Satellites We R E Within I - 1000 Km (About 600 Miles ) of GT-4 Spacecraft at the Time Ao Tronaut
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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 -
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 ........................................................................................................................... -
NASA News 01 National Aeronautics and Space Administration Washington, D.C
NASA News 01 National Aeronautics and Space Administration Washington, D.C. 20546 AC 202 755-8370 (0 3 For Release: o *[J£ Bill Pomeroy 00 c« Headquarters, Washington, D.C, 3 P. M., WEDNESDAY, Dfn (Phone: 202/755-8370) October 10, 1979 in ^ Ken Atchison 0 Headquarters, Washington, D.C, (Phone: 202/755-2497) a RELEASE NO: 79-126 a PEGASUS 2 REENTRY EXPECTED IN NOVEMBER w The Pegasus 2 spacecraft assembly, launched by NASA in 1965, is expected to reenter the Earth's atmosphere on or about Nov. 5, according to notification given NASA by the North American Air Defense Command. The command compiles information on satellite payloads, rocket bodies and other orbiting pieces that could survive the friction and heat of reentry and impact on Earth. Pegasus 2, launched May 25, 1965, was used to gather micrometeoroid data for use in the design of spacecraft. -more- -2- It was one of three such spacecraft, all launched in 1965. Pegasus 1 reentered Sept. 17, 1978, over Africa and Pegasus 3 reentered Aug. 4, 1969, over the Pacific Ocean. The Pegasus 2 assembly weighs about 10,430 kilograms (23,000 pounds) and is 21 meters (70 feet) long. The space- craft itself weighs about 1,450 kg (3,200 lb.). It is attached to the empty S-IV stage and the instrument unit of the Saturn I launch vehicle. None of the sections has any radioactive nuclear power sources or materials aboard. It is estimated that approximately 9,705 kg (21,400 lb.) of orbital hardware will be destroyed by reentry heating. -
John F. Kennedy Space Center, Operations and Checkout Building) First Street, Between Avenue D and Avenue E Cape Canaveral Brevard County Florida
CAPE CANAVERAL AIR FORCE STATION, LAUNCH COMPLEX 39, HAER FL-8-11-E ALTITUDE CHAMBERS FL-8-11-E (John F. Kennedy Space Center, Operations and Checkout Building) First Street, between Avenue D and Avenue E 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, LAUNCH COMPLEX 39, ALTITUDE CHAMBERS, (John F. Kennedy Space Center, Operation & Checkout Building) HAERNo. FL-8-11-E Location: Within the Operations and Checkout Building High Bay First Street, between Avenue D and Avenue E Cape Canaveral Brevard County Florida U.S.G.S. 7.5. minute Cape Canaveral, Florida, quadrangle, Universal Transverse Mercator coordinates: 17.534600.3155100 Date of Installation: 1965 Designer/ Manufacturer: Stokes Equipment Division of the Pennsalt Chemical Corporation (now Pennwalt Corporation), Philadelphia, Pennsylvania Installer: Pittsburgh Des Moines Steel Corporation; Elsbery Corporation; Fischer Electric Corporation Present Owner: National Aeronautics and Space Administration (NASA) Kennedy Space Center, FL 32899-0001 Present Use: Test facility (Chamber R); inactive (Chamber L) Significance: The two Altitude Chambers sit within the High Bay of the Operations and Checkout (O&C) Building. The O&C Building is located in the Industrial Area of the John F. Kennedy Space Center (KSC). The O&C Building was listed in the National Register of Historic Places (NRHP) in 2000 in recognition of its exceptional importance at the national level in the context of the Apollo program, for which it was used to assemble and test the Apollo spacecraft before launching. -
Water Sprays Inspace Retrieval Operations
