The high-pressure oxidizer turbopump (HPOTP) failure information propagation model (FIPM) is presented. The text includes a brief discussion of the FIPM methodology and the various elements which comprise a model. Specific details of the HPOTP FIPM are described. Listings of all the HPOTP data records are included as appendices.
Studies and Analyses of the Space Shuttle Main Engine: High-Pressure Oxidizer Turbopump Failure Information Propagation Model
1987
511 pages
Report
No indication
English