| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 11/02/2005 | EP1368611B1 Dissolvable thrust vector control vane |
| 11/01/2005 | US6959491 Strain control device for attaching transmission lines to deformable structures and methods employing same |
| 10/28/2005 | CA2504993A1 Injector system for rocket motors |
| 10/27/2005 | WO2005100858A1 Damping of vibration of a combustion chamber by resonators |
| 10/27/2005 | US20050235957 Engine systems and methods |
| 10/26/2005 | EP1587665A1 Method for making a thermally protective coating for a propulsive unit structure |
| 10/20/2005 | WO2005097557A2 Gas generator assembly |
| 10/20/2005 | US20050230176 Anti-roll thrust system for vehicles |
| 10/20/2005 | US20050229587 Adapter device for a rocket engine nozzle having a movable diverging portion |
| 10/19/2005 | EP1585896A1 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection |
| 10/13/2005 | US20050223695 Thrust vector control system for a plug nozzle rocket engine |
| 10/12/2005 | EP1583899A2 Controlled autoignition propellant systems |
| 10/11/2005 | US6952995 Apparatus and method for passive venting of rocket motor or ordnance case |
| 10/11/2005 | US6952917 Dual liquid engine and rocket using the same |
| 10/06/2005 | US20050218637 Gas generator assembly |
| 10/06/2005 | DE19927735B4 Schubkammer-Anordnung für Raumfahrt-Triebwerke Thrust chamber assembly for aerospace engines |
| 10/06/2005 | DE10245741B4 Schubdüse für eine Feststoffrakete Exhaust nozzle for a solid rocket |
| 09/29/2005 | US20050210862 Quantum jet turbine propulsion system |
| 09/29/2005 | DE10351715B4 Einspritzkopf für ein Flüssigkeitsraketentriebwerk Injection head for a liquid rocket engine |
| 09/27/2005 | US6948307 Rocket engine nozzle that is steerable by means of a moving diverging portion on a cardan mount |
| 09/27/2005 | US6948306 Apparatus and method of using supersonic combustion heater for hypersonic materials and propulsion testing |
| 09/22/2005 | US20050205717 Method of operating a satellite for end-of-life maneuvers |
| 09/21/2005 | CN1670353A 火箭发动机 Rocket Engine |
| 09/20/2005 | US6945495 Hydrogen powered toy rocket utilizing hydrogen from the electrolysis of water |
| 09/20/2005 | US6945032 Method for manufacturing outlet nozzles for rocket engines |
| 09/15/2005 | WO2004081452A3 Expander cycle rocket engine with staged combustion and heat exchange |
| 09/15/2005 | US20050198940 Ablative afterburner |
| 09/14/2005 | EP1574699A1 Afterburner with ablative nozzle |
| 09/08/2005 | US20050193917 Apparatus and method for passive venting of rocket motor or ordnance case |
| 09/08/2005 | DE102004006665A1 Coaxial injector with two combustion zones for kerosene and oxidant for rocket motor has axial entrance for kerosene and bores leading to first chamber leading to oxidant injection zones |
| 09/06/2005 | CA2214733C Fire mitigation device |
| 09/01/2005 | US20050188678 Component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 09/01/2005 | US20050188677 Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles |
| 09/01/2005 | DE102004008452A1 Strukturelement und Verfahren zur Herstellung desselben Structural element and method of manufacturing the same |
| 08/31/2005 | EP1568877A2 System and method for feeding at least a rocket motor |
| 08/31/2005 | EP1567761A2 Link between combustion chamber end wall and booster motor propeller nozzle |
| 08/25/2005 | WO2005077858A1 Structural element and method for producing said element |
| 08/25/2005 | US20050187516 Intradermal and subcutaneous injection device |
| 08/25/2005 | US20050183413 Pulse detonation engine and valve |
| 08/25/2005 | DE102004030303A1 Swivel nozzle assembly for steering boat, aircraft or spaceship has partially overlapping rings of progressively decreasing diameter pivoted so as to bend nozzle into curve |
| 08/23/2005 | US6931833 Pulse combustion device |
| 08/23/2005 | US6931832 Monopropellant combustion system |
| 08/18/2005 | US20050178886 Thrust vector actuation control system and method |
| 08/18/2005 | US20050178127 Rocket engine nozzle comprising a jet separation control system |
| 08/18/2005 | US20050178106 Enhanced performance torroidal coolant-collection manifold |
| 08/17/2005 | EP1564398A1 Toroidal coolant-collection manifold |
| 08/17/2005 | EP1198668B1 Hydrogen peroxide based propulsion system |
| 08/11/2005 | WO2005072220A2 Reversable space plane |
| 08/11/2005 | DE4337444B4 Verbesserungen bei bzw. im Zusammenhang mit Festtreibstoff-Brenneinrichtungen Improvements in or relating to solid fuel-burning equipment |
| 08/04/2005 | US20050166398 Advanced L-channel welded nozzle design |
| 08/03/2005 | EP1559539A1 Integrally woven ceramic composites |
