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Integrating Reliability Principles in the Design of the Plant Research Unit (PRU)
Technical Paper
2004-01-2393
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The design of reliable systems is especially important when they are intended for use on the International Space Station (ISS). Limits on crew time and the sensitive nature of experiments being performed require that the systems used to support those experiments have a very low probability of failure. The Plant Research Unit (PRU) has very strict reliability requirements and thus provides a good example of how the challenge of designing reliable systems can be met.
Authors
Citation
Stadler, J., Brideau, L., Emmerich, J., and Varma, N., "Integrating Reliability Principles in the Design of the Plant Research Unit (PRU)," SAE Technical Paper 2004-01-2393, 2004, https://doi.org/10.4271/2004-01-2393.Also In
References
- DOD 1980
- DOD 1991 Reliability Prediction of Electronic Equipment MIL-HDBK-217F
- NASA 1999 Failure Modes and Effects Analysis and Critical Items List Requirements for Space Station SSP-30234E
- NASA 2000 Space Station Approved Electrical, Electronic and Electromechanical Parts List SSP 30423H
- NASA 1996 Goddard Preferred Parts List GSFC PPL21
- NASA 2001 NASA Parts Selection List NPSL
- DOD 1994 NASA Standard Electrical, Electronic and Electromechanical (EEE) Parts List MIL-STD-975M
- NASA 2002 Consolidated SSBRP EEE Parts List ARC/BRP 40100
- DOD 1996a Test Method Standard Microcircuits MIL-STD-883
- DOD 1996b Environmental Stress Screening Process for Electronic Equipment MIL-HDBK-2164A