Guide assembly having unfoldable fins for projectiles and missil

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

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F42B 1332

Patent

active

047369094

ABSTRACT:
A guide assembly for a missile or projectile which has a plurality of space saving, foldable fins, with each such fin being composed of two fin blades that are connected together at their tips and whose root ends are fastened in different bearings. To prevent bending or bulging of the fin blades in the unfolded state of the fins, at least one bending prevention arrangement is disposed between the fin blades in the vicinity of their root ends.

REFERENCES:
patent: 2923241 (1960-02-01), House
patent: 3103886 (1963-09-01), Popenoe
patent: 3360216 (1967-12-01), Schwesig

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