ASTRONAUTICS RESEARCH REPORT NO. 77-2 (NASA-CR-149885) WATER SPRAYS IN SPACE N77-20128 RETRIEVAL OPERATIONS (Pennsylvania State CSCL 22A Univ.) 68 p HC A04/MF A01 Unclas G3/13 21653 WATER SPRAYS INSPACE RETRIEVAL OPERATIONS BY DOUGLAS C.FREESLAND PROJECT ASSISTANT -ASTRONAUTICS RESEARCH> THE PENNSYLVANIA STATE UNIVERSITY Department of Aerospace Engineering - J233 Hammond Building University Park, Pennsylvania 16802 APRIL 1977 , RESEARCH SUPPORTED BY NASA GRANT NSG-7078 ABSTRACT Recent experiments involving liquid jets exhausting into a vacuum have led to significant conclusions regarding techniques for detumbling and despinning disabled spacecraft during retrieval oper ations. A fine water spray directed toward a tumbling or spinning object may quickly form ice over its surface. The added mass of water will absorb angular momentum and slow the vehicle. As this ice sublimes it carries momentum away with it. Thus, a complete detumble or despin is possible by simply spraying water at a disabled vehicle. Experiments were conducted in a ground based vacuum chamber to deter mine physical properties of water-ice in a space-like environment. Additional ices, alcohol and ammonia, were also studied. An analytical analysis based on the conservation of angular momentum, resulted in despin performance parameters, i.e., total water mass requirements and despin times. The despin and retrieval of a disabled spacecraft was considered to illustrate a potential application of the water spray technique. TABLE OF CONTENTS Page ABSTRACT .... 11 LIST OF TABLES . Iv LIST OF FIGURES..................... v NOMENCLATURE . ......................... V ACKNOWLEDGMENTS....................... vi1 I. INTRODUCTION........................1 1.1 Historical Development ............. .... 1 1.2 Water Spray Technique .......... ...... 3 1 3 Purpose and Objectives .......... -
NASA Is Not Archiving All Potentially Valuable Data
‘“L, United States General Acchunting Office \ Report to the Chairman, Committee on Science, Space and Technology, House of Representatives November 1990 SPACE OPERATIONS NASA Is Not Archiving All Potentially Valuable Data GAO/IMTEC-91-3 Information Management and Technology Division B-240427 November 2,199O The Honorable Robert A. Roe Chairman, Committee on Science, Space, and Technology House of Representatives Dear Mr. Chairman: On March 2, 1990, we reported on how well the National Aeronautics and Space Administration (NASA) managed, stored, and archived space science data from past missions. This present report, as agreed with your office, discusses other data management issues, including (1) whether NASA is archiving its most valuable data, and (2) the extent to which a mechanism exists for obtaining input from the scientific community on what types of space science data should be archived. As arranged with your office, unless you publicly announce the contents of this report earlier, we plan no further distribution until 30 days from the date of this letter. We will then give copies to appropriate congressional committees, the Administrator of NASA, and other interested parties upon request. This work was performed under the direction of Samuel W. Howlin, Director for Defense and Security Information Systems, who can be reached at (202) 275-4649. Other major contributors are listed in appendix IX. Sincerely yours, Ralph V. Carlone Assistant Comptroller General Executive Summary The National Aeronautics and Space Administration (NASA) is respon- Purpose sible for space exploration and for managing, archiving, and dissemi- nating space science data. Since 1958, NASA has spent billions on its space science programs and successfully launched over 260 scientific missions. -
NASA, the First 25 Years: 1958-83. a Resource for the Book
