A support structure for a spacecraft is disclosed having a first side wall, a second side wall which is parallel to and opposite the first side wall, a third side wall attached to at least the first side wall, and a fourth side wall which is parallel to and opposite the third side wall; at least one interior panel attached between and perpendicular to the first side wall and to the second side wall, at least one first thermal coupling device bearing against the second side wall and attached to the interior panel, electronic devices arranged on and in direct thermal contact with at least a portion of the first thermal coupling device.
STRUCTURE PORTEUSE POUR VÉHICULE SPATIAL ET PROCÉDÉ DE MONTAGE D'UNE STRUCTURE PORTEUSE POUR VÉHICULE SPATIAL
SUPPORT STRUCTURE FOR A SPACECRAFT AND METHOD OF ASSEMBLING SAME
TRÄGERSTRUKTUR FÜR EIN RAUMFAHRZEUG UND MONTAGEVERFAHREN DAFÜR
2022-11-02
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
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