TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

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StratSat provides a geo-stationary platform at 20 km altitude capable of remaining on-station for up to five years. Payloads include high speed Internet services, direct broadcast TV, mobile telecommunication, etc. The envelope operates as a super-pressure hull(i. e. with no ballonet pressure control system). The hull will be of laminated fabric construction with Tedlar/Teflon, helium/weather barrier developed from AT-10/04. Multiple catenary curtain system supporting a payload module enclosed completely by the envelope. [The] payload module... comprises a single structural module with an externally mounted payload/mission system. The payload module provides a home for all of the airship's primary systems except for the propulsion system. The systems are close packed within the highly insulated module ensuring efficient heat and energy management. The payload module is pendulum stabilised within the envelope. The solar array provides the sole source of renewable energy for the airship. The array is placed over the upper quarter of the hull and extends over approximately three-quarters of the length of the craft. The array can be realigned to the daily sun location/angle by the roll rotation of the whole airship. The energy collected by the solar array is stored for use during the night in the series of batteries. Located in the stored for use during the night in a series of batteries. Located in the payload module, the batteries run the propulsion system, airship services and provide power to the mission system for up to 14 hours(during winter). The airship is propelled and steered by means of a ’Contra-Rotating Coned Rotor’ mounted on a tailcone at the rear of the envelope, as a part of a compound propulsion system. The unit provides longitudinal thrust(to counter the prevailing stratospheric winds) and lateral force(for manoeuvering) to enable the airship to hold station within a 1 km cube. The airship will be equipped with a multi-channel Flight Control Sy  7, fiche 1, Anglais, - StratSat%C2%AE

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StratSat® is a registered trademark.  8, fiche 1, Anglais, - StratSat%C2%AE

Fiche 1,  Justifications,  Français

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[...] le dirigeable géostationnaire britannique StratSat®, conçu par ATG (Advanced Technology Group) [est un] dirigeable souple d'environ 200 m de long pour 48 m de diamètre, [qui] devrait faire ses premiers vols vers 2005/2006 [...] Il pourra emporter 2 t de charge utile à 20 km d'altitude, avec une autonomie allant jusqu'à 5 ans. Pouvant se maintenir à poste avec une précision d'1 km³, il couvrira une surface au sol de 115 km de rayon.  1, fiche 1, Français, - StratSat%C2%AE

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

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A structure consisting of a platform and a payload.  3, fiche 2, Anglais, - observation%20platform

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BEOSAT is designed as a multifunctional Earth observation platform equipped with a microspectrometer and a debris sensor. The objectives are to analyse gases in Earth’s atmosphere and to detect the distribution of space debris in a 600-650 km sun-synchronous orbit. Other possible monitoring functions of BEOSAT are the detection of environmental pollution and the detection of light pollution to find new possible sites for Earth-based telescope locations that are not disturbed by the lights of nearby civilization.  4, fiche 2, Anglais, - observation%20platform

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observation platform: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  3, fiche 2, Anglais, - observation%20platform

Fiche 2,  Justifications,  Français

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Ensemble qui comporte une plate-forme et une charge utile.  1, fiche 2, Français, - plateforme%20d%27observation

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Pluriel : des plateformes, des plates-formes.  3, fiche 2, Français, - plateforme%20d%27observation

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plateforme (sing.); plateformes (pl.) : Ces graphies, puisées des Rectifications de l'orthographe recommandées par le Conseil supérieur de la langue française, sont attestées dans le Petit Robert (2004).  4, fiche 2, Français, - plateforme%20d%27observation

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plateforme d'observation : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  1, fiche 2, Français, - plateforme%20d%27observation

