Spiralling missile—B

A missile with a missile attachment, which said missile attachment consists of a tube with a protruding section, which said protruding section protrudes outward from the tube, and which said protruding section has a forward facing surface area, with the said tube attached to the missile such that a part of the said missile is encircled by the said tube and such that the said tube is able to rotate relative to the part of the missile that is encircled by the tube, with the tube able to achieve continuous rotation relative to the missile during flight of the missile due to impact between the forward facing surface area and air during flight of the missile, and which said missile has a friction inducing attachment, which said friction inducing attachment is attached to the missile, which friction inducing attachment has a moveable component and an actuating mechanism, and which moveable component can be moved by the actuating mechanism relative to the missile such that the moveable component can be moved towards the tube by the actuating mechanism and such that a continuous rubbing action can occur between the moveable component and the tube, thereby creating friction between the said moveable component and the said tube during flight of the missile such that with friction the friction inducing attachment can allow the tube to continue to rotate relative to the encircled part of the missile but restrict rotation of the tube relative to the encircled part of the missile to a rate of rotation that is lower than a rate of rotation that the tube could achieve relative to the encircled part of the missile if the moveable component was not moved towards the tube.

A missile with a missile attachment, which said missile attachment consists of a tube with a protruding section, which said protruding section protrudes outward from the tube, with the said tube attached to the missile such that a part of the said missile is encircled by the said tube and such that the said tube is able to rotate relative to the part of the missile that is encircled by the tube, with the tube able to achieve continuous rotation relative to the missile during flight of the missile due to impact between the protruding section and air during flight of the missile, and which said missile has a friction inducing attachment, which said friction inducing attachment is attached to the missile and which said friction inducing attachment has a moveable component and an actuating mechanism, and which moveable component can be moved by the actuating mechanism relative to the missile such that the moveable component can be moved towards the tube by the actuating mechanism and such that a continuous rubbing action can occur between the moveable component and the tube, thereby creating friction between the said moveable component and the said tube during flight of the missile such that with friction the friction inducing attachment can allow the tube to continue to rotate relative to the encircled part of the missile but restrict rotation of the tube relative to the encircled part of the missile to a rate of rotation that is lower than a rate of rotation that the tube could achieve if the moveable component was not moved towards the tube.

A missile with a missile attachment, which said missile attachment consists of a tube with an externally protruding section and an internally protruding section, with the said externally protruding section protruding outward from the tube, and the internally protruding section protruding inwardly of the tube, and which said externally protruding section has a forward facing surface area, with the said tube attached to the missile such that a part of the said missile is encircled by the said tube and such that the said tube is able to rotate relative to the part of the missile that is encircled by the tube, with the tube able to achieve continuous rotation relative to the missile during flight of the missile due to impact between the forward facing surface area and air during flight of the missile, and which said missile has a friction inducing attachment, which said friction inducing attachment is attached to the missile and which friction inducing attachment has a moveable component and an actuating mechanism, and which moveable component can be moved by the actuating mechanism relative to the missile such that the moveable component can be moved towards the internally protruding section of the said tube such that a continuous rubbing action can occur between the moveable component and the internally protruding section of the tube, thereby creating friction between the moveable component and the internally protruding section of the tube such that with frictional force the friction inducing attachment can allow the tube to continue to rotate relative to the encircled part of the missile but restrict rotation of the tube relative to the encirlced part of the missile to a rate of rotation that is lower than a rate of rotation that the tube could achieve relative to the encircled part of missile if the moveable component was not moved towards the internally protruding section of the tube.

A missile with a missile attachment, which said missile attachment consists of a tube with an externally protruding section and an internally protruding section, with the said externally protruding section protruding outward from the tube, and the internally protruding section protruding inwardly of the tube, and with the said tube attached to the missile such that a part of the said missile is encircled by the said tube and such that the said tube is able to rotate relative to the part of the missile that is encircled by the tube, with the tube able to achieve continuous rotation relative to the missile during flight of the missile due to impact between the externally protruding section and air during flight of the missile, and which said missile has a friction inducing attachment, which said friction inducing attachment is attached to the missile and which friction inducing attachment has a moveable component and an actuating mechanism, and which moveable component can be moved by the actuating mechanism relative to the missile such that the moveable component can be moved towards the internally protruding section of the said tube such that a continuous rubbing action can occur between the moveable component and the internally protruding section of the tube, thereby creating friction between the moveable component and the internally protruding section of the tube such that with frictional force the friction inducing attachment can allow the tube to rotate relative to the encirlced part of the missile but restrict rotation of the tube relative to the encircled part of the missile to a rate of rotation that is lower than a rate of rotation that the tube could achieve relative to the encirlced part of the missile if the moveable component was not moved towards the internally protruding section of the tube.