Patent Assignment
Reel/Frame 076068/0283
Assignment of Assignor's Interest
Recorded: 2026-07-27
Pages: 31
Assignors
L3HARRIS TECHNOLOGIES, INC.
Executed: 2026-07-25
AEROJET ROCKETDYNE, INC.
Executed: 2026-07-25
AEROJET ROCKETDYNE OF DE, INC.
Executed: 2026-07-25
L3HARRIS CINCINNATI ELECTRONICS CORPORATION
Executed: 2026-07-25
Assignee
ROCKETFORCE TECHNOLOGIES LLC
1025 W. NASA BLVD., MELBOURNE, FLORIDA, 32919
Covered Properties
(83)
Push-Pull Valve
Application:
18/861,333 →
Publication:
US US20250283553A1
Dual Active Bridge Powered Heaterless Hall Effect Thruster Configuration
Application:
19/150,649 →
Satellite De-Orbiting System
Application:
19/131,612 →
Publication:
US US20260184444A1
Pressure-Balanced Valve
Application:
19/136,952 →
Publication:
US US20260201979A1
Method of Manufacture for Hydrazine Composition
Application:
19/144,970 →
Publication:
US US20260217531A1
Hall Thruster with Electrical Isolation
Application:
19/483,281 →
Dielectric Barrier Discharge Device Configurations
Application:
18/901,527 →
Publication:
US US20260096003A1
Dielectric Barrier Discharge Device Configurations
Application:
18/901,402 →
Publication:
US US20260096002A1
Electric Thruster with Hexaboride Emitter
Application:
63/767,164 →
Electric Thruster with Hexaboride Emitter
Application:
19/318,682 →
Publication:
US US20260266270A1
Electric Thruster with Protective Coating on Thermionic Emitter
Application:
63/767,171 →
Electric Thruster with Protective Coating on Thermionic Emitter
Application:
19/307,369 →
Publication:
US US20260264890A1
Method and Apparatus for Controlling Paralleled Power Supplies
Application:
19/008,760 →
Publication:
US US20260196829A1
High-Temperature Spring for Dynamic Catalyst Rocket Engine
Application:
19/516,290 →
Enhanced Performance Torroidal Coolant-Collection Manifold
Deployable Electromagnetic Concentrator
Characteristic X-Ray Computed Laminography System for Home Made Explosives (Hme) Detection
Fastener Assembly for Connecting Rocket Engine Nozzles
Conductive Emissions Protection
Solid state heat pipe heat rejection system for space power systems
Nitrous Oxide System for Producing Breathing Air
Panel Assembly for a Space-Based Power Generation System
Cooling Device and Method with Synthetic Jet Actuator
Nuclear Fuel
Center-Tapped Solar Array and Power Distribution System for Same
Launch Abort and Orbital Maneuver System
Charge Balancing Topology
Power Converter
Thermoelectric Power Converter Support Structure
Apparatus for Electrical Isolation of Metallic Hardware
Fluid Separation System with Reduced Fouling
A Method of Assembling a Thermal Expansion Compensator
System for Bypassing and Isolating Electrical Power Cells
Ground Based Systems and Methods for Testing Reaction Thrusters
Hydroxylammonium Nitrate Monopropellant with Burn Rate Modifier
Electric Propulsion Power Circuit
Valve Assembly with Adjustable Spring Seat
Magnetic Latch Valve
Magnetic Latch Throttle Valve
Method and Composition for Moderated Nuclear Fuel
Dual Stage Catalytic Thruster
Propulsion System with Differential Throttling of Electric Thrusters
Solar Array Deployment
Short Circuit Protection for Switching Power Converters
Liquid Propellant Rocket Engine Nozzle with Passive Condensate Cooling
Copper Combustion Chamber Attached to Injector by Non-Copper Weld Transition Ring
Load Impedance Tester and Measurement Method
Power Converter Including a Recirculating Snubber
Hall Thruster with Annular Cathode
System and Method for Performing Layer Optimization of Stacked Resistive Random-Access Memory Device by Using Artificial Intelligence Technology
Electric Propulsion System Including Heaterless Dispenser Cathode
Electric Propulsion System Including Heaterless Dispenser Cathode
Catalytic Thruster
Reconfigurable Power Processing Unit for Spacecraft Operations
Catalyst-Containing Material
Shoot Through Current Detection and Protection Circuit
Satellite Including Crossover Power Processing Units for Electric Thrusters
Fuel-Isolation System Having Rupture Diaphragm
Dual Core Shoot-Through Protection Inductor Topology
Dynamic Quick Connector Coupling
Thermally Activatable Valve
Warm Gas Thruster System with Control Valve That Has a Soft Seal
Shoot-Through Protection Circuit
Planar Transformer
Magnetically Isolated Feedback Circuits and Regulated Power Supplies Incorporating the Same
Power Switching Circuits Having a Saturable Inductor
Capacitively Isolated Feedback Circuits and Regulated Power Supplies Incorporating the Same
Magnetically Saturable Components and Circuits
Energy-Harvesting Power Supplies
Satellite Onboard Imaging Systems and Methods for Space Applications
Time Synchronization for Computational System
Switching Power Supply Rectifier with Voltage Clamps to Clamp Voltage Transients on Output Coil of Transformer
Patent:
11,646,652 →
Application:
17/667,860 →
Hysteretic Power Supply Control Method
Frequency Tuned Resistor-Inductor-Capacitor Snubber for Switching Power Supply
Injector Assembly for a Rocket Engine
Rocket Engine Coolant System Including An Exit Manifold Having at Least One Flow Guide within the Manifold
Rocket Engine Pressure Sense Line
Rocket Thruster Nozzle with Connectors and Brace
Dual Active Bridge Powered Heaterless Hall Effect Thruster Configuration
PCT:
PCT/US2023/011920 ↗
Satellite De-Orbiting System
PCT:
PCT/US2023/014689 ↗
Method of Manufacture for Hydrazine Composition
PCT:
PCT/US2023/025837 ↗
Hall Thruster with Electrical Isolation
PCT:
PCT/US2023/027097 ↗
High-Temperature Spring for Dynamic Catalyst Rocket Engine
PCT:
PCT/US2023/081332 ↗
Related Assignments
(25)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Feb 12, 2004
From: CLARK, JIM A.; RICCIARDO, MARK
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 014987/0995 →
Assignment of Assignor's Interest
Aug 27, 2004
From: CARROLL, JOSEPH P.; MCCLANAHAN, JAMES A.
