| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 06/14/2006 | DE10356157B4 Verfahren und Vorrichtungen für den Marschflugkörper-Verschuß mittels Booster-Plattform Methods and devices for the cruise missile firing of using booster platform |
| 06/14/2006 | DE102005014238B3 Power unit for solid fuel rocket has outer drive set and inner drive set in form of external burner separated from out of the unit by annular gap |
| 06/14/2006 | CN1786451A Delay igniter for composite enhanced distance bullet rocket engine |
| 06/14/2006 | CN1786450A Method for preventing mutual interference between bottom row device and rocket engine |
| 06/13/2006 | US7061607 Engine spectrometer probe and method of use |
| 06/07/2006 | EP1352170B1 Rocket engine member and a method for manufacturing a rocket engine member |
| 06/07/2006 | CN1782360A Rocket engine jet nozzle of composite distance increasing shell |
| 06/01/2006 | WO2006057653A2 Integrated air inlet system for multi-propulsion aircraft engines |
| 06/01/2006 | WO2006056716A1 Assembly for a spacecraft propulsion system and propulsion system comprising at least one such assembly |
| 05/31/2006 | CN1779225A Methods and systems for operating oxidizer systems |
| 05/31/2006 | CN1258038C Pressure actuating joint system |
| 05/30/2006 | US7051659 Projectile structure |
| 05/30/2006 | US7051513 Rocket engine tubular chamber with single piece jacket |
| 05/30/2006 | US7051512 Fluidic diverter valve with a variable valve-bore clearance |
| 05/25/2006 | US20060107648 Integrated air inlet system for multi-propulsion aircraft engines |
| 05/24/2006 | DE10312419B4 Ausfahrbare Schubdüsenglocke für ein Raketentriebwerk Extensible thrust nozzle cone for a rocket engine |
| 05/23/2006 | US7047885 Multiple pulse cartridge ignition system |
| 05/16/2006 | US7044151 Piston-activated valve and methods and apparatus for restraining free play in a device |
| 05/11/2006 | WO2006048543A1 Device for the supply of a rocket motor with fuel and oxidiser |
| 05/10/2006 | EP1655097A1 Welding apparatus and method for welding a first panel partially contacting a second panel using means for reducing the pressure between the first and second panels and means for locating the generated deflections on the first panel with respect to the second panel |
| 05/04/2006 | US20060090453 Injection head for a liquid-propelled rocket engine |
| 05/03/2006 | CN1768200A Unitized hybrid rocket system |
| 05/02/2006 | US7037602 For combustion chambers or nozzles of missiles, interior layer is a fiber-reinforced ceramic whose matrix comprises phases of carbon and/or phases of silicon carbide and the outer layer is a polymer reinforced with carbon fibers |
| 05/02/2006 | US7036303 Ablative baffle for a liquid rocket engine thrust chamber |
| 04/20/2006 | WO2006010502A3 Beam control surface and method for the production of a beam control surface |
| 04/12/2006 | EP1645747A2 Adjustable nozzle for a solid-propellant engine, and engine featuring such an adjustable nozzle |
| 04/12/2006 | EP1352166B1 An outlet nozzle and a method for manufacturing an outlet nozzle |
| 04/06/2006 | US20060073282 Method for making a thermally protective coating for a propulsive unit structure |
| 04/06/2006 | DE10157752B4 Düsenverlängerung Nozzle extension |
| 04/04/2006 | US7022196 oxidizer package having arrayed solid oxidizer pellets and a polymeric binder with complimentary burn rates; hydrazinium nitroformate or nitronium perchlorate propellants with a polybutadienediol binder; improved flow stability, concentration and distribution of oxidizer solids |
| 04/04/2006 | US7021217 Versatile cavity actuator and systems incorporating same |
| 03/30/2006 | US20060064963 Hybrid propulsion system |
| 03/30/2006 | DE102004045855A1 Steuer- und/oder Antriebseinrichtung für einen Flugkörper Control and / or drive system for a missile |
| 03/28/2006 | US7017333 Wall structure |
| 03/23/2006 | US20060062984 Multilayer composite |
| 03/23/2006 | US20060059888 Control and/or drive device for a flying body |
| 03/23/2006 | DE102004037487A1 Strahlruder und Verfahren zur Herstellung eines Strahlruders Thrusters and methods for producing a jet vane |
| 03/22/2006 | CN1749620A Hingeless flapper valve for flow control |
| 03/21/2006 | CA2254025C Electric vehicle with battery regeneration dependent on battery charge state |
| 03/16/2006 | WO2006028516A2 Thrust vector control system for a plug nozzle rocket engine |
| 03/15/2006 | EP1635054A2 Solid-propellant engine casing, and solid-propellant engine featuring such a casing |
| 03/14/2006 | US7012233 Thrust vectoring a flight vehicle during homing using a multi-pulse motor |
| 03/14/2006 | US7012107 Elastomeric rocket motor insulation |
| 03/08/2006 | EP1631740A1 Micropump-based microthruster |
| 03/08/2006 | CN1744984A Production of thermal protection coatings on propulsion structures |
| 03/08/2006 | CN1244520C Method for generating energy utilizing metal exothermic reaction |
| 03/07/2006 | US7007456 Dual chamber pump and method |
