CHAMBER OF LIQUID-PROPELLANT ROCKET ENGINE OR GAS GENERATOR WITH LASER IGNITION DEVICE OF FUEL COMPONENTS, AND ITS STARTUP METHOD

FIELD: engines and pumps.SUBSTANCE: chamber of liquid-propellant rocket engine or gas generator with laser ignition device of components includes combustion chamber with nozzle, mixing head with component supply channels and laser ignition device of fuel components, which consists of small-size lase...

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Bibliographische Detailangaben
Hauptverfasser: REBROV SERGEJ GRIGOR'EVICH, GOLUBEV VIKTOR ALEKSANDROVICH, GOLIKOV ANDREJ NIKOLAEVICH
Format: Patent
Sprache:eng ; rus
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