Disclosed is a satellite including a cylindrical main body, the main body having an inner wall defining an inner space and an outer wall, and extending along a main axis between a lower end surface and an upper end surface, at least one of the lower end surface and the upper end surface including an interface mechanism intended for engaging with a complementary interface mechanism of another satellite or of a launcher, the satellite also including at least one external device attached to the outer wall of the main body, the outer device extending to project transversely from the outer wall relative to the main axis.
SATELLITE À CORPS PRINCIPAL CYLINDRIQUE, EMPILEMENT COMPRENANT UN TEL SATELLITE ET ENSEMBLE DE LANCEMENT POUR UN TEL SATELLITE
SATELLITE WITH CYLINDRICAL MAIN BODY, STACK COMPRISING SUCH A SATELLITE AND LAUNCH ASSEMBLY FOR SUCH A SATELLITE
SATELLIT MIT ZYLINDRISCHEM HAUPTKÖRPER, STAPEL MIT SOLCH EINEM SATELLITEN UND STARTANORDNUNG FÜR SOLCH EINEN SATELLITEN
2018-09-26
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
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