Detachable aerodynamic missile stabilizing system

F - Mech Eng,Light,Heat,Weapons – 42 – B

Patent

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Details

F42B 10/26 (2006.01) F42B 10/02 (2006.01)

Patent

CA 2670325

Provided is a detachable aerodynamic missile stabilizing system (130) for a missile (100) flying at low flight speeds. The system (130) includes a housing (134) adapted to couple to the missile (100). Extending outward from the housing (134) is at least one grid fin (136). Specifically the grid fin (136) extends from the housing (134) such that it is transverse to a longitudinal axis (110) of the housing (134) and the missile (100). The grid fin (136) provides a plurality of apertures (144). The apertures (144) are parallel to the longitudinal axis (110) of the housing (134) and the missile (100). A coupler (138) is adapted to detachably couple the housing (134) to the missile (100). A method of use is also provided.

L'invention concerne un système de stabilisation de missile aérodynamique détachable (130) destiné à un missile (100) volant à des vitesses de vol lentes. Le système (130) comprend un boîtier (134) adapté pour être couplé au missile (100). Au moins un empennage en treillis (136) s'étend vers l'extérieur depuis le boîtier (134). De manière spécifique, l'ailette de grille (136) s'étend depuis le boîtier (134) de telle sorte qu'il est transversal à un axe longitudinal (110) du boîtier (134) et au missile (100). L'empennage en treillis (136) fournit une pluralité d'ouvertures (144). Les ouvertures (144) sont parallèles à l'axe longitudinal (110) du boîtier (134) et au missile (100). Un dispositif de couplage (138) est adapté pour coupler le boîtier (134) au missile (100) de manière amovible. Un procédé d'utilisation est également fourni.

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