CTR Spring 1993, In-Orbit Testing, V.23
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Satellite Systems
Chapter 18 REST-OF-WORLD (ROW) SATELLITE SYSTEMS For the longest time, space exploration was an exclusive club comprised of only two members, the United States and the Former Soviet Union. That has now changed due to a number of factors, among the more dominant being economics, advanced and improved technologies and national imperatives. Today, the number of nations with space programs has risen to over 40 and will continue to grow as the costs of spacelift and technology continue to decrease. RUSSIAN SATELLITE SYSTEMS The satellite section of the Russian In the post-Soviet era, Russia contin- space program continues to be predomi- ues its efforts to improve both its military nantly government in character, with and commercial space capabilities. most satellites dedicated either to civil/ These enhancements encompass both military applications (such as communi- orbital assets and ground-based space cations and meteorology) or exclusive support facilities. Russia has done some military missions (such as reconnaissance restructuring of its operating principles and targeting). A large portion of the regarding space. While these efforts have Russian space program is kept running by attempted not to detract from space-based launch services, boosters and launch support to military missions, economic sites, paid for by foreign commercial issues and costs have lead to a lowering companies. of Russian space-based capabilities in The most obvious change in Russian both orbital assets and ground station space activity in recent years has been the capabilities. decrease in space launches and corre- The influence of Glasnost on Russia's sponding payloads. Many of these space programs has been significant, but launches are for foreign payloads, not public announcements regarding space Russian. -
Descendants of Joseph Randolph
Descendants of Joseph Randolph Generation 1 1. JOSEPH 1 RANDOLPH was born in 1750 in Spotsylvania County, VA. He died in 1810 in SC or GA. He married NANCY TURMAN . Notes for Joseph Randolph: Was a private in Revolutionary War. Joseph Randolph and Nancy Turman had the following child: 2. i. PEYTON SKIPWITH 2 RANDOLPH was born in 1792 in VA. He died on Jan 19, 1867. He married ELIZABETH FIELDS . She was born in 1796. She died on Apr 13, 1873. Generation 2 2. PEYTON SKIPWITH 2 RANDOLPH (Joseph 1) was born in 1792 in VA. He died on Jan 19, 1867. He married ELIZABETH FIELDS . She was born in 1796. She died on Apr 13, 1873. Notes for Peyton Skipwith Randolph: Died of pneumonia Notes for Elizabeth Fields: Died of pneumonia Peyton Skipwith Randolph and Elizabeth Fields had the following child: 3. i. PEYTON CALLAHAN 3 RANDOLPH was born on May 11, 1832. He died on Dec 03, 1893. He married Sarah Wallis Gilbert on Nov 15, 1869. She was born on Dec 17, 1839 in Saulsbury, TN. She died on Nov 02, 1931 in Mississippi. Generation 3 3. PEYTON CALLAHAN 3 RANDOLPH (Peyton Skipwith 2, Joseph 1) was born on May 11, 1832. He died on Dec 03, 1893. He married Sarah Wallis Gilbert on Nov 15, 1869. She was born on Dec 17, 1839 in Saulsbury, TN. She died on Nov 02, 1931 in Mississippi. Peyton Callahan Randolph and Sarah Wallis Gilbert had the following children: i. BENJAMIN FRANKLIN 4 RANDOLPH was born on Apr 07, 1870. -
Sts-51G Press Kit June 1985
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION SPACE SHUTTLE MISSION STS-51G PRESS KIT JUNE 1985 ARABSAT A; MORELOS A; TELSTAR 3-D; SPARTAN 1 Edited by Richard W. Orloff, 01/2001/Page 1 STS-5IG INSIGNIA S85-31266 -- The STS-51G insignia illustrates the advances in aviation technology in the United States within a relatively short span of the twentieth century. The flags of the French (Baudry) and Saudi Arabian (Al-Saud) payload specialists appear next to their name at the bottom of the insignia. The NASA insignia design for space shuttle flights is reserved for use by the astronauts and for other official use as the NASA Administrator may authorize. Public availability has been approved only in the form of illustrations by the various news media. When and if there is any change in this policy, which we do not anticipate, it will be publicly announced. PHOTO CREDIT: NASA or National Aeronautics and Space Administration. Edited by Richard W. Orloff, 01/2001/Page 2 RELEASE NO: 85-8 June 1985 CONTACTS Charles Redmond/Sarah Keegan Headquarters, Washington, DC (Phone: 202/453-8590) James Elliott Goddard Space Flight Center, Greenbelt, MD (Phone: 301/344-6256) David Alter Johnson Space Center, Houston, TX (Phone: 713/483-5111) Jim Ball Kennedy Space Center, FL (Phone: 305/867-2468) Ralph Jackson Dryden Flight Research Facility, Edwards, CA (Phone: 805/258-8381) Edited by Richard W. Orloff, 01/2001/Page 3 RELEASE NO: 85-83 June 1985 CONTENTS GENERAL RELEASE 5 51-G BRIEFING SCHEDULE 7 GENERAL INFORMATION 8 SHUTTLE MISSION 51-G -- QUICK LOOK FACTS -
