Core Technology Activity for Future Launchers
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Ariane-5 Completes Flawless Third Test Flight
r bulletin 96 — november 1998 Ariane-5 Completes Flawless Third Test Flight A launch-readiness review conducted on Friday engine shut down and Maqsat-3 was 16 and Monday 19 October had given the go- successfully injected into GTO. The orbital ahead for the final countdown for a launch just parameters at that point were: two days later within a 90-minute launch Perigee: 1027 km, compared with the window between 13:00 to 14:30 Kourou time. 1028 ± 3 km predicted The launcher’s roll-out from the Final Assembly Apogee: 35 863 km, compared with the Building to the Launch Zone was therefore 35 898 ± 200 km predicted scheduled for Tuesday 20 October at 09:30 Inclination: 6.999 deg, compared with the Kourou time. 6.998 ± 0.05 deg predicted. On 21 October, Europe reconfirmed its lead in providing space Speaking in Kourou immediately after the flight, transportation systems for the 21st Century. Ariane-5, on its third Fredrik Engström, ESA’s Director of Launchers qualification flight, left no doubts as to its ability to deliver payloads and the Ariane-503 Flight Director, confirmed reliably and accurately to Geostationary Transfer Orbit (GTO). The new that: “The third Ariane-5 flight has been a heavy-lift launcher lifted off in glorious sunshine from the Guiana complete success. It qualifies Europe’s new Space Centre, Europe’s spaceport in Kourou, French Guiana, at heavy-lift launcher and vindicates the 13:37:21 local time (16:37:21 UT). technological options chosen by the European Space Agency.” This third Ariane-5 test flight was intended ESA’s Director -
6. the INTELSAT 17 Satellite
TWO COMMUNICATIONS SATELLITES READY FOR LAUNCH Arianespace will orbit two communications satellite on its fifth launch of the year: INTELSAT 17 for the international satellite operator Intelsat, and HYLAS 1 for the European operator Avanti Communications. The choice of Arianespace by leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Based on its proven reliability and availability, Arianespace continues to confirm its position as the world’s benchmark launch system. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads. Arianespace and Intelsat have built up a long-standing relationship based on mutual trust. Since 1983, Arianespace has launched 48 satellites for Intelsat. Positioned at 66 degrees East, INTELSAT 17 will deliver a wide range of communication services for Europe, the Middle East, Russia and Asia. Built by Space Systems/Loral of the United States, this powerful satellite will weigh 5,540 kg at launch. It will also enable Intelsat to expand its successful Asian video distrubution neighborhood. INTELSAT 17 will replace INTELSAT 702. HYLAS 1 is Avanti Communications’ first satellite. A new European satellite operator, Avanti Communications also chose Arianespace to orbit its HYLAS 2 satellite, scheduled for launch in the first half of 2012. HYLAS 1 was built by an industrial consortium formed by EADS Astrium and the Indian Space Research Organisation (ISRO), using a I-2K platform. Fitted with Ka-band and Ku-band transponders, the satellite will be positioned at 33.5 degrees West, and will be the first European satellite to offer high-speed broadband services across all of Europe. -
View / Download
www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers. -
The Annual Compendium of Commercial Space Transportation: 2012
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA 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 (2013) 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. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly. -
Study of a 100Kwe Space Reactor for Exploration Missions
Preliminary study of a 100 kWe space reactor concept for exploration missions Elisa CLIQUET, Jean-Marc RUAULT 1), Jean-Pierre ROUX, Laurent LAMOINE, Thomas RAMEE 2), Christine POINOT-SALANON, Alexey LOKHOV, Serge PASCAL 3) 1) CNES Launchers Directorate,Evry, France 2) AREVA TA, Aix en Provence, France 3) CEA DEN/DM2S, F-91191 Gif-sur-Yvette, France NETS 2011 Overview ■ General context of the study ■ Requirements ■ Methodology of the study ■ Technologies selected for final trade-off ■ Reactor trade-off ■ Conversion trade-off ■ Critical technologies and development philosophy ■ Conclusion and perspectives CNES Directorate of Launchers Space transportation division of the French space agency ■ Responsible for the development of DIAMANT, ARIANE 1 to 4, ARIANE 5, launchers ■ System Architect for the Soyuz at CSG program ■ Development of VEGA launcher first stage (P80) ■ Future launchers preparation activities Multilateral and ESA budgets • To adapt the current launchers to the needs for 2015-2020 • To prepare launcher evolutions for 2025 - 2030, if needed • To prepare the new generation of expandable launchers (2025-2030) • To prepare the long future after 2030 with possible advanced launch vehicles ■ Future space transportation prospective activities, such as Exploration needs (including in particular OTV missions) Advanced propulsion technologies investigation General context ■ Background Last French studies on space reactors : • ERATO (NEP) in the 80’s, • MAPS (NTP) in the 90’s • OPUS (NEP) 2002-2004 ■ Since then Nuclear safe orbit -
