| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 09/17/2009 | US20090229241 Hybrid missile propulsion system with reconfigurable multinozzle grid |
| 09/16/2009 | EP2101056A1 Liquid-fuel storage vessell and vapor jet system using the same |
| 09/16/2009 | EP2099691A2 Two-piece aft closure for a rocket motor case |
| 09/10/2009 | US20090223202 Two-shaft gas turbine |
| 09/10/2009 | DE19901424B4 Brennkammer mit Transpirationskühlung Combustion chamber with transpiration |
| 09/03/2009 | US20090217642 Radial flow stereolithographic rocket motor |
| 09/02/2009 | EP2094964A1 Wall of a rocket engine |
| 09/02/2009 | EP2094420A1 A method of manufacturing a wall structure and a machining tool |
| 09/01/2009 | CA2539835C Rocket engine having guide vanes in the nozzle of the engine |
| 08/27/2009 | US20090211228 High performance liquid fuel combustion gas generator |
| 08/27/2009 | US20090211227 Hydroxyl Amine Based Staged Combustion Hybrid Rocket Motor |
| 08/27/2009 | US20090211226 Hybrid rocket motor with annular, concentric solid fuel elements |
| 08/27/2009 | US20090211225 Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles |
| 08/26/2009 | EP2093409A2 Nozzle extension and method for manufacturing same |
| 08/26/2009 | EP2093408A1 Tank pressurised by heated gases |
| 08/26/2009 | EP2092184A1 A liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith |
| 08/26/2009 | EP2092183A2 Spark-integrated propellant injector head with flashback barrier |
| 08/25/2009 | US7578452 Ablative composite assemblies and joining methods thereof |
| 08/25/2009 | US7578122 Rocket motor case using plank sections and method of manufacture |
| 08/25/2009 | US7578121 Thrust termination device for solid rocket motor |
| 08/20/2009 | US20090205313 Fast Response Solid Fuel Rocket Motor |
| 08/20/2009 | US20090205311 Combined cycle missile engine system |
| 08/19/2009 | CN101509439A Microflow rate liquid working substance supply and measuring system |
| 08/19/2009 | CA2654628A1 A tank having a piston pressurized by hot gas |
| 08/13/2009 | DE102009003376A1 Flügeldüsen zur Brennstoff- und Lufteinspritzung Wing nozzles for fuel and air injection |
| 08/13/2009 | DE102008006953A1 System und Verfahren zur Reduktion von Schadstoffen in Triebwerksabgasen System and method for reducing harmful substances in engine exhaust gases |
| 08/12/2009 | EP2087962A1 Tool for and method of bonding layers of a metallic axisymmetric structure having complex curvatures, the tool comprising a plurality of mandrel segments |
| 08/11/2009 | US7571610 Extendible exhaust nozzle bell for a rocket engine |
| 08/06/2009 | WO2009068791A3 Propulsion nozzle for the expansion of a supersonic gas jet |
| 08/05/2009 | EP2084394A2 Mixtures of oxides of nitrogen and oxygen as oxidizers for propulsion, gas generation and power generation applications |
| 08/05/2009 | EP2084387A2 Propulsion system with canted multinozzle grid |
| 07/29/2009 | CN100520036C Double group component hydraulic free-piston engine |
| 07/28/2009 | US7565797 Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles |
| 07/22/2009 | EP2006560A9 Resin-made cage and bearing |
| 07/22/2009 | EP1402166B1 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 07/16/2009 | US20090178415 Extendible exhaust nozzle bell for a rocket engine |
| 07/15/2009 | EP1735212A4 Reversable space plane |
| 07/09/2009 | DE102007010349B4 Ventilsteuereinheit für Staustrahlantrieb sowie Lenkflugkörper mit einer solchen Ventilsteuereinheit Valve control unit for ramjet propulsion and missile with such a valve control unit |
| 07/08/2009 | CN101476523A Miniature propeller based on MEMS nozzle chip |
| 07/02/2009 | WO2009082315A1 A component configured for being subjected to high thermal load during operation |
| 07/02/2009 | WO2009080595A2 Combustion chamber device |
| 07/02/2009 | US20090165437 Drive device on the basis of a gel-type propellant and method for conveying propellant |
| 07/01/2009 | CN100507253C Multi-pipe impulse detonating combustion camber and detonation method thereof |
| 06/25/2009 | WO2009047250A3 Method and device enabling a rocket engine pump to be driven by an internal combustion engine |
| 06/25/2009 | DE102007063539A1 Brennkammervorrichtung Combustion chamber device |
| 06/25/2009 | DE102007030410B4 Vorrichtung und Verfahren zur Reduktion der Krafteinwirkung auf eine Düse eines Raketentriebwerks Device and method for reduction of the force acting on a nozzle of a rocket engine |
| 06/18/2009 | WO2009076448A1 Thruster system |
| 06/18/2009 | WO2009047400A3 Device for injecting a fuel or a fuel/oxidiser pre-mixture, comprising means for passive control of the combustion instabilities |
| 06/18/2009 | WO2008060255A3 Electrically controlled extinguishable solid propellant motors |
| 06/18/2009 | WO2008027022A3 Methods of controlling solid propellant ignition, combustion, and extinguishment |
