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NASA NTRS · 19880042590

Reusable rocket engine optical condition monitoring

Abstract

Plume emission spectrometry and optical leak detection are described as two new applications of optical techniques to reusable rocket engine condition monitoring. Plume spectrometry has been used with laboratory flames and reusable rocket engines to characterize both the nominal combustion spectra and anomalous spectra of contaminants burning in these plumes. Holographic interferometry has been used to identify leaks and quantify leak rates from reusable rocket engine joints and welds.

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BibTeXRIS

Wyett, L., Maram, J., Barkhoudarian, S., Reinert, J.. 1987-12-01. Reusable rocket engine optical condition monitoring. https://ntrs.nasa.gov/citations/19880042590

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