A guided projectile includes a body and a deployable wing in which the deployable wing is coupled to and enclosed by the body. A linear distance from the leading edge to the trailing edge of the wing defines a chord line that, in the stowed position, forms an angle with a plane containing the chord line and extending parallel to a longitudinal dimension of the wing in a deployed position.
Space saving wing stowage
2020-12-09
Patent
Elektronische Ressource
Englisch
Variable Incidence Wing Aircraft having a Wing Stowage Mode
Europäisches Patentamt | 2023
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