Patent Assignment
Reel/Frame 039594/0887
Release of Security Interest
Recorded: 2016-08-05
Pages: 20
Assignor
U.S. BANK NATIONAL ASSOCIATION
Executed: 2016-07-15
Assignee
AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION)
2001 AEROJET ROAD, RANCHO CORDOVA, CALIFORNIA, 95742
Covered Properties
(180)
Combustible Compositions for Air-Augmented Rocket Engines
Patent:
6,736,912 →
Application:
05/783,919 →
Coolable Rocket Nozzle for a Rocket Engine
Patent:
5,582,000 →
Application:
07/308,157 →
Rocket Nozzle for a Rocket Engine
Patent:
5,683,033 →
Application:
07/629,112 →
Ceramic Fibers Produced by Electrophoretic Deposition of Particles
Patent:
5,580,835 →
Application:
07/637,848 →
Rocket Engine Auxiliary Power System
Patent:
5,873,241 →
Application:
07/704,537 →
Cryogenic Fluid Manifold
Patent:
5,564,753 →
Application:
07/770,216 →
Energetic Plasticizers for Polybutadiene-Type Solid Propellant Binders
Patent:
5,578,789 →
Application:
07/878,222 →
Long Life Catalytic Gas Generator for Space Propulsion Applications
Patent:
5,568,723 →
Application:
07/941,620 →
Axially Fed Hydrostatic Bearing/Seal
Patent:
5,310,265 →
Application:
08/076,885 →
Method and Apparatus for Cutting Blocks of Solid Energetic Materials
Patent:
5,881,619 →
Application:
08/080,890 →
Apparatus and Method for Suppressing a Fire
Patent:
5,449,041 →
Application:
08/082,137 →
Arcjet Anode
Patent:
5,464,961 →
Application:
08/120,615 →
Catalytic Decomposition of Hydroxylammonium Nitrate-Based Monopropellants
Patent:
5,485,722 →
Application:
08/132,980 →
Stator Assembly for a Rotary Machine Having a Centrifugal on Impeller and Volute
Patent:
5,332,359 →
Application:
08/134,726 →
Multiple Pintle Nozzle Propulsion Control System
Patent:
5,456,425 →
Application:
08/147,591 →
Pressure-Fed Rocket Booster System
Patent:
5,444,973 →
Application:
08/166,425 →
Process for the Electrophoretic Deposition of Defect-Free Metallic Oxide Coatings
Patent:
5,415,748 →
Application:
08/200,611 →
Method of Simultaneously Forming Rocket Thrust Chamber Cooling Tubes
Patent:
5,477,613 →
Application:
08/213,306 →
Method of Making Cooled Rocket Combustion Chamber Construction
Patent:
5,473,817 →
Application:
08/213,391 →
Polymerization of Energetic, Cyclic Ether Monomers Using Boron Trifluoride Tetrahydrofuranate
Patent:
5,468,841 →
Application:
08/226,919 →
Apparatus for Suppressing a Fire
Patent:
5,423,384 →
Application:
08/248,932 →
Rocket Preburner Injector with Tailored Gas Temperature Profile
Patent:
5,566,544 →
Application:
08/250,243 →
Tube Rocket Thrust Chamber Construction and Method
Patent:
5,557,928 →
Application:
08/291,385 →
Self-Actuating Control for Rocket Motor Nozzle
Patent:
5,491,973 →
Application:
08/325,891 →
Fabrication of Rocket Thrust Chambers
Patent:
5,546,656 →
Application:
08/346,646 →
Scramjet Fuel Injection System Having Independent Fuel Supplies for Supersonic and Hypersonic Operation
Patent:
5,660,040 →
Application:
08/359,808 →
Polymers and Prepolymers from Mono-Substituted Fluorinated Oxetane Monomers
Patent:
5,807,977 →
Application:
08/371,914 →
Fire Suppressing Apparatus for Generating Steam from a Water-Ice Mixture
Patent:
5,465,795 →
Application:
08/415,802 →
Method for Making a Cobalt-Boride Dispersion-Strengthened Copper
Patent:
5,534,086 →
Application:
08/432,061 →
Preparation of Alumina-Silica Sol Gel Compositions
Patent:
5,591,380 →
Application:
08/437,486 →
Apparatus and Method for Suppressing a Fire
Patent:
5,609,210 →
Application:
08/468,678 →
3-Azidomethyl-3-Nitratomethyloxetane
Patent:
5,489,700 →
Application:
08/469,329 →
Solvent-Free Process for the Preparation of Mono-Substituted Fluorinated Oxetane Monomers
Patent:
6,037,483 →
Application:
08/477,168 →
Polyether Coprepolymers Formed from Mono-Substituted Fluorinated Oxetane Monomers and Tetrahydrofuran
Patent:
5,668,250 →
Application:
08/483,219 →
Gamma Strengthened Single Crystal Turbine Blade Alloy for Hydrogen Fueled Propulsion Systems
Patent:
5,679,180 →
Application:
08/493,610 →
Abrasion-Resistant and Low Friction Coating Compositions
