NASA NTRS · 19930046924
High voltage spacecraft electrical systems design
Abstract
Factors which must be considered when designing the best and the most cost-effective high-voltage electrical system for a spacecraft are discussed with particular attention given to the EMC considerations, high-voltage power bus, and harnesses. It is emphasized that the use of serial data buses and lines greatly simplify the harness design and weight. Careful attention to the grounding concept and the EMC requirements is necessary for insuring a 'quiet' spacecraft.
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Stone, R. E.. 1993-02-01. High voltage spacecraft electrical systems design. https://ntrs.nasa.gov/citations/19930046924
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