Detachable aerodynamic missile stabilizing system

摘要

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.