Table of Artificial Satellites Launched in 1972
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Satellite Situation Report
NASA Office of Public Affairs Satellite Situation Report VOLUME 17 NUMBER 6 DECEMBER 31, 1977 (NASA-TM-793t5) SATELLITE SITUATION~ BEPORT, N8-17131 VOLUME 17, NO. 6 (NASA) 114 F HC A06/mF A01 CSCL 05B Unclas G3/15 05059 Goddard Space Flight Center Greenbelt, Maryland NOTICE .THIS DOCUMENT HAS'BEEN REPRODUCED FROM THE BEST COPY FURNISHED US BY THE SPONSORING AGENCY. ALTHOUGH IT IS RECOGNIZED THAT CERTAIN PORTIONS' ARE ILLEGIBLE, IT IS BEING RELEASED IN THE INTEREST OF MAKING AVAILABLE AS MUCH INFORMATION AS POSSIBLE. OFFICE OF PUBLIC AFFAIRS GCDDARD SPACE FLIGHT CENTER NATIONAL AERONAUTICS AND SPACE ADMINISTRATION VOLUME 17 NO. 6 DECEMBER 31, 1977 SATELLITE SITUATION REPORT THIS REPORT IS PUBLIShED AND DISTRIBUTED BY THE OFFICE OF PUBLIC AFFAIRS, GSFC. GODPH DRgP2 FE I T ERETAO5MUJS E SMITHSONIAN ASTRCPHYSICAL OBSERVATORY. SPACEFLIGHT TRACKING AND DATA NETWORK. NOTE: The Satellite Situation Report dated October 31, 1977, contained an entry in the "Objects Decayed Within the Reporting Period" that 1977 042P, object number 10349, decayed on September 21, 1977. That entry was in error. The object is still in orbit. SPACE OBJECTS BOX SCORE OBJECTS IN ORBIT DECAYED OBJECTS AUSTRALIA I I CANACA 8 0 ESA 4 0 ESRO 1 9 FRANCE 54 26 FRANCE/FRG 2 0 FRG 9 3 INCIA 1 0 INDONESIA 2 0 INTERNATIONAL TELECOM- MUNICATIONS SATELLITE ORGANIZATION (ITSO) 22 0 ITALY 1 4 JAPAN 27 0 NATC 4 0 NETHERLANDS 0 4 PRC 6 14 SPAIN 1 0 UK 11 4 US 2928 1523 USSR 1439 4456 TOTAL 4E21 6044 INTER- CBJECTS IN ORIT NATIONAL CATALOG PERIOD INCLI- APOGEE PERIGEE TQANSMITTTNG DESIGNATION NAME NUMBER SOURCE LAUNCH MINUTES NATION KM. -
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 -
Asa R-/ 130090
rl),,; ASA R-/130090 The University of Texas at Dallas Final Technical Report NASA Contract NAS 5-9075 on Measurement of the Degree of Anisotropy of the Cosmic Radiation Using the IMP Space Vehicle by R. A. R. Palmeira and F. R. Allum The University of Texas at Dallas Dallas, Texas This report was prepared for submission to NASA/Goddard Space Flight Center in partial fulfillment of the terms of the Contract NAS 5-9075. October 1972 (NASA-CR-130090 ) MEASUREMENT OF THE DEGREE N72-3376 OF ANISOTROPY OF THE COSMIC RADIATION USING 8 THE IMP SPACE VEHICLE Final Technical Report R.A.R. Palmeira, et al (Texas Unclas Univ.) Oct. 1972 31 p CSCL 03B G3/29 45262 The University of Texas at Dallas Final Technical Report on "Measurement of the Degree of Anisotropy of the Cosmic Radiation Using the IMP Space Vehicle" NASA Contract NAS 5-9075 by R.A.R. Palmeira and F. R. Allum The University of Texas at Dallas, Dallas, Texas INTRODUCTION This report describes the detector and data reduction techniques used in connection with the UTD cosmic-ray experiments designed for and flown on board the Explorer 34 and 41 satellites. It is intended to supplement and summarize the more detailed information supplied during the course of the program, including but not restricted to the information contained in the contractually required Monthly Technical Reports submitted throughout the duration of the program. This final technical report is divided into three categories: i) a brief history of the UTD program development; ii) a description of the particle detectors and the methods of data analysis; and iii) present status of data processing. -
Proceedings of the Nimbus Program Review
X-650-62-226 J, / N63 18601--N 63 18622 _,_-/ PROCEEDINGS OF THE NIMBUS PROGRAM REVIEW OTS PRICE XEROX S _9, ,_-_ MICROFILM $ Jg/ _-"/_j . J"- O NOVEMBER 14-16, 1962 PROCEEDINGS OF THE NIMBUS PROGRAM REVIEW \ November 14-16, 1962 GODDARD SPACE FLIGHT CENTER Greenbelt, Md. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION GODDARD SPACE FLIGHT CENTER PROCEEDINGS OF THE NIMBUS PROGRAM REVIEW FOREWORD The Nimbus program review was conducted at the George Washington Motor Lodge and at General Electric Missiles and Space Division, Valley Forge, Pennsylvania, on November 14, 15, and 16, 1962. The purpose of the review was twofold: first, to present to top management of the Goddard Space Flight Center (GSFC), National Aeronautics and Space Administration (NASA) Headquarters, other NASA elements, Joint Meteorological Satellite Advisory Committee (_MSAC), Weather Bureau, subsystem contractors, and others, a clear picture of the Nimbus program, its organization, its past accomplishments, current status, and remaining work, emphasizing the continuing need and opportunity for major contributions by the industrial community; second, to bring together project and contractor technical personnel responsible for the planning, execution, and support of the integration and test of the spacecraft to be initiated at General Electric shortly. This book is a compilation of the papers presented during the review and also contains a list of those attending. Harry P_ress Nimbus Project Manager CONTENTS FOREWORD lo INTRODUCTION TO NIMBUS by W. G. Stroud, GSFC _o THE NIMBUS PROJECT-- ORGANIZATION, PLAN, AND STATUS by H. Press, GSFC o METEOROLOGICAL APPLICATIONS OF NIMBUS DATA by E.G. Albert, U.S. -
Geological Applications of Nimbus Radiation Data in the Middle East
