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Electric propulsion power supply device for satellite and satellite electric propulsion management system
Electric propulsion power supply device for satellite and satellite electric propulsion management system
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机译：用于卫星的电力推进电源装置及卫星电力推进管理系统
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摘要
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.
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