| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 07/15/2003 | US6591499 Method for manufacturing outlet nozzles for rocket engines |
| 07/10/2003 | US20030126855 Net molded tantalum carbide rocket nozzle throat |
| 07/08/2003 | US6590403 Material regression sensor |
| 07/08/2003 | US6588199 High performance rocket engine having a stepped expansion combustion chamber and method of making the same |
| 07/08/2003 | CA2262854C Microturbomachinery |
| 07/02/2003 | CN1427145A Thrust control valve for reducing gain |
| 07/01/2003 | US6584774 High frequency pulsed fuel injector |
| 07/01/2003 | US6584764 Propulsion module |
| 07/01/2003 | US6584761 MAPP gas fuel for flight vehicles having pulse detonation engines and method of use |
| 06/26/2003 | WO2003052255A1 A component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 06/25/2003 | EP1321657A2 Reduced gain thrust control valve |
| 06/25/2003 | EP1189711A4 Manufacturing a dome from an undersized blank |
| 06/25/2003 | EP1161625B1 Nozzle structure for rocket nozzles having cooled nozzle wall |
| 06/25/2003 | EP1153213B1 Propellant grain capable of generating buffered boundary layer for reducing rocket nozzle recession |
| 06/24/2003 | US6582542 Method of producing a channeled wall fluid control apparatus |
| 06/24/2003 | US6581882 Low-thrust cryogenic propulsion module |
| 06/24/2003 | US6581881 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 |
| 06/24/2003 | CA2101341C Long range artillery shell |
| 06/19/2003 | WO2003050492A1 Measuring shear stress at an interface with two walls and two crossed sensor elements |
| 06/18/2003 | EP1319823A2 Method of producing an insultated rocket engine casing and insulated casing produced in this way |
| 06/18/2003 | EP1319123A2 Composition, method and device for pressurising a fuel tank |
| 06/18/2003 | EP1192115B1 Dinitramide based liquid mono-propellants |
| 06/12/2003 | WO2003047969A2 System and method for controlling a space-borne propulsion system |
| 06/12/2003 | US20030106452 Method for generating energy by using exothermic reaction of metal |
| 06/12/2003 | US20030106379 System and method for measuring stress at an interface |
| 06/11/2003 | CN1422832A Method for generating energy utilizing metal exothermic reaction |
| 06/10/2003 | US6574964 Rocket nozzle contour for flow separation control and side load reduction |
| 06/10/2003 | US6574952 Apparatus for controlling the flow separation line of rocket nozzles |
| 06/10/2003 | US6574951 Solar thermal rocket |
| 06/05/2003 | WO2003046359A1 Rocket motors with insensitive munitions systems |
| 06/05/2003 | US20030102409 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 |
| 06/05/2003 | US20030102408 Reusable space access launch vehicle system |
| 06/04/2003 | EP1316680A2 Method for generating energy by using exothermic reaction of metal |
| 06/04/2003 | EP1316505A1 A reusable space access launch vehicle system |
| 06/04/2003 | CN1421673A Repeatable using space entry carrier rocket system |
| 06/03/2003 | US6572030 Device for displacing to nozzle outlet or eliminating jet separation in rocket engine nozzles, and a nozzle including the device |
| 06/03/2003 | US6571618 Support device for a motorized flying instrument in a wind tunnel |
| 06/03/2003 | CA2385192A1 Method for generating energy by using exothermic reaction of metal |
| 05/30/2003 | WO2003044431A1 Flow-type body and combustion device provided with a flow-type body of this type |
| 05/29/2003 | US20030098397 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 |
| 05/29/2003 | US20030098396 Apparatus for load transfer between aerospace vehicle components, aerospace vehicles including same, and method of attachment of aerospace vehicle components |
| 05/29/2003 | US20030098107 Fuel in a combustion chamber and means for causing an oxidizer to flow past the fuel to cause combustion, heat transfer forms an unstable melt layer that forms droplets entrained in the oxidizer increasing the rate of burning |
| 05/28/2003 | EP1313938A1 Segmented rocket drive and method for producing the same |
| 05/28/2003 | EP1082213A4 Non-asbestos insulation for rocket motor casing |
| 05/27/2003 | US6568171 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 05/27/2003 | CA2091241C Low cost segmented structure for pressure vessels, rocket motors, piping |
| 05/22/2003 | US20030093987 Integrated tankage for propulsion vehicles and the like |
| 05/20/2003 | US6566420 EPDM rocket motor insulation |
