TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

The attitude and orbit control system(AOCS) is the spacecraft subsystem responsible for determining and controlling the vehicle's orbit and orientation.  5, record 1, English, - attitude%20and%20orbit%20control%20system

Record number: 1, Textual support number: 1 OBS

attitude and orbit control system; AOCS: designations officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  6, record 1, English, - attitude%20and%20orbit%20control%20system

Record number: 1, Textual support number: 2 OBS

attitude and orbital control system; AOCS: designations standardized by NATO.  6, record 1, English, - attitude%20and%20orbit%20control%20system

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

Ensemble d'équipements et de logiciels de bord qui assure les fonctions de pilotage et de guidage d'un engin spatial en vue de lui imposer l'orientation voulue et d'ajuster son orbite aux exigences de la mission.  1, record 1, French, - syst%C3%A8me%20de%20commande%20d%27orientation%20et%20d%27orbite

Record number: 1, Textual support number: 1 OBS

système de commande d'orientation et d'orbite : désignations publiées au Journal officiel de la République française le 25 juillet 2015.  6, record 1, French, - syst%C3%A8me%20de%20commande%20d%27orientation%20et%20d%27orbite

Record number: 1, Textual support number: 2 OBS

système de commande d'attitude et d'orbite; SCAO : désignations uniformisées par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  6, record 1, French, - syst%C3%A8me%20de%20commande%20d%27orientation%20et%20d%27orbite

Record number: 1, Textual support number: 3 OBS

système de commande de l'attitude et de commande en orbite; AOCS : désignations normalisées par l'OTAN.  6, record 1, French, - syst%C3%A8me%20de%20commande%20d%27orientation%20et%20d%27orbite

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

[The] attitude control subsystem(ACS) has yaw, roll, and pitch sensors that enable the attitude control processor(ACP) to maintain altitude accurately.  2, record 2, English, - attitude%20control%20processor

Record 2,  Textual support,  French

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

The RADARSAT-2 spacecraft control subsystem(SCS) provides spacecraft activity planning and scheduling, real-time spacecraft commanding, health and safety monitoring, telemetry archiving, and orbit determination, prediction, and maneuver planning.  2, record 3, English, - real%2Dtime%20spacecraft%20commanding

Record number: 3, Textual support number: 1 OBS

real-time spacecraft commanding: term officially approved by the RADARSAT-2 Terminology Approval Group (ROAG).  3, record 3, English, - real%2Dtime%20spacecraft%20commanding

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

Le sous-système de contrôle de RADARSAT-2 (SCS) assure la planification et la programmation des activités à bord du satellite de même que la commande en temps réel, le suivi de l'état de santé et de la sécurité, l'archivage de la télémétrie, la détermination et la prévision de l'orbite et la planification des manœuvres du satellite.  2, record 3, French, - commande%20en%20temps%20r%C3%A9el%20du%20satellite

Record number: 3, Textual support number: 2 OBS

commande en temps réel du satellite : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  1, record 3, French, - commande%20en%20temps%20r%C3%A9el%20du%20satellite

Record 3,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

Aircraft refuelling and defuelling is controlled by a separate subsystem within the overall fuel system. The aircraft is fuelled by means of a refuelling receptacle that connects to the refuelling tanker. From the receptacle it enters a refuelling gallery which distributes the incoming fuel to the various aircraft tanks. The control of fuel entry into each tank is undertaken by valves that are under the control of the fuel management system.  1, record 5, English, - aircraft%20refuelling

Record number: 5, Textual support number: 2 CONT

The airport ground refueling system supplies fuel to the aircraft at high enough flows and pressures to allow refueling of the aircraft in a short period of time. Aircraft refueling is performed prior to almost every flight whereas defueling is primarily performed during maintenance actions.  2, record 5, English, - aircraft%20refuelling

Record 5,  Textual support,  French

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 DEF

The subsystem within automatic train control that provides fail-safe protection against collisions, excessive speed, and other hazardous conditions.  2, record 6, English, - automatic%20train%20protection

Record 6,  Textual support,  French

Record 6,  Textual support,  Spanish

Record number: 6, Textual support number: 1 OBS

ATP: según su sigla en inglés (automatic train protection).  2, record 6, Spanish, - protecci%C3%B3n%20autom%C3%A1tica%20de%20trenes

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 DEF

A subsystem that contains its own reference monitor for resources under its control, but depends on other controls and on the base operating system for the control of subjects and the more primitive system objects.  2, record 7, English, - secure%20subsystem

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

Comparer «système sûr» et «système sécurisé».  1, record 7, French, - sous%2Dsyst%C3%A8me%20s%C3%A9curis%C3%A9

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The ranging subsystem determines the slant range from the ground control station to the satellite for precise transfer and geostationary orbit determination.  2, record 8, English, - ranging%20subsystem

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 CONT

Le rôle du sous-système mesure de distance est de fournir une mesure de la distance sol-satellite pour permettre la localisation du satellite.  2, record 8, French, - sous%2Dsyst%C3%A8me%20mesure%20de%20distance

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

... the attitude control subsystem provides beacon tracking signal for precise pointing of the antenna toward the earth coverage areas...  2, record 9, English, - beacon%20tracking%20signal

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

D'autre part, le satellite émet en permanence des signaux balises (beacons, Baken) qui permettent le pointage et la poursuite exactes par les stations terriennes.  2, record 9, French, - signaux%2Dbalises

