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
1972-08-01
Miscellaneous
No indication
English
METHOD OF PREPARING ROCKET FUEL COMPONENTS FOR REFUELING ROCKET PROPULSION SYSTEMS
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