Supercharged topping rocket propellant feed system

Power plants – Reaction motor – Electric – nuclear – or radiated energy fluid heating means

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60259, F02K 902

Patent

active

041716159

ABSTRACT:
A rocket propellant feed system utilizing a bleed turbopump to supercharge a topping turbopump. 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.

REFERENCES:
patent: 2625007 (1953-01-01), Truax
patent: 2816417 (1957-12-01), Bloomberg
patent: 3028729 (1962-04-01), Ledwith
patent: 3168807 (1965-02-01), Ledwith et al.

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