Record 9,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

Over 20 nations protect their sovereign airspace with command, control and communication systems produced by Hughes Aircraft Company, the world's most experienced developer of automated air defense systems. The systems are comprised of air defense radars, computers, displays and other electronic subsystem.  1, record 13, English, - command%2C%20control%20and%20communication%20system

Record number: 13, Textual support number: 1 OBS

command, control and communications system; C3 system: terms extracted from the "Disarmament and Peace Keeping" glossary with the permission of the United Nations Office at Geneva.  3, record 13, English, - command%2C%20control%20and%20communication%20system

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 OBS

système de commandement, de contrôle et de communications; système C3 : termes tirés du lexique «Désarmement et Maintien de la Paix» avec l'autorisation de l'Office des Nations Unies à Genève.  2, record 13, French, - syst%C3%A8me%20de%20commandement%2C%20de%20contr%C3%B4le%20et%20de%20communications

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 CONT

The major objective of this contract is to design a monopropellant propulsion system, which is a mission critical subsystem of the satellite Guidance and Navigation Control System.  2, record 14, English, - critical%20subsystem

Record 14,  Textual support,  French

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 CONT

The flight director subsystem converts guidance errors into pilot control cues or autopilot commands.  1, record 15, English, - flight%20director%20subsystem

Record 15,  Textual support,  French

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

Many spacecraft use small rockets called thrusters to move around in space. Thrusters can change the speed and direction of a spacecraft. They allow a spacecraft to steer in space, to jump to a higher orbit, or to fall back to Earth.  4, record 16, English, - thruster

Record number: 16, Textual support number: 2 CONT

The control rocket is a vernier or other rocket used to control the attitude of, or slightly change the speed of, a spacecraft.  5, record 16, English, - thruster

Record number: 16, Textual support number: 3 CONT

The propulsion subsystem featured sets of small thrusters and a main engine. The thrusters were used to perform Odyssey's attitude control and trajectory correction manoeuvres, while the main engine was used to place the spacecraft in orbit around Mars. The main engine, which used hydrazine propellant with nitrogen tetroxide as an oxidiser, produced a minimum thrust of 65. 3 kilograms of force. Each of the four thrusters used for attitude control produce a thrust of 0. 1 kilogram of force. Four 2. 3-kilogram-force thrusters were used for turning the spacecraft. In addition to miscellaneous tubing, pyro valves and filters, the propulsion subsystem also included a single gaseous helium tank used to pressurise the fuel and oxidiser tanks. The propulsion subsystem weighed 49. 7 kilograms.  4, record 16, English, - thruster

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 DEF

Moteur-fusée de très petite poussée.  4, record 16, French, - micropropulseur

Record number: 16, Textual support number: 1 CONT

Des micropulseurs télécommandés développent des impulsions radiales axiales qui corrigent l'attitude ou la position du satellite sur son orbite.  2, record 16, French, - micropropulseur

Record number: 16, Textual support number: 1 OBS

On prévoit dans de nombreux satellites de petits propulseurs [...] dont les emplacements sont fixes.  5, record 16, French, - micropropulseur

Record number: 16, Textual support number: 2 OBS

Micropropulseur télécommandé.  6, record 16, French, - micropropulseur

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 CONT

The RADARSAT-2 satellite ... consists of a Bus Module and a Payload Module [...] The RADARSAT-2 bus consists of elements that provide general support functions such as ... thermal control ...  2, record 17, English, - thermal%20control

Record number: 17, Textual support number: 1 OBS

The thermal control subsystem is a key system on which the successful performance of the spacecraft ultimately depends. Electronics equipment must operate within a relatively narrow temperature band if proper functioning is to be achieved and thermal failure avoided. This operating temperature range must be maintained in a vehicle that will be exposed to extreme temperature gradients. Heat generated internally must also be managed. Typically, satellites will spin to keep any part of the surface from getting too hot or cold.  3, record 17, English, - thermal%20control

Record number: 17, Textual support number: 2 OBS

thermal control: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 17, English, - thermal%20control

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 DEF

Ensemble des techniques passives et actives permettant de maintenir les différentes parties d'un engin spatial dans des gammes spécifiées de température.  3, record 17, French, - thermor%C3%A9gulation

Record number: 17, Textual support number: 1 CONT

Le satellite RADARSAT-2 est constitué d'une plate-forme et d'une charge utile. [...] La plate-forme est composée d'éléments qui assurent les fonctions générales de servitude du satellite telles [...] la thermorégulation [...]  4, record 17, French, - thermor%C3%A9gulation

Record number: 17, Textual support number: 1 OBS

Le sous-système de thermorégulation est un système essentiel dont dépend au bout du compte la performance du vaisseau spatial. L'équipement électronique doit fonctionner dans une gamme de températures relativement étroites pour obtenir de bons résultats et pour éviter les pannes. Cette fourchette de températures doit être conservée dans un véhicule qui sera exposé à des variations extrêmes de température. Il faut aussi gérer la température produite à l'intérieur du véhicule. De façon traditionnelle, les satellites tournent sur eux-mêmes pour éviter qu'une partie quelconque de leur surface ne devienne trop chaude ou trop froide.  5, record 17, French, - thermor%C3%A9gulation

Record number: 17, Textual support number: 2 OBS

thermorégulation : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  6, record 17, French, - thermor%C3%A9gulation

