SABCA PROPRIETARY – CONFIDENTIAL in USE a Quick Introduction to SABCA
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SABCA 1 Automated Warehouse A350 - Flap Support
S.A.B.C.A. ANNUAL REPORT 2014 © ESA–D.© ESA–D. Ducros, Ducros, 2014 2014 ANNUAL REPORT ANNUAL 2014 Gulfstream G650 Horizontal Stabilizer Skin (CFRP) – Assembly 2014 Annual Report of the Board of Directors Annual General Meeting, 28 May 2015 MANAGEMENT REPORT Group profile ......................................................................................................................................................................................................................................................................... 3 Statutory bodies ............................................................................................................................................................................................................................................................... 4 Message of the Chairman and the Chief Executive Officer ........................................................................................................................... 6 Principal activities in 2014 .............................................................................................................................................................................................................................. 9 Business Environment and Outlook .................................................................................................................................................................................................. 21 Research and Development .......................................................................................................................................................................................................................... -
Call for M5 Missions
ESA UNCLASSIFIED - For Official Use M5 Call - Technical Annex Prepared by SCI-F Reference ESA-SCI-F-ESTEC-TN-2016-002 Issue 1 Revision 0 Date of Issue 25/04/2016 Status Issued Document Type Distribution ESA UNCLASSIFIED - For Official Use Table of contents: 1 Introduction .......................................................................................................................... 3 1.1 Scope of document ................................................................................................................................................................ 3 1.2 Reference documents .......................................................................................................................................................... 3 1.3 List of acronyms ..................................................................................................................................................................... 3 2 General Guidelines ................................................................................................................ 6 3 Analysis of some potential mission profiles ........................................................................... 7 3.1 Introduction ............................................................................................................................................................................. 7 3.2 Current European launchers ........................................................................................................................................... -
Home at Airbus
Journal of Aircraft and Spacecraft Technology Original Research Paper Home at Airbus 1Relly Victoria Virgil Petrescu, 2Raffaella Aversa, 3Bilal Akash, 4Juan M. Corchado, 2Antonio Apicella and 1Florian Ion Tiberiu Petrescu 1ARoTMM-IFToMM, Bucharest Polytechnic University, Bucharest, (CE), Romania 2Advanced Material Lab, Department of Architecture and Industrial Design, Second University of Naples, 81031 Aversa (CE), Italy 3Dean of School of Graduate Studies and Research, American University of Ras Al Khaimah, UAE 4University of Salamanca, Spain Article history Abstract: Airbus Commerci al aircraft, known as Airbus, is a European Received: 16-04-2017 aeronautics manufacturer with headquarters in Blagnac, in the suburbs of Revised: 18-04-2017 Toulouse, France. The company, which is 100% -owned by the industrial Accepted: 04-07-2017 group of the same name, manufactures more than half of the airliners produced in the world and is Boeing's main competitor. Airbus was Corresponding Author: founded as a consortium by European manufacturers in the late 1960s. Florian Ion Tiberiu Petrescu Airbus Industry became a SAS (simplified joint-stock company) in 2001, a ARoTMM-IFToMM, Bucharest subsidiary of EADS renamed Airbus Group in 2014 and Airbus in 2017. Polytechnic University, Bucharest, (CE) Romania BAE Systems 20% of Airbus between 2001 and 2006. In 2010, 62,751 Email: [email protected] people are employed at 18 Airbus sites in France, Germany, the United Kingdom, Belgium (SABCA) and Spain. Even if parts of Airbus aircraft are essentially made in Europe some come from all over the world. But the final assembly lines are in Toulouse (France), Hamburg (Germany), Seville (Spain), Tianjin (China) and Mobile (United States). -
Annual Report 2015 Annual Report 2015
S.A.B.C.A. ANNUAL REPORT 2015 ANNUAL REPORT ANNUAL 2015 2015 report of the board of directors Annual General Meeting, 26 May 2016 MANAGEMENT REPORT Group profile ........................................................................................................................................................................................................................................................................... 3 Statutory bodies ................................................................................................................................................................................................................................................................. 4 Message of the Chairman and the Chief Executive Officer ............................................................................................................................ 6 1. Principal activities in 2015 ........................................................................................................................................................................................................................ 9 2. Business Environment and Outlook ............................................................................................................................................................................................ 21 3. Research and Development .................................................................................................................................................................................................................... -
