IP Library Assignment 064424/0180
Patent Assignment
Reel/Frame 064424/0180

Termination and Release of Security Interest in Patents

Recorded: 2023-07-28 Pages: 9
Covered Properties (49)
Combustible Compositions for Air-Augmented Rocket Engines
Patent: 6,736,912 →
Application: 05/783,919 →
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 →
Method of Inductive Bonding Sintered Compacts of Heavy Alloys
Patent: 5,760,378 →
Application: 08/843,903 →
Chemically Active Fire Suppression Composition
Patent: 6,024,889 →
Application: 09/015,359 →
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 →
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 →
Castable Double Base Solid Rocket Propellant Containing Ballistic Modifier Pasted in an Inert Polymer
Patent: 6,024,810 →
Application: 09/166,942 →
Magnetic Flux Shaping in Ion Accelerators with Closed Electron Drift
Patent: 6,208,080 →
Application: 09/191,749 →
Multistage Ion Accelerators with Closed Electron Drift
Patent: 6,215,124 →
Application: 09/251,530 →
Axial Flow Catalyst Pack
Patent: 6,746,651 →
Application: 09/371,973 →
Apparatus to Separate Gas from a Liquid Flow
Patent: 6,342,092 →
Application: 09/414,223 →
Uniform Gas Distribution in Ion Accelerators with Closed Electron Drift
Patent: 6,612,105 →
Application: 09/674,463 →
Rocket Vehicle Thrust Augmentation Within Divergent Section of Nozzle
Patent: 6,568,171 →
Application: 09/899,813 →
Publication: US 2003/0005701
Solid Rocket Motor Bolted Thrust Takeout Structure
Patent: 6,547,182 →
Application: 09/910,440 →
Publication: US 2003/0015623
Apparatus to Separate Gas from a Liquid Flow
Patent: 6,432,178 →
Application: 09/952,709 →
Publication: US 2002/0017196
High Performance Rocket Engine Having a Stepped Expansion Combustion Chamber and Method of Making the Same
Patent: 6,588,199 →
Application: 10/104,327 →
Publication: US 2003/0074886
Solid Propellant Formulations and Methods and Devices Employing the Same for the Destruction of Airborne Biological and/or Chemical Agents
Patent: 6,808,572 →
Application: 10/145,540 →
Publication: US 2004/0112487
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Patent: 6,982,520 →
Application: 10/241,820 →
Nozzle with Spiral Internal Cooling Channels
Patent: 6,802,179 →
Application: 10/308,645 →
Publication: US 2004/0168428
Diversion of Combustion Gas Within a Rocket Engine to Preheat Fuel
Patent: 6,799,417 →
Application: 10/359,434 →
Publication: US 2004/0148923
Expander Cycle Rocket Engine with Staged Combustion and Heat Exchange
Patent: 6,832,471 →
Application: 10/388,266 →
Publication: US 2004/0177603
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Patent: 7,216,474 →
Application: 10/784,482 →
Publication: US 2006/0107648
Single Phase Tungsten Alloy
Patent: 7,360,488 →
Application: 10/837,516 →
Publication: US 2005/0241522
Thrust Augmentation in Plug Nozzles and Expansion-Deflection Nozzles
Patent: 7,823,376 →
Application: 11/226,127 →
Publication: US 2007/0056261
Hall Effect Thruster with Anode Having Magnetic Field Barrier
Patent: 7,164,227 →
Application: 11/233,401 →
Publication: US 2006/0076872
Nozzle Assembly for Rocket and Ramjet Applications
Patent: 7,568,348 →
Application: 11/287,297 →
Publication: US 2007/0119151
Piston Tank with Compound Piston for High Loading and Expulsion Efficiency
Patent: 7,621,429 →
Application: 11/363,573 →
Publication: US 2007/0199957
Helicon Hall Thruster
Patent: 7,436,122 →
Application: 11/437,279 →
Nozzle with Temperature-Responsive Throat Diameter
Patent: 7,762,078 →
Application: 11/531,630 →
Publication: US 2009/0173077
Core Burning for Scramjet Engines
Patent: 7,797,943 →
