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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. -
An Overview of the Space Physics Data Facility (SPDF) in the Context of “Big Data”
An Overview of the Space Physics Data Facility (SPDF) in the Context of “Big Data” Bob McGuire, SPDF Project Scientist Heliophysics Science Division (Code 670) NASA Goddard Space Flight Center Presented to the Big Data Task Force, June 29, 2016 Topics • As an active Final Archive, what is SPDF? – Scope, Responsibilities and Major Elements • Current Data • Future Plans and BDTF Questions REFERENCE URL: http://spdf.gsfc.nasa.gov 8/3/16 2:33 PM 2 SPDF in the Heliophysics Science Data Management Policy • One of two (active) Final Archives in Heliophysics – Ensure the long-term preservation and ongoing (online) access to NASA heliophysics science data • Serve and preserve data with metadata / software • Understand past / present / future mission data status • NSSDC is continuing limited recovery of older but useful legacy data from media – Data served via FTP/HTTP, via user web i/f, via webservices – SPDF focus is non-solar missions and data • Heliophysics Data Environment (HpDE) critical infrastructure – Heliophysics-wide dataset inventory (VSPO->HDP) – APIs (e.g. webservices) into SPDF system capabilities and data • Center of Excellence for science-enabling data standards and for science-enabling data services 8/3/16 2:33 PM 3 SPDF Services • Emphasis on multi-instrument, multi-mission science (1) Specific mission/instrument data in context of other missions/data (2) Specific mission/instrument data as enriching context for other data (3) Ancillary services & software (orbits, data standards, special products) • Specific services include -
A Brief Survey of Attitude Control Systems for Small Satellites Using
I I A BRIEF SURVEY OF ATTITUDE CONTROL SYSTEMS FOR SMALL SATELLITES I USING MOMENTUM CONCEPTS I Ali Siahpush Globesat Inc. Logan. Utah and I Janet Gleave Honeywell Inc .• Satellite Systems Division I Glendale. Arizona High-accuracy pointing capabilities are desired for many three-axis I stabilized small satellites. Momentum-based attitude control system actuators, initially developed for larger satellites. are being utilized by small satellites to meetthesc pointing requirements. This paper provides I an overview of momentum devices available for small satellite applications and three-axis attitude control system (ACS) configurations using these devices. Factors affecting the selection and sizing of ACS components are also addressed. Included are suggestions for potential I ACS improvements and cost-saving measures that will make momentum I devices more accessible to the small satellite community. INTRODUCTION I Small satellites are currently being used in various mission/payload regimes that require high accuracy pointing capabilities. For example. small three-axis stabilized satellites are used to accurately pinpoint their instruments to specific objects or regions of space. Also, small commu I nication satellites. especially those employing multiple narrow-beam antennas. require tight pointing accuracies to ensure adequate antenna gain. Attitude control system technologies developed for larger satellites are being utilized to meet increasingly stringent pointing require I ments. At present. pointing accuracies of I degree or less are quite common for both spin and three-axis stabilized small satellites. I The selection of an attitude control system (ACS) is a function of many factors. including mission objectives. orbit. and available system budgets. Stabilization systems using momentum and reaction wheels as control torque sources are well-suited to small satellite applications due to their proven performance. -
Dataset of Post Stamps on Rocket and Satellite (1957-1959)
