Andrew B. Facciano

Person

Tucson, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Adaptive electronically steerable array (AESA) system for intercept...
- Patent number 9,541,364
- Issue date Jan 10, 2017
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Cluster rocket motor boosters
- Patent number 9,534,563
- Issue date Jan 3, 2017
- Raytheon Company
- Andrew B Facciano
- 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
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
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
Projectile and method that include speed adjusting guidance and pro...
- Patent number 8,729,443
- Issue date May 20, 2014
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Mitigation of drift effects in secondary inertial measurements of a...
- Patent number 8,552,350
- Issue date Oct 8, 2013
- Raytheon Company
- Michael S. Bielas
- G01 - MEASURING TESTING
Information Patent Grant
Multi-stage rocket, deployable raceway harness assembly and methods...
- Patent number 8,424,438
- Issue date Apr 23, 2013
- Raytheon Company
- Andrew B. Facciano
- F41 - WEAPONS
Information Patent Grant
Digital interface unit (DIU) and method for controlling stages of a...
- Patent number 8,104,719
- Issue date Jan 31, 2012
- Raytheon Company
- Chin Shiau
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile with system for separating subvehicles
- Patent number 8,082,848
- Issue date Dec 27, 2011
- Raytheon Company
- Gregg J. Hlavacek
- F42 - AMMUNITION BLASTING
Information Patent Grant
Methods and apparatus for non-axisymmetric radome
- Patent number 8,074,516
- Issue date Dec 13, 2011
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile airframe and structure comprising piezoelectric fibers and...
- Patent number 8,049,148
- Issue date Nov 1, 2011
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Methods and apparatus for transferring a fluid
- Patent number 7,989,744
- Issue date Aug 2, 2011
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integral composite rocket motor dome/nozzle structure
- Patent number 7,980,057
- Issue date Jul 19, 2011
- Raytheon Company
- Andrew B. Facciano
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Separable structure material method
- Patent number 7,819,048
- Issue date Oct 26, 2010
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Detachable aerodynamic missile stabilizing system
- Patent number 7,800,032
- Issue date Sep 21, 2010
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Piezoelectric fiber, active damped, composite electronic housings
- Patent number 7,767,944
- Issue date Aug 3, 2010
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Composite missile nose cone
- Patent number 7,681,834
- Issue date Mar 23, 2010
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Separable structure material
- Patent number 7,509,903
- Issue date Mar 31, 2009
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile control system and method
- Patent number 7,108,223
- Issue date Sep 19, 2006
- Raytheon Company
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile with multiple nosecones
- Patent number 7,082,878
- Issue date Aug 1, 2006
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Dissolvable thrust vector control vane
- Patent number 6,548,794
- Issue date Apr 15, 2003
- Raytheon Company
- Andrew B. Facciano
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Composite concentric launch canister
- Patent number 6,526,860
- Issue date Mar 4, 2003
- Raytheon Company
- Andrew B. Facciano
- F41 - WEAPONS
Information Patent Grant
Integral missile harness-fairing assembly
- Patent number 6,343,954
- Issue date Feb 5, 2002
- Raytheon Company
- Andrew B. Facciano
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Grant
Hybrid composite article and missile components and their fabrication
- Patent number 5,979,826
- Issue date Nov 9, 1999
- Raytheon Company
- Janis Brown
- F42 - AMMUNITION BLASTING
Information Patent Grant
Hybrid composite articles and missile components, and their fabrica...
- Patent number 5,824,404
- Issue date Oct 20, 1998
- Raytheon Company
- Janis Brown
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile jet vane control system and method
- Patent number 5,806,791
- Issue date Sep 15, 1998
- Raytheon Company
- William M. Hatalsky
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integral missile antenna-fuselage assembly
- Patent number 5,483,894
- Issue date Jan 16, 1996
- Hughes Missile Systems Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Stage separation mechanism for space vehicles
- Patent number 5,318,255
- Issue date Jun 7, 1994
- Hughes Aircraft Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING

Patents Applicationslast 30 patents

Information Patent Application
SEPARABLE PHYSICAL COUPLER USING PIEZOELECTRIC FORCES FOR DECOUPLING
- Publication number 20190048914
- Publication date Feb 14, 2019
- Christopher S. Nordahl
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
ADAPTIVE ELECTRONICALLY STEERABLE ARRAY (AESA) SYSTEM FOR INTERCEPT...
- Publication number 20160084623
- Publication date Mar 24, 2016
- Raytheon Company
- Andrew B. Facciano
- F41 - WEAPONS
Information Patent Application
ROCKET CLUSTER DIVERT AND ATTITUDE CONTROL SYSTEM
- Publication number 20150300780
- Publication date Oct 22, 2015
- Raytheon Company
- Andrew B. Facciano
- F41 - WEAPONS
Information Patent Application
SPECIAL FORCES REPLENISHMENT VEHICLE
- Publication number 20150284080
- Publication date Oct 8, 2015
- Raytheon Company
- Andrew B. Facciano
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INTEGRAL INJECTION THRUST VECTOR CONTROL WITH BOOSTER ATTITUDE CONT...
- Publication number 20150184988
- Publication date Jul 2, 2015
- Raytheon Company
- Andrew B Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
CLUSTER ROCKET MOTOR BOOSTERS
- Publication number 20150159587
- Publication date Jun 11, 2015
- Raytheon Company
- Andrew B. Facciano
- F41 - WEAPONS
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
MITIGATION OF DRIFT EFFECTS IN SECONDARY INERTIAL MEASUREMENTS OF A...
- Publication number 20130181086
- Publication date Jul 18, 2013
- Raytheon Company
- Michael S. Bielas
- G01 - MEASURING TESTING
Information Patent Application
PROJECTILE AND METHOD THAT INCLUDE SPEED ADJUSTING GUIDANCE AND PRO...
- Publication number 20120181373
- Publication date Jul 19, 2012
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
MULTI-STAGE ROCKET, DEPLOYABLE RACEWAY HARNESS ASSEMBLY AND METHODS...
- Publication number 20120137653
- Publication date Jun 7, 2012
- Raytheon Company
- Andrew B. Facciano
- F41 - WEAPONS
Information Patent Application
MISSILE WITH SYSTEM FOR SEPARATING SUBVEHICLES
- Publication number 20100276544
- Publication date Nov 4, 2010
- Gregg J. Hlavacek
- F42 - AMMUNITION BLASTING
Information Patent Application
MISSILE AIRFRAME AND STRUCTURE COMPRISING PIEZOELECTRIC FIBERS AND...
- Publication number 20100264251
- Publication date Oct 21, 2010
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
DETACHABLE AERODYNAMIC MISSILE STABILIZING SYSTEM
- Publication number 20100219285
- Publication date Sep 2, 2010
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
METHODS AND APPARATUS FOR NON-AXISYMMETRIC RADOME
- Publication number 20090320589
- Publication date Dec 31, 2009
- Raytheon Company
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
METHODS AND APPARATUS FOR TRANSFERRING A FLUID
- Publication number 20090194632
- Publication date Aug 6, 2009
- Raytheon Company
- ANDREW B. FACCIANO
- F42 - AMMUNITION BLASTING
Information Patent Application
SEPARABLE STRUCTURE MATERIAL METHOD
- Publication number 20090071320
- Publication date Mar 19, 2009
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
Integral composite rocket motor dome/nozzle structure
- Publication number 20080290191
- Publication date Nov 27, 2008
- Andrew B. Facciano
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
Piezoelectric fiber, active damped, composite electronic housings
- Publication number 20080217465
- Publication date Sep 11, 2008
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
Separable structure material
- Publication number 20080163748
- Publication date Jul 10, 2008
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
Scalable electronics architecture
- Publication number 20080092765
- Publication date Apr 24, 2008
- Raytheon Company
- Chin Shiau
- F42 - AMMUNITION BLASTING
Information Patent Application
Composite missile nose cone
- Publication number 20070228211
- Publication date Oct 4, 2007
- Andrew B. Facciano
- 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
Missile with multiple nosecones
- Publication number 20050000383
- Publication date Jan 6, 2005
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
Composite concentric launch canister
- Publication number 20020189432
- Publication date Dec 19, 2002
- Andrew B. Facciano
- F41 - WEAPONS
Information Patent Application
Dissolvable thrust vector control vane
- Publication number 20020130216
- Publication date Sep 19, 2002
- Andrew B. Facciano
- F42 - AMMUNITION BLASTING

