| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 01/11/2001 | WO2001002716A1 Erosion resistant rocket nozzle |
| 01/11/2001 | WO2001002131A1 Method of producing channeled wall apparatus |
| 01/11/2001 | CA2378019A1 Erosion resistant rocket nozzle |
| 01/09/2001 | US6170258 Liquid-propellant rocket engine |
| 01/09/2001 | US6170257 Variable thrust nozzle system |
| 01/09/2001 | US6170256 Anchor device for a member for actuating a steerable nozzle |
| 01/03/2001 | CN1278504A Multifunctional driving system for aviation, aerospace and navigation |
| 12/28/2000 | WO2000079167A2 Slip joint duct system |
| 12/28/2000 | WO2000079116A1 Rocket thrust chamber |
| 12/28/2000 | WO2000079115A1 Thrust chamber assembly |
| 12/28/2000 | DE19927735A1 Thrust chamber for space travel propulsion units has thermally conducting film at least in area on outside of preparation chamber wall on which fuel forms cooling film before combustion |
| 12/28/2000 | DE19927734A1 Thrust chamber housing for satellite/space transporter propulsion system has combustion nozzle part welded to chamber, expansion nozzle housings via platinum-rhodium alloy rings |
| 12/26/2000 | US6164060 Combustion chamber/nozzle assembly and fabrication process therefor |
| 12/21/2000 | DE4345153A1 Artilleriegranate langer Reichweite Artillery shell long-range |
| 12/14/2000 | DE19924907A1 Feststofftriebwerk für eine Staustrahlrakete Solid engine for a ramjet missile |
| 12/14/2000 | DE19648668A1 Langstrecken-Artilleriegeschoß Long-range artillery shell |
| 12/12/2000 | US6158693 Recoverable booster stage and recovery method |
| 12/07/2000 | WO2000049282A3 Propellant grain capable of generating buffered boundary layer for reducing rocket nozzle recession |
| 12/06/2000 | EP1057996A2 Solid propellant device for a ram jet |
| 12/06/2000 | CN1275939A Method for producing rotational-symmetrical articles of sheet metal with double curved surface and varying thickness of material |
| 12/05/2000 | US6155173 Model rocket motor retainer |
| 12/05/2000 | US6155041 Hybrid engine capable of employing at least a ramjet mode and a super ramjet mode |
| 11/30/2000 | WO2000071880A2 Simplified high-efficiency propulsion system |
| 11/28/2000 | US6152039 Initiation of propellants |
| 11/28/2000 | US6151900 Cryogenic densification through introduction of a second cryogenic fluid |
| 11/28/2000 | US6151887 Combustion chamber for rocket engine |
| 11/28/2000 | CA2037939C Missile piloting system with lateral jet steams |
| 11/22/2000 | EP1053394A1 Method and apparatus for total energy fuel conversion systems |
| 11/21/2000 | US6148610 Solid propellant charge for a propulsion unit and propulsion unit equipped with such a charge |
| 11/16/2000 | WO2000022291A9 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 11/14/2000 | US6146714 Method of forming metal, ceramic or ceramic/metal layers on inner surfaces of hollow bodies using pulsed laser deposition |
| 11/14/2000 | US6145299 Rocket engine |
| 11/09/2000 | DE19921067A1 Aerodynamic lift adjustment unit for the center of pressure in a modular construction aircraft, which may be propelled by solid fuel rocket motors |
| 11/02/2000 | WO2000043445A3 Novel epdm rocket motor insulation |
| 11/01/2000 | CN1271811A Jet engine with rotary combustion chamber |
| 10/31/2000 | US6138451 Rocket engine with combustion chamber step structure insert, and its fabrication |
| 10/31/2000 | US6138450 Rocket engine with integral combustion chamber step structure and its fabrication |
| 10/26/2000 | WO2000063139A2 Family of propellant compositions and method |
| 10/26/2000 | DE19901257C1 Regelventil für Tieftemperatur-Einsatz Control valve for low-temperature use |
| 10/26/2000 | CA2367454A1 Family of propellant compositions and method |
| 10/24/2000 | US6135393 Spacecraft attitude and velocity control thruster system |
| 10/24/2000 | US6134785 Method of fabricating an article of manufacture such as a heat exchanger |
| 10/24/2000 | US6134782 Method of forming a rocket thrust chamber |
| 10/24/2000 | US6134781 Method for making a throat insert for rocket thrusters |
| 10/19/2000 | WO2000024693A9 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 10/18/2000 | CN1270304A Disposable launching vehicle |
| 10/17/2000 | US6131858 Compact single-propellant unitary propulsion system for a small satellite |
| 10/17/2000 | US6131385 Integrated pulsed propulsion system for microsatellite |
| 10/17/2000 | US6131280 Method of repairing a rocket thrust chamber |
| 10/12/2000 | WO2000034731A3 Gas generating eject motor |
| 10/11/2000 | EP1043227A2 An expendable launch vehicle |
| 10/10/2000 | US6129236 Tank for the liquid storage and expulsion |
| 10/05/2000 | WO2000058619A1 Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines |
| 10/03/2000 | US6125763 Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same |
| 09/28/2000 | WO2000057048A2 Rocket engine |
| 09/28/2000 | WO2000043712A3 Steam generator injector |
| 09/28/2000 | WO2000043267A3 Payload carry and launch system |
| 09/14/2000 | WO2000045041B1 Device for supplying fuel for a rocket propulsion unit and heat exchanger to be used in said device |
| 09/13/2000 | EP1034063A1 A method for producing rotational-symmetrical articles of sheet metal with double curved surface and varying thickness of material |
| 09/12/2000 | US6116368 Electric vehicle with battery regeneration dependent on battery charge state |
| 09/12/2000 | US6116030 Vacuum pump and propellant densification using such a pump |
| 09/12/2000 | US6116020 Injector for liquid fueled rocket engine |
| 09/06/2000 | EP1033487A2 Ampoule with starting fuel for igniting liquid rocket propellant components |
| 09/06/2000 | EP1033303A2 Cryogenic densification through introduction of a second cryogenic fluid |
| 09/06/2000 | EP1033198A2 Method for producing a gas generator of welded-brazed construction |
| 09/05/2000 | US6112515 Device and process for fastening an injection element in the injection head of a rocket engine |
| 08/31/2000 | WO2000050363A1 Dinitramide based liquid mono-propellants |
| 08/30/2000 | EP1031729A2 A tank for liquid storage and expulsion |
| 08/30/2000 | EP1031724A2 Plug for a rocket combustion chamber |
| 08/29/2000 | CA2038091C Missile guiding system using side exhaust nozzles |
| 08/24/2000 | WO2000049282A2 Propellant grain capable of generating buffered boundary layer for reducing rocket nozzle recession |
| 08/23/2000 | EP1030049A1 Solid propellant rocket motor with safety device for conditions of intense thermal stresses |
| 08/22/2000 | US6107596 Method for producing a welded-brazed combustion chamber |
| 08/17/2000 | WO2000040919B1 Improved propulsion system |
| 08/15/2000 | US6101957 Apparatus for after-burning fuel rich rocket exhaust products |
| 08/15/2000 | US6101948 Method of manufacturing solid rocket motors |
| 08/15/2000 | US6101808 Cryogenic solid hybrid rocket engine and method of propelling a rocket |
| 08/10/2000 | WO2000024693A3 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 08/09/2000 | EP1025947A2 Method for producing a welded-brazed construction |
| 08/03/2000 | WO2000045041A1 Device for supplying fuel for a rocket propulsion unit and heat exchanger to be used in said device |
| 08/03/2000 | DE19903664A1 Einrichtung zur Treibstoffzufuhr für ein Raketentriebwerk und Wärmetauscher zur Verwendung in der Einrichtung Device for supplying fuel for a rocket engine and heat exchanger for use in the device |
| 08/01/2000 | US6094906 Design for a gun-launched rocket |
| 07/27/2000 | WO2000043712A2 Steam generator injector |
| 07/27/2000 | WO2000043445A2 Novel epdm rocket motor insulation |
| 07/27/2000 | WO2000043267A2 Payload carry and launch system |
| 07/27/2000 | WO2000005133A9 High regression rate hybrid rocket propellants |
| 07/27/2000 | DE19901424A1 Brennkammer mit Transpirationskühlung Combustion chamber with transpiration |
| 07/27/2000 | DE19901422A1 Brennkammer-Kühlstruktur für ein Raketentriebwerk Combustor cooling structure for a rocket engine |
| 07/26/2000 | EP1022456A2 Coating for a liquid-propellant rocket combustion chamber |
| 07/26/2000 | EP1022455A2 Liquid-propellant rocket engine chamber and its casing |
| 07/26/2000 | EP1022454A2 Liquid propellant rocket engine |
| 07/25/2000 | US6092366 Hybrid rocket system and integrated motor for use therein |
| 07/20/2000 | WO2000042310A1 Combustion chamber cooling structure for a rocket engine |
| 07/20/2000 | WO2000042309A1 Combustion chamber with transpiration cooling |
| 07/13/2000 | WO2000040919A1 Improved propulsion system |
| 07/13/2000 | WO2000022291A3 Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 07/13/2000 | DE19915082C1 Regeneratively cooled rocket motor nozzle comprizes spiraled coolant-flowed tubing subsequently sprayed with loadbearing and fixing layers once exterior mandrel former is stripped off. |
| 07/12/2000 | CN1054345C Integrated storage and transfer system and method for spacecraft propulsion systems |
| 07/11/2000 | US6085516 Hybrid rocket system and integrated motor for use therein |
| 07/06/2000 | WO2000014397A9 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |