Limitations of Spacecraft Redundancy: A Case Study Analysis
Date
2014-07-13
Authors
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Journal ISSN
Volume Title
Publisher
44th International Conference on Environmental Systems
Abstract
Redundancy can increase spacecraft safety by providing the crew or ground with multiple means of achieving a given function. However, redundancy can also decrease spacecraft safety by 1) adding additional failure modes to the system, 2) increasing design “opaqueness”, 3) encouraging operational risk, and 4) masking or “normalizing” design flaws. Two Loss of Crew (LOC) events—Soyuz 11 and Challenger STS 51-L—are presented as examples of these limitations. Together, these case studies suggest that redundancy is not necessarily a fail-safe means of improving spacecraft safety.
Description
Tucson, Arizona
Robert P. Ocampo, University of Colorado Boulder, USA
The 44th International Conference on Environmental Systems was held in Tuscon, Arizona, USA on 13 July 2014 through 17 July 2014.
Robert P. Ocampo, University of Colorado Boulder, USA
The 44th International Conference on Environmental Systems was held in Tuscon, Arizona, USA on 13 July 2014 through 17 July 2014.