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Organisational Structure, Programme Production and Audience
OBSERVATOIRE EUROPÉEN DE L'AUDIOVISUEL EUROPEAN AUDIOVISUAL OBSERVATORY EUROPÄISCHE AUDIOVISUELLE INFORMATIONSSTELLE http://www.obs.coe.int TELEVISION IN THE RUSSIAN FEDERATION: ORGANISATIONAL STRUCTURE, PROGRAMME PRODUCTION AND AUDIENCE March 2006 This report was prepared by Internews Russia for the European Audiovisual Observatory based on sources current as of December 2005. Authors: Anna Kachkaeva Ilya Kiriya Grigory Libergal Edited by Manana Aslamazyan and Gillian McCormack Media Law Consultant: Andrei Richter The analyses expressed in this report are the authors’ own opinions and cannot in any way be considered as representing the point of view of the European Audiovisual Observatory, its members and the Council of Europe. CONTENT INTRODUCTION ...........................................................................................................................................6 1. INSTITUTIONAL FRAMEWORK........................................................................................................13 1.1. LEGISLATION ....................................................................................................................................13 1.1.1. Key Media Legislation and Its Problems .......................................................................... 13 1.1.2. Advertising ....................................................................................................................... 22 1.1.3. Copyright and Related Rights ......................................................................................... -
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........................................................ -
Deep Space Network Ission Suppo
870-14, Rev. AF Deep Space Network ission Suppo Jet Propulsion Laboratory California institute of Technology JPL 0-0787,Rev. AF 870-14, Rev. AF October 1991 Deep Space Network ission Support Re uirements Reviewed by: L.M. McKinley TDA Mission Support Off ice Approved by: R.J. Amorose Manager, TDA Mission Support Jet Propulsion Laboratory California Institute of Technology JPL 0-0787, Rev. AF 870.14. Rev . AF CONTENTS INTRODUCTION............................................................ 1-1 A . PURPOSE AND SCOPE ................................................. 1-1 B . REVISION AND CONTROL .............................................. 1-1 C . ORGANIZATION OF DOCUMENT 870-14 ................................... 1-1 D . ABBREVIATIONS ..................................................... 1-1 ASTRO-D ................................................................. 2-1 BROADCASTING SATELLITE-3A AND -3B (BS-3A AND -3B) ....................... 3-1 CRAF/CASSINI (c/c)...................................................... 4-1 COSMIC BACKGROUND EXPLORER (COBE)....................................... 5-1 DYNAMICS EXPLORER-1 (DE-1).............................................. 6-1 EARTH RADIATION BUDGET SATELLITE (ERBS)................................. 7-1 ENGINEERING TEST SATELLITE-VI (ETS-VI).................................. 8-1 EUROPEAN TELECOMMUNICATIONS SATELLITE I1 (EUTELSAT 11) .................. 9-1 EXTREME ULTRAVIOLET EXPLORER (EWE)..................................... 10-1 FRENCH DIRECT TV BROADCAST SATELLITE (TDF-1 AND -2) .................... -
秘书处 Distr.: General 2 March 2004 Chinese Original: French
