2017 REGISTRATION DOCUMENT Including the Annual Financial Report CONTENTS

Total Page:16

File Type:pdf, Size:1020Kb

2017 REGISTRATION DOCUMENT Including the Annual Financial Report CONTENTS 2017 REGISTRATION DOCUMENT including the Annual Financial Report CONTENTS MESSAGE FROM THE CHAIRMAN OF THE BOARD 5 CORPORATE SOCIAL RESPONSIBILITY 191 OF DIRECTORS AND THE CHIEF EXECUTIVE OFFICER 2 Introduction: CSR policies and corporate strategy 193 GROUP PROFILE 4 5.1 Social information 196 5.2 Human resources information 206 5.3 Environmental information 214 1 PRESENTATION OF THE GROUP 9 5.4 CSR reporting methodology and 1.1 Safran overview 11 independent third-party report 218 1.2 Group strategy 16 1.3 Group businesses 17 6 CORPORATE GOVERNANCE 225 1.4 Competitive position 31 6.1 Safran's corporate governance structure 227 1.5 Research and development 31 6.2 Membership structure of the Board 1.6 Industrial investments 36 of Directors 229 1.7 Sites and production plants 38 6.3 Operating procedures and work of the Board of Directors and the Board 1.8 Group purchasing policy 39 Committees 255 1.9 Safran quality performance and policy 40 6.4 Application of the AFEP-MEDEF Corporate Governance Code 264 2 REVIEW OF OPERATIONS IN 2017 6.5 Directors’ interests in the Company’s share capital 265 AND OUTLOOK FOR 2018 43 6.6 Compensation policy for corporate 2.1 Comments on the Group’s performance officers and Directors and compensation in 2017 based on adjusted data 45 and benefits awarded 266 Comments on the consolidated financial 2.2 6.7 Cross-reference table for the corporate statements 61 governance report prepared in accordance 2.3 Comments on the parent company with Article L.225-37 of the French financial tatementss 64 Commercial Code 286 2.4 Outlook for 2018 68 2.5 Acquisition of Zodiac Aerospace 68 7 INFORMATION ABOUT THE COMPANY, 2.6 Subsequent events 70 THE CAPITAL AND SHARE OWNERSHIP 289 FINANCIAL STATEMENTS 73 7.1 General information and bylaws 291 3 7.2 Information on share capital 297 3.1 Group consolidated financial statements 7.3 Share ownership 301 at December 31, 2017 75 7.4 Relations with shareholders 305 3.2 Statutory Auditors’ report on the consolidated financial statements 144 7.5 Stock market information 307 3.3 Parent company financial statements at December 31, 2017 148 8 ANNUAL GENERAL MEETING 309 3.4 Statutory Auditors’ report on the financial 8.1 Agenda 311 statements 171 8.2 Report of the Board of Directors on the resolutions put forward at the Annual RISK FACTORS 175 General Meeting and text of the proposed 4 resolutions 312 4.1 Risk management 177 8.3 Use by the Board of Directors of an 4.2 Internal control system 178 authorization given at the June 15, 2017 4.3 Risk factors 181 Annual General Meeting 332 4.4 Insurance 189 8.4 Statutory Auditors’ Reports 337 9 ADDITIONAL INFORMATION 347 9.1 Persons responsible 349 9.2 Statutory Auditors 350 9.3 Historical financial information 350 9.4 Documents on display 351 9.5 Cross-reference tables 351 DOCUMENT 2017 INCLUDING THE ANNUAL REGISTRATIONFINANCIAL REPORT The Registration Document is available on the website at www.safran-group.com The French version of this Registration Document (document de référence) was filed with the French financial markets authority (Autorité des marchés financiers – AMF) on March 29, 2018 pursuant to Article 212-13 of the AMF's General Regulations. It may only be used in connection with a financial transaction if it is accompanied by a memorandum approved by the AMF. This document has been established by the issuer and is binding upon its signatories. The English language version of this report is a free translation from the original, which was prepared in French. In all matters of interpretation, views or opinions expressed in the original language version of the document in French take precedence over the translation. This Registration Document contains the Annual Financial Report in accordance with Article 222-3 of the AMF's General Regulations. The cross-reference table referring to information required in an Annual Financial Report is provided in section 9.5.3 of this Registration Document. MESSAGE FROM THE CHAIRMAN OF THE BOARD OF DIRECTORS AND THE CHIEF EXECUTIVE OFFICER MESSAGEFROM THE CHAIRMAN OF THE BOARD OF DIRECTORS AND THE CHIEF EXECUTIVE OFFICER We kicked off 2018 “ with a major event ROSS McINNES PHILIPPE PETITCOLIN Chairman of the Board of Directors Chief Executive Officer 2 SAFRAN – 2017 REGISTRATION DOCUMENT afran and Zodiac Aerospace joined Having moved swiftly on our decision to forces this year to create the world’s refocus operations on aerospace and defense, third largest aerospace company we were able to complete the disposal of our (excluding aircraft manufacturers), detection and security businesses under with more than 90,000 employees excellent financial conditions in the first half of worldwide and revenue of around 2017. Safran Identity & Security and Oberthur €21 billion(1). Technologies have combined to form a leading France-based digital security