Title :
Imaging Fourier transform spectrometry of jet engine exhaust with the telops FIRST-MWE
Author :
Bradley, Kenneth C. ; Bowen, Spencer ; Gross, Kevin C. ; Marciniak, Michael A. ; Perram, Glen P.
Author_Institution :
Air Force Inst. of Technol., Wright-Patterson Air Force Base, Dayton, OH
Abstract :
The Field-portable Imaging Radiometric Spectrometer Technology Midwave Extended (FIRST-MWE) system developed by Telops, Inc. was used to capture hyperspectral imagery of turbojet engine exhaust. The FIRST-MWE is a Michelson interferometer coupled to a 320 times 256 Indium Antimonide (InSb) focal plane array with instantaneous field of view (IFOV) of 0.35 mrad. Exhaust from a diesel-fueled Turbine Technologies, Ltd. SR-30 turbojet engine was imaged at three modes of operation from a side-plume vantage point close to the engine. Temporally-averaged spectral data featured strong CO2 emission near 2200-2450 cm-1. A simple radiative transfer model was used to produce spatially-resolved maps of the temperature and relative CO2 concentration. The model assumed an optically-thin plume that was homogeneous along each pixel´s line-of-sight. The Carbon Dioxide Spectroscopic Databank was used to compute molecular cross-sections used in fitting the temporally-averaged spectra.
Keywords :
Fourier transform spectroscopy; exhaust systems; image processing; interferometry; jet engines; mechanical engineering computing; Fourier transform spectrometry imaging; Michelson interferometer; carbon dioxide spectroscopic databank; hyperspectral imagery; indium antimonide focal plane array; instantaneous field of view; molecular cross-sections; optically-thin plume; radiative transfer model; spatially-resolved maps; temporally-averaged spectral data; turbojet engine exhaust; Fourier transforms; Hyperspectral imaging; Indium; Jet engines; Optical imaging; Radiometry; Spectroscopy; Stimulated emission; Temperature; Turbines;
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
DOI :
10.1109/AERO.2009.4839444