Classification of Geosynchronous Objects
esoc European Space Operations Centre Robert-Bosch-Strasse 5 D-64293 Darmstadt Germany T +49 (0)6151 900 www.esa.int CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Produced with the DISCOS Database Prepared by ESA’s Space Debris Office Reference GEN-DB-LOG-00211-OPS-GR Issue 20 Revision 0 Date of Issue 28 May 2018 Status Issued Document Type Technical Note Distribution ESA UNCLASSIFIED - Limited Distribution European Space Agency Agence spatiale europeenne´ Abstract This is a status report on geosynchronous objects as of 1 January 2018. Based on orbital data in ESA’s DISCOS database and on orbital data provided by KIAM the situation near the geostationary ring is analysed. From 1523 objects for which orbital data are available (of which 0 are outdated, i.e. the last available state dates back to 180 or more days before the reference date), 519 are actively controlled, 795 are drifting above, below or through GEO, 189 are in a libration orbit and 19 are in a highly inclined orbit. For 1 object the status could not be determined. Furthermore, there are 59 uncontrolled objects without orbital data (of which 54 have not been cata- logued). Thus the total number of known objects in the geostationary region is 1582. If you detect any error or if you have any comment or question please contact: Stijn Lemmens European Space Agency European Space Operations Center Space Debris Office (OPS-GR) Robert-Bosch-Str. 5 64293 Darmstadt, Germany Tel.: +49-6151-902634 E-mail: [email protected] Page 1 / 187 European Space Agency CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Agence spatiale europeenne´ Date 28 May 2018 Issue 20 Rev 0 Table of contents 1 Introduction 3 2 Sources 4 2.1 USSTRATCOM Two-Line Elements (TLEs) . -
Loral Space & Communications
LORAL SPACE & COMMUNICATIONS LTD FORM 10-K (Annual Report) Filed 3/31/1997 For Period Ending 12/31/1996 Address 600 THIRD AVE C/O LORAL SPACECOM CORP NEW YORK, New York 10016 Telephone 212-697-1105 CIK 0001006269 Industry Electronic Instr. & Controls Sector Technology Fiscal Year 12/31 SECURITIES AND EXCHANGE COMMISSION WASHINGTON, D.C. 20549 FORM 10-K TRANSITION REPORT PURSUANT TO SECTION 13 OR 15(d) OF THE SECURITIES EXCHANGE ACT OF 1934 FOR THE TRANSITION PERIOD FROM APRIL 1, 1996 TO DECEMBER 31, 1996 Commission file number 1-14180 LORAL SPACE & COMMUNICATIONS LTD. 600 Third Avenue New York, New York 10016 Telephone: (212) 697-1105 Jurisdiction of incorporation: Bermuda IRS identification number: 13-3867424 Securities registered pursuant to Section 12(b) of the Act: NAME OF EACH EXCHANGE TITLE OF EACH CLASS ON WHICH REGISTERED - ------------------------------------------------------------------ ------------------------ Common Stock, $.01 par value...................................... New York Stock Exchange The registrant has filed all reports required to be filed by Section 13 or 15(d) of the Securities Exchange Act of 1934 during the preceding 12 months or such shorter period as the registrant was required to file such reports and has been subject to such filing requirements for the past 90 days. Disclosure of delinquent filers pursuant to Item 405 of Regulation S-K is contained in the registrant's definitive proxy statement incorporated by reference in Part III of this Form 10-K. At February 28, 1997, 191,092,308 common shares were outstanding, and the aggregate market value of such shares (based upon the closing price on the New York Stock Exchange) held by non-affiliates of the registrant was approximately $3 billion. -
CABLE SATELLITES : the NEXT GENERATION Issues Facing Cable Operators and Programmers
CABLE SATELLITES : THE NEXT GENERATION Issues Facing Cable Operators and Programmers Robert Zitter Home Box Office, Inc. A development that will impact the ABSTRACT cable industry is the FCC mandate to phase-in a uniform 2-degree spacing The deployment of next-generation between U.S. domestic satellites. The satellites in compliance with the FCC's intent of the plan is to alleviate uniform 2-degree spacing plan, together overcrowding in the U.S. orbital arc. It with the movement of cable times the deployment of next generation programming, will occur during the next satellites with improvements in ground two years. A discussion of the transition station receiving characteristics in order scenario, the technical differences in the to control the ensuing increase in new satellites, and ground station adjacent satellite interference. requirements reveals that Cable TV and SMATV facilities will require This paper discusses the satellite reconfiguration and in some cases and orbital changes that are expected to replacement may be necessary. The occur during the next two years, and satellite movement and programming presents some critical issues and transfers in the early nineties compel the challenges facing satellite programmers cable industry to examine the future and cable operators . performance of existing facilities. o Time of Replacements In the early days, 4-degrees of separation within the two segments o Introduction assigned to U.S. domestic communication satellites -- 70 to I 04 C-Band satellites have become a degrees and 117 to 143 degrees West reliable means of delivery for cable Longitude (oWL) -- consisting of 15 television programs and have played an satellite slots were found adequate. -