SLeveraging the contribution of Zodiac company, Idemia. Aerospace, a leading supplier of aircraft systems, cabins and seats, the Group will be Our joint venture with Airbus, renamed able to provide its ever-expanding, ArianeGroup, is set to provide Europe with increasingly diversified customer base with independent access to space thanks to its a balanced offering of propulsion and next generation launch vehicles. Building on equipment solutions. the success of Ariane 5, ArianeGroup is busy preparing Ariane 6. The historic combination reflects the vigorous momentum generated in 2017, when the In 2018, we will be tackling three main Group successfully demonstrated that it challenges. had the means to reach its goals. The first is the continued ramp-up of LEAP Our revenue grew 7.4% on an organic basis, production. Between 1,100 and 1,200 LEAP beating forecasts to stand at €16.5 billion. engines will be delivered in 2018, backed by Recurring operating income, representing 15% clear objectives in terms of delivery of revenue at €2.47 billion, and cash flow of schedules, quality and costs. We will be €1.4 billion, representing 58% of recurring relentless in our efforts. operating income and nearly 80% of profit from continuing operations, were in line with The second is of course the integration of our objectives. In light of these performances, Zodiac Aerospace. We are working diligently a dividend of €1.60 per share has been put to to make that happen. Everyone is committed the approval of the Annual General Meeting to achieving the expected synergies, securing for 2017 (€1.52 for 2016). the operational turnaround, supporting the return to confidence among customers and Apart from the combination agreed with reaping all the benefits of the merger. It’s our Zodiac Aerospace, 2017 was shaped by the job to unlock the full potential of the new ramp-up of the LEAP program, which is organization and express all of the qualities critical to our future. A total of 459 LEAP that our two strategically matched, engines were delivered, proving that the world-class aerospace groups have to offer. transition from the CFM56 has been practically seamless, an exceptional feat in The third challenge has to do with innovation. the history of the global aerospace industry. Because, more than anything, innovation is what will allow us to make further strides In helicopter turbines, we made the best of toward greater aerospace fuel economy, a persistently tense market and are actively a reduced environmental footprint in line with preparing for the future. 2018 is expected society’s expectations, and more electric to be a year of recovery. aircraft. Against a backdrop of big data, augmented reality and additive manufacturing, In aircraft equipment, our competitiveness we need to stay at the cutting edge of drive is continuing to pay off.Faced with technology across our businesses by digitalizing a highly competitive environment, we are our processes, our services and our products. ready to ramp up large-scale programs such as the A330neo, fitted with our nacelles, All of our stakeholders – shareholders, wiring, power transmission and landing customers, partners and employees – systems. We delivered the first prototypes of are aware that today’s challenges present our Electric Taxiing by Safran system in late a unique opportunity. 2017, demonstrating our ability to differentiate our offering through continually innovative And we are convinced that Safran has the technology. means at its disposal to write a great new chapter in its history. Our Defense business had a successful year, reporting higher revenue in line with our projections. Ross McInnes and Philippe Petitcolin (1) Unaudited pro forma results based on the previous 12 months for both companies. SAFRAN – 2017 REGISTRATION DOCUMENT 3 GROUP PROFILE GROUP PROFILE Employing 58,324 The Group differentiates itself from the Safran enjoys particularly sound funda- people worldwide, competition through its technological mentals with front-ranking technical and Safran is an expertise. Its complementary businesses commercial positions, profitable and give it a genuine advantage, driving sustainable recurring service activities international high- growth and enabling the Group to with- offering high added value, truly innova- technology group stand economic cycles. From both a tive research and development, a healthy operating in the technological and managerial point of financial situation and strong operat- aircraft propulsion and view, the Group's various businesses are ing cash flow, which allow it to leverage equipment, space and integrated and complementary. opportunities for organic growth and defense markets. It is acquisition-led development. The combi- Safran has a strong positioning in nation with Zodiac Aerospace in early a leading global player Aerospace. Its installed fleet of engines, 2018, for example, led to the creation of a on markets in which especially the CFM56®, offers significant global leader in aircraft equipment.
