A Case Study in UML Model-Based Dynamic Validation: the Ariane-5 Launcher Software?
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Ariane-5 Completes Flawless Third Test Flight
r bulletin 96 — november 1998 Ariane-5 Completes Flawless Third Test Flight A launch-readiness review conducted on Friday engine shut down and Maqsat-3 was 16 and Monday 19 October had given the go- successfully injected into GTO. The orbital ahead for the final countdown for a launch just parameters at that point were: two days later within a 90-minute launch Perigee: 1027 km, compared with the window between 13:00 to 14:30 Kourou time. 1028 ± 3 km predicted The launcher’s roll-out from the Final Assembly Apogee: 35 863 km, compared with the Building to the Launch Zone was therefore 35 898 ± 200 km predicted scheduled for Tuesday 20 October at 09:30 Inclination: 6.999 deg, compared with the Kourou time. 6.998 ± 0.05 deg predicted. On 21 October, Europe reconfirmed its lead in providing space Speaking in Kourou immediately after the flight, transportation systems for the 21st Century. Ariane-5, on its third Fredrik Engström, ESA’s Director of Launchers qualification flight, left no doubts as to its ability to deliver payloads and the Ariane-503 Flight Director, confirmed reliably and accurately to Geostationary Transfer Orbit (GTO). The new that: “The third Ariane-5 flight has been a heavy-lift launcher lifted off in glorious sunshine from the Guiana complete success. It qualifies Europe’s new Space Centre, Europe’s spaceport in Kourou, French Guiana, at heavy-lift launcher and vindicates the 13:37:21 local time (16:37:21 UT). technological options chosen by the European Space Agency.” This third Ariane-5 test flight was intended ESA’s Director -
6. the INTELSAT 17 Satellite
TWO COMMUNICATIONS SATELLITES READY FOR LAUNCH Arianespace will orbit two communications satellite on its fifth launch of the year: INTELSAT 17 for the international satellite operator Intelsat, and HYLAS 1 for the European operator Avanti Communications. The choice of Arianespace by leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Based on its proven reliability and availability, Arianespace continues to confirm its position as the world’s benchmark launch system. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads. Arianespace and Intelsat have built up a long-standing relationship based on mutual trust. Since 1983, Arianespace has launched 48 satellites for Intelsat. Positioned at 66 degrees East, INTELSAT 17 will deliver a wide range of communication services for Europe, the Middle East, Russia and Asia. Built by Space Systems/Loral of the United States, this powerful satellite will weigh 5,540 kg at launch. It will also enable Intelsat to expand its successful Asian video distrubution neighborhood. INTELSAT 17 will replace INTELSAT 702. HYLAS 1 is Avanti Communications’ first satellite. A new European satellite operator, Avanti Communications also chose Arianespace to orbit its HYLAS 2 satellite, scheduled for launch in the first half of 2012. HYLAS 1 was built by an industrial consortium formed by EADS Astrium and the Indian Space Research Organisation (ISRO), using a I-2K platform. Fitted with Ka-band and Ku-band transponders, the satellite will be positioned at 33.5 degrees West, and will be the first European satellite to offer high-speed broadband services across all of Europe. -
ARIANE 5 Data Relating to Flight 225
KOUROU August 2015 ARIANE 5 Data relating to Flight 225 EUTELSAT 8 West B Intelsat 34 Data relating to Flight 225 Flight 225 Ariane 5 Satellites: EUTELSAT 8 WEST B – INTELSAT 34 Content 1. Introduction .................................................................... 3 2. Launcher L579 ............................................................... 4 3. Mission V225 ............................................................... 10 4. Payloads ...................................................................... 19 5. Launch campaign ........................................................ 32 6. Launch window ............................................................ 35 7. Final countdown .......................................................... 36 8. Flight sequence ........................................................... 40 9. Airbus Defence and Space and the ARIANE programmes ........................................................................ 42 2 Data relating to Flight 225 1. Introduction Flight 225 is the 81st Ariane 5 launch and the fourth in 2015. It follows on from a series of 66 consecutive successful Ariane 5 launches. This is the 51st ARIANE 5 ECA (Cryogenic Evolution type A), the most powerful version in the ARIANE 5 range. Flight 225 is a commercial mission for Ariane 5. The L579 launcher is the twenty-fifth to be delivered by Airbus Defence and Space to Arianespace as part of the PB production batch. The PB production contract was signed in March 2009 to guarantee continuity of the launch service after completion -
