| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 09/03/2002 | US6442931 Combustion chamber casing of a liquid-fuel rocket engine |
| 09/03/2002 | US6442930 Combined cycle pulse detonation turbine engine |
| 08/27/2002 | US6439507 Closed-loop spacecraft orbit control |
| 08/22/2002 | WO2002039032A3 Method and system for densifying cryogenic propellants |
| 08/20/2002 | US6437640 Addressable diode isolated thin film array |
| 08/14/2002 | CN1364218A Apparatus for controlling heat transfer to nozzle wall of expander cycle rocket engines |
| 08/14/2002 | CN1364217A Apparatus for controlling flow separation line of rocket nozzles |
| 08/13/2002 | US6431072 Propellant grain configuration |
| 08/13/2002 | US6430920 Nozzleless rocket motor |
| 08/13/2002 | US6430919 Shaped charged engine |
| 08/13/2002 | US6430918 Solid fuel turbine drive system |
| 08/08/2002 | WO2002061384A1 Pressure sensor and rocket engine incorporating same |
| 08/01/2002 | US20020100508 Magnetically actuated valve system |
| 07/31/2002 | EP1227071A2 Cooled ceramic rocket combustion chamber |
| 07/25/2002 | US20020097079 Addressable diode isolated thin film array |
| 07/24/2002 | EP1225327A1 Range control of a rocket-propelled projectile |
| 07/24/2002 | EP1121336A4 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 07/23/2002 | US6421999 Modular solid-fuel rocket charges with rigid support casings |
| 07/23/2002 | US6421998 Thruster device responsive to solar radiation |
| 07/18/2002 | WO2002055864A1 Rocket engine member and a method for manufacturing a rocket engine member |
| 07/18/2002 | WO2002055863A1 Rocket engine member and a method for manufacturing a rocket engine member |
| 07/18/2002 | WO2002055862A1 Rocket engine member and method for manufacturing a rocket engine member |
| 07/18/2002 | WO2002055861A1 Method for manufacturing outlet nozzles for rocket engines |
| 07/18/2002 | WO2002055860A1 An outlet nozzle and a method for manufacturing an outlet nozzle |
| 07/18/2002 | US20020092560 Piston-activated valve and methods and apparatus for restraining free play in a device |
| 07/18/2002 | US20020092291 Combustion chamber with enhanced heat transfer to a cooling device |
| 07/18/2002 | US20020092290 Burning nitrous oxide and a fuel |
| 07/16/2002 | US6419856 Method and apparatus for total energy fuel conversion systems |
| 07/16/2002 | US6418973 Integrally woven ceramic composites |
| 07/16/2002 | US6418710 Deployable diverging part for a thruster |
| 07/16/2002 | CA2122148C Turbine engine control system |
| 07/11/2002 | DE10108253C1 Molding of articles from curable liquid, comprises deep drawing plastic sheet to form separating and carrier sheets, gluing them together, enclosing in mold filled with liquid containing cross-linking agent, and removing molding |
| 07/10/2002 | CA2367197A1 Liquid/solid fuel hybrid propellant system for a rocket |
| 07/10/2002 | CA2367192A1 Propellant system for solid fuel rocket |
| 07/09/2002 | US6415596 Method for increasing the specific impulse in a liquid-propellant rocket engine and rocket powder unit for realising the same |
| 07/04/2002 | US20020084190 Method and arrangement for the galvanic deposition of nickel, cobalt, nickel alloys or cobalt alloys with periodic current pulses |
| 07/03/2002 | EP1080302B1 Modular solid-fuel rocket propelling charges with a casing, a fill-drain system, cooling and suspension |
| 07/02/2002 | US6412275 Solid propellant gas generator impulse management scheme for high mass flow turn-down ratio |
| 07/02/2002 | US6412274 Solar thermal rocket |
| 06/27/2002 | US20020079404 Method and apparatus for planar actuation of a flared surface to control a vehicle |
| 06/27/2002 | US20020078680 Hybrid injection thrust vector control |
| 06/27/2002 | DE10060768A1 Drive mechanism has catalyser bed screened with respect to energy medium injection tube by wire mesh. in form of at least one pressed wire object fixed in holder |
| 06/26/2002 | CN2497060Y Assembled rain-increasing anti-hail rocket engine |
| 06/25/2002 | US6408760 Method of manufacturing solid rocket motors |
| 06/20/2002 | US20020077794 Rocket motor propellant temperature simulator |
| 06/18/2002 | US6405526 Solid fuel propulsion system for a ram jet rocket |
| 06/13/2002 | WO2002046594A1 Adjustable liquid rocket engine |
| 06/13/2002 | US20020069636 Hybrid rocket engine and method of propelling a rocket |
| 06/12/2002 | EP1213372A2 Process and arrangement for the galvanic deposition of nickel, cobalt, nickel alloys or cobalt alloys with periodic current pulses and use of the process |
