Patent Assignment
Reel/Frame 064424/0087
Termination and Release of Security Interest in Patents
Recorded: 2023-07-28
Pages: 8
Assignor
Assignee
AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
P.O. BOX 13222, SACRAMENTO, CALIFORNIA, 95813-6000
Covered Properties
(41)
Rocket Engine Auxiliary Power System
Patent:
5,873,241 →
Application:
07/704,537 →
Method and Apparatus for Cutting Blocks of Solid Energetic Materials
Patent:
5,881,619 →
Application:
08/080,890 →
Process for Preparing Spherical Energetic Compounds
Patent:
5,801,453 →
Application:
08/661,437 →
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 →
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 →
Hydrostatic Bearing with Compensatory Fluid Injection
Patent:
6,053,636 →
Application:
09/189,335 →
Catalyst Bed
Gas Generator for Producing Adjustable Flow
Method for Preparing Refractory Carbides
Heat Exchanger Panel
Variable Geometry Inlet Design for Scram Jet Engine
Hypergolic Fuel System
Propulsion System with Integrated Rocket Accelerator
Rocket Engine Tubular Chamber with Single Piece Jacket
Rocket Engine Combustion Chamber
Multichannel Hall Effect Thruster
Enhanced Performance Torroidal Coolant-Collection Manifold
Reduced Gain Thrust Control Valve
Cooling Scheme for Scramjet Variable Geometry Hardware
High Temperature Dynamic Seal for Scramjet Variable Geometry
Staged Emitter-Attractor Ion Drive
Energetic Detonation Propulsion
Cryogenic Insulation
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
Semi-Axisymmetric Scramjet Flowpath with Conformal Nozzle
Rocket Chamber Heat Exchanger
Booster Rocket Engine Using Gaseous Hydrocarbon in Catalytically Enhanced Gas Generator Cycle
Rocket Engine Combustion Chamber
Coaxial Ignition Assembly
Heat Exchange Injector for Use in a Rocket Engine
Dual-Function Stirling Engine System
Three Component Injector for Kerosene-Oxygen Rocket Engine
Recast Removal Method
Fastener Assembly for Connecting Rocket Engine Nozzles
Conductive Emissions Protection
Nano-Grained Aluminum Alloy Bellows
Related Assignments
(7)
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 →
Assignment of Assignor's Interest
May 17, 2016
From: GUIMONT, JOHN
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 038621/0131 →
Assignment of Assignor's Interest
May 18, 2016
From: GUIMONT, JOHN
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 038638/0517 →
Assignment of Assignor's Interest
Jun 6, 2016
From: BECKEL, STEPHEN A; BLEVINS, JAMES D; VERDI, THOMAS
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 038821/0598 →
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, INC. (F/K/A AEROJET-GENERAL CORPORATION)
Reel/Frame 039594/0887 →