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
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