DocumentCode
264377
Title
Application of Fault Management theory to the quantitative selection of a launch vehicle Abort Trigger suite
Author
Lo, Yunnhon ; Johnson, Stephen B. ; Breckenridge, Jonanthan T.
Author_Institution
Jacobs ESSSA Group, Ducommun Miltec, Huntsville, AL, USA
fYear
2014
fDate
22-25 June 2014
Firstpage
1
Lastpage
16
Abstract
This paper describes the quantitative application of the theory of System Health Management and its operational subset, Fault Management, to the selection of Abort Triggers for a human-rated launch vehicle, the United States´ National Aeronautics and Space Administration´s (NASA) Space Launch System (SLS). The results demonstrate the efficacy of the theory to assess the effectiveness of candidate failure detection and response mechanisms to protect humans from time-critical and severe hazards. The quantitative method was successfully used on the SLS to aid selection of its suite of Abort Triggers.
Keywords
aerospace computing; fault diagnosis; space vehicles; NASA space launch system; National Aeronautics and Space Administration; failure detection mechanism; failure response mechanism; fault management theory; launch vehicle abort trigger suite; quantitative selection; system health management theory; Barium; Bismuth; DH-HEMTs; Hafnium; Abort Triggers; Fault Management; failure response; human rating; launch vehicle; probabilistic risk assessment; state estimation;
fLanguage
English
Publisher
ieee
Conference_Titel
Prognostics and Health Management (PHM), 2014 IEEE Conference on
Conference_Location
Cheney, WA
Type
conf
DOI
10.1109/ICPHM.2014.7036380
Filename
7036380
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