An electrical power system (300) including a first plurality of power sources (371) including at least one of a first solar array (304), a first supercapacitor (308), and a first battery (306). The electrical power system further includes a second plurality of power sources (372) including at least one of a second solar array, a second supercapacitor, and a second battery. The electrical power system further includes a first ESMC (311) in electronic communication with the first plurality of power sources. The electrical power system further includes a second ESMC (312) in electronic communication with the second plurality of power sources. The electrical power system further includes a multi-channel DC bus (320) which supplies electric power to a load. The first ESMC supplies electric power to a first channel (321) of the multi-channel DC bus. The second ESMC supplies electric power to a second channel (322) of the multi-channel DC bus.
SOLAR POWERED SPACECRAFT POWER SYSTEM
SOLARBETRIEBENES RAUMFAHRZEUGSTROMVERSORGUNGSSYSTEM
SYSTÈME D'ALIMENTATION D'ENGIN SPATIAL ALIMENTÉ PAR ÉNERGIE SOLAIRE
04.09.2024
Patent
Elektronische Ressource
Englisch
IPC: | H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen |