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Reel/Frame:064424/0271   Pages: 7
Recorded: 07/28/2023
Attorney Dkt #:017625.004996
Conveyance: TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS
Total properties: 26
1
Patent #:
6736912
Issue Dt:
05/18/2004
Application #:
05783919
Filing Dt:
03/24/1977
Title:
COMBUSTIBLE COMPOSITIONS FOR AIR-AUGMENTED ROCKET ENGINES
2
Patent #:
5784877
Issue Dt:
07/28/1998
Application #:
08745641
Filing Dt:
11/08/1996
Title:
ROCKET-RAMJET ENGINE CASING PORT CLOSURE
3
Patent #:
5831155
Issue Dt:
11/03/1998
Application #:
08758867
Filing Dt:
12/02/1996
Title:
APPARATUS AND METHOD FOR SIMULATING ROCKET-TO-RAMJET TRANSITION IN A PROPULSION SYSTEM
4
Patent #:
5760378
Issue Dt:
06/02/1998
Application #:
08843903
Filing Dt:
04/17/1997
Title:
METHOD OF INDUCTIVE BONDING SINTERED COMPACTS OF HEAVY ALLOYS
5
Patent #:
6024889
Issue Dt:
02/15/2000
Application #:
09015359
Filing Dt:
01/29/1998
Title:
CHEMICALLY ACTIVE FIRE SUPPRESSION COMPOSITION
6
Patent #:
6173565
Issue Dt:
01/16/2001
Application #:
09058314
Filing Dt:
04/09/1998
Title:
THREE AXIS THRUSTER
7
Patent #:
6397580
Issue Dt:
06/04/2002
Application #:
09112390
Filing Dt:
07/09/1998
Title:
HIGH PERFORMANCE ROCKET ENGINE HAVING A STEPPED EXPANSION COMBUSTION CHAMBER AND METHOD OF MAKING THE SAME
8
Patent #:
6031334
Issue Dt:
02/29/2000
Application #:
09143294
Filing Dt:
08/28/1998
Title:
METHOD AND APPARATUS FOR SELECTIVELY DISTRIBUTING POWER IN A THRUSTER SYSTEM
9
Patent #:
6024810
Issue Dt:
02/15/2000
Application #:
09166942
Filing Dt:
10/06/1998
Title:
CASTABLE DOUBLE BASE SOLID ROCKET PROPELLANT CONTAINING BALLISTIC MODIFIER PASTED IN AN INERT POLYMER
10
Patent #:
6208080
Issue Dt:
03/27/2001
Application #:
09191749
Filing Dt:
11/13/1998
Title:
MAGNETIC FLUX SHAPING IN ION ACCELERATORS WITH CLOSED ELECTRON DRIFT
11
Patent #:
6215124
Issue Dt:
04/10/2001
Application #:
09251530
Filing Dt:
02/17/1999
Title:
MULTISTAGE ION ACCELERATORS WITH CLOSED ELECTRON DRIFT
12
Patent #:
6746651
Issue Dt:
06/08/2004
Application #:
09371973
Filing Dt:
08/10/1999
Title:
AXIAL FLOW CATALYST PACK
13
Patent #:
6342092
Issue Dt:
01/29/2002
Application #:
09414223
Filing Dt:
10/07/1999
Title:
APPARATUS TO SEPARATE GAS FROM A LIQUID FLOW
14
Patent #:
6612105
Issue Dt:
09/02/2003
Application #:
09674463
Filing Dt:
01/29/2001
Title:
UNIFORM GAS DISTRIBUTION IN ION ACCELERATORS WITH CLOSED ELECTRON DRIFT
15
Patent #:
6568171
Issue Dt:
05/27/2003
Application #:
09899813
Filing Dt:
07/05/2001
Publication #:
US20030005701
Pub Dt:
01/09/2003
Title:
ROCKET VEHICLE THRUST AUGMENTATION WITHIN DIVERGENT SECTION OF NOZZLE
