with solid propellant

Industry

CPC
F02K9/763

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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

F02K9/763with solid propellant

Industries

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Patents Grantslast 30 patents

Information Patent Grant
System for multiple burns from a rocket motor
- Patent number 11,859,579
- Issue date Jan 2, 2024
- Triad National Security, LLC
- Nicholas Dallmann
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
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
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
Solid rocket motors including flight termination systems, and relat...
- Patent number 10,781,773
- Issue date Sep 22, 2020
- Northrop Grumman Innovation Systems, Inc.
- Joseph J. Kliger
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Propulsion system comprising plurality of individually selectable s...
- Patent number 9,790,895
- Issue date Oct 17, 2017
- Pacific Scientific Energetic Materials Company
- Steven Nelson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Cluster rocket motor boosters
- Patent number 9,534,563
- Issue date Jan 3, 2017
- Raytheon Company
- Andrew B Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Combined cycle missile engine system
- Patent number 8,056,319
- Issue date Nov 15, 2011
- Aerojet-General Corporation
- Melvin J. Bulman
- F42 - AMMUNITION BLASTING
Information Patent Grant
Precision controlled variable thrust solid propellant rocket motor
- Patent number 7,958,718
- Issue date Jun 14, 2011
- Alliant Techsystems Inc.
- L. Don Berchtold
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion enhancement arrangement for rocket
- Patent number 7,814,835
- Issue date Oct 19, 2010
- Zhongwei Shi
- F42 - AMMUNITION BLASTING
Information Patent Grant
Propulsion enhancement arrangement for rocket
- Patent number 6,796,242
- Issue date Sep 28, 2004
- Zhong-Wei Shi
- F42 - AMMUNITION BLASTING
Information Patent Grant
MEMS microthruster array
- Patent number 6,378,292
- Issue date Apr 30, 2002
- Honeywell International Inc.
- Daniel W. Youngner
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Gas generating eject motor
- Patent number 6,352,030
- Issue date Mar 5, 2002
- Cordant Technologies Inc.
- Daniel W. Doll
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Integral solid booster and hybrid thrust sustaining system and proj...
- Patent number 6,125,763
- Issue date Oct 3, 2000
- Environmental Aeroscience Corp.
- Korey R. Kline
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Modular solid-propellant launch vehicle and related launch facility
- Patent number 5,217,188
- Issue date Jun 8, 1993
- TRW Inc.
- John M. Thole
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of making solid propellant canister loaded rocket motor
- Patent number 5,206,989
- Issue date May 4, 1993
- Thiokol Corporation
- Bradley W. Smith
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Reverse bulged forward acting scored rupture disc bulkhead structur...
- Patent number 5,160,070
- Issue date Nov 3, 1992
- Fike Corporation
- Donald R. Hibler
- F42 - AMMUNITION BLASTING
Information Patent Grant
Solid propellant canister loaded multiple pulsed or staged rocket
- Patent number 5,070,691
- Issue date Dec 10, 1991
- Thiokol Corporation
- Bradley W. Smith
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Solid rocket motor with dual interrupted thrust
- Patent number 4,972,673
- Issue date Nov 27, 1990
- Her Majesty the Queen as represented by the Minister of National Defence of H...
- Joseph L. C. Carrier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Solid propellant canister loaded multiple pulsed or staged rocket m...
- Patent number 4,956,971
- Issue date Sep 18, 1990
- Morton Thiokol, Inc.
- Bradley W. Smith
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Integrated two stage rocket
- Patent number 4,924,775
- Issue date May 15, 1990
- The United States of America as represented by the Secretary of the Army
- John M. Humphrey
- F42 - AMMUNITION BLASTING
Information Patent Grant
Multiple propellant solid rocket motor
- Patent number 4,840,024
- Issue date Jun 20, 1989
- Morton Thiokol, Inc.
- Allan J. McDonald
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Pulsed rocket motor
- Patent number 4,829,765
- Issue date May 16, 1989
- Morton Thiokol, Inc.
- Christopher W. Bolieau
- F42 - AMMUNITION BLASTING
Information Patent Grant
Rocket propelled vehicle forward end control method and apparatus
- Patent number 4,819,426
- Issue date Apr 11, 1989
- Morton Thiokol, Inc.
- Victor Singer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Apparatus for the connection between two stages of a self-propelled...
- Patent number 4,250,705
- Issue date Feb 17, 1981
- Societe Nationale des Poudres et Explosifs
- Hubert A. Zante
- F42 - AMMUNITION BLASTING
Information Patent Grant
Self-propelled engine with separable stages
- Patent number 4,198,896
- Issue date Apr 22, 1980
- Societe Nationale des Poudres et Explosifs
- Jackie G. Lamic
- F42 - AMMUNITION BLASTING
Information Patent Grant
Barrier system for dual-pulse rocket motor
- Patent number 4,085,584
- Issue date Apr 25, 1978
- The United States of America as represented by the Secretary of the Air Force
- Roy A. Jones
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Partition for rocket motors
- Patent number 4,075,832
- Issue date Feb 28, 1978
- Dynamit Nobel Aktiengesellschaft
- Walter Helmut Diesinger
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3888079
- Patent number 3,888,079
- Issue date Jun 10, 1975
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
3879942
- Patent number 3,879,942
- Issue date Apr 29, 1975
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