| 03/02/2006 | DE102004008452B4 Strukturelement und Verfahren zur Herstellung desselben Structural element and method of manufacturing the same |
| 02/28/2006 | US7003942 System and method of controlling pressure oscillations of hydrodynamic origin for a solid propellant thruster |
| 02/28/2006 | US7003941 Thruster device responsive to solar radiation and associated methods |
| 02/23/2006 | DE3934071B3 Staustrahltriebwerk mit Rohrstruktur und durch ein solches Staustrahltriebwerk antreibbare Flugkörper Ramjet with tubular structure and by such a ramjet driven missile |
| 02/23/2006 | DE102004038039A1 Raketenmotor Rocket motor |
| 02/21/2006 | US7000398 Ramjet engine combustion chamber and ramjet engine equipped with same |
| 02/21/2006 | US7000377 Super-staged and continuously staged rocket |
| 02/16/2006 | US20060032212 Lightweight rocket engine combustion chamber and associated method |
| 02/14/2006 | US6996973 Method of achieving jet separation of an un-separated flow in a divergent nozzle body of a rocket engine |
| 02/09/2006 | DE102004060650B3 Luft-Kraftstoffverhältnis-Regelgerät für einen Verbrennungsmotor Air-fuel ratio control device for an internal combustion engine |
| 02/08/2006 | EP1624178A1 Rocket motor |
| 02/02/2006 | WO2006010502A2 Beam control surface and method for the production of a beam control surface |
| 02/01/2006 | EP1621753A1 Energetic detonation propulsion |
| 01/19/2006 | WO2006005833A1 Method for detecting complete draining of a propellant tank and for propellant management onboard a satellite |
| 01/17/2006 | US6986285 Pressure sensor and a rocket engine incorporating it |
| 01/17/2006 | US6986246 Side thruster valve and side thruster device |
| 01/12/2006 | US20060009567 Novel EPDM rocket motor insulation |
| 01/12/2006 | US20060006289 Reversable space plane |
| 01/10/2006 | US6983587 Method and apparatus for thrust augmentation for rocket nozzles |
| 01/10/2006 | US6983586 Two-stage pulse detonation system |
| 01/03/2006 | US6981364 Combine engine for single-stage spacecraft |
| 01/03/2006 | CA1341492C Tubular structure ramjet, and missile propelled by such ramjet |
| 12/29/2005 | US20050284130 Air-fuel ratio control apparatus for an internal combustion engine |
| 12/29/2005 | US20050284128 Rocket motor nozzle throat area control system and method |
| 12/28/2005 | EP1608863A2 Unitized hybrid rocket system |
| 12/28/2005 | CN1712689A Air-fuel ratio control apparatus for an internal combustion engine |
| 12/22/2005 | US20050279082 Hybrid rocket motor design and apparatus |
| 12/22/2005 | US20050279077 Off-axis pulse detonation configuration for gas turbine engine |
| 12/15/2005 | WO2005118507A1 High bond strength interlayer for rhenium hot gas erosion protective coatings |
| 12/15/2005 | DE10050715B4 Solarwärme-Rakete Solar thermal rocket |
| 12/13/2005 | US6974111 Asonic aerospike engine |
| 12/13/2005 | US6973773 Propellant supply device |
| 12/06/2005 | US6972064 Method of forming laminar structures having variable angle tape wrap |
| 12/01/2005 | US20050267792 Method and system for laboratory management |
| 12/01/2005 | US20050266163 Extremely strain tolerant thermal protection coating and related method and apparatus thereof |
| 12/01/2005 | DE19524875B4 Triebwerks-Brennkammer mit dichter Verbindung zwischen Verbund-Gehäuse und Boden Engine combustor with tight connection between composite housing and land |
| 11/29/2005 | US6968704 Method and system for densifying cryogenic propellants |
| 11/29/2005 | US6968676 Propulsion from combustion of solid propellant pellet-projectiles |
| 11/29/2005 | US6968673 Cool gas generator and ultra-safe rocket engine |
| 11/24/2005 | DE10158295B4 Strömungskörper Flow body |
| 11/23/2005 | EP0927299B1 Combustion chamber and method for producing a combustion chamber |
| 11/22/2005 | US6966264 Rocket motors with insensitive munitions systems and projectiles including same |
| 11/22/2005 | US6966176 System and fabrication method for actively cooling high performance components |
| 11/15/2005 | US6964154 Axisymmetric, throttleable non-gimballed rocket engine |
| 11/10/2005 | WO2002036955A8 Method and device for a multiple step rocket |
| 11/10/2005 | DE102004018725A1 Dämpfung von Schwingungen einer Brennkammer durch Resonatoren Damping of oscillations of a combustion chamber through resonators |
| 11/10/2005 | DE10118005B4 Mikrotriebwerk Micro-engine |
| 11/09/2005 | EP1593831A2 Reduced gain thrust control valve |
| 11/08/2005 | US6962323 Apparatus comprising a rotary-acting pilot valve |
| 11/03/2005 | US20050242557 Anti-roll thrust system for hydrogen powered vehicles |
| 11/03/2005 | US20050241294 Injector system for rocket motors |
| 11/03/2005 | DE102004022358B3 Method for coating substrates with hard materials, useful in producing radiation guides, comprises spraying them with induction plasma |
| 11/02/2005 | EP1590565A1 Method of producing a thermal barrier coating comprising inclined layers and structures thus obtained |