of Deep Space and Planetary Probes 1958–2000 ASIF A. SIDDIQI Monographs in Aerospace History Number 24 June 2002 National Aeronautics and Space Administration Office of External Relations NASA History Office Washington, DC 20546-0001 Library of Congress Cataloging-in-Publication Data Siddiqi, Asif A., 1966 Deep space chronicle: a chronology of deep space and planetary probes, 1958-2000 / by Asif A. Siddiqi. p.cm. – (Monographs in aerospace history; no. 24) (NASA SP; 2002-4524) Includes bibliographical references and index. 1. Space flight—History—20th century. I. Title. II. Series. III. NASA SP; 4524 TL 790.S53 2002 629.4’1’0904—dc21 2001044012 Table of Contents Foreword by Roger D. -
UNIVERSITY of CALIFORNIA Los Angeles Charged
UNIVERSITY OF CALIFORNIA Los Angeles Charged Particle Energization and Transport in the Magnetotail during Substorms A dissertation submitted in partial satisfaction of the requirements for the degree Doctor of Philosophy in Physics by Qingjiang Pan 2015 ABSTRACT OF THE DISSERTATION Charged Particle Energization and Transport in the Magnetotail during Substorms by Qingjiang Pan Doctor of Philosophy in Physics University of California, Los Angeles, 2015 Professor Maha Ashour-Abdalla, Chair This dissertation addresses the problem of energization of particles (both electrons and ions) to tens and hundreds of keV and the associated transport process in the magnetotail during substorms. Particles energized in the magnetotail are further accelerated to even higher energies (hundreds of keV to MeV) in the radiation belts, causing space weather hazards to human activities in space and on ground. We develop an analytical model to quantitatively estimate flux changes caused by betatron and Fermi acceleration when particles are transported along narrow high-speed flow channels from the magnetotail to the inner magnetosphere. The model shows that energetic particle flux can be significantly enhanced by a modest compression of the magnetic field and/or ii shrinking of the distance between the magnetic mirror points. We use coordinated spacecraft measurements, global magnetohydrodynamic (MHD) simulations driven by measured upstream solar wind conditions, and large-scale kinetic (LSK) simulations to quantify electron local acceleration in the near-Earth reconnection region and nonlocal acceleration during plasma earthward transport. Compared to the analytical model, application of the LSK simulations is much less restrictive because trajectories of millions of test particles are calculated in the realistically determined global MHD fields and the results are statistical. -
ISEE&Hyphen;3 Wave Measurements in the Distant Geomagnetic Tail And
GEOPHYSICALRESEARCH LETTERS, VOL. 11, NO. 4, PAGES335-338, APRIL 1984 ISEE-3 WAVE MEASUREMENTS IN THE DISTANT GEOMAGNETIC TAIL AND BOUNDARY LAYER Fß L. Scarfl , F. V. Coroniti1, Cß F. KennelI , Rß Wß Fredricks1 D. A. Gurnett2, andE ß Jß Smith3 1TRWSpace and Technology Group, Redondo Beach, California 90278 2Universityof Iowa,Iowa City, Iowa 52242 3jet PropulsionLaboratory, Pasadena, California 91109 Abstractß The ISEE-3 excursion into the dis- field configuration for the first relatively tant tail region reveals a complex structure with close-in traversal of the tail (r < 94 Re) and several wave, particle and field characteristics for the first deep excursion to r = 225 Re. In that differ significantly from those measured another recent report, Bame et al. (1983) pre- closer to earth. The most striking results are Sented initial results from the ISEE-3 plasma found within the distant boundary layer where in- analyzer, and they showed that all plasma regimes tense electrostatic turbulence levels are de- identified from earlier measurements (plasma tected in association with bi-directional