DOCUMENT RESUME ED 252 377 SE 045 294 AUTHOR Thorne, Muriel M., Ed. TITLE NASA, The First 25 Years: 1958-83. A Resource for Teachers. A Curriculum Project. INSTITUTION National Aeronautics and Space Administration, Washington, D.C. REPORT NO EP-182 PUB DATE 83 NOTE 132p.; Some colored photographs may not reproduce clearly. AVAILABLE FROMSuperintendent of Documents, Government Printing Office, Washington, DC 20402. PUB TYPE Books (010) -- Reference Materials - General (130) Historical Materials (060) EDRS PRICE MF01 Plus Postage. PC Not Available from EDRS. DESCRIPTORS Aerospace Education; *Aerospace Technology; Energy; *Federal Programs; International Programs; Satellites (Aerospace); Science History; Secondary Education; *Secondary School Science; *Space Exploration; *Space Sciences IDENTIFIERS *National Aeronautics and Space Administration ABSTRACT This book is designed to serve as a reference base from which teachers can develop classroom concepts and activities related to the National Aeronautics and Space Administration (NASA). The book consists of a prologue, ten chapters, an epilogue, and two appendices. The prologue contains a brief survey of the National Advisory Committee for Aeronautics, NASA's predecessor. The first chapter introduces NASA--the agency, its physical plant, and its mission. Succeeding chapters are devoted to these NASA program areas: aeronautics; applications satellites; energy research; international programs; launch vehicles; space flight; technology utilization; and data systems. Major NASA projects are listed chronologically within each of these program areas. Each chapter concludes with ideas for the classroom. The epilogue offers some perspectives on NASA's first 25 years and a glimpse of the future. Appendices include a record of NASA launches and a list of the NASA educational service offices. -
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. -
Satellite Situation Report
X-537-65-217 SPACE OPERATIONS CONTROL CENTER SATELLITE SITUATION REPORT VOL. 6, NO. 2 DqG-iRA JANUARY 31, 1966 GODDARD SPACE FLIGHT CENTER 209 GREENBELT, ME). (ACCESSION NUMER) (THUI G) (PAGES) (CODE) NATIONALRpoduced by TEC-NICAL .. /.INFORMATION SERVICE NA 4O 0.TR US Dopar t O Commo.e NA GRO T RR (CATiGORY) SpringleIld, VA. 22151 to"AncR SPACE OPERATIONS CONTROL CENTER GODDARD SPACE FLIGHT CENTER NATIONAL AERONAUTICS AND SPACE ADMINISTRATION VOLUME 6, NO. 2 JANUARY 31, 1966 SATELLITE SITUATION REPORT THE FOLLOWING REPORT REFLECTS DATA COMPUTED AND COMPILED BY THE GODDARD SPACE FLIGHT CENTER, NORAD, AND THE SMITHSONIAN ASTROPHYSICAL OBSERVATORY AS OF 1200Z ON JANUARY 31, 1966 OBJECTS IN ORBIT CATALOGUE PERIOD INGLI- APOGEE PERIGEE TRANSMITTING OBJECT CODE NAME NUMBER SOURCE LAUNCH MINUTES NATION Km. Km. FREQ. (MC/S) 1958 LAUNCHES ALPHA I EXPLORER 1 004 US 1 FEB 103.8 33.18 1536 341 BETA 1 ROCKET BODY 016 us 17 MAR 138.4 34.26 4326 641 BETA 2 VANGUARD 1 005 US 17 MAR 134.0 34.22 3938 650 BETA 3 1576 Us 17 MAR 132.7 34.20 3826 651 1959 LAUNCHES ALPHA 1 VANGUARD 2 011 US 17 FEB 125.4 32.87 3283 557 ALPHA 2 ROCKET BODY 0L2 US 17 FEB 129.7 32.91 3661 551 ETA 1 VANGUARD 3 020 US 18 SEP 129.8 33.33 3714 512 MU 1 LUNIK 1 112 USSR 2 JAN HELIOCENTRIC ORBIT NU I PIONEER 4 113 US 3 MAR HELIOCENTRIC ORBIT IOTA 1 EXPLORER 7 022 US 13 OCT I01.i 50.33 1074 551 IOTA 2 ROCKET BODY 023 US 13 OCT 100.9 50.31 1047 554 1960 LAUNCHES ALPHA I PIONEER 5 027 US 11 MAR HELIOCENTRIC ORBIT BETA 1 ROCKET BODY 028 US 1 APR 99.1 48.39 740 690 BETA 2 TIROS 1 029 US -
The NASA/National Space Science Data Center Trapped
https://ntrs.nasa.gov/search.jsp?R=19930001815 2020-03-17T09:43:31+00:00Z NSSDC/WDC-A-R&S 91-29 The NASA/National Space Science Data Center Trapped Radiation Environment Model Program (1964-1991) James I. Vette November 1991 National Space Science Data Center (NSSDC) World Data Center A for Rockets and Satellites (WDC-A-R&S) National Aeronautics and Space Administration Goddard Space Flight Center Greenbelt, Maryland 20771 Contents L Introduction ........................................................................................................................... 