04588146 is referenced by 15 patents and cites 3 patents.

This invention disclosure describes a wing concept which can be folded al two axes. In the folded configuration, the semi-span of the wing lies parallel to the centerline of the missile fuselage. At deployment, the wing rotates about an axis parallel to the missile centerline. A second rotation follows when the wing's semi-span is made perpendicular to the missile's centerline. Finally the wing is locked into place and the deployed flight configuration is assumed.

Title
Biaxial folding lever wing
Application Number
6/594658
Publication Number
4588146
Application Date
March 29, 1984
Publication Date
May 13, 1986
Inventor
Ronald L West
Huntsville
AL, US
Jimmy M Madderra
Huntsville
AL, US
John A Schaeffel Jr
Cullman
AL, US
Agent
Harold W Hilton
Robert P Gibson
Anthony T Lane
Assignee
The United States of America represented by the Secretary of the Army
DC, US
IPC
F42B 13/32
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