Project Number: JMW-USC1
Project Number: JMW-USC1 Department of Social Science and Policy Studies THE FUTURE OF UNMANNED SPACE: A SPECULATIVE ANALYSIS OF THE COMMERCIAL MARKET An Interactive Qualifying Project Report: Submitted to the Faculty of the WORCESTER POLYTECHNIC INSTITUTE in partial fulfillment of the requirements for the Degree of Bachelor of Science by ______________________________ Peter Brayshaw ______________________________ Brooks Farnham ______________________________ Jon Leslie December 16, 2004 _____________________________ ________________________________ Professor John M. Wilkes, Advisor Professor Peter Campisano, Co-Advisor Abstract: This report is one of many which deal with the unmanned space race. It is a prediction of who will have the greatest competitive advantage in the commercial market over the next 25 years, based on historical analogy. Background information on Russia, China, Japan, the United States and the European Space Agency, including the launch vehicles and launch services each provides, is covered. The new prospect of space platforms is also investigated. 2 Table of Contents Abstract: ...................................................................................................... 2 Table of Contents ......................................................................................... 3 Introduction ................................................................................................. 5 Literature Review ...................................................................................... 5 Project -
Design by Contract: the Lessons of Ariane
. Editor: Bertrand Meyer, EiffelSoft, 270 Storke Rd., Ste. 7, Goleta, CA 93117; voice (805) 685-6869; [email protected] several hours (at least in earlier versions of Ariane), it was better to let the computa- tion proceed than to stop it and then have Design by to restart it if liftoff was delayed. So the SRI computation continues for 50 seconds after the start of flight mode—well into the flight period. After takeoff, of course, this com- Contract: putation is useless. In the Ariane 5 flight, Object Technology however, it caused an exception, which was not caught and—boom. The exception was due to a floating- point error during a conversion from a 64- The Lessons bit floating-point value, representing the flight’s “horizontal bias,” to a 16-bit signed integer: In other words, the value that was converted was greater than what of Ariane can be represented as a 16-bit signed inte- ger. There was no explicit exception han- dler to catch the exception, so it followed the usual fate of uncaught exceptions and crashed the entire software, hence the onboard computers, hence the mission. This is the kind of trivial error that we Jean-Marc Jézéquel, IRISA/CNRS are all familiar with (raise your hand if you Bertrand Meyer, EiffelSoft have never done anything of this sort), although fortunately the consequences are usually less expensive. How in the world everal contributions to this made up of respected experts from major department have emphasized the European countries, which produced a How in the world could importance of design by contract report in hardly more than a month. -
2015152450 Presentation-Airbus
Accès Européen à l’Espace, pourquoi Ariane 6 et Airbus Safran Launchers ? Assemblée Générale ISAE 11/06/2015 H. GILIBERT – CTO - Airbus Safran Launchers 1 Eléments de contexte This document is the property of Airbus Safran Launchers. It shall be not communicated to third parties without prior written agreement. Its content shall not be disclosed. Airbus Safran Launchers Holding/SAS/GmbH. All rights reserved. Janvier 2015 2 Le contexte des lanceurs spatiaux en Europe • Les lanceurs spatiaux servent avant tout la Garantie de l’Accès Stratégique à l’Espace pour les Etats Européens. • L’activité est supportée par les Etats Membres de l’Agence Spatiale Européenne (esa). • Quelques lancements institutionnels à l’année (essentiellement avec VEGA, et SOYOUZ actuellement). • L’économie de la filière est rendue supportable pour les Etats Européens par la capture de lancements commerciaux, qui assurent la récurrence de production et forcent à la compétitivité. • Ariane 5 (6 à 7 lancements par an) réalise > 80 % de ses lancements sur le marché commercial (leader mondial ~50 % du marché ouvert). This document is the property of Airbus Safran Launchers. It shall be not communicated to third parties without prior written agreement. Its content shall not be disclosed. Airbus Safran Launchers Holding/SAS/GmbH. All rights reserved. janvier 2015 3 L’activité Lancements Spatiaux dans le monde This document is the property of Airbus Safran Launchers. It shall be not communicated to third parties without prior written agreement. Its content shall not be disclosed. Airbus Safran Launchers Holding/SAS/GmbH. All rights reserved. janvier 2015 4 Les évolutions du marché des lancements (1/2) Les « moyens à gros » Les lancements sur le marché commercial sont essentiels pour soutenir l’Accès Européen Autonome à l’Espace Apparition de satellites à propulsion électrique, plus légers -> modifiera peu à peu les besoins mission sur la décennie à venir. -
Hi-Rel Solutions for Space Launch Vehicles a Single Network for All
