| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 10/28/2004 | WO2004038208A3 Method and apparatus for thrust vectoring a flight vehicle using a multi-pulse rocket motor |
| 10/27/2004 | EP1470326A2 Apparatus and method for passive venting of rocket motor or ordnance case |
| 10/26/2004 | US6808145 Dual-mode airbreathing propulsion system |
| 10/26/2004 | US6807805 Hypergolic fuel system |
| 10/26/2004 | US6807804 Hybrid rocket motor having a precombustion chamber |
| 10/19/2004 | US6806600 Actuator apparatus including a marker device |
| 10/19/2004 | US6805055 Plasma firing mechanism and method for firing ammunition |
| 10/13/2004 | EP1187978B1 Thrust chamber assembly |
| 10/12/2004 | US6802179 Nozzle with spiral internal cooling channels |
| 10/07/2004 | WO2004085252A2 Unitized hybrid rocket system |
| 10/07/2004 | WO2004085016A2 Hydrogen powered toy rocket with electrolysis of water |
| 10/07/2004 | US20040195363 Thrust control valve |
| 10/07/2004 | US20040194941 Active cooling panel of thermostructural composite material and method for its manufacture |
| 10/07/2004 | US20040194445 Antimatter engine |
| 10/07/2004 | DE10312776A1 Ausfahrbare Schubdüsenglocke für ein Raketentriebwerk Extensible thrust nozzle cone for a rocket engine |
| 10/07/2004 | DE10312419A1 Ausfahrbare Schubdüsenglocke für ein Raketentriebwerk Extensible thrust nozzle cone for a rocket engine |
| 10/06/2004 | CN2646402Y Highly overloaded solid-propellant rocket engine for shells |
| 10/05/2004 | US6799418 Rocket engine member and method for manufacturing a rocket engine member |
| 10/05/2004 | US6799417 Diversion of combustion gas within a rocket engine to preheat fuel |
| 09/30/2004 | US20040190638 Process for synchronization of communication involving multiple user equipments with a head-end equipment by means of OFDM modulation in the upstream channel |
| 09/30/2004 | DE10311010A1 Thrust generation for rocket engine, involves heating propellant to evaporate and expand, and adding alkali metal and fluoride compound to chemically react with propellant |
| 09/30/2004 | DE102004011556A1 Hypergoles Treibstoffsystem, Verfahren zum Erzeugen von Schub sowie Raketenmotor Hypergolic fuel system, and method of generating thrust rocket motor |
| 09/28/2004 | US6796242 Propulsion enhancement arrangement for rocket |
| 09/23/2004 | WO2004081452A2 Expander cycle rocket engine with staged combustion and heat exchange |
| 09/23/2004 | WO2004051068B1 Nozzle with spiral internal cooling channels |
| 09/22/2004 | EP1460259A1 Deployable rocket engine nozzle |
| 09/22/2004 | EP1460258A1 Deployable rocket engine nozzle |
| 09/22/2004 | EP1458968A1 A component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 09/22/2004 | EP0828929B1 Reduced pollution power generation system and gas generator therefore |
| 09/16/2004 | US20040177604 Hypergolic fuel system |
| 09/16/2004 | US20040177603 Expander cycle rocket engine with staged combustion and heat exchange |
| 09/16/2004 | DE10219502B4 Verfahren zum Herstellen gelöteter Wärmetauscherstrukturen, insbesondere regenerativ gekühlter Brennkammern A method for producing brazed heat exchanger structures, especially regenerative cooled combustors |
| 09/14/2004 | US6790332 Ia/ic ratio is 1-1.5, and wherein a charge ratio qa/qc=taia/tcic of charge qa, transported during an anode pulse of duration ta, to a charge qc, transported during a cathode pulse of duration tc, is 30-45. |
| 09/14/2004 | US6789316 Method for manufacturing outlet nozzles for rocket engines |
| 09/08/2004 | EP1455076A2 Propulsion device, flying object comprising the same and propulsion device igniting method |
| 09/07/2004 | US6787586 Comprising solid filler powder, silica, carbon fibers or aramid fibers, providing adhesion, storage stability, shelf life |
| 09/02/2004 | US20040168428 Nozzle with spiral internal cooling channels |
| 09/01/2004 | EP1451544A1 Measuring shear stress at an interface with two walls and two crossed sensor elements |
| 08/31/2004 | US6783824 Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same |
| 08/31/2004 | US6782693 Case burning rocket with drive system for combustion chamber and nozzle |
| 08/26/2004 | WO2004072465A2 Diversion of combustion gas within a rocket engine to preheat fuel |
| 08/26/2004 | US20040167278 HIgh-strength rubber formulations, and shear ply made from the same |
| 08/24/2004 | US6779458 Method and apparatus for installing aft insulation in rocket motor case |
| 08/24/2004 | US6779335 Burning nitrous oxide and a fuel |
| 08/19/2004 | US20040159740 Hydrogen powered toy rocket utilizing hydrogen from the electrolysis of water |
| 08/18/2004 | EP1446611A1 Flow-type body and combustion device provided with a flow-type body of this type |
