Publication Date:
2013-08-31
Description:
The parts of electric motors which should be duplicated in order to provide maximum reliability in spacecraft application are identified. Various common types of redundancy are described. The advantages and disadvantages of each are noted. The principal types are illustrated by reference to specific examples. For each example, constructional details, basic performance data and failure modes are described, together with a discussion of the suitability of particular redundancy techniques to motor types.
Keywords:
ELECTRONICS AND ELECTRICAL ENGINEERING
Type:
NASA. Lewis Research Center The 20th Aerospace Mechanics Symposium; p 179-194
Format:
application/pdf
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