using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Industry

CPC
F42B10/663

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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F42Ammunition F42BEXPLOSIVE CHARGES F42B10/00Means for influencing

Current Industry

F42B10/663using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Kinetic energy vehicle with three-thruster divert control system
- Patent number 11,473,884
- Issue date Oct 18, 2022
- Raytheon Company
- Huy P. Nguyen
- F42 - AMMUNITION BLASTING
Information Patent Grant
Kinetic energy vehicle with attitude control system having paired t...
- Patent number 11,353,301
- Issue date Jun 7, 2022
- Raytheon Company
- Huy P. Nguyen
- F42 - AMMUNITION BLASTING
Information Patent Grant
Device and system for controlling missiles and kill vehicles operat...
- Patent number 11,084,605
- Issue date Aug 10, 2021
- BAYERN-CHEMIE GESELLSCHAFT FÜR FLUGCHEMISCHE ANTRIEBE MBH
- Jürgen Ramsel
- F41 - WEAPONS
Information Patent Grant
More compact side force steering and attitude control system, and a...
- Patent number 10,895,443
- Issue date Jan 19, 2021
- ARIANEGROUP SAS
- Pascal Caubet
- F42 - AMMUNITION BLASTING
Information Patent Grant
Deflector for a thrust flow powered vehicle and thrust flow powered...
- Patent number 10,774,785
- Issue date Sep 15, 2020
- MBDA UK LIMITED
- Ross William Poulton
- F42 - AMMUNITION BLASTING
Information Patent Grant
Method for controlling a flight vehicle
- Patent number 10,712,138
- Issue date Jul 14, 2020
- Valley Tech Systems, Inc.
- Russell Carlson
- F42 - AMMUNITION BLASTING
Information Patent Grant
Projectile, and system and method for steering a projectile
- Patent number 10,704,874
- Issue date Jul 7, 2020
- Israel Aerospace Industries Ltd.
- Asher Lotan
- F42 - AMMUNITION BLASTING
Information Patent Grant
Combined steering and drag-reduction device
- Patent number 9,500,456
- Issue date Nov 22, 2016
- ROXEL FRANCE
- Andre Pfiffer
- F42 - AMMUNITION BLASTING
Information Patent Grant
Rocket cluster divert and attitude control system
- Patent number 9,377,279
- Issue date Jun 28, 2016
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
System for steering a flying object using pairs of lateral nozzles
- Patent number 9,212,880
- Issue date Dec 15, 2015
- MBDA France
- Rinaldo Rossi
- F42 - AMMUNITION BLASTING
Information Patent Grant
In-flight attitude control and direct thrust flight control system...
- Patent number 9,194,332
- Issue date Nov 24, 2015
- Herakles
- Pascal Caubet
- F42 - AMMUNITION BLASTING
Information Patent Grant
Tail thruster control for projectiles
- Patent number 9,157,714
- Issue date Oct 13, 2015
- BAE Systems Information and Electronic Systems Integration Inc.
- Robert D. Frey
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integral injection thrust vector control with booster attitude cont...
- Patent number 9,115,964
- Issue date Aug 25, 2015
- Raytheon Company
- Andrew B Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Air vehicle with bilateral steering thrusters
- Patent number 9,068,808
- Issue date Jun 30, 2015
- Raytheon Company
- Robert W Morgan
- F42 - AMMUNITION BLASTING
Information Patent Grant
Rocket propelled payload with divert control system within nose cone
- Patent number 9,018,572
- Issue date Apr 28, 2015
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integrated propulsion and attitude control system from a common pre...
- Patent number 8,975,565
- Issue date Mar 10, 2015
- Raytheon Company
- Doron Strassman
- F42 - AMMUNITION BLASTING
Information Patent Grant
Tail thruster control for projectiles
- Patent number 8,624,171
- Issue date Jan 7, 2014
- BAE Systems Information and Electronic Systems Integration Inc.
- Robert D. Frey
- F42 - AMMUNITION BLASTING
Information Patent Grant
Steerable projectile charging system
- Patent number 8,362,408
- Issue date Jan 29, 2013
- Honeywell International Inc.
- Robert J. Carlson
- F42 - AMMUNITION BLASTING
Information Patent Grant
Actuation assembly
- Patent number 8,338,768
- Issue date Dec 25, 2012
- Honeywell International Inc.
- Casey Hanlon
- F42 - AMMUNITION BLASTING
Information Patent Grant
Guidance control system for projectiles
- Patent number 8,269,156
- Issue date Sep 18, 2012
- The Charles Stark Draper Laboratory, Inc.
- Edward Bergmann
- F42 - AMMUNITION BLASTING
Information Patent Grant
Flight control of missiles
- Patent number 8,119,959
- Issue date Feb 21, 2012
- Short Brothers PLC
- Richard Sutton Ransom
- F42 - AMMUNITION BLASTING
Information Patent Grant
Control system for an exoatmospheric kill vehicle
- Patent number 8,084,726
- Issue date Dec 27, 2011
- Honeywell International, Inc.
- J. Casey Hanlon
- F42 - AMMUNITION BLASTING
Information Patent Grant
Steering system and method for a guided flying apparatus
- Patent number 8,080,771
- Issue date Dec 20, 2011
- Israel Aerospace Industries Ltd.
- Mordechai Shai
- F42 - AMMUNITION BLASTING
Information Patent Grant
Guided projectile
- Patent number 7,891,298
- Issue date Feb 22, 2011
- Pratt & Whitney Rocketdyne, Inc.
- Alan B. Minick
- F42 - AMMUNITION BLASTING
Information Patent Grant
Post boost control power assembly
- Patent number 7,875,838
- Issue date Jan 25, 2011
- The United States of America as represented by the Secretary of the Navy
- George M. Starken
- F42 - AMMUNITION BLASTING
Information Patent Grant
Methods and apparatus for guiding a projectile
- Patent number 7,872,215
- Issue date Jan 18, 2011
- Raytheon Company
- Thomas R. Blackburn
- F42 - AMMUNITION BLASTING
Information Patent Grant
Pulsed detonation engines for reaction control systems
- Patent number 7,506,498
- Issue date Mar 24, 2009
- Science Applications International Corporation
- Shmuel Eidelman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rocket engine having guide vanes in the nozzle of the engine
- Patent number 7,478,778
- Issue date Jan 20, 2009
- Nammo Raufoss AS
- Erland Ørbekk
- F42 - AMMUNITION BLASTING
Information Patent Grant
Pulsed detonation engines for reaction control systems
- Patent number 7,410,131
- Issue date Aug 12, 2008
- Science Applications International Corporation
- Shmuel Eidelman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Telescoped projectile
- Patent number 7,380,504
- Issue date Jun 3, 2008
- Raytheon Company
- Richard Dryer
- F41 - WEAPONS

