| Patent Number |
Title Of Patent |
Date Issued |
| 5657947 |
Precision guidance system for aircraft launched bombs |
August 19, 1997 |
| The disclosure relates to a low cost and highly accurate precision guided system suitable for use in conventional aircraft launched bombs. The system includes a kit mounted upon the nose of the conventional bomb which replaces the conventional fuse disposed in a fuse well, the kit includ |
| 5507452 |
Precision guidance system for aircraft launched bombs |
April 16, 1996 |
| The disclosure relates to a low cost and highly accurate precision guided system suitable for use in conventional aircraft launched bombs. The system includes a kit mounted upon the nose of the conventional bomb which replaces the conventional fuse disposed in a fuse well, the kit includ |
| 5456429 |
Thrust maneuver system |
October 10, 1995 |
| A thrust maneuver system for steerable vehicles comprising a plurality of thrusters of varying impulsive force, some of which provide a base force, and others varying multiples of the base force. The forces may be used additively or subtractively to obtain a desired force for any given |
| 4808999 |
Towed decoy with fiber optic link |
February 28, 1989 |
| A rf decoy for use with rf repeater devices, transponders, noise jammers and other jamming devices. The decoy is adapted to be towed behind an aircraft using a tow line which incorporates a fiber optic link through which signals are transmitted. The device is excited through rf energy |
| 4423505 |
Cued adaptive canceller |
December 27, 1983 |
| An adaptive canceller construction for cancelling signals received by a radio receiver operating in close proximity to a transmitter having means for extending the usefulness of the device over a wide band of frequencies. The canceller is provided with a memory which will remember th |