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

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The Special Purpose Dexterous Manipulator(SPDM) is an essential tool for maintaining and servicing the Space station. With its dual-arm design providing added flexibility, the SPDM will remove and replace smaller components; on the Station exterior, where precise handling : is required. It will be equipped with lights, video equipment, a tool platform and four tool holder. The SPDM can perform dexterous tasks by sensing various forces and moments on the payload. In response, it can automatically compensate its movements to ensure the payload is manipulated smoothly. With its two arms, the SPDM will load and unload objects, use robotic tools, attach and detach covers and install various units of the Space Station. It will either be attached to the end of Canadarm2 or ride independently on the Mobile Base System [MBS] and have Canadarm2 deliver equipment to it for servicing. It also has four cameras that will provide the crew inside the Station with additional views of the work areas. Like Canadarm2 and the MBS, the Special Purpose Dexterous Manipulator will be controlled by the crew inside the International Space Station. This system will allow the crew to perform many of the tasks that would otherwise require an astronaut to perform during a demanding spacewalk.  5, fiche 3, Anglais, - special%20purpose%20dexterous%20manipulator

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special purpose dexterous manipulator; SPDM: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  6, fiche 3, Anglais, - special%20purpose%20dexterous%20manipulator

Fiche 3,  Justifications,  Français

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Le manipulateur agile spécialisé (SPDM) est un outil essentiel à l'entretien de la Station spatiale. Grâce à ses deux bras, qui lui donnent une souplesse accrue, le SPDM pourra enlever et remplacer de petites composantes à l'extérieur de la Station, là ou une manipulation de précision est requise. II sera équipé de projecteurs, de matériel vidéo, d'une plate-forme d'outils et de quatre porte-outils. Le SPDM peut effectuer des tâches délicates en captant des forces et des moments sur la charge utile. En réponse, il peut automatiquement compenser ses mouvements pour assurer une manipulation en douceur de la charge utile. Grâce à ses deux bras, le SPDM chargera et déchargera des objets, utilisera des outils robotiques, fixera et enlèvera des couvercles et installera divers éléments de la Station spatiale. II sera fixé à l'extrémité du Canadarm2 ou fonctionnera indépendamment sur la Base mobile tandis que le Canadarm2 lui fournira l'équipement d'entretien. II est aussi équipé de quatre caméras qui donneront aux astronautes à l'intérieur de la Station des points d'observation supplémentaires des secteurs de travail. À l'instar du Canadarm2 et du MBS, le Manipulateur agile spécialisé sera commandé par l'équipage se trouvant à l'intérieur de la Station spatiale internationale. Le système permettra ainsi à l'équipage d'accomplir bon nombre des tâches qui autrement nécessiteraient une éprouvante sortie extravéhiculaire de la part d'un astronaute.  5, fiche 3, Français, - manipulateur%20agile%20sp%C3%A9cialis%C3%A9

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manipulateur agile spécialisé; SPDM : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  6, fiche 3, Français, - manipulateur%20agile%20sp%C3%A9cialis%C3%A9

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Fiche 4,  Justifications,  Anglais

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The Proteus piloted aircraft was designed and built by Scaled Composites, Inc., and is currently also operated by them. It is a twin turbofan high altitude platform with a crew of two and a seat for one additional person. It has a wingspan of 78 ft, gross weight of 12, 500 lb, fuel capacity of 5500 lb, can carry a 6900 lb podded payload, and supply 20 kW payload power.  2, fiche 4, Anglais, - piloted%20aircraft

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piloted aircraft: term standardized by ISO.  3, fiche 4, Anglais, - piloted%20aircraft

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Sondage atmosphérique. [...] Ces mesures [pression, température, humidité, vent, etc.] sont effectuées soit par capteurs aérotransportés (ballons libres, ou captifs, aéronefs pilotés ou téléguidés) ou largués par avion ou par fusées [...]  2, fiche 4, Français, - a%C3%A9ronef%20pilot%C3%A9

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aéronef piloté : terme normalisé par l'ISO.  3, fiche 4, Français, - a%C3%A9ronef%20pilot%C3%A9

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Fiche 5,  Justifications,  Anglais

