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Rocket engine injector PatentRocket engine injector orifice to accommodate changes in density, velocity, and pressure, thereby maintaining constant mass flow rate of propellant into rocket combustion chamber
Document ID
19710015260
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Stein, S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
November 5, 1968
Subject Category
Propulsion Systems
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-591014
Patent Number: US-PATENT-3,408,816
Patent Number: NASA-CASE-XLE-03157
Accession Number
71N24736
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,408,816|NASA-CASE-XLE-03157
Patent Application
US-PATENT-APPL-SN-591014

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