1 2. Historical Background and Purpose of Program ................................................................... 3 3. Philosophy and Approach ...................................................................................................... 5 4. Summary of Accomplishments ............................................................................................. 7 5. A View of the Future .............................................................................................................. 11 Knowledge of Trapped Protons .................................................................................... 1] Knowledge of Energetic Electrons ............................................................................... 13 Prospective Data for Near-Term Modeling ................................................................. 16 The Long-Term View .................................................................................................... 18 6. Appendix: -
GSFG OP~RATIONS, CONTROL L:C-ENTER
/ r / ,, - ) 'J " ' I I • I ,. ·; GSFG OP~RATIONS , CONTROL l: C-ENTER / X I Mercer I ( I ~ N'OVEMBER ' 30, 1'969 I Rob.... ---:--:----'---,-------'- GODDARD. SPACE FliGHT CENTIR GREENBELT, MD. / OBJECTS IN ORBIT CATALOGUE PERIOD I NCLI- APOGEE= PERIGEE TRANSMITTING OBJECT CODE NAME NUMBER SOURCE LAUNCH MINUTES NATION KM. KM . FRE Q. I MC/S l 1958 LAUNCHES ALPHA 1 EXPLORER 1 4 us 1 FEB 94.6 3.1 690 305 BETA 1 16 us 17 r~AR 138.3 34.2 4307 652 RETA 2 VANGUARD 1 5 us 17 t~AR 133.8 34.2 3929 650 BEiA 3 157A us 17 I~AR 132.1 34.2 3772 66() 1959 LAUNCH ES ALPHA 1 VANGlJARD 2 11 us 17 FEF\ 125.1 32.8 3256 556 ALPHA 2 1? us 17 FER 129.3 3?..9 3630 55'5 f.TA 1 VAN GI JARD 3 20 us 18 SEP 129.4 33.3 3680 512 I OTA 1 EXP LORER 7 2?. lJS 13 OCT 100.9 50.3 1052 550 IIJTA 2 23 tJS 13 OCT 100.3 50.3 1006 545 MU 1 LlJ NIK 1 11? US SR 2 JAN HELIOCENTRIC ORBIT 1\J U 1 PIONEF.R 4 113 us 3 MAR HELIOCENTRIC ORBIT 19AO LA IJMCHES ALPHA 1 PI 01\1f"ER 5 27 liS 11 r~AR HELIOCENTRIC ORBIT Rf' TA 1 ?.P. tJS 1 APR 98.8 4R.3 726 683 RE TA ?. TIRns 1 29 liS 1 APR 99.1 48.3 740 691 Rf"T A. -
Nasa Cr 6 12 78
https://ntrs.nasa.gov/search.jsp?R=19690020432 2020-03-12T03:45:20+00:00Z W 60 29810 NASA CR 6 1278 NASA CONTRACTOR NASA CR-61278 REPORT April 8, 1969 PREFEASIBILITY STUDY OF A SPACE ENVIRONMENT MONITORING SYSTEM (SEMOS) Prepared under Contract No. NAS 8-20082 by Chou, ChihKang, B. D. DeBaryshe, A. S. Hill, and M. C. Thadani NORTHROP SPACE LABORATORIES For NASA-GEORGE C. MARSHALL SPACE FLIGHT CENTER Marshall Space Flight Center, Alabama April 8, 1969 NASA CR-6 1278 PREFEASIBILITY STUDY OF A SPACE ENVIRONMENT MONITORING SYSTEM (SEMOS) Chou, ChihKang, B. D. DeBaryshe, A. S. Hill, and M. C. Thadani Prepared under Contract No. NAS 8-20082 by NORTHROP SPACE LABORATORIES Huntsville, Alabama For Ae ro-As trodynamic s Laboratory Distribution of this report is provided in the interest of information exchange. Responsibility for the contents resides in the author or organization that prepared it. NASA-GEORGE C. MARSHALL SPACE FLIGHT CENTER a FOREWORD Although this report was prepared in early 1966, it contains ideas and concepts which may still be of value in planning future aerospace environment measuring programs. The work reported was accomplished to assess the need for a space environment monitoring system and briefly develop the requirements and some possible concepts. The material con- tained in this report represents only pre-feasibility considerations and reflects the ideas and opinions from representatives of many private firms, universities, and government organizations at the time (March 1966). The report is published to document the effort as a contribution to future endeavors on the subject. iii PREFACE ‘rliis report was prepared by the Northrop Corporation, Norair Division, North r op Space Laboratories, Huntsville, Alabama, under .