Patent:
5,674,951 →
Application:
08/510,686 →
Preparation of Mono-Substituted Fluorinated Monomers and Tetrahydro- Furan
Patent:
5,668,251 →
Application:
08/539,405 →
Preparation of Mono-Substituted Fluorinated Oxetane Prepolymers
Patent:
5,650,483 →
Application:
08/539,555 →
Mono-Substituted Fluorinated Oxetane Monomers
Patent:
5,654,450 →
Application:
08/539,696 →
Parallel Arcjet Starter System
Patent:
5,605,039 →
Application:
08/543,659 →
Thermally Stable Gas Generating Composition
Patent:
5,641,938 →
Application:
08/582,079 →
Process for Preparing Spherical Energetic Compounds
Patent:
5,801,453 →
Application:
08/661,437 →
Low Temperature Autoigniting Propellant Composition
Patent:
5,866,842 →
Application:
08/683,286 →
Apparatus for Suppressing a Fire
Patent:
5,613,562 →
Application:
08/704,214 →
Rocket-Ramjet Engine Casing Port Closure
Patent:
5,784,877 →
Application:
08/745,641 →
Apparatus and Method for Simulating Rocket-to-Ramjet Transition in a Propulsion System
Patent:
5,831,155 →
Application:
08/758,867 →
A Closed Electron Drift Hall Effect Plasma Accelerator with All Magnetic Sources Located to the Rear of the Anode
Patent:
5,751,113 →
Application:
08/760,952 →
Hall Effect Plasma Accelerator
Patent:
5,847,493 →
Application:
08/761,948 →
Hall Effect Plasma Thruster
Patent:
5,845,880 →
Application:
08/763,692 →
Method of Inductive Bonding Sintered Compacts of Heavy Alloys
Patent:
5,760,378 →
Application:
08/843,903 →
Liquid Oxygen Gasifying System for Rocket Engines
Patent:
5,918,460 →
Application:
08/850,259 →
Method Manufacturing Solid Rocket Motors
Patent:
6,408,760 →
Application:
08/993,811 →
Apparatus for Preparing Spherical Energetic Compounds
Patent:
5,962,803 →
Application:
09/047,678 →
Three Axis Thruster
Patent:
6,173,565 →
Application:
09/058,314 →
Rocket Engine with One-Piece Combustion Chamber Step Structure, and Its Fabrication
Patent:
6,079,101 →
Application:
09/076,032 →
Hall Field Plasma Accelerator with an Inner and Outer Anode
Patent:
6,075,321 →
Application:
09/107,343 →
High Performance Rocket Engine Having a Stepped Expansion Combustion Chamber and Method of Making the Same
Patent:
6,397,580 →
Application:
09/112,390 →
Rocket Motor Case Using Plank Sections and Methods of Manufacturing
Patent:
7,484,353 →
Application:
09/119,516 →
Method and Apparatus for Selectively Distributing Power in a Thruster System
Patent:
6,031,334 →
Application:
09/143,294 →
Distributed Charge Inflator System
Patent:
6,062,143 →
Application:
09/149,630 →
Castable Double Base Solid Rocket Propellant Containing Ballistic Modifier Pasted in an Inert Polymer
Patent:
6,024,810 →
Application:
09/166,942 →
Hydrostatic Bearing with Compensatory Fluid Injection
Patent:
6,053,636 →
Application:
09/189,335 →
Magnetic Flux Shaping in Ion Accelerators with Closed Electron Drift
Patent:
6,208,080 →
Application:
09/191,749 →
Tandem Hall Field Plasma Accelerator
Patent:
6,150,764 →
Application:
09/215,598 →
Multistage Ion Accelerators with Closed Electron Drift
Patent:
6,215,124 →
Application:
09/251,530 →
Premixed Liquid Monopropellant Solutions and Mixtures
Patent:
6,984,273 →
Application:
09/363,013 →
Axial Flow Catalyst Pack
Patent:
6,746,651 →
Application:
09/371,973 →
Polyester with Partially Fluorinated Side Chains
Patent:
6,383,651 →
Application:
09/384,464 →
Radiation Curable Coating Containing Polyfuorooxetane
Patent:
6,673,889 →
Application:
09/397,715 →
Apparatus to Separate Gas from a Liquid Flow
Patent:
6,342,092 →
Application:
09/414,223 →
Method and Apparatus for Magnetic Voltage Isolation
Patent:
6,518,693 →
Application:
09/437,795 →
Monohydric Polyfluorooxetane Polymer and Radiation Curable Coatings Containing a Monofunctional Polyfluorooxetane Polymer
Patent:
6,403,760 →
Application:
09/473,518 →
Fluorinated Polyurethane Elastomers Prepared from Polyether Prepolymers Formed from Monosubstituted Fluorinated Oxetane Monomers and Tetrahydrofuran
Patent:
6,891,013 →
Application:
09/520,476 →
Fluorinated Polyurethane Elastomers Prepared from Polyether Prepolymers Formed from Mono-Substituted Fluorinated Oxetane Monomers
