ACTS Technology Description and Results
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Thales Alenia Space Experience on Plasma Propulsion
Thales Alenia Space Experience on Plasma Propulsion IEPC-2007-301 Presented at the 30th International Electric Propulsion Conference, Florence, Italy September 17-20, 2007 Michel LYSZYK* and Laurent LECARDONNEL.† Thales Alenia Space, Cannes, 06150, France Abstract: Thales Alenia Space experience on plasma propulsion has been developed in the frame of Stentor, Astra 1K and GEI programs with plasma propulsion systems using SPT100 thrusters manufactured by Fakel and commercialized by Snecma . The PPS (plasma propulsion system) use in house equipments such as Power Processing Unit (PPU) manufactured by TAS-ETCA in Charleroi and the Thruster Orientation Mechanism (TOM) manufactured by TAS-France in Cannes . The PPS subsystem is used on board our SpaceBus satellite family to perform North-South station keeping. The on going activity on the XPS (Xenon Propulsion System) is devoted to the next European platform Alphabus currently under joint development by Thales Alenia Space and Astrium with CNES and ESA support. The XPS uses also the PPU manufactured by TAS-ETCA , the TOM manufactured by TAS-France and the Xe tank developed by TAS-Italy ; it use also the PPS1350 thruster under qualification by Snecma , a xenon regulator and a latch valve under development at Marotta Ireland. I. Introduction HIS document describes the Thales Alenia Space experience gained through Stentor , Astra 1K , GEI, T Spacebus and Alphabus programs on plasma Hall effect thrusters propulsion subsystems . For Spacebus application a description of the subsystem is given together with the general achieved performances . For Alphabus application a general status of the on going activities is given . * Head of electric propulsion section, Propulsion Department, [email protected]. -
GEO, Geonetcast and Building a Low Cost Ground Receiving Station
GEO, GEONETCast and building a low cost ground receiving station Ben Maathuis & Chris Mannaerts Dept Water Resources ITC-Enschede, The Netherlands Layout of presentation . Group on Earth Observation (GEO) . Global EO System of Systems . EUMETSAT’s contribution to GEO: EUMETCast . Services and data broadcasted . Ground reception system components . Data Management . Concluding remarks GEO: the Group on Earth Observations An Intergovernmental Organization with 89 Member Countries, the European Commission and around 67 Participating Organizations U.S. Department of State, Washington DC July 31, 2003 GEO objectives . Improve and coordinate earth (land & ocean) observation systems . Provide easier and more open data access . Foster use (science, applications) also through capacity building … to answer Society’s need for informed decision making GOAL of GEO: GOAL GEOSS: A Global, Coordinated, Comprehensive and Sustained System of Observing Systems GEO open data access & sharing principles • Open Access & exchange of data (globally) from Airborne, Space based and In Situ Observation Systems • Data and Products at Minimum Time delay and Minimum Cost • Free of Charge or cost of reproduction for Research and Education GEONETCast as backbone for data provision GEONETCast provides free near real-time environmental and Earth observation data and derived products to a worldwide user community using a telecommunication satellite based data distribution system. GEONETCast – system layout Layout of the GEONETCast telecommunication satellite based data distribution system GEONETCast - Africa Near real-time satellite image reception using a communication satellite based data distribution system, example MSG GEONETCast - Africa After central ground processing at EUMETSAT, images in full resolution are transmitted in HRIT mode, within five minutes of observation…. -
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. -
IAC-18-B2.1.7 Page 1 of 16 a Technical Comparison of Three