| 05/20/2003 | US6564542 Ignition system for combustion chambers of rocket engines |
| 05/15/2003 | US20030089434 Method and apparatus for the preparation and usage of a cryogenic propellant or explosive system |
| 05/14/2003 | EP1310659A1 Apparatus and method for initiating a combustion reaction with slurry fuel |
| 05/14/2003 | EP1309523A1 Net molded tantalum carbide rocket nozzle throat |
| 05/14/2003 | EP0960317B1 Case for combustible materials and process for forming the same |
| 05/08/2003 | US20030085112 Apparatus and method for initiating a combustion reaction with slurry fuel |
| 05/06/2003 | US6557339 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 |
| 05/06/2003 | CA2275927C Method and apparatus for total energy fuel conversion systems |
| 05/01/2003 | US20030079905 Strain control device for attaching transmission lines to defromable structures and methods employing same |
| 05/01/2003 | US20030079464 Rocket motors with insensitive munitions systems |
| 05/01/2003 | US20030079463 Turbojet with precompressor injected oxidizer |
| 04/30/2003 | CN1107164C Method for mfg. outlet nozzles for rocket engines |
| 04/24/2003 | US20030074887 Catalyst bed |
| 04/24/2003 | US20030074886 High performance rocket engine having a stepped expansion combustion chamber and method of making the same |
| 04/24/2003 | US20030074883 Efficient power generation systems contains a turbine, a combustor and a rocket engine with nozzle and a compressor |
| 04/22/2003 | US6550235 Combined cycle pulse detonation turbine engine operating method |
| 04/16/2003 | EP1003989B1 Quick-acting valve |
| 04/15/2003 | US6548794 Dissolvable thrust vector control vane |
| 04/10/2003 | US20030067229 Actuator apparatus including a marker device |
| 04/09/2003 | EP1299673A2 Method and system for densifying cryogenic propellants |
| 04/08/2003 | US6543717 Compact optimal and modulatable thrust device for controlling aerospace vehicles |
| 04/08/2003 | US6543135 Method for producing a nozzle for a rocket engine |
| 04/02/2003 | EP1298389A1 Coaxial spray nozzle injector |
| 04/01/2003 | US6539703 Spacecraft component with microthruster actuation and operation thereof |
| 03/27/2003 | WO2003024797A2 Propellant utilization system |
| 03/27/2003 | US20030056838 Variable-gravity anti-vortex and vapor-ingestion-suppression device |
| 03/25/2003 | US6537617 Manufacturing method of ceramic matrix composite |
| 03/25/2003 | US6536208 Device for supplying fuel for a rocket propulsion unit and heat exchanger to be used in said device |
| 03/20/2003 | WO2002103199A3 Method and apparatus for ignition detection |
| 03/20/2003 | US20030051536 Method and apparatus for testing engines |
| 03/20/2003 | US20030051462 Rocket Propulsion System |
| 03/18/2003 | US6532750 Method and system for densifying cryogenic propellants |
| 03/18/2003 | US6532741 Gas generator for producing adjustable flow |
| 03/18/2003 | US6532730 Slip joint duct system for a rocket fuel duct |
| 03/13/2003 | US20030046923 Pintle injector rocket with expansion-deflection nozzle |
| 03/13/2003 | US20030046922 Rocket nozzle assembly having rotatable variable thrust control cylinders, and rocket assembly comprising the same |
| 03/13/2003 | US20030046920 Shaped charge engine |
| 03/12/2003 | EP0975863B1 Missile with safe rocket ignition system |
| 03/11/2003 | US6530213 Method and apparatus for ignition detection |
| 03/11/2003 | US6530212 Laser plasma thruster |
| 03/05/2003 | EP1053394A4 Method and apparatus for total energy fuel conversion systems |
| 02/27/2003 | WO2003016849A2 Method and apparatus for testing engines |
| 02/26/2003 | EP1286039A2 Rocket engine with injection of an additional mass flow |
| 02/26/2003 | EP1286038A1 Autonomous working gas supply system, use of such a system to pressurize a container, laucher stage including such a system |
| 02/19/2003 | CN1397725A Pressure actuating joint system |
| 02/18/2003 | US6519928 Process for the production of a transverse thrust in a flying object |
| 02/13/2003 | US20030029162 Propulsion module |
| 02/13/2003 | US20030029161 Mapp gas fuel for flight vehicles having pulse detonation engines and method of use |
| 02/13/2003 | US20030029160 Combined cycle pulse detonation turbine engine |
| 02/12/2003 | EP1283347A1 Auxiliary propulsion system of a cryogenic launcher stage and launcher stage comprising such a system |
| 02/11/2003 | US6516872 High heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine |
| 02/11/2003 | US6516605 Pulse detonation aerospike engine |