| 06/17/2009 | EP2069633A2 Regression and erosion measurement system and method |
| 06/10/2009 | EP2067975A1 Nozzle system of a rocket engine |
| 06/04/2009 | WO2009068791A2 Propulsion nozzle for the expansion of a supersonic gas jet |
| 06/04/2009 | WO2009068488A1 Spacecraft afterbody device |
| 06/04/2009 | US20090139206 Dual-mode chemical-electric thrusters for spacecraft |
| 06/04/2009 | US20090139205 Pourable centerport inhibitor for solid propellant rocket motors |
| 06/04/2009 | US20090139204 Hybrid Rocket System |
| 06/04/2009 | CA2706988A1 Spacecraft afterbody device |
| 06/03/2009 | EP2064436A1 Nozzle arrangement for use in a gas thruster, gas thruster, method for manufacturing a nozzle arrangement, method for in-situ repairing of a nozzle arrangement and a method for operating a gas thrusters |
| 06/03/2009 | EP2064432A2 Pintle-controlled propulsion system with external dynamic seal |
| 06/02/2009 | US7540145 Unitized hybrid rocket system |
| 05/28/2009 | US20090137700 Low cost, low-density, ablative rubber insulation for rocket motors |
| 05/28/2009 | US20090133405 Combustible outgassing material lined altitude compensating rocket nozzle |
| 05/28/2009 | DE102007055239A1 Device for measuring rotational speed of hollow shaft mounted in turbine housing of turbo machine, particularly jet engine, has toothing and measuring head, which are arranged on interior of hollow shaft |
| 05/20/2009 | EP2059669A2 Nozzle with temperature-responsive throat diameter |
| 05/20/2009 | DE102007054967A1 Verfahren und Vorrichtung zur Plasma-Reformierung von Brennstoff für Triebwerksanwendungen Method and apparatus for plasma-reforming of the fuel for engine applications |
| 05/14/2009 | WO2009061586A2 In situ optical probe and methods |
| 05/14/2009 | WO2009061289A2 Dual-mode chemical-electric thrusters for spacecraft |
| 05/14/2009 | US20090120060 Catalytically activated transient decomposition propulsion system |
| 05/14/2009 | US20090120057 Deployable aircraft/spacecraft propulsion system and methods |
| 05/12/2009 | US7530314 Thermally initiated venting system and method of using same |
| 05/12/2009 | CA2596260C Rocket engine cooling system |
| 05/07/2009 | WO2009057100A1 Casing for insensitive munitions and process for making same |
| 05/07/2009 | DE102005024608B4 Einspritzvorrichtung für Brennkammern von Flüssigkeitsraketentriebwerken Injector for combustion chambers of liquid rocket engines |
| 04/22/2009 | EP1144344A4 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 04/16/2009 | WO2009047400A2 Device for injecting a fuel or a fuel/oxidiser pre-mixture, comprising means for passive control of the combustion instabilities |
| 04/16/2009 | WO2009047250A2 Method and device enabling a rocket engine pump to be driven by an internal combustion engine |
| 04/16/2009 | WO2009047218A1 Device for powering the pump of a rocket engine using an inertia wheel |
| 04/16/2009 | WO2008155221A3 Propellant unit with enhanced performance |
| 04/16/2009 | DE102007048642A1 Elektrischer Antrieb, insbesondere für eine Kraftstoffzumesseinheit für ein Flugzeugtriebwerk Electric drive, especially for a fuel metering unit for an aircraft engine |
| 04/16/2009 | DE102007048527A1 Schubtriebwerk Thruster |
| 04/16/2009 | CA2700786A1 Method and device enabling a rocket engine pump to be driven by an internal combustion engine |
| 04/16/2009 | CA2700273A1 Device for powering the pump of a rocket engine using an inertia wheel |
| 04/15/2009 | EP2048344A2 Jet or rocket engine with heat insulated exhaust nozzle |
| 04/02/2009 | WO2008033699A3 Nozzle with temperature-responsive throat diameter |
| 04/02/2009 | DE102008007936A1 Exhaust gas cleaning system for propellant combustion rocket engine i.e. liquid-fuel rocket engine, has engine and nozzle parts guided with catalytic active materials contacting exhaust gases and coated with catalytic active materials |
| 04/01/2009 | CN101400910A Resin-made cage and bearing |
| 03/25/2009 | EP2038536A1 Methane engine for rocket propulsion |
| 03/24/2009 | US7506500 Propulsion from combustion of solid propellant pellet-projectiles |
| 03/17/2009 | US7503165 Hybrid propulsion system |
| 03/12/2009 | WO2009032447A1 Multi-functional pulse-divided rocket |
| 03/12/2009 | DE10037776B4 Brennkammer für ein Flüssigkeitsraketentriebwerk A combustion chamber of a liquid rocket engine |
| 03/11/2009 | EP2034167A1 Optimised propulsion device |
| 03/04/2009 | EP2029881A1 Injection head, mixing space and power plant |
| 02/25/2009 | CN100463835C Method for determining scattered band of exploding fragments of liquid rocket |
| 02/24/2009 | US7494153 Anti-roll thrust system for vehicles |
| 02/19/2009 | WO2008142290A3 Method and device for supplying a space propulsion engine with liquid cryogenic propellants |
| 02/19/2009 | US20090044716 Slow cook off rocket igniter |
| 02/18/2009 | EP2025908A2 Ignition device |
| 02/18/2009 | EP2025907A2 Rocket engine |