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2A2 Maintainability Design or Support? F J Kreuze
2A3 Optimizing the Tradeoff Between Reliability and Maintainability Design H S Goldman
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Air Force application approach Assurance availability basic bility capacitors cathode checkout circuit complete component configuration considered cost curve defined design review determine distribution effect electrical electronic elements environment equation equipment errors established estimate evaluation example Failure Analysis failure modes failure rate Figure flight function hardware heater incentive indicated input klystron limits maintenance malfunction manufacturing mathematical maximum measure ment method minimum missile mission MTBF NASA normal normally distributed North American Aviation operating optimum parameters performance phase prediction probability problem procedure Quality Control radiation random random variables redundancy relia reliabil Reliability Engineering reliability program reliability requirements Report Research resistor S-II sample Sandia Corporation satellite sequential simulation space specific standard standard deviation statistical stress subsystem supersystem system reliability Table tasks techniques test program tion trade-off tubes ullage motor values variables vehicle vendor voltage Weibull Weibull distribution