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 CONT

The spacecraft bus for RADARSAT-2... SAR payload... Thermal Subsystem : In its sun-synchronous orbit, one side of RADARSAT-2 is usually exposed to continuous sunlight. Between the left-and right-looking imaging mode, different areas of the SAR antenna are exposed to varying intensities of sunlight. Thermal control is required to reflect or dissipate the heat of the Sun on the spacecraft body and SAR antenna, as well as to dissipate the heat that is generated internally by the satellite's electronics.  1, record 18, English, - thermal%20subsystem

Record number: 18, Textual support number: 1 OBS

thermal subsystem: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  2, record 18, English, - thermal%20subsystem

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 OBS

Le système de régulation thermique sert à réfléchir ou à dissiper la chaleur du Soleil sur le corps du satellite et sur l'antenne SAR. Ce système est également utilisé pour dissiper la chaleur qui se dégage de l'équipement électronique à l'intérieur du satellite.  1, record 18, French, - syst%C3%A8me%20thermique%20auxiliaire

Record number: 18, Textual support number: 2 OBS

système thermique auxiliaire : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  1, record 18, French, - syst%C3%A8me%20thermique%20auxiliaire

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, Textual support number: 1 CONT

Three Axis Magnetometer [-] TAM... Redundant TAMs are provided to sense the local strength and direction of the Earth's magnetic field. Each TAM consists of a sensor and a separately packaged electronics unit. The analog outputs provided by the TAM allow for sensing magnetic field data in three orthogonal axes. TAM-Operation Once the TAM is powered there will be no ground interactions necessary. The TAM data is used by the FSW ACS [Flight Software Attitude Control Subsystem routine to determine the local magnetic field when reaction wheel momentum unloading is deemed necessary via the magnetic torque rods [Landsat].  3, record 19, English, - three%20axis%20magnetometer

Record number: 19, Textual support number: 1 OBS

three axis magnetometer; CAM: term and abbreviation officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 19, English, - three%20axis%20magnetometer

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 CONT

On peut mesurer ainsi l'intensité d'un champ magnétique axial. Certains magnétomètres plus sophistiqués peuvent mesurer un champ global selon ses 3 axes x, y et z. On parle alors de magnétomètre triaxial.  2, record 19, French, - magn%C3%A9tom%C3%A8tre%20triaxial

Record number: 19, Textual support number: 1 OBS

magnétomètre triaxial : terme uniformisé par le Groupe de travail de la terminologie de Radarsat-2 (GTTR0).  3, record 19, French, - magn%C3%A9tom%C3%A8tre%20triaxial

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, Textual support number: 1 OBS

The Kinetic Energy Anti-Satellite(KE-ASAT) program is intended to provide the United States with the capability to neutralize hostile satellites. The objective of the KE-ASAT program is to define, develop, integrate and test the necessary Kill Vehicle(KV), weapon control subsystem component and subsystems technologies to demonstrate hit-to-kill performance, including debris mitigation against hostile satellites.  3, record 20, English, - Kinetic%20Energy%20Anti%2DSatellite

Record 20,  Textual support,  French

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  English

Record number: 21, Textual support number: 1 CONT

There are three key components of a hypothetical particle beam weapon system. First, there is the source of the beam-the beam generator-consisting of a particle accelerator and its associated supply of electrical power, energy storage, and conditioning. Second, there is a beam control subsystem to aim the beam at the target and determine that the beam has hit. Last, the particle beam weapon must have a fire control subsystem which acquires all the targets that need to be engaged, selects the one to engage, and tells the beam control subsystem where to look to find it.  2, record 21, English, - particle%20beam%20weapon%20system

Record 21,  Textual support,  French

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 DEF

The part of the job entry subsystem that provides centralized storage and retrieval of : 1) system input and output data for each job, 2) control tables representing jobs, thus forming a queue of work, and 3) job tables used during job execution.  2, record 22, English, - job%20entry%20central%20services

Record 22,  Textual support,  French

Record 22,  Textual support,  Spanish

Record number: 22, Textual support number: 1 DEF

Parte del subsistema de entrada de trabajos que proporciona un almacenamiento centralizado y la recuperación de: (a) entradas del sistema y salidas de datos para cada trabajo; (b) tablas de control representando los trabajos, formándose así una cola o fila de espera de trabajos, y (c) tablas de trabajos utilizadas durante la ejecución individual del trabajo.  1, record 22, Spanish, - servicios%20centrales%20de%20entrada%20de%20trabajos

Record 23,  Textual support,  English

Record number: 23, Textual support number: 1 OBS

ACCS is a subsystem of the Financial Management System(FMS) dedicated to the function of Commitment Control in the Supply Revolving Fund and the Operating Expenditures Vote. It provides control requirements for management, and support to the Responsibility Centre Managers, in the form of reports and on-line enquiries.  1, record 23, English, - Allotment%20Commitment%20Control%20System

Record 23,  Textual support,  French

Record 23,  Textual support,  Spanish

Record 24,  Textual support,  English

Record number: 24, Textual support number: 1 CONT

Pressurized Mating Adaptor(PMA) 3 will provide a place for an orbiter to dock with the U. S. segment of the International Space Station(ISS). PMA-3 includes mechanical interfaces, spacewalk hardware and thermal control equipment, electrical power subsystem(EPS) and command and data handling(C&DH) passthroughs. PMA-3 will not be used for docking until Mission 4A.  5, record 24, English, - pressurized%20mating%20adapter%2D3

