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
1987-10-01
Conference paper
No indication
English
SPACE SHUTTLE MAIN ENGINE TURBOPUMP DESIGN
SAE Technical Papers | 1973
|Space shuttle main engine turbopump design and development
Tema Archive | 1975
|Turbopump configuration selection for the Space Shuttle main engine
Tema Archive | 1974
|