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| Application No. | Application Title | Issue Date |
| 20100237186 | DRAG-STABILIZED WATER-ENTRY PROJECTILE AND CARTRIDGE ASSEMBLY A drag-stabilized water-entry projectile having a projectile body, one or more drag-stabilizing elements, such as fins, flares or canards, and one or more attachment members adapted to hold the one or more drag-stabilizing elements to the projectile body. The one or mor... | 09/23/2010 |
| 20100219285 | DETACHABLE AERODYNAMIC MISSILE STABILIZING SYSTEM Provided is a detachable aerodynamic missile stabilizing system for a missile flying at low flight speeds. The system includes a housing adapted to couple to couple to the missile. Extending outward from the housing is at least one grid fin. Specifically the grid fin ex... | 09/02/2010 |
| 20100032515 | FUZE GUIDANCE SYSTEM WITH MULTIPLE CALIBER CAPABILITY A fuze guidance system is configurable by an end user, allowing the end user to select between different configurations of canards of the system. The different configurations of canards may include canards with different surface areas, optimized for providing appropriat... | 02/11/2010 |
| 20070102568 | Ejectable aerodynamic stability and control The disclosed system and method for improving aerodynamic stability of aeronautic vehicles generally includes an ejectable grid fin adapted for releasable engagement with aeronautic vehicles. The grid fin is generally configured to optimize the flight performance charac... | 05/10/2007 |
| 20070075183 | Wing arrangement as well as a missile A wing arrangement (10), which can be pushed onto a structure, such as a missile, and which includes a number of tubular segments (14) and a number of wings (16) which are arranged on the tubular segments (14). In order to allow the wing arra... | 04/05/2007 |
