DIRECTIONAL WARHEAD FUZE
Assignee
Raytheon
Filed as: RAYTHEON COMPANY, A DE CORP.
Filed
Sep 19, 1990
Granted
Nov 1, 1994
Location
CHELMSFORD MA US
Abstract
A directional ordnance for a missile. The missile contains circuitry to determine the direction of a target relative to the missile and to selectively detonate directing charges to force the blast from the warhead towards the target. The circuitry for determining the direction of the target includes two transmit antennas, each transmitting a different pseudo noise sequence, and two receive antennas; each coupled to a receiver which can determine the level of each pseudo noise sequence at each receive antenna. The relative strengths of the different pseudo noise sequences tell the direction of the target relative to the transmit and receive antennas.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 9, 1991
Rescinded
May 19, 1994
Duration
3 years, 1 month
Inventor
- 1ALEX J. IVANOV
Record Details
- Patent number
- US 5359934
- Application
- 07584681
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
RaytheonMore from this assignee
Related by domain
MULTIPLE INFRARED MISSILE JAMMER
LOCKHEED SANDERS INC, A DELAWARE CORPORATION
MISSILE GUIDANCE SYSTEM
Raytheon
RETICLE FOR USE IN A GUIDANCE SEEKER FOR A SPINNING PROJECTILE
PRIMEX TECHNOLOGIES, INC.
SEEKER HEAD FOR MISSILES
BODENSEEWERK GERATETECHNIK GMBH
PROXIMITY FUSE/TIME FUSE FOR MISSILES
DAIMLER-BENZ AEROSPACE AG
PROJECTILE WITH VARIABLE TARGET TRANSITION DETECTION CAPABILITY AND METHOD THEREFOR
GENERAL DYNAMICS DECISION SYSTEMS, INC.