TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

The Solid State Power Control Module(SSPCM) delivers 120 volts DC [Direct Current] from the Station to the racks and converts it to 28 volts DC, and delivers that power to a three-outlet power strip for use by the payloads. The SSPCM sends 120 volts DC to the RIC [Rack Interface Controller], the AAA [Avionics Air Assembly], and the PEHB [Payload Ethernet Hub/Bridge]. The SSPCM also provides data interfaces for payloads, including analog(two for each middeck locker and one for each ISIS [International Subrack Interface Standard] drawer) and bidirectional discrete(three for each middeck locker and two for each ISIS drawer).  2, record 1, English, - solid%20state%20power%20control%20module

Record number: 1, Textual support number: 1 OBS

solid state power control module; SSPCM: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 1, English, - solid%20state%20power%20control%20module

Record number: 1, Textual support number: 2 OBS

International Space Station official approval Group (ISSOAG): Later known as the International Space Station Terminology Approval Group (ISSTAG).  4, record 1, English, - solid%20state%20power%20control%20module

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 OBS

module de commande d'alimentation à semi-conducteur; SSPCM : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 1, French, - module%20de%20commande%20d%27alimentation%20%C3%A0%20semi%2Dconducteur

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

At selected locations in the U. S. Lab(9 ISPRs-International Standard Payload Racks) and the [Japanese Experiment Module-JEM](5 ISPRs), a low-temperature water loop(0. 6-10 °C or 33-50 °F) is provided via a 1. 3 cm(0. 5 in.) line with a quick-disconnect. The maximum return temperature on this loop is 21 °C(70 °F). A pressure drop of 40 kPa(5. 8 psid) is allowed across the inlet and outlet of both water loop interfaces. Payloads can also dissipate small amounts of heat into the cabin air. Depending on the temperature conditions set by the crew, a minimum of 500 W can be dissipated into both the U. S. Lab and Columbus(complement of all payloads within the module). Negotiations are underway with Japan on the allowable heat dissipation into the JEM.  2, record 2, English, - low%2Dtemperature%20water%20loop

Record number: 2, Textual support number: 1 OBS

low-temperature water loop: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 2, English, - low%2Dtemperature%20water%20loop

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 CONT

La boucle de régulation thermique (autonome à bord) permet d'avoir une très bonne stabilité des températures des équipements de la charge-utile [...]  1, record 2, French, - boucle%20de%20r%C3%A9gulation%20thermique

Record number: 2, Textual support number: 1 OBS

boucle de régulation thermique : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 2, French, - boucle%20de%20r%C3%A9gulation%20thermique

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Thermal Management.... At selected locations in the U. S. Lab(9 ISPRs-[International Standard Payload Racks]) and the JEM-[Japanese Experiment Module](5 ISPRs), a low-temperature water loop(0. 6 to-10 °C or 33 to-50 °F) is provided via a 1. 3 cm(0. 5 in.) line with a quick-disconnect. The maximum return temperature on this loop is 21 °C(70 °F). A pressure drop of 40 kPa(5. 8 psid) is allowed across the inlet and outlet of both water loop interfaces.  2, record 3, English, - water%20loop%20interface

Record number: 3, Textual support number: 1 OBS

water loop interface: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 3, English, - water%20loop%20interface

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

interface de boucle fluide : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 3, French, - interface%20de%20la%20boucle%20fluide

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The Minus Eighty Degrees Celsius Laboratory Freezer for ISS [International Space Station](MELFI) is a fully integrated rack facility, hosted in an ISPR [International Standard Payload Rack], to condition, freeze and store life sciences and biological samples aboard the Space Station. MELFI will also be used to transport frozen specimens to/from the Station flying fully powered inside the Mini-Pressurised Logistic Module aboard the Space Shuttle.... MELFI characteristics :[a] Volume : 300 litres total in 4 independent dewars(minimum configuration 1 dewar at-80 °C; 2-4 dewars in combinations of 3 modes : below-68 °C,-37 °C to-23 °C, +0. 5 °C to +6 °C; [b] Temperatures maintained for 8 hours without power Sample storage : cell culture 1-10 ml, fluids(blood, media, etc.) 1-500 ml, tissue 2-10 ml, whole specimens 10-500 ml Cooling time(from +23 °C to-68 °C) : 2 ml 18-25 min; 10 ml 44-56 min; 500 ml 460 min.  2, record 4, English, - minus%20eighty%20degrees%20celsius%20laboratory%20freezer

Record number: 4, Textual support number: 1 OBS

minus eighty degrees celsius laboratory freezer; MELFI: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  6, record 4, English, - minus%20eighty%20degrees%20celsius%20laboratory%20freezer

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

MELFI [Minus Eighty degree celsius Laboratory Freezer for ISS] est un congélateur/réfrigérateur destiné à la Station spatiale internationale et plus particulièrement aux modules américains (USLab) et japonais (Japanese Experiment Module : JEM). MELFI permet le refroidissement et le stockage d'une large variété d'échantillons (de 2 à 1000 ml) issus des différentes expériences de science de la vie menées à bord de l'ISS [International Space Station]. Le volume de stockage des échantillons est de 300 litres répartis en quatre enceintes froides (dewars) pouvant fonctionner indépendamment et à trois niveaux de température différents (+4 °C, -26 °C et -80 °C). La production de froid est assurée par une machine cryogénique fonctionnant selon le cycle thermodynamique de Brayton [...] Un circuit d'azote permet d'assurer la distribution du froid vers les enceintes froides.  5, record 4, French, - cong%C3%A9lateur%20de%20laboratoire%20%C3%A0%20%2D80%20%C2%B0C

Record number: 4, Textual support number: 1 OBS

congélateur de laboratoire à -80 °C; congélateur MELFI; MELFI : termes et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  6, record 4, French, - cong%C3%A9lateur%20de%20laboratoire%20%C3%A0%20%2D80%20%C2%B0C

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

A permanently attached multipurpose laboratory module, located so as to contain the optimum microgravity environment of the [International] Space Station payload accommodations, with complete basic functional outfitting, including accommodations for international standard payload racks and provisions for storage of NASA spares and secondary storage of crew provisions.  3, record 5, English, - multipurpose%20laboratory%20module

Record 5,  Textual support,  French

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

A hosted payload is a module attached to a commercial satellite with communications circuitry that operates independently of the main spacecraft but which shares the satellite's power supply and transponders.  2, record 6, English, - hosted%20payload

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 DEF

Charge utile embarquée sur un satellite hôte, dont la mission est indépendante de celle de ce satellite hôte.  1, record 6, French, - charge%20utile%20h%C3%A9berg%C3%A9e

Record number: 6, Textual support number: 1 OBS

La charge utile hébergée bénéficie de l'accès à l'orbite du satellite hôte qui lui fournit en outre les services nécessaires à son fonctionnement.  1, record 6, French, - charge%20utile%20h%C3%A9berg%C3%A9e

Record number: 6, Textual support number: 2 OBS

charge utile hébergée : terme, définition et observation publiés au Journal officiel de la République française le 28 juin 2017.  2, record 6, French, - charge%20utile%20h%C3%A9berg%C3%A9e

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

... each JEM-EF [Japanese experiment module-exposed facility] payload must have a space shuttle-compatible grapple fixture to allow handling of the payload by the JEM remote manipulator system(JEM-RMS), a robotic arm system used for the transport and positioning of external user payloads. The JEM-RMS has both a main arm and a fine arm for robotics manipulation and is operated by the crew from within the JEM-PM [JEM pressurized module] with the aid of a viewing port.  7, record 7, English, - Japanese%20experiment%20module%20remote%20manipulator%20system