Record number: 24, Textual support number: 2 CONT

The PMA-3 is a truncated conical shell with a 24-inch axial offset in the diameters between the end rings. It is a ring-stiffened shell structure machined from 2219 aluminum alloy roll ring forgings welded together. PMA-3 mechanical interfaces include a passive common berthing mechanism and a Russian APAS [Androgynous Docking Adapter - Russian acronym].  5, record 24, English, - pressurized%20mating%20adapter%2D3

Record number: 24, Textual support number: 1 OBS

pressurized mating adapter-3; PMA-3: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  6, record 24, English, - pressurized%20mating%20adapter%2D3

Record 24,  Textual support,  French

Record number: 24, Textual support number: 1 CONT

[...] deux astronautes devraient entreprendre une sortie extravéhiculaire d'une durée de six heures et demie visant à fixer un nouveau port d'amarrage (l'adapteur pressurisé-3) et à préparer l'élément de structure Z1 [pour y installer] les immenses panneaux solaires qui seront livrés à la station à la fin du mois de novembre. La première tâche que devront effectuer Wisoff et Lopez-Alegria sera de dégager les verrous qui maintiennent le PMA-3 en place et fournir à Wakata, aux commandes du bras robotique, des indications visuelles pour qu'il puisse extraire lentement le PMA-3 de sa plate-forme de soutien située dans la soute de Discovery. Au moment où Wakata déplacera le PMA-3 vers son nouvel emplacement sur le module Unity, Wisoff et Lopez-Alegria dégageront les verrous du dispositif de fixation situés sur la partie supérieure de la structure Z1 et prépareront les points d'ancrage pour l'installation des immenses panneaux solaires [...]  3, record 24, French, - adaptateur%20pressuris%C3%A9%203

Record number: 24, Textual support number: 1 OBS

adaptateur pressurisé 3; PMA 3 : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  5, record 24, French, - adaptateur%20pressuris%C3%A9%203

Record 24,  Textual support,  Spanish

Record 25,  Textual support,  English

Record number: 25, Textual support number: 1 CONT

Propulsion Module. The ATV [Automatic Transfer Vehicle] Space Craft itself includes the propulsion bay accommodating the Propulsion and Reboost Subsystem. This bi-propellant system comprises : four main engines of 490 N each with a specific impulse of more than 310 s each twenty attitude control thrusters of 220 N each and a minimum impulse bit MIP) of less than 5 Ns. The system uses mixed oxides of nitrogen as oxidiser. Fuel and oxidiser are stored in eight identical 1 m-diameter titanium tanks. The same tanks are used for ATV propulsion and International Space Station reboost.  2, record 25, English, - propulsion%20module

Record number: 25, Textual support number: 1 OBS

propulsion module: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 25, English, - propulsion%20module

Record 25,  Textual support,  French

Record number: 25, Textual support number: 1 CONT

L'ATV [Automatic Transfer Vehicle] n'est que le prolongement de l'étage supérieur d'une Ariane 5. Il se présente donc sous la forme d'un cylindre de 5,45 mètres de diamètre sur 2,5 mètres de longueur. Il est équipé en standard d'un module de propulsion composé de huit petits moteurs à réaction et d'un module d'avionique qui intègre les réservoirs d'ergols, les circuits électroniques ainsi que les systèmes de régularisation thermique, de production d'énergie et de télécommunications.  3, record 25, French, - module%20de%20propulsion

Record number: 25, Textual support number: 2 CONT

Trois configurations de base sont prévues pour l'ATV [Automatic Transfer Vehicle]. Il peut notamment recevoir une mini-module logistique pressurisé (MPLM), une coque porteuse et deux palettes logistiques non pressurisées (ULC), ou un module pressurisé en plus d'une structure porte-réservoir ouverte.  4, record 25, French, - module%20de%20propulsion

Record number: 25, Textual support number: 1 OBS

module de propulsion : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et le Comité d'uniformisation de la terminologie spatiale (CUTS).  5, record 25, French, - module%20de%20propulsion

Record 25,  Textual support,  Spanish

Record 26,  Textual support,  English

Record number: 26, Textual support number: 1 CONT

The Attitude Control Subsystem(ACS) design is based on the Viking Lander approach updated with state-of-the-art components.  3, record 26, English, - attitude%20control%20sub%2Dsystem

Record 26,  Textual support,  French

Record number: 26, Textual support number: 1 OBS

Tous les organismes, à l'exception de l'ESA, utilisent le terme attitude au lieu d'orientation.  2, record 26, French, - sous%2Dsyst%C3%A8me%20de%20commande%20d%27orientation

Record 26,  Textual support,  Spanish

Record 27,  Textual support,  English

Record number: 27, Textual support number: 1 CONT

The Attitude Measurement Electronics uses inputs from the spacecraft Sun Sensors, Attitude and Orbit Control Electronics(AOCE) and ground commands to provide the spacecraft subsystems with refined Sun pulse information, and to control the position of the fuel regulation valves and heaters in the Reaction Control Subsystem. It also takes power from the AOCS power converters and provides power switching for other units within the AOCS.  2, record 27, English, - attitude%20measurement%20electronics

