| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
|---|
| 06/25/2008 | EP1936354A1 Apparatus and method for thermo-erosive testing of materials used as thermal shields for solid propellant rockets. |
| 06/25/2008 | EP1934547A2 Exhaust assembly for mass ejection drive system |
| 06/25/2008 | EP1934457A2 Advanced hypersonic magnetic jet/electric turbine engine |
| 06/24/2008 | US7389636 Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle |
| 06/19/2008 | US20080142639 Method For Detecting Complete Draining of a Propellant Tank and For Propellant Management onBoard a Satellite |
| 06/19/2008 | US20080141653 Engine propulsion system and methods of assembling the same |
| 06/19/2008 | DE10107668B4 Solarwärmerakete Solar thermal rocket |
| 06/18/2008 | EP1931871A2 Thrust augmentation in plug nozzles and expansion-deflection nozzles |
| 06/12/2008 | WO2008069705A1 A liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith |
| 06/12/2008 | US20080134667 Systems, methods and apparatus for propulsion |
| 06/11/2008 | EP1929147A1 A method of producing an engine wall structure |
| 06/05/2008 | WO2008066486A1 Micro system based solid state gas storage |
| 06/04/2008 | EP1926904A1 An engine wall structure and a method of producing an engine wall structure |
| 05/29/2008 | US20080121548 Coating for components requiring hydrogen peroxide compatibility |
| 05/28/2008 | CN100390113C Method and apparatus for total energy fuel conversion systems |
| 05/22/2008 | WO2008060255A2 Electrically controlled extinguishable solid propellant motors |
| 05/21/2008 | EP1807621B1 Device for the supply of a rocket motor with fuel and oxidiser |
| 05/20/2008 | US7373885 Device for venting a container housing an energetic material and method of using same |
| 05/20/2008 | US7373774 Enhanced performance torroidal coolant-collection manifold |
| 05/15/2008 | DE202008001702U1 Anlage zur Abgasreinigung für Raketentriebwerke For exhaust gas purification system for rocket engines |
| 05/14/2008 | EP1352167B1 Method for manufacturing outlet nozzles for rocket engines |
| 05/13/2008 | US7371784 EPDM rocket motor insulation |
| 05/13/2008 | US7370469 Rocket chamber heat exchanger |
| 05/07/2008 | EP1918565A2 Ignition anode for re-ignitable rocket thrust chambers |
| 05/06/2008 | US7368025 Method for making a thermally protective coating for a propulsive unit structure |
| 05/06/2008 | CA2364284C Rocket engine |
| 04/30/2008 | EP1352169B1 Rocket engine member and a method for manufacturing a rocket engine member |
| 04/24/2008 | US20080092521 Electrically controlled extinguishable solid propellant motors |
| 04/24/2008 | US20080092518 Variable area flow duct employing secondary flows, and method therefor |
| 04/22/2008 | US7360355 Long range artillery shell |
| 04/17/2008 | US20080087003 Methods of controlling solid propellant ignition, combustion, and extinguishment |
| 04/16/2008 | EP1608863A4 Unitized hybrid rocket system |
| 04/09/2008 | EP1908949A1 Rocket engine |
| 04/09/2008 | CN101158321A Low-temperature plasma non-hot point fire steadying flame device |
| 04/09/2008 | CN101157175A A processing method of titanium alloy closing end |
| 04/03/2008 | US20080078164 Rocket engine combustion chamber |
| 04/02/2008 | EP1905997A1 Rocket enginge |
| 03/27/2008 | DE19648668B4 Langstrecken-Artilleriegeschoß Long-range artillery shell |
| 03/26/2008 | EP1903206A2 Injector for rocket engine |
| 03/26/2008 | CN101149028A Cooling heat transferring channel for ultra-combustion ramjet engine and rocket engine |
| 03/25/2008 | US7347041 Rocket engine combustion chamber |
| 03/19/2008 | CN101144442A Multi-pipe impulse detonating combustion camber and detonation method thereof |
| 03/19/2008 | CN101144441A Turbine-rocket embedded type engine |
| 03/18/2008 | US7344111 Reversible space plane |
| 03/18/2008 | US7343732 Rocket engine chamber with layered internal wall channels |
| 03/13/2008 | WO2008030175A1 Nozzle arrangement for use in a gas thruster, gas thruster, method for manufacturing a nozzle arrangement, method for in-situ repairing of a nozzle arrangement and a method for operating a gas thrusters |
| 03/13/2008 | WO2008029303A2 Triple helical flow vortex reactor |
| 03/12/2008 | EP1897929A1 Method for total energy fuel conversion systems |
| 03/12/2008 | EP1896718A1 Gel-type fuel based drive device and method for supplying fuel |
| 03/12/2008 | EP1671025B1 Rocket engine having guide vanes in the nozzle of the engine |
| 03/06/2008 | WO2008027022A2 Methods of controlling solid propellant ignition, combustion, and extinguishment |
