Re-ignitable or restartable rocket- engine plants Intermittently operated rocket-engine plants

Industry

CPC
F02K9/94

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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

F02K9/94Re-ignitable or restartable rocket- engine plants Intermittently operated rocket-engine plants

Industries

Patents Grantslast 30 patents

Information Patent Grant
Ignition safety device for a multi-pulse or multi-stage rocket moto...
- Patent number 11,988,172
- Issue date May 21, 2024
- Raytheon Company
- Shawn Coffee
- F42 - AMMUNITION BLASTING
Information Patent Grant
Propulsion system with initiators for selective activation of multi...
- Patent number 11,846,252
- Issue date Dec 19, 2023
- Raytheon Company
- Edward Little
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Thrust panel
- Patent number 11,773,808
- Issue date Oct 3, 2023
- POSTECH Research and Business Development Foundation
- Jeongrak Lee
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Extinguishable divert system
- Patent number 11,680,543
- Issue date Jun 20, 2023
- Valley Tech Systems, Inc.
- Russell Carlson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Multi-pulse solid rocket motor ignition method
- Patent number 11,512,668
- Issue date Nov 29, 2022
- Raytheon Company
- Frederick B. Koehler
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Flight vehicle control system
- Patent number 11,448,165
- Issue date Sep 20, 2022
- Valley Tech Systems, Inc.
- Russell Carlson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Dual stage catalytic thruster
- Patent number 11,236,703
- Issue date Feb 1, 2022
- Aerojet Rocketdyne, Inc.
- Matthew Dawson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Satellite with integral thrusters
- Patent number 11,174,048
- Issue date Nov 16, 2021
- Raytheon Company
- Frederick B. Koehler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Extinguishable divert system
- Patent number 11,143,143
- Issue date Oct 12, 2021
- Valley Tech Systems, Inc.
- Russell Carlson
- 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
Integrated warhead ESAD/multi-pulse rocket motor EISD device
- Patent number 11,047,340
- Issue date Jun 29, 2021
- Raytheon Company
- Adam I. Lefcourt
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Microwave ignition of electrically operated propellants
- Patent number 10,808,649
- Issue date Oct 20, 2020
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
Methods and systems for restartable, hybrid-rockets
- Patent number 10,774,789
- Issue date Sep 15, 2020
- Utah State University
- Stephen Whitmore
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Attitude control system
- Patent number 10,598,128
- Issue date Mar 24, 2020
- Valley Tech Systems, Inc.
- Russell Carlson
- F42 - AMMUNITION BLASTING
Information Patent Grant
Electrically operated propellant for solid rocket motor thrust mana...
- Patent number 10,563,617
- Issue date Feb 18, 2020
- Raytheon Company
- James K. Villarreal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Device for pressurizing propellant tanks of a rocket engine
- Patent number 10,533,523
- Issue date Jan 14, 2020
- ARIANEGROUP SAS
- Gérard Roz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Restartable ignition devices, systems, and methods thereof
- Patent number 10,527,004
- Issue date Jan 7, 2020
- Utah State University
- Stephen A. Whitmore
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Grant
Reusable high pressure and high temperature energetic ignition system
- Patent number 10,443,545
- Issue date Oct 15, 2019
- Goodrich Corporation
- Matthew Salois
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Method of regulating the pressure within a first rocket engine prop...
- Patent number 10,415,507
- Issue date Sep 17, 2019
- ARIANEGROUP SAS
- Valentin Hue
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Spark plug and associated propellant ignition system
- Patent number 10,371,099
- Issue date Aug 6, 2019
- The Boeing Company
- Leora Peltz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Solid propellant with integral electrodes, and method
- Patent number 10,259,756
- Issue date Apr 16, 2019
- Raytheon Company
- Jeremy C. Danforth
- B05 - SPRAYING OR ATOMISING IN GENERAL APPLYING LIQUIDS OR OTHER FLUENT MATER...
Information Patent Grant
Electrical/chemical thruster using the same monopropellant and method
- Patent number 10,180,118
- Issue date Jan 15, 2019
- The Curators of the University of Missouri
- Steven P. Berg
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Electrode ignition and control of electrically operated propellants
- Patent number 10,145,337
- Issue date Dec 4, 2018
- Raytheon Company
- Matt H. Summers
- B60 - VEHICLES IN GENERAL
Information Patent Grant
Thrust control valve and flying object
- Patent number 10,138,844
- Issue date Nov 27, 2018
- Mitsubishi Heavy Industries, Ltd.
- Shozo Hidaka
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Vapor jetting device and spacecraft
- Patent number 9,989,012
- Issue date Jun 5, 2018
- IHI Corporation
- Taku Izumiyama
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Anaerobic hybrid propulsion device with fuel present in the form of...
- Patent number 9,957,919
- Issue date May 1, 2018
- AIRBUS DEFENCE AND SPACE SAS
- Christophe Figus
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Reactants sprayed into plasma flow for rocket propulsion
- Patent number 9,505,503
- Issue date Nov 29, 2016
- Lockheed Martin Corporation
- Larry D. Knauer
- 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
Thruster and spacecraft
- Patent number 9,376,987
- Issue date Jun 28, 2016
- IHI Aerospace Co., Ltd.
- Toru Nagao
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
THRUST PANEL
- Publication number 20230235716
