Fin assembly for a projectile

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

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F42B 1014

Patent

active

050783378

ABSTRACT:
A fin assembly comprises a plurality of fin elements 12 each formed of flexible sheet material (e.g. cloth) which are stowed in collapsed form adjacent the aft motor nozzle and are deployed to an extended form on which they provide effective aerodynamic surfaces.

REFERENCES:
patent: Re26380 (1968-04-01), Rogallo
patent: 2666387 (1954-01-01), Richey
patent: 3188957 (1965-06-01), Petre
patent: 3369780 (1968-02-01), Wieland et al.
patent: 3430562 (1969-03-01), Sautier
patent: 4411398 (1988-10-01), Wedertz et al.
patent: 4586681 (1986-05-01), Wedertz et al.

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