第69卷 增刊 地 理 学 报 Vol.69, Supplement 2014年8月 ACTA GEOGRAPHICA SINICA August, 2014 Dataset of post stamps on rocket and satellite (1957-1959) LIU Chuang (Institute of Geographic Sciences and Natural Resources Research, CAS, Beijing 100101, China) Abstract: The launching of rocket and satellite was one of the major tasks of International Geophysical Year (IGY). The first of Russia satellite named Sputnik 1 was successful launched on 4 October 1957, which is recognized as a milestone for a new era - a space age. Besides the satellites of Sputnik 1, 2 and 3, Luna 1, 2 and 3 from Russia, the Explorer 1, 3, 4, 6, 7, Vanguard 1, 2, 3, Pioneer 1,2,3, 4, Discoverer 1, 2, 5, 6, 7, 8 and Score from USA were successful launched from 1957-1959 in IGY (The Rocket and Satellite task was extended for implementation for one more year in 1959 than that of tasks else from 1957-1958). For celebrating and commemorating the great achievements in human history, 23 countries in the world issued post stamps during IGY, the first three years of the space era. The collection of post stamps consisted of 349 pieces from 23 countries are archived in LIN Chao Geomuseum (www.geomuseum.cn), The dataset consisted of 349 .jpg files for all of archived stamps and one table file which is the list of the collections. The code, image, date issued, country issued, contributor and descriptions are listed at the table items. Keywords: rocket; satellites; post stamps; dataset; IGY; 1957-1959 DOI: 10.11821/dlxb2014S005 Citation: LIU Chuang. -
REINTERPRETING PIONEER DEEP SPACE STATION Alexander Paul
REINTERPRETING PIONEER DEEP SPACE STATION Alexander Paul Ray Submitted in partial fulfillment of the requirements for the degree Master of Science in Historic Preservation Graduate School of Architecture, Planning, and Preservation Columbia University May 2017 Ray 0 Acknowledgements …………………………………………………………………......….1 List of figures …………………………………………………………………………........2 Introduction ……………………….…………………………………………………...…..3 Part I: Relevance to the preservation field Definition of a space probe Why should preservationists be involved? What should audiences take away? Part II: Methodology Literature review Case study selection Terminology Chapter 1: Historical context ……………………………………………………….…..17 Why are space probes historically significant? History of robotic space exploration in the United States Chapter 2: Interpretive content ………………………………………………….……..48 Pioneer as case study Statement of interpretive themes Development of interpretive themes Chapter 3: Current interpretations of historic space probes ………………….……...62 Public perception Audience Current interpretation Effective methods Chapter 4: Proposal for reinterpreting Pioneer Deep Space Station …………….…..83 Conclusion …………………………………………….………………………………...111 Bibliography ……………………………………………………………………….…....113 Ray 0 Acknowledgements First and foremost, I want to thank my thesis advisor, Jessica Williams. Simply put, I could not have imagined a better person to work with on this thing. Thanks also to all of the Historic Preservation faculty for their support, and in particular Paul Bentel and Chris Neville for their helpful feedback last semester. I am also especially grateful to my thoughtful readers, Will Raynolds and Mark Robinson. My gratitude also goes out to the entire Lunar Reconnaissance Obiter Camera team at Arizona State University. Having the opportunity to meet with these talented and welcoming people got me excited to write about space probes. Last but not least, thank you to all of my classmates. -
177-/L.7 S- -,---- I ,S -5-- 5- - -5 —2
