A rocket propellant feed system utilizing a bleed turbopump to supercharge a topping turbopump is presented. The bleed turbopump is of a low pressure type to meet the cavitation requirements imposed by the propellant storage tanks. The topping turbopump is of a high pressure type and develops 60 to 70 percent of the pressure rise in the propellant.
Supercharged topping rocket propellant feed system
23.10.1979
Sonstige
Keine Angabe
Englisch
Supercharged Topping Rocket Propellant Feed System
NTIS | 1966
|Rocket propellant manometer system
Engineering Index Backfile | 1962
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