Paper Session II-A-Current Status of the Ariane 4 Program and of The
1994 (31st) Space Exploration and Utilization The Space Congress® Proceedings for the Good of the World Apr 27th, 1:00 PM - 4:00 PM Paper Session II-A - Current Status of the Ariane 4 Program and of the Ariane 5 Development James R. Youdale Arianespace Inc. Washington, D.C. Douglas A. Heydon Arianespace Inc. Washington, D.C. Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Youdale, James R. and Heydon, Douglas A., "Paper Session II-A - Current Status of the Ariane 4 Program and of the Ariane 5 Development" (1994). The Space Congress® Proceedings. 16. https://commons.erau.edu/space-congress-proceedings/proceedings-1994-31st/april-27-1994/16 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Current Status of the Ariane 4 Program and of the Ariane 5 Development James R. Youdale1 and Douglas A. Heyden~ Arianespace Inc. Washington, D.C. Abstract This paper provides an overview of the commercial siruation of Arianespace, a general update regarding its technical and operational activities and its near and medium term prospects. A summary of the Ariane 4 "track record" is given and the latest improvement to its third staae the HIO III, is presented. Operational improvements that reduce the interval between two = ' consecutive laWlches are also addressed. The ratiollale for going to Ariane 5 is discussed and the current status of the Ariane 5 development program is reviewed. -
Launch Vehicle Control Center Architectures
Launch Vehicle Control Center Architectures Michael D. Watson1, Amy Epps2, and Van Woodruff3 NASA Marshall Space Flight Center, Huntsville, AL 35812 Michael Jacob Vachon4 NASA Johnson Space Center, Houston, TX 77058 Julio Monreal5 European Space Agency, Launchers Directorate, Paris, France Marl Levesque6 United Launch Alliance, Vandenberg AFB and Randall Williams7 and Tom McLaughlin8 Aerospace Corporation, El Segundo, CA 90245 Launch vehicles within the international community vary greatly in their configuration and processing. Each launch site has a unique processing flow based on the specific launch vehicle configuration. Launch and flight operations are managed through a set of control centers associated with each launch site. Each launch site has a control center for launch operations; however flight operations support varies from being co-located with the launch site to being shared with the space vehicle control center. There is also a nuance of some having an engineering support center which may be co-located with either the launch or flight control center, or in a separate geographical location altogether. A survey of control center architectures is presented for various launch vehicles including the NASA Space Launch System (SLS), United Launch Alliance (ULA) Atlas V and Delta IV, and the European Space Agency (ESA) Ariane 5. Each of these control center architectures shares some similarities in basic structure while differences in functional distribution also exist. The driving functions which lead to these factors are considered and a model of control center architectures is proposed which supports these commonalities and variations. I. INTRODUCTION Launch vehicles in both Europe and the United States have been operating successfully for several decades. -
Indian Remote Sensing Satellites (IRS)
Topic: Indian Remote Sensing Satellites (IRS) Course: Remote Sensing and GIS (CC-11) M.A. Geography (Sem.-3) By Dr. Md. Nazim Professor, Department of Geography Patna College, Patna University Lecture-5 Concept: India's remote sensing program was developed with the idea of applying space technologies for the benefit of human kind and the development of the country. The program involved the development of three principal capabilities. The first was to design, build and launch satellites to a sun synchronous orbit. The second was to establish and operate ground stations for spacecraft control, data transfer along with data processing and archival. The third was to use the data obtained for various applications on the ground. India demonstrated the ability of remote sensing for societal application by detecting coconut root-wilt disease from a helicopter mounted multispectral camera in 1970. This was followed by flying two experimental satellites, Bhaskara-1 in 1979 and Bhaskara-2 in 1981. These satellites carried optical and microwave payloads. India's remote sensing programme under the Indian Space Research Organization (ISRO) started off in 1988 with the IRS-1A, the first of the series of indigenous state-of-art operating remote sensing satellites, which was successfully launched into a polar sun-synchronous orbit on March 17, 1988 from the Soviet Cosmodrome at Baikonur. It has sensors like LISS-I which had a spatial resolution of 72.5 meters with a swath of 148 km on ground. LISS-II had two separate imaging sensors, LISS-II A and LISS-II B, with spatial resolution of 36.25 meters each and mounted on the spacecraft in such a way to provide a composite swath of 146.98 km on ground. -
