The invention relates to a reflective satellite (1) comprising at least one curved reflection surface (11), the satellite (1) being characterised in that it comprises at least one load-bearing structure (10) connected to at least four positioning and orientation systems (12) for controlling the attitude and the orbit of the reflective satellite, said positioning and orientation systems comprising at least one thruster system, said positioning and orientation systems being synchronised and arranged so as to allow orientation of the reflector satellite relative to at least two axes of rotation. A satellite assembly including a source satellite and a reflective satellite is also disclosed.
SATELLITE RÉFLECTEUR ET ENSEMBLE SATELLITAIRE COMPRENANT UN TEL SATELLITE
REFLECTIVE SATELLITE AND SATELLITE ASSEMBLY COMPRISING SUCH A SATELLITE
REFLEKTIERENDER SATELLIT UND SATELLITENANORDNUNG MIT EINEM SOLCHEN SATELLIT
2024-07-24
Patent
Elektronische Ressource
Französisch
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