Recommended publications
  • 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 ...........................................................................................................................................
    [Show full text]
  • Robust Gas Turbine and Airframe System Design in Light of Uncertain
    Robust Gas Turbine and Airframe System Design in Light of Uncertain Fuel and CO2 Prices Stephan Langmaak1, James Scanlan2, and András Sóbester3 University of Southampton, Southampton, SO16 7QF, United Kingdom This paper presents a study that numerically investigated which cruise speed the next generation of short-haul aircraft with 150 seats should y at and whether a con- ventional two- or three-shaft turbofan, a geared turbofan, a turboprop, or an open rotor should be employed in order to make the aircraft's direct operating cost robust to uncertain fuel and carbon (CO2) prices in the Year 2030, taking the aircraft pro- ductivity, the passenger value of time, and the modal shift into account. To answer this question, an optimization loop was set up in MATLAB consisting of nine modules covering gas turbine and airframe design and performance, ight and aircraft eet sim- ulation, operating cost, and optimization. If the passenger value of time is included, the most robust aircraft design is powered by geared turbofan engines and cruises at Mach 0.80. If the value of time is ignored, however, then a turboprop aircraft ying at Mach 0.70 is the optimum solution. This demonstrates that the most fuel-ecient option, the open rotor, is not automatically the most cost-ecient solution because of the relatively high engine and airframe costs. 1 Research Engineer, Computational Engineering and Design 2 Professor of Aerospace Design, Computational Engineering and Design, AIAA member 3 Associate Professor in Aircraft Engineering, Computational Engineering and Design, AIAA member 1 I. Introduction A. Background IT takes around 5 years to develop a gas turbine engine, which then usually remains in pro- duction for more than two decades [1, 2].
    [Show full text]
  • Introduction Firstly, We Have Given a Little Background of France, in Terms
    Introduction Firstly, we have given a little background of France, in terms of its geographic, Demographic, political and economic characteristics and a brief History of France from its old age till the Modern times. Secondly, In order to find the absolute and comparative advantages of France, in terms of its international trade and economic prosperity, we have categorized the imports and exports of France into the following categories: Mineral products, Wood products, Metal products, Stones and glass products, Paper goods, Agriculture products, Animal products, Food stuffs, Weapons, Footwear and headwear, Animal hides, Textiles, Transportations, Machineries, Arts and antiques, Precious metals, Chemical products, instruments, plastics and rubbers. We have kept the imports/exports data of the year 2013 and 2014 under observations and had a relative comparison of France’s imports and exports commodities of these three years. The relative comparison of which are listed in the appendix, in terms of monetary value, percentage value of each categories and the overall imports and exports. Since, the imports and exports were in large numbers, thus we have taken the top 5 imports and exports of each category, as mentioned in the above paragraph, to find out the absolute and comparative advantages of France. Furthermore, we have: revealed the best comparative advantage by applying porter’s diamond model; determined the destination countries, where commodities are exported, by selecting a single company with in the industry that has the best comparative advantage. And finally, we determined the mode expansion using Foreign Direct Investment model. Background Geographically: France, with an Area of 643,801 Sq.
    [Show full text]
  • Aerospace Engine Data
    AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16
    [Show full text]
  • CRUISE MISSILE THREAT Volume 2: Emerging Cruise Missile Threat
    By Systems Assessment Group NDIA Strike, Land Attack and Air Defense Committee August 1999 FEASIBILITY OF THIRD WORLD ADVANCED BALLISTIC AND CRUISE MISSILE THREAT Volume 2: Emerging Cruise Missile Threat The Systems Assessment Group of the National Defense Industrial Association ( NDIA) Strike, Land Attack and Air Defense Committee performed this study as a continuing examination of feasible Third World missile threats. Volume 1 provided an assessment of the feasibility of the long range ballistic missile threats (released by NDIA in October 1998). Volume 2 uses aerospace industry judgments and experience to assess Third World cruise missile acquisition and development that is “emerging” as a real capability now. The analyses performed by industry under the broad title of “Feasibility of Third World Advanced Ballistic & Cruise Missile Threat” incorporate information only from unclassified sources. Commercial GPS navigation instruments, compact avionics, flight programming software, and powerful, light-weight jet propulsion systems provide the tools needed for a Third World country to upgrade short-range anti-ship cruise missiles or to produce new land-attack cruise missiles (LACMs) today. This study focuses on the question of feasibility of likely production methods rather than relying on traditional intelligence based primarily upon observed data. Published evidence of technology and weapons exports bears witness to the failure of international agreements to curtail cruise missile proliferation. The study recognizes the role LACMs developed by Third World countries will play in conjunction with other new weapons, for regional force projection. LACMs are an “emerging” threat with immediate and dire implications for U.S. freedom of action in many regions .
