TWIN-CHAMBER LIQUID PROPELLANT ENGINE WITH CONTROLLED THRUST VECTOR

FIELD: engines and pumps.SUBSTANCE: in two-chamber liquid propellant engine with controlled thrust vector comprising two chambers with the possibility of oscillating in their own stabilization planes in journals and spreader bars relative to oscillation axis passing through the chamber nozzle throat...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Podgornyj Nikolaj Vasilevich, Gorokhov Viktor Dmitrievich, Fomin Valerij Mitrofanovich
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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