A preliminary report on the development of a system for monitoring the High Pressure Oxidizer Turbopump (HPOTP) of the Space Shuttle Main Energine (SSME) is presented. The system development will proceed by defining the degradation mechanisms of the turbopump, identifying those sensor measurments, both conventional and advanced, which can monitor these mechanisms, and determing the digiretal processing requirements for these measurements. Once the failures and associated measurements have been defined, an expert system will be nostic inferences about the condition and performance of the turbopump.
An expert system approach to turbopump health monitoring
Expertensystem zur Ueberwachung des Zustands von Turbopumpen
AIAA-Papers ; Jul ; 1-6
1988
6 Seiten, 9 Bilder
Aufsatz (Konferenz)
Englisch
An expert system approach to turbopump health monitoring
AIAA | 1988
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