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Method for continuous variation of propellant flow and thrust in propulsive devices PatentContinuous variation of propellant flow and thrust by application of liquid foam flow theory to injection orifice
Document ID
19700031051
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Morrell, G. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 5, 2013
Publication Date
July 24, 1962
Subject Category
Propulsion Systems
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-10812
Patent Number: NASA-CASE-XLE-00177
Patent Number: US-PATENT-3,045,424
Accession Number
70N40367
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-XLE-00177|US-PATENT-3,045,424
Patent Application
US-PATENT-APPL-SN-10812

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