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Thermal flux transfer systemA thermal flux transfer system for use in maintaining the thrust chamber of an operative reaction motor at given temperatures is described. The system is characterized by an hermetically sealed chamber surrounding a thrust chamber to be cooled, with a plurality of parallel, longitudinally spaced, disk-shaped wick members formed of a metallic mesh and employed in delivering a working fluid, in its liquid state, radially toward the thrust chamber and delivering the working fluid, in its vapor state, away from the nozzle for effecting a cooling of the nozzle, in accordance with known principles of an operating heat pipe.
Document ID
19730023873
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Freggens, R. A.
(Radio Corp. of America Princeton, NJ, United States)
Date Acquired
September 2, 2013
Publication Date
September 18, 1973
Subject Category
Propulsion Systems
Report/Patent Number
Patent Number: NASA-CASE-NPO-12070-1
Patent Application Number: US-PATENT-APPL-SN-153542
Patent Number: US-PATENT-3,759,443
Accession Number
73N32606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-12070-1|US-PATENT-3,759,443
Patent Application
US-PATENT-APPL-SN-153542
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