Disclosed is artificial satellite including: a mounting structure supporting equipment-bearing walls; a launcher-adapter rigidly connected to the mounting structure; a first radiator; and at least one first system for transporting heat by a fluid, including at least one duct having a first heat-exchange section and a second heat-exchange section, the second heat-exchange section being capable of being in thermal contact with the first radiator. The first heat-exchange section is in thermal contact with at least one portion of the launcher-adapter. Also disclosed is a method for filling a tank of propellant gas of the artificial satellite.
SATELLITE ARTIFICIEL ET PROCÉDÉ DE REMPLISSAGE D'UN RÉSERVOIR DE GAZ PROPULSIF DUDIT SATELLITE ARTIFICIEL
ARTIFICIAL SATELLITE AND METHOD FOR FILLING A TANK OF PROPELLENT GAS OF SAID ARTIFICIAL SATELLITE
KÜNSTLICHER SATELLIT UND VERFAHREN ZUM FÜLLEN EINES TANKS EINES TREIBGASES DES BESAGTEN KÜNSTLICHEN SATELLITEN
2017-11-22
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
European Patent Office | 2016
|European Patent Office | 2016
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