Patent Assignment
Reel/Frame 030656/0667
Security Agreement
Recorded: 2013-06-21
Received: 2013-06-21
Pages: 22
Assignor
AEROJET-GENERAL CORPORATION
Executed: 2013-06-14
Assignee
U.S. BANK NATIONAL ASSOCIATION
ONE CALIFORNIA STREET, SUITE 1000, GLOBAL CORPORATE TRUST SERVICES, SAN FRANCISCO, CA, 95853-7012, UNITED STATES
Covered Properties
(100)
Method for Producing a Fragment / Reactive Material Assembly
Application:
61/788,608 →
Mitigation of Orbiting Space Debris by Momentum Exchange with Drag-Inducing Particles
Application:
13/704,554 →
End-Burning Propellant Grain with Area-Enhanced Burning Surface
Application:
13/703,787 →
Inducer with Cavitation Instability Controls to Reduce Vibrations and Radial Loads
Application:
13/493,554 →
Injector Having Multiple Impingement Lengths
Application:
13/467,238 →
Rocket Nozzles for Unconventional Vehicles
Application:
13/462,909 →
Energetic Adhesive for Venting Cookoff
Application:
13/415,155 →
Cyclic Energetic Nitramines Desensitized with Linear Nitramines
Application:
13/264,721 →
Selectable Ramjet Propulsion System
Application:
13/355,949 →
Centrifugal Impeller
Application:
13/299,718 →
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 →
Agglomerator with Ceramic Matrix Composite Obstacles
Application:
13/180,755 →
Catalyst, Gas Generator, and Thruster with Improved Thermal Capability and Corrosion Resistance
Application:
13/151,155 →
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 →
High Voltage Multiple Phase Power Supply
Application:
12/578,404 →
Nano-Grained Aluminum Alloy Bellows
Application:
12/234,851 →
Conductive Emissions Protection
Application:
12/212,975 →
Fastener Assembly for Connecting Rocket Engine Nozzles
Application:
12/189,587 →
Heat Exchanger for a Rocket Engine
Application:
12/147,396 →
Recast Removal Method
Application:
12/138,710 →
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 →
Supercritical CO2 Turbine for Use in Solar Power Plants
Application:
11/636,247 →
Core Burning for Scramjet Engines
Application:
11/582,589 →
Nozzle with Temperature-Responsive Throat Diameter
Application:
11/531,630 →
Three Component Injector for Kerosene-Oxygen Rocket Engine
Application:
11/516,417 →
Dual-Function Stirling Engine System
Application:
11/500,117 →
Heat Exchange Injector for Use in a Rocket Engine
Application:
11/479,082 →
High temperature molten salt receiver
Application:
11/479,635 →
Helicon Hall Thruster
Application:
11/437,279 →
Coaxial Ignition Assembly
Application:
11/414,605 →
Solar Tracker
Application:
11/376,849 →
Piston Tank with Compound Piston for High Loading and Expulsion Efficiency
Application:
11/363,573 →
Rocket Engine Combustion Chamber
Application:
11/296,961 →
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 →
Booster Rocket Engine Using Gaseous Hydrocarbon in Catalytically Enhanced Gas Generator Cycle
Application:
11/175,671 →
Multiple Phase Power Supply for Rocket Engines
Application:
11/123,374 →
Rocket Chamber Heat Exchanger
Application:
11/011,314 →
Amorphous Polyether Glycols Based on Bis-Substituted Oxetane and Tetrahydrofuran Monomers
Application:
10/999,362 →
Semi-Axisymmetric Scramjet Flowpath with Conformal Nozzle
Application:
10/999,602 →
Cold Gas Dynamic Spraying of High Strength Copper
Application:
10/995,876 →
Method of Assembling a Rocket Engine with a Transition Zone Between the Combustion Chamber and the Coolant System
Application:
10/985,273 →
Method of Making an Easily Cleanable Polymer Laminate
Application:
10/966,528 →
Cryogenic Insulation
Application:
10/927,978 →
Staged Emitter-Attractor Ion Drive
Application:
10/895,775 →
Energetic Detonation Propulsion
Application:
10/895,777 →
Polymeric Surfactants Derived from Cyclic Monomers Having Pendant Fluorinated Carbon Groups
Application:
10/882,738 →
Single Phase Tungsten Alloy
Application:
10/837,516 →
Cooling Scheme for Scramjet Variable Geometry Hardware
Application:
10/829,890 →
High Temperature Dynamic Seal for Scramjet Variable Geometry
Application:
10/830,272 →
Reduced Gain Thrust Control Valve
Application:
10/825,254 →
Thrust Vector Control System for a Plug Nozzle Rocket Engine
Application:
10/823,380 →
Coating Derived from Polyesters Crosslinked with Melamine Formaldehyde
Application:
10/492,572 →
Rocket Engine Chamber with Layered Internal Wall Channels
Application:
10/794,390 →
Enhanced Performance Torroidal Coolant-Collection Manifold
Application:
10/777,435 →
Fluorinated Polymer and Amine Resin Compositions and Products Formed Therefrom
Application:
10/774,187 →
Multichannel Hall Effect Thruster
Application:
10/726,398 →
Fluorinated Thermoset Polyurethane Elastomers Prepared from Polyether Prepolymers Formed from Mono-Substituted Fluorinated Oxetane Monomers
Application:
10/678,663 →
Polymeric Surfactants Derived from Cyclic Monomers Having Pendant Fluorinated Carbon Groups
Application:
10/657,056 →
Rocket Engine Combustion Chamber
Application:
10/458,123 →
Rocket Engine Tubular Chamber with Single Piece Jacket
Application:
10/456,824 →
Propulsion System with Integrated Rocket Accelerator
Application:
10/414,321 →
Expander Cycle Rocket Engine with Staged Combustion and Heat Exchange
Application:
10/388,266 →
Hypergolic Fuel System
Application:
10/386,308 →
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 →
Monohydric Polyfluorooxetane Oligomers, Polymers, and Copolymers and Coating Containing the Same
Application:
10/316,412 →
Rocket Propulsion System
Application:
10/065,968 →
Nozzle with Spiral Internal Cooling Channels
Application:
10/308,645 →
Cured Polyesters Containing Fluorinated Side Chains
Application:
10/294,942 →
Variable Geometry Inlet Design for Scram Jet Engine
Application:
10/264,172 →
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Application:
10/241,820 →
Controlled Autoignition Propellant Systems
Application:
10/200,597 →
Solid Propellant Formulations and Methods and Devices Employing the Same for the Destruction of Airborne Biological and/or Chemical Agents
Application:
10/145,540 →
Scram Jet Engine Design
Application:
10/112,635 →
Monohydric Polyfluorooxetane Polymer and Radiation Curable Coatings Containing a Monofunctional Polyfluorooxetane Polymer
Application:
10/108,916 →
Monohydric Polyfluorooxetane Polymer and Radiation Curable Coatings Containing a Monofunctional Polyfluorooxetane Polymer
Application:
10/108,318 →
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 →
Heat Exchanger Panel
Application:
10/058,621 →
Nozzle Throat Area Control Apparatus and Method
Application:
10/038,858 →
Hybrid Fire Extinguisher
Application:
09/937,868 →
Adaptable Solid-Hybrid Rocket for Crew Escape and Orbital Injection Propulsion
Application:
09/996,532 →
Apparatus to Separate Gas from a Liquid Flow
Application:
09/952,709 →
Solid Rocket Motor Bolted Thrust Takeout Structure
Application:
09/910,440 →
Method for Preparing Refractory Carbides
Application:
09/906,198 →