The results of an analysis performed on seven successive Space Shuttle Main Engine (SSME) static test firings, utilizing envelope detection of external accelerometer data are discussed. The results clearly show the great potential for using envelope detection techniques in SSME incipient failure detection.
Incipient failure detection of space shuttle main engine turbopump bearings using vibration envelope detection
01.10.1987
Aufsatz (Konferenz)
Keine Angabe
Englisch
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