The European Launchers Between Commerce and Geopolitics
The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3. -
ARIANE 5 Data Relating to Flight 225
KOUROU August 2015 ARIANE 5 Data relating to Flight 225 EUTELSAT 8 West B Intelsat 34 Data relating to Flight 225 Flight 225 Ariane 5 Satellites: EUTELSAT 8 WEST B – INTELSAT 34 Content 1. Introduction .................................................................... 3 2. Launcher L579 ............................................................... 4 3. Mission V225 ............................................................... 10 4. Payloads ...................................................................... 19 5. Launch campaign ........................................................ 32 6. Launch window ............................................................ 35 7. Final countdown .......................................................... 36 8. Flight sequence ........................................................... 40 9. Airbus Defence and Space and the ARIANE programmes ........................................................................ 42 2 Data relating to Flight 225 1. Introduction Flight 225 is the 81st Ariane 5 launch and the fourth in 2015. It follows on from a series of 66 consecutive successful Ariane 5 launches. This is the 51st ARIANE 5 ECA (Cryogenic Evolution type A), the most powerful version in the ARIANE 5 range. Flight 225 is a commercial mission for Ariane 5. The L579 launcher is the twenty-fifth to be delivered by Airbus Defence and Space to Arianespace as part of the PB production batch. The PB production contract was signed in March 2009 to guarantee continuity of the launch service after completion -
Paper Session II-A-Current Status of the Ariane 4 Program and of The
1994 (31st) Space Exploration and Utilization The Space Congress® Proceedings for the Good of the World Apr 27th, 1:00 PM - 4:00 PM Paper Session II-A - Current Status of the Ariane 4 Program and of the Ariane 5 Development James R. Youdale Arianespace Inc. Washington, D.C. Douglas A. Heydon Arianespace Inc. Washington, D.C. Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Youdale, James R. and Heydon, Douglas A., "Paper Session II-A - Current Status of the Ariane 4 Program and of the Ariane 5 Development" (1994). The Space Congress® Proceedings. 16. https://commons.erau.edu/space-congress-proceedings/proceedings-1994-31st/april-27-1994/16 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Current Status of the Ariane 4 Program and of the Ariane 5 Development James R. Youdale1 and Douglas A. Heyden~ Arianespace Inc. Washington, D.C. Abstract This paper provides an overview of the commercial siruation of Arianespace, a general update regarding its technical and operational activities and its near and medium term prospects. A summary of the Ariane 4 "track record" is given and the latest improvement to its third staae the HIO III, is presented. Operational improvements that reduce the interval between two = ' consecutive laWlches are also addressed. The ratiollale for going to Ariane 5 is discussed and the current status of the Ariane 5 development program is reviewed. -
Launch Vehicle Control Center Architectures
Launch Vehicle Control Center Architectures Michael D. Watson1, Amy Epps2, and Van Woodruff3 NASA Marshall Space Flight Center, Huntsville, AL 35812 Michael Jacob Vachon4 NASA Johnson Space Center, Houston, TX 77058 Julio Monreal5 European Space Agency, Launchers Directorate, Paris, France Marl Levesque6 United Launch Alliance, Vandenberg AFB and Randall Williams7 and Tom McLaughlin8 Aerospace Corporation, El Segundo, CA 90245 Launch vehicles within the international community vary greatly in their configuration and processing. Each launch site has a unique processing flow based on the specific launch vehicle configuration. Launch and flight operations are managed through a set of control centers associated with each launch site. Each launch site has a control center for launch operations; however flight operations support varies from being co-located with the launch site to being shared with the space vehicle control center. There is also a nuance of some having an engineering support center which may be co-located with either the launch or flight control center, or in a separate geographical location altogether. A survey of control center architectures is presented for various launch vehicles including the NASA Space Launch System (SLS), United Launch Alliance (ULA) Atlas V and Delta IV, and the European Space Agency (ESA) Ariane 5. Each of these control center architectures shares some similarities in basic structure while differences in functional distribution also exist. The driving functions which lead to these factors are considered and a model of control center architectures is proposed which supports these commonalities and variations. I. INTRODUCTION Launch vehicles in both Europe and the United States have been operating successfully for several decades. -