Vega: the European Small-Launcher Programme
r bulletin 109 — february 2002 Vega: The European Small-Launcher Programme R. Barbera & S. Bianchi Vega Department, ESA Directorate of Launchers, ESRIN, Frascati, Italy Background The programme was adopted by ESA in June The origins of the Vega Programme go back to 1998, but the funding was limited to a Step 1, the early 1990s, when studies were performed with the aim of getting the full approval by the in several European countries to investigate the European Ministers meeting in Brussels in May possibility of complementing, in the lower 1999. This milestone was not met, however, payload class, the performance range offered because it was not possible to obtain a wide by the Ariane family of launchers. The Italian consensus from ESA’s Member States for Space Agency (ASI) and Italian industry, in participation in the programme. This gave rise to particular, were very active in developing a period of political uncertainty and to a series concepts and starting pre-development work of negotiations aimed at finding an agreeable based on established knowhow in solid compromise. It is important, on the other hand, propulsion. When the various configuration to record that during the same period the options began to converge and the technical technical definition work continued without feasibility was confirmed, the investigations major disruption, and development tests on the were extended to include a more detailed Zefiro motor were successfully conducted. definition in terms of a market analysis and related cost targets. The subsequent extension of the duration of Step 1 provided the opportunity to revisit and By the end of 2001, the development programme for Europe’s new update the market analysis, based on the small Vega launcher was well underway. -
Technology Acceleration Process for the THEMIS Low Cost and Reusable Prototype
DOI: 10.13009/EUCASS2019-97 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Technology acceleration process for the THEMIS low cost and reusable prototype Jerome VILA* and Jeremie HASSIN** *ArianeWorks / CNES [email protected] **ArianeWorks / CNES [email protected] Abstract While Ariane 6 and Vega-C are about to being fielded and entering operations, CNES and Arianegroup are already actively preparing next generation of European launchers. With the PROMETHEUS oxygen/methan engine starting subsystems testing in 2018, and the CALLISTO experimental reusable vehicle about to complete Preliminary Design, engineering work has been initiated for next step on the European roadmap: THEMIS. THEMIS is both a demonstrator and a prototype of a low cost and reusable first stage, meant as the centrepiece of future Ariane architectures. It is intended to feature PROMETHEUS and will build upon technologies and lessons learned from the CALLISTO programme. Several challenges lie ahead for THEMIS, with two highlights: meeting an aggressive cost targets consistent with the 50% launch cost cut sought beyond Ariane 6, and keeping a swift tempo for getting THEMIS ready well before 2025. To address those challenges, a specific initiative was undertaken by CNES and Arianegroup, under codename ArianeWorks: combining both a “Skunkworks like” approach and an open-innovation platform, ArianeWorks is tasked with getting the project done quicker and bolder than through a conventional organization. The paper will discuss the system engineering approach adopted for THEMIS design, by identifying and then allocating technical objectives related to Ariane 6 evolution/Ariane NEXT between CALLISTO and different sized THEMIS options. Then, the early hardware/testing “agile” development process will be detailed, with an aim at speeding up design iterations and technology maturations. -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 1st Quarter 1998 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 1ST QUARTER 1998 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
Download Here Avio's Company Profile
