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Thrust vector control apparatus PatentThrust vector control by secondary injection of fluid into rocket nozzle flow field to separate exhaust flow
Document ID
19700024978
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Conrad, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 5, 2013
Publication Date
May 12, 1964
Subject Category
Propulsion Systems
Report/Patent Number
Patent Number: US-PATENT-3,132,476
Patent Number: NASA-CASE-XLE-00208
Patent Application Number: US-PATENT-APPL-SN-106135
Accession Number
70N34294
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,132,476|NASA-CASE-XLE-00208
Patent Application
US-PATENT-APPL-SN-106135

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