A radiator for a satellite intended for being placed in geostationary orbit around the earth in a tilted plane relative to the plane of the ecliptic, includes at least one panel having at least one radiative surface, and including: a mounting foot supporting the panel; and control and motor elements for pivoting the mounting foot about an axis of rotation tilted relative to the radiative surface which is perpendicular to a radiation axis, the radiation axis and the axis of rotation being tilted relative to one another by a non-zero working angle, corresponding to the tilt angle of the plane of the orbit of the satellite relative to the plane of the ecliptic, the working angle being fixed, such that for any rotation of the mounting foot about the axis of rotation owing to the control and motor elements, the radiative surface remains parallel to the plane of the ecliptic.
RADIATEUR À ENSOLEILLEMENT RÉDUIT POUR SATELLITE ET SATELLITE MUNI D'UN TEL RADIATEUR
RADIATOR WITH REDUCED SOLAR IRRADIATION FOR SATELLITE AND SATELLITE PROVIDED WITH SUCH A RADIATOR
RADIATOR MIT REDUZIERTER SONNENBESTRAHLUNG FÜR SATELLITEN UND SATELLIT MIT SOLCH EINEM RADIATOR
2017-11-08
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
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