Spacecraft power system architecture to mitigate spacecraft charging effects

A power system architecture for a spacecraft and a method of a power supply for a spacecraft are presented which take advantage of the reduced plasma interaction associated with positive ground high voltage photovoltaic arrays and provide a negative ground power supply for electrical loads of the sp...

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Bibliographische Detailangaben
1. Verfasser: Manner, David B.
Format: Report
Sprache:eng
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