A Technical Comparison of Three Low Earth Orbit Satellite Constellation Systems to Provide Global Broadband Inigo del Portilloa,*, Bruce G. Cameronb, Edward F. Crawleyc a Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge 02139, USA, [email protected] b Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge 02139, USA, [email protected] c Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge 02139, USA, [email protected] * Corresponding Author Abstract The idea of providing Internet access from space has made a strong comeback in recent years. After a relatively quiet period following the setbacks suffered by the projects proposed in the 90’s, a new wave of proposals for large constellations of low Earth orbit (LEO) satellites to provide global broadband access emerged between 2014 and 2016. Compared to their predecessors, the main differences of these systems are: increased performance that results from the use of digital communication payloads, advanced modulation schemes, multi-beam antennas, and more sophisticated frequency reuse schemes, as well as the cost reductions from advanced manufacturing processes (such as assembly line, highly automated, and continuous testing) and reduced launch costs. This paper compares three such large LEO satellite constellations, namely SpaceX’s 4,425 satellites Ku-Ka-band system, OneWeb’s 720 satellites Ku-Ka-band system, and Telesat’s 117 satellites Ka-band system. First, we present the system architecture of each of the constellations (as described in their respective FCC filings as of September 2018), highlighting the similarities and differences amongst the three systems. -
Eutelsat Communications Q3 2015-16 PR FINAL
THIRD QUARTER 2015-16 REVENUES • Third Quarter revenues of €383 million, up 4.2% reported and 1.1% at constant currency • Nine month revenues of €1,157 million, up 6.1% reported and 1.3% at constant currency • Order backlog of €5.9 billion, representing four years of revenues • Current and next year objectives adjusted to reflect tougher industry conditions • Adapting strategy to lower growth environment Paris, 12 May 2016 – Eutelsat Communications (ISIN: FR0010221234 - Euronext Paris: ETL) today reported revenues for the third quarter and the nine months ended 31 March 2016. Key data: three months to 31 March 2016 Change at constant Q3 2014-15 Q3 2015-16 Actual change currency In € millions Video Applications 225.3 239.1 +6.1% +4.9% Data Services 58.1 54.4 -6.3% -12.6% Value-Added Services 23.4 25.3 +8.0% +7.7% Government Services 49.5 49.7 +0.5% -7.4% Other revenues 11.4 14.5 +27.0% +25.5% Sub-total 367.7 383.0 +4.2% +1.1% Non-recurring revenues - - - - Total 367.7 383.0 +4.2% +1.1% EUR/USD exchange rate 1.197 1.095 - - Revenue growth in the Third Quarter was below expectations, reflecting a worse than expected environment in several emerging markets, in particular in Latin America, where much of our new capacity is targeted and the spread of tough competitive conditions in Data Services to all markets. As a result, we now expect Full Year Revenues 2015-16 to be broadly flat (versus bottom-end of the 2-3% range previously). -
Classification of Geosynchronous Objects
esoc European Space Operations Centre Robert-Bosch-Strasse 5 D-64293 Darmstadt Germany T +49 (0)6151 900 www.esa.int CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Produced with the DISCOS Database Prepared by ESA’s Space Debris Office Reference GEN-DB-LOG-00211-OPS-GR Issue 20 Revision 0 Date of Issue 28 May 2018 Status Issued Document Type Technical Note Distribution ESA UNCLASSIFIED - Limited Distribution European Space Agency Agence spatiale europeenne´ Abstract This is a status report on geosynchronous objects as of 1 January 2018. Based on orbital data in ESA’s DISCOS database and on orbital data provided by KIAM the situation near the geostationary ring is analysed. From 1523 objects for which orbital data are available (of which 0 are outdated, i.e. the last available state dates back to 180 or more days before the reference date), 519 are actively controlled, 795 are drifting above, below or through GEO, 189 are in a libration orbit and 19 are in a highly inclined orbit. For 1 object the status could not be determined. Furthermore, there are 59 uncontrolled objects without orbital data (of which 54 have not been cata- logued). Thus the total number of known objects in the geostationary region is 1582. If you detect any error or if you have any comment or question please contact: Stijn Lemmens European Space Agency European Space Operations Center Space Debris Office (OPS-GR) Robert-Bosch-Str. 5 64293 Darmstadt, Germany Tel.: +49-6151-902634 E-mail: [email protected] Page 1 / 187 European Space Agency CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Agence spatiale europeenne´ Date 28 May 2018 Issue 20 Rev 0 Table of contents 1 Introduction 3 2 Sources 4 2.1 USSTRATCOM Two-Line Elements (TLEs) . -