Record number: 7, Textual support number: 1 OBS

Japanese robotic arm system; JEM remote manipulator system; JEM-RMS: terms and abbreviation officially approved by the International Space Station Terminology Approval Group (ISSTAG).  8, record 7, English, - Japanese%20experiment%20module%20remote%20manipulator%20system

Record 7,  Textual support,  French

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

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, record 8, English, - StratSat%C2%AE

Record number: 8, Textual support number: 1 OBS

StratSat® is a registered trademark.  8, record 8, English, - StratSat%C2%AE

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 CONT

[...] 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, record 8, French, - StratSat%C2%AE

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

Although ATV [Automated Transfer Vehicle] will dock to the Russian Zvezda module, it will carry most of its dry payload for the US elements of the ISS [International Space Station]. At the launch site in Kourou, French Guiana, six weeks before flight, Jules Verne will be loaded with 1 300 kg of dry cargo out of the 5 500 kg maximum capacity. Most of the dry cargo provided by NASA will be clothes, food, towels and wipes for the crew, logistics items such as batteries and spare parts for maintenance of the Station. This cargo will also include ESA [European Space Agency] experiments such as ANITA, which will constantly monitor the cabin air, and some Russian hardware to be added to the panels of the Station's Russian Service Module.  2, record 9, English, - dry%20cargo

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

Au total, l'ATV [véhicule de transfert automatique] a livré 9,357 kg de charge dont 6,019 kg de cargo et 3,556 kg d'ergols. Dans le cargo, il y a 1,150 kg de charge sèche (vêtements, nourriture, équipements, etc.), 269 kg d'eau, 21 kg d'oxygène, 861 kg d'ergols pour la Station et 302 kg d'ergols pour la rehausse de la Station.  2, record 9, French, - charge%20s%C3%A8che

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 CONT

The Laser Retro Reflector(LRR), mounted on the owner's side of the payload module, reflects the laser beams directed to the satellite back to the tracking station. The two-way travel time is a measure for the distance between the satellite and the tracking station. Tracking information from various sites throughout the world provides the essential information for computing the ERS [European Remote Sensing Satellite] orbits.  3, record 10, English, - lasar%20retro%20reflector

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 CONT

[Le] réflecteur laser LRR (Laser Retro-Reflector) [est un] instrument passif [qui] permet de déterminer précisément l'orbite du satellite grâce à des tirs laser à partir de stations terrestres. (ESA, réalisé par Alcatel Space à Cannes)  1, record 10, French, - r%C3%A9flecteur%20laser%20LRR

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 DEF

Any equipment or cargo carried by a spacecraft or launch vehicle or mounted on an orbiting space platform or space station.  2, record 11, English, - payload

Record number: 11, Textual support number: 1 OBS

In terms of the mass budget, the term payload also includes the crew of a manned spacecraft. For unmanned spacecraft, the term is used to differentiate between equipment concerned directly with the spacecraft's application(the payload) and that which supports the operation of that payload(the subsystems contained within the service module).  2, record 11, English, - payload

Record number: 11, Textual support number: 2 OBS

payload: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  3, record 11, English, - payload

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 DEF

Élément ou ensemble d'éléments que peut transporter un véhicule spatial et qui est destiné à remplir une mission déterminée.  2, record 11, French, - charge%20utile

Record number: 11, Textual support number: 1 OBS

La notion de charge utile varie selon les points de vue; ainsi ce terme peut s'appliquer à un satellite par rapport au lanceur qui le porte, ou bien au bloc expérimental embarqué sur un satellite par rapport à ce satellite. Dans un engin spatial d'observation ou de sondage, la charge utile comporte généralement plusieurs instruments.  2, record 11, French, - charge%20utile

Record number: 11, Textual support number: 2 OBS

D'un point de vue budgétaire, la charge utile comprend l'équipage d'un véhicule spatial habité. Lorsqu'il s'agit d'un véhicule non habité, le terme désigne alors l'ensemble des équipements nécessaires au fonctionnement du véhicule et de la charge utile elle-même, c'est-à-dire les sous-systèmes du module de service.  3, record 11, French, - charge%20utile

Record number: 11, Textual support number: 3 OBS

charge utile : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR) et par le Comité d'uniformisation de la terminologie spatiale (CUTS).  3, record 11, French, - charge%20utile

Record number: 11, Textual support number: 1 PHR

Charge utile en bande S.  3, record 11, French, - charge%20utile

Record 11,  Textual support,  Spanish

Record number: 11, Textual support number: 1 OBS

De un satélite.  2, record 11, Spanish, - carga%20%C3%BAtil

Record 12,  Textual support,  English

Record number: 12, 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 12, English, - thermal%20control

Record number: 12, 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 12, English, - thermal%20control

Record number: 12, Textual support number: 2 OBS

thermal control: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 12, English, - thermal%20control

Record 12,  Textual support,  French

Record number: 12, 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 12, French, - thermor%C3%A9gulation

Record number: 12, 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 12, French, - thermor%C3%A9gulation

Record number: 12, 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 12, French, - thermor%C3%A9gulation

Record number: 12, Textual support number: 2 OBS

thermorégulation : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  6, record 12, French, - thermor%C3%A9gulation

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 CONT

[...] en effet ces deux soliccites se sont égarés, leur lancement ayant raté en raison du mauvais fonctionnement du moteur d'appoint PAM (module d'assistance pour charge utile).  1, record 13, French, - module%20d%27assistance%20pour%20charge%20utile

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 DEF

[A module] on which [a satellite's] instruments and payload support equipments are accommodated.  2, record 14, English, - payload%20module

Record number: 14, Textual support number: 1 CONT

The Payload Module consisted of the Payload Electronics Module(PEM) and the Antenna Support Structure(ASS).  3, record 14, English, - payload%20module

Record number: 14, Textual support number: 1 OBS

payload module : term officially approved by the RADARSAT-2 Terminology Approval Group(RTAG).  4, record 14, English, - payload%20module

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 DEF

[Module] qui transporte les sous-systèmes d'appui dédiés aux instruments et à la charge utile.  2, record 14, French, - module%20de%20charge%20utile

Record number: 14, Textual support number: 1 CONT

Le module de charge utile présente la même définition structurelle que la plate-forme. Il est conçu afin d'assurer le découplage thermique de la plate-forme et du module.  4, record 14, French, - module%20de%20charge%20utile

Record number: 14, Textual support number: 1 OBS

module de charge utile : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  5, record 14, French, - module%20de%20charge%20utile

Record 14,  Textual support,  Spanish

Record number: 14, Textual support number: 1 CONT

El módulo de carga útil es aquel en que están instalados los instrumentos que justifican la misión espacial. Algunos de ellos son muy sofisticados: podemos encontrar desde cámaras hasta telescopios, pasando por detectores sensibles a fenómenos atmosféricos, antenas y amplificadores para comunicaciones, entre otros.  1, record 14, Spanish, - m%C3%B3dulo%20de%20carga%20%C3%BAtil

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 DEF

[An antenna] equipped with distributed transmit/receive modules which provide distinct transmit and receive beams.  4, record 15, English, - active%2Dphased%20array%20antenna

