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Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 DEF

Cords or webbing of silk, nylon, cotton, rayon, or other textile materials which connect the drap surface of the parachute [and paraglider] to the harness.  5, fiche 1, Anglais, - suspension%20line

Record number: 1, Textual support number: 1 CONT

A paraglider is made up of the wing, rigging(lines), small carabiner, and risers.... Lines. Commonly known as lines(a set of rigging) measuring variously between 0. 4-1. 7 mm, even 2. 2 mm, their high level of strength or weight resistance depends on their thickness and the properties of material used in its construction. They are usually concerned with a protective sheath to guard against ground friction and are made from dyneema, kevlar, spectra, superaramid and so on. The lines attach the wing to risers which in turn are attached to the pilots harness, and extend from the wings downward side in the order specified by the particular manufacturer, gradually tapering off in thickness and number via a series of quick links. Finally they end up in tiny linkages(known as small carabiner) from the risers.  6, fiche 1, Anglais, - suspension%20line

Record number: 1, Textual support number: 1 OBS

Terms usually used in plural.  7, fiche 1, Anglais, - suspension%20line

Record number: 1, Textual support number: 2 OBS

Terms used for paragliding equipment.  7, fiche 1, Anglais, - suspension%20line

Fiche 1,  Justifications,  Français

Record number: 1, Textual support number: 1 DEF

[...] câbles qui relient le harnais d'un parachute [et parapente] à la voilure.  4, fiche 1, Français, - suspente

Record number: 1, Textual support number: 1 CONT

Les suspentes sont des câbles en nylon/kevlar qui relient la voile aux élévateurs. On distingue 4 types de suspentage que l'on appelle aussi des lignes de suspentage : Ligne A (avant), Ligne B (intermédiaire), Ligne C (arrière), Ligne de commande (commandes de frein).  5, fiche 1, Français, - suspente

Record number: 1, Textual support number: 1 OBS

La drisse est un terme qui nous vient des marins («Hissez la drisse de grand voile!»). C'est donc un cordage. En parapente, on appelle les drisses, les suspentes.  5, fiche 1, Français, - suspente

Record number: 1, Textual support number: 2 OBS

Termes habituellement utilisés au pluriel.  6, fiche 1, Français, - suspente

Record number: 1, Textual support number: 3 OBS

Termes qui s'appliquent à l'équipement du parapente.  6, fiche 1, Français, - suspente

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 DEF

A wing from which the rest of the aircraft is suspended by ties.  3, fiche 2, Anglais, - parasol%20wing

Record number: 2, Textual support number: 1 OBS

parasol : raised above a pilot's head to permit downward vision(parasol wings).  4, fiche 2, Anglais, - parasol%20wing

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 DEF

Type d'aile placée au-dessus du fuselage et reliée à celui-ci par une «cabane».  2, fiche 2, Français, - aile%20parasol

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, 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, fiche 3, Anglais, - roll%20axis

Record number: 3, 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, fiche 3, Anglais, - roll%20axis

Record number: 3, 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, fiche 3, Anglais, - roll%20axis

Record number: 3, 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, fiche 3, Anglais, - roll%20axis

Fiche 3,  Justifications,  Français

Record number: 3, 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, fiche 3, Français, - axe%20de%20roulis

Record number: 3, 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, fiche 3, Français, - axe%20de%20roulis

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

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.  2, fiche 4, Anglais, - pitch%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.  3, fiche 4, Anglais, - pitch%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."  3, fiche 4, Anglais, - pitch%20axis

Record number: 4, 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, fiche 4, Anglais, - pitch%20axis

Fiche 4,  Justifications,  Français

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.  2, fiche 4, Français, - axe%20de%20tangage

Record number: 4, 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, fiche 4, Français, - axe%20de%20tangage

Fiche 4,  Justifications,  Espagnol