| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 02/12/2009 | WO2008135695A3 Electrolytic igniter for rocket engines using monopropellants |
| 02/12/2009 | WO2008135693A3 Electrolytic igniter for rocket engines using liquid propellants |
| 02/05/2009 | US20090031700 Mixtures of oxides of nitrogen and oxygen as oxidizers for propulsion, gas generation and power generation applications |
| 02/05/2009 | DE102007036883A1 Raketenmotor Rocket motor |
| 02/03/2009 | US7484353 Rocket motor case using plank sections and methods of manufacturing |
| 02/03/2009 | CA2596503C Rotor system |
| 01/27/2009 | US7481784 Wall structure |
| 01/22/2009 | WO2008082677A3 Hybrid rocket fuel |
| 01/20/2009 | US7479302 Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same |
| 01/20/2009 | US7478778 Rocket engine having guide vanes in the nozzle of the engine |
| 01/20/2009 | US7478742 Method for brazing ceramic surfaces |
| 01/20/2009 | US7478526 Speed control apparatus for a rotary sprinkler |
| 01/15/2009 | WO2009008524A1 Ignition and chemical reaction accelerator and flame stabilizer, speed-type internal combustion engine, and furnace |
| 01/15/2009 | US20090013663 Methane engine for rocket propulsion |
| 01/15/2009 | DE102007032760A1 Hot gas chamber device e.g. for rocket engines, has hot gas chamber and probe with air-conditioning device provided for cooling of probe which has cooling fluid for chamber |
| 01/08/2009 | US20090007543 Pintle injector tip with active cooling |
| 01/08/2009 | US20090007542 Titanium treatment to minimize fretting |
| 01/07/2009 | EP2010363A1 Method of producing a fibrous layer for the manufacture of a preform of a composite part |
| 01/06/2009 | US7472544 Pressurizer for a rocket engine |
| 01/02/2009 | DE102007030410A1 Device for reducing force effect of nozzle of rocket engine, has flow device that is positioned around nozzle and separated from rocket engine for generating gas flow with component in direction of gas-discharging channel of nozzle |
| 12/24/2008 | WO2008155221A2 Propellant unit with enhanced performance |
| 12/24/2008 | WO2008105967A3 Propulsion system with canted multinozzle grid |
| 12/24/2008 | EP2006560A2 Resin-made cage and bearing |
| 12/24/2008 | EP2004979A1 Apparatus and method for determining the fuel mass in a spacecraft |
| 12/24/2008 | CA2689150A1 Propellant device of enhanced performance |
| 12/23/2008 | US7467684 Anti-roll thrust system for hydrogen powered vehicles |
| 12/18/2008 | WO2008152285A1 Cryotechnic space propulsion device and its control method |
| 12/18/2008 | WO2008129372A3 Rocket engine laval nozzle with gas injection device |
| 12/17/2008 | CN201165916Y Solid rocket engine |
| 12/16/2008 | US7464535 Rocket motor nozzle throat area control system and method |
| 12/09/2008 | US7461503 Low-cost, low-density, ablative rubber insulation for rocket motors |
| 12/03/2008 | EP1998036A2 Resonance driven glow plug torch igniter and ignition method |
| 12/03/2008 | EP1998035A2 Fluidic vectoring for exhaust nozzle |
| 12/02/2008 | US7458201 Propulsion device with enclosed plenum |
| 11/27/2008 | WO2008144324A1 Hydroxy amine based staged combustion hybrid rocket motor |
| 11/27/2008 | WO2008143033A1 Dual-pulse rocket motor |
| 11/27/2008 | WO2008142290A2 Method and device for supplying a space propulsion engine with liquid cryogenic propellants |
| 11/27/2008 | WO2008123895A3 Spark-integrated propellant injector head with flashback barrier |
| 11/26/2008 | EP1995444A2 Compact, high performance swirl combustion rocket engine |
| 11/19/2008 | CN101307720A Method and apparatus for total energy fuel conversion systems |
| 11/18/2008 | CA2519936C Unitized hybrid rocket system |
| 11/13/2008 | WO2008135695A2 Electrolytic igniter for rocket engines using monopropellants |
| 11/13/2008 | WO2008135693A2 Electrolytic igniter for rocket engines using liquid propellants |
| 11/13/2008 | US20080276596 Engine Wall Structure and a Method of Producing an Engine Wall Structure |
| 11/06/2008 | WO2008097361A3 Regression and erosion measurement system and method |
| 11/06/2008 | US20080272239 Reversible space plane |
| 11/05/2008 | CN100430648C Method and apparatus for generating power by combustion of vaporized fuel |
| 10/30/2008 | WO2008129372A2 Rocket engine laval nozzle with gas injection device |
| 10/30/2008 | US20080264035 Coolant flow swirler for a rocket engine |
| 10/30/2008 | DE102005049686B4 Einspritzelement Injection member |
| 10/23/2008 | US20080256925 Compact, high performance swirl combustion rocket engine |
| 10/23/2008 | US20080256924 Ultra-compact, high performance aerovortical rocket thruster |
| 10/22/2008 | EP1983183A2 Ultra-compact, high-performance aerovortical rocket thruster |
| 10/16/2008 | WO2008123895A2 Spark-integrated propellant injector head with flashback barrier |
| 10/15/2008 | CN101285433A Micro engine, mini-engine and method for manufacturing the micro engine |
| 10/14/2008 | US7434384 Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts |
