using auxiliary rocket nozzles

Industry

CPC
F02K9/88

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Parent Industries

FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F02Combustion engines F02KJET-PROPULSION PLANTS F02K9/00Rocket- engine plants

Current Industry

F02K9/88using auxiliary rocket nozzles

Industries

Patents Grantslast 30 patents

Information Patent Grant
Non-axisymmetric heat shield, a nozzle defined at least partially b...
- Patent number 12,163,491
- Issue date Dec 10, 2024
- Thomas Ryan McCullough
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Annular aerospike nozzle with widely-spaced thrust chambers, engine...
- Patent number 12,152,553
- Issue date Nov 26, 2024
- Thomas Ryan McCullough
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Ring-shaped booster rocket
- Patent number 11,852,103
- Issue date Dec 26, 2023
- Raytheon Company
- Ryan Starkey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Ring-shaped booster rocket
- Patent number 11,732,677
- Issue date Aug 22, 2023
- Raytheon Company
- Ryan Starkey
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Chemical and cold gas propellant systems and methods
- Patent number 11,346,306
- Issue date May 31, 2022
- Ball Aerospace & Technologies Corp.
- Gordon C. Wu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Device and system for controlling missiles and kill vehicles operat...
- Patent number 11,084,605
- Issue date Aug 10, 2021
- BAYERN-CHEMIE GESELLSCHAFT FÜR FLUGCHEMISCHE ANTRIEBE MBH
- Jürgen Ramsel
- F41 - WEAPONS
Information Patent Grant
Small satellite propulsion system
- Patent number 10,940,961
- Issue date Mar 9, 2021
- Lloyd J. Droppers
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Microfluidic homogeneous catalyzation systems and methods, and appa...
- Patent number 10,794,332
- Issue date Oct 6, 2020
- The University of Vermont and State Agricultural College
- Kevin R. Gagne
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Deflector for a thrust flow powered vehicle and thrust flow powered...
- Patent number 10,774,785
- Issue date Sep 15, 2020
- MBDA UK LIMITED
- Ross William Poulton
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integrated thruster
- Patent number 10,662,898
- Issue date May 26, 2020
- Raytheon Company
- Matthew H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Grant
Vectored-thrust propulsor
- Patent number 10,018,153
- Issue date Jul 10, 2018
- Vladimir E. Ivanov
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet propulsion device and fuel supply method
- Patent number 9,771,897
- Issue date Sep 26, 2017
- SNECMA
- Nicolas Soulier
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Cryogenic thruster assembly using regenerative heating from main an...
- Patent number 9,446,862
- Issue date Sep 20, 2016
- SNECMA
- Jean-Luc Barthoulot
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rocket nozzles for unconventional vehicles
- Patent number 8,601,787
- Issue date Dec 10, 2013
- Aerojet-General Corporation
- Melvin J. Bulman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control and/or drive device for a flying body
- Patent number 8,245,496
- Issue date Aug 21, 2012
- Astrium GmbH
- Thomas Maier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket nozzles for unconventional vehicles
- Patent number 8,186,145
- Issue date May 29, 2012
- Aerojet-General Corporation
- Melvin J. Bulman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Control and/or drive device for a flying body
- Patent number 7,707,820
- Issue date May 4, 2010
- Astrium GmbH
- Thomas Maier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dual-mode chemical-electric thrusters for spacecraft
- Patent number 7,703,273
- Issue date Apr 27, 2010
- Gregory G. Spanjers
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Side thruster module
- Patent number 7,610,747
- Issue date Nov 3, 2009
- Agency for Defense Development
- Won-Hoon Kim
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Rocket engine having guide vanes in the nozzle of the engine
- Patent number 7,478,778
- Issue date Jan 20, 2009
- Nammo Raufoss AS
- Erland Ørbekk
- F42 - AMMUNITION BLASTING
Information Patent Grant
Fluidic diverter valve with a variable valve-bore clearance
- Patent number 7,051,512
- Issue date May 30, 2006
- Honeywell International, Inc.
- Donald J. Christensen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Fluent control valve
- Patent number 6,988,705
- Issue date Jan 24, 2006
- Karl V. Hoose
- Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC
Information Patent Grant
Side thruster valve and side thruster device
- Patent number 6,986,246
- Issue date Jan 17, 2006
- Mitsubishi Heavy Industries, Ltd.
- Toshiharu Fujita
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aerospike augmentation of microthruster impulse
- Patent number 6,487,844
- Issue date Dec 3, 2002
- TRW Inc.
- Peter D. Lohn
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Hybrid rocket propulsion system including array of hybrid or fluid...
- Patent number 6,393,830
- Issue date May 28, 2002
- Alliant Techsystems Inc.
- Rolf E. Hamke
- F42 - AMMUNITION BLASTING
Information Patent Grant
Lateral-thrust control arrangement for missiles with solid-fuel hot...
- Patent number 6,289,669
- Issue date Sep 18, 2001
- LKF Lenkflugkörpersysteme GmbH
- Karl Smirra
- F42 - AMMUNITION BLASTING
Information Patent Grant
Multiple pintle nozzle propulsion control system
- Patent number 5,456,425
- Issue date Oct 10, 1995
- Aerojet-General Corporation
- Joseph W. Morris
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket engine expansion nozzle with complementary annular nozzle
- Patent number 5,067,316
- Issue date Nov 26, 1991
- Societe Europeene De Propulsion
- Claude E. Bonniot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Reaction control system
- Patent number 4,955,558
- Issue date Sep 11, 1990
- British Aerospace Public Limited Company
- Anthony Machell
- F42 - AMMUNITION BLASTING
Information Patent Grant
Reaction jet control system
- Patent number 4,856,734
- Issue date Aug 15, 1989
- Plessey Overseas Limited
- Guy E. Davies
- F42 - AMMUNITION BLASTING

