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.
Cryogenic flow control components for rocket propulsion systems
01.08.1972
Sonstige
Keine Angabe
Englisch
METHOD OF PREPARING ROCKET FUEL COMPONENTS FOR REFUELING ROCKET PROPULSION SYSTEMS
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