    [Show full text]
  • Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft
    Air s.Pace ELectric Innovative Commuter Aircraft D2.1 Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft Name Function Date Author: Maximilian Spangenberg (ASP) WP2 Co-Lead 31.03.2020 Approved by: Markus Wellensiek (ASP) WP2 Lead 31.03.2020 Approved by: Dr. Qinyin Zhang (RRD) Project Lead 31.03.2020 D2.1 Economic Feasibility Study page 1 of 81 Clean Sky 2 Grant Agreement No. 864551 © ELICA Consortium No export-controlled data Non-Confidential Air s.Pace Table of contents 1 Executive summary .........................................................................................................................3 2 References ........................................................................................................................................4 2.1 Abbreviations ...............................................................................................................................4 2.2 List of figures ................................................................................................................................5 2.3 List of tables .................................................................................................................................6 3 Introduction ......................................................................................................................................8 4 ELICA market study ...................................................................................................................... 12 4.1 Turboprop and piston engine
    [Show full text]
  • Powerpoint Template with New NAHEMA Logo
    5 & 6 OCTOBER 2016 LISBON, PORTUGAL 1. NH90 programme 2. JMAAN organization 3. EMAR Transition for NH90 (EMAR-T) 4. Conclusion NATO UNCLASSIFIED 2 1. NH90 programme 2. JMAAN organization 3. EMAR Transition for NH90 (EMAR-T) 4. Conclusion NATO UNCLASSIFIED 3 Corporate Identity: NAHEMO is a subsidiary body of NATO NAHEMA is the international programme office of NAHEMO Established: In 1992, in Aix-en-Provence (France) in vicinity of industrial consortium NHIndustries Mission: Management of the NH90 programme on behalf of the NAHEMO Nations, during the design & development, production & post-design and in-service support phases NATO UNCLASSIFIED 4 1 product: NH90 2 Versions: TTH, NFH >20 Variants: TGEA, GITA, TFRA, HITN, NBEN, NNLN, … Customer: NAHEMA 11 Nations: BEL, DEU, FRA, ITA, NLD, AUS, ESP, FIN, NOR, NZL, SWE, (GRC, OMN) Contractor: NHIndustries 4 Industries: AH, AHD, FK, LHD Design & Development (D&D) development of two versions TTH and NFH signed in 1992 Export Production Investment/ Production (PIP) production of the serial helicopters in different variants signed in 2000 (25 Contract Amendments so far) first serial helicopter delivered in 2006 (IOC) and 2012 (FOC) In-service support more than 240 helicopter in service with over 100k logged flight hours NATO UNCLASSIFIED 5 1. NH90 programme 2. JMAAN organization 3. EMAR Transition for NH90 (EMAR-T) 4. Conclusion NATO UNCLASSIFIED 6 JMAAN is a body of the NH90 Community JMAAN regulates all processes in the field of: • Military Design Organisation Approval • Rule-making
    [Show full text]
  • SP's Naval Force June-July 2010
    June-July l 2010 Volume 5 No 3 rs 100.00 (india-based buyer only) SP’s AN SP GUIDE PUBLICATION www.spsnavalforces.net ROUNDUP 3 PAGe STOP PRESS A Global Concern NAvAL vARIANT OF LCA ROLLS OUT India, in cooperation with its allies and friends The country’s first naval variant of Light Combat Aircraft, the LCA (Navy) Trainer around the world, will have to work to ensure Naval Project (NP)–1 was rolled out by the Defence Minister A.K. Antony from HAL that lawful private and public activities in the Aircraft Research and Design Centre at a glittering function in Bengaluru on July 6, maritime domain are protected against attack 2010. The Chief of Naval Staff Admiral Nirmal Verma, Secretary Defence Production by hostile exploitations R.K. Singh, Scientific Adviser to the Defence Minister, Dr. V.K. Saraswat, HAL Chair - man Ashok Nayak, Director Aeronautical Development Agency P.S. Subramanyam Cdr Sandeep Dewan were present on the occasion. The Defence Minister described the development as a ‘defining and memorable event’ for the nation. PAGe 4 Around the Sea A report on Commander Dilip Donde’s TeTe-e-TeTe successful completion of the first solo circumnavigation by an Indian Rear Admiral (Retd) Sushil Ramsay ‘Cooperation and interaction in the PAGe 6 Stealthy Ships maritime domain will continue to be an important aspect of IN’s vision’ PhotograPh: abhishek / sP guide Pubns Chief of Naval Staff Admi - ral Nirmal Verma , in an interaction with SP’s Naval The scope of accessing technologies from Forces , throws light on the the western world, so far denied to India, is security measures to deal witnessing an upward swing with the growing incidents Rear Admiral (Retd) Sushil Ramsay of piracy.
