Patents
Sitemap › F42 - Ammunition; Blasting › F42B - Explosive charges, e.g. for blasting; Fireworks; Ammunition › F42B 15 - Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Patents for F42B 15 - Self-propelled projectiles or missiles, e.g. rockets; Guided missiles (2,618)
04/2004
04/20/2004US6724341 Autonomous onboard absolute position and orientation referencing system
04/20/2004US6723972 Method and apparatus for planar actuation of a flared surface to control a vehicle
04/15/2004US20040069135 Rocket launcher system and method for controlling a rocket launcher system
04/13/2004US6718883 Device for neutralizing a payload
04/13/2004US6718881 Ordnance control and initiation system and related method
04/01/2004WO2004027343A1 Apparatus and method for releaseably joining elements
03/2004
03/30/2004US6711890 Pressure-actuated joint system
03/25/2004US20040057787 Apparatus and method for releaseably joining elements
03/25/2004DE4333596B4 Filtereinrichtung Filter means
03/18/2004US20040050282 Rocket motors with insensitive munitions systems and projectiles including same
03/16/2004US6705566 Active mirror guidance system
03/11/2004DE20319044U1 Hydraulic rocket, has warhead secured to front end and ring wall and nozzle secured to rear end of rocket body
03/04/2004WO2004018292A1 Operating method for launch rockets and a set of rocket boosters for carrying out said method
03/04/2004US20040041058 Vehicle, lightweight pneumatic pilot valve and related systems therefor
02/2004
02/26/2004DE10211493B3 Covering cap for a cruise missile comprises a cap held on its edge by a hinge joint and a pull-off fixing which during explosive severing pivots about the movement pole of the hinge joint
02/05/2004US20040021034 Guided artillery missile with extremely long range
01/2004
01/20/2004US6679453 Jettisonable protective element
01/20/2004US6679177 Resettable and redundant NEA-initiated hold-down and release mechanism for a flight termination system
01/08/2004WO2002032762A3 Artillery launched flyer assembly
01/02/2004EP1373822A2 Method and system for correcting for curvature in determining the trajectory of a projectile
12/2003
12/31/2003WO2003057560A3 Improvements in or relating to underwater vehicles
12/30/2003US6669126 Payout device for data transmission lines and method for the production of payout device
12/25/2003US20030235673 Method for obtaining reduced thermal flux in silicone resin composites
12/24/2003WO2003106914A1 Device for unwinding a wire providing data transmission of any type between two mobile elements operating in a fluid
12/23/2003US6666410 Load relief system for a launch vehicle
12/23/2003US6666144 Warhead decoupling bearing
12/11/2003WO2003102505A1 Airborne reconnaissance system
12/11/2003DE10220440C1 Failed space rocket impact point estimation method uses data provided by onboard global satellite navigation system for calculating momentary position and velocity of rocket
12/09/2003US6659393 Retarding and lock apparatus and method for retardation and interlocking of elements
11/2003
11/18/2003US6647889 Propelling device for a projectile in a missile
11/12/2003EP1361411A2 Device with a mobile element, for provisionally connecting and pyrotechnically separating two units
11/11/2003US6646242 Rotational canted-joint missile control system
11/04/2003US6640720 Translation and locking mechanism in missile
10/2003
10/23/2003US20030196544 Temporary connection and pyrotechnic separation device for two elements, without breakage
10/22/2003EP1355120A1 Device for provisionally connecting and pyrotechnically separating two elements, with no rupture
10/22/2003CN1450334A Secondary propelling method for bullet
10/07/2003US6630902 Shipboard point defense system and elements therefor
09/2003
09/30/2003US6626040 High-g hardened sensors
09/24/2003EP1346186A1 Rocket launcher system and method for controlling a rocket launcher system
09/16/2003US6619029 Rocket motors with insensitive munitions systems
09/12/2003WO2003016849A3 Method and apparatus for testing engines
09/12/2003WO2002082097A3 Method and system for correcting for curvature in determining the trajectory of a projectile
09/10/2003EP1342981A2 Gun-launched rocket
09/04/2003US20030163986 Pressure-actuated joint system
08/2003