Andrew B. Facciano

Person

Patents Grantslast 30 patents

Adaptive electronically steerable array (AESA) system for intercept...

Cluster rocket motor boosters

Rocket cluster divert and attitude control system

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

Rocket propelled payload with divert control system within nose cone

Projectile and method that include speed adjusting guidance and pro...

Mitigation of drift effects in secondary inertial measurements of a...

Multi-stage rocket, deployable raceway harness assembly and methods...

Digital interface unit (DIU) and method for controlling stages of a...

Missile with system for separating subvehicles

Methods and apparatus for non-axisymmetric radome

Missile airframe and structure comprising piezoelectric fibers and...

Methods and apparatus for transferring a fluid

Integral composite rocket motor dome/nozzle structure

Separable structure material method

Detachable aerodynamic missile stabilizing system

Piezoelectric fiber, active damped, composite electronic housings

Composite missile nose cone

Separable structure material

Missile control system and method

Missile with multiple nosecones

Dissolvable thrust vector control vane

Composite concentric launch canister

Integral missile harness-fairing assembly

Hybrid composite article and missile components and their fabrication

Hybrid composite articles and missile components, and their fabrica...

Missile jet vane control system and method

Integral missile antenna-fuselage assembly

Stage separation mechanism for space vehicles

Patents Applicationslast 30 patents

SEPARABLE PHYSICAL COUPLER USING PIEZOELECTRIC FORCES FOR DECOUPLING

ADAPTIVE ELECTRONICALLY STEERABLE ARRAY (AESA) SYSTEM FOR INTERCEPT...

ROCKET CLUSTER DIVERT AND ATTITUDE CONTROL SYSTEM

SPECIAL FORCES REPLENISHMENT VEHICLE

INTEGRAL INJECTION THRUST VECTOR CONTROL WITH BOOSTER ATTITUDE CONT...

CLUSTER ROCKET MOTOR BOOSTERS

ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE

MITIGATION OF DRIFT EFFECTS IN SECONDARY INERTIAL MEASUREMENTS OF A...

PROJECTILE AND METHOD THAT INCLUDE SPEED ADJUSTING GUIDANCE AND PRO...

MULTI-STAGE ROCKET, DEPLOYABLE RACEWAY HARNESS ASSEMBLY AND METHODS...

MISSILE WITH SYSTEM FOR SEPARATING SUBVEHICLES

MISSILE AIRFRAME AND STRUCTURE COMPRISING PIEZOELECTRIC FIBERS AND...

DETACHABLE AERODYNAMIC MISSILE STABILIZING SYSTEM

METHODS AND APPARATUS FOR NON-AXISYMMETRIC RADOME

METHODS AND APPARATUS FOR TRANSFERRING A FLUID

SEPARABLE STRUCTURE MATERIAL METHOD

Integral composite rocket motor dome/nozzle structure

Piezoelectric fiber, active damped, composite electronic housings

Separable structure material

Scalable electronics architecture

Composite missile nose cone

MISSILE CONTROL SYSTEM AND METHOD

Missile with multiple nosecones

Composite concentric launch canister

Dissolvable thrust vector control vane