ESA-Corporate-Presentation 2013
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CZ-Space Day Intro
16.7.2010 ESA TECHNOLOGY → PROGRAMMES AND STRATEGY Czech Space Technology Day - GSTP July 2010 CONTENTS • The European Space Agency -ESA • Space Technology • ESA’s Technology Programmes • Doing business with ESA • ESA’s Long Term Plan 2 1 16.7.2010 → THE EUROPEAN SPACE AGENCY PURPOSE OF ESA “To provide for and promote, for exclusively peaceful purposes, cooperation among European states in space research and technology and their space applications. ” - Article 2 of ESA Convention 4 2 16.7.2010 ESA FACTS AND FIGURES • Over 30 years of experience • 18 Member States • Five establishments, about 2000 staff • 3.7 billion Euro budget (2010) • Over 60 satellites designed, tested and operated in flight • 17 scientific satellites in operation • Five types of launcher developed • Over 190 launches 5 18 MEMBER STATES Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, Norway, the Netherlands, Portugal, Spain, Sweden, Switzerland and the United Kingdom. Canada takes part in some programmes under a Cooperation Agreement. Hungary, Romania, Poland, Slovenia, and Estonia are European Cooperating States. Cyprus and Latvia have signed Cooperation Agreements with ESA. 6 3 16.7.2010 ACTIVITIES ESA is one of the few space agencies in the world to combine responsibility in nearly all areas of space activity. • Space science • Navigation • Human spaceflight • Telecommunications • Exploration • Technology • Earth observation • Operations • Launchers 7 ESA PROGRAMMES All Member States participate (on In addition, -
ACT-RPR-SPS-1110 Sps Europe Paper
62nd International Astronautical Congress, Cape Town, SA. Copyright ©2011 by the European Space Agency (ESA). Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-11-C3.1.3 PROSPECTS FOR SPACE SOLAR POWER IN EUROPE Leopold Summerer European Space Agency, Advanced Concepts Team, The Netherlands, [email protected] Lionel Jacques European Space Agency, Advanced Concepts Team, The Netherlands, [email protected] In 2002, a phased, multi-year approach to space solar power has been published. Following this plan, several activities have matured the concept and technology further in the following years. Despite substantial advances in key technologies, space solar power remains still at the weak intersections between the space sector and the energy sector. In the 10 years since the development of the European SPS Programme Plan, both, the space and the energy sectors have undergone substantial changes and many key enabling technologies for space solar power have advanced significantly. The present paper attempts to take account of these changes in view to assess how they influence the prospect for space solar power work for Europe. Fresh Look Study as well as the work on a European I INTRODUCTION sail tower concept by Klimke and Seboldt [16], [17]. Based on these results, which re-confirmed the The concept of generating solar power in space and principal technical viability of space solar power transmitting it to Earth to contribute to terrestrial energy concepts, the focus of the first phase of the European systems has received period attention since P. Glaser SPS programme plan has been to enlarge the evaluation published the first engineering approach to it in 1968 scope of space solar power by including expertise from [1]. -
Jules Verne ATV Launch Approaching 11 February 2008
Jules Verne ATV launch approaching 11 February 2008 will carry up to 9 tonnes of cargo to the station as it orbits 400 km above the Earth. Equipped with its own propulsion and navigation systems, the ATV is a multi-functional spacecraft, combining the fully automatic capabilities of an unmanned vehicle with the safety requirements of a crewed vehicle . Its mission in space will resemble that, on the ground, of a truck (the ATV) delivering goods and services to a research establishment (the space station). A new-generation high-precision navigation system will guide the ATV on a rendezvous trajectory towards the station. In early April, Jules Verne will automatically dock with the station’s Russian Preview of the maiden launch and docking of ESA's Jules Verne ATV. Jules Verne will be lifted into space on Service Module, following a number of specific board an Ariane 5 launch vehicle. Credits: ESA - D. operations and manoeuvres (on 'Demonstration Ducros Days') to show that the vehicle is performing as planned in nominal and contingency situations. It will remain there as a pressurised and integral After the successful launch of ESA’s Columbus part of the station for up to six months until a laboratory aboard Space Shuttle Atlantis on controlled re-entry into the Earth’s atmosphere Thursday (7 February), it is now time to focus on takes place, during which it will burn up and, in the the next imminent milestone for ESA: the launch of process, dispose of 6.3 tonnes of waste material no Jules Verne, the first Automated Transfer Vehicle longer needed on the station. -
