The Effect of Maintainability on the Mission Reliability of Two-Element Redundant Spacecraft Subsystems.
ResearchPublished 1965
Presentation of a technique for assessing the effect of maintenance on the reliability of those spacecraft systems in which the prime system is backed up by a redundant secondary one. Two types of reliability are considered. The first applies to such critical systems as life support, and failure is defined as the event in which both prime and secondary elements are inoperable even though repairable. The second applies to cases where temporary inoperability of both elements is allowed, and failure is defined as the event where both prime and secondary elements are nonrepairable. A key concept is that, in case of breakdown, repair is not necessarily assured. An index of repairability is developed to define the probability that a randomly occurring breakdown can be repaired, and the general structure of the two-element redundant repairable system and the parameters affecting mission reliability are defined. 62 pp
Document Details
- Copyright: RAND Corporation
- Availability: Web Only
- Year: 1965
- Pages: 62
- Document Number: RM-4824-PR
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