| 03/06/2008 | US20080056961 Three fluid flow vortexes, double end orbiting plasma arc to sustain combustion; first vortex is fuel and combusted gases away from fuel inlet; second vortex starts at gas outlet, is confined to thin layer at inner wall, spirals in reverse; third starts at inlet in thin layer at wall, vortex as first |
| 03/06/2008 | US20080053064 Rocket engine power cycle |
| 03/06/2008 | US20080053063 Three component injector for kerosene-oxygen rocket engine |
| 02/26/2008 | US7334396 Method and apparatus for a rocket engine power cycle |
| 02/20/2008 | EP1888488A1 Structural element and method for producing the same |
| 02/13/2008 | EP1171705B1 Rocket engine |
| 02/12/2008 | US7328571 Semi-axisymmetric scramjet flowpath with conformal nozzle |
| 02/06/2008 | EP1884638A2 Method and apparatus for total energy fuel conversion systems |
| 01/30/2008 | EP1882842A1 Heat transfer thruster |
| 01/24/2008 | WO2008010748A1 Method for manufacturing a wall structure |
| 01/10/2008 | WO2008004744A1 Methane engine for rocket propulsion |
| 01/10/2008 | US20080006020 Explosive material sensitivity control |
| 01/09/2008 | EP1875153A1 Missile control system and method |
| 01/08/2008 | CA2344232C Castable double base solid rocket propellant containing ballistic modifier pasted in an inert polymer |
| 01/03/2008 | US20080000217 Method and apparatus for a rocket engine power cycle |
| 01/02/2008 | EP1873390A2 Heat exchange injector for use in a rocket engine |
| 12/27/2007 | WO2007147522A1 Injection head, mixing space and power plant |
| 12/27/2007 | WO2007035298A3 Advanced hypersonic magnetic jet/electric turbine engine |
| 12/27/2007 | WO2005097557A3 Gas generator assembly |
| 12/27/2007 | DE102006029586A1 Einblaskopf, Mischungsraum und Triebwerk Blowing head, mixing chamber and engine |
| 12/26/2007 | EP1868891A2 Two-phase cold gas propulsion system and tank for such a space craft propulsion system |
| 12/26/2007 | CN101092916A Rocket motor with replaceable fuel body |
| 12/13/2007 | US20070285304 Target orbit modification via gas-blast |
| 12/06/2007 | WO2007139452A1 Method for fastening of a heater |
| 12/05/2007 | CN101082312A Double group component sydraulic free-piston engine |
| 12/04/2007 | US7302794 Rocket engine member and a method for manufacturing a rocket engine member |
| 11/29/2007 | DE102006014729B3 Steerable projectile for average caliber ammunition comprises a drive based on a gel, an annular nozzle with a receiver for steering information and a cross-shift control unit with an energy supply from the stream of a diffuser |
| 11/27/2007 | US7299636 Extendible exhaust nozzle bell for a rocket engine |
| 11/27/2007 | US7299622 Component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 11/27/2007 | US7299551 Method of assembling a rocket engine with a transition zone between the combustion chamber and the coolant system |
| 11/21/2007 | CN100350142C Air-fuel ratio control apparatus for an internal combustion engine |
| 11/20/2007 | US7296396 Method for using variable supersonic Mach number air heater utilizing supersonic combustion |
| 11/15/2007 | US20070261386 Single-Piece Hybrid Rocket Motor |
| 11/15/2007 | US20070261385 Basalt fiber and nanoclay compositions, articles incorporating the same, and methods of insulating a rocket motor with the same |
| 11/13/2007 | US7293403 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
| 11/13/2007 | US7293402 Injection head for a liquid-propelled rocket engine |
| 11/08/2007 | WO2007125249A1 Method of producing a fibrous layer for the manufacture of a preform of a composite part |
| 11/08/2007 | DE102007020010A1 Two component fuel injection device for use in e.g. non-hypergolic fuel, rocket propulsion, has injecting unit injecting fuel into combustion chamber, where non-conductive layer is arranged on external area of conductive layer of unit |
| 11/07/2007 | CN100347433C Unitized hybrid rocket system |
| 11/07/2007 | CN100346959C Production of thermal protection coatings on propulsion structures |
| 10/30/2007 | US7287369 Method for extending a nozzle and extended nozzle for rocket drives |
| 10/25/2007 | WO2007118453A1 Apparatus and method for determining the fuel mass in a spacecraft |
| 10/24/2007 | EP1053394B1 Method for energy fuel conversion systems |
| 10/24/2007 | CN200964906Y Terminal guided fodder impulse correction engine |
| 10/24/2007 | CN101059097A Ring-shape cylinder piston wheel engine |
| 10/23/2007 | CA1341559C Thermal lining for jet engine combustion chamber |
| 10/18/2007 | WO2007001427A3 Universal carnot propulsion systems for turbo rocketry |
| 10/17/2007 | EP1163152B1 Payload carry and launch system |
| 10/17/2007 | CN101054932A Nuclear power engine and aerocraft produced thereby and spacecraft |