联合国 ST/SG/SER.E/445 秘书处 Distr.: General 2 March 2004 Chinese Original: French 和平利用外层空间委员会 依照《关于登记射入外层空间物体的公约》递交的资料 2004 年 1 月 28 日法国常驻联合国(维也纳)代表团 致秘书长的普通照会 法国常驻联合国(维也纳)代表团向联合国秘书长致意,并谨依照《关于 登记射入外层空间物体的公约》(大会第 3235(XXIX)号决议附件)第四条的 规定,转交法国 1965 年至 2003 年期间发射的空间物体的资料(见附件)。本 资料取代法国以往提交的登记数据。 V.04-51401 (C) GY 100504 110504 *0451401* 2 附件 ST/SG/SER.E/445 法国登记的空间物体数据,1965-2003 年 表 1 法国登记的空间物体数据,1965-1978 年 基本轨道特点 发射装置 交点周期 倾角 远地点 近地点 登记号 发射日期 发射场 类型 (分) (度) (公里) (公里) 空间物体的一般功用 1965 年 1965 096 A 1965 年 11 月 26 日 阿尔及利亚,阿马吉尔 Diamant 99 59.7 797 663 A1 号试验卫星 1965 096 B 1965 年 11 月 26 日 阿尔及利亚,阿马吉尔 Diamant 105 34.3 1 479 516 Diamant 号发射装置推进级 1965 096 C 1965 年 11 月 26 日 阿尔及利亚,阿马吉尔 Diamant 97 34.3 787 453 不起作用的发射装置组件 1965 096 D 1965 年 11 月 26 日 阿尔及利亚,阿马吉尔 Diamant 95 34.2 619 425 不起作用的发射装置组件 1966 年 1966 013 A 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 115 34.1 2 398 498 Diapason D1 号试验卫星 1966 013 B 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 113 34.1 2 239 497 Diamant 号发射装置推进级 1966 013 C 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 95 34.1 555 433 不起作用的发射装置组件 1966 013 D 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 95 34.1 693 377 不起作用的发射装置组件 1966 013 E 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 92 34.1 435 268 不起作用的发射装置组件 1966 013 F 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 91 34.1 325 280 不起作用的发射装置组件 1966 013 G 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 101 34.1 1 206 472 不起作用的发射装置组件 1966 013 H 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant - 34.1 722 433 不起作用的发射装置组件 1966 013 J 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 92 34.1 386 352 不起作用的发射装置组件 1966 013 K 1966 年 2 月 17 日 阿尔及利亚,阿马吉尔 Diamant 107 34.1 1 674 475 不起作用的发射装置组件 1966 -
NASA NASA - NSSDC - Spacecraft - Query Results
Cronología de Lanzamientos Espaciales Año 1988 Recopilación de datos Ing. Eladio Miranda Batlle. Los textos, imágenes y tablas fueron obtenidos de la National Space Science. Data Center. NASA NASA - NSSDC - Spacecraft - Query Results Saturday, 05 February 2011 NSSDC Master Catalog Search Spacecraft Experiments Data Collections Spacecraft Query Results Personnel Publications There were 144 spacecraft returned. Maps Spacecraft Name NSSDC ID Launch Date New/Updated Data Astra 1A 1988-109B 1988-12-11 Lunar/Planetary Events Buran 1988-100A 1988-11-15 Cosmos 1908 1988-001A 1988-01-06 Cosmos 1909 1988-002A 1988-01-15 Cosmos 1910 1988-002B 1988-01-15 Cosmos 1911 1988-002C 1988-01-15 Cosmos 1912 1988-002D 1988-01-15 Cosmos 1913 1988-002E 1988-01-15 Cosmos 1914 1988-002F 1988-01-15 Cosmos 1915 1988-004A 1988-01-26 Cosmos 1916 1988-007A 1988-02-03 Cosmos 1917 1988-009A 1988-02-18 Cosmos 1918 1988-009B 1988-02-18 Cosmos 1919 1988-009C 1988-02-18 Cosmos 1920 1988-010A 1988-02-18 Cosmos 1921 1988-011A 1988-02-19 Cosmos 1922 1988-013A 1988-02-26 Cosmos 1923 1988-015A 1988-03-10 Cosmos 1924 1988-016A 1988-03-11 Cosmos 1925 1988-016B 1988-03-11 Cosmos 1926 1988-016C 1988-03-11 Cosmos 1927 1988-016D 1988-03-11 Cosmos 1928 1988-016E 1988-03-11 Cosmos 1929 1988-016F 1988-03-11 Cosmos 1930 1988-016G 1988-03-11 Cosmos 1931 1988-016H 1988-03-11 Cosmos 1932 1988-019A 1988-03-14 Cosmos 1933 1988-020A 1988-03-15 Cosmos 1934 1988-023A 1988-03-22 Cosmos 1935 1988-025A 1988-03-24 Cosmos 1936 1988-027A 1988-03-30 Cosmos 1937 1988-029A 1988-04-05 Cosmos 1938 1988-030A -
Daniel F.Hastings Assoc
France and Japan in Space: Niche Market Players, with Evolving Assets and Roles by Damon R. Wells B.S., University of Oklahoma (1984) Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE IN TECHNOLOGY AND POLICY at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY September 1991 @ Damon R. Wells, 1991. All rights reserved. The author hereby grants to MIT permission to reproduce and to distribute copies of this thesis document in whole or in part. Author......................:'...... ... ::............................. ........ Department of Aýetics and Astronautics August, 1991 Certified by ................................................ .................. ..... Leon Trilling Professor, Aeronautics and Astronautics Thesis Supervisor Certified by .......................... ... ... Os......... ... .. Daniel F.Hastings Assoc. Professor, Aeronautics and Astronautics Thesis Supervisor Accepted by...... * .......... .• ..... ;.•...... * .. -..-..'. ......... Prof. Richard de Neufville ,, Cqhajr anjTechnology and Policy Program A A. r1A.L.~j~L.~LL U)..... .U .. P6f: HUirold Y. Wachman Chairman, Departmental Graduate Committee SEP- 21 4 1991 Aam France and Japan in Space: Niche Market Players, with Evolving Assets and Roles by Damon R. Wells Submitted to the Department of Aeronautics and Astronautics on August, 1991, in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE IN TECHNOLOGY AND POLICY Abstract This thesis examines the nature, capabilities, and growth policies of the increasingly successful French and Japanese space programs, with an emphasis on their strate- gies for competing with the larger U.S. and Soviet programs. Toward that end, information and analyses are first presented with respect to the context and policy environment for the programs, including such issues as program structure, funding patterns, overall program goals, and the more general trends in each nation regard- ing high technology policies. -
Proton (UR-500) Family Home Launch Vehicles USSR / Russia
Please make a donation to support Gunter's Space Page. Thank you very much for visiting Gunter's Space Page. I hope that this site is useful a nd informative for you. If you appreciate the information provided on this site, please consider supporting my work by making a simp le and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much. Proton (UR-500) family Home Launch Vehicles USSR / Russia Proton Proton-K Proton-K Blok-D (Zond L1) Proton-K Blok-D-1 (Granat) [ILS] Proton-K Blok-DM-2 Proton-K Blok-DM1 (Inmarsat-3 F3) similar: Proton-K Blok-D, Proton-K Blok-D-2 Proton-K Blok-DM2 Proton-K Blok-DM3 Proton-M Briz-M (Thor 5) [ILS] similar: Proton-K Blok-DM-5 similar: Proton-K Blok-DM4, similar: Proton-K Briz-M Proton-K Blok-DM-2M Version Stage 1 Stage 2 Stage 3 Stage 4 Proton (8K82) 8S810 / 6 × RD-253 8S811 / 3 × RD-0208 + 1 × RD-0209 - - Proton-K (8K82K) 8S810 / 6 × RD-253 8S811 / 3 × RD-0210 + 1 × RD-0211 8S812 / RD-0212 - Proton-K Blok-D (8K82K 11S824) 8S810 / 6 × RD-253 8S811 / 3 × RD-0210 + 1 × RD-0211 8S812 / RD-0212 Blok-D / RD-58 Proton-K Blok-D-1 (8K82K 11S824M) 8S810 / 6 × RD-253 8S811 / 3 × RD-0210 + 1 × RD-0211 8S812 / RD-0212 Blok-D-1 / RD-58M Proton-K Blok-D-2 (8K82K 11S824F) 8S810 / 6 × RD-253 8S811 / 3 × RD-0210 + 1 × RD-0211 8S812 / RD-0212 Blok-D-2 / RD-58M Proton-K Blok-DM (8K82K 11S86) 8S810 / 6 × RD-253 8S811 / 3 × RD-0210 + 1 × RD-0211 8S812 / RD-0212 Blok-DM / RD-58M Proton-K Blok-DM-2 (8K82K 11S861) 8S810 / 6 × RD-253 8S811 / 3 × RD-0210 + 1 × RD-0211 8S812 -
Federal Space Agency of Russia Activity of Russian
FEDERAL SPACE AGENCY OF RUSSIA ACTIVITY OF RUSSIAN FEDERATION ON SPACE DEBRIS PROBLEM 44-th session of the Scientific and Technical Subcommittee of the UN Committee on the Peaceful Uses of Outer Space (COPOUS) Vienna - February, 2007 1 FEDERAL SPACE AGENCY OF RUSSIA • Federal Space Agency of Russia continues consecutive activity in the field of space debris problems. This work concerns the safety of spacecraft and International Space Station, the latest one in a especial meaning. • The activity on debris mitigation is being carried out within the framework of Russian National Legislation, taking into account the dynamics of similar measures and practices of other space-faring nations. • Since 2000 designers and operators of spacecraft and orbital stages are in charge to follow the requirements of Federal Space Agency Standard "Space Technology Items. General Requirements for Mitigation of Space Debris Population" in all projects of space vehicles being again developed. 2 FEDERAL SPACE AGENCY OF RUSSIA DYNAMICS OF LAUNCHES IN RUSSIA AND IN OTHER STATES AND ORGANIZATIONS 3 FEDERAL SPACE AGENCY OF RUSSIA Totally 25 launches of various purposes were realized by Russia in 2006 The launchers used in 2006 are listed in the table. / Launcher Type Apogee Motor Number of Type of Orbit Launchings 1 “Proton-K" “DM" 2 Circular 2 “Proton-M" “Briz-M" 3 + 1*) MEO 3 “Soyuz-U” 6 Circular 4 "Soyuz-FG" " Fregat" 2 Circular 5 "Soyuz-2 (1a)" " Fregat" 2 Circular 6 "Soyuz-2 (1b)" " Fregat" 1 Circular 7 " Molniya-M" 1 Highly elliptic orbit 8 “Tsiklon-2" 1 Circular 9 " Kosmos-3M" 1 Circular 10 “Start-1" 1 Circular 11 " Dnepr" 1 + 1**) Circular 12 " Shtil" 1 Circular 13 " Rokot " “Briz-" 1 Circular Total: 25 *) – Emergency on February 28, 2006 **) – Emergency on July 28, 2006 4 FEDERAL SPACE AGENCY OF RUSSIA THE NET OF OPTICAL MEANS OF RUSSIAN ACADEMY OF SCIENCES AND THE OTHER OBSERVATORIES FOR OBSERVATION OF SPACECRAFT AND SPACE DEBRIS IN GEOSTATIONARY REGION Scientific optical network • The net of optical means consists of 12 observatories from Bolivia to Ussuriysk. -
About the Associate Administrator for Commercial Space Transportation (Ast) and the Commercial Space Transportation Advisory Committee (Comstac)
2000 COMMERCIAL SPACE TRANSPORTATION FORECASTS Federal Aviation Administration’s Associate Administrator for Commercial Space Transportation (AST) and the Commercial Space Transportation Advisory Committee (COMSTAC) May 2000 ABOUT THE ASSOCIATE ADMINISTRATOR FOR COMMERCIAL SPACE TRANSPORTATION (AST) AND THE COMMERCIAL SPACE TRANSPORTATION ADVISORY COMMITTEE (COMSTAC) The Federal Aviation Administration’s senior executives from the U.S. commercial Associate Administrator for Commercial Space space transportation and satellite industries, Transportation (AST) licenses and regulates U.S. space-related state government officials, and commercial space launch activity as authorized other space professionals. by Executive Order 12465, Commercial Expendable Launch Vehicle Activities, and the The primary goals of COMSTAC are to: Commercial Space Launch Act of 1984, as amended. AST’s mission is to license and • Evaluate economic, technological and regulate commercial launch operations to ensure institutional issues relating to the U.S. public health and safety and the safety of commercial space transportation industry property, and to protect national security and foreign policy interests of the United States • Provide a forum for the discussion of issues during commercial launch operations. The involving the relationship between industry Commercial Space Launch Act of 1984 and the and government requirements 1996 National Space Policy also direct the Federal Aviation Administration to encourage, • Make recommendations to the Administrator facilitate, and promote commercial launches. on issues and approaches for Federal policies and programs regarding the industry. The Commercial Space Transportation Advisory Committee (COMSTAC) provides Additional information concerning AST and information, advice, and recommendations to the COMSTAC can be found on AST’s web site, at Administrator of the Federal Aviation http://ast.faa.gov. -
5 Orbit and Ground Track of a Satellite
5 Orbit and Ground Track of a Satellite 5.1 Position of the Satellite on its Orbit Let (O; x, y, z) be the Galilean reference frame already defined. The satellite S is in an elliptical orbit around the centre of attraction O. The orbital plane P makes a constant angle i with the equatorial plane E. However, although this plane P is considered as fixed relative to in the Keplerian motion, in a real (perturbed) motion, it will in fact rotate about the polar axis. This is precessional motion,1 occurring with angular speed Ω˙ , as calculated in the last two chapters. A schematic representation of this motion is given in Fig. 5.1. We shall describe the position of S in using the Euler angles. 