Inventor
FACCIANO ANDREW B
US26 patents
⚠️ This page may combine multiple inventors who share the name “FACCIANO ANDREW B”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
RAYTHEON CO
20 patentsUS5806791ASep 15, 1998
Missile jet vane control system and method
RAYTHEON CO75 citations91
US7082878B2Aug 1, 2006
Missile with multiple nosecones
RAYTHEON CO25 citations87
US6343954B1Feb 5, 2002
Integral missile harness-fairing assembly
RAYTHEON CO19 citations86
US6526860B2Mar 4, 2003
Composite concentric launch canister
RAYTHEON CO43 citations85
US6548794B2Apr 15, 2003
Dissolvable thrust vector control vane
RAYTHEON CO31 citations84
US7819048B2Oct 26, 2010
Separable structure material method
RAYTHEON CO8 citations83
US7509903B2Mar 31, 2009
Separable structure material
RAYTHEON CO11 citations83
US7681834B2Mar 23, 2010
Composite missile nose cone
RAYTHEON CO14 citations82
US7108223B2Sep 19, 2006
Missile control system and method
RAYTHEON CO11 citations82
US7800032B1Sep 21, 2010
Detachable aerodynamic missile stabilizing system
RAYTHEON CO12 citations79
US7980057B2Jul 19, 2011
Integral composite rocket motor dome/nozzle structure
RAYTHEON CO16 citations77
US9534563B2Jan 3, 2017
Cluster rocket motor boosters
RAYTHEON CO4 citations71
US9018572B2Apr 28, 2015
Rocket propelled payload with divert control system within nose cone
RAYTHEON CO5 citations71
US8049148B2Nov 1, 2011
Missile airframe and structure comprising piezoelectric fibers and method for active structural response control
RAYTHEON CO5 citations71
US7767944B2Aug 3, 2010
Piezoelectric fiber, active damped, composite electronic housings
RAYTHEON CO5 citations71
US9115964B2Aug 25, 2015
Integral injection thrust vector control with booster attitude control system
RAYTHEON CO2 citations60
US7989744B2Aug 2, 2011
Methods and apparatus for transferring a fluid
RAYTHEON CO4 citations57
US9377279B2Jun 28, 2016
Rocket cluster divert and attitude control system
RAYTHEON CO2 citations55
US10816026B2Oct 27, 2020
Separable physical coupler using piezoelectric forces for decoupling
RAYTHEON CO0 citations48
US9541364B2Jan 10, 2017
Adaptive electronically steerable array (AESA) system for interceptor RF target engagement and communications
RAYTHEON CO0 citations33
FACCIANO ANDREW B
3 patentsUS8729443B2May 20, 2014
Projectile and method that include speed adjusting guidance and propulsion systems
FACCIANO ANDREW B3 citations53
US8424438B2Apr 23, 2013
Multi-stage rocket, deployable raceway harness assembly and methods for controlling stages thereof
FACCIANO ANDREW B1 citations42
US8074516B2Dec 13, 2011
Methods and apparatus for non-axisymmetric radome
FACCIANO ANDREW B1 citations39