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Engine spectrometer probe and method of useThe engine spectrometer probe and method of using the same of the present invention provides a simple engine spectrometer probe which is both lightweight and rugged, allowing an exhaust plume monitoring system to be attached to a vehicle, such as the space shuttle. The engine spectrometer probe can be mounted to limit exposure to the heat and debris of the exhaust plume. The spectrometer probe 50 comprises a housing 52 having an aperture 55 and a fiber optic cable 60 having a fiber optic tip 65. The fiber optic tip 65 has an acceptance angle 87 and is coupled to the aperture 55 so that the acceptance angle 87 intersects the exhaust plume 30. The spectrometer probe can generate a spectrum signal from light in the acceptance angle 506 and the spectrum signal can be provided to a spectrometer 508.
Document ID
20080008674
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Barkhoudarian, Sarkis
Kittinger, Scott A.
Date Acquired
August 24, 2013
Publication Date
June 13, 2006
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-10/428,693
Patent Number: US-Patent-7,061,607
Funding Number(s)
CONTRACT_GRANT: NAS8-01140
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,061,607
Patent Application
US-Patent-Appl-SN-10/428,693
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