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Water cooled static pressure probeAn improved static pressure probe containing a water cooling mechanism is disclosed. This probe has a hollow interior containing a central coolant tube and multiple individual pressure measurement tubes connected to holes placed on the exterior. Coolant from the central tube symmetrically immerses the interior of the probe, allowing it to sustain high temperature (in the region of 2500 F) supersonic jet flow indefinitely, while still recording accurate pressure data. The coolant exits the probe body by way of a reservoir attached to the aft of the probe. The pressure measurement tubes are joined to a single, larger manifold in the reservoir. This manifold is attached to a pressure transducer that records the average static pressure.
Document ID
19920012343
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Lagen, Nicholas T.
(NASA Langley Research Center Hampton, VA, United States)
Eves, John W.
(NASA Langley Research Center Hampton, VA, United States)
Reece, Garland D.
(NASA Langley Research Center Hampton, VA, United States)
Geissinger, Steve L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
December 31, 1991
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-575695
Patent Number: NASA-CASE-LAR-14340-1-CU
Patent Number: US-PATENT-5,076,103
Accession Number
92N21586
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-14340-1-CU|US-PATENT-5,076,103
Patent Application
US-PATENT-APPL-SN-575695
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