To: BOEING COMPANY THE
Reel/Frame 015745/0436 →
Assignment of Assignor's Interest
Mar 27, 2006
From: BOEING COMPANY AND BOEING MANAGEMENT COMPANY, THE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 017681/0537 →
Assignment of Assignor's Interest
May 16, 2006
From: BOEING C OMPANY AND BOEING MANAGEMENT COMPANY, THE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 017882/0126 →
Confirmatory License
May 30, 2006
From: UNITED TECHNOLOGIES CORPORATION, F29601-03-C-0147 (THE BOEING COMPANY, PRIME CONTRACTOR)
To: AIR FORCE, UNITED STATES
Reel/Frame 017927/0920 →
Assignment of Assignor's Interest
Oct 1, 2007
From: JOHNSON, GREGORY A.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 019900/0659 →
Assignment of Assignor's Interest
Aug 11, 2008
From: JOHNSON, BRADLEY C.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 021369/0358 →
Assignment of Assignor's Interest
Sep 18, 2008
From: HERTEL, THOMAS A.; SOENDKER, ERICH H.; SALDIVAR, HORACIO
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 021550/0657 →
Assignment of Assignor's Interest
Sep 30, 2008
From: LU, CHENG-YI; MCCLANAHAN, JAMES A.; CARROLL, JOSEPH P.; DETERMAN, WILLIAM
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 021681/0448 →
Assignment of Assignor's Interest
Jul 28, 2009
From: GERLACH, DAVID W.
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 023013/0208 →
Assignment of Assignor's Interest
Jul 31, 2009
From: LU, CHEN-YI; WAIT, DAVID; SUTIN, BRIAN M.; HOWERTON, RICK L.
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 023034/0928 →
Assignment of Assignor's Interest
Oct 3, 2011
From: HAMILTON SUNDSTRAND CORPORATION
To: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.
Reel/Frame 027006/0424 →
Assignment of Assignor's Interest
Dec 13, 2011
From: LARIVIERE, BRIAN W.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 027378/0137 →
Assignment of Assignor's Interest
Sep 6, 2012
From: PAPROTNA CUNHA, LINDA A.
To: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.
Reel/Frame 028906/0840 →
Corrective Assignment to Correct the Assignor Improperly Recorded as Linda a. Paprotna Cunha Previously Recorded on Reel 028906 Frame 0840. Assignor(S) Hereby Confirms the Assignor Hamilton Sundstrand Corporation.
Oct 3, 2012
From: HAMILTON SUNDSTRAND CORPORATION
To: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.
Reel/Frame 029067/0180 →
Assignment of Assignor's Interest
Nov 8, 2012
From: HAMILTON SUNDSTRAND CORPORATION
To: PRATT & WHITNEY, ROCKETDYNE, INC.
Reel/Frame 029293/0682 →
Corrective Assignment to Correct the Assignee's Name on Original Cover Sheet Previously Recorded on Reel 017882 Frame 0126. Assignor(S) Hereby Confirms the Assignee Was Incorrectly Recorded as "United Technologies Corporation". Assignee Should Be "Ruby Acquisition Enterprises Co.".
Jun 12, 2013
From: THE BOEING COMPANY AND BOEING MANAGEMENT COMPANY
To: RUBY ACQUISITION ENTERPRISES CO.
Reel/Frame 030592/0954 →
Change of Name
Jun 12, 2013
From: RUBY ACQUISITION ENTERPRISES CO.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 030593/0055 →
Security Agreement
Jun 17, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0408 →
Security Agreement
Jun 17, 2013
From: AEROJET-GENERAL CORPORATION
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0319 →
Assignment of Assignor's Interest
Jun 19, 2013
From: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 030644/0677 →
Security Agreement
Jun 21, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0615 →
Security Agreement
Jun 21, 2013
From: AEROJET-GENERAL CORPORATION
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0667 →
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 →