5.1.1 Position of the Satellite The three Euler angles ψ, θ and χ were introduced in Sect. 2.3.2 to specify the orbit and its perigee in space. In the present case, we wish to specify S. We obtain the correspondence between the Euler angles and the orbital elements using Fig. 2.1: ψ = Ω, (5.1) θ = i, (5.2) χ = ω + v. (5.3) Although they are fixed for the Keplerian orbit, the angles Ω, ω and M − nt vary in time for a real orbit. The inclination i remains constant, however. The distance from S to the centre of attraction O is given by (1.41), expressed in terms of the true anomaly v : a(1 − e2) r = . (5.4) 1+e cos v 1 The word ‘precession’, meaning ‘the action of preceding’, was coined by Coper- nicus around 1530 (præcessio in Latin) to speak about the precession of the equinoxes, i.e., the retrograde motion of the equinoctial points. -
Gennaio 2019
Organo Ufficiale della Unione Radioamatori Italiani Sperimentazione - Volontariato - Protezione Civile Anno 4° - N. 28 Gennaio 2019 Organo Ufficiale della Unione Radioamatori Italiani Sperimentazione - Volontariato - Protezione Civile Anno 4° - N. 28 Gennaio 2019 EXECUTIVE DIRECTOR I0SNY Nicola Sanna COLLABORATORS IZ3KVD Giorgio Laconi, I0PYP Marcello Pimpinelli, IZ0EIK Erica Sanna, ZS6YE Heather Holland, I6GII Antonio Fucci, I5DOF Franco Donati, I0KBL Leonardo Benedetti, IK8HEQ Dorina Piscopo, IW0SAQ Gianni Santevecchi, I6RKB Giuseppe Ciucciarelli, IK8ESU Domenico Caradonna, IK1VHX Bruno Lusuriello, IZ6DWH Salvatore Latorre, IU8HTS Giuseppe Cuomo, JH3DMQ Munehiro Mizutani, IK1GJH Massimo Servente, IK8MEY Angelo Maffongelli, IK8HIS Luigi Colucci, IK0IXI Fabio Bonucci, EA4EQ Juan Carlos Calvo, XE1FSD Luis Adolfo, F4DHQ Sophie Malhomme, IW2NOD Emanuele Cogliati, IU2IFW Pasquale Fabrizio Salerno, IT9CEL Santo Pittalà, IK5KID Massimo Marras, IK1WGZ Simone Accili, Fabio Teoli, IN3UFW Marco Paglionico, IZ1XBB Pier Paolo Liuzzo, IT9GCG Enzo Cuppone, IT9JPW Marco Mora, IT9FDB Salvatore De Filippi, IU1ATT Nancy Gentile, IK8HVO Antonio Migliaccio, IZ8XJJ Giovanni Iacono, Bernardeta Grochowska, IZ3NVM Andrea Galvani, IZ8QMF Paolo Guadagno, SV3RND Mario Ragagli, IZ0VLL Salvatore Mele, IS0JXO Antonio Solinas, IW8PGT Francesco Ciacco, IK1YLO Alberto Barbera, IW1RFH Ivan Greco, IU5CJP Massimiliano Casucci, IK0ELN Giovanni Lorusso, IT9DSA Antonino Di Bella, IW6DTM Alberto Tallevi, IW1AXG Luciano Seeber, IZ1HHT Giorgio Guala, IU3BZW Carla Granese, IK3GES -
General Assembly Distr.: General 17 December 1999
United Nations A/AC.105/734 General Assembly Distr.: General 17 December 1999 Original: English Committee on the Peaceful Uses of Outer Space Disposal of satellites in geosynchronous orbit Report by the Secretariat Contents Paragraphs Page I. Introduction ....................................................... 1-2 2 II. Standards and recommendations on geosynchonous satellite disposal ........ 3-8 2 III. Examples of the GSO disposal policy .................................. 9-15 3 A. Intelsat....................................................... 10 3 B. Canadian Space Agency ......................................... 11-12 4 C. Centre National d’Etudes Spatiales................................ 13 4 D. European Space Agency ........................................ 14 4 E. EUMETSAT.................................................. 15 4 IV. Situation near the geostationary orbit................................... 16-20 4 V. Conclusions ....................................................... 21 5 Annex. Statistical data....................................................................... 6 V.99-91115 (E) A/AC.105/734 I. Introduction (b) Every reasonable effort should be made to shorten the lifetime of debris in the transfer orbit; 1. At its forty-second session, the Committee on the (c) A geostationary satellite at the end of its life Peaceful Uses of Outer Space agreed1 that the Scientific should be transferred, before complete exhaustion of its and Technical Subcommittee, at its thirty-seventh session, propellant, to a supersynchronous