© Airbus Safran Launchers 2016 © A Single Network for All Data Traffic Hi-Rel Solutions for Space Launch Vehicles www.tttech.com/space We are delighted that our network solution based on Deterministic Ethernet is providing a very powerful platform “ simplifying the electronic architectures of launch vehicles worldwide! Georg Kopetz, Member of the Executive Board, TTTech Computertechnik AG ” Over the last 25 years, space launch vehicle designs have utilized several different solutions for their on-board data handling. For the safety-critical command and control data, the very robust MIL-1553 bus served as a standard solution, originally designed as a military avionic data bus. For redundancy purposes, this widespread standard enforces two MIL-1553 buses running in parallel. This fact creates the first challenge, namely managing redundant fieldbuses in software and in parallel separate channels for additional data, e.g. telemetry. The second challenge arises from increasing data rates: MIL-1553 is limited to 1 Mbit/s, while there actually is both a need for higher control data rates and an interest in new types of sensors like video cameras. Adding more field buses would be possible, but would increase both weight and software complexity as well as qualification efforts. Finally, despite the need for higher bandwidth and a simplified network, no system cost increase can be tolerated, as in recent years the market for launch vehicles has become extremely competitive. This has led launch vehicle manufacturers worldwide to look for automotive or industrial solutions in order to reduce the cost of the electronics used throughout their vehicles. © Airbus Safran Launchers 2015 After several years of research funded by the ► French space agency (CNES) and afterwards by PROJECT ▼ the European Space Agency (ESA), architectures Launcher avionics A GLANCE AT based on TTEthernet are considered a great fit ► CHALLENGE for launch vehicles. -
Variations of Solid Rocket Motor Preliminary Design for Small TSTO Launcher
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Institute of Transport Research:Publications Space Propulsion 2012 – ID 2394102 Variations of Solid Rocket Motor Preliminary Design for Small TSTO launcher Etienne Dumont Space Launcher Systems Analysis (SART), DLR, Bremen, Germany [email protected] NGL New/Next Generation Launcher Abstract SI Structural Index (mdry / mpropellant) Several combinations of solid rocket motors and ignition SRM Solid Rocket Motor strategies have been considered for a small Two Stage to TSTO Two Stage To Orbit Orbit (TSTO) launch vehicle based on a big solid rocket US Upper Stage motor first stage and cryogenic upper stage propelled by VENUS Vega New Upper Stage the Vinci engine. In order to reach the target payload avg average during the flight performance of about 1400 kg into GTO for the clean s.l. sea level version and 2700 to 3000 kg for the boosted version, the vac vacuum influence of the selected solid rocket motors on the upper 2 + 2 P23 4 P23: two ignited on ground and two with a stage structure has been studied. Preliminary structural delayed ignition designs have been performed and the thrust histories of the solid rocket motor have been tweaked to limit the upper stage structural mass. First stage and booster 1. Introduction combinations with acceptable general loads are proposed. Solid rocket motors (SRM) are commonly used for boosters or launcher first stage. Indeed they can provide high thrust levels while being compact, light and Nomenclature relatively simple compared to a liquid rocket engine Isp specific impulse s providing the same thrust level. -
Trade Studies Towards an Australian Indigenous Space Launch System
TRADE STUDIES TOWARDS AN AUSTRALIAN INDIGENOUS SPACE LAUNCH SYSTEM A thesis submitted for the degree of Master of Engineering by Gordon P. Briggs B.Sc. (Hons), M.Sc. (Astron) School of Engineering and Information Technology, University College, University of New South Wales, Australian Defence Force Academy January 2010 Abstract During the project Apollo moon landings of the mid 1970s the United States of America was the pre-eminent space faring nation followed closely by only the USSR. Since that time many other nations have realised the potential of spaceflight not only for immediate financial gain in areas such as communications and earth observation but also in the strategic areas of scientific discovery, industrial development and national prestige. Australia on the other hand has resolutely refused to participate by instituting its own space program. Successive Australian governments have preferred to obtain any required space hardware or services by purchasing off-the-shelf from foreign suppliers. This policy or attitude is a matter of frustration to those sections of the Australian technical community who believe that the nation should be participating in space technology. In particular the provision of an indigenous launch vehicle that would guarantee the nation independent access to the space frontier. It would therefore appear that any launch vehicle development in Australia will be left to non- government organisations to at least define the requirements for such a vehicle and to initiate development of long-lead items for such a project. It is therefore the aim of this thesis to attempt to define some of the requirements for a nascent Australian indigenous launch vehicle system. -
Gao-21-306, Nasa
United States Government Accountability Office Report to Congressional Committees May 2021 NASA Assessments of Major Projects GAO-21-306 May 2021 NASA Assessments of Major Projects Highlights of GAO-21-306, a report to congressional committees Why GAO Did This Study What GAO Found This report provides a snapshot of how The National Aeronautics and Space Administration’s (NASA) portfolio of major well NASA is planning and executing projects in the development stage of the acquisition process continues to its major projects, which are those with experience cost increases and schedule delays. This marks the fifth year in a row costs of over $250 million. NASA plans that cumulative cost and schedule performance deteriorated (see figure). The to invest at least $69 billion in its major cumulative cost growth is currently $9.6 billion, driven by nine projects; however, projects to continue exploring Earth $7.1 billion of this cost growth stems from two projects—the James Webb Space and the solar system. Telescope and the Space Launch System. These two projects account for about Congressional conferees included a half of the cumulative schedule delays. The portfolio also continues to grow, with provision for GAO to prepare status more projects expected to reach development in the next year. reports on selected large-scale NASA programs, projects, and activities. This Cumulative Cost and Schedule Performance for NASA’s Major Projects in Development is GAO’s 13th annual assessment. This report assesses (1) the cost and schedule performance of NASA’s major projects, including the effects of COVID-19; and (2) the development and maturity of technologies and progress in achieving design stability. -
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.