Patents Applicationslast 30 patents

Information Patent Application
KINETIC ENERGY VEHICLE WITH THREE-THRUSTER DIVERT CONTROL SYSTEM
- Publication number 20210223012
- Publication date Jul 22, 2021
- Raytheon Company
- Huy P. Nguyen
- F42 - AMMUNITION BLASTING
Information Patent Application
KINETIC ENERGY VEHICLE WITH ATTITUDE CONTROL SYSTEM HAVING PAIRED T...
- Publication number 20210223011
- Publication date Jul 22, 2021
- Raytheon Company
- Huy P. Nguyen
- F42 - AMMUNITION BLASTING
Information Patent Application
A MORE COMPACT SIDE FORCE STEERING AND ATTITUDE CONTROL SYSTEM, AND...
- Publication number 20180347957
- Publication date Dec 6, 2018
- ARIANEGROUP SAS
- Pascal CAUBET
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
PROJECTILE, AND SYSTEM AND METHOD FOR STEERING A PROJECTILE
- Publication number 20180306563
- Publication date Oct 25, 2018
- ISRAEL AEROSPACE INDUSTRIES LTD
- Asher LOTAN
- F42 - AMMUNITION BLASTING
Information Patent Application
AIR VEHICLE WITH BILATERAL STEERING THRUSTERS
- Publication number 20140224921
- Publication date Aug 14, 2014
- Raytheon Company
- Robert W. Morgan
- F42 - AMMUNITION BLASTING
Information Patent Application
SYSTEM FOR STEERING A FLYING OBJECT USING PAIRS OF LATERAL NOZZLES
- Publication number 20140224923
- Publication date Aug 14, 2014
- Rinaldo Rossi
- F42 - AMMUNITION BLASTING
Information Patent Application
ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE
- Publication number 20140138475
- Publication date May 22, 2014
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
In-Flight Attitude Control and Direct Thrust Flight Control System...
- Publication number 20140109552
- Publication date Apr 24, 2014
- HERAKLES
- Pascal Caubet
- F42 - AMMUNITION BLASTING
Information Patent Application
INTEGRATED PROPULSION AND ATTITUDE CONTROL SYSTEM FROM A COMMON PRE...
- Publication number 20140061364
- Publication date Mar 6, 2014
- Raytheon Company
- Doron Strassman
- F42 - AMMUNITION BLASTING
Information Patent Application
GUIDANCE CONTROL SYSTEM FOR PROJECTILES
- Publication number 20120187235
- Publication date Jul 26, 2012
- Edward Bergmann
- F42 - AMMUNITION BLASTING
Information Patent Application
ACTUATION ASSEMBLY
- Publication number 20120181372
- Publication date Jul 19, 2012
- Honeywell International Inc.
- Casey Hanlon
- F42 - AMMUNITION BLASTING
Information Patent Application
TAIL THRUSTER CONTROL FOR PROJECTILES
- Publication number 20120048991
- Publication date Mar 1, 2012
- Robert D. Frey, JR.
- F42 - AMMUNITION BLASTING
Information Patent Application
STEERABLE PROJECTILE CHARGING SYSTEM
- Publication number 20110094372
- Publication date Apr 28, 2011
- Honeywell International Inc.
- Robert J. Carlson
- F42 - AMMUNITION BLASTING
Information Patent Application
METHODS AND APPARATUS FOR A TANDEM DIVERT AND ATTITUDE CONTROL SYSTEM
- Publication number 20110029160
- Publication date Feb 3, 2011
- Raytheon Company
- Philip W. Pagliara
- F42 - AMMUNITION BLASTING
Information Patent Application
GUIDED PROJECTILE
- Publication number 20100307367
- Publication date Dec 9, 2010
- Alan B. Minick
- F42 - AMMUNITION BLASTING