Patents Applicationslast 30 patents

Information Patent Application
A NON-AXISYMMETRIC HEAT SHIELD, A NOZZLE DEFINED AT LEAST PARTIALLY...
- Publication number 20240208676
- Publication date Jun 27, 2024
- STOKE Space Technologies, Inc.
- Thomas Ryan McCullough
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
JET PROPULSION DEVICE AND FUEL SUPPLY METHOD
- Publication number 20140260181
- Publication date Sep 18, 2014
- SNECMA
- Nicolas Soulier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VECTORED-THRUST PROPULSOR
- Publication number 20140223915
- Publication date Aug 14, 2014
- Vladimir E. Ivanov
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CRYOGENIC THRUSTER ASSEMBLY
- Publication number 20140203148
- Publication date Jul 24, 2014
- SNECMA
- Jean-Luc Barthoulot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY
- Publication number 20130340407
- Publication date Dec 26, 2013
- FIRESTAR ENGINEERING, LLC
- David J. Fisher
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Rocket Nozzles for Unconventional Vehicles
- Publication number 20120233983
- Publication date Sep 20, 2012
- Aerojet-General Corporation
- Melvin J. Bulman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR MANEUVERING ROCKETS
- Publication number 20100275576
- Publication date Nov 4, 2010
- Technion Research & Development Foundation Ltd.
- Shaul Gutman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONTROL AND/OR DRIVE DEVICE FOR A FLYING BODY
- Publication number 20100170223
- Publication date Jul 8, 2010
- Astrium GmbH
- Thomas MAIER
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Satellite Control
- Publication number 20090299553
- Publication date Dec 3, 2009
- INMARSAT GLOBAL LIMITED
- Dean Richard HOPE
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Rocket nozzles for unconventional vehicles
- Publication number 20090211258
- Publication date Aug 27, 2009
- Aerojet-General Corporation, a corporation of the State of Ohio.
- Melvin J. Bulman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Dual-mode chemical-electric thrusters for spacecraft
- Publication number 20090139206
- Publication date Jun 4, 2009
- Gregory G. Spanjers
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FORCE BALANCED BUTTERFLY PROPORTIONAL HOT GAS VALVE
- Publication number 20080302991
- Publication date Dec 11, 2008
- Honeywell International, Inc.
- Raymond R. Tseng
- F42 - AMMUNITION BLASTING
Information Patent Application
Side thruster module
- Publication number 20070193250
- Publication date Aug 23, 2007
- AGENCY FOR DEFENSE DEVELOPMENT
- Won-Hoon Kim
- F42 - AMMUNITION BLASTING
Information Patent Application
Rocket engine having guide vanes in the nozzle of the engine
- Publication number 20070152096
- Publication date Jul 5, 2007
- Erland Ørbekk
- F42 - AMMUNITION BLASTING
Information Patent Application
Control and/or drive device for a flying body
- Publication number 20060059888
- Publication date Mar 23, 2006
- EADS SPACE TRANSPORTATION GmbH
- Thomas Maier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FLUIDIC DIVERTER VALVE WITH A VARIABLE VALVE-BORE CLEARANCE
- Publication number 20050150207
- Publication date Jul 14, 2005
- Donald J. Christensen
- F42 - AMMUNITION BLASTING
Information Patent Application
Side thruster valve and side thruster device
- Publication number 20030217547
- Publication date Nov 27, 2003
- Toshiharu Fujita
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

