Patent Assignment
Reel/Frame 030628/0319
Security Agreement
Recorded: 2013-06-17
Received: 2013-06-17
Pages: 12
Assignor
AEROJET-GENERAL CORPORATION
Executed: 2013-06-14
Assignee
WELLS FARGO BANK, NATIONAL ASSOCIATION
1525 WEST W.T. HARRIS BLVD., MAIL CODE NC 0680, CHARLOTTE, NC, 28262, UNITED STATES
Covered Properties
(43)
Injector Having Multiple Impingement Lengths
Application:
13/467,238 →
Centrifugal Impeller
Application:
13/299,718 →
Targets for Heliostat Health Monitoring
Application:
13/286,185 →
Agglomerator with Ceramic Matrix Composite Obstacles
Application:
13/180,755 →
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 →
Recast Removal Method
Application:
12/138,710 →
Supercritical CO2 Turbine for Use in Solar Power Plants
Application:
11/636,247 →
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 →
Coaxial Ignition Assembly
Application:
11/414,605 →
Solar Tracker
Application:
11/376,849 →
Rocket Engine Combustion Chamber
Application:
11/296,961 →
Booster Rocket Engine Using Gaseous Hydrocarbon in Catalytically Enhanced Gas Generator Cycle
Application:
11/175,671 →
Rocket Chamber Heat Exchanger
Application:
11/011,314 →
Current Threshold Circuit
Application:
11/009,110 →
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 →
Cryogenic Insulation
Application:
10/927,978 →
Staged Emitter-Attractor Ion Drive
Application:
10/895,775 →
Energetic Detonation Propulsion
Application:
10/895,777 →
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 →
Enhanced Performance Torroidal Coolant-Collection Manifold
Application:
10/777,435 →
Multichannel Hall Effect Thruster
Application:
10/726,398 →
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 →
Hypergolic Fuel System
Application:
10/386,308 →
Rocket Propulsion System
Application:
10/065,968 →
Variable Geometry Inlet Design for Scram Jet Engine
Application:
10/264,172 →
Changeable Means for Different Total Tracks and Its Method
Application:
10/174,920 →
Scram Jet Engine Design
Application:
10/112,635 →
Heat Exchanger Panel
Application:
10/058,621 →
Adaptable Solid-Hybrid Rocket for Crew Escape and Orbital Injection Propulsion
Application:
09/996,532 →
Method for Preparing Refractory Carbides
Application:
09/906,198 →
Catalyst Bed
Application:
09/896,355 →
Gas Generator for Producing Adjustable Flow
Application:
09/896,608 →