Inventor · disambiguated record
Andrew B. Facciano
Also filed as: FACCIANO ANDREW · FACCIANO ANDREW B
29 granted patents·1 pending application·416 citations·filing 1992–2017
97Inventor score
Files withRAYTHEON CO23FACCIANO ANDREW B3BIELAS MICHAEL S1HUGHES AIRCRAFT CO1HUGHES MISSILE SYSTEMS1
Top patents by PatentIndex Score
30 records- 0189US5806791AMissile jet vane control system and methodRAYTHEON CO·Filed 1995·Granted Sep 15, 1998·75 cites·10 claims
- 0282US8552350B2Mitigation of drift effects in secondary inertial measurements of an isolated detector assemblyBIELAS MICHAEL S·Filed 2012·Granted Oct 8, 2013·13 cites·20 claims
- 0382US6526860B2Composite concentric launch canisterRAYTHEON CO·Filed 2001·Granted Mar 4, 2003·43 cites·32 claims
- 0481US7681834B2Composite missile nose coneRAYTHEON CO·Filed 2006·Granted Mar 23, 2010·14 cites·22 claims
- 0580US5318255AStage separation mechanism for space vehiclesHUGHES AIRCRAFT CO·Filed 1992·Granted Jun 7, 1994·41 cites·14 claims
- 0676US7509903B2Separable structure materialRAYTHEON CO·Filed 2005·Granted Mar 31, 2009·11 cites·22 claims
- 0776US7082878B2Missile with multiple noseconesRAYTHEON CO·Filed 2003·Granted Aug 1, 2006·25 cites·33 claims
- 0873US7980057B2Integral composite rocket motor dome/nozzle structureRAYTHEON CO·Filed 2007·Granted Jul 19, 2011·16 cites·18 claims
- 0972US7819048B2Separable structure material methodRAYTHEON CO·Filed 2008·Granted Oct 26, 2010·8 cites·20 claims
- 1072US7800032B1Detachable aerodynamic missile stabilizing systemRAYTHEON CO·Filed 2006·Granted Sep 21, 2010·12 cites·10 claims
- 1170US6343954B1Integral missile harness-fairing assemblyRAYTHEON CO·Filed 2000·Granted Feb 5, 2002·19 cites·14 claims
- 1268US8049148B2Missile airframe and structure comprising piezoelectric fibers and method for active structural response controlRAYTHEON CO·Filed 2010·Granted Nov 1, 2011·5 cites·20 claims
- 1368US6548794B2Dissolvable thrust vector control vaneRAYTHEON CO·Filed 2001·Granted Apr 15, 2003·31 cites·43 claims
- 1466US9534563B2Cluster rocket motor boostersRAYTHEON CO·Filed 2013·Granted Jan 3, 2017·4 cites·19 claims
- 1566US9018572B2Rocket propelled payload with divert control system within nose coneRAYTHEON CO·Filed 2012·Granted Apr 28, 2015·5 cites·20 claims
- 1664US5483894AIntegral missile antenna-fuselage assemblyHUGHES MISSILE SYSTEMS·Filed 1994·Granted Jan 16, 1996·23 cites·19 claims
- 1762US7767944B2Piezoelectric fiber, active damped, composite electronic housingsRAYTHEON CO·Filed 2007·Granted Aug 3, 2010·5 cites·23 claims
- 1861US7108223B2Missile control system and methodRAYTHEON CO·Filed 2002·Granted Sep 19, 2006·11 cites·26 claims
- 1957US8729443B2Projectile and method that include speed adjusting guidance and propulsion systemsFACCIANO ANDREW B·Filed 2011·Granted May 20, 2014·3 cites·29 claims
- 2056US7989744B2Methods and apparatus for transferring a fluidRAYTHEON CO·Filed 2008·Granted Aug 2, 2011·4 cites·21 claims
- 2156US5979826AHybrid composite article and missile components and their fabricationRAYTHEON CO·Filed 1998·Granted Nov 9, 1999·19 cites·10 claims
- 2255US5824404AHybrid composite articles and missile components, and their fabricationRAYTHEON CO·Filed 1995·Granted Oct 20, 1998·18 cites·11 claims
- 2353US9115964B2Integral injection thrust vector control with booster attitude control systemRAYTHEON CO·Filed 2013·Granted Aug 25, 2015·2 cites·20 claims
- 2453US8104719B2Digital interface unit (DIU) and method for controlling stages of a multi-stage missleSHIAU CHIN·Filed 2005·Granted Jan 31, 2012·5 cites·10 claims
- 2552US8424438B2Multi-stage rocket, deployable raceway harness assembly and methods for controlling stages thereofFACCIANO ANDREW B·Filed 2010·Granted Apr 23, 2013·1 cites·30 claims
- 2649US10816026B2Separable physical coupler using piezoelectric forces for decouplingRAYTHEON CO·Filed 2017·Granted Oct 27, 2020·0 cites·16 claims
- 2749US9377279B2Rocket cluster divert and attitude control systemRAYTHEON CO·Filed 2014·Granted Jun 28, 2016·2 cites·20 claims
- 2841US9541364B2Adaptive electronically steerable array (AESA) system for interceptor RF target engagement and communicationsRAYTHEON CO·Filed 2014·Granted Jan 10, 2017·0 cites·21 claims
- 2937US8074516B2Methods and apparatus for non-axisymmetric radomeFACCIANO ANDREW B·Filed 2009·Granted Dec 13, 2011·1 cites·18 claims
- 3034US2015284080A1Special forces replenishment vehicleRAYTHEON CO·Filed 2014·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →