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L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Human Spaceflight Plans of Russia, China and India
Presentation to the ASEB Committee on NASA Technology Roadmaps Panel on Human Health and Surface Exploration June 1, 2011 by Marcia S. Smith Space and Technology Policy Group, LLC Russia Extensive experience in human spaceflight First animal in space (1957), first man in space (1961), first woman in space (1963), first spacewalk (1965), first space station (1971) Seven successful space stations (Salyut 1, 3, 4, 5, 6, 7 and Mir) before partnering in International Space Station (ISS) No people beyond low Earth orbit (LEO), however For earth orbit, continues to rely on Soyuz, first launched in 1967, but upgraded many times and is key to ISS operations Designed space shuttle, Buran, but launched only once in automated mode (no crew) in 1988 06-01-2011 2 Russia (2) Existing reliable launch vehicles Proton is largest: 21 tons to LEO; 5.5 tons to geostationary transfer orbit (GTO) Attempts to build Saturn V-equivalent in 1960s and 1970s failed (N1 failed four times in four attempts 1969-1972) Energiya booster in 1980s only flew twice (1987 with Polyus and 1988 with Buran). Abandoned for financial reasons. Was 100 tons to LEO; 18-20 tons to GTO; 32 tons to lunar trajectory. RD-170 engines for Energiya’s strap-ons live on today in other forms for Zenit, Atlas V, and Angara (under development) 06-01-2011 3 Russia (3) Robotic planetary space exploration mixed Excellent success at – Moon (Luna and Lunokhod series, plus Zond circumlunar flights) Venus (Venera series) Halley’s Comet (Vega 1 and 2—also Venus) Jinxed at Mars More than a dozen failures in 1960s - 1970s Partial success with Phobos 2 in 1988 (Phobos 1 failed) Mars 96 failed to leave Earth orbit Phobos-Grunt scheduled for later this year; designed as sample return from Phobos (includes Chinese orbiter) 06-01-2011 4 Russia (4) Grand statements over decades about sending people to the Moon and Mars, but never enough money to proceed. -
Proton Accident with GLONASS Satellites
3/29/2018 Proton accident with GLONASS satellites Previous Proton mission: SES6 PICTURE GALLERY A Proton rocket with the Block D 11S861 stage and 813GLN34 payload firing shortly before liftoff on July 2, 2013. Upcoming book on space exploration Read more and watch videos in: Site map Site update log About this site About the author The illfated Proton rocket lifts off on July 2, 2013, at 06:38:21.585 Moscow Time (July 1, 10:38 p.m. EDT). The rocket crashed approximately 32.682 seconds later, Roskosmos said on July 18, 2013. Mailbox Russia's Proton crashes with a trio of navigation satellites SUPPORT THIS SITE! Published: July 1; updated: July 2, 3, 4, 5, 9, 11, 15, 18, 19; 23; Aug. 11 Related pages: Russia's Proton rocket crashed less than a minute after its liftoff from Baikonur, Kazakhstan. A ProtonM vehicle No. 53543 with a Block DM03 (11S86103) upper stage lifted off as scheduled from Pad No. 24 at Site 81 (launch complex 8P882K) in Baikonur Cosmodrome on July 2, 2013, at 06:38:21.585 Moscow Time (on July 1, 10:38 p.m. EDT). The rocket started veering off course right after leaving the pad, deviating from the vertical path in various RD253/275 engines directions and then plunged to the ground seconds later nose first. The payload section and the upper stage were sheered off the vehicle moments before it impacted the ground and exploded. The flight lasted no more than 30 seconds. Searching for details: The Russian space agency's ground processing and launch contractor, TsENKI, was broadcasting the launch live and captured the entire process of the vehicle's disintegration and its crash. -
KOREASAT 6 Ku-Band Commercial Communications Satellite
