Steerable Projectile

• US 20110101154A1
• Filed: 03/11/2009
• Published: 05/05/2011
• Est. Priority Date: 03/13/2008
• Status: Active Grant

• Current Assignee: Thales Holdings UK Plc (Thales SA)
• Original Assignee: Thales Holdings UK Plc (Thales SA)
• Inventors: Mallon, Paddy
• Granted Patent: US 8,716,639 B2
• Time in Patent Office: Days
• US Class Current: 244/3.11
• CPC Class Codes: F42B 10/46 Streamlined nose cones; Windshields; Radomes F42B12/105 takes precedence
• CPC Class Codes: F42B 10/52 Nose cones
• CPC Class Codes: F42B 10/62 Steering by movement of flight surfaces

Abstract

A steerable projectile (30) comprises a body portion (32) and a nose portion (34). The nose portion and body portion are substantially coaxially arranged and rotatable relative to one another about their co-axis. The nose portion further comprises an asymmetric formation (36) operable to enable the projectile to be subjected to off-axis drag during flight.

Claims

1. A steerable projectile comprising a body portion and a nose portion, the nose portion and the body portion being substantially coaxially arranged along a co-axis and rotatable relative to one another about said co-axis, the nose portion further comprising an asymmetric formation operable to enable said projectile to be subjected to off-axis drag during flight, wherein said asymmetric formation comprises one or more active surfaces, each active surface being defined on a projection substantially radially projecting from said nose but not beyond the radial extent of said body portion, and each active surface being defined so as to cause the imparting of a drag component on said projectile wherein the drag component is perpendicular to the trajectory of said projectile.

2. A projectile in accordance with claim 1 wherein the body portion is substantially cylindrical and the nose portion is, but for the asymmetric formation, substantially rotationally symmetrical and coaxial with the body portion.

3. A projectile in accordance with claim 1 wherein said nose portion is substantially semi-ellipsoidal in shape, but for said asymmetric formation.

4. A projectile in accordance with claim 1 and comprising rotation means operable to cause relative rotation of said nose portion with respect to said body portion.

5. A projectile in accordance with claim 4 and comprising orientation monitoring means operable to determine orientation of said nose portion with respect to an external reference frame, and control means operable to control rotation of said nose portion with respect to said body portion.

6. A projectile in accordance with claim 5 wherein said control means is operable to cause said rotation means to rotate said nose portion such that said nose portion is rotationally stationary with respect to said reference frame.

7. A projectile in accordance with claim 5 wherein said control means is operable to cause said rotation means to rotate said nose portion such that said asymmetric formation causes an off-axis steering force to be imparted on said projectile.

8. A projectile in accordance with claim 5 and including communication means operable to receive a guidance signal, and wherein said control means is operable to cause said rotation means to rotate said nose portion in response to said guidance signal.

9. A projectile in accordance with claim 2 wherein said nose portion is substantially semi-ellipsoidal in shape, but for said asymmetric formation.

10. A projectile in accordance with claim 2 and comprising rotation means operable to cause relative rotation of said nose portion with respect to said body portion.

11. A projectile in accordance with claim 3 and comprising rotation means operable to cause relative rotation of said nose portion with respect to said body portion.

12. A projectile in accordance with claim 9 and comprising rotation means operable to cause relative rotation of said nose portion with respect to said body portion.

13. A projectile in accordance with claim 10 and comprising orientation monitoring means operable to determine orientation of said nose portion with respect to an external reference frame, and control means operable to control rotation of said nose portion with respect to said body portion.

14. A projectile in accordance with claim 11 and comprising orientation monitoring means operable to determine orientation of said nose portion with respect to an external reference frame, and control means operable to control rotation of said nose portion with respect to said body portion.

15. A projectile in accordance with claim 12 and comprising orientation monitoring means operable to determine orientation of said nose portion with respect to an external reference frame, and control means operable to control rotation of said nose portion with respect to said body portion.

16. A projectile in accordance with claim 13 wherein said control means is operable to cause said rotation means to rotate said nose portion such that said nose portion is rotationally stationary with respect to said reference frame.

17. A projectile in accordance with claim 14 wherein said control means is operable to cause said rotation means to rotate said nose portion such that said nose portion is rotationally stationary with respect to said reference frame.

18. A projectile in accordance with claim 6 wherein said control means is operable to cause said rotation means to rotate said nose portion such that said asymmetric formation causes an off-axis steering force to be imparted on said projectile.

19. A projectile in accordance with claim 6 and including communication means operable to receive a guidance signal, and wherein said control means is operable to cause said rotation means to rotate said nose portion in response to said guidance signal.

20. A projectile in accordance with any claim 7 and including communication means operable to receive a guidance signal, and wherein said control means is operable to cause said rotation means to rotate said nose portion in response to said guidance signal.