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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. -
2002-03-10 Po
Your hom etown newspaper serving Plym outh and Plym outh Tow nship for 116 years Sunday, March 10, 2002 www. observerandeccentric. com 7 5 $ Volume 116 Number 56 Plymouth Michigan ©2002 HomeTown Communications Network™ T H E WEEK Local AHEAD Kmart MONDAY avoids Drug seminar: A s e m in a r on what kinds of drugs kids can be exposed to at parties and clubs w ill be cuts the topic of discussion at Plymouth’s Kmart store avoided the the Canton H igh School chopping block Friday as the financial DuBois Theater. Kenneth ly troubled retail giant disclosed its list Krygel, a drug recognition of under-performing stores scheduled to be closed expert from Macomb Nearby stores that are scheduled to Com munity College's shut down include the Livonia Big Kmart on Plymouth Road near the Crim inal Justice Train Wonderland Mall and the Novi Big in g C e n te r; w ill give an Kmart on West Oaks Drive overview of the rave cul Store managers at the Plymouth Kmart refused to comment when con tu re , current drugs of tacted Friday, referring all questions ch o ice, signs and symp Sta ff P hoto b y b b y a n M itch ell to the company’s corporate office m Name game: Bird Elementary School was named for long-time educator Nellie Bird, part of the toms of drug use, a n d a Troy Plymouth-Canton school district’s history of naming elementary school buildings after its key The company announced it will close display of drug parapher educators. -
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 -
ESWW7 Abstract Book.Pdf
2 Table of Contents Committees ......................................................................................................................................................4 Sponsors ...........................................................................................................................................................5 Programme Monday, 15 November 2010...............................................................................................................6 Tuesday, 16 November 2010...............................................................................................................9 Wednesday, 17 November 2010 .......................................................................................................11 Thursday, 18 November 2010 ...........................................................................................................13 Friday, 19 November 2010 ................................................................................................................15 Poster Sessions ..................................................................................................................................17 Abstracts.........................................................................................................................................................25 3 Committees Programme Committee A. Belehaki (Co‐Chair, NOA & COST ES0803) A. Glover (Co‐Chair, ESA) M. Hapgood (RAL/STFC, SWWT) J.‐P. Luntama (ESA) R. Van der Linden (SIDC‐STCE) P. Vanlommel (STCE) T. -
Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE)
Space Sci Rev DOI 10.1007/s11214-013-9965-x Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE) D.G. Mitchell · L.J. Lanzerotti · C.K. Kim · M. Stokes · G. Ho · S. Cooper · A. Ukhorskiy · J.W. Manweiler · S. Jaskulek · D.K. Haggerty · P. Brandt · M. Sitnov · K. Keika · J.R. Hayes · L.E. Brown · R.S. Gurnee · J.C. Hutcheson · K.S. Nelson · N. Paschalidis · E. Rossano · S. Kerem Received: 30 June 2012 / Accepted: 1 February 2013 © The Author(s) 2013. This article is published with open access at Springerlink.com Abstract The Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE) on the two Van Allen Probes spacecraft is the magnetosphere ring current instrument that will provide data for answering the three over-arching questions for the Van Allen Probes Pro- gram: RBSPICE will determine “how space weather creates the storm-time ring current around Earth, how that ring current supplies and supports the creation of the radiation belt populations,” and how the ring current is involved in radiation belt losses. RBSPICE is a time-of-flight versus total energy instrument that measures ions over the energy range from ∼20 keV to ∼1 MeV. RBSPICE will also measure electrons over the energy range ∼25 keV to ∼1 MeV in order to provide instrument background information in the radiation belts. A description of the instrument and its data products are provided in this chapter. Keywords Magnetosphere · Ring current · Time-of-flight · Radiation belt · Space weather 1 Introduction The idea, or concept, of a “ring current” around Earth and its association with geomagnetic storms began in the early days of the twentieth century. -
