CONTROL SYSTEM UNIT OF SPIN-STABILIZED MISSILE

FIELD: control systems of spin-stabilized missiles, applicable in salvo-launching projectiles. ^ SUBSTANCE: the control system unit of spin-stabilized projectile has an electronic-measuring equipment, angular displacement meter, vernier engine, current source and body components. The control devices...

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Bibliographische Detailangaben
Hauptverfasser:	PLISIN JURIJ VASIL'EVICH, DENEZHKIN GENNADIJ ALEKSEEVICH, STOLJAROV VIKTOR ALEKSANDROVICH, MAKAROVETS NIKOLAJ ALEKSANDROVICH, BELOBRAGIN VITALIJ NIKOLAEVICH, SEMILET VIKTOR VASIL'EVICH, BARYSHNIKOV BORIS PAVLOVICH, RODIONOV SERGEJ ALEKSANDROVICH
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: control systems of spin-stabilized missiles, applicable in salvo-launching projectiles. ^ SUBSTANCE: the control system unit of spin-stabilized projectile has an electronic-measuring equipment, angular displacement meter, vernier engine, current source and body components. The control devices are made in the form of self-contained structural units and positioned for installation, removal and wiring of each of them in a single direction coinciding with the longitudinal axis of the control system unit, and their longitudinal axes are matched with the unit longitudinal axis. ^ EFFECT: reduced projectile moment of inertia and, as a result, reduced forces required for control of the projectile, and easier access to the devices for servicing-repair work. ^ 1 dwg