| 10/09/2008 | US20080245072 Damping of Vibration of a Combustion Chamber By Resonators |
| 10/09/2008 | CA2682257A1 Pintle-controlled propulsion system with external ring actuator |
| 10/02/2008 | US20080236140 Noncircular transient fluid fuel injector control channels in propellant injector combustion systems |
| 10/02/2008 | US20080236136 Linkage system with wear reduction |
| 10/02/2008 | DE10312776B4 Ausfahrbare Schubdüsenglocke für ein Raketentriebwerk Extensible thrust nozzle cone for a rocket engine |
| 10/02/2008 | DE102007001024B4 Verfahren zur rechnergestützten Regelung und/oder Steuerung eines technischen Systems insbesondere einer Gasturbine Method for computer-aided regulation and / or control of a technical system, in particular a gas turbine |
| 10/02/2008 | DE102005039742B4 Schubdüse für Raketen mit ausfahrbarer Düsenverlängerung The thruster rocket with extendable nozzle extension |
| 10/02/2008 | DE10044624B4 Koaxial-Einspritzdüse Coaxial injector |
| 10/01/2008 | EP1766220B1 Method for detecting complete draining of a propellant tank and for propellant management onboard a satellite |
| 09/24/2008 | EP1972775A1 Pyrotechnical propulsion method and device with thrust modulation |
| 09/23/2008 | CA2356308C Plugging system for a line port, specifically, for the port of a channel used in administering air into a ramjet engine combustion chamber |
| 09/18/2008 | WO2008094731A3 Active material actuated louver system |
| 09/18/2008 | US20080223135 Method of detecting damage to an engine bearing |
| 09/17/2008 | CN100419245C Delay igniter for composite enhanced distance bullet rocket engine |
| 09/12/2008 | WO2008107555A1 Nozzle system for controlling the trajectory of a mobile |
| 09/11/2008 | US20080216462 Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method |
| 09/11/2008 | DE10163561B4 Verfahren zur Messung des dynamischen Dämpfungsverhaltens eines Raketentriebwerkes A method for measuring the dynamic damping behavior of a rocket engine |
| 09/10/2008 | CN100417801C 火箭发动机 Rocket engine |
| 09/04/2008 | US20080210778 Aircraft engine exhaust shroud |
| 09/04/2008 | DE102007010349A1 Valve controller for ramjet fuel supply in guided missile, integrates valve, actuator and electronics, in structural molding occupying intermediate space associated with ramjet motor |
| 09/04/2008 | DE102007008942A1 Einspritzkopf für die Brennkammer eines Raketentriebwerks Injection head for the combustion chamber of a rocket engine |
| 09/02/2008 | US7418814 Dual expander cycle rocket engine with an intermediate, closed-cycle heat exchanger |
| 08/27/2008 | EP1961945A2 Injection head for the reaction chamber of a rocket engine |
| 08/27/2008 | EP1960654A1 Hybrid rocket system |
| 08/21/2008 | WO2008100186A1 A component configured for being subjected to high thermal load during operation |
| 08/20/2008 | EP1959124A2 Device for controlling the nozzle thrust direction of a rocket engine |
| 08/20/2008 | CN101245745A Laminated board sweat cooling structure by strong endothermic reaction |
| 08/19/2008 | US7412831 Integral cooling system for rotary engine |
| 08/13/2008 | EP1955988A1 Method for casting a solid fuel propulsion unit |
| 08/13/2008 | CN101240757A Heavy caliber asymmetric layout swinging hose |
| 08/12/2008 | US7410607 Introducing cross-linkable polymer (diene-ethylene-propylene terpolymer) and carbon fibers into a kneader and rotating the screw along its longitudinal axis while superimposing the longitudinal reciprocating motion to the screw under solvent-free conditions and curing |
| 08/07/2008 | DE102007006444A1 Micro engine e.g. monergol-hydrazine engine, for use as satellite position controlling engine, has resistance heater for heating substrate material sections to preset temperature, where sections form catalyzer |
| 08/06/2008 | EP1953378A2 Monopropellant reactor system and operating method for a reactor system |
| 08/05/2008 | US7406821 Adapter device for a rocket engine nozzle having a movable diverging portion |
| 07/30/2008 | EP1950523A1 System of nozzles for controlling the trajectory of a moving body |
| 07/29/2008 | US7404288 High propulsion mass fraction hybrid propellant system |
| 07/24/2008 | US20080173020 Spark-integrated propellant injector head with flashback barrier |
| 07/23/2008 | CN201090319Y Improved apparatus capable of enhancing rocket thrust force |
| 07/09/2008 | CN201083164Y Turbine-rocket embedded type engine |
| 07/09/2008 | CN100400841C Method for designing gas liquid co-axial injector by utilizing conception of 'retraction angle' |
| 07/03/2008 | DE102007001024A1 Technical system i.e. gas turbine, controlling and/or regulating method, involves selecting learning and/or optimization procedure suitable for technical system, and regulating and/or controlling system by selected procedure |
| 06/26/2008 | WO2008076008A1 Wall of a rocket engine |
| 06/26/2008 | DE202008004337U1 Aggregat zur Erzeugung von Kraft und/oder Wärme Unit for producing power and / or heat |
| 06/26/2008 | CA2670598A1 Two-piece aft closure for a rocket motor case |