Information Patent Application
METHODS AND APPARATUS FOR GUIDING A PROJECTILE
- Publication number 20100288869
- Publication date Nov 18, 2010
- Raytheon Company
- Thomas R. BLACKBURN
- F42 - AMMUNITION BLASTING
Information Patent Application
CONTROL SYSTEM FOR AN EXOATMOSPHERIC KILL VEHICLE
- Publication number 20100282892
- Publication date Nov 11, 2010
- Honeywell International Inc.,
- Casey Hanlon
- F42 - AMMUNITION BLASTING
Information Patent Application
STEERING SYSTEM AND METHOD FOR A GUIDED FLYING APPARATUS
- Publication number 20090084888
- Publication date Apr 2, 2009
- Mordechai Shai
- F42 - AMMUNITION BLASTING
Information Patent Application
FORCE BALANCED BUTTERFLY PROPORTIONAL HOT GAS VALVE
- Publication number 20080302991
- Publication date Dec 11, 2008
- Honeywell International, Inc.
- Raymond R. Tseng
- F42 - AMMUNITION BLASTING
Information Patent Application
PULSED DETONATION ENGINES FOR REACTION CONTROL SYSTEMS
- Publication number 20080099627
- Publication date May 1, 2008
- Science Applications International Corporation
- Shmuel Eidelman
- F42 - AMMUNITION BLASTING
Information Patent Application
Pulsed Detonation Engines For Reaction Control Systems
- Publication number 20080053058
- Publication date Mar 6, 2008
- Science Applications International Corporation
- Shmuel Eidelman
- F42 - AMMUNITION BLASTING
Information Patent Application
Telescoped projectile
- Publication number 20080000380
- Publication date Jan 3, 2008
- Richard Dryer
- F42 - AMMUNITION BLASTING
Information Patent Application
Rocket engine having guide vanes in the nozzle of the engine
- Publication number 20070152096
- Publication date Jul 5, 2007
- Erland Ørbekk
- F42 - AMMUNITION BLASTING
Information Patent Application
MISSILE CONTROL SYSTEM AND METHOD
- Publication number 20060284006
- Publication date Dec 21, 2006
- Daniel B. Chasman
- F42 - AMMUNITION BLASTING
Information Patent Application
Pulsed detonation engines for reaction control systems
- Publication number 20060201134
- Publication date Sep 14, 2006
- Science Applications International Corporation
- Shmuel Eidelman
- F42 - AMMUNITION BLASTING
Information Patent Application
PROJECTILE SEEKER
- Publication number 20060054734
- Publication date Mar 16, 2006
- RAFAEL - ARMAMENT DEVELOPMENT AUTHORITY LTD.
- Ehud Chishinski
- F42 - AMMUNITION BLASTING
Information Patent Application
FLUIDIC DIVERTER VALVE WITH A NON-SPHERICAL SHUTTLE ELEMENT
- Publication number 20060000514
- Publication date Jan 5, 2006
- Donald J. Christensen
- F42 - AMMUNITION BLASTING
Information Patent Application
FLUIDIC DIVERTER VALVE WITH A VARIABLE VALVE-BORE CLEARANCE
- Publication number 20050150207
- Publication date Jul 14, 2005
- Donald J. Christensen
- F42 - AMMUNITION BLASTING
Information Patent Application
MISSILE CONTROL SYSTEM AND METHOD
- Publication number 20050011989
- Publication date Jan 20, 2005
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Application
Three-axis attitude control propulsion device and flying object com...
- Publication number 20040245371
- Publication date Dec 9, 2004
- Toshiharu Fujita
- F42 - AMMUNITION BLASTING

