TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 OBS

Each TTCS receives commands, SAR control tables and other data from the MCF [Metadata Configuration file] and transmits them to the satellite; it receives telemetry data from the spacecraft and transmits them to the MCF; it also carries out tracking measurements on the satellite and transmits the results to the MCF. Additional TT&C stations(the external TT&C network) will be used for support during the Launch and Early Orbit Period(LEOP) and potentially during other parts of the mission.  2, record 1, English, - telemetry%2C%20tracking%20and%20command%20station

Record number: 1, Textual support number: 2 OBS

telemetry, tracking and command station; TTCS: term and abbreviation officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 1, English, - telemetry%2C%20tracking%20and%20command%20station

Record number: 1, Textual support number: 1 PHR

Telemetry, tracking and command station - optical (SPTT-O); telemetry, tracking and command station - radar (SPTT-R).  4, record 1, English, - telemetry%2C%20tracking%20and%20command%20station

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 OBS

station de poursuite, de télécommande et de télémesure; SPTT : terme et abréviation uniformisés par le Comité d'uniformisation de la terminologie spatiale (CUTS) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 1, French, - station%20de%20poursuite%2C%20de%20t%C3%A9l%C3%A9commande%20et%20de%20t%C3%A9l%C3%A9mesure

Record number: 1, Textual support number: 1 PHR

Station de poursuite, de télécommande et de télémesure - optique; station de poursuite, de télécommande et de télémesure - radars.  2, record 1, French, - station%20de%20poursuite%2C%20de%20t%C3%A9l%C3%A9commande%20et%20de%20t%C3%A9l%C3%A9mesure

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

Launch and early orbit phase. The launch phase involves a series of delicate operations not only for the... launcher, but also for the fully-assembled satellite... The launch phase... ends 18 minutes and 25 seconds after lift-off when the satellite separates from the launcher. The satellite, controlled by its onboard computer, then begins a series of automatic operations known as the "acquisition sequence". At the end of this sequence, the payload instruments are pointing earthward and the satellite's internal configuration is very close to that required for routine operations.  3, record 2, English, - launch%20and%20early%20orbit%20phase

Record number: 2, Textual support number: 1 OBS

launch and early orbit phase; LEOP: term and abbreviation officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 2, English, - launch%20and%20early%20orbit%20phase

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 CONT

[...] la phase de lancement et de début de vol du satellite [...] est caractérisée par la séparation du satellite de son lanceur, le dégagement de l'engin spatial et le déploiement des panneaux solaires qui alimentent ce dernier en énergie [...]  4, record 2, French, - phase%20de%20lancement%20et%20de%20d%C3%A9but%20de%20vol

Record number: 2, Textual support number: 1 OBS

phase de lancement et de début de vol; LEOP : terme et abréviation uniformisés par le Groupe de travail de la terminologie de RADARSAT-2 GTTR.  2, record 2, French, - phase%20de%20lancement%20et%20de%20d%C3%A9but%20de%20vol

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Electrical Integration is a vital part of Assembly, Integration & Testing(AIT) process of spacecraft, which plays its role from Layout Design till Launch. AIT is the process in which the satellite subsystems are integrated in a predetermined sequence, performance and interface checks carried out to arrive at a complete spacecraft in full configuration. At launch site, the spacecraft will go through different phases of assembly and testing as per pre-launch operation plan before being cleared for launch.  2, record 3, English, - assembly%2C%20integration%20and%20testing

Record number: 3, Textual support number: 1 OBS

assembly, integration and testing; AIT: term and abbreviation officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  5, record 3, English, - assembly%2C%20integration%20and%20testing

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 CONT

L'AIE : Processus d'intégration des sous-systèmes d'un satellite selon une séquence pré-établie. Les essais de performance et d'interface effectués permettent de connaître la configuration complète du véhicule spatial. Sur le site de lancement, le véhicule doit passer toutes les étapes d'assemblage et d'essai prévus au plan opérationnel de pré-lancement avant que ne soit donné l'aval pour le lancement.  6, record 3, French, - assemblage%2C%20int%C3%A9gration%20et%20essai

Record number: 3, Textual support number: 1 OBS

assemblage, intégration et tests; AIT : terme et abréviation uniformisés par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  6, record 3, French, - assemblage%2C%20int%C3%A9gration%20et%20essai

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The propulsion system for the Ariane-5 launcher's cryogenic main stage operated successfully for 280 seconds(the nominal time authorised for a battleship tank configuration) in a test carried out on Thursday, 17 November 1994 in the launch zone at the Guiana Space centre(CSG) in Kourou, French Guiana.  3, record 4, English, - battleship%20tank

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 DEF

Réservoir d'essai dont les parois sont plus épaisses.  2, record 4, French, - r%C3%A9servoir%20lourd

Record number: 4, Textual support number: 1 CONT

1992, dans l'été, un réservoir lourd de l'étage central d'Ariane 5 est monté sur une structure support en métal et amené sur la zone de lancement pour des tests de compatibilité. Cette version Battle Ship BS sera équipé d'un moteur Vulcain et servira en 1994 pour des essais de mise à feu sur le pad.  3, record 4, French, - r%C3%A9servoir%20lourd

