Tripropellant rocket engine with injector

Details Tripropellant rocket engine with injector Tripropellant rocket engine with injector

1986-10-20

1988-09-20

Casaregola, Louis J.

Power plants

Reaction motor

Liquid oxidizer

60259, 60 39463, 60742, 2394193, 239424, F02K 900, F02K 942, F02K 972

Patent

active

047715995

ABSTRACT:
Fuel for a rocket engine consisting of hydrogen, oxygen and a hydrocarbon is admitted into the combustion zone through an injector whereby the hydrogen and hydrocarbon components are either pre-mixed in the injector or independently delivered and the oxygen is always independently delivered into the combustion zone.

REFERENCES:
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patent: 2667740 (1954-02-01), Goddard
patent: 3390528 (1968-07-01), Howell et al.
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patent: 3534909 (1970-10-01), Paine
patent: 3581495 (1971-06-01), Kah, Jr.
patent: 3625435 (1971-12-01), Mitchell et al.
patent: 3662547 (1972-05-01), Paine et al.
patent: 3802193 (1974-04-01), Wong
patent: 3863443 (1975-02-01), Chamberlain
patent: 3910037 (1975-10-01), Salkeld
patent: 3937011 (1976-02-01), Caruel et al.
patent: 4220001 (1980-09-01), Beichel
patent: 4327547 (1982-05-01), Hughes et al.

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