Patent Assignment
Reel/Frame 027603/0556
Security Agreement
Recorded: 2012-01-27
Received: 2012-01-27
Pages: 14
Assignor
AEROJET-GENERAL CORPORATION
Executed: 2011-11-18
Assignee
WELLS FARGO BANK, NATIONAL ASSOICATION, AS ADMINISTRATIVE AGENT
1525 WEST W.T. HARRIS BLVD., 1ST FLOOR, CHARLOTTE, NC, 28262, UNITED STATES
Covered Properties
(62)
Waste Heat Recovery for Forced Convection Biomass Stove
Application:
13/189,257 →
Enhanced Radiative Transfer and Heat Recovery for Combustion Device
Application:
13/189,300 →
Catalyst, Gas Generator, and Thruster with Improved Thermal Capability and Corrosion Resistance
Application:
13/151,155 →
Energetic Adhesive for Venting Cookoff
Application:
61/450,332 →
Media Rotation and Translation Mechanism
Application:
13/030,503 →
Selectable Ramjet Propulsion System
Application:
61/442,929 →
Combined Cycle Integrated Combustor and Nozzle System
Application:
13/008,939 →
Co-Sintered Multi-System Tungsten Alloy Composite
Application:
12/952,426 →
Internal Resistive Heating of Catalyst Bed for Monopropellant Catalyst
Application:
12/948,558 →
Propulsion System With Movable Thermal Choke
Application:
12/811,910 →
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Application:
12/871,125 →
Cathode Heater
Application:
12/664,034 →
High Voltage Multiple Phase Power Supply
Application:
12/578,404 →
Propellant and Explosives Production Method by Use of Resonant Acoustic Mix Process
Application:
12/251,694 →
Wrench with Reinforced Hollow Handle
Application:
12/168,202 →
Slow Cook Off Rocket Igniter
Application:
12/148,027 →
Single Phase Tungsten Alloy for Shaped Charge Liner
Application:
12/043,593 →
Pintle-Controlled Propulsion System with External Ring Actuator
Application:
12/041,810 →
Multi-Functional Pulse-Divided Rocket
Application:
12/041,797 →
Rocket Nozzles for Unconventional Vehicles
Application:
12/072,487 →
Two-Piece Aft Closure for a Rocket Motor Case
Application:
11/953,717 →
Combined Cycle Missile Engine System
Application:
11/983,244 →
Co-Sintered Multi-System Tungsten Alloy Composite
Application:
11/811,949 →
Combined Cycle Integrated Combustor and Nozzle System
Application:
11/640,646 →
Core Burning for Scramjet Engines
Application:
11/582,589 →
Nozzle with Temperature-Responsive Throat Diameter
Application:
11/531,630 →
Pintle-Controlled Propulsion System with External Dynamic Seal
Application:
11/531,655 →
Hybrid fire extinguisher for extended suppression times
Application:
11/471,283 →
Helicon Hall Thruster
Application:
11/437,279 →
Piston Tank with Compound Piston for High Loading and Expulsion Efficiency
Application:
11/363,573 →
Nozzle Assembly for Rocket and Ramjet Applications
Application:
11/287,297 →
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Application:
11/233,401 →
Thrust Augmentation in Plug Nozzles and Expansion-Deflection Nozzles
Application:
11/226,127 →
Multiple Phase Power Supply for Rocket Engines
Application:
11/123,374 →
Single Phase Tungsten Alloy
Application:
10/837,516 →
Thrust Vector Control System for a Plug Nozzle Rocket Engine
Application:
10/823,380 →
Rocket Engine Chamber with Layered Internal Wall Channels
Application:
10/794,390 →
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Application:
10/784,482 →
Expander Cycle Rocket Engine with Staged Combustion and Heat Exchange
Application:
10/388,266 →
Destroying Airborne Biological and/or Chemical Agents with Solid Propellants
Application:
10/377,773 →
Solid Propellant Formulations and Methods and Devices Employing the Same for the Destruction of Airborne Biological and/or Chemical Agents
Application:
10/377,775 →
Rocket Motors Having Controlled Autoignition Propellant Systems
Application:
10/376,297 →
Diversion of Combustion Gas Within a Rocket Engine to Preheat Fuel
Application:
10/359,434 →
Nozzle with Spiral Internal Cooling Channels
Application:
10/308,645 →
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Application:
10/241,820 →
Controlled Autoignition Propellant Systems
Application:
10/200,597 →
Back Reamer Assembly
Application:
10/176,188 →
Solid Propellant Formulations and Methods and Devices Employing the Same for the Destruction of Airborne Biological and/or Chemical Agents
Application:
10/145,540 →
High Performance Rocket Engine Having a Stepped Expansion Combustion Chamber and Method of Making the Same
Application:
10/104,327 →
Fire Extinguisher
Application:
10/085,884 →
Apparatus and Method for Passive Venting of Rocket Motor or Ordnance Case
Application:
10/042,391 →
Nozzle Throat Area Control Apparatus and Method
Application:
10/038,858 →
Soft Shift System and Method
Application:
10/038,132 →
Hybrid Fire Extinguisher
Application:
09/937,868 →
Apparatus to Separate Gas from a Liquid Flow
Application:
09/952,709 →
Solid Rocket Motor Bolted Thrust Takeout Structure
Application:
09/910,440 →
Rocket Vehicle Thrust Augmentation Within Divergent Section of Nozzle
Application:
09/899,813 →
Shallow Depth, Coiled Tubing Horizontal Drilling System
Application:
09/896,025 →
Broken Shear Pin Indicating System
Application:
09/871,273 →
Low turbulence air blast system
Application:
09/840,247 →
Broom and Blower Control Method and Apparatus
Application:
09/840,501 →
Uniform Gas Distribution in Ion Accelerators with Closed Electron Drift
Application:
09/674,463 →