A satellite electric propulsion power supply unit comprises: an internal source of electrical power; an external input adapted to receive an electrical power supply from an external source of electrical power; a first external output and a second external output adapted to deliver as output, respectively, a first electrical power supply and a second electrical power supply; a first selector element and a second selector element such that: the first selector element is equipped with a first internal input connected to the internal source and with two outputs: the first external output and an internal output connected to a second internal input of the second selector element; and the second selector element is equipped with an output corresponding to the second external output and with two inputs: the external input and the second internal input.
UNITÉ D'ALIMENTATION DE PROPULSION ÉLECTRIQUE DE SATELLITE ET SYSTÈME DE GESTION DE PROPULSION ÉLECTRIQUE D'UN SATELLITE
SATELLITE ELECTRIC PROPULSION SUPPLY UNIT AND SYSTEM FOR MANAGING ELECTRIC PROPULSION OF A SATELLITE
STROMVERSORGUNGSEINHEIT EINES ELEKTRISCHEN ANTRIEBS EINES SATELLITEN, UND STEUERSYSTEM DES ELEKTRISCHEN ANTRIEBS EINES SATELLITEN
2017-05-24
Patent
Electronic Resource
French
Système d’alimentation électrique d’un système de propulsion électrique d’un aéronef.
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