NASA NTRS ยท 19920066432
Fiberoptic sensors for rocket engine applications
Abstract
A 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.
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Ballard, R. O.. 1992-07-01. Fiberoptic sensors for rocket engine applications. https://ntrs.nasa.gov/citations/19920066432
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