the component comprising a binary propellant

Industry

CPC
C06B47/02

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Parent Industries

CCHEMISTRY METALLURGY C06Explosives C06BEXPLOSIVES OR THERMIC COMPOSITIONS MANUFACTURE THEREOF USE OF SINGLE SUBSTANCES AS EXPLOSIVES C06B47/00Compositions in which the components are separately stored until the moment of burning or explosion

Current Industry

C06B47/02the component comprising a binary propellant

Industries

Patents Grantslast 30 patents

Information Patent Grant
Hypergolic system
- Patent number 11,572,320
- Issue date Feb 7, 2023
- NEWROCKET LTD.
- Avihay Habibi
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Hypergolic system
- Patent number 11,242,295
- Issue date Feb 8, 2022
- NEWROCKET LTD.
- Avihay Habibi
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Dual mode chemical rocket engine and dual mode propulsion system co...
- Patent number 10,316,794
- Issue date Jun 11, 2019
- ECAPS AB
- Göran Bergman
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Catalytic hypergolic bipropellants
- Patent number 8,758,531
- Issue date Jun 24, 2014
- The United States of America as represented by the Secretary of the Air Force
- Stefan Schneider
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
High performance, low toxicity hypergolic fuel
- Patent number 8,685,186
- Issue date Apr 1, 2014
- CFD Research Corporation
- Debasis Sengupta
- A24 - TOBACCO CIGARS CIGARETTES SMOKERS' REQUISITES
Information Patent Grant
Method and device for mixing and initiating a pyrotechnic charge
- Patent number 8,603,271
- Issue date Dec 10, 2013
- BAE Systems Bofors AB
- Mats Runemard
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Hypergolic liquid or gel fuel mixtures
- Patent number 8,435,364
- Issue date May 7, 2013
- The United States of America as represented by the Secretary of the Army
- William H. Stevenson
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Method and device for mixing and initiating a pyrotechnic charge
- Patent number 8,308,879
- Issue date Nov 13, 2012
- BAE Systems Bofors AB
- Mats Runemard
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Methods and compositions for decreasing carbon emissions
- Patent number 8,192,511
- Issue date Jun 5, 2012
- Pichang Wei
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Method for producing cryogenic, solid monopropellants and solid pro...
- Patent number 8,147,628
- Issue date Apr 3, 2012
- Roger E. Lo
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Hypergolic fuels
- Patent number 8,034,202
- Issue date Oct 11, 2011
- The United States of America as represented by the Secretary of the Air Force
- Tommy W. Hawkins
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Rocket motor having a catalytic hydroxylammonium (HAN) decomposer a...
- Patent number 8,024,918
- Issue date Sep 27, 2011
- Honeywell International Inc.
- Donald L. Mittendorf
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Bi-propellant rocket motor having controlled thermal management
- Patent number 7,921,638
- Issue date Apr 12, 2011
- Combustion Propulsion & Ballistic Technology Corp.
- Kenneth K. Kuo
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
High performance, low toxicity hypergolic fuel
- Patent number 7,749,344
- Issue date Jul 6, 2010
- CFO Research Corporation
- Debasis Sengupta
- A24 - TOBACCO CIGARS CIGARETTES SMOKERS' REQUISITES
Information Patent Grant
Catalyst system for rendering organic propellants hypergolic with h...
- Patent number 7,083,690
- Issue date Aug 1, 2006
- Wiley Organics, Inc.
- Thomas A. Dobbins
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Propulsion from combustion of solid propellant pellet-projectiles
- Patent number 6,968,676
- Issue date Nov 29, 2005
- Vinu B. Krishnan
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Amine azide propellant
- Patent number 6,962,633
- Issue date Nov 8, 2005
- The United States of America as represented by the Secretary of the Army
- Michael J. McQuaid
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Hypergolic azide fuels with hydrogen peroxide
- Patent number 6,949,152
- Issue date Sep 27, 2005
- The Boeing Company
- Ramona E. A. Hallit
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Monoprolellant/hypergolic powered proportional actuator
- Patent number 6,935,109
- Issue date Aug 30, 2005
- Vanderbilt University
- Michael Goldfarb
- F15 - FLUID-PRESSURE ACTUATORS HYDRAULICS OR PNEUMATICS IN GENERAL
Information Patent Grant
High regression rate hybrid rocket propellants and method of selecting
- Patent number 6,880,326
- Issue date Apr 19, 2005
- The Board of Trustees of the Leland Stanford Junior University
- M. Arif Karabeyoglu
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Hypergolic fuel system
- Patent number 6,807,805
- Issue date Oct 26, 2004
- United Technologies Corporation
- William B. Watkins
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Reduced toxicity hypergolic bipropellant fuels
- Patent number 6,695,938
- Issue date Feb 24, 2004
- The United States of America as represented by the Secretary of the Navy
- Amos Diede
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
High regression rate hybrid rocket propellants
- Patent number 6,684,624
- Issue date Feb 3, 2004
- The Board of Trustees of the Leland Stanford Junior University
- M. Arif Karabeyoglu
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Non-toxic hypergolic miscible fuel with stable storage characteristics
- Patent number 6,419,771
- Issue date Jul 16, 2002
- The United States of America as represented by the Secretary of the Navy
- Bradley M. Lormand
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Rocket fuels based on metal hydrides and poly-DCPD
- Patent number 6,383,319
- Issue date May 7, 2002
- A.P.T. Aerospace, L.L.C.
- Ronald W. Humble
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Propulsion system containing a mixed-phase propellant and a method...
- Patent number 6,367,244
- Issue date Apr 9, 2002
- Hy-Pat Corporation
- Kevin W. Smith
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Modular cryogenic solid fuel rocket drive sets
- Patent number 6,311,479
- Issue date Nov 6, 2001
- Roger E. Lo
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Gas-generating liquid compositions (persol 1)
- Patent number 6,230,491
- Issue date May 15, 2001
- The United States of America as represented by the Secretary of the Navy
- Kerry L. Wagaman
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Gas-generating liquid compositions (PERSOL 1)
- Patent number 6,165,295
- Issue date Dec 26, 2000
- Kerry L. Wagaman
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Cryogenic solid hybrid rocket engine and method of propelling a rocket
- Patent number 6,101,808
- Issue date Aug 15, 2000
- Orbital Technologies Corporation
- William H. Knuth
- C06 - EXPLOSIVES MATCHES

