LIQUID PROPELLANT ROCKET ENGINE Russian patent published in 2012 - IPC F02K9/48 

Abstract RU 2450153 C1

FIELD: engines and pumps.

SUBSTANCE: proposed engine comprises chamber with nozzle head and cooling jacket, fuel pump plant with pumps and two-stage turbine fed by fuel component gasified in chamber cooling jacket. Note here that chamber between fuel pump plant turbine first and second stages is communicated with chamber nozzle head while turbine second stage outlet is communicated with pipeline feeding fuel liquid component to pump.

EFFECT: higher reliability and power output.

1 dwg

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RU 2 450 153 C1

Authors

Efimochkin Aleksandr Frolovich

Vovcharenko Konstantin Ivanovich

Dates

2012-05-10Published

2011-02-07Filed