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NASA NTRS · 20090011277

Optical Pressure-Temperature Sensor for a Combustion Chamber

Abstract

A compact sensor for measuring temperature and pressure in a combusti on chamber has been proposed. The proposed sensor would include two optically birefringent, transmissive crystalline wedges: one of sapph ire (Al2O3) and one of magnesium oxide (MgO), the optical properties of both of which vary with temperature and pressure. The wedges wou ld be separated by a vapor-deposited thin-film transducer, which wou ld be primarily temperaturesensitive (in contradistinction to pressur e- sensitive) when attached to a crystalline substrate. The sensor w ould be housed in a rugged probe to survive the extreme temperatures and pressures in a combustion chamber.

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BibTeXRIS

Wiley, John, Korman, Valentin, Gregory, Don. 2008-07-01. Optical Pressure-Temperature Sensor for a Combustion Chamber. https://ntrs.nasa.gov/citations/20090011277

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