- Publication date Jul 27, 2023
- POSTECH Research and Business Development Foundation
- Jeongrak Lee
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM WITH INITIATORS FOR SELECTIVE ACTIVATION OF MULTI...
- Publication number 20230072320
- Publication date Mar 9, 2023
- Raytheon Company
- Edward Little
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROCKET MOTOR AUXILIARY POWER GENERATION UNIT SYSTEMS AND METHODS
- Publication number 20220307449
- Publication date Sep 29, 2022
- GOODRICH CORPORATION
- Matthew D. Salois
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MULTI-PULSE SOLID ROCKET MOTOR IGNITION METHOD
- Publication number 20220170432
- Publication date Jun 2, 2022
- Raytheon Company
- Frederick B. Koehler
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
IGNITION SAFETY DEVICE FOR A MULTI-PULSE OR MULTI-STAGE ROCKET MOTO...
- Publication number 20220154670
- Publication date May 19, 2022
- Raytheon Company
- Shawn Coffee
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Extinguishable Divert System
- Publication number 20210404418
- Publication date Dec 30, 2021
- Valley Tech Systems, Inc.
- Russell Carlson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INTEGRATED WARHEAD ESAD/MULTI-PULSE ROCKET MOTOR EISD DEVICE
- Publication number 20210071621
- Publication date Mar 11, 2021
- Raytheon Company
- Adam I. Lefcourt
- F42 - AMMUNITION BLASTING
Information Patent Application
Methods and Systems for Restartable, Hybrid-Rockets
- Publication number 20200025151
- Publication date Jan 23, 2020
- Utah State University
- Stephen Whitmore
- C06 - EXPLOSIVES MATCHES
Information Patent Application
SPARK PLUG AND ASSOCIATED PROPELLANT IGNITION SYSTEM
- Publication number 20190309707
- Publication date Oct 10, 2019
- The Boeing Company
- Leora Peltz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SATELLITE PROPELLED BY LASER ABLATION
- Publication number 20180222604
- Publication date Aug 9, 2018
- THALES
- Alexandre GARUS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REUSABLE HIGH PRESSURE AND HIGH TEMPERATURE ENERGETIC IGNITION SYSTEM
- Publication number 20180223772
- Publication date Aug 9, 2018
- GOODRICH CORPORATION
- Matthew Salois
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUAL STAGE CATALYTIC THRUSTER
- Publication number 20180135559
- Publication date May 17, 2018
- Aerojet Rocketdyne, Inc.
- Matthew Dawson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ACTUATOR STRUCTURE AND METHOD OF IGNITION OF ELECTRICALLY OPERATED...
- Publication number 20180058377
- Publication date Mar 1, 2018
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DEVICE FOR PRESSURIZING PROPELLANT TANKS OF A ROCKET ENGINE
- Publication number 20160177874
- Publication date Jun 23, 2016
- SNECMA
- Gérard ROZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Restartable Ignition Devices, Systems, and Methods Thereof
- Publication number 20150322892
- Publication date Nov 12, 2015
- Utah State University
- Stephen A. Whitmore
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REACTANTS SPRAYED INTO PLASMA FLOW FOR ROCKET PROPULSION
- Publication number 20140290212
- Publication date Oct 2, 2014
- Lockheed Martin Corporation
- Larry D. KNAUER
- 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
ELECTRICALLY OPERATED PROPELLANTS
- Publication number 20140174313
- Publication date Jun 26, 2014
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUAL USE HYDRAZINE PROPULSION THRUSTER SYSTEM
- Publication number 20130327015
- Publication date Dec 12, 2013
- Pamela Pollet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Thruster and Spacecraft
- Publication number 20130305687
- Publication date Nov 21, 2013
- Ihi Aerospace Co., Ltd.
- Toru Nagao
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
IGNITER FOR A ROCKET ENGINE, METHOD FOR IGNITION OF A ROCKET ENGINE
- Publication number 20130205750
- Publication date Aug 15, 2013
- AEROSPACE PROPULSION PRODUCTS B. V.
- Eduardus Josephus Vermeulen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR CONTROLLING AN OBJECT TRAVELING THROUGH EXOAT...
- Publication number 20130097995
- Publication date Apr 25, 2013
- General Dynamics Ordnance and Tactical Systems, Inc.
- Richard W. Schroeder
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
UNIFIED CHEMICAL ELECTRIC PROPULSION SYSTEM
- Publication number 20130047578
- Publication date Feb 28, 2013
- Space Systems/Loral, Inc.
- Nicolas Claude Gascon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MICROFLUIDIC FLAME BARRIER
- Publication number 20120279196
- Publication date Nov 8, 2012
- FIRESTAR ENGINEERING, LLC
- Gregory S. Mungas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NITROUS OXIDE FLAME BARRIER
- Publication number 20120279197
- Publication date Nov 8, 2012
- FIRESTAR ENGINEERING, LLC
- Gregory S. Mungas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROCKET ENGINE INJECTORHEAD WITH FLASHBACK BARRIER
- Publication number 20100275577
- Publication date Nov 4, 2010
- FIRESTAR ENGINEERING, LLC
- Gregory S. Mungas
- 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
METHOD AND A DEVICE FOR CALCULATING A STARTING OR STOP SEQUENCE FOR...
- Publication number 20100094522
- Publication date Apr 15, 2010
- SNECMA
- Serge Le Gonidec
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW MINIMUM IMPULSE BIT PROPELLANT GAS THRUSTER
- Publication number 20100036579
- Publication date Feb 11, 2010
- Honeywell International Inc.,
- Steve Abel
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Device for injecting mono-propellant at a flow rate that can be mod...
- Publication number 20100006677
- Publication date Jan 14, 2010
- SNECMA
- Hervé Goislot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Re-ignitable or restartable rocket- engine plants Intermittently operated rocket-engine plants