ESRO SP-72 European Space Research Organisation
ESRO SP-72 I. Proc. ESRO-GRI ESRO SP-72 I. Proc ESRO-GRI European Space Research Organisation Colloquium March 1971 European Space Research Organisation Colloquium March 1971 COLLOQUIUM ON WAVE-PARTICLE INTER II. ESRO SP-72 COLLOQUIUM ON WAVE-PARTICLE INTER II. ESRO SP-72 ACTIONS IN THE MAGNETOSPHERE HI. Texts in English ACTIONS IN THE MAGNETOSPHERE III. Texts in English September 1971 September 1971 iv + 284 pages iv + 284 pages The Colloquium on wave-particle interactions in the magnetosphere held in The Colloquium on wave-particle interactions in the magnetosphere held in Orleans (March 17-19,1971) intended to review the outstanding problems still unsolved Orleans (March 17-19, 1971) intended to review the outstanding problems still unsolved in this field : in this field : — large-scale dynamics of the magnetosphere; — large-scale dynamics of the magnetosphere; — distribution of 'Oasma parameters; — distribution of plasma parameters; — decoupling of n..gnetospheric from ionospheric plasma; — decoupling of magnetospheric from ionospheric plasma; — acceleration and convection mechanisms; — acceleration and convection mechanisms; — substorms; — substorms; — polar wind..., — polar wind..., as well as the theoretical and experimental work needed to solve these problems in the as well as the theoretical and experimental work needed to solve these problems in the light of previous experiments (rocket launchings in auroral zone, Ariel 3 satellite...) light of previous experiments (rocket launchings in auroral zone, Ariel 3 satellite...) and of technical achievements (onboard computers, new sensors...). and of technical achievements (onboard computers, new sensors...). Ensuing discussions attempted to define types of missions which could be carried Ensuing discussions attempted to define types of missions which could be carried out in the future by the Small Scientific Satellites now being considered by ESRO. -
<> 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 -
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. -
Index of Astronomia Nova
Index of Astronomia Nova Index of Astronomia Nova. M. Capderou, Handbook of Satellite Orbits: From Kepler to GPS, 883 DOI 10.1007/978-3-319-03416-4, © Springer International Publishing Switzerland 2014 Bibliography Books are classified in sections according to the main themes covered in this work, and arranged chronologically within each section. General Mechanics and Geodesy 1. H. Goldstein. Classical Mechanics, Addison-Wesley, Cambridge, Mass., 1956 2. L. Landau & E. Lifchitz. Mechanics (Course of Theoretical Physics),Vol.1, Mir, Moscow, 1966, Butterworth–Heinemann 3rd edn., 1976 3. W.M. Kaula. Theory of Satellite Geodesy, Blaisdell Publ., Waltham, Mass., 1966 4. J.-J. Levallois. G´eod´esie g´en´erale, Vols. 1, 2, 3, Eyrolles, Paris, 1969, 1970 5. J.-J. Levallois & J. Kovalevsky. G´eod´esie g´en´erale,Vol.4:G´eod´esie spatiale, Eyrolles, Paris, 1970 6. G. Bomford. Geodesy, 4th edn., Clarendon Press, Oxford, 1980 7. J.-C. Husson, A. Cazenave, J.-F. Minster (Eds.). Internal Geophysics and Space, CNES/Cepadues-Editions, Toulouse, 1985 8. V.I. Arnold. Mathematical Methods of Classical Mechanics, Graduate Texts in Mathematics (60), Springer-Verlag, Berlin, 1989 9. W. Torge. Geodesy, Walter de Gruyter, Berlin, 1991 10. G. Seeber. Satellite Geodesy, Walter de Gruyter, Berlin, 1993 11. E.W. Grafarend, F.W. Krumm, V.S. Schwarze (Eds.). Geodesy: The Challenge of the 3rd Millennium, Springer, Berlin, 2003 12. H. Stephani. Relativity: An Introduction to Special and General Relativity,Cam- bridge University Press, Cambridge, 2004 13. G. Schubert (Ed.). Treatise on Geodephysics,Vol.3:Geodesy, Elsevier, Oxford, 2007 14. D.D. McCarthy, P.K. -
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.