MISSILE CONTROL SYSTEM AND METHOD

Details for Australian Patent Application No. 2003291229 (hide)

Owner RAYTHEON COMPANY

Inventors CHASMAN, Daniel; HAIGHT, Stephen, D.; FACCIANO, Andrew, B.

Pub. Number AU-A-2003291229

PCT Number PCT/US2003/0352

PCT Pub. Number WO2004/044519

Priority 10/289,651 07.11.02 US

Filing date 3 November 2003

Wipo publication date 3 June 2004

International Classifications

F42B 010/66 Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles

F42B 010/64 Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles

Event Publications

8 April 2004 Complete Application Filed

  Priority application(s): 10/289,651 07.11.02 US

8 July 2004 Application Open to Public Inspection

  Published as AU-A-2003291229

21 July 2005 Application Lapsed, Refused Or Withdrawn, Patent Ceased or Expired

  This application lapsed under section 142(2)(f)/See Reg. 8.3(3). Examination has not yet been requested or directed for this application. Note that applications or patents shown as lapsed or ceased may be restored at a later date.

Legal

The information provided by the Site not in the nature of legal or other professional advice. The information provided by the Site is derived from third parties and may contain errors. You must make your own enquiries and seek independent advice from the relevant industry professionals before acting or relying on any information contained herein. Check the above data against the Australian Patent Office AUSPAT database.

Next and Previous Patents/Applications

2003291230-HIGH CALIPER WEB AND WEBMAKING BELT FOR PRODUCING THE SAME

2003291228-APPARATUS FOR DIVERTING SUCCESSIVE ARTICLES IN A SINGLE LANE TO PLURAL LANES