Publication Date:
2019-06-28
Description:
Performance and reliability models of alternate microcomputer architectures as a methodology for optimizing system design were examined. A methodology for selecting an optimum microcomputer architecture for autonomous operation of planetary spacecraft power systems was developed. Various microcomputer system architectures are analyzed to determine their application to spacecraft power systems. It is suggested that no standardization formula or common set of guidelines exists which provides an optimum configuration for a given set of specifications.
Keywords:
SPACECRAFT PROPULSION AND POWER
Type:
NASA-CR-168412
,
JPL-PUB-82-1
Format:
application/pdf
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