X-901-76-164 GEOLOGICAL APPLICATIONS OF NIMBUS RADIATION DATA IN THE MIDDLE EAST (NASI-TM-X-71207) GEOLOGICAL APPLICATIONS N77-10616 OF NIMBUS RADIATION DATA IN MIDDLE EAST (NASA) 106 p HC A06/MF 101 CSCL 08G Unclas G3/43 09624 LEWIS J. ALLISON OCTOBER 1976 GODDARD SPACE FLIGHT CENTER I GREENBELT, MARYLAND For information concerning availability of this document contact. Technical Information &Administrative Support Division Code 250 Goddard Space Night Center Greenbelt, Maryland 20771 (Telephone 301-982-4488) "This paper presents the views of-the author(s), and does not necessarily reflect the views of the Goddard Space Flight Center, or NASA." X-901-76-164 GEOLOGICAL APPLICATIONS OF NIMBUS RADIATION DATA IN THE MIDDLE EAST Lewis J. Allison Meteorology Program Office October 1976 GODDARD SPACE FLIGHT CENTER Greenbelt, Maryland GEOLOGICAL APPLICATIONS OF NIMBUS RADIATION DATA IN THE MIDDLE EAST Lewis J. Allison Goddard Space Flight Center Greenbelt, Maryland 20771 ABSTRACT Large plateaus of Eocene limestone and exposed limestone escarp ments, in Egypt and Saudi Arabia respectively, were indicated by cool brightness temperatures TB < 2400 to 2650 K by the Nimbus 5 Electrically Scanning Microwave Radiometer (ESMR) over a 2-year period. Nubian sandstone, desert eolian sand and igneous metamorphic rocks of the Pliocene, Miocene, Oligocene and Cretaceous period were differentiated from these limestone areas by warm TB values (> 2650 to 300'K). These brightness tempera ture differences are a result of seasonal in-situ ground tempera tures and differential emissivity of limestone (0. 7) and sand, sandstone and granite (0. 9) whose dielectric constants are (6 to 8.9) and (2.9 and 4.2 to 5.3) respectively at 19.35 GHz. -
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. -
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. -
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 -
Solar-Terrestrial Models and Application Software
NSSDC/WDC-A-R&S 90-19 Solar-Terrestrial Models and Application Software Dieter Bflitza July 1990 National Space Science Data Center/ World Data Center A for Rockets and Satellites CONTENTS Introduction ............................................................................................................................. Ionosphere ................................................................................................................................ General Models 2-3 Intemational Reference Ionosphere ............................................................................ Electron Density Models Chiu Ionospheric Model ............................................................................................... 2- 4 Bent Ionospheric Model ............................................................................................... 2- 5 Penn State Mk Ill Model ............................................................................................... 2- 6 SLIM Model ................................................................................................................... 2- 7 FAIM Model .................................................................................................................. 2- 7 F2-Peak Models and Applications CCIRfoF2 and M(3000)F2 Model Maps ........................................................................ 2- 8 2-9 URSI foF2 Model Maps ................................................................................................. 2-10 ISS-b foF2 Maps .......................................................................................................... -
A Y' 1969-Deeber 1972
- -7 5, 41, AN MA 969-DECEMBER43 D 47 197 AY' 1969-DEEBER 1972 S(NASA-TM-X-70481) TRAJECTORIES OF N73-33809 EXPLORERS 33, 35, 41, 43 AND 47, MAY 1969 - DEC. 1972 (NASA) 72 p HC $5.75 CSCL 22C Unclas "f -" G3/30 19441 D.' -'.FAIRFIELD K. W. BEAANNON( R. P LEPPING N. F. NESS "NFORMATN SERVI-E i -- SSpringfield, _ e te. VA.o Com 22151 e 1 AR -SPAC FLIGHT CETER S-ENBET MA RYLAND -N 14 N- TRAJECTORIES OF EXPLORERS 33, 35, 41, 43 and 47 May 1969-Dec 1972 D.H. Fairfield K.W. Behannon R.P. Lepping N.F. Ness Laboratory for Extraterrestrial Physics Goddard Space Flight Center Greenbelt, Maryland October 1973 /0 This document represents a continuation of a previous document (Behannon et al. 1970) and is presented with the intention that it will stimulate and facilitate correlative studies of data from various spacecraft. Figures 1-54 consist primarily of solar ecliptic plane projections of orbits of five different satellites although a limited number of XZ projections are shown to illustrate the large excursions of Explorer 33 away from the ecliptic plane. Nominal positions of the magnetopause and bow shock are included for reference. The plots are intended only to represent the trajectory of the spacecraft and imply nothing about the operational status of the various experiments nor the availability of the data. Information on these latter points can be ob- tained from the National Space Science Data Center, (e.g. King, 1971). It should be pointed out, however, that Explorers33 and 35 were very long lived spacecraft (> 2 yrs) and numerous experiments either ceased operation or exhibited a gradual deterioration during the extended lifetime.