| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 02/01/2007 | WO2006106204A3 Two-phase cold gas propulsion system and tank for such a space craft propulsion system |
| 02/01/2007 | US20070022741 Combustion chamber comprising a cooling unit and method for producing said combustion chamber |
| 02/01/2007 | DE102005036137A1 Brennkammer und Verfahren zur Herstellung einer Brennkammer Combustion chamber and method of manufacturing a combustion chamber |
| 01/18/2007 | WO2007007213A1 A nozzle-vane system for a 122-mm diameter rocket |
| 01/11/2007 | WO2007003270A1 Gel-type fuel based drive device and method for supplying fuel |
| 01/11/2007 | US20070006568 Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle |
| 01/10/2007 | EP1741917A2 Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle |
| 01/10/2007 | CN1892011A Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle |
| 01/04/2007 | DE102005030437A1 Antriebsvorrichtung auf Basis gelförmigen Treibstoffs und Verfahren zur Treibstoff-Förderung Drive device based gel fuel and process for fuel-promotion |
| 01/03/2007 | EP1738112A1 Damping of vibration of a combustion chamber by resonators |
| 01/02/2007 | US7155898 Thrust vector control system for a plug nozzle rocket engine |
| 12/27/2006 | EP1735532A2 Thrust vector control system for a plug nozzle rocket engine |
| 12/27/2006 | EP1735212A2 Reversable space plane |
| 12/14/2006 | US20060278284 Reduced gain thrust control valve |
| 12/07/2006 | WO2006128686A1 Structural element and method for producing the same |
| 12/07/2006 | DE102005026635A1 Strukturelement und Verfahren zur Herstellung desselben Structural element and method of manufacturing the same |
| 11/30/2006 | WO2006126397A1 Two-liquid type liquid propellant, method of propelling flight vehicle and propelling machinery |
| 11/30/2006 | DE10350735B4 Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer Combustion chamber with cooling means and methods for making the combustion chamber |
| 11/30/2006 | DE102005024608A1 Injection device for fuel chambers of liquid-fueled rocket engines comprises injection nozzles each having an inlet bore opening into a combustion chamber |
| 11/30/2006 | DE10054333B4 Brennkammer mit erhöhtem Wärmeeintrag in eine Kühleinrichtung Combustion chamber with increased heat input into a cooling device |
| 11/29/2006 | CN1869424A Hydrogen rocker |
| 11/23/2006 | DE10126923B4 Raketentriebwerk mit Trennung von Innenmantel und Außenmantel Rocket engine with separation of inner shell and outer shell |
| 11/21/2006 | US7137255 Compact swirl augmented afterburners for gas turbine engines |
| 11/21/2006 | US7137254 Coaxial spray nozzle injector |
| 11/21/2006 | US7137244 Reactor for decomposition of ammonium dinitramide-based liquid monopropellants and process for the decomposition |
| 11/21/2006 | CA2180501C Ramjet engine for supersonic and/or hypersonic aircraft |
| 11/09/2006 | WO2006028516B1 Thrust vector control system for a plug nozzle rocket engine |
| 11/09/2006 | DE102005002283A1 Rocket propulsion, has combustion chamber including thrust pipe, where thrust pipe is spaced out simultaneously with presonic velocities of gas and also with supersonic velocities |
| 11/08/2006 | EP1718857A2 Integrated air inlet system for multi-propulsion aircraft engines |
| 11/08/2006 | EP1718578A1 Structural element and method for producing said element |
| 11/02/2006 | WO2006115605A1 Missile control system and method |
| 11/02/2006 | US20060242830 Method of manufacturing a duct for a gas turbine engine |
| 11/02/2006 | EP1717432A1 Rotable exhaust nozzle for an aircraft engine |
| 11/01/2006 | CN1282823C Minitype chemical propeller with pressure sensor |
| 10/31/2006 | US7128532 Transpiration cooling system |
| 10/26/2006 | WO2005072220A3 Reversable space plane |
| 10/25/2006 | EP1715173A1 Pintle injector |
| 10/25/2006 | EP1714871A2 Acoustic dampers |
| 10/24/2006 | US7124574 Method and apparatus for a substantially coaxial injector element |
| 10/19/2006 | US20060230764 Compact swirl augmented afterburners for gas turbine engines |
| 10/19/2006 | US20060230745 Pintle injector |
| 10/18/2006 | EP1712742A2 Method of manufacturing a duct for a gas turbine engine |
| 10/12/2006 | WO2006106204A2 Two-phase cold gas propulsion system and tank for such a space craft propulsion system |
| 10/12/2006 | US20060225426 Turobjet axisymmetric nozzle controlled hot flap shutter |
| 10/11/2006 | EP1710157A1 Method for refining multifunctional launch vehicles of combined scheme with cruise liquid rocket engine systems (LRESs) |
| 10/10/2006 | US7117797 Pyrotechnic charge structure |
| 10/10/2006 | US7117682 Turbojet axisymmetric nozzle controlled hot flap shutter |
| 10/10/2006 | US7117681 Thrust control valve |
| 10/05/2006 | WO2006103774A1 Vertically movable flying body |
