| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 03/19/2002 | US6359188 Combusting propellant concurrent spraying with liquid |
| 03/19/2002 | US6357357 Propulsion system |
| 03/13/2002 | EP1185778A2 Simplified high-efficiency propulsion system |
| 03/13/2002 | CN1339652A High energy jet engine |
| 03/13/2002 | CN1080823C Controlled temperature rocket nozzle |
| 03/12/2002 | US6354075 Vented rocket motor spacer |
| 03/12/2002 | US6354074 Hybrid injection thrust vector control |
| 03/07/2002 | WO2002018772A1 Segmented rocket drive and method for producing the same |
| 03/07/2002 | WO2001054981A3 Propulsion module |
| 03/07/2002 | US20020026788 Ignition system for combustion chambers of rocket engines |
| 03/06/2002 | EP1184560A2 Rocket nozzle assembly having rotatable thrust control cylinders, and rocket assembly comprising the same |
| 03/06/2002 | EP1184559A1 Closure device for the entry of a duct, in particular for an air inlet duct to a ramjet combustion chamber |
| 03/05/2002 | US6352030 Gas generating eject motor |
| 03/05/2002 | US6351939 Swirling, impinging sheet injector |
| 02/28/2002 | US20020023484 Support device for a motorised flying instrument in a wind tunnel |
| 02/28/2002 | US20020023428 Blanking-cap system for an orifice of a conduit, in particular for an orifice of an air-intake duct into the combustion chamber of a ramjet |
| 02/28/2002 | US20020023427 Micro-colloid thruster system |
| 02/27/2002 | CN1337912A Payload carry and Launch system |
| 02/26/2002 | US6350394 Generation power with rocket engines, nozzles, compressors, carbon feeds |
| 02/21/2002 | DE10109509A1 Verfahren und Vorrichtung zum Positionieren von Satelliten in eine niedrige Erdumlaufbahn Method and device for positioning of satellites in low Earth orbit |
| 02/20/2002 | CN2477844Y Auxiliary appts. of rocket engine |
| 02/19/2002 | CA2188393C A device for controlling a spacecraft by gating gas via a moving nozzle |
| 02/19/2002 | CA2188341C System for controlling a space vehicle by gating gas |
| 02/14/2002 | US20020018847 Blend of carbon fiber and ethylene-propylene-ethylidenenorbornene terpolymer; uniform mixing |
| 02/13/2002 | EP1179132A1 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines |
| 02/13/2002 | EP1179131A1 An apparatus for controlling the flow separation line of rocket nozzles |
| 02/07/2002 | US20020014070 Rocket engine having a transition attachment between a combustion chamber and an injector |
| 02/05/2002 | US6343464 Solar thermal rocket |
| 01/30/2002 | CN1078665C 火箭发动机喷管 Rocket engine nozzle |
| 01/24/2002 | WO2002006119A1 Multistage modularised boost rocket |
| 01/23/2002 | EP1173668A1 Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines |
| 01/17/2002 | WO2002004382A1 Net molded tantalum carbide rocket nozzle throat |
| 01/17/2002 | WO2001046581A3 System and method for feeding at least a booster motor, and electrically-driven feed pump with high frequency variable reluctance actuator |
| 01/17/2002 | DE19958310C2 Raketentriebwerk für Flüssigtreibstoffe mit einem geschlossenen Triebwerkskreislauf Rocket engine for liquid fuels with a closed cycle engine |
| 01/17/2002 | DE10061186C1 Electroplating of nickel, cobalt, and their alloys onto rocket engine components, uses differing current densities and pulsed charge ratios at anode and cathode |
| 01/16/2002 | EP1172545A1 Ignition system for combustion chambers in rocket engines |
| 01/16/2002 | EP1172544A1 Combined turbo and rocket engine with air liquefier and air separator |
| 01/16/2002 | EP1171705A2 Rocket engine |
| 01/10/2002 | WO2002002990A1 Coaxial spray nozzle injector |
| 01/02/2002 | EP1167941A1 Support for a motorised flying device in a wind tunnel |
| 01/02/2002 | EP1167188A1 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 |
| 12/20/2001 | DE10126797A1 Solare thermische Rakete Solar thermal rocket |
| 12/19/2001 | EP1163152A2 Payload carry and launch system |
| 12/18/2001 | US6330793 Erosion resistant rocket nozzle |
| 12/18/2001 | US6330792 Rocket engine thrust chamber assembly |
| 12/18/2001 | CA2016346C Fringed thermal protection device and method of manufacturing it |
| 12/13/2001 | US20010049935 Process for the production of a transverse thrust in a flying object |
| 12/12/2001 | EP1162139A1 Reusable booster for the first stage of a launcher |
| 12/12/2001 | EP1161625A1 Nozzle structure for rocket nozzles having cooled nozzle wall |
| 12/05/2001 | EP1160222A2 Manufacturing method of ceramic matrix composite |
