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Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 DEF

An aerospace vehicle designed to send a spacecraft into space through the use of a propulsion system.  7, record 1, English, - launch%20vehicle

Record number: 1, Textual support number: 1 PHR

expendable launch vehicle, fully reusable launch vehicle, reusable launch vehicle, semi-reusable launch vehicle  7, record 1, English, - launch%20vehicle

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

Véhicule aérospatial conçu pour envoyer un engin spatial dans l'espace au moyen d'un système de propulsion.  3, record 1, French, - lanceur%20spatial

Record number: 1, Textual support number: 1 PHR

lanceur spatial entièrement réutilisable, lanceur spatial non réutilisable, lanceur spatial réutilisable, lanceur spatial semi-réutilisable  3, record 1, French, - lanceur%20spatial

Record 1,  Textual support,  Spanish

Record number: 1, Textual support number: 1 CONT

[La] invención se centra en el diseño de un vehículo espacial multietapa de transferencia a órbita terrestre baja, que presenta dos novedades fundamentales: comprende un vehículo lanzador entendido como primera etapa y concebido como un dirigible semirrígido, que asciende hasta la estratosfera, lanza un cohete y regresa a tierra para ser reutilizado totalmente, otro vehículo entendido como segunda etapa y concebido como un cohete monoetapa, que todo él se considera como carga útil, sin que se desprenda durante el viaje ninguna parte de él.  1, record 1, Spanish, - veh%C3%ADculo%20lanzador

Record number: 1, Textual support number: 1 OBS

vehículo lanzador: designación validada por un experto de la Comisión de Terminología, Sociedad Española de Astronomía, España.  2, record 1, Spanish, - veh%C3%ADculo%20lanzador

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 DEF

A structure mounted on top of a manned expendable launch vehicle, containing rocket motors which can be used to pull the spacecraft capsule clean of the launch vehicle in case of emergency.  6, record 2, English, - launch%20abort%20system

Record number: 2, Textual support number: 1 OBS

Escape towers were used with Olencucy, Apollo and Soyuz spacecrafts.  6, record 2, English, - launch%20abort%20system

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 DEF

Dans le cas d'un lancement spatial habité, dispositif permettant d'arracher l'habitacle de son lanceur en cas de danger pendant la phase initiale du vol.  4, record 2, French, - tour%20de%20sauvetage

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

Programme CELV.  2, record 3, French, - lanceur%20non%20r%C3%A9utilisable%20CELV

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors: Vector L is colinear with position vector P (on the axis between the Earth’s centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane (vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, record 4, English, - roll%20axis

Record number: 4, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation : roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle's centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight.... The axes of a cylindrical spacecraft(e. g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft(i. e. defined relative to the pilot's seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc" : the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth's spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  4, record 4, English, - roll%20axis

Record number: 4, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  4, record 4, English, - roll%20axis

Record number: 4, Textual support number: 2 OBS

roll axis; axis of roll: terms officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  5, record 4, English, - roll%20axis

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  1, record 4, French, - axe%20de%20roulis

Record number: 4, Textual support number: 1 OBS

axe de roulis : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 4, French, - axe%20de%20roulis

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors: Vector L is colinear with position vector P (on the axis between the Earth’s centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane (vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  2, record 5, English, - pitch%20axis

Record number: 5, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation : roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle's centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight.... The axes of a cylindrical spacecraft(e. g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft(i. e. defined relative to the pilot's seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc" : the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth's spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  3, record 5, English, - pitch%20axis

Record number: 5, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  3, record 5, English, - pitch%20axis

Record number: 5, Textual support number: 2 OBS

pitch axis: term officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 5, English, - pitch%20axis

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  2, record 5, French, - axe%20de%20tangage

Record number: 5, Textual support number: 1 OBS

axe de tangage : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2.  3, record 5, French, - axe%20de%20tangage

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

An expendable launch system is a single-use launch vehicle usually used to launch a payload into space. This is in opposition to a reusable launch system where a single launch vehicle is launched more than once.  5, record 6, English, - expendable%20launch%20vehicle

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 DEF

Engin à usage unique, utilisé pour le lancement de charges utiles dans l'espace.  4, record 6, French, - lanceur%20non%2Dr%C3%A9utilisable

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

The Evolved Expendable Launch Vehicle(EELV) program is a space launch system development program. The purpose of this program is to replace the current fleet of medium to heavy-lift class expendable launch vehicles(Titan II), Delta II, Atlas II, and Itan IV) with a more affordable family of space launch vehicles.  3, record 7, English, - evolved%20expendable%20launch%20vehicle

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

Ce type de lanceur fait partie d'un programme américain dont le nom n'a pas de traduction officielle en français.  2, record 7, French, - lanceur%20non%20r%C3%A9utilisable%20EELV

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

In 1979, Boeing and the US Air Force Rocket Propulsion Laboratory proposed a small unmanned "Air-Launched Sortie Vehicle", ALSV consisting of a reusable spaceplane and a huge expendable propellant tank. The vehicle could overfly any point on Earth within 90 minutes of the launch order and also perform other military missions such as satellite inspection. It then returns to a military airbase and lands horizontally like the Space Shuttle.  2, record 8, English, - air%2Dlaunched%20sortie%20vehicle

Record 8,  Textual support,  French

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

A specific increment's planning operation may begin several years before the relevant STS launch(or OMV [Orbital Maneuvering Vehicle] deployment from the manned base). A specific increment's executions operations begin with the Station Program's realtime support to launch of the relevant transportation mission(STS/OMV), and generally extends through the initiation of similar support to the respective follow on transportation mission. ELV [Expendable Launch Vehicle] arrivals at Station elements are contained within the relevant increment. For the manned base, increment duration may vary according to the number of STS visits per year(for eight flights per year, increment duration is 45 days; for five flights per year, 72 days). For platforms, increment duration is related to the period between servicing, between deployment and return to Earth, or between deployment and the end of its operational lifetime.  1, record 9, English, - increment%20planning%20operation

Record number: 9, Textual support number: 1 OBS

increment planning operation: term officially approved by the International Space Station official approval Group (ISSOAG).  2, record 9, English, - increment%20planning%20operation

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 OBS

opération de planification incrémentée : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, record 9, French, - op%C3%A9ration%20de%20planification%20incr%C3%A9ment%C3%A9e

Record 9,  Textual support,  Spanish