Vom D Heft Nr. 258 / 18MB
W E L T R A U M - PHILATELI E Mitteilungsblatt Daheim bei Hermann Oberth: Nr. 258 ISSN 0948-6097 Jahreshauptversammlung 2015 Weltraum Philatelie e. V. 1. Vorsitzender, Geschäftsstelle : Dr. Stephen Lachhein, Schöne Aussicht 3c, 51381 Leverkusen, e-mail: [email protected] Stellv. Vorsitzender, Schriftführer, Mitteilungsblatt, Eil-Informationsdienst: Jürgen Peter Esders, Rue Paul Devigne 21-27, #6, 1030 Bruxelles, Belgien. E-mail: jpes- [email protected], Tel. +32 2 248.26.20 Schatzmeister: Michael Anderiasch, Irkensbusch 12 b, 46535 Dinslaken, Tel. 02064/970418, e-mail: [email protected] Beisitzer: Dr. Hans-Ferdinand Virnich, Bergstraße 1, 35764 Sinn, e-mail: [email protected] Siegfried Zimmerer, Stuttgarter Straße 177, 70469 Stuttgart-Feuerbach, e-mail: siegfried.zimmerer@t- online.de Mitgliedsbeitrag mit BDPh-Mitgliedschaft: 44 Euro Mitgliedsbeitrag ohne BDPh-Mitgliedschaft: 25 Euro Jugendliche: 10 Euro Bankverbindung: Kreissparkasse Waiblingen (BLZ 602 500 10), Konto Nr. 8 225 801 IBAN: DE73 6025 0010 0008 2258 01 – BIC: SOLADE S1 WBN Paypal: [email protected] Impressum : Weltraum Philatelie, Mitteilungsblatt ISSN 0948-6097 Herausgeber : Weltraum Philatelie e. V., Sitz Stuttgart, in Zusammenarbeit mit den Gmünder Weltraumfreunden, Gmünd/Österreich Verantwortlicher Redakteur (verantwortlich im Sinne der Pressegesetze): Jürgen Peter Esders, Brüssel, Belgien Auflage: bis zu 450 Exemplaren. Das Mitteilungsblatt erscheint 4 mal jährlich. Druck: Kopierbüro Schmidt, Markt 11, 01471 Radeburg, http://www.kopierschmidt.de Redaktionelle Beiträge von Vereinsmitgliedern oder Außenstehenden können ohne Begründung abge- lehnt. Kürzungen oder sinnenthaltende Textänderungen sowie eine Veröffentlichung zu einem späteren Zeitpunkt bleiben der Schriftleitung vorbehalten. Mit Verfassernamen oder Pseudonym gezeichnete Beiträge müssen nicht unbedingt mit der Meinung der Vorstandsmitglieder übereinstimmen bzw. können deren private Meinung darstellen. -
Britain Back in Space
Spaceflight A British Interplanetary Society Publication Britain back in Space Vol 58 No 1 January 2016 £4.50 www.bis-space.com 1.indd 1 11/26/2015 8:30:59 AM 2.indd 2 11/26/2015 8:31:14 AM CONTENTS Editor: Published by the British Interplanetary Society David Baker, PhD, BSc, FBIS, FRHS Sub-editor: Volume 58 No. 1 January 2016 Ann Page 4-5 Peake on countdown – to the ISS and beyond Production Assistant: As British astronaut Tim Peake gets ready for his ride into space, Ben Jones Spaceflight reviews the build-up to this mission and examines the Spaceflight Promotion: possibilities that may unfold as a result of European contributions to Suszann Parry NASA’s Orion programme. Spaceflight Arthur C. Clarke House, 6-9 Ready to go! 27/29 South Lambeth Road, London, SW8 1SZ, England. What happens when Tim Peake arrives at the International Space Tel: +44 (0)20 7735 3160 Station, where can I watch it, listen to it, follow it, and what are the Fax: +44 (0)20 7582 7167 broadcasters doing about special programming? We provide the Email: [email protected] directory to a media frenzy! www.bis-space.com 16-17 BIS Technical Projects ADVERTISING Tel: +44 (0)1424 883401 Robin Brand has been busy gathering the latest information about Email: [email protected] studies, research projects and practical experiments now underway at DISTRIBUTION the BIS, the first in a periodic series of roundups. Spaceflight may be received worldwide by mail through membership of the British 18 Icarus Progress Report Interplanetary Society. -
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 -
20030106126.Pdf
