TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

This internal instrumentation system for a nuclear reactor comprises at least : a probe for measuring the neutron flux in the core of the nuclear reactor; a displacement cable for moving the probe inside the core; a rotary drive device for the displacement cable; and a determination device for determining the angular position of the rotary drive device...  1, record 1, English, - internal%20instrumentation%20system

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 CONT

Système d'instrumentation interne d'un réacteur nucléaire, du type comprenant au moins : - une sonde de mesure du flux neutronique dans le cœur du réacteur nucléaire, - un câble de déplacement de la sonde à l'intérieur du cœur, - un dispositif rotatif d'entraînement du câble de déplacement [...]  1, record 1, French, - syst%C3%A8me%20d%27instrumentation%20interne

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 OBS

The System uses a constellation of satellites placed in orbit at an altitude of 20, 178 km. They complete their circular orbits in half a sidereal day, that is 11 hr 57 min. These satellites emit two sets of signals on 1, 227MHz [megahertz] and 1, 575 MHz in the L-band. These signals carry the transmitting satellites’ identification and position, as well as the time and other information. The airborne equipment is entirely passive. It consists of a receiver whose position is determined by measuring its distance from four of the system's satellites.  9, record 2, English, - Navigation%20Satellite%20Timing%20and%20Ranging%20Global%20Positioning%20System

Record 2,  Textual support,  French

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 DEF

An electronic navigational system by which hyperbolic lines of position are determined by measuring the difference in the time of reception of synchronized pulse signals from two fixed transmitters.  3, record 3, English, - long%20range%20navigation

Record number: 3, Textual support number: 1 OBS

LORAN A operates in the 1750-1950 kHz frequency band. LORAN C and D operate in the 90–110 kHz frequency band.  3, record 3, English, - long%20range%20navigation

Record number: 3, Textual support number: 2 OBS

long range navigation; LORAN: term and abbreviation officially approved by the Department of National Defence.  6, record 3, English, - long%20range%20navigation

Record number: 3, Textual support number: 3 OBS

long range air navigation; LORAN: term, abbreviation and definition standardized by the Glossary for Pilots and Air Traffic Services Personnel Committee.  7, record 3, English, - long%20range%20navigation

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 DEF

Système électronique de navigation à l'aide duquel des lignes de position hyperboliques sont déterminées en mesurant les différences des temps de réception de signaux d'impulsions synchronisées issus de deux émetteurs fixes.  2, record 3, French, - navigation%20%C3%A0%20longue%20distance

Record number: 3, Textual support number: 1 OBS

Le LORAN A fonctionne dans la bande de fréquence de 1750 à 1950 kHz. Le LORAN C et le LORAN D fonctionnent dans la bande de fréquence de 90 à 110 kHz.  2, record 3, French, - navigation%20%C3%A0%20longue%20distance

Record number: 3, Textual support number: 2 OBS

navigation à longue distance; LORAN : terme et abréviation uniformisés par le ministère de la Défense nationale.  4, record 3, French, - navigation%20%C3%A0%20longue%20distance

Record number: 3, Textual support number: 3 OBS

navigation aérienne longue portée; LORAN : terme, abréviation et définition normalisés par le Comité sur le Glossaire à l'intention des pilotes et du personnel des services de la circulation aérienne.  5, record 3, French, - navigation%20%C3%A0%20longue%20distance

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The Long Spacer, measuring 8. 5 by 4. 9 by 4. 9 m, performs two major functions. It physically separates the P6 solar arrays from the P4 solar arrays when the P6 is located in its permanent position, and it will provide temporary cooling to the US laboratory Destiny when it arrives at the ISS [International Space Station] in 2001. The cooling system uses ammonia as a working fluid and can eject 14, 000 watts of heat per orbit.  3, record 4, English, - long%20spacer

Record number: 4, Textual support number: 2 CONT

The P6 integrated truss structure is made up of three elements: the Photovoltaic Array Assembly, the Integrated Equipment Assembly, and the Long Spacer.  3, record 4, English, - long%20spacer

Record number: 4, Textual support number: 1 OBS

long spacer: term officially approved by the International Space Station official approval Group (ISSOAG).  4, record 4, English, - long%20spacer

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 OBS

espaceur : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 4, French, - espaceur

