Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1987-06-05
1988-04-12
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
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
Boder Dieter
Primus Michael
Carone Michael J.
Jordan Charles T.
Rheinmetall GmbH
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