| 08/03/2005 | EP1167188A4 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lrps), hybrid multifunction booster rocket with cruising lrps and development test therefor |
| 07/27/2005 | CN1646450A Protection against oxidation of parts made of composite material |
| 07/26/2005 | US6921014 Method for forming a channel on the surface of a metal substrate |
| 07/26/2005 | US6920750 Rocket engine member and a method for manufacturing a rocket engine member |
| 07/20/2005 | EP1555420A1 Process and apparatus for optimizing the flow regulation of a fluid by adapting the pressure drop |
| 07/20/2005 | EP1555419A1 Process and apparatus for optimizing the flow regulation of a fluid by adapting the pressure drop |
| 07/19/2005 | US6918243 Bi-propellant injector with flame-holding zone igniter |
| 07/14/2005 | US20050154347 Needle-free Injection device |
| 07/14/2005 | US20050152779 Inlet partial blades for structural integrity and performance |
| 07/14/2005 | US20050150207 Fluidic diverter valve with a variable valve-bore clearance |
| 07/12/2005 | US6915627 Rocket engine |
| 07/12/2005 | US6915626 Blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet |
| 07/07/2005 | US20050145679 Method for brazing ceramic surfaces |
| 07/07/2005 | DE10356157A1 Cruise missile, for launching from surface ships or submarines, uses unmodified air/ground missiles in launch containers with a booster platform for the initial thrust which is separated when the missile in on its trajectory |
| 07/05/2005 | US6912839 Ignition systems for hybrid and solid rocket motors |
| 06/30/2005 | WO2004099600A3 Method & apparatus for thrust augmentation for rocket nozzles |
| 06/30/2005 | US20050138933 Pulse detonation engine and method for initiating detonations |
| 06/30/2005 | DE10141108B4 Raketentriebwerk mit geschlossenen Triebwerkskreislauf mit modularer Zuführung der Turbinenabgase Rocket engine with closed cycle engine with modular supply the turbine exhaust |
| 06/23/2005 | DE10237381B4 Brennkammerstruktur und Verfahren zu deren Herstellung Combustion chamber structure and process for their preparation |
| 06/22/2005 | CN1629462A Explosion type engine |
| 06/21/2005 | US6907662 Method for manufacturing outlet nozzles for rocket engines |
| 06/16/2005 | DE10351715A1 Einspritzkopf für ein Flüssigkeitsraketentriebwerk Injection head for a liquid rocket engine |
| 06/15/2005 | EP1541850A1 Device to adapt the nozzle of a rocket motor with thrust vectoring control |
| 06/15/2005 | EP0920575B1 Microturbomachinery |
| 06/14/2005 | US6904755 Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same |
| 06/14/2005 | US6904749 Polyoxymethylene as structural support member and propellant |
| 06/09/2005 | US20050120704 System and fabrication method for actively cooling high performance components |
| 06/09/2005 | US20050120703 Steerable, intermittently operable rocket propulsion system |
| 06/09/2005 | US20050120700 Two-stage pulse detonation system |
| 06/09/2005 | DE10350735A1 Cooled combustion chamber for rocket engine, has cooling channels linked by openings in dividing walls |
| 06/08/2005 | EP1250526B1 Electrically-driven feed pump with high frequency variable reluctance actuator |
| 06/07/2005 | US6902809 Rhenium tantalum metal alloy |
| 06/07/2005 | US6901955 Cryogenic rotary coupling, and use thereof in particular in articulated fluid feed lines, and in cryogenic propellant rocket engines |
| 06/07/2005 | US6901740 Engine with a central spike for a space launcher |
| 06/02/2005 | WO2005049999A1 Process for igniting a rocket engine and rocket engine |
| 06/02/2005 | WO2005049998A1 Injection element |
| 06/02/2005 | US20050116084 Self-propelled projectile |
| 06/02/2005 | US20050115439 Multiple pulse segmented gas generator |
| 06/02/2005 | US20050115220 Hydraulic rocket |
| 06/02/2005 | CA2546371A1 Process for igniting a rocket engine and rocket engine |
| 06/01/2005 | CN1204019C Miniature integral cold air propeller |
| 05/25/2005 | EP1533511A1 Process for igniting a rocket engine and rocket engine |
| 05/24/2005 | US6895991 Lightweight pneumatic valves capable of withstanding the hostile environment generated from solid propellant or other propellants such as those used in rocket/missile applications ; does not need fins as its primary steering mechanism |
| 05/24/2005 | US6895756 Compact swirl augmented afterburners for gas turbine engines |
| 05/24/2005 | US6895743 Liquid propellant rocket motor |
| 05/17/2005 | US6893597 Method of insulating a case of a solid propellant rocket motor |
| 05/17/2005 | US6892525 Micropump-based microthruster |
| 05/12/2005 | US20050097883 Ablative baffle for a liquid rocket engine thrust chamber |
| 05/12/2005 | US20050097738 Strain control device for attaching transmission lines to deformable structures and methods employing same |