METHOD FOR PROTECTION OF SENSING ELEMENTS OF GUIDED MISSILE ROLL GYROSCOPE FROM ACTION OF LAUNCH G-LOADS, GUIDED MISSILE FOR ITS REALIZATION AND METHOD FOR ITS ASSEMBLY

摘要

FIELD: guide missiles that are launched from the gun barrel and designed for destruction of ground armored targets.;SUBSTANCE: the method consists in the fact the action of launch g-loads is preliminarily compensated by the counter force of tightening of the sensing elements of the roll gyroscope. The gyroscope sensing elements are positioned with a shift from the missile longitudinal axis. The expansion clearances between the interrelated sensing elements of the gyroscope are adjusted by radial insertion of the sensing elements in the gyroscope for displacement both along the missile axis and in the direction of its spinning at adjustment of the gyroscope relative to the control actuator. The roll-stabilized missile launched from the gun and the method for its assembly realize the described method for protection of the sensing elements of the roll gyroscope.;EFFECT: provided serviceability of the missile at an action of considerable (up to 6000 units) of launch g-loads, enhanced reliability of operation and simplified construction.;3 cl, 6 dwg