Patent:
6,417,314 →
Application:
09/520,815 →
Copolymers and coprepolymers formed from mono-substituted fluorinated oxetane monomers and tetrahydrofuran
Patent:
6,380,351 →
Application:
09/521,258 →
Polymers and Prepolymers Formed from Mono-Substituted Fluorinated Oxetane Monomers
Patent:
6,448,368 →
Application:
09/521,263 →
Amorphous Polyether Glycols Based on Bis-Substituted Oxetane Monomers
Patent:
6,479,623 →
Application:
09/615,160 →
Uniform Gas Distribution in Ion Accelerators with Closed Electron Drift
Patent:
6,612,105 →
Application:
09/674,463 →
Cured Polyesters Containing Fluorinated Side Chains
Patent:
6,686,051 →
Application:
09/698,554 →
Monohydric Polyfluorooxetane Oligomers, Polymers, and Copolymers and Coatings Containing the Same
Fluorinated Short Carbon Atom Side Chain and Polar Group Containing Polymer, and Flow, or Leveling, or Wetting Agents Thereof
Catalyst Bed
Gas Generator for Producing Adjustable Flow
Rocket Vehicle Thrust Augmentation Within Divergent Section of Nozzle
Method for Preparing Refractory Carbides
Solid Rocket Motor Bolted Thrust Takeout Structure
Hybrid Fire Extinguisher
Patent:
6,702,033 →
Application:
09/937,868 →
Apparatus to Separate Gas from a Liquid Flow
Adaptable Solid-Hybrid Rocket for Crew Escape and Orbital Injection Propulsion
Nozzle Throat Area Control Apparatus and Method
Heat Exchanger Panel
Rocket Propulsion System
Fire Extinguisher
Patent:
6,612,243 →
Application:
10/085,884 →
High Performance Rocket Engine Having a Stepped Expansion Combustion Chamber and Method of Making the Same
Monohydric Polyfluorooxetane Polymer and Radiation Curable Coatings Containing a Monofunctional Polyfluorooxetane Polymer
Monohydric Polyfluorooxetane Polymer and Radiation Curable Coatings Containing a Monofunctional Polyfluorooxetane Polymer
Scram Jet Engine Design
Solid Propellant Formulations and Methods and Devices Employing the Same for the Destruction of Airborne Biological and/or Chemical Agents
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Patent:
6,982,520 →
Application:
10/241,820 →
Variable Geometry Inlet Design for Scram Jet Engine
Cured Polyesters Containing Fluorinated Side Chains
Patent:
6,579,966 →
Application:
10/294,942 →
Nozzle with Spiral Internal Cooling Channels
Monohydric Polyfluorooxetane Oligomers, Polymers, and Copolymers and Coating Containing the Same
Diversion of Combustion Gas Within a Rocket Engine to Preheat Fuel
Hypergolic Fuel System
Expander Cycle Rocket Engine with Staged Combustion and Heat Exchange
Propulsion System with Integrated Rocket Accelerator
Rocket Engine Tubular Chamber with Single Piece Jacket
Rocket Engine Combustion Chamber
Coating Derived from Polyesters Crosslinked with Melamine Formaldehyde
Polymeric Surfactants Derived from Cyclic Monomers Having Pendant Fluorinated Carbon Groups
Fluorinated Thermoset Polyurethane Elastomers Prepared from Polyether Prepolymers Formed from Mono-Substituted Fluorinated Oxetane Monomers
Multichannel Hall Effect Thruster
Fluorinated Polymer and Amine Resin Compositions and Products Formed Therefrom
Enhanced Performance Torroidal Coolant-Collection Manifold
Rocket Engine Chamber with Layered Internal Wall Channels
Thrust Vector Control System for a Plug Nozzle Rocket Engine
Reduced Gain Thrust Control Valve
Cooling Scheme for Scramjet Variable Geometry Hardware
High Temperature Dynamic Seal for Scramjet Variable Geometry
Single Phase Tungsten Alloy
Polymeric Surfactants Derived from Cyclic Monomers Having Pendant Fluorinated Carbon Groups
Staged Emitter-Attractor Ion Drive
Energetic Detonation Propulsion
Cryogenic Insulation
Method of Making an Easily Cleanable Polymer Laminate
Method of Assembling a Rocket Engine with a Transition Zone Between the Combustion Chamber and the Coolant System
Cold Gas Dynamic Spraying of High Strength Copper
Amorphous Polyether Glycols Based on Bis-Substituted Oxetane and Tetrahydrofuran Monomers
Semi-Axisymmetric Scramjet Flowpath with Conformal Nozzle