Record 27,  Textual support,  French

Record 27,  Textual support,  Spanish

Record 28,  Textual support,  English

Record number: 28, Textual support number: 1 OBS

RCA is developing a Shuttle Compatible Orbital Transfer Subsystem(SCOTS) for delivering communications satellites in a transfer orbit from the Space Shuttle parking orbit. SCOTS includes guidance and control equipment, a solid-rocket motor, and a reusable cradle assembly in the shuttle cargo bay. Separation from the bay is accomplished by a simple spring mechanism to eject the spacecraft into a nonspinning, free-float mode.  1, record 28, English, - Shuttle%20Compatible%20Orbital%20Transfer%20Subsystem

Record 28,  Textual support,  French

Record 28,  Textual support,  Spanish

Record 29,  Textual support,  English

Record number: 29, Textual support number: 1 CONT

TSA(Test & Simulation Assembly). Test station for MACS [Modular Attitude Control System]-based AOCS [Attitude and Orbit Control Subsystem] includes :... software models of spacecraft dynamics, AOCS sensors and AOCS actuators; interpreter for test control language; facilities for sending telecommands and receiving telemetry; tool for displaying simulation data; tool for post processing of test data.  2, record 29, English, - test%20%26%20simulation%20assembly

Record 29,  Textual support,  French

Record 29,  Textual support,  Spanish

Record 30,  Textual support,  English

Record number: 30, Textual support number: 1 CONT

The European Robotic Arm(ERA) will be attached to the Russian segment of the International Space Station.... The Manipulator Joint Subsystem... includes [a] high-precision joint position sensor to feed the joint position to the joint control electronics...  3, record 30, English, - joint%20control%20electronics

Record number: 30, Textual support number: 1 OBS

joint control electronics; JCE: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 30, English, - joint%20control%20electronics

Record 30,  Textual support,  French

Record number: 30, Textual support number: 1 OBS

circuit électronique de commande d'articulation; JCE : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 30, French, - circuit%20%C3%A9lectronique%20de%20commande%20d%27articulation

Record 30,  Textual support,  Spanish

Record 31,  Textual support,  English

Record number: 31, Textual support number: 1 CONT

Using the DPA, the crew gives commands to each experiment or subsystem via a Remote Acquisition Unit(RAU). Signals passing through the RAU are routed through one of two ’data busses. ’One data bus handles experiment data while the other handles information on the status of Spacelab subsystems. The data are then processed by the computers for display, transmission, or storage as directed by a crew member operating a keyboard at the control center rack.  2, record 31, English, - remote%20acquisition%20unit

Record 31,  Textual support,  French

Record 31,  Textual support,  Spanish

Record 32,  Textual support,  English

Record number: 32, Textual support number: 1 CONT

The design of the Magellan spacecraft was driven by the need for a low-cost, high-performance vehicle. Some of the Magellan spacecraft components were already in existence or at least designed. Protoflight spacecraft were available from storage at no cost. These include the 3. 7 meter diameter, high-gain antenna(HGA), the spacecraft bus, propulsion system components, thermal control louvers, and much of the radio subsystem.  2, record 32, English, - protoflight%20spacecraft

Record 32,  Textual support,  French

Record 32,  Textual support,  Spanish

Record 33,  Textual support,  English

Record number: 33, Textual support number: 1 OBS

The satellite Attitude Determination and Control Subsystem(ADCS) is used to maintain proper satellite attitude and satellite pointing states. The subsystem also provides real-time information on attitude and orbit.  1, record 33, English, - Attitude%20Determination%20and%20Control%20Subsystem

Record 33,  Textual support,  French

Record 33,  Textual support,  Spanish

Record 34,  Textual support,  English

Record number: 34, Textual support number: 1 CONT

The Rack Interface Controller(RIC), Payload Internet Hub/Bridge(PIHB), and EXPRESS Memory Unit(EMU) connects the racks with the Station's Internet and video services. These units also control the EXPRESS Rack subsystem operations, allowing computer and video control from either on Station or the ground. The RIC coordinates and routes command and control functions, the PIHB provides the necessary interfaces, and the EMU has 320 MB of memory to store rack software and application programs and to help transfer files between payloads and the PIHB.  2, record 34, English, - EXPRESS%20memory%20unit

Record number: 34, Textual support number: 1 OBS

EXPRESS memory unit; EMU: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 34, English, - EXPRESS%20memory%20unit

Record 34,  Textual support,  French

Record number: 34, Textual support number: 1 OBS

unité de mémoire EXPRESS; EMU : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 34, French, - unit%C3%A9%20de%20m%C3%A9moire%20EXPRESS

Record 34,  Textual support,  Spanish

Record 35,  Textual support,  English

Record number: 35, 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 35, English, - extendible%20support%20structure

Record number: 35, Textual support number: 1 OBS

extendible support structure; ESS: term and abbreviation officially approved by the RADARSAT-2 official approval Group (ROAG).  5, record 35, English, - extendible%20support%20structure

Record 35,  Textual support,  French

Record number: 35, 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 35, French, - structure%20porteuse%20d%C3%A9pliable

Record number: 35, 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 35, French, - structure%20porteuse%20d%C3%A9pliable

Record 35,  Textual support,  Spanish

Record 36,  Textual support,  English

Record number: 36, Textual support number: 1 CONT

An external Ultra High Frequency(UHF) antenna... will be attached to the station's U. S. laboratory Destiny... The antenna, on a four-foot boom, is part of the UHF Communications Subsystem of the station. It will interact with systems already aboard the ISS [International Space Station], including the Space-to-Space Station Radio(SSSR) transceivers. A second antenna will be delivered on STS-115/11A next year. Once in operation the UHF subsystem will be used for space-to-space communication(voice, commands and telemetry for the space station). It can support up to five users on the same frequency and provides : Two-way voice communications between the station and space walkers, the station and orbiter and between the Mission Control Center in Houston and space walkers(using the UHF with the S-band subsystem).  3, record 36, English, - ultra%20high%20frequency%20antenna

Record number: 36, Textual support number: 1 OBS

ultra high frequency antenna: term officially approved by the International Space Station official approval Group (ISSOAG).  4, record 36, English, - ultra%20high%20frequency%20antenna

Record 36,  Textual support,  French

Record number: 36, Textual support number: 1 CONT

[Une] antenne à ondes décimétriques (UHF) [permettra] d'améliorer les communications entre la navette et la Station, lors des sorties extravéhiculaires.  3, record 36, French, - antenne%20%C3%A0%20ondes%20d%C3%A9cim%C3%A9triques

Record number: 36, Textual support number: 2 CONT

[...] une antenne à ondes décimétriques [est installée] sur la paroi extérieure de Destiny.  4, record 36, French, - antenne%20%C3%A0%20ondes%20d%C3%A9cim%C3%A9triques

Record number: 36, Textual support number: 1 OBS

antenne à ondes décimétriques : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  5, record 36, French, - antenne%20%C3%A0%20ondes%20d%C3%A9cim%C3%A9triques

Record 36,  Textual support,  Spanish

Record 37,  Textual support,  English

Record number: 37, Textual support number: 1 CONT

The Integrated Equipment Assembly measures 16 x 16 x 16 feet, weighs nearly 17, 000 pounds and is designed to condition and store the electrical power collected by the photovoltaic arrays for use on board the Station. The IEA integrates the energy storage subsystem, the electrical equipment, the thermal control system, structural framework and the Solar Array Rotary Joint(SARJ). The IEA consist of three major elements : 1. The power system electronics... [;] 2. The Photovoltaic Thermal Control System... [;] 3. The computers used to control the P6 module.  3, record 37, English, - integrated%20equipment%20assembly

Record number: 37, Textual support number: 1 OBS

integrated equipment assembly; IEA: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 37, English, - integrated%20equipment%20assembly

Record 37,  Textual support,  French

Record number: 37, Textual support number: 1 OBS

ensemble intégré d'équipements; IEA : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 37, French, - ensemble%20int%C3%A9gr%C3%A9%20d%27%C3%A9quipements

Record 37,  Textual support,  Spanish

Record 38,  Textual support,  English

Record number: 38, Textual support number: 1 CONT

The on-orbit Attitude Determination and Control Subsystem(ADACS) provides three axis pointing control for the satellite. The ADACS maintains system pointing by controlling torque in three mutually orthogonal wheels. The torque is determined by analysis of spacecraft orientation in space. Input to these computations are acquired from the Earth Sensor Assembly(ESA) for pitch and roll, and an inertial reference with sun sensor updates for yaw.  2, record 38, English, - inertial%20reference

Record 38,  Textual support,  French

Record number: 38, Textual support number: 1 CONT

Ce chapitre concerne l'étude fine d'un gyroscope [...], monté à 3 degrés de liberté [...] grâce à 2 armatures de Cardan. L'appareil est «le passager» d'une plate-forme stabilisée [...], d'orientation fixe dans un repère inertiel. I Description du montage : 1°) La plate-forme : [...] est un solide [...], emporté dans un véhicule (avion, sous marin, lanceur etc...), et conservant une orientation fixe par rapport à un repère inertiel. Ce qui ne veut pas dire que [la plate-forme stabilisée] est en translation uniforme, simplement en translation quelconque, avec accélération et vitesse.  3, record 38, French, - r%C3%A9f%C3%A9rence%20inertielle

Record number: 38, Textual support number: 2 CONT

Équipement de navigation. Ce type d'équipement guide l'aéronef vers son lieu de destination et intègre de nombreux produits tels que les systèmes de positionnement mondial [(...] GPS), la centrale anémobarométrique, qui calcule la vitesse aérodynamique, l'altitude et la vitesse verticale de l'appareil, les IRS («Inertial Reference System» - systèmes de référence inertielle) - qui sont les principaux capteurs de mouvement et de navigation de la cellule utilisés par un nombre très élevé de systèmes avioniques [...]  4, record 38, French, - r%C3%A9f%C3%A9rence%20inertielle

Record 38,  Textual support,  Spanish

Record 39,  Textual support,  English

Record number: 39, Textual support number: 1 CONT

The VG400CA is a high performance, solid-state vertical gyro intended for airborne applications such as UAV control, avionics, and platform stabilization. This high reliability, strap-down inertial subsystem provides attitude measurement with static and dynamic accuracy comparable to traditional spinning mass vertical gyros.  1, record 39, English, - spinning%20mass%20vertical%20gyro

Record 39,  Textual support,  French

Record number: 39, Textual support number: 1 OBS

[...] les systèmes inertiels se composent d'un minimum de deux gyroscopes, chacun desquels supporte une masse globulaire placée à l'intérieur d'un cardan. [...] Nous savons [...] que l'axe de l'objet qui tourne présente une verticale parfaite. S'il y a inclinaison de la plate-forme, comme par exemple lors d'un virage sur l'aile, le cardan s'incline en tandem avec l'avion tandis que la masse tournante demeure à la verticale. On peut dès lors mesurer l'angle d'inclinaison.  2, record 39, French, - gyroscope%20de%20verticale%20%C3%A0%20masse%20tournante

