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Cryogenic flow control components for rocket propulsion systemsThe design of cryogenic flow control components, specifically the prevalve, for the Saturn 5 vehicle is discussed. Design systems are assessed and component requirements revealed significant improvements in mass flow rate, temperature, and pressure.
Document ID
19730004123
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Potter, J. H. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 7, 2013
Publication Date
August 1, 1972
Publication Information
Publication: Res. Achievements Rev., Vol. 4, No. 6
Subject Category
Propellants
Accession Number
73N12850
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19730004113Collected WorksResearch Achievements Review, volume 4, no. 6: Chemical propulsion research at MSFC
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