| 08/18/2004 | EP1402166A4 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 08/18/2004 | EP1299673A4 Method and system for densifying cryogenic propellants |
| 08/18/2004 | CN1522339A Shaped charge engine |
| 08/17/2004 | US6776372 Method of operating a satellite for end-of-life maneuvers |
| 08/17/2004 | US6776049 System and method for measuring stress at an interface |
| 08/12/2004 | WO2004067943A1 Method of producing a thermal barrier coating comprising inclined layers and structures thus obtained |
| 08/12/2004 | WO2004067264A1 Method of depositing inclined fibrous layers on a support |
| 08/12/2004 | WO2004053320A3 Link between combustion chamber end wall and booster motor propeller nozzle |
| 08/12/2004 | WO2004051068A3 Nozzle with spiral internal cooling channels |
| 08/12/2004 | US20040157979 Fiber-reinforced rocket motor insulation |
| 08/11/2004 | EP1445466A2 Compact afterburners for gas turbine engines |
| 08/05/2004 | WO2004065106A1 Method for making a thermally protective coating for a propulsive unit structure |
| 08/05/2004 | US20040149045 Apparatus and method for measuring stress at an interface |
| 08/05/2004 | US20040148925 Pressurizer for a rocket engine |
| 08/05/2004 | US20040148924 Combustion chamber structure and its manufacturing process |
| 08/05/2004 | US20040148923 Diversion of combustion gas within a rocket engine to preheat fuel |
| 08/05/2004 | CA2512105A1 Method for making a thermally protective coating for a propulsive unit structure |
| 08/04/2004 | CN1160511C Nozzle structure for rocket nozzle having cooled nozzle wall |
| 08/03/2004 | US6770821 Strain control device for attaching transmission lines to deformable structures and methods employing same |
| 08/03/2004 | US6769651 Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method for refining it |
| 08/03/2004 | US6769242 Rocket engine |
| 08/03/2004 | CA2267957C Reloadable/modular solid propellant rocket motor |
| 07/30/2004 | CA2456403A1 An active cooling panel of thermostructural composite material and method for its manufacture |
| 07/30/2004 | CA2456402A1 A method of manufacturing an active cooling panel out of thermostructural compositeb material |
| 07/29/2004 | US20040144886 System and method of controlling pressure oscillations of hydrodynamic origin for a solid propellant thruster |
| 07/29/2004 | US20040144280 Propulsion enhancement arrangement for rocket |
| 07/28/2004 | EP1440233A1 Rocket motors with insensitive munitions systems |
| 07/27/2004 | US6766638 Hydrogen peroxide based propulsion system |
| 07/22/2004 | WO2004061286A1 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection |
| 07/22/2004 | US20040139721 Rocket engine member and a method for manufacturing a rocket engine member |
| 07/15/2004 | US20040134195 Ramjet engine combustion chamber and ramjet engine equipped with same |
| 07/15/2004 | US20040134184 Shaped charge engine |
| 07/14/2004 | EP1189711B1 Method of manufacturing a dome from an undersized blank |
| 07/13/2004 | US6761335 Apparatus for load transfer between aerospace vehicle components, aerospace vehicles including same, and method of attachment of aerospace vehicle components |
| 07/08/2004 | US20040128980 Rocket engine |
| 07/08/2004 | US20040128979 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
| 07/01/2004 | US20040124306 Thrust vectoring a flight vehicle during homing using a multi-pulse motor |
| 07/01/2004 | US20040123460 Method for manufacturing outlet nozzles for rocket engines |
| 06/30/2004 | EP1117918B1 Method for manufacturing outlet nozzles for rocket engines |
| 06/29/2004 | US6755378 System and method for controlling a space-borne propulsion system |
| 06/24/2004 | WO2004053320A2 Link between combustion chamber end wall and booster motor propeller nozzle |
| 06/24/2004 | US20040118103 Dual Liquid engine and rocket using the same |
| 06/24/2004 | DE10156124B4 Flüssigkeitsgekühltes Raketentriebwerk mit mäanderförmigen Kühlkanälen Liquid-cooled rocket engine with meandering cooling channels |
| 06/23/2004 | CN1506567A Attachment for rocket engine |
| 06/22/2004 | US6752351 Low mass flow reaction jet |
| 06/22/2004 | US6751945 Pressurizer for a rocket engine |
| 06/17/2004 | WO2004051068A2 Nozzle with spiral internal cooling channels |
| 06/17/2004 | DE4341376B4 Raketenmotor Rocket motor |
| 06/15/2004 | US6750293 High-strength rubber formulations, and shear ply made from the same |
| 06/15/2004 | US6749726 Lasers/fiber optics are used for fuel ignition; propulsion engines |
| 06/10/2004 | US20040107692 Method and apparatus for a substantially coaxial injector element |
| 06/09/2004 | DE4345153B4 Artilleriegranate großer Reichweite Artillery shell long range |
| 06/09/2004 | DE10043303B4 Raketentriebwerk in Segmentbauweise Rocket engine in segments |
| 06/08/2004 | US6745983 Integrated tankage for propulsion vehicles and the like |