Record number: 39, Textual support number: 2 OBS

Sur certains gyroscopes perfectionnés, des cercles divisés permettent de relever avec précision la position de la masse rotative, de sorte qu'on peut, avec cet instrument, déterminer la position du plan méridien, celle de l'axe du monde, et par suite, la latitude.  3, record 39, French, - gyroscope%20de%20verticale%20%C3%A0%20masse%20tournante

Record 39,  Textual support,  Spanish

Record 40,  Textual support,  English

Record number: 40, Textual support number: 1 CONT

The VG400CA is a high performance, solid-state vertical gyro intended for airborne applications such as UAV control, avionics, and platform stabilization. This high reliability, strap-down inertial subsystem provides attitude measurement with static and dynamic accuracy comparable to traditional spinning mass vertical gyros.  1, record 40, English, - solid%2Dstate%20vertical%20gyro

Record number: 40, Textual support number: 1 OBS

solid state technology: A general term for sensors that do not have moving parts.  2, record 40, English, - solid%2Dstate%20vertical%20gyro

Record number: 40, Textual support number: 2 OBS

solid state: Pertaining to a circuit, device, or system that depends on some combination of electrical, magnetic, and optical phenomena within a solid that is usually a crystalline semiconductor material.  3, record 40, English, - solid%2Dstate%20vertical%20gyro

Record 40,  Textual support,  French

Record number: 40, Textual support number: 1 OBS

Les gyroscopes vibrants représentent aujourd'hui une nouvelle et importante technologie inertielle, non seulement parce que, pour certains d'entre eux, ils on montré leur capacité à être très performants (on dit alors qu'ils sont de classe inertielle), mais que, surtout, dans les autres technologies dites «solid-state» [semiconducteurs] (gyroscopes laser et à fibre optique), les gyroscopes n'ont pas la même aptitude que les gyroscopes vibrants à être miniaturisés et fabriqués à des coûts faibles.  2, record 40, French, - gyroscope%20de%20verticale%20%C3%A0%20semi%2Dconducteur

Record 40,  Textual support,  Spanish

Record 41,  Textual support,  English

Record number: 41, Textual support number: 1 CONT

The Extravehicular Mobility Unit(EMU) consists of an integrated Space Suit Assembly(SSA) and Life Support Subsystem(LSS) with other crew items designed for Extravehicular Activity(EVA) outside the shuttle Space Transportation System(STS) orbiter or ISS. The NASA EMU provides life support functions, such as oxygen supply, carbon dioxide removal, a pressurized enclosure, temperature control and micrometeoroid protection, so astronauts can leave their shirtsleeve environment and work effectively in space.  4, record 41, English, - extravehicular%20mobility%20unit

Record number: 41, Textual support number: 1 OBS

Although the term space suit is sometimes used to designate the "extravehicular mobility unit" [EMU], "space suit" is, in fact, synonymous with "space suit assembly" which is a component of the EMU.  3, record 41, English, - extravehicular%20mobility%20unit

Record number: 41, Textual support number: 2 OBS

extravehicular mobility unit; EMU: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 41, English, - extravehicular%20mobility%20unit

Record 41,  Textual support,  French

Record number: 41, Textual support number: 1 CONT

La combinaison qui protège les astronautes lors de leurs sorties dans l'espace compte parmi les plus importantes et plus complexes pièces d'équipement à leur disposition. Elle est en fait un mini-vaisseau spatial, capable de fournir tout ce qui est nécessaire à la vie et à la sécurité des astronautes pendant qu'ils travaillent dans le vide spatial. Connue officiellement sous le nom de scaphandre EMU (pour Extravehicular Mobility Unit), la combinaison est constituée de deux composantes principales : la combinaison spatiale comme telle (SSA, pour Space Suit Assembly) et le système de survie de base (PLSS pour Primary Life Support System).  4, record 41, French, - combinaison%20EMU

Record number: 41, Textual support number: 1 OBS

Dans l'usage, les termes «combinaison spatiale» et «scaphandre spatial» sont souvent utilisés pour désigner à la fois un générique, le «extravehicular mobility unit (EMU)» et un spécifique, le «space suit assembly», qui est une composante de l'EMU. Pour solutionner ce problème, lorsque l'on veut désigner l'EMU, il convient de spécifier «combinaison EMU» ou «scaphandre EMU».  3, record 41, French, - combinaison%20EMU

Record number: 41, Textual support number: 2 OBS

combinaison EMU : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  3, record 41, French, - combinaison%20EMU

Record 41,  Textual support,  Spanish

Record 42,  Textual support,  English

Record number: 42, Textual support number: 1 CONT

The Environmental Control Subsystem(ECS) enables pressurization of the cabin and space suits, controls the temperature of electronic equipment, and provides breathable oxygen for the astronauts. It also provides water for drinking, cooling, fire extinguishing, and food preparation and supplies oxygen and water to the portable life support system(PLSS).  2, record 42, English, - environmental%20control%20sub%2Dsystem