using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Kinetic energy vehicle with three-thruster divert control system

Kinetic energy vehicle with attitude control system having paired t...

Device and system for controlling missiles and kill vehicles operat...

More compact side force steering and attitude control system, and a...

Deflector for a thrust flow powered vehicle and thrust flow powered...

Method for controlling a flight vehicle

Projectile, and system and method for steering a projectile

Combined steering and drag-reduction device

Rocket cluster divert and attitude control system

System for steering a flying object using pairs of lateral nozzles

In-flight attitude control and direct thrust flight control system...

Tail thruster control for projectiles

Integral injection thrust vector control with booster attitude cont...

Air vehicle with bilateral steering thrusters

Rocket propelled payload with divert control system within nose cone

Integrated propulsion and attitude control system from a common pre...

Tail thruster control for projectiles

Steerable projectile charging system

Actuation assembly

Guidance control system for projectiles

Flight control of missiles

Control system for an exoatmospheric kill vehicle

Steering system and method for a guided flying apparatus

Guided projectile

Post boost control power assembly

Methods and apparatus for guiding a projectile

Pulsed detonation engines for reaction control systems

Rocket engine having guide vanes in the nozzle of the engine

Pulsed detonation engines for reaction control systems

Telescoped projectile

Patents Applicationslast 30 patents

KINETIC ENERGY VEHICLE WITH THREE-THRUSTER DIVERT CONTROL SYSTEM

KINETIC ENERGY VEHICLE WITH ATTITUDE CONTROL SYSTEM HAVING PAIRED T...

A MORE COMPACT SIDE FORCE STEERING AND ATTITUDE CONTROL SYSTEM, AND...

PROJECTILE, AND SYSTEM AND METHOD FOR STEERING A PROJECTILE

AIR VEHICLE WITH BILATERAL STEERING THRUSTERS

SYSTEM FOR STEERING A FLYING OBJECT USING PAIRS OF LATERAL NOZZLES

ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE

In-Flight Attitude Control and Direct Thrust Flight Control System...

INTEGRATED PROPULSION AND ATTITUDE CONTROL SYSTEM FROM A COMMON PRE...

GUIDANCE CONTROL SYSTEM FOR PROJECTILES

ACTUATION ASSEMBLY

TAIL THRUSTER CONTROL FOR PROJECTILES

STEERABLE PROJECTILE CHARGING SYSTEM

METHODS AND APPARATUS FOR A TANDEM DIVERT AND ATTITUDE CONTROL SYSTEM

GUIDED PROJECTILE

METHODS AND APPARATUS FOR GUIDING A PROJECTILE

CONTROL SYSTEM FOR AN EXOATMOSPHERIC KILL VEHICLE

STEERING SYSTEM AND METHOD FOR A GUIDED FLYING APPARATUS

FORCE BALANCED BUTTERFLY PROPORTIONAL HOT GAS VALVE

PULSED DETONATION ENGINES FOR REACTION CONTROL SYSTEMS

Pulsed Detonation Engines For Reaction Control Systems

Telescoped projectile

Rocket engine having guide vanes in the nozzle of the engine

MISSILE CONTROL SYSTEM AND METHOD

Pulsed detonation engines for reaction control systems

PROJECTILE SEEKER

FLUIDIC DIVERTER VALVE WITH A NON-SPHERICAL SHUTTLE ELEMENT

FLUIDIC DIVERTER VALVE WITH A VARIABLE VALVE-BORE CLEARANCE

MISSILE CONTROL SYSTEM AND METHOD

Three-axis attitude control propulsion device and flying object com...