| 10/05/2006 | DE202006007717U1 Electrical magnetic plasma drive for space flight to Mars has liquid argon tank and flows gas between electrodes with a magnetic coil to form plasma and with argon recovery system |
| 10/04/2006 | EP1707788A2 Configuration of a solid propellant charge |
| 10/03/2006 | US7114323 Jet exhaust noise reduction system and method |
| 09/28/2006 | US20060213182 Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing |
| 09/28/2006 | US20060213181 High propulsion mass fraction hybrid propellant system |
| 09/27/2006 | CN1837598A Method for designing gas liquid co-axial injector by utilizing conception of 'retraction angle' |
| 09/19/2006 | US7108223 Missile control system and method |
| 09/19/2006 | US7107755 Engine arrangement |
| 09/19/2006 | CA2299225C Method and apparatus for manufacturing ceramic-based composite member |
| 09/13/2006 | EP1700024A1 Process for igniting a rocket engine and rocket engine |
| 09/12/2006 | US7104507 Very safe manned rocket and method of entertaining |
| 09/12/2006 | CA2180502C Ramjet engine for supersonic and/or hypersonic aircraft |
| 09/08/2006 | WO2006093198A1 Heat transfer thruster |
| 09/05/2006 | US7102113 Three-axis attitude control propulsion device and flying object comprising the same |
| 08/30/2006 | EP1696116A2 Thrust vectoring using fluid jets |
| 08/30/2006 | CN1824940A Dispositif et procede pour reduire les forces laterales non stationnaires agissant sur une tuyere d'un moteur de fusee |
| 08/24/2006 | WO2006028516A3 Thrust vector control system for a plug nozzle rocket engine |
| 08/24/2006 | US20060188764 Fuel cell generation system |
| 08/23/2006 | EP1167188B1 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lres) |
| 08/22/2006 | US7093800 Method of operating a satellite for end-of-life maneuvers |
| 08/17/2006 | US20060180201 Piston-activated valve and methods and apparatus for restraining free play in a device |
| 08/16/2006 | EP1689996A1 Injection element |
| 08/16/2006 | EP1373386B1 Fiber-reinforced rocket motor insulation |
| 08/15/2006 | CA2225964C Improved safety in solid fuel rocket motors |
| 08/10/2006 | DE102005005156A1 Engine for e.g. satellite drive system, has combustion chamber that is downstream to decomposition chamber, where outlet of combustion chamber is connected with inlet of expansion nozzle |
| 08/09/2006 | CN1268839C Attachment for rocket engine |
| 08/03/2006 | DE4438495B4 Einspritzsystem und zugehörige trikoaxiale Einspritzelemente Injection system and associated trikoaxiale injection elements |
| 08/02/2006 | EP1494981B1 Protection against oxidation of parts made of composite material |
| 08/02/2006 | CN1267635C Gas turbine and its combustion chamber |
| 08/01/2006 | US7083141 Self-propelled projectile |
| 08/01/2006 | US7082750 Pressurizer for a rocket engine |
| 07/27/2006 | DE19542234B4 Duale, konzentrische Tellerventile, um das Verhältnis von zwei Fluidströmungen über einen Betriebsbereich einer Ventilöffnung im wesentlichen konstant zu halten Dual, concentric disc valves, to maintain the ratio of two fluid flows over an operating range of a valve opening is substantially constant |
| 07/27/2006 | DE10123957B4 Fügeverbindungseinrichtung und Verfahren zur Herstellung einer Fügeverbindungseinrichtung Joining connection means and methods for producing a joint connection means |
| 07/26/2006 | EP1337750B1 Method and device for a multiple step rocket |
| 07/26/2006 | CN2799873Y Combustion type engine |
| 07/20/2006 | WO2006001927A3 Carnot cycle jet and rocket engine configurations |
| 07/19/2006 | CN1804386A Minisize propeller with electrolyzing water function |
| 07/18/2006 | US7077011 Apparatus and method for measuring stress at an interface |
| 07/12/2006 | EP1389271B1 Reactor for decomposition of ammonium dinitramide-based liquid monopropellants and process for the decomposition |
| 07/06/2006 | US20060145018 Unitized hybrid rocket system |
| 07/06/2006 | US20060144037 Rocket nozzle material |
| 07/05/2006 | CN1796230A Method for determining scattered band of exploding fragments of liquid rocket |
| 07/04/2006 | US7070705 Fiber-reinforced rocket motor insulation |
| 07/04/2006 | US7069719 Air-fuel ratio control apparatus for an internal combustion engine |
| 07/04/2006 | US7069717 Hybrid propulsion system |
| 06/29/2006 | DE102004045855B4 Steuer- und/oder Antriebseinrichtung für einen Flugkörper Control and / or drive system for a missile |
| 06/21/2006 | EP1671025A1 Rocket engine having guide vanes in the nozzle of the engine |
| 06/21/2006 | EP1352168B1 Rocket engine member and method for manufacturing a rocket engine member |
| 06/14/2006 | EP1669587A1 Propulsion system |
| 06/14/2006 | EP1669586A2 Cooled rocket chamber wall |
| 06/14/2006 | EP1668236A1 Combustion chamber comprising a cooling unit and method for producing said combustion chamber |