MISSILE HAVING DEPLOYMENT MECHANISM OF RETRACTABLE STABILIZERS Russian patent published in 2008 - IPC F42B10/14 

Abstract RU 2320952 C2

FIELD: missile armament, in particular, stabilizers deployed after lauding of the missile.

SUBSTANCE: the deployment mechanism automatically turns, about the hinge and deploys the stabilizer from the stowed position to the deployed position. The mechanism has a spring that produces a shifting force making the stabilizer to change the stowed position to the deployed position.

EFFECT: simplified consumption and enhanced reliability of the deployment mechanism and fixing of the stabilizers.

10 cl, 15 dwg

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RU 2 320 952 C2

Authors

Ajzentraut Rudol'F Adol'F

Kebshull Martin Allen

Parin Dzhon Kristofer

Dates

2008-03-27Published

2003-03-14Filed