GUIDED MISSILE ACTUATOR ASSEMBLY Russian patent published in 1998 - IPC

Abstract RU 2101667 C1

FIELD: defence equipment, applicable in design development of guided missiles. SUBSTANCE: actuator assembly improves the dynamic characteristics of the actuator assembly by increasing the developed torque due to spacing of the hinge axes of each pair of control surfaces along the missile longitudinal axis at a distance of not more than 0.4 of the caliber of the control actuator compartment, arrangement of the actuators on different sides of the control - surface hinge axes. EFFECT: improved dynamic characteristics. 2 dwg

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RU 2 101 667 C1

Authors

Zybin I.M.

Fimushkin V.S.

Golovanov N.S.

Dates

1998-01-10—Published

1996-10-01—Filed