Record 42,  Textual support,  French

Record 42,  Textual support,  Spanish

Record 43,  Textual support,  English

Record number: 43, Textual support number: 1 DEF

In process control, the analog data channel between the connector and the analog-to-digital converter in the analog input subsystem.  1, record 43, English, - analog%20input%20channel

Record number: 43, Textual support number: 1 OBS

This channel may include a filter, an analog signal multiplexer, and one or more amplifiers.  1, record 43, English, - analog%20input%20channel

Record number: 43, Textual support number: 2 OBS

analog input channel: term and definition reproduced with the permission of the copyright holder, the Canadian Standards Association (CSA), 178 Rexdale Blvd., Toronto, Ontario Canada M9W 1R3. However, CSA shall not be responsible for the manner in which the information is presented, nor for any interpretations thereof. This CSA material may not have been updated to reflect amendments subsequently made to the original content. For further information, contact CSA.  2, record 43, English, - analog%20input%20channel

Record 43,  Textual support,  French

Record number: 43, Textual support number: 1 DEF

En commande de processus, voie de données analogiques établie entre le connecteur et le convertisseur analogique-numérique employés dans un sous-système d'entrée analogique.  1, record 43, French, - voie%20d%27entr%C3%A9e%20analogique

Record number: 43, Textual support number: 1 OBS

Cette voie peut comporter un filtre, un multiplexeur de signaux analogiques et un ou plusieurs amplificateurs.  1, record 43, French, - voie%20d%27entr%C3%A9e%20analogique

Record number: 43, Textual support number: 2 OBS

voie d'entrée analogique : terme et définition reproduits avec l'autorisation de l'Association canadienne de normalisation (CSA), 178, boul. Rexdale, Toronto (Ontario), Canada M9W 1R3 (détentrice des droits d'auteur). La CSA décline toute responsabilité quant à la façon dont la matière est présentée et quant à toute interprétation pouvant en découler. L'information reproduite pourrait ne pas être à jour. Pour plus de renseignements, communiquer avec la CSA.  2, record 43, French, - voie%20d%27entr%C3%A9e%20analogique

Record 43,  Textual support,  Spanish

Record 44,  Textual support,  English

Record number: 44, Textual support number: 1 OBS

Control to open a door.  2, record 44, English, - entry%20control

Record number: 44, Textual support number: 1 CONT

Figure 8. Array of security subsystems and subsystem elements which comprise an integrated system : entry control, etc.  3, record 44, English, - entry%20control

Record 44,  Textual support,  French

Record 44,  Textual support,  Spanish

Record 45,  Textual support,  English

Record number: 45, Textual support number: 1 CONT

The array of security subsystems and subsystem elements which comprise an integrated system are depicted in Figure 8 : duress sensors, entry control, etc.  1, record 45, English, - duress%20sensor

Record 45,  Textual support,  French

Record 45,  Textual support,  Spanish

Record 46,  Textual support,  English

Record number: 46, Textual support number: 1 CONT

The control distribution matrix(extreme left cabinet) [which is a part of the distribution and supervisory subsystem seen in the ICS3 installation on HMS Invincible] contains a number of press-button switches which allow any user to be rapidly connected to any radio circuit.  1, record 46, English, - control%20distribution%20matrix

Record 46,  Textual support,  French

Record 46,  Textual support,  Spanish

Record 47,  Textual support,  English

Record number: 47, Textual support number: 1 CONT

Sperry Flight Systems, of Phoenix, Ariz., is responsible for providing the cockpit control and display subsystem...  1, record 47, English, - control%20and%20display%20subsystem

Record 47,  Textual support,  French

Record 47,  Textual support,  Spanish

Record 48,  Textual support,  English

Record number: 48, Textual support number: 1 OBS

Routing and Control Devices : Routing circuits include the networks or busses that direct the flow of information between the other functional parts of the hardware subsystem....  2, record 48, English, - routing%20switch

Record 48,  Textual support,  French

Record number: 48, Textual support number: 1 OBS

Dans un circuit électronique.  2, record 48, French, - s%C3%A9lecteur%20d%27acheminement

Record 48,  Textual support,  Spanish

Record 49,  Textual support,  English

Record number: 49, Textual support number: 1 CONT

The Tornado AFDS is a digital integrated subsystem that allows the automatic control of the aircraft in all three flight axes. It also provides the pilot with information on instruments and displays. So the pilot can manually guide the aircraft using the flight director mode or can monitor the automatic flight.  1, record 49, English, - autopilot%20and%20flight%20director%20system

Record number: 49, Textual support number: 1 OBS

Paper read by J. Stocker, Messerschmitt, at the "45th Agard Avionics Symposium", Ottawa, 1983.  4, record 49, English, - autopilot%20and%20flight%20director%20system

Record number: 49, Textual support number: 2 OBS

APFDS (L-1011).  5, record 49, English, - autopilot%20and%20flight%20director%20system

Record 49,  Textual support,  French

Record number: 49, Textual support number: 1 OBS

Terme et abréviations uniformisés par le CUTA Opérations aériennes.  2, record 49, French, - pilote%20automatique%2Fdirecteur%20de%20vol

Record 49,  Textual support,  Spanish

Record 50,  Textual support,  English

Record number: 50, Textual support number: 1 CONT

second, there is a beam control subsystem to aim the beam at the target and determine that the beam has hit the target.  1, record 50, English, - beam%20control%20subsystem

Record 50,  Textual support,  French

Record 50,  Textual support,  Spanish