X-601-72-487 PREPRINT A MODEL OF THE STARFISH FLUX IN THE INNER RADIATION ZONE U U: ULU TURN TO UBRAR'! M. J. TEAGUE E. G. STASSINOPOULOS DECEMBER 1972 GODDARD SPACE FLIGHT CENTER GREENBELT, MARYLAND 25 7J RESEARCH & Ii • T. LC.3 177-/l.7 S- -,---- I ,S -5-- 5- - -5 —2 5-Y --T• T S.- SS_ - : : ;- / - - - — -5- - -- - - --- - - - - - - - / - - c -- - - - - - '--.- - - -- - _ -- - ,- - -• .. Al 5---- -f -- -- _z 5- - - - - - - --5- -z - - - -'7 - - - / 5- 5 -- - - - - - 5- - -- - .5, 5- - -- -5- _-f k - - ------- --- - -'---- - 5-'- -"c-- - c - 7- - -- Si i- - r ---- ____.__5: ------ -- - - -- - : 15-- - -- _ - - - - - - -5•E - - - - --SS -• — ._---S - -- -- 5--- 5- '- . -. - 5-. - - - - 1-. -- __- 7-- 5-1-• '2 2 - - 4 - r X-601-72-487 PREPRINT A MODEL OF THE STARFISH FLUX IN THE INNER RADIATION ZONE by Michael J. Teague The KMS Technology Center and E. G. Stassinopoulos National Space Science Data Center National Space Science Data Center National Aeronautics and Space Administration Goddard Space Flight Center Greenbelt, Maryland 20771 December 1972 Page intentionally left blank Page intentionally left blank A MODEL OF THE STARFISH FLUX IN THE INNER RADIATION ZONE by Michael J. Teague The KNS Technology Center and E. G. Stassinopoulos National Space Science Data Center ABSTRACT A model of the Starfish electrons injected into the radiation belt in July 1962 has been determined for epoch September 1964. This model distinguishes be- tween artificial and natural electrons and provides the artificial unidirectional electron flax as a function of equatorial pitch angle, energy, and L value. The model is based primarily upon data from the OCO 1, OGO 3, OGO 5, 1963-38C, and the OV3-3 satellites. -
L-G-0003855083-0002286116.Pdf
Geophysical Monograph Series Including IUGG Volumes Maurice Ewing Volumes Mineral Physics Volumes Geophysical Monograph Series 164 Archean Geodynamics and Environments Keith Benn, 182 The Stromboli Volcano: An Integrated Study of Jean-Claude Mareschal, and Kent C. Condie (Eds.) the 2002–2003 Eruption Sonia Calvari, Salvatore 165 Solar Eruptions and Energetic Particles Inguaggiato, Giuseppe Puglisi, Maurizio Ripepe, Natchimuthukonar Gopalswamy, Richard Mewaldt, and Mauro Rosi (Eds.) and Jarmo Torsti (Eds.) 183 Carbon Sequestration and Its Role in the Global 166 Back-Arc Spreading Systems: Geological, Biological, Carbon Cycle Brian J. McPherson and Chemical, and Physical Interactions David M. Christie, Eric T. Sundquist (Eds.) Charles Fisher, Sang-Mook Lee, and Sharon Givens (Eds.) 184 Carbon Cycling in Northern Peatlands Andrew J. Baird, 167 Recurrent Magnetic Storms: Corotating Solar Lisa R. Belyea, Xavier Comas, A. S. Reeve, and Wind Streams Bruce Tsurutani, Robert McPherron, Lee D. Slater (Eds.) Walter Gonzalez, Gang Lu, José H. A. Sobral, and 185 Indian Ocean Biogeochemical Processes and Natchimuthukonar Gopalswamy (Eds.) Ecological Variability Jerry D. Wiggert, 168 Earth’s Deep Water Cycle Steven D. Jacobsen and Raleigh R. Hood, S. Wajih A. Naqvi, Kenneth H. Brink, Suzan van der Lee (Eds.) and Sharon L. Smith (Eds.) 169 Magnetospheric ULF Waves: Synthesis and 186 Amazonia and Global Change Michael Keller, New Directions Kazue Takahashi, Peter J. Chi, Mercedes Bustamante, John Gash, and Pedro Silva Dias Richard E. Denton, and Robert L. Lysak (Eds.) (Eds.) 170 Earthquakes: Radiated Energy and the Physics 187 Surface Ocean–Lower Atmosphere Processes of Faulting Rachel Abercrombie, Art McGarr, Corinne Le Quèrè and Eric S. Saltzman (Eds.) Hiroo Kanamori, and Giulio Di Toro (Eds.) 188 Diversity of Hydrothermal Systems on Slow Spreading Ocean Ridges Peter A. -
Multiwavelength Spectral Analysis of Accretion Disk and Astrophysical Jet Connection in Low-Mass X-Ray Binaries