| 06/12/2002 | EP1212566A2 Slip joint duct system |
| 06/11/2002 | US6403403 Diode isolated thin film fuel cell array addressing method |
| 06/11/2002 | US6402091 Flow-through thrust takeout apparatus |
| 06/06/2002 | WO2002018772B1 Segmented rocket drive and method for producing the same |
| 06/06/2002 | US20020066267 Process and device for collecting air, and engine associated therewith |
| 06/05/2002 | EP0862688B1 Controlled temperature rocket nozzle |
| 06/04/2002 | US6397580 High performance rocket engine having a stepped expansion combustion chamber and method of making the same |
| 05/30/2002 | US20020062756 Propellant grain configuration |
| 05/29/2002 | EP1209344A1 Rocket nozzle |
| 05/29/2002 | DE10054333A1 Brennkammer mit erhöhtem Wärmeeintrag in eine Kühleinrichtung Combustion chamber with increased heat input into a cooling device |
| 05/28/2002 | US6393830 Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines |
| 05/23/2002 | WO2002040429A1 Pyrotechnic charge structure |
| 05/23/2002 | US20020060271 Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (LRES), multifunctional launch vehicle of combined scheme with cruise LRES and method for refining it |
| 05/23/2002 | US20020059800 Device for reducing or eliminating jet separation in rocket engine nozzles, and a nozzle including the device |
| 05/21/2002 | US6392313 Microturbomachinery |
| 05/21/2002 | US6389801 Jet propulsion power unit with non-metal components |
| 05/16/2002 | WO2002039032A2 Method and system for densifying cryogenic propellants |
| 05/16/2002 | WO2002025091A3 Composition, method and device for pressurising a fuel tank |
| 05/16/2002 | US20020056762 Coolable nozzle and method for producing such a nozzle for a rocket engine |
| 05/16/2002 | CA2415313A1 Method and system for densifying cryogenic propellants |
| 05/14/2002 | US6385963 Optical system for generating endothermic fuel for use in a propulsion producing engine |
| 05/10/2002 | WO2002036955A1 Method and device for a multiple step rocket |
| 05/09/2002 | US20020053197 Combustion chamber casing of a liquid-fuel rocket engine |
| 05/08/2002 | EP1203879A2 Cooling for a combustion chamber for rockets |
| 05/08/2002 | DE10052422A1 Familie modularer Raketentriebwerke Family of modular rocket engines |
| 05/07/2002 | US6381949 Rocket engine having a transition attachment between a combustion chamber and an injector |
| 05/02/2002 | EP1200726A1 Erosion resistant rocket nozzle |
| 04/30/2002 | US6378436 Portable propellant cutting assembly, and method of cutting propellant with assembly |
| 04/30/2002 | US6378292 MEMS microthruster array |
| 04/24/2002 | EP1198668A1 Hydrogen peroxide based propulsion system |
| 04/24/2002 | EP1198500A1 Rocket motor insulation containing hydrophobic particles |
| 04/17/2002 | EP1196360A2 Family of propellant compositions and method |
| 04/16/2002 | US6370867 Throttleable rocket injector assembly |
| 04/16/2002 | US6370861 Solid fuel afterburner and method of using the same to improve thrust and starting capabilities of a turbojet engine |
| 04/11/2002 | WO2002029233A1 An annular combustor for a liquid-fuel rocket engine |
| 04/11/2002 | US20020040951 Asonic aerospike engine |
| 04/10/2002 | CN1343869A Impulse administration plan of solid propellant gas generator having high quality flow regulating rate |
| 04/09/2002 | US6367244 Propulsion system containing a mixed-phase propellant and a method for propelling an object with the same |
| 04/09/2002 | US6367243 Atomic-based combined cycle propulsion system and method |
| 04/03/2002 | EP1192115A1 Dinitramide based liquid mono-propellants |
| 04/03/2002 | CN1343282A 火箭发动机 Rocket engine |
| 03/28/2002 | WO2002025091A2 Composition, method and device for pressurising a fuel tank |
| 03/28/2002 | US20020036038 Flow of an oxidizer past the fuel to cause combustion with a flame and because of heat transfer from the flame, fuel forms an unstable melt layer causing droplets which entrined in oxidizer flow thereby increasing rate of burning of the fuel |
| 03/27/2002 | EP1189711A1 Manufacturing a dome from an undersized blank |
| 03/26/2002 | US6361018 Coaxial valve with electric actuating drive |
| 03/26/2002 | US6360993 Expendable launch vehicle |
| 03/26/2002 | US6360526 Rocket motor with desensitizer injector |
| 03/21/2002 | DE10043303A1 Raketentriebwerk in Segmentbauweise Rocket engine in segments |
| 03/20/2002 | EP1187979A1 Rocket thrust chamber |
| 03/20/2002 | EP1187978A1 Thrust chamber assembly |
| 03/20/2002 | CN1341086A Dinitramide based liquid mono-propellants |