DIRECTIONAL CONTROL DEVICE FOR AIRBORNE OR SEABORNE MISSILES

摘要

A missile for airborne and seaborne use in which directional control about a flight axis comprises a nose deflectable angularly in relation to the flight axis of the body of the missile to form steering means by changing the fluid flow involved over the body, and means between the nose and the body to effect angular deflection about a universal pivoting point between the nose and the body.