LIQUID ROCKET ENGINE WITH BAFFLE AT NOZZLE SECTION

FIELD: engines and pumps.SUBSTANCE: invention relates to control thrust vector of liquid propellant engine (LPE). Liquid-propellant engine includes chamber with cooled supersonic nozzle part, uncooled nozzle from carbon-carbon composite material, control units and a frame, external surface of an unc...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GOROKHOV VIKTOR DMITRIEVICH, KHRISANFOV SERGEJ PETROVICH, FEDOROV SERGEJ ANATOLEVICH, KAFARENA PAVEL VIKTOROVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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