Record number: 15, Textual support number: 1 CONT

The most significant difference between RADARSAT-2 and RADARSAT-1 payload technology is that RADARSAT-2 uses a fully-active phased array antenna, rather than the passive slotted waveguide antenna used by RADARSAT-1. Fully-active phased arrays offer a number of very significant benefits over passive antenna, but they also add great complexity.... The phased array is made up of 512 individual radiating elements, organized into 16 columns(picture below shows a single column) along the 15-metre antenna length, each with 32 rows across the 1. 5-metre width. The phase shifters and amplitude control are built into the Transmit/Receive(T/R) modules, which feed the radiating elements. Each column has a computer that controls the 32 T/R module settings and these 16 computers are all linked to another computer(in the spacecraft bus) that orchestrates the overall antenna behaviour.  5, record 15, English, - active%2Dphased%20array%20antenna

Record number: 15, Textual support number: 1 OBS

active array antenna: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  6, record 15, English, - active%2Dphased%20array%20antenna

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 DEF

Antenne composée de plusieurs éléments rayonnants, installée à bord d'un satellite et destinée à la transmission et à la réception des données.  4, record 15, French, - antenne%2Dr%C3%A9seau%20active

Record number: 15, Textual support number: 1 CONT

Le radar à synthèse d'ouverture [de RADARSAT-2] comprend un système électronique sophistiqué qui alimente une antenne active à réseau d'éléments en phase qui consiste en 512 modules de transmission-réception (TRM) avec des réseaux de distribution de puissance et fréquences radio.  3, record 15, French, - antenne%2Dr%C3%A9seau%20active

Record number: 15, Textual support number: 1 OBS

antenne-réseau active : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  5, record 15, French, - antenne%2Dr%C3%A9seau%20active

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

The Electrical Power Subsystem [RADARSAT-2] is responsible for generating, storing, and regulating electrical power for the satellite. Power is generated from the two solar array wings, each consisting of three panels. The solar panels are designed to generate 2400 watts at end-of-life. Power is stored on-board in a Nickel-Hydrogen battery.  3, record 16, English, - electrical%20power%20subsystem

Record number: 16, Textual support number: 1 OBS

The spacecraft is comprised of three major sub-systems : the bus module, the payload module, and the extendible support structure.  4, record 16, English, - electrical%20power%20subsystem

Record number: 16, Textual support number: 2 OBS

electrical power subsystem; EPS: term and abbreviation officially approved by the RADARSAT-2 Official Approval Group (ROAG).  5, record 16, English, - electrical%20power%20subsystem

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 CONT

Sous-système électrique de satellite.  3, record 16, French, - sous%2Dsyst%C3%A8me%20%C3%A9lectrique

Record number: 16, Textual support number: 1 OBS

Le circuit électrique [de RADARSAT-2] sert à la génération, au stockage et à la régulation électrique du satellite. Ce circuit comporte deux ailes solaires constituées chacune de trois panneaux capables de générer en tout temps 2400 watts d'électricité. À bord du satellite, l'énergie est emmagasinée dans une pile nickel-hydrogène.  2, record 16, French, - sous%2Dsyst%C3%A8me%20%C3%A9lectrique

Record number: 16, Textual support number: 2 OBS

sous-système électrique; EPS : terme et abréviation uniformisés par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 16, French, - sous%2Dsyst%C3%A8me%20%C3%A9lectrique

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 CONT

When it is completed, the K-1 will be the first commercially available, fully reusable launch vehicle to provide low-cost access to space for low earth-orbiting satellites. The K-1 is powered by modified Russian rocket engines, provided by Aerojet, that burn LOX (liquid oxygen) and kerosene. Thrust is produced when the appropriate mixture of LOX and kerosene is pumped into the combustion chamber and ignited.  6, record 17, English, - K%2D1%20reusable%20launch%20vehicle

Record number: 17, Textual support number: 2 CONT

The K-1 will be able to deliver approximately 3, 200 kg(7, 000 lbm) of pressurized cargo to the ISS and return approximately 900 kg(2, 000 lbm) of recoverable downmass. The K-1 cargo module can accommodate a volume of 30 m³(1, 000 ft³) equivalent to five International Standard Payload Racks. The K-1 is also capable of providing up to 40km(25 nmi) reboost and attitude control for ISS, an important feature for maintaining the ISS orbit, and conducting on-orbit technology demonstration as precursor risk reduction missions.  4, record 17, English, - K%2D1%20reusable%20launch%20vehicle

Record number: 17, Textual support number: 1 PHR

K-1 is equipped with an active dispenser.  7, record 17, English, - K%2D1%20reusable%20launch%20vehicle

Record number: 17, Textual support number: 2 PHR

K1 fully reusable, two-stage.  7, record 17, English, - K%2D1%20reusable%20launch%20vehicle

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 CONT

Le premier vaisseau spatial entièrement réutilisable sera l'engin K-1 de la Société Kistler Aerospace. Il devrait voler à la fin de 1999. Cette fusée à deux étages utilise des moteurs russes qui fonctionnent au kérosène et à l'oxygène liquide. Les étages séparés retourneront sur Terre par parachute.  2, record 17, French, - lanceur%20r%C3%A9cup%C3%A9rable%20K%2D1

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 DEF

Pressurized module carried in space in the Space Shuttle payload bay that is used to transport materials and supplies.  4, record 18, English, - mini%20pressurized%20logistics%20module

Record number: 18, Textual support number: 1 CONT

When the International Space Station(ISS) was redesigned again in 1993, NASA & the Italian Space Agency decided to expand the original Mini-Pressurized Logistics Module design. The new MultiPurpose Logistics Module is twice as long and an carry up to 9000 kg of cargo to ISS.... The module carries up to sixteen refrigerator-sized(203 x 105cm) payload racks, five of which may contain refrigerators/freezers. Other so-called "EXPRESS Racks" can be outfitted with lockers for small experiments. Additional cargo can be carried in center aisle stowage containers.  5, record 18, English, - mini%20pressurized%20logistics%20module

Record number: 18, Textual support number: 1 OBS

mini pressurized logistics module; MPLM: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  6, record 18, English, - mini%20pressurized%20logistics%20module

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 CONT

La boîte à gants [...] devrait être lancée dans le mini-module logistique pressurisé en mai 2002.  4, record 18, French, - minimodule%20logistique%20pressuris%C3%A9

Record number: 18, Textual support number: 1 OBS

minimodule logistique pressurisé; MPLM : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  5, record 18, French, - minimodule%20logistique%20pressuris%C3%A9

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, 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 :... power generation and storage...  1, record 19, English, - power%20generation%20and%20storage

Record number: 19, Textual support number: 1 OBS

power generation and storage: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  2, record 19, English, - power%20generation%20and%20storage

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 CONT

Le satellite RADARSAT-2 est constitué d'une plateforme et d'une charge utile. [...] La plateforme est composée d'éléments qui assurent les fonctions générales de servitude du satellite telles [...] la génération et le stockage de l'énergie [...]  1, record 19, French, - g%C3%A9n%C3%A9ration%20et%20stockage%20de%20l%27%C3%A9nergie

Record number: 19, Textual support number: 1 OBS

génération et stockage de l'énergie : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 19, French, - g%C3%A9n%C3%A9ration%20et%20stockage%20de%20l%27%C3%A9nergie

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, Textual support number: 1 CONT

