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Reliability Design Analysis for Space Systems
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English
Abstract
This paper presents a description of some of the problems encountered in the design of space systems and discusses some of the approaches, considerations, and analytic tools which may be useful in solving those problems. The techniques and problems to be discussed are; reliability estimation, weight-reliability tradeoffs, and spares and redundancy considerations. The analytic approaches discussed are meant to be representative of the types of analysis available and are used to illustrate some of the techniques which have been satisfactorily used on space programs.
Citation
Weisberg, S., "Reliability Design Analysis for Space Systems," SAE Technical Paper 670677, 1967, https://doi.org/10.4271/670677.Also In
References
- Esary, J.D. Proschan, F. “Coherent Structures of Non-Identical Components” Technometrics May 1963
- Birnbaum, F.W. Esary, J.D. Saunders, S.C. “Multi-Component Systems and Structures and Their Reliability” Technometrics February 1961
- Weisberg, S.A. Schmidt, J.H. “Computer Technique For Estimating System Reliability” Proceedings, 1966 Annual Symposium on Reliability January 1966
- Weisberg, S.A. Chin, J.H.S. “Reliability and Availability of Some Redundant Systems” Proceedings, U.S.A.F. Electronic Systems Division Maintainability Conference March 1963