Application: 11/582,589 →
Publication: US 2008/0092519
Combined Cycle Integrated Combustor and Nozzle System
Patent: 7,886,516 →
Application: 11/640,646 →
Publication: US 2009/0071120
Co-Sintered Multi-System Tungsten Alloy Composite
Patent: 8,486,541 →
Application: 11/811,949 →
Publication: US 2008/0102303
Two-Piece Aft Closure for a Rocket Motor Case
Patent: 7,717,280 →
Application: 11/953,717 →
Publication: US 2008/0143058
Combined Cycle Missile Engine System
Patent: 8,056,319 →
Application: 11/983,244 →
Publication: US 2009/0205311
Multi-Functional Pulse-Divided Rocket
Patent: 8,291,691 →
Application: 12/041,797 →
Publication: US 2011/0167794
Pintle-Controlled Propulsion System with External Ring Actuator
Patent: 8,016,211 →
Application: 12/041,810 →
Publication: US 2009/0230212
Single Phase Tungsten Alloy for Shaped Charge Liner
Patent: 7,921,778 →
Application: 12/043,593 →
Publication: US 2010/0275800
Rocket Nozzles for Unconventional Vehicles
Patent: 8,186,145 →
Application: 12/072,487 →
Publication: US 2009/0211258
Slow Cook Off Rocket Igniter
Patent: 7,762,195 →
Application: 12/148,027 →
Publication: US 2009/0044716
High Voltage Multiple Phase Power Supply
Patent: 8,572,945 →
Application: 12/578,404 →
Publication: US 2010/0263349
Propulsion System With Movable Thermal Choke
Patent: 8,763,361 →
Application: 12/811,910 →
Publication: US 2011/0023451
Integrated Air Inlet System for Multi-Propulsion Aircraft Engines
Patent: 43,731 →
Application: 12/871,125 →
Co-Sintered Multi-System Tungsten Alloy Composite
Application: 12/952,426 →
Publication: US 2011/0064600
Combined Cycle Integrated Combustor and Nozzle System
Patent: 8,701,379 →
Application: 13/008,939 →
Publication: US 2011/0107738
Catalyst, Gas Generator, and Thruster with Improved Thermal Capability and Corrosion Resistance
Application: 13/151,155 →
Publication: US 2012/0304620
Related Assignments (14)
Other recorded transfers of the patents in this record — the chain of ownership.
Merger Sep 5, 2013
From: AEROJET-GENERAL CORPORATION
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 031147/0333 →
Merger Dec 5, 2013
From: AEROJET-GENERAL CORPORATION
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 031726/0655 →
Merger and Change of Name May 14, 2016
From: AEROJET-GENERAL CORPORATION; AEROJET ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 038596/0682 →
Merger and Change of Name May 15, 2016
From: AEROJET-GENERAL CORPORATION; AEROJET-GENERAL CORPORATION
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 038596/0912 →
Change of Name May 17, 2016
From: PRIMEX AEROSPACE COMPANY
To: GENERAL DYNAMICS OTS (AEROSPACE), INC.
Reel/Frame 038621/0075 →
Assignment of Assignor's Interest May 17, 2016
From: STECHMAN, RUPERT C, JR; WOLL, PETER E; NEIDERMAN, JOEL M; JENSEN, JEFFREY J
To: KAISER AEROSPACE AND ELECTRONICS CORPORATION
Reel/Frame 038620/0714 →
Assignment of Assignor's Interest May 17, 2016
From: KAISER AEROSPACE & ELECTRONICS CORPORATION
To: BI-PROPELLANT ROCKET RESEARCH CORPORATION
Reel/Frame 038620/0876 →
Assignment of Assignor's Interest May 17, 2016
From: LICHON, PAUL G; ZUBE, DIETER M
To: PRIMEX AEROSPACE COMPANY
Reel/Frame 038620/0982 →
Assignment of Assignor's Interest May 18, 2016
From: FIGGE, IRVING EDWARD, SR; GRAHAM, PHILLIP HENRY
To: ATLANTIC RESEARCH CORPORATION
Reel/Frame 038634/0126 →
Assignment of Assignor's Interest Jun 17, 2016
From: HUGHES ELECTRONICS CORPORATION
To: THE BOEING COMPANY
Reel/Frame 038945/0604 →
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 →
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 064424/0238 →
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 →