The Leonardo Multipurpose Logistics Module, which was built by the Italian Space Agency (ASI), is the first of three such pressurized modules that will serve as the International Space Station’s "moving vans," carrying laboratory racks filled with equipment, experiments and supplies to and from the Station aboard the Space Shuttle. The unpiloted, reusable logistics modules function as both a cargo carrier and a Space Station module when they are flown. Mounted in the Space Shuttle’s cargo bay for launch and landing, they are berthed to the Station using the shuttle’s robotic arm after the shuttle has docked. While berthed to the Station, racks of equipment are unloaded from the module and then old racks and equipment may be reloaded to be taken back to Earth. The logistics module is then detached from the Station and positioned back into the Shuttle’s cargo bay for the trip home. When in the cargo bay, the cargo module is independent of the Shuttle cabin, and there is no passageway for Shuttle crewmembers to travel from the Shuttle cabin to the module. In order to function as an attached Station module as well as a cargo transport, the logistics modules also include components that provide some life support, fire detection and suppression, electrical distribution and computer functions. Eventually, the modules also will carry refrigerator freezers for transporting experiment samples and food to and from the station.  4, record 20, English, - multi%2Dpurpose%20logistics%20module

Record number: 20, Textual support number: 2 CONT

When the International Space Station(ISS) was redesigned again in 1993, NASA & the Italian Space Agency decided to expand the original Mini-Pressurized Logistics Module design. The new MultiPurpose Logistics Module is twice as long and an carry up to 9000kg of cargo to ISS.... The module carries up to sixteen refrigerator-sized(203 x 105cm) payload racks, five of which may contain refrigerators/freezers. Other so-called "EXPRESS Racks" can be outfitted with lockers for small experiments. Additional cargo can be carried in center aisle stowage containers.  5, record 20, English, - multi%2Dpurpose%20logistics%20module

Record number: 20, Textual support number: 1 OBS

multi-purpose logistics module; MPLM: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  6, record 20, English, - multi%2Dpurpose%20logistics%20module

Record 20,  Textual support,  French

Record number: 20, Textual support number: 1 CONT

Le MPLM [Multi-Purpose Logistics Module] est un module pressurisé doté d'un système de soutien-vie interne sophistiqué, à l'intérieur duquel les astronautes peuvent travailler. Il est le seul module pouvant livrer à la Station des expériences dans leurs bâtis spéciaux venant s'intégrer aux laboratoires de l'ISS [International Space Station]. Il sert aussi de «fourgonnette» à l'aller comme au retour, transportant d'autres équipements et fournitures, et reste attaché à la Station pendant son déchargement et son chargement.  6, record 20, French, - module%20logistique%20italien

Record number: 20, Textual support number: 2 CONT

L'Italian Multi-Purpose Laboratory Modules (MPLMs) est un élément construit sur le modèle du COF [Colombus Orbital Facility] européen et abritera l6 emplacements normalisés aptes à recevoir des charges italiennes, européennes ou américaines.  7, record 20, French, - module%20logistique%20italien

Record number: 20, Textual support number: 1 OBS

module logistique italien; MPLM : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  8, record 20, French, - module%20logistique%20italien

Record number: 20, Textual support number: 1 PHR

Module logistique polyvalent Donatello, Raffaello.  8, record 20, French, - module%20logistique%20italien

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  English

Record number: 21, Textual support number: 1 CONT

The Columbus External Payload Facility(CEPF) is a set of structures added to the starboard end-cone of the Columbus module intended to carry four payload adapters mechanically similar to those used in the NASA ExPRESS Pallet(ExP) programme [RD 2]. Unlike the ExP, the CEPF provides one adapter location that normally points to notional zenith, one oriented to notional nadir, and two to starboard.  2, record 21, English, - Columbus%20external%20payload%20facility

Record number: 21, Textual support number: 1 OBS

In summary, the CEPF provides suitable interfaces for a small sized remote sensing instrument, either internally pointed/stabilised, or tolerating large excursions around a nominal direction. Large fields of view can be accommodated. The ground track pattern is not optimised for localised studies, nor repeatable on the long term due to altitude variations.  2, record 21, English, - Columbus%20external%20payload%20facility

Record number: 21, Textual support number: 2 OBS

Columbus external payload facility; CEPF: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 21, English, - Columbus%20external%20payload%20facility

Record 21,  Textual support,  French

Record number: 21, Textual support number: 1 OBS

Dans la perspective d'une telle évolution future, il [cône arrière] pourrait aussi recevoir divers points d'accrochage nécessaires au raccordement d'une plate-forme de charge utile extérieure.  2, record 21, French, - plateforme%20de%20charge%20utile%20ext%C3%A9rieure%20de%20Columbus

Record number: 21, Textual support number: 2 OBS

plateforme de charge utile extérieure de Columbus; CEPF : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 21, French, - plateforme%20de%20charge%20utile%20ext%C3%A9rieure%20de%20Columbus

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 CONT

An Exposed Payload Facility is planned for Columbus. It will consist of two separate support structures attached to the Columbus Pressurized Module end cone in the zenith and nadir positions.  3, record 22, English, - exposed%20payload%20facility

Record number: 22, Textual support number: 2 CONT

The principal new feature for an exposed payload facility is the presence of a single, multi-purpose robotic servicing capability. Whilst providing a substantial amount of operational flexibility, this feature requires that careful consideration be given to accommodation aspects.  4, record 22, English, - exposed%20payload%20facility

Record number: 22, Textual support number: 1 OBS

exposed payload facility; EPF: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  5, record 22, English, - exposed%20payload%20facility

Record number: 22, Textual support number: 1 PHR

COF Exposed Payload Facility (EPF).  2, record 22, English, - exposed%20payload%20facility

Record 22,  Textual support,  French

Record number: 22, Textual support number: 1 CONT

Le cône arrière [du COF] est prévu pour recevoir optionnellement sa propre antenne de liaison et un équipement de télécommunications autonome avec le sol via le système de relais de données européen DRS [...] il pourrait aussi recevoir divers points d'accrochage nécessaires au raccordement d'une plate-forme de charge utile extérieure.  4, record 22, French, - plateforme%20de%20charge%20utile%20ext%C3%A9rieure

Record number: 22, Textual support number: 1 OBS

plate-forme de charge utile extérieure; EPF : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  3, record 22, French, - plateforme%20de%20charge%20utile%20ext%C3%A9rieure

Record 22,  Textual support,  Spanish

Record 23,  Textual support,  English

Record number: 23, Textual support number: 1 CONT

... The Progress supply vehicle to the ISS [International Space Station] is an automated version of the Soyuz, and was developed to carry propellant and cargo to the Salyut and Mir space station. It will serve the same purpose for the ISS. Although the ISS has its own propulsion system, generally it is the Progress vehicle that will perform periodic reboost maneuvers to maintain the ISS orbital altitude. The Progress is approximately the same size as the Soyuz, but it has a slightly higher mass at launch of approximately 7150 kg. The Progress spacecraft docks automatically to the ISS, and the TORU [Teleoperated Control System-Manual Docking System on Zarya] system acts as a backup remote control docking system. Progress is composed of three modules : the Cargo Module, the Refueling Module, and the Instrument/Propulsion Module. A modified version of the Progress M, called the Progress M1, is planned for operation with the ISS. This version will have more propellant tanks for refueling, as the entire Refueling Module is devoted to fuel. Water will be carried in the Cargo Module. The Progress payload includes cargo in the pressurized Cargo Module and propellant in the Refueling Module. Excess propellant that is usually in the propulsion system tanks in the Instrumentation/Propulsion Module can also be used by the ISS.  10, record 23, English, - Progress%20supply%20vehicle

Record number: 23, Textual support number: 1 OBS

Progress supply vehicle; Progress cargo ship; Progress cargo craft; Progress resupply ship: terms officially approved by the International Space Station official approval Group (ISSOAG).  12, record 23, English, - Progress%20supply%20vehicle

Record number: 23, Textual support number: 1 PHR

Progress M1-3 cargo spacecraft, M-44 craft.  12, record 23, English, - Progress%20supply%20vehicle

