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NASA NTRS · 19880065900

Non-intrusive Space Shuttle Main Engine nozzle exit diagnostics

Abstract

The results of a conceptual design study on the feasibility of nonintrusive optical diagnostics have shown that UV laser-excited Raman scattering can furnish reliable and accurate temperature and multiple-species data for the Space Shuttle Main Engine's exhaust flow. Enhanced OH flow tagging by UV photodissociation of H2O was used in velocity measurements; a time-delayed pulsed dye laser beam at 308 nm excites fluorescence from OH, and the location of the convected enhanced OH zone is measured with an optical multichannel detector.

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BibTeXRIS

Shirley, John A., Boedeker, Laurence R.. 1988-07-01. Non-intrusive Space Shuttle Main Engine nozzle exit diagnostics. https://ntrs.nasa.gov/citations/19880065900

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