CONTROLLABLE LIQUID-PROPELLANT MULTI-CHAMBER ROCKET VEHICLE

rocketry. SUBSTANCE: proposed rocket vehicle has case with oxidizer and fuel tanks, power plant consisting of several reaction chambers, single-axle articulated suspensions for mounting the chambers on rocket vehicle for their turn required for control of flight and servo units for performing such t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	PRISHCHEPA V.I, BAKHMUTOV A.A, BUKANOV V.T, KLEPIKOV I.A
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:	rocketry. SUBSTANCE: proposed rocket vehicle has case with oxidizer and fuel tanks, power plant consisting of several reaction chambers, single-axle articulated suspensions for mounting the chambers on rocket vehicle for their turn required for control of flight and servo units for performing such turns. Axle of articulated suspension is perpendicular to plane passing through longitudinal axes of vehicle and respective chamber, thus ensuring control of flight in pitch and yaw. Vehicle is provided with reaction nozzles for roll control. EFFECT: possibility of performing controllable flight at partial disconnection of reaction chambers. 2 dwg