Record 23,  Textual support,  French

Record number: 23, Textual support number: 1 CONT

La station sera ravitaillée par un premier Progress M1. Ce vaisseau automatique [...] apportera principalement les tonnes de carburant nécessaires pour maintenir l'altitude et l'orientation de la station.  9, record 23, French, - vaisseau%2Dcargo%20Progress

Record number: 23, Textual support number: 1 OBS

vaisseau-cargo Progress; vaisseau de ravitaillement Progress; vaisseau Progress : termes uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  8, record 23, French, - vaisseau%2Dcargo%20Progress

Record number: 23, Textual support number: 1 PHR

Vaisseau-cargo Progress-M.  8, record 23, French, - vaisseau%2Dcargo%20Progress

Record number: 23, Textual support number: 2 PHR

Vaisseau-cargo Progress non habité.  8, record 23, French, - vaisseau%2Dcargo%20Progress

Record 23,  Textual support,  Spanish

Record 24,  Textual support,  English

Record number: 24, Textual support number: 1 CONT

The COF Element is a multi-purpose cylindrical pressurised laboratory with an Earth-like atmosphere, permanently attached to the ISS. It has a capacity for 10 international standard payload racks(5 of which are allocated for use by other International Partners) with the facilities to be used primarily for the materials science, fluid physics and compatible life science disciplines. The COF also has external attachment points providing resources for Space Science, Earth Observation and Technology disciplines. The COF... will be attached to the "front-end" of the ISS at Node 2. The primary structure is based on the Italian Space Agency's Mini Payload Logistics Module(MPLM) primary structure and is 6. 7 m long by 4. 46 m diameter.  7, record 24, English, - Columbus%20orbital%20facility

Record number: 24, Textual support number: 1 OBS

The steady-state operations of the COF systems and the European Payloads located within the COF will be supported by a number of organisations, teams and ground segment facilities both in Europe and the US ... Each facility is interconnected with the ESA provided IGS (Interconnect Ground Subnet). This wide area network will be implemented around a hub in Europe, with relays at the major points of data entry (MCC-H, PDSS) and nodes at each of the sites in Europe involved in COF operations. It will be based on a combination of leased lines and a public service provided ATM Virtual Private Network (VPN).  7, record 24, English, - Columbus%20orbital%20facility

Record number: 24, Textual support number: 2 OBS

Columbus orbital facility; COF: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  8, record 24, English, - Columbus%20orbital%20facility

Record 24,  Textual support,  French

Record number: 24, Textual support number: 1 CONT

Le COF se présente physiquement sous la forme d'un cylindre accusant 9500 kg au lancement, mesurant 6,7 mètres sur 4,5 mètres. Raccordé au point de branchement numéro 2 (node 2), il en recevra sa puissance électrique sous la forme de courant continu à 120 volts et d'autres ressources. Sa consommation pourra aller jusqu'à 13,5 kW. Vu de l'extérieur, le COF est une coque pressurisée cylindrique munie de deux cônes d'extrémité, ainsi que de tourillons servant au transport et à la manutention du module. Rigidifiée et recouverte de plusieurs couches d'isolant thermique et d'un blindage de protection contre les météorites ainsi que les débris spatiaux de plus en plus nombreux, elle est en outre équipée d'une structure d'accrochage sur la coque extérieure en vue des opérations de manutention et d'assemblage au moyen du bras télémanipulateur de la Station spatiale (SSRMS) pouvant aussi servir à la transmission de signaux électriques et de données au moyen de relais integrés.  11, record 24, French, - module%20laboratoire%20Columbus

Record number: 24, Textual support number: 1 OBS

[...] le laboratoire européen Columbus [est] doté d'un petit bras pour les manipulations extérieures.  12, record 24, French, - module%20laboratoire%20Columbus

Record number: 24, Textual support number: 2 OBS

module laboratoire Columbus; COF : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  13, record 24, French, - module%20laboratoire%20Columbus

Record number: 24, Textual support number: 1 PHR

Coque extérieure du COF.  13, record 24, French, - module%20laboratoire%20Columbus

Record 24,  Textual support,  Spanish

Record 25,  Textual support,  English

Record number: 25, Textual support number: 1 CONT

The Spacehab's Logistics Double Module [LDM] is a 20-foot long, 14-foot wide, 11. 2-foot high pressurized aluminum module carried in Atlantis’ payload bay and connected to the middeck area of the orbiter by an access tunnel. For STS-106, the LDM will carry approximately 8, 100 pounds of hardware, equipment and logistical supplies to outfit the International Space Station. Designed to augment the Shuttle's middeck, the double module has a total cargo capacity of up to 10, 000 pounds and contains the systems necessary to support the crewmembers, such as ventilation, lighting and limited power.  2, record 25, English, - Spacehab%20logistics%20double%20module

Record number: 25, Textual support number: 1 OBS

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

Record 25,  Textual support,  French

Record number: 25, Textual support number: 1 CONT

Le module double SPACEHAB emportant 2223 kg de cargo [...] nouvelles batteries, 4 ventilateurs, 3 extincteurs d'incendie et 10 détecteurs de fumée. Des fournitures en vue de la première occupation permanente de la Station seront aussi incluses dont des effets personnels, équipement médical et d'exercice, équipement de communications et vidéo, ordinateurs et imprimantes, et 4 grands contenants d'eau.  2, record 25, French, - module%20double%20Spacehab

Record number: 25, Textual support number: 1 OBS

SPACEHAB est un large cylindre pressurisé, situé à l'arrière de la soute de la navette, qui sert à ranger l'équipement et qui est accessible à l'équipage une fois en orbite.  3, record 25, French, - module%20double%20Spacehab

Record number: 25, Textual support number: 2 OBS

module double Spacehab : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  4, record 25, French, - module%20double%20Spacehab

Record 25,  Textual support,  Spanish

Record 26,  Textual support,  English

Record number: 26, Textual support number: 1 CONT

[The] EMCS consists of a gas tight incubator containing two centrifuges with space for 4 Experiment Containers on each rotor; also the life support and water supply system, the illumination and the observation system are located on the rotors. External to the incubator are the Standard Payload Computer(SPLC), the gas supply module and the thermal control system. The flight unit is accommodated in an EXPRESS Rack on the International Space Station. Ground controls will be performed in dedicated Experiment Reference Models, one located in Europe, the other at NASA Ames Research Center.  3, record 26, English, - European%20modular%20cultivation%20system

Record number: 26, Textual support number: 2 CONT

[The] EMCS is dedicated to experiments on plants, especially multi-generation (seed-to-seed) experiments and studies on gravity effects on early development and growth, on signal perception and transduction in plant tropisms. Experiments with insects or amphibia as well as studies with cell and tissue cultures are also foreseen in EMCS.  3, record 26, English, - European%20modular%20cultivation%20system

Record number: 26, Textual support number: 1 OBS

European modular cultivation system; EMCS: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 26, English, - European%20modular%20cultivation%20system

Record 26,  Textual support,  French

Record number: 26, Textual support number: 1 CONT

[Le] European Modular Cultivation System (EMCS) [est] destiné à l'étude biologique des plantes (croissance, développement, influence de la microgravité).  2, record 26, French, - module%20europ%C3%A9en%20d%27%C3%A9tude%20biologique%20des%20plantes

Record number: 26, Textual support number: 1 OBS

module européen d'étude biologique des plantes; EMCS : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 26, French, - module%20europ%C3%A9en%20d%27%C3%A9tude%20biologique%20des%20plantes