Master’s Programme in Electronics and Nanotechnology Multiwavelength Spectral Analysis of Accretion Disk and Astrophysical Jet Connection in Low-Mass X-ray Binaries Moniaallonpituustutkimus kertymäkiekon ja astrofysikaalisen hiukkassuihkun välisestä yhteydestä matalamassaisissa röntgenkaksoistähdissä Alexandros Binios MASTER’S THESIS Multiwavelength Spectral Analysis of Accretion Disk and Astrophysical Jet Connection in Low-Mass X-ray Binaries Alexandros Binios School of Electrical Engineering Thesis submitted for examination for the degree of Master of Science in Technology. Helsinki 28.9.2020 Supervisor Prof. Anne Lähteenmäki Advisor Ph.D. Karri I. I. Koljonen Copyright ⃝c 2020 Alexandros Binios Aalto University, P.O. BOX 11000, 00076 AALTO www.aalto.fi Abstract of the master’s thesis Author Alexandros Binios Title Multiwavelength Spectral Analysis of Accretion Disk and Astrophysical Jet Connection in Low-Mass X-ray Binaries Degree programme Master’s Programme in Electronics and Nanotechnology Major Space Science and Technology Code of major ELEC3039 Supervisor Prof. Anne Lähteenmäki Advisor Ph.D. Karri I. I. Koljonen Date 28.9.2020 Number of pages 110+13 Language English Abstract X-ray binaries (XRBs) are powerful double star systems where a normal star feeds through accretion a compact object, e.g. a black hole, and the liberation of accre- tion energy results in strong radiation throughout the electromagnetic spectrum. Performing simultaneous multiwavelength observations of XRBs allow us to study their fundamental astrophysical properties and processes, which are ultimately governed by the mass flow rate from the donor star to the accretor. The primary objective of this master’s thesis was to perform multiwavelength spectral studies of known XRBs focusing on the accretion disk and astrophysical jet connection, i.e. -
The Chelsea Board of Y Voted Feb
m m m ***#***##*#****## f'.AR--ft T SORT *#CO&S i 379 '10-21-95 45W. 12P 1 IS m c k u n e m e m o r i a l l i b r a r y 221- S. MAIN STREET CHELSEA MI 43118 h n ONE HUNDRED TWENTY-SIXTH YEAR— No. 37 CHELSEA, MICHIGAN, THURSDAY, FEBRUARY 12, 1998 28.P ages This W eek Supplement t o V i t t Beach school hit by flu outbreak „ Beach M iddle School has seen a rash of Illness lately- with up'to 170 kids absent By Erie Bowen" parently fheyer recorded~byr from school last week, Prin Staff W riter ' t h e s t a t e . cipal Bill W estcott reported Sylvan Township Board vlyers ; said ‘ the ~ council to the Chelsea Board of Y voted Feb. 3 to.protest the an voted to annex the land, be Education Monday. nexation into the village of cause it w as the easiest way to W estcott said a flu virus property near the Chelsea Re include as part, of the village thathas been traveling tirem ent Community. Supervi what he believed to be already around schools hit Beach sor Jerry Dress el house said within the' boundaries. Sylvan hard at the beginning of the the board thought it would be Township decided to contest w eek but has tapered off in detrimental to‘ Chelsea’s the annexation to forestall the recent-days-— — -— -• - downtown with the village’s boundary • commission fr 0|m ‘ Itw as-bad-there last; intention toV onverl the village including it in the city B ound1" week," W estcott said. -
Eastern Range Launch History Listing by Year - 1950 Through 2010
Eastern Range Launch History Listing by Year - 1950 through 2010 Run Date: 6/30/2010 Total Launches: 3,415 Year Vehicle Site ID SeqSerial # Payload/Comments/Ship 1950 07/24/1950 BUMPER 03 8 N/A - N/A 07/29/1950 BUMPER 03 7 N/A - N/A 10/25/1950 LARK Unknown 225 N/A - N/A 10/26/1950 LARK Unknown 226 N/A - N/A 11/21/1950 LARK Unknown 227 N/A - N/A Total Launches: 5 1951 04/11/1951 LARK Unknown 231 N/A - N/A 04/17/1951 LARK Unknown 232 N/A - N/A 05/03/1951 LARK Unknown 234 N/A - N/A 05/11/1951 LARK Unknown 235 N/A - N/A 05/29/1951 LARK Unknown 242 N/A - N/A 06/07/1951 LARK Unknown 236 N/A - N/A 06/07/1951 LARK Unknown 238 N/A - N/A 06/20/1951 MATADOR Unknown GM-544 N/A - N/A 06/29/1951 MATADOR Unknown GM-545 N/A - N/A 07/03/1951 LARK Unknown 240 N/A - N/A 07/18/1951 MATADOR Unknown GM-546 N/A - N/A 07/20/1951 LARK Unknown 239 N/A - N/A 08/10/1951 MATADOR Unknown GM-548 N/A - N/A 08/31/1951 MATADOR Unknown GM-549 N/A - N/A 09/06/1951 MATADOR Unknown GM-550 N/A - N/A 09/13/1951 LARK Unknown 593 N/A - N/A 09/19/1951 LARK Unknown 595 N/A - N/A 10/04/1951 LARK Unknown 597 N/A - N/A 10/26/1951 MATADOR Unknown GM-551 N/A - N/A 12/07/1951 MATADOR Unknown GM-547 N/A - N/A 12/11/1951 LARK Unknown 598 N/A - N/A 12/13/1951 MATADOR Unknown GM-552 N/A - N/A Total Launches: 22 1952 01/15/1952 MATADOR Unknown GM-554 N/A - N/A 01/28/1952 LARK Unknown 600 N/A - N/A 02/12/1952 LARK Unknown 604 N/A - N/A Page: 1/101 Eastern Range Launch History Listing by Year - 1950 through 2010 Run Date: 6/30/2010 Total Launches: 3,415 Year Vehicle Site ID SeqSerial # Payload/Comments/Ship -
