Studies and analyses of the space shuttle main engine: High-pressure oxidizer turbopump failure information propagation model

Rudy, S. W.
Glover, R. C.
Tischer, A. E.

Publication date

April 1987

Language

English

Abstract

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

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Studies and analyses of the space shuttle main engine: High-pressure oxidizer turbopump failure information propagation model

Abstract

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Studies and analyses of the space shuttle main engine: High-pressure oxidizer turbopump failure information propagation model

Abstract

Extracted data

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