Record 26,  Textual support,  Spanish

Record 27,  Textual support,  English

Record number: 27, Textual support number: 1 CONT

The payload module is essentially a large cryostat with a toroidal tank which contained at launch, over 2000 litres of super fluid helium.... Some of the infrared detectors are directly coupled to the helium tank and are at a temperature of around 2K. All other units are cooled by means of the cold boil-off gas from the liquid helium.  2, record 27, English, - boil%2Doff%20gas

Record 27,  Textual support,  French

Record 27,  Textual support,  Spanish

Record 28,  Textual support,  English

Record number: 28, Textual support number: 1 CONT

The Rack Level Test Facility is the formal verification tool used for the functional and operational testing of internal payloads. The Rack Level Test Facility will however, be modified to also allow the verification of external payloads and centre-aisle payloads, but this capability does not currently exist. This verification is carried out before installation into the Columbus Laboratory(for the initial internal payload complement), or prior to shipment to the Kennedy Space Centre for installation into the Multi Purpose Logistics Module, for transportation to the ISS.  3, record 28, English, - rack%20level%20test%20facility

Record number: 28, Textual support number: 1 OBS

rack level test facility; RLTF: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 28, English, - rack%20level%20test%20facility

Record 28,  Textual support,  French

Record number: 28, Textual support number: 1 OBS

système d'essai niveau bâtis; RLTF : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 28, French, - syst%C3%A8me%20d%27essai%20niveau%20b%C3%A2tis

Record 28,  Textual support,  Spanish

Record 29,  Textual support,  English

Record number: 29, Textual support number: 1 CONT

Each NASA ISPR provides 1. 6 m³(55. 5ft³) of internal volume. The rack weighs 104 kg(230 lbm) and can accommodate an additional 700 kg(1543 lbm) of payload equipment. The rack has internal mounting provisions to allow attachment of secondary structure. The ISPRs will be outfitted with a thin center post to accommodate sub-rack-sized payloads, such as the 48. 3 cm(19 in) Spacelab Standard Interface Rack(SIR) Drawer or the Space Shuttle Middeck Locker. Utility pass-through ports are located on each side to allow cables to be run between racks. Module attachment points are provided at the top of the rack, and via pivot points at the bottom of the rack. The pivot points support installation and maintenance. Tracks on the exterior front posts allow mounting of payload equipment and laptop computers. Additional adapters on the ISPRs are provided for ground handling.  3, record 29, English, - international%20standard%20payload%20rack

Record number: 29, Textual support number: 1 OBS

international standard payload rack; ISPR: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 29, English, - international%20standard%20payload%20rack

Record number: 29, Textual support number: 1 PHR

ISPR adaptor.  4, record 29, English, - international%20standard%20payload%20rack

Record 29,  Textual support,  French

Record number: 29, Textual support number: 1 CONT

Ces bâtis, qui constituent une évolution technologique majeure, sont dénommés ISPR, pour «International Standard Payload Rack». ... Du fait que les modules européen, américain et japonais utilisent le même concept d'ISPR, les bâtis sont interchangeables entre les laboratoires, à l'exception des laboratoires russes qui n'ont pas adopté ce standard. Le [Columbus Orbital Facility] COF peut recevoir simultanément dix bâtis ISPR de type scientifique comportant divers instruments et expériences ainsi que trois bâtis de stockage d'équipements. La capacité de chaque bâti est de 1,5m³ pour une charge maximale de 700 kg.  5, record 29, French, - b%C3%A2ti%20de%20charge%20utile%20normalis%C3%A9

Record number: 29, Textual support number: 1 OBS

bâti de charge utile normalisé; ISPR : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 29, French, - b%C3%A2ti%20de%20charge%20utile%20normalis%C3%A9

Record number: 29, Textual support number: 1 PHR

Bâti de stockage, de type scientifique.  2, record 29, French, - b%C3%A2ti%20de%20charge%20utile%20normalis%C3%A9

Record number: 29, Textual support number: 2 PHR

Bâti interchangeable.  2, record 29, French, - b%C3%A2ti%20de%20charge%20utile%20normalis%C3%A9

Record 29,  Textual support,  Spanish

Record 30,  Textual support,  English

Record number: 30, Textual support number: 1 CONT

... the JEM-EF provides a total of l2 attachment ports called Exposed Facility Units(EFUs) to which space-exposed hardware may be mated using a standard Payload Interface Unit(PIU).... A total of 10 EFUs are available for User payloads, the other two being allocated to the ELM-ES [Experiment Logistics Module-Exposed Section] which transports payloads to orbit and stores them when they are not active, and the Interorbit Communication System(ICS). Five of the 10 EFUs are available for NASA payloads.  2, record 30, English, - exposed%20facility%20unit

Record number: 30, Textual support number: 2 CONT

The JEM-EF can provide the resources of power, communication and heat rejection capability to the payload via the EEU [Equipment Exchange Unit]. The EEU consists of an Exposed Facility Unit (EFU) and a Payload Interface Unit (PIU). The EFU can connect and disconnect the payload with/from the JEM-EF. The PIU [Payload Interface Unit] should be attached to all JEM-EF experiment payloads.  3, record 30, English, - exposed%20facility%20unit

Record number: 30, Textual support number: 1 OBS

exposed facility unit; EFU: term and abbreviation officially approved by th e International Space Station official approval Group (ISSOAG).  4, record 30, English, - exposed%20facility%20unit

Record 30,  Textual support,  French

Record number: 30, Textual support number: 1 OBS

port de fixation EFU : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 30, French, - port%20de%20fixation%20EFU

Record 30,  Textual support,  Spanish

Record 31,  Textual support,  English

Record number: 31, Textual support number: 1 CONT

The GFE [Government Furnished Equipment] for an ISS [Internation Space Station] Attached Payload for the full-truss site consists of the Payload Support and Interface Module(PSIM) [which] provides interfaces for the science instrument package on the ISS external attach site. [It] is designed and configured to utilize the ISS resources-Starboard Upper Inboard Site : S3[, ] serves as a carrier in the Shuttle cargo-bay during launch and landing, [has an] on-orbit life of 4 years, [is] EVA [Extra-Vehicular Activity] and EVR [Extra-Vehicular Robotics] compatible.  2, record 31, English, - payload%20support%20and%20interface%20module

Record number: 31, Textual support number: 1 OBS

payload support and interface module; PSIM : term and abbreviation officially approved by the International Space Station official approval Group(ISSOAG).  3, record 31, English, - payload%20support%20and%20interface%20module

Record 31,  Textual support,  French

Record number: 31, Textual support number: 1 OBS

module d'interface et de support de charge utile; PSIM : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 31, French, - module%20d%27interface%20et%20de%20support%20de%20charge%20utile

Record 31,  Textual support,  Spanish

Record 32,  Textual support,  English

Record number: 32, Textual support number: 1 CONT

... the JEM-EF [Japanese Experiment Module-Exposed Facility] provides a total of l2 attachment ports called Exposed Facility Units(EFUs) to which space-exposed hardware may be mated using a standard Payload Interface Unit(PIU). It is through the PIU that payloads receive all utilities.  2, record 32, English, - payload%20interface%20unit

Record number: 32, Textual support number: 1 OBS

payload interface unit; PIU: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 32, English, - payload%20interface%20unit

Record 32,  Textual support,  French

Record number: 32, Textual support number: 1 OBS

module d'interface de charge utile; PIU : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 32, French, - module%20d%27interface%20de%20charge%20utile

