DocumentCode :
1890423
Title :
Space Transportation Main Engine reliability demonstration technique
Author :
Pugh, Richard L.
Author_Institution :
Div. of Gov. Engines & Space Propulsion, Pratt & Whitney, West Palm Beach, FL, USA
fYear :
1993
fDate :
26-28 Jan 1993
Firstpage :
173
Lastpage :
180
Abstract :
To satisfy the Space Transportation Main Engine (STME) reliability requirement demonstration of 99% reliability at 90% confidence, the Space Propulsion Integrated Reliability Team (SPIRT) developed a cost-efficient and effective approach using the binomial model in combination with the US Army Materiel Systems Analysis Activity (AMSAA) growth model. Using the binomial model as the base, the number of tests necessary to meet the requirement demonstration is established by assuming no failures during the demonstration test. To assist in ascertaining whether the zero failure requirement can be met during the reliability demonstration, the AMSAA growth trend will be assessed through the development testing. The results of the trend will be used to decide whether more development testing is required or the reliability demonstration can be initiated
Keywords :
aerospace engines; aerospace testing; reliability; AMSAA growth trend; Space Transportation Main Engine; binomial model; development testing; number of tests; reliability demonstration; zero failure requirement; Bayesian methods; Cost function; Design methodology; Engines; Propulsion; Quality function deployment; Rockets; Space technology; System testing; Transportation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1993. Proceedings., Annual
Conference_Location :
Atlanta, GA
Print_ISBN :
0-7803-0943-X
Type :
conf
DOI :
10.1109/RAMS.1993.296858
Filename :
296858
Link To Document :
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