CHAMBER OF LIQUID-PROPELLANT ROCKET ENGINE Russian patent published in 2003 - IPC

Abstract RU 2204731 C2

FIELD: rocketry. SUBSTANCE: proposed chamber of liquid-propellant rocket engine contains combustion chamber, injector assembly with valves, propellant components delivery channels and manifolds with spray nozzles. Propellant components delivery channels are made in valves, with propellant manifolds being fitted at their outlet. Axes of spray nozzles of propellant manifolds intersect ring groove made on wall of combustion chamber. EFFECT: improved dynamic characteristics of engine, facilitated modification of engine. 2 cl, 2 dwg

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RU 2 204 731 C2

Authors

Ivanov V.N.

Dates

2003-05-20—Published

1999-03-09—Filed