Record 32,  Textual support,  Spanish

Record 33,  Textual support,  English

Record number: 33, Textual support number: 1 CONT

The JEM-EF [Japanese Experiment Module-Exposed Facility] payload sites can accommodate two mass classes of payloads. Eight sites are limited to 500 Kg. The ram-port site, EFU 9, and the innermost wake site, EFU 2, can both accommodate 2500 Kg. The paylad envelope is 0. 8 m x 1. 0 m x 1. 85 m with the longest dimension radiating from the JEM-EF.  2, record 33, English, - payload%20site

Record number: 33, Textual support number: 1 OBS

payload site: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 33, English, - payload%20site

Record 33,  Textual support,  French

Record number: 33, Textual support number: 1 OBS

emplacement de charge utile : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 33, French, - emplacement%20de%20charge%20utile

Record 33,  Textual support,  Spanish

Record 34,  Textual support,  English

Record number: 34, Textual support number: 1 CONT

An Exposed Payload Facility is planned for Columbus. It will consist of two separate support structures attached to the Columbus pressurized module end cone in the zenith and nadir positions.  3, record 34, English, - end%20cone

Record number: 34, Textual support number: 1 OBS

end cone; end-cone: terms officially approved by the International Space Station official approval Group (ISSOAG).  4, record 34, English, - end%20cone

Record 34,  Textual support,  French

Record number: 34, Textual support number: 1 CONT

Vu de l'extérieur, le COF [Élément orbital européen - Columbus Orbital Facility] est une coque pressurisée cylindrique munie de deux cônes d'extrémité, ainsi que de tourillons servant au transport et à la manutention du module.  3, record 34, French, - c%C3%B4ne%20arri%C3%A8re

Record number: 34, Textual support number: 1 OBS

Le cône arrière est prévu pour recevoir optionnellement sa propre antenne de liaison et un équipement de télécommunications autonome avec le sol via le système de relais de données européen DRS.  3, record 34, French, - c%C3%B4ne%20arri%C3%A8re

Record number: 34, Textual support number: 2 OBS

cône arrière; cône d'extrémité : termes uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  4, record 34, French, - c%C3%B4ne%20arri%C3%A8re

Record 34,  Textual support,  Spanish

Record 35,  Textual support,  English

Record number: 35, Textual support number: 1 CONT

In the ESTEC Battery Test Centre, accelerated Stentor battery module lifetime tests were carried out for CNES, while the Compact Payload Test Range was used for major antenna, EMC and RFC tests, including those for MetOp.  2, record 35, English, - battery%20test%20centre

Record 35,  Textual support,  French

Record number: 35, Textual support number: 1 CONT

À La Rochelle, l'EIGSI (École d'ingénieurs en génie des systèmes industriels) développe des activités de contrôle et d'optimisation des systèmes industriels de production informatique intégrée pour les systèmes de transport et de production... Elle abrite un centre d'essais des batteries et des modules de traction destinés au véhicule électrique lié au projet régional VEDELIC (Véhicule démonstrateur laboratoire Lithium Carbone).  2, record 35, French, - centre%20d%27essais%20des%20batteries

Record 35,  Textual support,  Spanish

Record 36,  Textual support,  English

Record number: 36, Textual support number: 1 CONT

The Fluid Science Laboratory(FSL) is a multi-user research capability to study dynamic phenomena of fluid media in the absence of gravitational forces. FSL occupies one ISPR [International Standard Payload Rack]. For facility users, the most significant FSL element is the Facility Core Element that houses the central experiment module, the optical diagnostics module and the standardised Experiment Containers(ECs).... The FSL can be operated in fully automatic or semi-automatic modes by the flight crew, or in a remote-control mode from the ground(telescience).  3, record 36, English, - fluid%20science%20laboratory

Record number: 36, Textual support number: 1 OBS

fluid science laboratory; FSL: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 36, English, - fluid%20science%20laboratory

Record 36,  Textual support,  French

Record number: 36, Textual support number: 1 CONT

Le «Fluid Science Laboratory» (FSL), équipement modulaire pour l'étude des fluides en microgravité [...], peut être commandé par les astronautes, ou de la Terre, grâce à la téléscience. Ajouté au «Materials Science Laboratory», le [FSL fait] partie du programme «Microgravity Facilities for Columbus» (MFC) de l'ESA.  5, record 36, French, - laboratoire%20sur%20la%20science%20des%20fluides

Record number: 36, Textual support number: 1 OBS

laboratoire sur la science des fluides; FSL : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  4, record 36, French, - laboratoire%20sur%20la%20science%20des%20fluides

Record 36,  Textual support,  Spanish

Record 37,  Textual support,  English

Record number: 37, Textual support number: 1 CONT

GFE [Government Furnished Equipment] for an ISS Attached Payload for the full-truss site consists of the Payload Support and Interface Module(PSIM) and NASA-provided project services.  2, record 37, English, - attached%20payload

Record number: 37, Textual support number: 1 OBS

attached payload: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 37, English, - attached%20payload

Record number: 37, Textual support number: 1 PHR

External attached payload space, individual attached payload.  4, record 37, English, - attached%20payload

Record 37,  Textual support,  French

Record number: 37, Textual support number: 1 OBS

arrimage : Fixation d'une charge utile à l'intérieur ou à l'extérieur d'un véhicule spatial.  4, record 37, French, - charge%20utile%20arrim%C3%A9e

Record number: 37, Textual support number: 2 OBS

charge utile arrimée : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  5, record 37, French, - charge%20utile%20arrim%C3%A9e

Record 37,  Textual support,  Spanish

Record 38,  Textual support,  English

Record number: 38, Textual support number: 1 OBS

There are other control centers around the world that work together with the POIC for payload operations and the SSCC for systems operations. The Space Station Information and Promotion Center(SSIPC) in Japan, Mission Control Center-Moscow(MCC-M) in Russia, and the Attached Pressurized Module Control Center(APM-CC) in Europe each work with the scientists, or users, who have payloads in their respective modules.  2, record 38, English, - Attached%20Pressurised%20Module%20Control%20Centre

Record 38,  Textual support,  French

Record 38,  Textual support,  Spanish

Record 39,  Textual support,  English

Record number: 39, Textual support number: 1 CONT

Destiny Laboratory. The Destiny Laboratory Module is the centerpiece of the International Space Station, where unprecedented science experiments will be performed in the near-zero gravity of space. The lab consists of three cylindrical sections and two endcones with hatches that will be mated to other station components. A 50. 9-centimeter-(20-inch-) diameter window is located on one side of the center module segment. This pressurized module is designed to accommodate pressurized payloads. It has a capacity of 24 rack locations. Payload racks will occupy 13 locations specially designed to support experiments.  9, record 39, English, - Destiny%20laboratory%20module

Record number: 39, Textual support number: 1 OBS

Destiny laboratory module; U.S. laboratory Destiny; Destiny module: terms officially approved by the International Space Station official approval Group (ISSOAG).  10, record 39, English, - Destiny%20laboratory%20module

Record 39,  Textual support,  French

Record number: 39, Textual support number: 1 CONT

Le laboratoire scientifique américain [est] un module pressurisé, habitable, conçu pour accueillir les charges utiles et les expériences devant s'accommoder d'une atmosphère terrestre. Sa capacité est de 24 bâtis modulables, dont 13 sont spécialement conçus pour recevoir des expériences nécessitant un interfaçage complet avec la station et ses ressources.  9, record 39, French, - laboratoire%20Destiny

Record number: 39, Textual support number: 1 OBS

Le module Destiny représente le principal centre d'activités de recherche de la Station spatiale internationale.  10, record 39, French, - laboratoire%20Destiny

