NASA NTRS · 19730004123
Cryogenic flow control components for rocket propulsion systems
Abstract
The 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.
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Potter, J. H.. 1972-08-01. Cryogenic flow control components for rocket propulsion systems. https://ntrs.nasa.gov/citations/19730004123
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