elec- sheet, low latitude boundary levels, mantle, lobe tron distributions. The wave amplitudes appear and magnetosheath) remained recognizable in the to increase with increasing downstream distance distant tail, although the regimes appeared to be and the polarizations are those expected for ion "intermingled" far from earth, and a well-defined acoustic oscillations. Near the boundary of the low density tail lobe was rarely encountered. distant plasmas sheet the turbulence spectra are The distant tail plasma was also characterized by essentially identical to those measured much unusually large flow speeds (generally tailward) closer to earth on IMP-8. -
An Analysis of Solar Energetic Particle Spectra Throughout the Inner Heliosphere
An Analysis of Solar Energetic Particle Spectra Throughout the Inner Heliosphere J. Douglas Patterson 19th December 2002 Contents 1 Previous Studies and Results 1 1.1 Solar Structure and the Heliosphere . 1 1.2 Source of the Solar Wind and the Interplanetary Magnetic Field . 6 1.2.1 Solar Wind Outflow . 6 1.2.2 Interplanetary Magnetic Field (IMF) . 9 1.3 Global Chracteristics of the Inner Heliosphere . 10 1.3.1 The Solar Wind and Solar Magnetic Field . 10 1.3.2 Solar Energetic Particles . 10 1.3.3 Co-Rotating Interaction Regions . 12 1.3.4 Anomalous and Galactic Cosmic Rays . 12 1.4 Acceleration Processes . 13 1.4.1 DC Electric Field Acceleration . 13 1.4.2 Wave-Particle Interactions . 13 1.4.3 Shock Drift and Diffusive Acceleration . 17 2 Spacecraft Mission Descriptions 25 2.1 The Ulysses Mission . 25 2.1.1 Mission Goals and Objectives . 26 2.1.2 The Spacecraft . 26 2.1.3 Trajectory . 28 2.2 The Advanced Composition Explorer (ACE) Mission . 29 2.2.1 Mission Goals and Objectives . 29 2.2.2 The Spacecraft . 29 2.2.3 Trajectory . 31 2.3 The EPAM and the HISCALE Instruments . 31 2.3.1 The Hardware and Detector Types . 31 2.3.2 On-Board Data Processing and Data Format . 36 ii 2.3.3 Instrument-Specific Problems . 38 2.4 The IMP-8 Spacecraft and CPME Instrument . 40 2.4.1 Spacecraft and Trajectory . 42 2.4.2 Charged Particle Measurement Experiment . 42 3 Data Reduction and Analysis Procedures 46 3.1 Determination of the Background Rates for EPAM and HISCALE . -
<> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA
1 SATELITES ARTIFICIALES. Capítulo 5º Subcap. 10 <> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA TIERRA. Esta es una relación cronológica de todos los lanzamientos de satélites artificiales de nuestro planeta, con independencia de su éxito o fracaso, tanto en el disparo como en órbita. Significa pues que muchos de ellos no han alcanzado el espacio y fueron destruidos. Se señala en primer lugar (a la izquierda) su nombre, seguido de la fecha del lanzamiento, el país al que pertenece el satélite (que puede ser otro distinto al que lo lanza) y el tipo de satélite; este último aspecto podría no corresponderse en exactitud dado que algunos son de finalidad múltiple. En los lanzamientos múltiples, cada satélite figura separado (salvo en los casos de fracaso, en que no llegan a separarse) pero naturalmente en la misma fecha y juntos. NO ESTÁN incluidos los llevados en vuelos tripulados, si bien se citan en el programa de satélites correspondiente y en el capítulo de “Cronología general de lanzamientos”. .SATÉLITE Fecha País Tipo SPUTNIK F1 15.05.1957 URSS Experimental o tecnológico SPUTNIK F2 21.08.1957 URSS Experimental o tecnológico SPUTNIK 01 04.10.1957 URSS Experimental o tecnológico SPUTNIK 02 03.11.1957 URSS Científico VANGUARD-1A 06.12.1957 USA Experimental o tecnológico EXPLORER 01 31.01.1958 USA Científico VANGUARD-1B 05.02.1958 USA Experimental o tecnológico EXPLORER 02 05.03.1958 USA Científico VANGUARD-1 17.03.1958 USA Experimental o tecnológico EXPLORER 03 26.03.1958 USA Científico SPUTNIK D1 27.04.1958 URSS Geodésico VANGUARD-2A -
