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On-board Optical Spectrometry for Detection of Mixture Ratio and Eroded Materials in Rocket Engine Exhaust PlumeOptical spectrometry can provide means to characterize rocket engine exhaust plume impurities due to eroded materials, as well as combustion mixture ratio without any interference with plume. Fiberoptic probes and cables were designed, fabricated and installed on Space Shuttle Main Engines (SSME), allowing monitoring of the plume spectra in real time with a Commercial of the Shelf (COTS) fiberoptic spectrometer, located in a test-stand control room. The probes and the cables survived the harsh engine environments for numerous hot-fire tests. When the plume was seeded with a nickel alloy powder, the spectrometer was able to successfully detect all the metallic and OH radical spectra from 300 to 800 nanometers.
Document ID
20070013796
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Barkhoudarian, Sarkis
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Kittinger, Scott
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: JANNAF Conference
Location: San Diego, CA
Country: United States
Start Date: December 4, 2006
End Date: December 8, 2006
Sponsors: Department of the Air Force, NASA Headquarters, Department of the Navy, Department of the Army
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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