ROCKET SOLID-PROPELLANT POWER PLANT

FIELD: rocket manufacturing. ^ SUBSTANCE: rocket solid-propellant power plant incorporates the previous and subsequent stage engines with combustion chambers separated by a common bottom and a subsequent stage engine hinged nozzle moved into the combustion chamber and provided with a steering gear....

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	SOKOLOVSKIJ MIKHAIL IVANOVICH, ZARITSKIJ VLADIMIR IGNAT'EVICH, MAKAREVICH JURIJ LEONIDOVICH
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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Beschreibung
Zusammenfassung:	FIELD: rocket manufacturing. ^ SUBSTANCE: rocket solid-propellant power plant incorporates the previous and subsequent stage engines with combustion chambers separated by a common bottom and a subsequent stage engine hinged nozzle moved into the combustion chamber and provided with a steering gear. The previous stage combustion chamber accommodates, right behind the hinged nozzle and with a gap, a stationary mouth. The latter is coupled to the common bottom by a shell to form a closed space between the said shell and the hinged nozzle walls to accommodate a steering gear. The said stationary mouth is designed so that with hinged nozzle departed by a maximum angle the said nozzle outlet section does not beyond the stationary mouth inlet section. ^ EFFECT: higher reliability of the power plant ensured by the steering gear thermal protection. ^ 1 dwg