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The 1. 4-million pound mobile launching platform is what the Atlas 5 sits upon from the time it is stacked together in the VIF [Vertical Integration Facility] until the main engine is fired at liftoff.... The platform is 45 feet wide, 55 feet long and 185 feet tall to the top of the mast, which features a wind damper that holds the rocket steady while exposed to the weather on the pad and routes propellant lines to the Centaur and conditioned air to the payload inside the nose cone.  2, fiche 5, Anglais, - wind%20damper

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Fiche 5,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

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The Starboard 0(S0) truss segment is the first major element of the International Space Station's enormous exterior framework. The S0 Truss is 13. 4 meters(44 feet) long and 4. 6 meters(15 feet) wide and weighs 12, 247 kilograms(27, 000 pounds). It is the center segment of 11 integrated trusses that will provide the foundation for station subsystem hardware installation, utility distribution, power generation, heat rejection and external payload accommodations. The S0 truss acts as the junction from which external utilities are routed to the pressurized modules by means of EVA-deployed umbilicals. The S0 truss is going to the space station with a complement of pre-integrated hardware to increase ISS functionality, including the Mobile Transporter, the Trailing Umbilical System, the Portable Work Platform, four Global Positioning System antennas, two rate gyros, an Extravehicular Charged Particle Detection System and umbilicals for U. S. on-orbit elements.  2, fiche 6, Anglais, - S0%20truss

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S0 truss; integrated truss structure S0; S0; ITS-S0: terms and abbreviations officially approved by the International Space Station official approval Group (ISSOAG).  13, fiche 6, Anglais, - S0%20truss

Fiche 6,  Justifications,  Français

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Atlantis (STS-110, mission 8A) rejoignait l'ISS [International Space Station] pour doter la Station d'une nouvelle structure : l'Integrated Truss Structure SO (le segment central de la poutre de 91 m à terme). Cette poutre de 13 m et lourde de 12 tonnes a été fixée au-dessus du laboratoire américain Destiny. Elle servira de base à des dizaines de tonnes d'équipements qui seront installés ces prochaines années : panneaux solaires, appareils de refroidissement et autres systèmes nécessaires au fonctionnement de l'ISS. Enfin, les astronautes d'Atlantis ont installé le transporteur mobile, un petit wagonnet qui doit servir de base mobile pour le bras robotique Canadarm2. Une fois opérationnel, le transporteur mobile circulera le long d'un rail installé le long de la poutre S0.  5, fiche 6, Français, - poutre%20S0

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poutre S0; segment de poutre intégrée S0; S0; ITS-S0 : termes et abréviations uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  4, fiche 6, Français, - poutre%20S0

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Fiche 7,  Justifications,  Anglais

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The Polar Platform activities are proceeding according to plan. Manufacture of the Service Module flight-model structure is well advanced and should be completed by end-1994. Integration of the flight model will start in early 1995. Availability of the Payload Module structural model has been delayed due to manufacturing difficulties.  2, fiche 7, Anglais, - service%20module%20flight%20model%20structure

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Fiche 8,  Justifications,  Anglais

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The structure design is one of the fundamental defining subsystems of the spacecraft, and as such the AMP structure is the baseline structure. This structure presents several challenges to be used on a microsatellite, namely the cost, AIT operations and adaptability to change. Also, the fact that this structure has not flown before, makes it more difficult to predict what are the problems that one might encounter when actually building the spacecraft. On the other hand, this structure allows a generous payload capacity in a low total mass platform. The accommodation study performed, shows that it is possible to fit the mission in the AMP structure...  2, fiche 8, Anglais, - accommodation%20study

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Fiche 9,  Justifications,  Anglais

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The Mobile Base System is an aluminum structure mounted on the mobile transporter. It serves as a storage location and a work platform for astronauts. The MBS is equipped with four Power Data Grapple Fixtures and a Latching End Effector to hold payloads. The MBS also provides a Common Attach System to accommodate payload transportation and servicing, and provides structural and electrical interfaces to users.  1, fiche 9, Anglais, - mobile%20base%20system