08/28/2003US20030160129 Rotational canted-joint missile control system
08/28/2003US20030159609 Ordnance control and initiation system and related method
08/27/2003EP1337750A1 Method and device for a multiple step rocket
08/14/2003US20030150961 Load relief system for a launch vehicle
08/12/2003US6604705 Control group for directional fins on missiles and/or shells
08/05/2003US6603421 Shipboard point defense system and elements therefor
07/2003
07/23/2003CN1115542C Armor piercing projectile
07/17/2003WO2003057560A2 Improvements in or relating to underwater vehicles
07/15/2003US6592070 Interference-aided navigation system for rotating vehicles
07/10/2003US20030127009 Imaging device and method
07/09/2003CN2559956Y Traction type rain-increasing hail suppression rocket launcher
07/08/2003US6588699 Radar-guided missile programmable digital predetection signal processor
07/01/2003US6587078 Interference-aided navigation with temporal beam forming in rotating vehicles
06/2003
06/24/2003US6581870 Method and apparatus for reducing pressure and temperature on the front of a missile at ultrasonic speed
06/18/2003EP1319920A1 Pyrotechnical separator and separation system equipped with said separator
06/17/2003US6578491 Externally accessible thermal ground plane for tactical missiles
06/10/2003US6576880 Flyer assembly
06/03/2003US6571618 Support device for a motorized flying instrument in a wind tunnel
06/03/2003CA2278500C System for accurately determining missile vertical velocity and altitude
05/2003
05/29/2003US20030097951 Modular missile and method of assembly
05/27/2003US6568330 Modular missile and method of assembly
05/21/2003CN1419101A Composite material made box body structure for storage and conveying launch box
05/20/2003US6565036 Technique for improving accuracy of high speed projectiles
05/15/2003US20030089820 Flyer assembly
05/14/2003EP1309831A1 Guided artillery missile with extremely long range
05/13/2003US6563763 Method and system for correcting for curvature in determining the trajectory of a projectile
05/07/2003EP0910245B1 Device for controlling bird strike hazards
05/06/2003US6557475 Separation system for a booster payload fairing
05/01/2003US20030079464 Rocket motors with insensitive munitions systems
04/2003
04/29/2003US6556896 Magnetic roll rate sensor
04/24/2003US20030075641 Radar-guided missile programmable digital predetection signal processor
04/22/2003US6551663 Polysiloxane matrix with a glass or quartz fiber embedded reinforcement and an organic polymeric layer were multi-cycle heat treated with quartz lamps
04/08/2003US6543716 Shipboard point defense system and elements therefor
04/02/2003CN1407311A Long range attack shells for high altitude blockade
03/2003
03/26/2003CN1405527A Jet propelling aircraft
03/25/2003US6536350 Stagnation pressure activated fuel release mechanism for hypersonic projectiles
03/20/2003WO2003023317A1 Externally accessible thermal ground plane for tactical missiles
03/20/2003US20030051536 Method and apparatus for testing engines
03/19/2003CN1403781A Portable dual high-speed air defense missile
03/18/2003US6533221 Device for supporting a payload in a launch vehicle of said payload
03/13/2003WO2002068896A3 Supercavitating underwater projectile
03/13/2003US20030047103 Externally accessible thermal ground plane for tactical missiles
03/12/2003EP0975863B1 Missile with safe rocket ignition system
03/11/2003US6530539 Internal fluid cooled window assembly
03/05/2003EP0930994B1 Rocket launching system employing thermal-acoustic detection for rocket ignition
02/2003
02/27/2003WO2003016849A2 Method and apparatus for testing engines
02/20/2003WO2002032762A9 Artillery launched flyer assembly
02/19/2003CN1397725A Pressure actuating joint system
02/18/2003US6520448 Spinning-vehicle navigation using apparent modulation of navigational signals
02/05/2003EP1281927A1 Guided Missile
01/2003
01/23/2003WO2002055954A3 Method for obtaining reduced thermal flux in a composite
01/07/2003US6502522 Coil restraint device
12/2002
12/24/2002US6497530 Universal flange joint for attaching
12/18/2002EP1266825A1 Method for separating an airborne rocket from its carrier
12/17/2002US6494140 Modular rocket boosted penetrating warhead
12/12/2002US20020187699 Heat insulating material
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