Classification of Geosynchronous Objects
esoc European Space Operations Centre Robert-Bosch-Strasse 5 D-64293 Darmstadt Germany T +49 (0)6151 900 www.esa.int CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Produced with the DISCOS Database Prepared by T. Flohrer & S. Frey Reference GEN-DB-LOG-00195-OPS-GR Issue 18 Revision 0 Date of Issue 3 June 2016 Status ISSUED Document Type TN European Space Agency Agence spatiale europeenne´ Abstract This is a status report on geosynchronous objects as of 1 January 2016. Based on orbital data in ESA’s DISCOS database and on orbital data provided by KIAM the situation near the geostationary ring is analysed. From 1434 objects for which orbital data are available (of which 2 are outdated, i.e. the last available state dates back to 180 or more days before the reference date), 471 are actively controlled, 747 are drifting above, below or through GEO, 190 are in a libration orbit and 15 are in a highly inclined orbit. For 11 objects the status could not be determined. Furthermore, there are 50 uncontrolled objects without orbital data (of which 44 have not been cata- logued). Thus the total number of known objects in the geostationary region is 1484. In issue 18 the previously used definition of ”near the geostationary ring” has been slightly adapted. If you detect any error or if you have any comment or question please contact: Tim Flohrer, PhD European Space Agency European Space Operations Center Space Debris Office (OPS-GR) Robert-Bosch-Str. 5 64293 Darmstadt, Germany Tel.: +49-6151-903058 E-mail: tim.fl[email protected] Page 1 / 178 European Space Agency CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Agence spatiale europeenne´ Date 3 June 2016 Issue 18 Rev 0 Table of contents 1 Introduction 3 2 Sources 4 2.1 USSTRATCOM Two-Line Elements (TLEs) . -
Commercial Spacecraft Mission Model Update
Commercial Space Transportation Advisory Committee (COMSTAC) Report of the COMSTAC Technology & Innovation Working Group Commercial Spacecraft Mission Model Update May 1998 Associate Administrator for Commercial Space Transportation Federal Aviation Administration U.S. Department of Transportation M5528/98ml Printed for DOT/FAA/AST by Rocketdyne Propulsion & Power, Boeing North American, Inc. Report of the COMSTAC Technology & Innovation Working Group COMMERCIAL SPACECRAFT MISSION MODEL UPDATE May 1998 Paul Fuller, Chairman Technology & Innovation Working Group Commercial Space Transportation Advisory Committee (COMSTAC) Associative Administrator for Commercial Space Transportation Federal Aviation Administration U.S. Department of Transportation TABLE OF CONTENTS COMMERCIAL MISSION MODEL UPDATE........................................................................ 1 1. Introduction................................................................................................................ 1 2. 1998 Mission Model Update Methodology.................................................................. 1 3. Conclusions ................................................................................................................ 2 4. Recommendations....................................................................................................... 3 5. References .................................................................................................................. 3 APPENDIX A – 1998 DISCUSSION AND RESULTS........................................................ -
<> 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 -
COMSAT Technical Review