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Ignition safety device for a multi-pulse or multi-stage rocket moto...

Propulsion system with initiators for selective activation of multi...

Thrust panel

Extinguishable divert system

Multi-pulse solid rocket motor ignition method

Flight vehicle control system

Dual stage catalytic thruster

Satellite with integral thrusters

Extinguishable divert system

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

Integrated warhead ESAD/multi-pulse rocket motor EISD device

Microwave ignition of electrically operated propellants

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

Methods and systems for restartable, hybrid-rockets

Attitude control system

Electrically operated propellant for solid rocket motor thrust mana...

Device for pressurizing propellant tanks of a rocket engine

Restartable ignition devices, systems, and methods thereof

Reusable high pressure and high temperature energetic ignition system

Method of regulating the pressure within a first rocket engine prop...

Spark plug and associated propellant ignition system

Solid propellant with integral electrodes, and method

Electrical/chemical thruster using the same monopropellant and method

Electrode ignition and control of electrically operated propellants

Thrust control valve and flying object

Vapor jetting device and spacecraft

Anaerobic hybrid propulsion device with fuel present in the form of...

Reactants sprayed into plasma flow for rocket propulsion

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

Thruster and spacecraft

Patents Applicationslast 30 patents

THRUST PANEL

PROPULSION SYSTEM WITH INITIATORS FOR SELECTIVE ACTIVATION OF MULTI...

ROCKET MOTOR AUXILIARY POWER GENERATION UNIT SYSTEMS AND METHODS

MULTI-PULSE SOLID ROCKET MOTOR IGNITION METHOD

IGNITION SAFETY DEVICE FOR A MULTI-PULSE OR MULTI-STAGE ROCKET MOTO...

Extinguishable Divert System

INTEGRATED WARHEAD ESAD/MULTI-PULSE ROCKET MOTOR EISD DEVICE

Methods and Systems for Restartable, Hybrid-Rockets

SPARK PLUG AND ASSOCIATED PROPELLANT IGNITION SYSTEM

SATELLITE PROPELLED BY LASER ABLATION

REUSABLE HIGH PRESSURE AND HIGH TEMPERATURE ENERGETIC IGNITION SYSTEM

DUAL STAGE CATALYTIC THRUSTER

ACTUATOR STRUCTURE AND METHOD OF IGNITION OF ELECTRICALLY OPERATED...

DEVICE FOR PRESSURIZING PROPELLANT TANKS OF A ROCKET ENGINE

Restartable Ignition Devices, Systems, and Methods Thereof

REACTANTS SPRAYED INTO PLASMA FLOW FOR ROCKET PROPULSION

CRYOGENIC THRUSTER ASSEMBLY

ELECTRICALLY OPERATED PROPELLANTS

DUAL USE HYDRAZINE PROPULSION THRUSTER SYSTEM

Thruster and Spacecraft

IGNITER FOR A ROCKET ENGINE, METHOD FOR IGNITION OF A ROCKET ENGINE

SYSTEM AND METHOD FOR CONTROLLING AN OBJECT TRAVELING THROUGH EXOAT...

UNIFIED CHEMICAL ELECTRIC PROPULSION SYSTEM

MICROFLUIDIC FLAME BARRIER

NITROUS OXIDE FLAME BARRIER

ROCKET ENGINE INJECTORHEAD WITH FLASHBACK BARRIER

CONTROL AND/OR DRIVE DEVICE FOR A FLYING BODY

METHOD AND A DEVICE FOR CALCULATING A STARTING OR STOP SEQUENCE FOR...

LOW MINIMUM IMPULSE BIT PROPELLANT GAS THRUSTER

Device for injecting mono-propellant at a flow rate that can be mod...