KOREASAT 6 Ku-band Commercial Communications Satellite GEO Communications FACTS AT A GLANCE Mission Description Coverage: Orbital ATK teamed with Thales Alenia Space of France to supply the KOREASAT 6 commercial Korea communications satellite for KT Corporation of the Republic of Korea. Orbital ATK provided its GEOStar-2™ satellite platform; carried out engineering, manufacturing, integration and final spacecraft testing at its satellite manufacturing facility located in Dulles, Virginia; and performed launch site operations in Kourou, French Guiana. Thales Alenia Space was prime contractor for the project and provided the communications payload. In addition, the team delivered a ground system to support on- orbit operations of the satellite. Orbital ATK provided six months of on-site support after the satellite was handed over to the customer. KOREASAT 6 carries 24 Ku-band channels to provide Fixed Satellite Services (FSS) and six channels for Direct Broadcast Services (DBS) to the people of Korea. The spacecraft generates 3.4 kilowatts of Mission: payload power and has a 15-year on-orbit mission life. KOREASAT 6 was launched in December 2010 Ku-band communications to provide to a final orbital slot at 116 degrees East Longitude. Direct Broadcast Services (DBS) and Fixed Satellite Services (FSS) The GEOStar™ Advantage Customer: Orbital ATK’s highly successful Geosynchronous Earth Orbit (GEO) communications satellites are based KT Corporation on the company’s GEOStar spacecraft platform, which is able to accommodate all types of commercial (Thales Alenia Space – Prime communications payloads and is compatible with all major commercial launchers. The company’s Contractor) GEOStar product line includes the GEOStar-2 design, which is optimized for smaller satellite missions that can support up to 5.0 kilowatts of payload power. -
Igor AFANASYEV, Dmitry VORONTSOV Cosmonautics | Event
cosmonautics | event Andrey Morgunov Igor AFANASYEV, Dmitry VORONTSOV AANGARA’SNGARA’S FFIRSTIRST BBLASTOFFLASTOFF At 16.04 hrs Moscow time on 9 July 2014, the Plesetsk space launch centre saw the launching facility in February 2014 to the first launch of the Angara-1.2PP launch vehicle of the advanced space rocket practice its fuelling and the nose fairing was family being developed by the Khrunichev state space research and production fitted on the rocket in March. The successful ground tests were followed by the prelaunch centre. The maiden blastoff conducted as part of the Angara flight test programme preparations. was aimed at testing the solutions embodied in the design of the URM-1 and URM-2 The date of the launch was put off for versatile rocket modules and the Angara’s launch and technical facilities as well. 27 June 2014 due to extra checks required. In this connection, orbiting an actual spacecraft had not been considered, with On 9 June, Khrunichev hosted a session of an inseparable full-scale mock-up used as payload. The flight was suborbital to the Chief Designers Council, dedicated to prevent cluttering near-Earth orbit with space junk. the preparation of the Angara to its flight tests. The session pronounced the rocket fit To say the Angara’s first launch had been In spite of the hurdles, the developer, for the trials. anticipated for a long time would be an nevertheless, got in the stretch with the Angara The LV had been taken out of the assembly understatement: it was slated for 2005 under programme. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Evolved Expendable Launch Operations at Cape Canaveral, 2002-2009
EVOLVED EXPENDABLE LAUNCH OPERATIONS AT CAPE CANAVERAL 2002 – 2009 by Mark C. Cleary 45th SPACE WING History Office PREFACE This study addresses ATLAS V and DELTA IV Evolved Expendable Launch Vehicle (EELV) operations at Cape Canaveral, Florida. It features all the EELV missions launched from the Cape through the end of Calendar Year (CY) 2009. In addition, the first chapter provides an overview of the EELV effort in the 1990s, summaries of EELV contracts and requests for facilities at Cape Canaveral, deactivation and/or reconstruction of launch complexes 37 and 41 to support EELV operations, typical EELV flight profiles, and military supervision of EELV space operations. The lion’s share of this work highlights EELV launch campaigns and the outcome of each flight through the end of 2009. To avoid confusion, ATLAS V missions are presented in Chapter II, and DELTA IV missions appear in Chapter III. Furthermore, missions are placed in three categories within each chapter: 1) commercial, 2) civilian agency, and 3) military space operations. All EELV customers employ commercial launch contractors to put their respective payloads into orbit. Consequently, the type of agency sponsoring a payload (the Air Force, NASA, NOAA or a commercial satellite company) determines where its mission summary is placed. Range officials mark all launch times in Greenwich Mean Time, as indicated by a “Z” at various points in the narrative. Unfortunately, the convention creates a one-day discrepancy between the local date reported by the media and the “Z” time’s date whenever the launch occurs late at night, but before midnight. (This proved true for seven of the military ATLAS V and DELTA IV missions presented here.) In any event, competent authorities have reviewed all the material presented in this study, and it is releasable to the general public. -
SOYUZ THROUGH the AGES the R-7 Rocket That Led to the Family of Soyuz Vehicles Launching Today Lifted Off for the First Time Onfeb
RUSSIAN SPACE SOYUZ THROUGH THE AGES The R-7 rocket that led to the family of Soyuz vehicles launching today lifted off for the first time onFeb. 17, 1959. The last launch, on Dec. 27, 2018, was number 1,898. Irene Klotz and Maxim Pyadushkin Vostochny Cosmodrome anufactured by the Progress Rocket Space Center in Sama- Evolution of Soyuz-Family Launch Vehicles ra, Russia, the medium-lift expendable booster originally was used for Soviet-era human space missions and later became the R-7 Soyuz Soyuz-L workhorse for the country’s civilian and military space programs. M 1957 First launch of the ICBM (SS-6 1966-76 (32 launches, 1970-71 (three launches, Sapwood) that served as a basis for including 30 successful, all successful, The first rocket officially named Soyuz was launched in Soviet/Russian launch vehicles from Baikonur) from Baikonur) 1966 and has since flown 1,050 times, of which 1,023 were including the Soyuz family successful. Production of Soyuz rockets peaked in the early Soyuz 1980s at about 60 vehicles per year. Medium-Class Launch Vehicle Russia began offering Soyuz launch services internationally in the mid-1980s through Glavkosmos, a commercial entity set up to sell Soviet rocket and space technologies. Manufacturer: Progress Rocket Space Soyuz-U/-U2 Soyuz-M Center, Samara, Russia In 1996, Russia created Starsem, a joint venture (35% ArianeGroup, 25% Roscosmos, 25% RKTs Progress, 15% 1991 Breakup of the 1973-2017 1971-76 (eight launches, Soviet Union, (859 launches, including all successful, from Plesetsk) Dimensions Arianespace) that had exclusive rights to provide commercial launch services on Soyuz launch vehicles. -
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........................................................ -
U S E R M a N U
•Introduction 6/04/01 11:09 Page 1 SOYUZ USER’ S MANUAL ST-GTD-SUM-01 - ISSUE 3 - REVISION 0 - APRIL 2001 © Starsem 2001. All rights reserved. •Introduction 6/04/01 11:09 Page 2 •Introduction 6/04/01 11:09 Page 3 SOYUZ USER’S MANUAL ST-GTD-SUM-01 ISSUE 3, REVISION 0 APRIL 2001 FOREWORD Starsem is a Russian-European joint venture founded in 1996 that is charged with the commercialization of launch services using the Soyuz launch vehicle, the most frequently launched rocket in the world and the only manned vehicle offered for commercial space launches. Starsem headquarters are located in Paris, France and the Soyuz is launched from the Baikonour Cosmodrome in the Republic of Kazakhstan. Starsem is a partnership with 50% European and 50% Russian ownership. Its shareholders are the European Aeronautic, Defence, and Space Company, EADS (35%), Arianespace (15%), the Russian Aeronautics and Space Agency, Rosaviacosmos (25%), and the Samara Space Center, TsSKB-Progress (25%). Starsem is the sole organization entrusted to finance, market, and conduct the commercial sale of the Soyuz launch vehicle family, including future upgrades such as the Soyuz/ST. Page3 •Introduction 6/04/01 11:09 Page 4 SOYUZ USER’S MANUAL ST-GTD-SUM-01 ISSUE 3, REVISION 0 APRIL 2001 REVISION CONTROL SHEET Revision Date Revision No. Change Description 1996 Issue 1, Revision 0 New issue June 1997 Issue 2, Revision 0 Complete update April 2001 Issue 3, Revision 0 Complete update ST-GTD-SUM-01 General modifications that reflect successful flights in 1999-2000 and Starsem’s future development plans. -
2001 Commercial Space Transportation Forecasts
2001 Commercial Space Transportation Forecasts Federal Aviation Administration's Associate Administrator for Commercial Space Transportation (AST) and the Commercial Space Transportation Advisory Committee (COMSTAC) May 2001 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.