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Improved maintainability of space-based reusable rocket enginesAdvanced, noninferential, noncontacting, in situ measurement technologies, combined with automated testing and expert systems, can provide continuous, automated health monitoring of critical space-based rocket engine components, requiring minimal disassembly and no manual data analysis, thus enhancing their maintainability. This paper concentrates on recent progress of noncontacting combustion chamber wall thickness condition-monitoring technologies.
Document ID
19880060810
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barkhoudarian, S.
(Rockwell International Corp. Canoga Park, CA, United States)
Szemenyei, B.
(Rockwell International Corp. Canoga Park, CA, United States)
Nelson, R. S.
(Rockwell International Corp. Canoga Park, CA, United States)
Pauckert, R.
(Rockwell International Corp. Canoga Park, CA, United States)
Harmon, T.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 88-3113
Accession Number
88A48037
Funding Number(s)
CONTRACT_GRANT: NAS3-23773
Distribution Limits
Public
Copyright
Other

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