Trace Contaminant Control During the International Space Station's On
https://ntrs.nasa.gov/search.jsp?R=20170012333 2019-08-30T16:48:33+00:00Z National Aeronautics and NASA/TP—2017–219689 Space Administration IS02 George C. Marshall Space Flight Center Huntsville, Alabama 35812 Trace Contaminant Control During the International Space Station’s On-Orbit Assembly and Outfitting J.L. Perry Marshall Space Flight Center, Huntsville, Alabama October 2017 The NASA STI Program…in Profile Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. Collected advancement of aeronautics and space science. The papers from scientific and technical conferences, NASA Scientific and Technical Information (STI) symposia, seminars, or other meetings sponsored Program Office plays a key part in helping NASA or cosponsored by NASA. maintain this important role. • SPECIAL PUBLICATION. Scientific, technical, The NASA STI Program Office is operated by or historical information from NASA programs, Langley Research Center, the lead center for projects, and mission, often concerned with NASA’s scientific and technical information. The subjects having substantial public interest. NASA STI Program Office provides access to the NASA STI Database, the largest collection of • TECHNICAL TRANSLATION. aeronautical and space science STI in the world. English-language translations of foreign The Program Office is also NASA’s institutional scientific and technical material pertinent to mechanism for disseminating the results of its NASA’s mission. research and development activities. These results are published by NASA in the NASA STI Report Specialized services that complement the STI Series, which includes the following report types: Program Office’s diverse offerings include creating custom thesauri, building customized databases, • TECHNICAL PUBLICATION. Reports of organizing and publishing research results…even completed research or a major significant providing videos. -
Maurizio Cheli Vide Per La Prima Volta L'everest Da Una Prospettiva
UN ASTRONAUTA il 1969 e Maurizio Cheli, un bambino di 10 anni della provincia di Modena, guardando rapito le immagini in bianco e nero dello sbarco sulla Luna che scorrono su una piccola TV, decide che, SULL’EVEREST Èda grande, anche lui farà l’astronauta. Il suo sogno si avvera nel 1993, quando ottiene l’agognata qualifica presso il John- son Space Center di Houston della NASA. Nel 1996, a bordo dello Space Shuttle Columbia, partecipa alla missione STS-75 Tethered Satellite in cui ricopre, primo italiano, il ruolo di mission specialist. Plurilaureato, nel 2005 fonda la startup CFM Air per la progettazione di velivoli leggeri avanzati e due anni dopo la Digisky che sviluppa elettronica di bordo per velivoli sportivi. Ma Cheli, che oggi fa anche parte del CdA dell’Agenzia Spaziale Italiana, continua a inseguire nuove avventure: decide di dedicarsi all’alpinismo e, lo scorso mag- gio, a 59 anni, entra nella ristretta élite degli italiani che sono riusciti ad arrivare in vetta all’Everest. Sig. Cheli, nel suo libro Tutto in un istante del 2015, lei ha affermato di essere sempre stato ‘il pilota della sua vita’. La sua passione per il volo l’ha spinta fino a diventare astronauta. Quando ha deciso, però, di dedicarsi all’al pinismo e quali ragioni l’hanno indotta a scalare l’Eve rest, ‘il tetto del mondo’? La voglia di salire mi è venuta guardando l’Everest dall’orbi- ta terrestre, durante la spedizione del 1996 con il Columbia. Ho pensato che mi sarebbe piaciuto molto ammirarlo da un’altra prospettiva, scalandolo con i miei mezzi. -
→ Space for Europe European Space Agency
number 153 | February 2013 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Poland, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams (to Dec 2012) → by elaborating and implementing a long-term European space policy, by recommending space objectives to the Member States, and by concerting the Director General: J.-J. Dordain policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States. -
The EXOD Search for Faint Transients in XMM-Newton Observations
UvA-DARE (Digital Academic Repository) The EXOD search for faint transients in XMM-Newton observations Method and discovery of four extragalactic Type I X-ray bursters Pastor-Marazuela, I.; Webb, N.A.; Wojtowicz, D.T.; van Leeuwen, J. DOI 10.1051/0004-6361/201936869 Publication date 2020 Document Version Final published version Published in Astronomy & Astrophysics Link to publication Citation for published version (APA): Pastor-Marazuela, I., Webb, N. A., Wojtowicz, D. T., & van Leeuwen, J. (2020). The EXOD search for faint transients in XMM-Newton observations: Method and discovery of four extragalactic Type I X-ray bursters. Astronomy & Astrophysics, 640, [A124]. https://doi.org/10.1051/0004-6361/201936869 General rights It is not permitted to download or to forward/distribute the text or