Rocket Chamber Heat Exchanger
Multiple Phase Power Supply for Rocket Engines
Booster Rocket Engine Using Gaseous Hydrocarbon in Catalytically Enhanced Gas Generator Cycle
Thrust Augmentation in Plug Nozzles and Expansion-Deflection Nozzles
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Nozzle Assembly for Rocket and Ramjet Applications
Rocket Engine Combustion Chamber
Piston Tank with Compound Piston for High Loading and Expulsion Efficiency
Solar Tracker
Coaxial Ignition Assembly
Helicon Hall Thruster
Patent:
7,436,122 →
Application:
11/437,279 →
Heat Exchange Injector for Use in a Rocket Engine
High temperature molten salt receiver
Dual-Function Stirling Engine System
Three Component Injector for Kerosene-Oxygen Rocket Engine
Nozzle with Temperature-Responsive Throat Diameter
Core Burning for Scramjet Engines
Supercritical CO2 Turbine for Use in Solar Power Plants
Combined Cycle Integrated Combustor and Nozzle System
Co-Sintered Multi-System Tungsten Alloy Composite
Two-Piece Aft Closure for a Rocket Motor Case
Combined Cycle Missile Engine System
Multi-Functional Pulse-Divided Rocket
Pintle-Controlled Propulsion System with External Ring Actuator
Single Phase Tungsten Alloy for Shaped Charge Liner
Rocket Nozzles for Unconventional Vehicles
Recast Removal Method
Heat Exchanger for a Rocket Engine
Slow Cook Off Rocket Igniter
Fastener Assembly for Connecting Rocket Engine Nozzles
Conductive Emissions Protection
Nano-Grained Aluminum Alloy Bellows
High Voltage Multiple Phase Power Supply
Propulsion System With Movable Thermal Choke
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Patent:
43,731 →
Application:
12/871,125 →
Internal Resistive Heating of Catalyst Bed for Monopropellant Catalyst
Application:
12/948,558 →
Publication:
US 2011/0165030
Co-Sintered Multi-System Tungsten Alloy Composite
Application:
12/952,426 →
Publication:
US 2011/0064600
Combined Cycle Integrated Combustor and Nozzle System
Catalyst, Gas Generator, and Thruster with Improved Thermal Capability and Corrosion Resistance
Application:
13/151,155 →
Publication:
US 2012/0304620
Agglomerator with Ceramic Matrix Composite Obstacles
Waste Heat Recovery for Forced Convection Biomass Stove
Application:
13/189,257 →
Publication:
US 2013/0019849
Enhanced Radiative Transfer and Heat Recovery for Combustion Device
Application:
13/189,300 →
Publication:
US 2013/0019850
Cyclic Energetic Nitramines Desensitized with Linear Nitramines
Centrifugal Impeller
Application:
13/299,718 →
Publication:
US 2013/0129524
Energetic Adhesive for Venting Cookoff
Application:
13/415,155 →
Publication:
US 2012/0232189
Rocket Nozzles for Unconventional Vehicles
Injector Having Multiple Impingement Lengths
Application:
13/467,238 →
Publication:
US 2013/0074472
Inducer with Cavitation Instability Controls to Reduce Vibrations and Radial Loads
End-Burning Propellant Grain with Area-Enhanced Burning Surface
Mitigation of Orbiting Space Debris by Momentum Exchange with Drag-Inducing Particles
Application:
13/704,554 →
Publication:
US 2013/0181061
Related Assignments
(9)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Jul 8, 2013
From: UNITED TECHNOLOGIES CORPORATION
To: RPW ACQUISITION LLC
Reel/Frame 030750/0283 →
Merger/Change of Name
Jul 8, 2013
From: RPW ACQUISITION LLC
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 030754/0248 →
Change of Name
May 8, 2014
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 032845/0909 →
Merger and Change of Name
May 14, 2016
From: AEROJET-GENERAL CORPORATION; AEROJET ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 038596/0682 →
Notice of Succession of Agency (Intellectual Property)
Jun 20, 2016
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
To: BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
Reel/Frame 039079/0857 →
Release of Security Interest
Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0087 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0271 →
Termination and Release of Security Interest in Patents
Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0180 →