FIELD: engines and pumps.
SUBSTANCE: invention relates to jet machinery. Liquid-propellant engine comprises engine chamber, turbine, fuel pump and jet pre-pump and differs from known designs in that jet pre-pump injection nozzle communicates with turbine inlet or outlet or with chamber cooling circuit.
EFFECT: higher efficiency of jet pre-pumps.
3 dwg
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LIQUID PROPELLANT ROCKET ENGINE | 2014 |
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Authors
Dates
2014-02-10—Published
2012-05-22—Filed