part of it without the consent of the author(s) and/or copyright holder(s), other than for strictly personal, individual use, unless the work is under an open content license (like Creative Commons). Disclaimer/Complaints regulations If you believe that digital publication of certain material infringes any of your rights or (privacy) interests, please let the Library know, stating your reasons. In case of a legitimate complaint, the Library will make the material inaccessible and/or remove it from the website. Please Ask the Library: https://uba.uva.nl/en/contact, or a letter to: Library of the University of Amsterdam, Secretariat, Singel 425, 1012 WP Amsterdam, The Netherlands. You will be contacted as soon as possible. UvA-DARE is a service provided by the library of the University of Amsterdam (https://dare.uva.nl) Download date:02 Oct 2021 A&A 640, A124 (2020) Astronomy https://doi.org/10.1051/0004-6361/201936869 & c ESO 2020 Astrophysics The EXOD search for faint transients in XMM-Newton observations: Method and discovery of four extragalactic Type I X-ray bursters I. -
Pete Aldridge Well, Good Afternoon, Ladies and Gentlemen, and Welcome to the Fifth and Final Public Hearing of the President’S Commission on Moon, Mars, and Beyond
The President’s Commission on Implementation of United States Space Exploration Policy PUBLIC HEARING Asia Society 725 Park Avenue New York, NY Monday, May 3, and Tuesday, May 4, 2004 Pete Aldridge Well, good afternoon, ladies and gentlemen, and welcome to the fifth and final public hearing of the President’s Commission on Moon, Mars, and Beyond. I think I can speak for everyone here when I say that the time period since this Commission was appointed and asked to produce a report has elapsed at the speed of light. At least it seems that way. Since February, we’ve heard testimonies from a broad range of space experts, the Mars rovers have won an expanded audience of space enthusiasts, and a renewed interest in space science has surfaced, calling for a new generation of space educators. In less than a month, we will present our findings to the White House. The Commission is here to explore ways to achieve the President’s vision of going back to the Moon and on to Mars and beyond. We have listened and talked to experts at four previous hearings—in Washington, D.C.; Dayton, Ohio; Atlanta, Georgia; and San Francisco, California—and talked among ourselves and we realize that this vision produces a focus not just for NASA but a focus that can revitalize US space capability and have a significant impact on our nation’s industrial base, and academia, and the quality of life for all Americans. As you can see from our agenda, we’re talking with those experts from many, many disciplines, including those outside the traditional aerospace arena. -
Sentinel-2 and Sentinel-3 Mission Overview and Status
Sentinel-2 and Sentinel-3 Mission Overview and Status Craig Donlon – Sentinel-3 Mission Scientist and Ferran Gascon – Sentinel-2 QC manager and others @ESA IOCCG-21, Santa Monica, USA 1-3rd March 2016 Overview – What is Copernicus? – Sentinel-2 mission and status – Sentinel-3 mission and status Sentinel-3A OLCI first light Svalbard: 29 Feb 14:07:45-14:09:45 UTC Bands 4, 6 and 7 (of 21) at 490, 560, 620 nm Spain and Gibraltar 1 March 10:32:48-10:34:48 UTC California USA 29 Feb 17:44:54-17:46:54 UTC What is Copernicus? Space Component In-Situ Services A European Data Component response to global needs 6 What is Copernicus? – Space in Action for You! • A source of information for policymakers, industry, scientists, business and the public • A European response to global issues: • manage the environment; • understand and to mitigate the effects of climate change; • ensure civil security • A user-driven programme of services for environment and security • An integrated Earth Observation system (combining space-based and in-situ data with Earth System Models) Components & Competences Coordinators: Partners: Private Space Industries companies Component National Space Agencies Overall Programme EMCWF EMSA Mercator snd Ocean Coordination FRONTEX Service Services operators Component EUSC EEA JRC In-situ data are supporting the Space and Services Components Copernicus Funding Funding for Development Funding for Operational Phase until 2013 (c.e.c.): Phase as from 2014 (c.e.c.): ~€ 3.7 B (from ESA and € 4.3 B for the EU) whole programme (from EU) -
Metop Second Generation Payload