| 12/04/2001 | US6324833 Reinforced composite articles and method of making same |
| 12/04/2001 | US6324832 Ampoule with starting fuel for igniting LRE propellant components |
| 11/29/2001 | US20010046563 Manufacturing method of ceramic matrix composite |
| 11/29/2001 | US20010045248 Multi-ignition controllable solid-propellant gas generator |
| 11/27/2001 | US6321774 Control valve for cryogenic use |
| 11/27/2001 | US6321528 Turbine, for a liquid-propellant rocket engine mainly |
| 11/27/2001 | US6321450 Method for producing a gas generator of welded-brazed construction |
| 11/27/2001 | US6321449 Method of forming hollow channels within a component |
| 11/20/2001 | US6318071 Controlled temperature rocket nozzle |
| 11/14/2001 | EP1153214A1 Device for supplying fuel for a rocket propulsion unit and heat exchanger to be used in said device |
| 11/14/2001 | EP1153213A2 Propellant grain capable of generating buffered boundary layer for reducing rocket nozzle recession |
| 11/14/2001 | CN1322276A Nozzle structure for rocket nozzle having cooled nozzle wall |
| 11/14/2001 | CN1322275A Rocket nozzle contour for flow separation control and side load reduction |
| 11/13/2001 | US6314978 Reciprocating feed system for fluids |
| 11/13/2001 | US6314720 Rocket combustion chamber coating |
| 11/13/2001 | US6314719 Ignition system for a propulsion producing engine |
| 11/08/2001 | DE10107668A1 Solar heating rocket has solar concentrator which through selective directing devices focuses solar energy on heat storage section or on direct yield section |
| 11/07/2001 | CN1321219A Method for mfg. outlet nozzles for rocket engines |
| 11/06/2001 | US6311479 Modular cryogenic solid fuel rocket drive sets |
| 11/01/2001 | US20010035005 Rocket motor with desensitizer injector |
| 10/30/2001 | US6308514 Rocket engine nozzle |
| 10/30/2001 | US6308408 Fabrication process for combustion chamber/nozzle assembly |
| 10/25/2001 | WO2000043445A9 Novel epdm rocket motor insulation |
| 10/18/2001 | DE10018494A1 Regulator valve for solid fuel powered engine has oppositely disposed inlet openings at closed end of gas duct facing gas generator and principal axes of which are located approximately perpendicularly to principal axis of gas duct |
| 10/17/2001 | EP1144942A1 Improved propulsion system |
| 10/17/2001 | EP1144836A1 Combustion chamber cooling structure for a rocket engine |
| 10/17/2001 | EP1144835A2 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |
| 10/17/2001 | EP1144344A2 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 10/17/2001 | CN1318130A Rocket assembly ablative materials formed from, as precursor, staple cellulose fibers, and method of insulating or thermall protecting rocket assembly with same |
| 10/11/2001 | DE10015369A1 Tri-Koaxiales Einspritzelement Tri-coaxial injection element |
| 10/10/2001 | EP1141119A2 Novel epdm rocket motor insulation |
| 10/09/2001 | US6298659 Vortex flow field and apparatus and method for producing the same |
| 10/09/2001 | US6298658 Multi-stable thrust vectoring nozzle |
| 10/04/2001 | US20010025483 Tricoaxial injection element |
| 10/04/2001 | EP1138923A1 A multi-staged rocket engine with an interstage separation bulkhead |
| 10/04/2001 | EP1138922A1 Combined cycle pulse detonation turbine engine |
| 09/27/2001 | US20010023583 Controlled temperature rocket nozzle |
| 09/26/2001 | EP1135588A1 Rocket nozzle contour for flow separation control and side load reduction |
| 09/25/2001 | US6293503 Space Launch system with pressure reduction devices between stages |
| 09/20/2001 | WO2001069136A1 Laser ignition |
| 09/20/2001 | WO2001069070A1 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines |
| 09/20/2001 | WO2001069069A1 An apparatus for controlling the flow separation line of rocket nozzles |
| 09/18/2001 | US6290185 Solar thermal rocket |
| 09/18/2001 | US6289671 Plug for a liquid-propellant rocket engine chamber |
| 09/18/2001 | US6289669 Lateral-thrust control arrangement for missiles with solid-fuel hot-gas generator |
| 09/07/2001 | WO2001065103A1 Shaped charge engine |
| 09/07/2001 | WO2001064513A1 Method and apparatus for placing satellites in low earth orbit |
| 09/07/2001 | CA2401759A1 Shaped charge engine |
| 09/04/2001 | US6283412 Anti-slosh liquid propellant tank for launch vehicles |
| 09/04/2001 | US6282887 Bellows units for a chamber of a liquid-propellant rocket engine with afterburning |