Do Statistical Models Capture the Dynamics of the Magnetopause
manuscript submitted to JGR: Space Physics 1 Do statistical models capture the dynamics of the 2 magnetopause during sudden magnetospheric 3 compressions? 1 1 1 2 3 4 F. A. Staples , I. J. Rae , C. Forsyth , A. R. A. Smith , K.R. Murphy , K. 4 5 6 7 6 5 M. Raymer , F. Plaschke , N. A. Case , C. J. Rodger , J. A. Wild , S. E. 4 4 6 Milan , S. M. Imber 1 7 Mullard Space Science Laboratory, University College London, London, UK 2 8 School of GeoSciences, University of Edinburgh, Edinburgh, UK 3 9 NASA Goddard Space Flight Centre, Greenbelt, MD, USA 4 10 Department of Physics and Astronomy, University of Leicester, Leicester, UK 5 11 Space Research Institute, Austrian Academy of Sciences, Graz, Austria. 6 12 Department of Physics, Lancaster University, Lancaster, UK 7 13 Department of Physics, University of Otago, Dunedin, New Zealand 14 Key Points: 15 • Measured magnetopause location is statistically closer to the Earth than Shue et 16 al. (1998) modelled for storm sudden commencements (SYM-H ≥ 15 nT). 17 • When the magnetopause is compressed below 8 RE, the average measured loca- 18 tion is > 1 RE inside of the Shue et al. (1998) model location. 19 • Extreme magnetopause compressions rarely reach the outer radiation belt, there- 20 fore rapid outward radial transport is required to fully explain most shadowing 21 events. Corresponding author: Frances A. Staples, [email protected] {1{ manuscript submitted to JGR: Space Physics 22 Abstract 23 Under periods of strong solar wind driving, the magnetopause can become compressed, 24 playing a significant role in draining electrons from the outer radiation belt. -
NASA Astronauts
PUBLISHED BY Public Affairs Divisio~l Washington. D.C. 20546 1983 IColor4-by-5 inch transpar- available free to information lead and sent to: Non-informstionmedia may obtain identical material for a fee through a photographic contractor by using the order forms in the rear of this book. These photqraphs are government publications-not subject to copyright They may not be used to state oiimply the endorsement by NASA or by any NASA employee of a commercial product piocess or service, or used in any other manner that might mislead. Accordingly, it is requested that if any photograph is used in advertising and other commercial promotion. layout and copy be submitted to NASA prior to release. Front cover: "Lift-off of the Columbia-STS-2 by artist Paul Salmon 82-HC-292 82-ti-304 r 8arnr;w u vowzn u)rorr ~ nsrvnv~~nrnno................................................ .-- Seasat .......................................................................... 197 Skylab 1 Selected Pictures .......................................................150 Skylab 2 Selected Pictures ........................................................ 151 Skylab 3 Selected Pictures ........................................................152 Skylab 4 Selected Pictures ........................................................ 153 SpacoColony ...................................................................183 Space Shuttle ...................................................................171 Space Stations ..................................................................198 \libinn 1 1f.d Apoiio 17/Earth 72-HC-928 72-H-1578 Apolb B/Earth Rise 68-HC-870 68-H-1401 Voyager ;//Saturn 81-HC-520 81-H-582 Voyager I/Ssturian System 80-HC-647 80-H-866 Voyager IN~lpiterSystem 79-HC-256 79-H-356 Viking 2 on Mars 76-HC-855 76-H-870 Apollo 11 /Aldrin 69-HC-1253 69-H-682 Apollo !I /Aldrin 69-HC-684 69-H-1255 STS-I /Young and Crippen 79-HC-206 79-H-275 STS-1- ! QTPLaunch of the Columbia" 82-HC-23 82-H-22 Major Launches NAME UUNCH VEHICLE MISSIONIREMARKS 1956 VANGUARD Dec.