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 DEF

An inertial guidance system that makes use of a three-gimbal mounting whose inner gimbal is a stable platform on which three gyroscopes and accelerometers are mounted; the gyroscopes sense any rotation of the vehicle and drive the gimbals in the opposite direction, so that the inner platform remains fixed in inertial space.  3, record 5, English, - gimbaled%20inertial%20system

Record number: 5, Textual support number: 1 CONT

Automatic Calibration of Transducers for Gimballed Inertial Navigation System on Uncontrolled Gyros. In the work a new approach to calibration of gimbaled Inertial Navigation system(INS) based on two electrostatically suspended gyros(ESG) is considered. The automatic calibration procedure of the inertial measuring unit(IMU) error models parameters, namely, the gimbal pick-off errors, is examined. The measurement errors for angle rotor position are described by equation. The gimbal pick-off errors are described by equation. The relationship between the gimbal pick-off errors and INS output errors is described by equation.  2, record 5, English, - gimbaled%20inertial%20system

Record number: 5, Textual support number: 1 OBS

Gimballed.  4, record 5, English, - gimbaled%20inertial%20system

Record number: 5, Textual support number: 2 OBS

Gimbaled.  5, record 5, English, - gimbaled%20inertial%20system

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

Un nouveau type de centrale inertielle, déjà utilisée sur des avions comme les Airbus A 310 et A 320 [...] vient concurrencer les centrales inertielles à cardans (gimbaled inertial system). Il s'agit d'une centrale dite à composants liés (sous-entendu à la structure de l'avion) appelée en anglais «strap down inertial system». Dans ce cas, en effet, les accéléromètres et les gyromètres (ou les gyroscopes) sont fixés rigidement sur la structure.  1, record 5, French, - centrale%20inertielle%20%C3%A0%20cardans

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 DEF

In astronomy, a system for measuring the position of astronomical objects on the celestial sphere.  2, record 6, English, - equatorial%20co%2Dordinate

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 DEF

Système de coordonnées sphériques, défini par la ligne des pôles terrestres orientée positivement vers le nord, dans lequel peut être repéré un objet céleste.  1, record 6, French, - coordonn%C3%A9e%20%C3%A9quatoriale

Record number: 6, Textual support number: 1 OBS

Les coordonnées équatoriales peuvent être envisagées pour n'importe quelle planète.  1, record 6, French, - coordonn%C3%A9e%20%C3%A9quatoriale

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

The British device is described officially as a Laser True Airspeed System(LATAS) ;it might be more accurate to call it a "potential" or "future" airspeed measuring system, since its function is to advise the pilot what his airspeed will be when he traverses a zone located a short distance ahead of his current position at any given moment. Normally this distance is in the 500-600 m range, far enough ahead at normal approach speeds of 360-450 km/h(200-250kn) to give the pilot some four to six seconds warning to recognize an impending change in true airspeed [due to turbulence] and to take any necessary corrective action.  1, record 7, English, - Laser%20True%20Airspeed%20System

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 CONT

Le dispositif britannique est officiellement appelé "Laser True Airspeed System" ou LATAS (système laser de mesure de la vitesse propre), mais il serait sans doute plus exact de le considérer comme un système de mesure de la vitesse propre "possible" ou "future", puisque son rôle est d'indiquer au pilote quelle sera la vitesse de l'avion lorsqu'il traversera une zone située à une faible distance de la position du moment. Normalement, cette distance sera de l'ordre de 500 à 600 m, ce qui, aux vitesses normales d'approche (360 à 450 km/h), devrait avertir le pilote quatre à six secondes à l'avance des modifications imminentes de la vitesse propre et lui permettre de prendre les mesures correctives nécessaires.  1, record 7, French, - syst%C3%A8me%20laser%20de%20mesure%20de%20la%20vitesse%20propre

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

There are a variety of aircraft position measuring systems in use today, the most common of which incorporates manually operated theodolites or automatic tracking theodolites.  1, record 8, English, - position%20measuring%20system

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 DEF

Système implanté principalement au sol et permettant de transmettre vers un avion, peu de temps avant l'impact son écart latéral par rapport à l'axe de la piste.  1, record 8, French, - syst%C3%A8me%20de%20reconformation

Record number: 8, Textual support number: 1 CONT

Le service technique de la navigation aérienne fait étudier un système (principalement implanté au sol) de reconformation [...].  1, record 8, French, - syst%C3%A8me%20de%20reconformation

Record 8,  Textual support,  Spanish