Record number: 39, Textual support number: 2 OBS

laboratoire Destiny; laboratoire scientifique américain Destiny; module Destiny : termes uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  11, record 39, French, - laboratoire%20Destiny

Record number: 39, Textual support number: 1 PHR

Positionner le laboratoire sur la station.  11, record 39, French, - laboratoire%20Destiny

Record number: 39, Textual support number: 2 PHR

Coque extérieure du laboratoire Destiny.  11, record 39, French, - laboratoire%20Destiny

Record 39,  Textual support,  Spanish

Record 40,  Textual support,  English

Record number: 40, Textual support number: 1 CONT

Cryorack, an International Standard Payload Rack(ISPR) outfitted with a liner(mechanical infrastructure) and subsystems to support operations of the freezers as well as transportation and operations in the Mini Pressurised Logistic Module(MPLM)...  2, record 40, English, - cryorack

Record number: 40, Textual support number: 1 OBS

cryorack: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 40, English, - cryorack

Record 40,  Textual support,  French

Record number: 40, Textual support number: 1 OBS

bâti congélateur cryogénique : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 40, French, - b%C3%A2ti%20cong%C3%A9lateur%20cryog%C3%A9nique

Record 40,  Textual support,  Spanish

Record 41,  Textual support,  English

Record number: 41, Textual support number: 1 CONT

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, record 41, English, - service%20module%20flight%20model%20structure

Record 41,  Textual support,  French

Record 41,  Textual support,  Spanish

Record 42,  Textual support,  English

Record number: 42, Textual support number: 1 CONT

Integration of the Payload Equipment Bay engineering model has started, and integration of the proto-flight Service Module will commence soon. The structure of the proto-flight payload carrier has been completed and is undergoing qualification static testing at CASA in Spain.  2, record 42, English, - qualification%20static%20testing

Record 42,  Textual support,  French

Record 42,  Textual support,  Spanish

Record 43,  Textual support,  French

Record 43,  Textual support,  Spanish

Record 44,  Textual support,  French

Record 44,  Textual support,  Spanish

Record 45,  Textual support,  English

Record 45,  Textual support,  French

Record number: 45, Textual support number: 1 DEF

Étage-fusée servant à expédier des satellites de classe Delta jusqu'en orbite géostationnaire.  2, record 45, French, - module%20d%27appoint%2Ftype%20delta

Record 45,  Textual support,  Spanish

Record 46,  Textual support,  English

Record number: 46, Textual support number: 1 CONT

The Standard Payload Computer(SPLC) provides a modular and configurable data-handling system based on an industrial-standard VME Bus [Versa Module Europe bus] and a self-standing processor with interfaces connected via a standardised local bus.  2, record 46, English, - standard%20payload%20computer

Record number: 46, Textual support number: 1 OBS

standard payload computer; SPLC: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 46, English, - standard%20payload%20computer

Record 46,  Textual support,  French

Record number: 46, Textual support number: 1 OBS

ordinateur de charge utile standard; SPLC : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 46, French, - ordinateur%20de%20charge%20utile%20standard

Record 46,  Textual support,  Spanish

Record 47,  Textual support,  English

Record number: 47, Textual support number: 1 CONT

The OPAR [On-Orbit Preservation Assembly Rack], housed in one ISPR [International Standard Payload Rack], is outfitted with a liner and the subsystems to accommodate and support the CSF [Cryogenic Storage Freezer] and QSF [Quick/Snap Freezer] operations, and is intended to be integrated into the Centrifuge Accommodation Module(CAM).  1, record 47, English, - on%2Dorbit%20preservation%20assembly%20rack

Record number: 47, Textual support number: 1 OBS

The major elements of Cryosystem consist of the Cryogenic Storage Freezer (CSF), the Quick/Snap Freezer (QSF), the On-Orbit Preservation Assembly Rack (OPAR) and the Transportation Rack (Track).  1, record 47, English, - on%2Dorbit%20preservation%20assembly%20rack

Record number: 47, Textual support number: 2 OBS

on-orbit preservation assembly rack; OPAR: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  2, record 47, English, - on%2Dorbit%20preservation%20assembly%20rack

Record 47,  Textual support,  French

Record number: 47, Textual support number: 1 OBS

bâti de l'unité de conservation en orbite; OPAR : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 47, French, - b%C3%A2ti%20de%20l%27unit%C3%A9%20de%20conservation%20en%20orbite

Record 47,  Textual support,  Spanish

Record 48,  Textual support,  English

Record number: 48, Textual support number: 1 CONT

NASDA Accommodations.... for Japanese users are based on 5 ISPRs [International Standard Payload Racks] in the JEM [Japanese Experiment Module] pressurized module, and 5 ports on the JEM-EF [JEM-Exposed Facility]. Multi-user facilities for Japanese users on the EF remain to be defined, however. The 5 ISPR [International Standard Payload Rack] spaces will consist of three Materials Science Racks and two Life Sciences Racks.  2, record 48, English, - life%20sciences%20rack

Record number: 48, Textual support number: 1 OBS

life sciences rack: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 48, English, - life%20sciences%20rack

Record 48,  Textual support,  French

Record number: 48, Textual support number: 1 OBS

bâti d'expériences en science de la vie : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 48, French, - b%C3%A2ti%20d%27exp%C3%A9riences%20en%20sciences%20de%20la%20vie

Record 48,  Textual support,  Spanish

Record 49,  Textual support,  English

Record number: 49, Textual support number: 1 CONT

... the JEM-EF [Japanese Experiment Module-Exposed Facility] provides a total of l2 attachment ports called Exposed Facility Units(EFUs) to which space-exposed hardware may be mated using a standard Payload Interface Unit(PIU). It is through the PIU that payloads receive all utilities. A total of 10 EFUs available for User payloads, the other two being allocated to the ELM-ES [Experiment Logistics Module-Exposed Section], which transports payloads to orbit and stores them when they are not active, and the Interorbit Communication System(ICS). Five of the 10 available EFUs are available for NASA payloads.  2, record 49, English, - user%20payload

Record number: 49, Textual support number: 1 OBS

user payload: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 49, English, - user%20payload

Record 49,  Textual support,  French

Record number: 49, Textual support number: 1 OBS

charge utile utilisateur : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 49, French, - charge%20utile%20utilisateur

Record 49,  Textual support,  Spanish

Record 50,  Textual support,  English

Record number: 50, Textual support number: 1 CONT

The Commercial Protein Crystal Growth-H experiment consists of 1, 008 individual experiments contained in a High-Density Protein Crystal Growth Assembly. This assembly is then stored in the Commercial Refrigerator Incubator Module(CRIM) at 22 degrees Celsius(72 degrees Fahrenheit). The Space Station crew will install the CRIM into a locker in the Space Station EXPRESS Rack 4 in the U. S. Lab, activate the crystal growth experiments and conduct daily status checks. These daily checks consist of checking temperature readings and cleaning the air filter. When the payload is scheduled to return to Earth, the crew will deactivate the experiments and return the module.  2, record 50, English, - commercial%20refrigerator%20incubator%20module

Record number: 50, Textual support number: 1 OBS

commercial refrigerator incubator module; CRIM: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  3, record 50, English, - commercial%20refrigerator%20incubator%20module

Record 50,  Textual support,  French

Record number: 50, Textual support number: 1 OBS

module d'incubation et de réfrigération commercial; CRIM : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 50, French, - module%20d%27incubation%20et%20de%20r%C3%A9frig%C3%A9ration%20commercial

Record 50,  Textual support,  Spanish