Sale Price Drives Potential Effects on DOD and Commercial Launch Providers
United States Government Accountability Office Report to Congressional Addressees August 2017 SURPLUS MISSILE MOTORS Sale Price Drives Potential Effects on DOD and Commercial Launch Providers Accessible Version GAO-17-609 August 2017 SURPLUS MISSILE MOTORS Sale Price Drives Potential Effects on DOD and Commercial Launch Providers Highlights of GAO-17-609, a report to congressional addressees Why GAO Did This Study What GAO Found The U.S. government spends over a The Department of Defense (DOD) could use several methods to set the sale billion dollars each year on launch prices of surplus intercontinental ballistic missile (ICBM) motors that could be activities as it strives to help develop a converted and used in vehicles for commercial launch if current rules prohibiting competitive market for space launches such sales were changed. One method would be to determine a breakeven and assure its access to space. Among price. Below this price, DOD would not recuperate its costs, and, above this others, one launch option is to use price, DOD would potentially save. GAO estimated that DOD could sell three vehicles derived from surplus ICBM Peacekeeper motors—the number required for one launch, or, a “motor set”—at motors such as those used on the Peacekeeper and Minuteman missiles. a breakeven price of about $8.36 million and two Minuteman II motors for about The Commercial Space Act of 1998 $3.96 million, as shown below. Other methods for determining motor prices, such prohibits the use of these motors for as fair market value as described in the Federal Accounting Standards Advisory commercial launches and limits their Board Handbook, resulted in stakeholder estimates ranging from $1.3 million per use in government launches in part to motor set to $11.2 million for a first stage Peacekeeper motor. -
Indian Remote Sensing Satellites (IRS)
Topic: Indian Remote Sensing Satellites (IRS) Course: Remote Sensing and GIS (CC-11) M.A. Geography (Sem.-3) By Dr. Md. Nazim Professor, Department of Geography Patna College, Patna University Lecture-5 Concept: India's remote sensing program was developed with the idea of applying space technologies for the benefit of human kind and the development of the country. The program involved the development of three principal capabilities. The first was to design, build and launch satellites to a sun synchronous orbit. The second was to establish and operate ground stations for spacecraft control, data transfer along with data processing and archival. The third was to use the data obtained for various applications on the ground. India demonstrated the ability of remote sensing for societal application by detecting coconut root-wilt disease from a helicopter mounted multispectral camera in 1970. This was followed by flying two experimental satellites, Bhaskara-1 in 1979 and Bhaskara-2 in 1981. These satellites carried optical and microwave payloads. India's remote sensing programme under the Indian Space Research Organization (ISRO) started off in 1988 with the IRS-1A, the first of the series of indigenous state-of-art operating remote sensing satellites, which was successfully launched into a polar sun-synchronous orbit on March 17, 1988 from the Soviet Cosmodrome at Baikonur. It has sensors like LISS-I which had a spatial resolution of 72.5 meters with a swath of 148 km on ground. LISS-II had two separate imaging sensors, LISS-II A and LISS-II B, with spatial resolution of 36.25 meters each and mounted on the spacecraft in such a way to provide a composite swath of 146.98 km on ground. -
User's Manual If Any
User’s Manual Issue 2/ Revision 0 September 2004 Approved and issued by ARIANESPACE Edouard Perez Senior Vice President Engineering Washington, D.C.,U.S.A. Singapore Siège social / Headquarters Tel : +33 1 60 87 60 00 Tel : +1 202 628-3936 Tel : +65 223 6426 Boulevard de l'Europe Fax : +33 1 60 87 62 47 Fax : +1 202 628-3949 Fax : +65 223 4268 B.P. 177 Tokyo Kourou 91006 Evry-Courcouronnes cedex S.A. au capital de 2 087 910 000 F Tel : +81 3 3592-2766 Tel : +594 33 67 07 www.arianespace.com France RCS Evry B 318 516 457 Fax : +81 3 3592-2768 Fax : +594 33 62 66 User’s Manual Preface This document contains the technical information which is necessary : - to assess compatibility of a spacecraft with the VEGA launches, - to prepare all the technical and operational documentation related to a launch of any spacecraft on VEGA. This document is revised periodically, comments and suggestions on all aspects of this manual will be encouraged and appreciated. Inquiries concerning clarification or interpretation of this manual should be directed to: ARIANESPACE Commercial Directorate / Technical Support Division B.P. 177 - 91006 EVRY Courcouronnes Cedex France Telephone: +33 1 60 87 62 87 Telefax : +33 1 60 87 64 59 Vega User’s manual Foreword Issue 2 FOREWORD The Vega launcher to orbit small payloads in Arianespace Service Vega is being developed within a European Program organised under the aegis of the European Space Agency. The launcher’s prime contractor is ELV S.p.A, a joint company of Fiat Avio and the Italian Space Agency (ASI).