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Circulating head for rocket engine, has injection ports disposed with respect to each other such that addition of propellant or fuel components occurs in gaseous phase under effect of ejection of jets from one component leaving one port
Circulating head for rocket engine, has injection ports disposed with respect to each other such that addition of propellant or fuel components occurs in gaseous phase under effect of ejection of jets from one component leaving one port
The head has injection ports (3, 4) for injecting fuel or propellant jets from respective propellant or fuel components with high and low impulsions, respectively into a combustion chamber of a rocket engine. The ports are disposed with respect to each other such that addition of the components takes place in a gaseous phase under the effect of ejection of jets from one component leaving the injection port (3).
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