    [Show full text]
  • 액체로켓 메탄엔진 개발동향 및 시사점 Development Trends of Liquid
    Journal of the Korean Society of Propulsion Engineers Vol. 25, No. 2, pp. 119-143, 2021 119 Technical Paper DOI: https://doi.org/10.6108/KSPE.2021.25.2.119 액체로켓 메탄엔진 개발동향 및 시사점 임병직 a, * ㆍ 김철웅 a⋅ 이금오 a ㆍ 이기주 a ㆍ 박재성 a ㆍ 안규복 b ㆍ 남궁혁준 c ㆍ 윤영빈 d Development Trends of Liquid Methane Rocket Engine and Implications Byoungjik Lim a, * ㆍ Cheulwoong Kim a⋅ Keum-Oh Lee a ㆍ Keejoo Lee a ㆍ Jaesung Park a ㆍ Kyubok Ahn b ㆍ Hyuck-Joon Namkoung c ㆍ Youngbin Yoon d a Future Launcher R&D Program Office, Korea Aerospace Research Institute, Korea b School of Mechanical Engineering, Chungbuk National University, Korea c Guided Munitions Team, Hyundai Rotem, Korea d Department of Aerospace Engineering, Seoul National University, Korea * Corresponding author. E-mail: [email protected] ABSTRACT Selecting liquid methane as fuel is a prevailing trend for recent rocket engine developments around the world, triggered by its affordability, reusability, storability for deep space exploration, and prospect for in-situ resource utilization. Given years of time required for acquiring a new rocket engine, a national-level R&D program to develop a methane engine is highly desirable at the earliest opportunity in order to catch up with this worldwide trend towards reusing launch vehicles for competitiveness and mission flexibility. In light of the monumental cost associated with development, fabrication, and testing of a booster stage engine, it is strategically a prudent choice to start with a low-thrust engine and build up space application cases.
    [Show full text]
  • Rotorcraft (2011)
    Rotorcraft Overview The rotorcraft industry produces aircraft, powered by either turboshaft or reciprocating engines, capable of performing vertical take-off and landing (VTOL) operations. The rotorcraft sector includes helicopters, gyrocopters, and tiltrotor aircraft. Helicopters, which employ a horizontal rotor for both lift and propulsion, are the mainstay of the industry. Gyrocopters are produced in much smaller quantities, primarily for use in recreational flying. Tiltrotor aircraft, such as the V-22 Osprey1, can take off vertically and then fly horizontally as a fixed-wing aircraft. Rotorcraft are manufactured in most industrialized countries, based on indigenous design or in collaboration with, or under license from, other manufacturers. Manufacturers in the United States of civilian helicopters include American Eurocopter, Bell, Enstrom, Kaman, MD Helicopters, Robinson, Schweizer (now a subsidiary of Sikorsky), and Sikorsky. Bell moved its civilian helicopter production to Canada, with the last U.S. product completed in 1993.2 American Eurocopter—a subsidiary of the European manufacturer and subsidiary of EADS NV—has manufacturing and assembly facilities in Grand Prairie, Texas and Columbus, Missouri. European producers include AgustaWestland, Eurocopter, NHIndustries, and PZL Swidnik. Russian manufacturers including Mil Moscow, Kamov and Kazan helicopters, as well as a number of other rotorcraft related companies, have been consolidated under the Russian government majority-owned OAO OPK Oboronprom.3 (See this report’s Russia
    [Show full text]
  • ESPA Ring Datasheet
    PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites.
    [Show full text]
  • 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.
    [Show full text]