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Two-step rocket engine bipropellant valve PatentSolenoid two-step valve for bipropellant flow rate control to rocket engine
Document ID
19700012887
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Capps, J. E. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ferguson, R. E. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Pohl, H. O. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 5, 2013
Publication Date
January 20, 1969
Subject Category
Machine Elements And Processes
Report/Patent Number
Patent Number: US-PATENT-3,490,238
Patent Application Number: US-PATENT-APPL-SN-797057
Patent Number: NASA-CASE-XMS-04890-1
Accession Number
70N22192
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,490,238|NASA-CASE-XMS-04890-1
Patent Application
US-PATENT-APPL-SN-797057

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