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SSME HPOTP post-test diagnostic system enhancement projectAn assessment of engine and component health is routinely made after each test or flight firing of a space shuttle main engine (SSME). Currently, this health assessment is done by teams of engineers who manually review sensor data, performance data, and engine and component operating histories. Based on review of information from these various sources, an evaluation is made as to the health of each component of the SSME and the preparedness of the engine for another test or flight. The objective of this project is to further develop a computer program which automates the analysis of test data from the SSME high-pressure oxidizer turbopump (HPOTP) in order to detect and diagnose anomalies. This program fits into a larger system, the SSME Post-Test Diagnostic System (PTDS), which will eventually be extended to assess the health and status of most SSME components on the basis of test data analysis. The HPOTP module is an expert system, which uses 'rules-of-thumb' obtained from interviews with experts from NASA Marshall Space Flight Center (MSFC) to detect and diagnose anomalies. Analyses of the raw test data are first performed using pattern recognition techniques which result in features such as spikes, shifts, peaks, and drifts being detected and written to a database. The HPOTP module then looks for combination of these features which are indicative of known anomalies, using the rules gathered from the turbomachinery experts. Results of this analysis are then displayed via a graphical user interface which provides ranked lists of anomalies and observations by engine component, along with supporting data plots for each.
Document ID
19950015041
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bickmore, Timothy W.
(Aerojet Technical Systems Co. Sacramento, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publisher: NASA
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-9372
NASA-CR-4643
NAS 1.26:4643
Report Number: E-9372
Report Number: NASA-CR-4643
Report Number: NAS 1.26:4643
Accession Number
95N21458
Funding Number(s)
CONTRACT_GRANT: NAS3-25883
PROJECT: RTOP 584-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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