Patents Applicationslast 30 patents

Information Patent Application
HYPERGOLIC COMPOSITION
- Publication number 20240166573
- Publication date May 23, 2024
- NEWROCKET LTD.
- Roy SAGI
- C06 - EXPLOSIVES MATCHES
Information Patent Application
METHOD AND SYSTEM FOR UNZIPPING POLYMERS FOR ENHANCED ENERGY RELEASE
- Publication number 20240002310
- Publication date Jan 4, 2024
- The Regents of the University of California
- Haiyang Wang
- C06 - EXPLOSIVES MATCHES
Information Patent Application
HYPERGOLIC SYSTEM
- Publication number 20220324774
- Publication date Oct 13, 2022
- NEWROCKET LTD.
- Avihay HABIBI
- C06 - EXPLOSIVES MATCHES
Information Patent Application
METHOD AND DEVICE FOR MIXING AND INITIATING A PYROTECHNIC CHARGE
- Publication number 20130233192
- Publication date Sep 12, 2013
- BAE Systems Bofors AB
- Mats RUNEMARD
- F42 - AMMUNITION BLASTING
Information Patent Application
HIGH PERFORMANCE, LOW TOXICITY HYPERGOLIC FUEL
- Publication number 20130133242
- Publication date May 30, 2013
- CFD Research Corporation
- Debasis Sengupta
- A24 - TOBACCO CIGARS CIGARETTES SMOKERS' REQUISITES
Information Patent Application
PROPULSION METHOD AND DEVICE COMPRISING A LIQUID OXIDANT AND A SOLI...
- Publication number 20130019586
- Publication date Jan 24, 2013
- HERAKLES
- Pierre Yvart
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REDUCED TOXICITY HYPERGOLIC PROPELLANTS
- Publication number 20120273099
- Publication date Nov 1, 2012
- William Anderson
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Hypergolic Liquid Or Gel Fuel Mixtures
- Publication number 20110272071
- Publication date Nov 10, 2011
- The United States of America as represented by the Secretary of the Army
- William H. Stevenson, III
- C06 - EXPLOSIVES MATCHES
Information Patent Application
METHOD AND DEVICE FOR MIXING AND INITIATING A PYROTECHNIC CHARGE
- Publication number 20110011294
- Publication date Jan 20, 2011
- Mats Runemard
- F42 - AMMUNITION BLASTING
Information Patent Application
METHODS AND COMPOSITIONS FOR DECREASING CARBON EMISSIONS
- Publication number 20090320728
- Publication date Dec 31, 2009
- Pichang WEI
- C06 - EXPLOSIVES MATCHES
Information Patent Application
METHODS AND SYSTEMS FOR PROPELLING A VEHICLE
- Publication number 20090266049
- Publication date Oct 29, 2009
- Honeywell International Inc.
- Donald L. Mittendorf
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Mixtures of oxides of nitrogen and oxygen as oxidizers for propulsi...
- Publication number 20090031700
- Publication date Feb 5, 2009
- Space Propulsion Group, Inc.
- Arif Karabeyoglu
- C06 - EXPLOSIVES MATCHES
Information Patent Application
NITROGEN BASED FUEL SYSTEMS
- Publication number 20090025282
- Publication date Jan 29, 2009
- Barnet R. Adelman
- C06 - EXPLOSIVES MATCHES
Information Patent Application
High Performance, Low Toxicity Hypergolic Fuel
- Publication number 20080202655
- Publication date Aug 28, 2008
- CFD Research Corporation
- Debasis Sengupta
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Bi-propellant rocket motor having controlled thermal management
- Publication number 20080173004
