Counter-rotating folding wings

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

Patent

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Details

244 329, F42B 1332

Patent

active

045925259

ABSTRACT:
A missile which has folding wings at opposite side of the missile and exting longitudinally of the missile for allowing high density packaging of the missile in a launcher or container and the folding wings are deployed after the missile is ejected from a launcher or otherwise extended to a launch position to provide a cruciformed shaped wing structure about said missile for accurate guidance thereof.

REFERENCES:
patent: 3711040 (1973-01-01), Carver
patent: 4453426 (1984-06-01), Groutage et al.

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