MetOp Second Generation Payload Marc Loiselet, Ville Kangas, Ilias Manolis, Franco Fois, Salvatore d’Addio European Space Agency, ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands E-mail: [email protected] MetOp-Second Generation Satellite Instruments Instrument Provider The ESA MetOp Second Generation (MetOp-SG) Programme was approved at the ESA Council Meeting at Ministerial level in Naples in Sat-A METimage DLR via EUMETSAT November 2012. IASI-NG CNES via EUMETSAT MetOp-SG is a follow-on to the current, first generation series of MetOp satellites, which is now established as a cornerstone of the global MWS ESA – MetOp-SG network of meteorological satellites. RO ESA – MetOp-SG The MetOp-SG programme is being implemented in collaboration with EUMETSAT. 3MI ESA – MetOp-SG ESA will develop the prototype MetOp-SG satellites (including associated instruments) and procure, on behalf of EUMETSAT, the recurrent Sentinel-5 ESA – GMES satellites (and associated instruments). The overall MetOp-SG space segment architecture consists of two series of satellites (Sat-A, Sat-B), each carrying different suites of instruments and operating in LEO polar orbit. The planned launches of the first of each series of satellites Sat-B SCA ESA – MetOp-SG are at the beginning of 2021 and at end 2022, respectively. MWI ESA – MetOp-SG RO ESA – MetOp-SG More information can be found in the “MetOp Second Generation – Overview” presentation from Graeme Mason, Hubert Barré, Maurizio ICI ESA – MetOp-SG Betto, ESA-ESTEC, The Netherlands. Argos-4 CNES via EUMETSAT Payload ESA is responsible for instrument design of six instruments, namely the MicroWave Sounder (MWS), Scatterometer (SCA), the Radio Occultation (RO), the MicroWave Imaging (MWI), the Ice Cloud Imager (ICI), and the Multi-viewing, Multi-channel, Multi-polarisation imager (3MI). -
Update on PROBA-2 TDM and ALPHASAT TDP8 Flight Data
Update on PROBA-2 TDM and ALPHASAT TDP8 Flight Data Christian POIVEY, Gerard PLANES CONANGLA, Marco d’ALESSIO, Reno HARBOE-SORENSEN ESA ESTEC CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 OUTLINE 1. PROBA-2 TDM 2. Summary of PROBA-2 TDM SEE flight data on memories 3. ALPHASAT TDP8 4. Summary of ALPHASAT TDP8 SEE flight data on memories CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 PROBA-2 Launched on November 2, 2009 LEO orbit: 713-733 km, 98 degrees inclination PROBA-2 - TDM 1. TDM : Memories on board TDM/Proba II a. TID (RADFETs) Atmel AT68166 (4*AT60142) 2M x 8 b. Reference SEU monitor Alliance AS7C34096A-12TI 512K x 8 c. SEL experiment Semi. – SEL Samsung K6R4008V1D 512K x 8 – SEU ISSI IS61LV5128AL-12 512K x 8 d. Flash memory experiment. 2. Period analyzed ISSI IS62WV20488BLL 2M x8 a. March 2010-January 2015 Samsung K9FG08U0M 1G x 8 – (1769 days) CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 PROBA-2 TDM CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 SEL experiment, SEL Data SEL experiment in TDM/Proba-2 Tot SAA Alliance Semi. AS7C34096A-12TI 512K x 8 3 2 Samsung K6R4008V1D-TI10 512K x 8 8 4 ISSI IS61LV5128AL-12 512K x 8 357 293 ISSI IS62WV20488BLL 2M x8 12 5 CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 SEL experiment, SEL Data IS61LV5128AL Differential latchup rate (smoothed in blue) CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 SEL experiment, SEL Data Comparison with Calculated Rates SEL rate prediction was performed for the 4 SRAMs using OMERE under solar maximum conditions, a sensitive volume thickness of 1 micron and 10 mm of Aluminum shielding. -
Cluster Keeping Algorithms for the Satellite Swarm Sensor Network Project
5th Federated and Fractionated Satellite Systems Workshop November 2-3, 2017, ISAE SUPAERO – Toulouse, France Cluster Keeping Algorithms for the Satellite Swarm Sensor Network Project Eviatar Edlerman and Pini Gurfil Technion – Israel Institute of Technology, Haifa 32000, Israel [email protected]; [email protected] Abstract This paper develops cluster control algorithms for the Satellite Swarm Sensor Network (S3Net) project, whose main aim is to enable fractionation of space-based remote sensing, imaging, and observation satellites. A methodological development of orbit control algorithms is provided, supporting the various use cases of the mission. Emphasis is given on outlining the algorithms structure, information flow, and software implementation. The methodology presented herein enables operation of multiple satellites in coordination, to enable fractionation of space sensors and augmentation of data provided therefrom. 1. INTRODUCTION In the field of earth observation from space, modern approaches show a trend of moving away from the classical single satellite missions, where one satellite includes a complete set of sensors and instruments, towards fractionated and distributed sensor missions, where multiple satellites, possibly carrying different types of sensors, act in a formation or swarm. Such missions promise an increase of imaging quality, an increase of service quality and, in many cases, a decrease of deployment costs for satellites that can become smaller and less complex due to mission requirements. Need for incremental deployment can be caused by funding limitations or issues. Although a combination of funds from different interest groups is possible, it can be difficult to achieve. A higher degree of independence for service providers can be enabled through lower cost satellites that allow integration into satellite swarms.