INSPACE PROPULSION--WHERE WE STAND AND WHAT'S NEXT Robert L. Sackheim Assistant Director and Chief Engineer for Propulsion NASA Marshall Space Flight Center, Marshall Space Flight Center, Alabama USA GBSTRGCT launch vehicles, many spacecraft suppliers, such as Baeing (formerly Hughes), Loral, and Northrop- The focus of this paper will be on the three stages Grumman (formerly TRW), have developed integral of in-space transportation propulsion systems, now propulsion systems (IPSs) on board their spacecraft commonly referred to as in-space propulsion (ISP); to perform many of the more conventional orbit i.e., the transfer of payloads from low-Earth orbits transfer functions. Some examples include the into higher orbits or into trajectories for planetary Hughes 601 and 702 commercial series of satellite encounters, including planetary landers and sample buses and the Northrop-Grumman IPS for the return launchers, if required. Functions required recent Chandra final orbit insertion functions. There at the operational location where ISP must provide have only been three complete upper stages devel- thrust for orbit include maintenance, position oped over the last 30 years: (1) The basic Centaur control, stationkeeping, and spacecraft altitude con- and all the associated upgrades, (2) the advanced trol; i.e., proper pointing and dynamic stability in Centaurs for the Delta 3 and 4 and the Atlas 3 and 5, inertial space; and the third function set to enable and (3) the inertial upper stage which is the only operations at various planetary locations, such upper stage that is currently certified for launch as atmospheric entry and capture, descent to the in a shuttle. -
Eutelsat S.A. €800,000,000 2.000 Per Cent Bonds Due 2 October 2025 Issue Price: 99.400 Per Cent
EUTELSAT S.A. €800,000,000 2.000 PER CENT BONDS DUE 2 OCTOBER 2025 ISSUE PRICE: 99.400 PER CENT The €800,000,000 aggregate principal amount 2.000 per cent. bonds due 2 October 2025 (the Bonds , and each a Bond ) of Eutelsat S.A. (the Issuer ) will be issued on 2 October 2018 (the Bond Issue ). Each Bond will bear interest on its principal amount at a fixed rate of 2.000 per cent. per annum from (and including) 2 October 2018 (the Issue Date ) to (but excluding) 2 October 2025, payable in Euro annually in arrears on 2 October of each year and commencing on 2 October 2019, as further described in "Terms and Conditions of the Bonds – Interest". Unless previously redeemed or purchased and cancelled in accordance with their terms and conditions, the Bonds will be redeemed at their principal amount on 2 October 2025 (the Maturity Date ). The Issuer may, at its option, and in certain circumstances shall, redeem all (but not part) of the Bonds at par plus any accrued and unpaid interest upon the occurrence of certain tax changes as further described in "Terms and Conditions of the Bonds – Redemption and Purchase – Redemption for tax reasons". The Bonds may also be redeemed (i) at the option of the Issuer, in whole or in part, at any time, prior to the Maturity Date, as further described in "Terms and Conditions of the Bonds — Redemption and Purchase — Make Whole Redemption by the Issuer", (ii) at any time prior to the Maturity Date, in whole (but not in part), at par plus accrued interest, if eighty (80) per cent. -
Here the Italian Space Agency ASI Holds 30% of the Shares and the Rest Is the Property of Avio Spa
Goliat the first Romanian satellite is approaching the launch date- less than 6 months since Romania will have its first space mission At a recent press conference, Jean-Yves Le Gall the director of ArianeSpace, shared with the public the plans of the company for 2011. Like for the last year we will have a busy schedule with not less than 12 launches (double than for 2010). As before the central point will be the veteran Ariane 5 rocket, but part of the new managerial strategy, ArianeSpace will look also for the segment of medium and small launchers meeting the demands of the worldwide customers. It is hoped that some part of the operations will be transferred gradually to these niches and thus to be over passed the record set last year when approximately 60% of the world GEO telecom satellites have been launched by ArianeSpace. The perspectives are very good with another 12 additional GEO transfer contracts being signed in 2010 (about 63% from the international commercial market). The technical procedures which make sure these flights are accomplished are also at the highest standards (proved by the last 3 launches of 2010 separated by one month each i.e. October, November and December) and the Ariane 5 rocket, because of the proven reliability has became today the preferred of the commercial launches (since December 2002 when the version ECA has been put into operation and when the inaugural flight ended by loosing the 2 satellite transported onboard-Stentor and Hot Bird 7- the rocket has an impressive record of 36 successful flights).