Pressure pump and injector valve system for liquid-propellant en

Power plants – Reaction motor – Liquid oxidizer

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Details

60259, 417417, 417493, F02K 900

Patent

active

046961607

ABSTRACT:
A liquid-propellant delivery system using low-pressure propellant storage tanks instead of heavier high-pressure tanks. Liquid propellant material is pumped from the low-pressure tanks by a solenoid-actuated high-pressure pump, and delivered to the rocket engine through a pressure-actuated injector valve.

REFERENCES:
patent: 2547174 (1951-04-01), Rogers
patent: 2995008 (1961-08-01), Fox
patent: 3088406 (1963-05-01), Horner
patent: 3348488 (1967-10-01), Wolff
patent: 3408816 (1968-11-01), Stein
patent: 3709639 (1973-01-01), Suda et al.
patent: 3742701 (1943-07-01), Feemster et al.
patent: 3769879 (1973-11-01), Lofquist, Jr.
patent: 4036192 (1977-07-01), Nakayama

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