초록 ▼

An apparatus for changing the flight path of a missile is disclosed. The apparatus comprises the tip of the missile which is installed so as to be pivotable in the nose of the missile and at least one actuator to tilt the pivotable nose cone. One end of the actuator is coupled to the internal outer

An apparatus for changing the flight path of a missile is disclosed. The apparatus comprises the tip of the missile which is installed so as to be pivotable in the nose of the missile and at least one actuator to tilt the pivotable nose cone. One end of the actuator is coupled to the internal outer edge of the nose cone and the other end of the actuator is coupled internally within the main missile body. The outer wall of the forward part of the missile additionally contains at least one annular flexible element extending perpendicularly to the axis of the missile body which facilitates the tilting of the nose cone.

대표청구항 ▼

Apparatus for changing the flight path of a missile having a main body and a forward missile body structure coupled ahead of the main body comprising: nose cone means coupled to the forward missile body structure and capable of pivoting in at least one plane; actuator means coupled to the main body

Apparatus for changing the flight path of a missile having a main body and a forward missile body structure coupled ahead of the main body comprising: nose cone means coupled to the forward missile body structure and capable of pivoting in at least one plane; actuator means coupled to the main body and to the nose cone means, capable of tilting the nose cone means about the at least one plane; and a plurality of annular flexible element means located between the nose cone means and the main body and being disposed at spaced intervals in the forward missile body structure to allow deformation of said forward missile body structure upon tilting of said nose cone means.