using auxiliary rocket nozzles

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Non-axisymmetric heat shield, a nozzle defined at least partially b...

Annular aerospike nozzle with widely-spaced thrust chambers, engine...

Ring-shaped booster rocket

Ring-shaped booster rocket

Chemical and cold gas propellant systems and methods

Device and system for controlling missiles and kill vehicles operat...

Small satellite propulsion system

Microfluidic homogeneous catalyzation systems and methods, and appa...

Deflector for a thrust flow powered vehicle and thrust flow powered...

Integrated thruster

Vectored-thrust propulsor

Jet propulsion device and fuel supply method

Cryogenic thruster assembly using regenerative heating from main an...

Rocket nozzles for unconventional vehicles

Control and/or drive device for a flying body

Rocket nozzles for unconventional vehicles

Control and/or drive device for a flying body

Dual-mode chemical-electric thrusters for spacecraft

Side thruster module

Rocket engine having guide vanes in the nozzle of the engine

Fluidic diverter valve with a variable valve-bore clearance

Fluent control valve

Side thruster valve and side thruster device

Aerospike augmentation of microthruster impulse

Hybrid rocket propulsion system including array of hybrid or fluid...

Lateral-thrust control arrangement for missiles with solid-fuel hot...

Multiple pintle nozzle propulsion control system

Rocket engine expansion nozzle with complementary annular nozzle

Reaction control system

Reaction jet control system

Patents Applicationslast 30 patents

A NON-AXISYMMETRIC HEAT SHIELD, A NOZZLE DEFINED AT LEAST PARTIALLY...

JET PROPULSION DEVICE AND FUEL SUPPLY METHOD

VECTORED-THRUST PROPULSOR

CRYOGENIC THRUSTER ASSEMBLY

CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY

Rocket Nozzles for Unconventional Vehicles

SYSTEM AND METHOD FOR MANEUVERING ROCKETS

CONTROL AND/OR DRIVE DEVICE FOR A FLYING BODY

Satellite Control

Rocket nozzles for unconventional vehicles

Dual-mode chemical-electric thrusters for spacecraft

FORCE BALANCED BUTTERFLY PROPORTIONAL HOT GAS VALVE

Side thruster module

Rocket engine having guide vanes in the nozzle of the engine

Control and/or drive device for a flying body

FLUIDIC DIVERTER VALVE WITH A VARIABLE VALVE-BORE CLEARANCE

Side thruster valve and side thruster device