SPIN-STABILIZED MISSILE WITH ELECTRIC CONTROL ACTUATOR

FIELD: armament. ^ SUBSTANCE: spin-stabilized missile (1) with an electric control actuator has electric motor (2), reduction gear (5), command driver (10), electronic power amplifier (11), feedback potentiometer (9), correcting feedback circuit and control surfaces (7). Rotor (12) of electric motor...

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Bibliographische Detailangaben
Hauptverfasser:	VLASOV BORIS VIKTOROVICH, ZHAROV JURIJ NIKOLAEVICH, KORNEEV ALEKSEJ BORISOVICH, MAJOROV VALERIJ VLADIMIROVICH, MAMATKAZIN IBRAGIM KHAMIDOVICH, BELOV ALEKSANDR NIKOLAEVICH, KOLEDOV ALEKSANDR SERGEEVICH, MARTSINKEVICH EVGENIJ VLADIMIROVICH, CHUBAR' ANATOLIJ FEDOROVICH, GORJUNOV IGOR' FEDOROVICH, SERBENJUK NIKOLAJ AVKSENT'EVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: armament. ^ SUBSTANCE: spin-stabilized missile (1) with an electric control actuator has electric motor (2), reduction gear (5), command driver (10), electronic power amplifier (11), feedback potentiometer (9), correcting feedback circuit and control surfaces (7). Rotor (12) of electric motor (2) is installed in stator (13) for retention in one of its extreme positions by means of magnetic forces, displacement by the value of damping relative to stator (13) and engagement in its other extreme position with additionally adjusted supports (14) fastened on frame (15) of electric motor (2). ^ EFFECT: improved dynamic characteristics of missile. ^ 5 cl, 3 dwg