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

The Ariane 5 launch vehicle is composed of a lower composite and an upper composite. The lower composite is an assembly comprising two solid rocket motors and a main cryogenic stage, which basically functions like a traditional second stage. The lower composite is identical for all missions, whereas the configuration of the upper composite changes according to the assigned mission.  2, record 5, English, - upper%20composite

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

À côté de la case à équipements qui contrôle tout le vol du lanceur, le principal élément de la partie composite supérieure du lanceur Ariane 5 est l'étage à propergol stockable (EPS). L'étage cryotechnique principal ayant été largué, l'EPS assure l'augmentation continue de la vitesse nécessaire pour injecter les charges utiles sur l'orbite visée, et avec la précision requise.  3, record 5, French, - partie%20composite%20sup%C3%A9rieure

Record number: 5, Textual support number: 2 CONT

La case à équipements du lanceur (VEB) est souvent appelée le «cerveau» du lanceur. Elle se trouve au sommet de l'étage cryotechnique principal et se raccorde à la partie haute ou composite supérieure comprenant l'étage de propergol stockable Aestus qui vient se nicher au centre de la case.  4, record 5, French, - partie%20composite%20sup%C3%A9rieure

Record number: 5, Textual support number: 1 OBS

composite : Les exemples trouvés donnent ce nom au féminin alors que dans les dictionnaires ce mot est masculin.  5, record 5, French, - partie%20composite%20sup%C3%A9rieure

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

Launch configuration. The BepiColombo spacecraft is a composite of five modules : two for propulsion : Solar Electric Propulsion Module(SEPM), and Chemical Propulsion Module(CPM), and three carrying scientific instruments, namely : Mercury Planetary Orbiter, Mercury Magnetospheric Satellite(MeMS), Mercury Surface Element(MSE).  2, record 6, English, - solar%20electric%20propulsion%20module

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 OBS

propulsion solaire-électrique : SMART-1 2002. Ce petit engin expérimental fera la démonstration de l'utilisation de la propulsion solaire-électrique et emportera un ensemble d'instruments scientifiques pour inspecter la Lune.  2, record 6, French, - module%20de%20propulsion%20solaire%2D%C3%A9lectrique

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

The Extendible Support Structure(ESS) deploys and supports the SAR antenna panels in its mission configuration. The ESS assembly consists of an Electronic Control Unit(ECU), a drive mechanism assembly, and two identical independently-deployable wing assemblies. Each wing includes a deployment mechanism, a truss structure supporting two SAR antenna panels, and a variety of sensors. The ESS subsystem also includes command and telemetry to control and monitor the ESS prior to and during deployment. During launch, the ESS is supported by the SAR antenna panels which are restrained against the Spacecraft Support Structure by Antenna Tie-Downs at six locations per wing. Deployment of the ESS is initiated by a ground command sometime after the release of the antenna tie-downs. Following deployment, the ESS is capable of supporting the SAR antenna panels such that the peak-to-peak deviation due to thermo-elastic distortion is not greater than 1. 1 mm over the entire antenna surface.  4, record 7, English, - extendible%20support%20structure

Record number: 7, Textual support number: 1 OBS

extendible support structure; ESS: term and abbreviation officially approved by the RADARSAT-2 official approval Group (ROAG).  5, record 7, English, - extendible%20support%20structure

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 DEF

[...] mécanisme conçu pour se déployer et soutenir les panneaux du radar à synthèse d'ouverture une fois en orbite, selon une configuration précise.  2, record 7, French, - structure%20porteuse%20d%C3%A9pliable

Record number: 7, Textual support number: 1 OBS

structure porteuse dépliable; ESS : terme et abréviation uniformisés par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 7, French, - structure%20porteuse%20d%C3%A9pliable

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The orbital aircraft has the capability to fly suborbital missions without propellant transfer, to distances of 3, 000 to 6, 000 nautical miles, depending on the aerodynamic configuration This capability exists because the airframe is capable of independent takeoff and landing. This offers a transcontinental range for a number of alternate missions that are difficult to imagine for an air launch concept. For the same reason, the tanker and orbital aircraft may be based at different locations, and interfaced only in flight. This offers more basing flexibility and removes the requirements for specialized facilities and ground support equipment such as that needed to mate the Shuttle orbiter to its carrier aircraft.  2, record 8, English, - orbital%20aircraft

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 DEF

Avion hypersonique dont une partie du vol est conçu pour se dérouler en orbite à la manière des satellites.  2, record 8, French, - avion%20orbital

Record number: 8, Textual support number: 1 CONT

Enfin un avion orbital monoétage doté d'un moteur combiné, le statoréacteur (réacteur à double flux) assurant la poussée jusqu'à 35000 mètres, le propulseur de fusée fournissant l'énergie nécessaire à la mise en orbite.  2, record 8, French, - avion%20orbital

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  French

Record 9,  Textual support,  Spanish