| 摘要 |
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 |