- Publication date Jul 24, 2008
- COMBUSTION PROPULSION & BALLISTIC TECHNOLOGY CORP.
- Kenneth K. Kuo
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Hypergolic Liquid Or Gel Fuel Mixtures
- Publication number 20080127551
- Publication date Jun 5, 2008
- United States of America, represented by Secretary of the U.S. Army
- William H. Stevenson, III
- C06 - EXPLOSIVES MATCHES
Information Patent Application
CATALYTIC BIPROPELLANT HOT GAS GENERATION SYSTEM
- Publication number 20070169461
- Publication date Jul 26, 2007
- Honeywell International Inc.
- Mike S. Koerner
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Ionic liquid energetic materials
- Publication number 20050269001
- Publication date Dec 8, 2005
- Charles L. Liotta
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Method for producing cryogenic, solid monopropellants and solid pro...
- Publication number 20050189051
- Publication date Sep 1, 2005
- Robert E. Lo
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Hypergolic fuel analytical device
- Publication number 20050058572
- Publication date Mar 17, 2005
- Swift Enterprises, Ltd.
- Timothee Pourpoint
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Monoprolellant/hypergolic powered proportional actuator
- Publication number 20050044851
- Publication date Mar 3, 2005
- Michael Goldfarb
- B25 - HAND TOOLS PORTABLE POWER-DRIVEN TOOLS MANIPULATORS
Information Patent Application
Liquid hypergolic propellant
- Publication number 20050022911
- Publication date Feb 3, 2005
- Swift Enterprises, Ltd.
- John Rusek
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Hypergolic azide fuels with hydrogen peroxide
- Publication number 20040221933
- Publication date Nov 11, 2004
- Ramona E.A. Hallit
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Hypergolic fuel system
- Publication number 20040177604
- Publication date Sep 16, 2004
- William B. Watkins
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Reduced toxicity hypergolic bipropellant fuels
- Publication number 20030192633
- Publication date Oct 16, 2003
- Amos Diede
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Rocket fuels based on metal hydrides and poly-DCPD
- Publication number 20030164215
- Publication date Sep 4, 2003
- A.P.T. Aerospace, L.L.C.
- Charles S. Woodson
- C06 - EXPLOSIVES MATCHES
Information Patent Application
HIGH REGRESSION RATE HYBRID ROCKET PROPELLANTS AND METHOD OF SELECTING
- Publication number 20030098107
- Publication date May 29, 2003
- M. ARIF KARABEYOGLU
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Method for powering a drive
- Publication number 20030089823
- Publication date May 15, 2003
- Norbert Auner
- C06 - EXPLOSIVES MATCHES
Information Patent Application
Catalyst system for rendering organic propellants hypergolic with h...
- Publication number 20030015268
- Publication date Jan 23, 2003
- Thomas A. Dobbins
- C06 - EXPLOSIVES MATCHES
Information Patent Application
High Regression Rate Hybrid Rocket Propellants and Method of Selecting
- Publication number 20020036038
- Publication date Mar 28, 2002
- M. Arif Karabeyoglu
- C06 - EXPLOSIVES MATCHES

