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Fiberoptic sensors for rocket engine applicationsA research effort was completed to summarize and evaluate the current level of technology in fiberoptic sensors for possible applications in integrated control and health monitoring (ICHM) systems in liquid propellant engines. The environment within a rocket engine is particuarly severe with very high temperatures and pressures present combined with extremely rapid fluid and gas flows, and high-velocity and high-intensity acoustc waves. Application of fiberoptic technology to rocket engine health monitoring is a logical evolutionary step in ICHM development and presents a significant challenge. In this extremely harsh environment, the additional flexibility of fiberoptic techniques to augment conventional sensor technologies offer abundant future potential.
Document ID
19920066432
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ballard, R. O.
(Sverdrup Technology, Inc.; NASA, Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 92-3536
Accession Number
92A49056
Funding Number(s)
CONTRACT_GRANT: NAS8-37814
Distribution Limits
Public
Copyright
Other

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