PEAK CAN TRC File Format
PEAK CAN TRC File Format PEAK CAN TRC File Format Copyright (C) 2010-2020 PEAK-System Technik GmbH All rights reserved. Last update: 2020-07-27 Contents Version 1.0 ...................................................................................................................................... 3 Example ....................................................................................................................................... 3 General ........................................................................................................................................ 3 Columns ...................................................................................................................................... 3 Error Warnings ............................................................................................................................ 4 Error Frames ................................................................................................................................ 4 Version 1.1 ...................................................................................................................................... 6 Example ....................................................................................................................................... 6 General ........................................................................................................................................ 6 Changes compared to Version 1.0 .............................................................................................. -
The Relation Between Solar Cell Flight Performance Data and Materials and Manufacturing Data
The Relation Between Solar Cell Flight Performance Data and Materials and Manufacturing Data Report No. 1 First Quarterly Report Contract No. NASW - 1732 Prepared by The CARA Corporation 101 N. 33rd Street Philadelphia, Pennsylvania S. R. Pollack, Ph.D. L. A. Girifalco, Ph.D. Principal Investigator Staff Scientist Abstract An initial determination of seven groups of flights has been made that may be suitable for the purposes of this study. Each of these groups consists of flights that have been in orbit and transmitting for at least three months, are unclassified, and have similar space environ- ments. Computer searches have been performed to obtain docu- ments on silicon solar cells and on the flights in the seven groups mentioned above. As a result, a number of documents have been obtained. Appropriate channels have been ascertained and indi- viduals contacted to obtain data on radiation and thermal environments. These channels have been tested by request- ing information on a restricted number of flights in order to determine the effectiveness and rapidity by which infor- mation can be obtained. A general coding procedure has been devised to con- veniently summarize and display the availability of the information needed in this study. A number of pertinent documents have been obtained, and more are being received continually. i Table of Contents I. Introduction 1 Statement of the Problem Division into Phases Status of the Study 11. The Flight Selection Problem 3 Preliminary Screening Environmental Flight Classification 111. Information and Data Gathering 9 Computer Searche s Flight Documentation Environmental Data IV. Classification Codes 16 General and Specific Codes Code Forms V.