Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1985-02-07
1986-06-03
Kyle, Deborah L.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
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.
Madderra Jimmy M.
Schaeffel, Jr. John A.
Bush Freddie M.
Carone Michael
Deaton James T.
Gibson Robert P.
Kyle Deborah L.
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