Title:
SATELLITE ELECTRIC PROPULSION POWER SUPPLY UNIT AND SYSTEM FOR MANAGING THE ELECTRIC PROPULSION OF SATELLITE
Document Type and Number:
Japanese Patent JP2016199259
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a satellite electric propulsion power supply unit and a system for managing the electric propulsion of a satellite.SOLUTION: A satellite electric propulsion power supply unit UAPE comprises: an internal source Sint of electrical power; an external input line E adapted to receive an electrical power supply from an external source of electrical power; a first external output line S1 and a second external output line S2 adapted to deliver as output, respectively, a first electrical power supply and a second electrical power supply; and a first selector element SEL1 and a second selector element SEL2. The first selector element SEL1 is equipped with a first internal input line Ei1 connected to the internal source Sint and with two output lines: the first external output line S1 and an internal output line Si connected to a second internal input line Ei2 of the second selector element SEL2. The second selector element SEL2 is equipped with an output line corresponding to the second external output line S2 and with two input lines: the external input line E and the second internal input line Ei2.SELECTED DRAWING: Figure 2
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Inventors:
ALAIN GRUWE
PHILIPPE LEDENT
PHILIPPE LEDENT
Application Number:
JP2016076339A
Publication Date:
December 01, 2016
Filing Date:
April 06, 2016
Export Citation:
Assignee:
THALES SA
International Classes:
B64G1/22; B64G1/40; H02J1/00; H02J9/06
Attorney, Agent or Firm:
Kawaguchi International Patent Office