SPACE IS CLOSER CORPORATE PROFILE Where we come from Avio is a space propulsion leader, with over 1,000 employees located in Italy, France and French Guiana. Since its foundation in 1912, the company has played a key role in the design, manufacturing and integration of space launcher systems and tactical missiles. With such a long history and track record, Avio today has extensive expertise in solid and liquid propulsion systems, chemicals and propellants, composite materials, system integration, experimental testing, flight and simulation software, on-board avionics and satellite launch operations. Evolving towards the future Since 2017 Avio has been listed on the STAR segment of the Italian Stock Exchange and was the first rocket manufacturing company in the world to become a public company with over 70% of its share capital floating on the market. With such a set-up Avio is today equipped to accelerate its investment ambitions, pursuing rapid growth for the future. In recent years Avio has delivered revenue growth at an average annual rate in excess of 15%. Our mission Our mission is to provide reliable and competitive access to space to improve life on earth. To this end, Avio has developed the Vega Launch System, a combination of launchers and adapters to carry any small-medium satellite into Low Earth Orbit on single, dual or multi-payload missions, serving any type of customer globally. Avio is committed to over time deliver new versions of the Vega system to continuously improve reliability, flexibility and cost-competitiveness. Vega Launchers Avio has designed, manufactured and assembled solid and liquid propulsion systems for more than 50 years. -
The Ariane-5 ECA Heavy-Lift Launcher
Berkes 9/13/05 10:46 AM Page 14 Ariane-5 ECA Uwe L. Berkes Ariane Project Department, Directorate of Launchers, ESA, Paris The Ariane-5 ECA Heavy-Lift riane-5 ECA made a flawless qualification flight on 12 February 2005, heralding this version of the launcher’s readiness to enter the launch- services market. This major step forward was the result of more than two years of very intense efforts within the framework of the Ariane Launcher ARecovery Plan, endorsed by the ESA Council on Ministerial Level in May 2003, after the failure of the ECA version’s maiden flight in December 2002. The recovery involved ESA, CNES, Arianespace and European Industry in a consolidated effort to establish this launcher as the European launch- services ‘workhorse’ for many years to come. Introduction programmes: the Ariane-5 Evolution Principal Cryotechnique), and the Vulcain ESA’s Ariane Development Programme is Programme, and the Ariane-5 Plus main engine. The latter concentrated on the funded by 14 Participating States. Ariane- Programme. The aim of the former was to development of new upper stages, of 5 has been launched 21 times to date from improve the performance of the launcher’s which the ESC-A (Etage Superieur the European Spaceport (CSG) in Kourou, lower composite, consisting of the Cryotechnique A) has become the upper- French Guiana, with four of those launches boosters, the central EPC stage (Etage stage of Ariane-5 ECA. dedicated to the flight-qualification of the various versions. The commercial flights are prepared and operated by Arianespace, which orders the production launchers from European Industry. -
Soyuz to Launch Globalstar
SOYUZ TO LAUNCH GLOBALSTAR Starsem's current mission will launch four satellites for Globalstar, a leading provider of mobile satellite voice and data services. These four satellites, together with four additional satellites to be launched by Starsem later this year, will be used to augment the company’s current first-generation LEO (low earth orbit) satellite constellation. Between February and November 1999, Starsem successfully launched twenty four Globalstar satellites, one half of the original constellation, using six Soyuz launch vehicles. Globalstar has once again reaffirmed its confidence in Starsem with these two 2007 launches to inject the four 450 kilograms satellites into a circular phasing orbit at an altitude of 920 km and at an orbital inclination of 52 degrees. Visit us on www.starsem.com 1 MISSION DESCRIPTION The Globalstar launch will be performed from the Baikonur Cosmodrome, Launch Pad #6. The launch will occur on Tuesday, May 29, 2007, at 08:31 p.m. UTC: 02:31 a.m. Baikonur time (Wednesday, May 30) 00:31 a.m. Moscow time (Wednesday, May 30) 10:31 p.m. Paris time (Tuesday, May 29) 01:31 p.m. Pacific Daylight Time (Tuesday, May 29) The launch window : ±1sec The Launch Vehicle Flight at a Glance After lift-off from the Baikonur Cosmodrome, the flight of the three lower stages of the Soyuz launch vehicle will last for 8 minutes and 48 seconds. At this time, the Soyuz third stage will separate from the nose module, consisting of the Fregat upper stage, the satellite dispenser and the four Globalstar satellites. The three lower Soyuz stages will fall back to Earth.