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The MSS [Mobile Servicing System] consists of three main elements: the Space Station Remote Manipulator System (SSRMS), known as Canadarm2, the Mobile Base System (MBS), and the Special Purpose Dexterous Manipulator (SPDM). Canadarm2 and the MBS, its platform, are essential tools for the assembly of the ISS [International Space Station].  2, fiche 9, Anglais, - mobile%20base%20system

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mobile base system; MBS: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, fiche 9, Anglais, - mobile%20base%20system

Fiche 9,  Justifications,  Français

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La Base mobile (MBS) constitue une plate-forme mobile et un poste d'entreposage à l'intention des astronautes pendant les sorties extravéhiculaires. La MBS est équipée de quatre bornes électromécaniques, elle peut donc simultanément servir de base pour le Canadarm2 et pour le Manipulateur agile spécialisé. Puisqu'elle est montée sur un transporteur mobile de fabrication américaine, la MBS peut déplacer ces éléments clés vers le poste de travail requis en faisant glisser le transporteur sur des rails installés sur toute la largeur de la Station.  3, fiche 9, Français, - base%20mobile

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base mobile; MBS : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  4, fiche 9, Français, - base%20mobile

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Fiche 10,  Justifications,  Anglais

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The Window Observational Research Facility(WORF). The WORF will provide a stable platform such that the full capacity of the U. S. Laboratory window(the highest optical quality window ever flown on an inhabited spacecraft) can be utilized. The WORF will provide payload support infrastructure including mounting hardware, power, cooling, and access to the ISS [International Space Station] data system. The WORF will provide protection for the interior of the Lab window and control stray light exchange between the Lab interior and the external Station environment. The WORF will be economically based upon structures and electronics already designed and certified for operation onboard the ISS and will allow easy periodic upgrade and changeout of support subsystems. WORF computer interfaces will maximize commonality with ISS command and data handling systems.  2, fiche 10, Anglais, - window%20observational%20research%20facility

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window observational research facility; WORF: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, fiche 10, Anglais, - window%20observational%20research%20facility

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Window observational research facility block 2.  3, fiche 10, Anglais, - window%20observational%20research%20facility

Fiche 10,  Justifications,  Français

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Window Observational Research Facility. Cet élément un peu particulier comporte un hublot pratiqué dans la paroi du module laboratoire équipé d'un verre de qualité optique. Il peut recevoir différents instruments dédiés à l'observation de la surface terrestre et sera utilisé notamment pour l'étude des continents ou des phénomènes atmosphériques.  2, fiche 10, Français, - hublot%20d%27observation%20du%20laboratoire%20Destiny

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hublot d'observation du laboratoire Destiny; WORF : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, fiche 10, Français, - hublot%20d%27observation%20du%20laboratoire%20Destiny

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Fiche 11,  Justifications,  Anglais

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The Envisat Mission System Preliminary Design Review(EMS-PDR) has been completed with a Review Board meeting in the second half of July 1994. All elements of the Envisat-1 mission, including the Polar Platform, the payload instruments and the ground segment, have been reviewed together for the first time, showing good overall progress. Problems have been identified in some specific areas and the necessary remedial actions have been defined. The industrial consortia, led by BAe and Dornier, have been briefed on the main results of the Review.  2, fiche 11, Anglais, - Envisat%20mission%20system%20preliminary%20design%20review

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Fiche 12,  Justifications,  Anglais

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The INTEGRAL ISVV project deals with four different SW modules; the attitude control computer SW, the star tracker SW, the central data management unit SW and the digital processing electronics(DPE) common services SW(CSSW). This case only covers the last SW component, the DPE CSSW. Together the DPE and the DPE CSSW provide a computing platform for the payload(scientific instruments) on the INTEGRAL satellite.  2, fiche 12, Anglais, - digital%20processing%20electronics

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