the component comprising a binary propellant

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Hypergolic system

Hypergolic system

Dual mode chemical rocket engine and dual mode propulsion system co...

Catalytic hypergolic bipropellants

High performance, low toxicity hypergolic fuel

Method and device for mixing and initiating a pyrotechnic charge

Hypergolic liquid or gel fuel mixtures

Method and device for mixing and initiating a pyrotechnic charge

Methods and compositions for decreasing carbon emissions

Method for producing cryogenic, solid monopropellants and solid pro...

Hypergolic fuels

Rocket motor having a catalytic hydroxylammonium (HAN) decomposer a...

Bi-propellant rocket motor having controlled thermal management

High performance, low toxicity hypergolic fuel

Catalyst system for rendering organic propellants hypergolic with h...

Propulsion from combustion of solid propellant pellet-projectiles

Amine azide propellant

Hypergolic azide fuels with hydrogen peroxide

Monoprolellant/hypergolic powered proportional actuator

High regression rate hybrid rocket propellants and method of selecting

Hypergolic fuel system

Reduced toxicity hypergolic bipropellant fuels

High regression rate hybrid rocket propellants

Non-toxic hypergolic miscible fuel with stable storage characteristics

Rocket fuels based on metal hydrides and poly-DCPD

Propulsion system containing a mixed-phase propellant and a method...

Modular cryogenic solid fuel rocket drive sets

Gas-generating liquid compositions (persol 1)

Gas-generating liquid compositions (PERSOL 1)

Cryogenic solid hybrid rocket engine and method of propelling a rocket

Patents Applicationslast 30 patents

HYPERGOLIC COMPOSITION

METHOD AND SYSTEM FOR UNZIPPING POLYMERS FOR ENHANCED ENERGY RELEASE

HYPERGOLIC SYSTEM

METHOD AND DEVICE FOR MIXING AND INITIATING A PYROTECHNIC CHARGE

HIGH PERFORMANCE, LOW TOXICITY HYPERGOLIC FUEL

PROPULSION METHOD AND DEVICE COMPRISING A LIQUID OXIDANT AND A SOLI...

REDUCED TOXICITY HYPERGOLIC PROPELLANTS

Hypergolic Liquid Or Gel Fuel Mixtures

METHOD AND DEVICE FOR MIXING AND INITIATING A PYROTECHNIC CHARGE

METHODS AND COMPOSITIONS FOR DECREASING CARBON EMISSIONS

METHODS AND SYSTEMS FOR PROPELLING A VEHICLE

Mixtures of oxides of nitrogen and oxygen as oxidizers for propulsi...

NITROGEN BASED FUEL SYSTEMS

High Performance, Low Toxicity Hypergolic Fuel

Bi-propellant rocket motor having controlled thermal management

Hypergolic Liquid Or Gel Fuel Mixtures

CATALYTIC BIPROPELLANT HOT GAS GENERATION SYSTEM

Ionic liquid energetic materials

Method for producing cryogenic, solid monopropellants and solid pro...

Hypergolic fuel analytical device

Monoprolellant/hypergolic powered proportional actuator

Liquid hypergolic propellant

Hypergolic azide fuels with hydrogen peroxide

Hypergolic fuel system

Reduced toxicity hypergolic bipropellant fuels

Rocket fuels based on metal hydrides and poly-DCPD

HIGH REGRESSION RATE HYBRID ROCKET PROPELLANTS AND METHOD OF SELECTING

Method for powering a drive

Catalyst system for rendering organic propellants hypergolic with h...

High Regression Rate Hybrid Rocket Propellants and Method of Selecting