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Linear Spectral Analysis of Plume Emissions Using an Optical Matrix ProcessorPlume spectrometry provides a means to monitor the health of a burning rocket engine, and optical matrix processors provide a means to analyze the plume spectra in real time. By observing the spectrum of the exhaust plume of a rocket engine, researchers have detected anomalous behavior of the engine and have even determined the failure of some equipment before it would normally have been noticed. The spectrum of the plume is analyzed by isolating information in the spectrum about the various materials present to estimate what materials are being burned in the engine. Scientists at the Marshall Space Flight Center (MSFC) have implemented a high resolution spectrometer to discriminate the spectral peaks of the many species present in the plume. Researchers at the Stennis Space Center Demonstration Testbed Facility (DTF) have implemented a high resolution spectrometer observing a 1200-lb. thrust engine. At this facility, known concentrations of contaminants can be introduced into the burn, allowing for the confirmation of diagnostic algorithms. While the high resolution of the measured spectra has allowed greatly increased insight into the functioning of the engine, the large data flows generated limit the ability to perform real-time processing. The use of an optical matrix processor and the linear analysis technique described below may allow for the detailed real-time analysis of the engine's health. A small optical matrix processor can perform the required mathematical analysis both quicker and with less energy than a large electronic computer dedicated to the same spectral analysis routine.
Document ID
19970022765
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Gary, C. K.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1992
Publication Information
Publisher: University of Cincinnati
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-112466
NAS 1.15:112466
Meeting Information
Meeting: Space System Health Management Technology
Location: Cincinnati, OH
Country: United States
Start Date: November 17, 1992
End Date: November 18, 1992
Accession Number
97N72145
Distribution Limits
Public
Copyright
Public Use Permitted.
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