Patent ID: 7185846
Filing Date: 2007-03-06
Classification: F42B

Abstract:
1. Asymmetrical control surface system for an air vehicle, the air vehicle having a horizontal midplane axis, a controlling computer, vertical tails and further being stowable in and launchable from a tube, said asymmetrical control surface system comprising: a plurality of stowable wings, said wings being deployable upon launch of the air vehicle from the tube, at least one of said wings being movably attached to the vehicle above said midplane axis and at least one of said wings being movably attached to the vehicle below said midplane axis; a plurality of horizontal tails, at least one of said horizontal tails being movably attached to the vehicle above said midplane axis and at least one of said horizontal tails being movably attached to the vehicle below said midplane axis; and a means to deploy said wings and horizontal tails in response to the controlling computer.