Restraining mechanism

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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F41G 726

Patent

active

049384341

ABSTRACT:
A restraining mechanism for a gimbal in a gyroscopically-stabilized seeker in a cannon-launched projectile is shown to consist of a movable latch, so shaped and disposed that relative longitudinal motion between the gimbal and the body of such projectile is prevented during the launching phase, and a release mechanism whereby the movable latch is cleared of the gimbal after the launching phase.

REFERENCES:
patent: 2963973 (1960-12-01), Estey
patent: 4155521 (1979-05-01), Evans et al.
patent: 4267988 (1981-05-01), Rodgers

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