16
Patent #:
6547182
Issue Dt:
04/15/2003
Application #:
09910440
Filing Dt:
07/19/2001
Publication #:
US20030015623
Pub Dt:
01/23/2003
Title:
SOLID ROCKET MOTOR BOLTED THRUST TAKEOUT STRUCTURE
17
Patent #:
6432178
Issue Dt:
08/13/2002
Application #:
09952709
Filing Dt:
09/14/2001
Publication #:
US20020017196
Pub Dt:
02/14/2002
Title:
APPARATUS TO SEPARATE GAS FROM A LIQUID FLOW
18
Patent #:
6588199
Issue Dt:
07/08/2003
Application #:
10104327
Filing Dt:
03/22/2002
Publication #:
US20030074886
Pub Dt:
04/24/2003
Title:
HIGH PERFORMANCE ROCKET ENGINE HAVING A STEPPED EXPANSION COMBUSTION CHAMBER AND METHOD OF MAKING THE SAME
19
Patent #:
6808572
Issue Dt:
10/26/2004
Application #:
10145540
Filing Dt:
05/15/2002
Publication #:
US20040112487
Pub Dt:
06/17/2004
Title:
SOLID PROPELLANT FORMULATIONS AND METHODS AND DEVICES EMPLOYING THE SAME FOR THE DESTRUCTION OF AIRBORNE BIOLOGICAL AND/OR CHEMICAL AGENTS
20
Patent #:
6982520
Issue Dt:
01/03/2006
Application #:
10241820
Filing Dt:
09/10/2002
Title:
HALL EFFECT THRUSTER WITH ANODE HAVING MAGNETIC FIELD BARRIER
21
Patent #:
6802179
Issue Dt:
10/12/2004
Application #:
10308645
Filing Dt:
12/02/2002
Publication #:
US20040168428
Pub Dt:
09/02/2004
Title:
NOZZLE WITH SPIRAL INTERNAL COOLING CHANNELS
22
Patent #:
6799417
Issue Dt:
10/05/2004
Application #:
10359434
Filing Dt:
02/05/2003
Publication #:
US20040148923
Pub Dt:
08/05/2004
Title:
DIVERSION OF COMBUSTION GAS WITHIN A ROCKET ENGINE TO PREHEAT FUEL
23
Patent #:
6832471
Issue Dt:
12/21/2004
Application #:
10388266
Filing Dt:
03/12/2003
Publication #:
US20040177603
Pub Dt:
09/16/2004
Title:
EXPANDER CYCLE ROCKET ENGINE WITH STAGED COMBUSTION AND HEAT EXCHANGE
24
Patent #:
7216474
Issue Dt:
05/15/2007
Application #:
10784482
Filing Dt:
02/19/2004
Publication #:
US20060107648
Pub Dt:
05/25/2006
Title:
INTEGRATED AIR INLET SYSTEM FOR MULTI-PROPULSION AIRCRAFT ENGINES
25
Patent #:
7360488
Issue Dt:
04/22/2008
Application #:
10837516
Filing Dt:
04/30/2004
Publication #:
US20050241522
Pub Dt:
11/03/2005
Title:
SINGLE PHASE TUNGSTEN ALLOY
26
Patent #:
RE43731
Issue Dt:
10/16/2012
Application #:
12871125
Filing Dt:
08/30/2010
Title:
INTEGRATED AIR INLET SYSTEM FOR MULTI-PROPULSION AIRCRAFT ENGINES
Assignor
1
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
Exec Dt:
07/28/2023
Assignee
1
AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
P.O. BOX 13222
SACRAMENTO, CALIFORNIA 95813-6000
Correspondence name and address
MOORE & VAN ALLEN PLLC
100 NORTH TRYON STREET
SUITE 4700, ATTN: IP DEPARTMENT
CHARLOTTE, NC 28202

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