COMSAT Technical Review Volume 17 Number 1, Spring 1987 Advisory Board Joseph V. Charyk COMSAT TECHNICAL REVIEW John V. Evans Spring 1987 Editorial Board Geoffrey Hyde, Chairman Volume 17 Number 1 , Richard A. Arndt Ali E. Atia S. Joseph Campanella I DESIGN AND MODELING OF A GaAs MONOI.I'THIC 2- TO 6-GHz Dattakumar M. Chitre R. K. Gupta , .1. H. Reynolds, Russell J. Fang FEEDBACK AMPLIFIER Howard W. Flieger M. C. Fu , AND T. Heikkila Melvyn Grossman 23 A 120-Mbit/s TDMA QPSK MODEM FOR ON-BOARD APPLICATIONS Ivor N. Knight , AND F. T. Assal Larry C. Palmer R. G. Egri , K. Karimullab Edward E. Reinhart 55 AN ADAPTIVE EQUALIZER FOR 120-Mblt/s QPSK TRANSMISSION David V. Rogers Hans J. Weiss J. M. Kappes Albert E. Williams 87 MODULATION SELECTION FOR ILL MOBILE SATELI,FI'F EXPERIMENT Pier L. Bargellini, Editor Emeritus (MSAT-X) K. M. Mackenthun Editorial Staff MANAGING EDITOR Margaret B. Jacocks 105 HURWrrZ STABII .II'Y ANALYSIS OF AN ADPCM SYSTEM TECHNICAL EDITORS S. Dimolitsas AND U. Bhaskar Barbara J. Wassell Diane Haugen APPROXIMATIONS FOR THE RAISED COSINE FILTER PRODUCTION 127 POLE-ZERO J. J. Poklemba Barbara J. Wassell FAMILY Louis P. Stephens, Jr. 159 A SIMULATION STUDY OF RAIN ATTENUATION AND DIVERSITY EFFECTS CIRCULATION LINKS J. Mass Shirley H. Taylor ON SATELLITE COMSAT TECHNICAL REVIEW is published twice a year by 189 PROGRAMMABL E CONVOLUTIONAL ENCODER AND THRESHOLD Communications Satellite Corporation (COMSAT). Subscriptions, DECODER J. S. Snyder which include the two issues published within a calendar year, are: one year, $15 U.S.; two years, $25; three years, $35; 201 CTR NOTE : GEOSTATIONARY SATELLITE LOG FOR YEAR END 1986 single copies, $10; article reprints, $2.50. -
CONGRESS of the INTERNATIONAL ASTRONAUTICAL FEDERATION BUDAPEST HUNGARY 10-15 OCTOBER 1983 M M XXXIV CONGRESS of the INTERNATIONAL ASTRONAUTICAL FEDERATION
INIS-jnf—8969 BUDAPLCi <*» CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION BUDAPEST HUNGARY 10-15 OCTOBER 1983 m m XXXIV CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION ABSTRACTS OF PAPERS BUDAPEST, HUMGABr Oct. 10-15, FOREWORD Abstracts included in this book art ordered according to the IAF nuuber assigned to each paper eooepted for presentation at XZZI? IAP Congress. Experience hae shown that the chosen arrangement is the nost conrenient one and allows the easiest access to the abstraots. The IA? paper nuBber can be found in the Final Programe of the Congress under: - the Technical Session,wbere the paper is presented - the author's name, listed at the end of the Programe. The Abstracts of the Student Conference and of Space Law Colloquium are at the end of this book. Abstracts of papers arriTed later than August 1st are not included in thie collection. ftingarian Astronautieal Society - 2 - IAr-83~O1 EXOSAT/DELTA - DEMONSTRATED SHORT-TERM BACKUP LAUIfCHER CAPABILITY THROUGH INTERNATIONAL COOPERATION by J. K. Oanoung, Manager, Spacecraft Integration, Delta Program McDonnell Douglas Astronautics Company G. Altnann, EXOSAT Project Manager, European Space Agency P. Eaton, Chief, Expendable Launch Vehicle Programs National Aeronautics and Space Administration J. D. Kraft, Delta Mission Analysis and Integration Manager, National Aeronautics and Space Administration ABSTRACT An important exploration of eosnie x-ray sources currently under wey Wan made possible by a unique example of international cooperation. The EXOSAT spacecraft, designed, developed, qualified, and prepared for launch by the European Space Agency (ESA), was successfully launched by the National Aeronautics and Space Administration (NASA) Delta launch vehicle in May 1983* EXOSAT was originally scheduled for launch on the European Ariane rocket, but due to unforeseen schedule realignments, ESA, in cooperation with NASA, selected the Delta for this mission in February 1983. -
China Dream, Space Dream: China's Progress in Space Technologies and Implications for the United States
China Dream, Space Dream 中国梦,航天梦China’s Progress in Space Technologies and Implications for the United States A report prepared for the U.S.-China Economic and Security Review Commission Kevin Pollpeter Eric Anderson Jordan Wilson Fan Yang Acknowledgements: The authors would like to thank Dr. Patrick Besha and Dr. Scott Pace for reviewing a previous draft of this report. They would also like to thank Lynne Bush and Bret Silvis for their master editing skills. Of course, any errors or omissions are the fault of authors. Disclaimer: This research report was prepared at the request of the Commission to support its deliberations. Posting of the report to the Commission's website is intended to promote greater public understanding of the issues addressed by the Commission in its ongoing assessment of U.S.-China economic relations and their implications for U.S. security, as mandated by Public Law 106-398 and Public Law 108-7. However, it does not necessarily imply an endorsement by the Commission or any individual Commissioner of the views or conclusions expressed in this commissioned research report. CONTENTS Acronyms ......................................................................................................................................... i Executive Summary ....................................................................................................................... iii Introduction ................................................................................................................................... 1