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
BOOST THRUST ROCKET MOTOR
- Publication number 20210102790
- Publication date Apr 8, 2021
- BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC
- David J. Schorr
- F42 - AMMUNITION BLASTING
Information Patent Application
SOLID ROCKET MOTORS INCLUDING FLIGHT TERMINATION SYSTEMS, AND RELAT...
- Publication number 20170122259
- Publication date May 4, 2017
- Joseph J. Kliger
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM COMPRISING PLURALITY OF INDIVIDUALLY SELECTABLE S...
- Publication number 20160061148
- Publication date Mar 3, 2016
- Steven NELSON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Propulsion Enhancement Arrangement for Rocket
- Publication number 20090212163
- Publication date Aug 27, 2009
- Zhongwei Shi
- F42 - AMMUNITION BLASTING
Information Patent Application
Combined cycle missile engine system
- Publication number 20090205311
- Publication date Aug 20, 2009
- Aerojet-General Corporation, a corporation of the State of Ohio.
- Melvin J. Bulman
- F42 - AMMUNITION BLASTING
Information Patent Application
Propulsion enhancement arrangement for rocket
- Publication number 20040144280
- Publication date Jul 29, 2004
- Zhong-Wei Shi
- F42 - AMMUNITION BLASTING

with solid propellant

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

System for multiple burns from a rocket motor

Ring-shaped booster rocket

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

Ring-shaped booster rocket

Solid rocket motors including flight termination systems, and relat...

Propulsion system comprising plurality of individually selectable s...

Cluster rocket motor boosters

Combined cycle missile engine system

Precision controlled variable thrust solid propellant rocket motor

Propulsion enhancement arrangement for rocket

Propulsion enhancement arrangement for rocket

MEMS microthruster array

Gas generating eject motor

Integral solid booster and hybrid thrust sustaining system and proj...

Modular solid-propellant launch vehicle and related launch facility

Method of making solid propellant canister loaded rocket motor

Reverse bulged forward acting scored rupture disc bulkhead structur...

Solid propellant canister loaded multiple pulsed or staged rocket

Solid rocket motor with dual interrupted thrust

Solid propellant canister loaded multiple pulsed or staged rocket m...

Integrated two stage rocket

Multiple propellant solid rocket motor

Pulsed rocket motor

Rocket propelled vehicle forward end control method and apparatus

Apparatus for the connection between two stages of a self-propelled...

Self-propelled engine with separable stages

Barrier system for dual-pulse rocket motor

Partition for rocket motors

3888079

3879942

Patents Applicationslast 30 patents

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

BOOST THRUST ROCKET MOTOR

SOLID ROCKET MOTORS INCLUDING FLIGHT TERMINATION SYSTEMS, AND RELAT...

PROPULSION SYSTEM COMPRISING PLURALITY OF INDIVIDUALLY SELECTABLE S...

Propulsion Enhancement Arrangement for Rocket

Combined cycle missile engine system

Propulsion enhancement arrangement for rocket