Publikationsdatum:
2019-06-27
Beschreibung:
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.
Schlagwort(e):
SPACECRAFT PROPULSION AND POWER
Format:
application/pdf
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