| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 08/30/2001 | US20010017183 Rocket engine thrust chamber assembly |
| 08/28/2001 | US6279872 Quick-acting valve |
| 08/28/2001 | US6279812 Method for producing rotational-symmetrical articles of sheet metal with double curved surface and varying thickness of material |
| 08/23/2001 | US20010015063 Liquid fuel rocket engine with a closed flow cycle |
| 08/22/2001 | EP1126233A2 Multiple pulse cartridge ignition system |
| 08/21/2001 | US6276125 Pressure balanced poppet valve |
| 08/14/2001 | US6272847 Centrifugal direct injection engine |
| 08/14/2001 | US6272845 Acoustic igniter and ignition method for propellant liquid rocket engine |
| 08/09/2001 | WO2001056880A1 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 |
| 08/09/2001 | US20010011715 Coaxial valve with electric actuating drive |
| 08/08/2001 | EP1121336A2 Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate |
| 08/07/2001 | US6269647 Rotor system |
| 08/07/2001 | US6269630 Rocket engine with internal chamber step structure |
| 08/02/2001 | WO2001054981A2 Propulsion module |
| 07/31/2001 | US6267330 Liquid oxygen downcomer |
| 07/26/2001 | WO2001053683A1 Rocket motor nozzle assembly comprising a refractory metal shell |
| 07/26/2001 | WO2000079167A9 Slip joint duct system |
| 07/25/2001 | EP1117918A1 Method for manufacturing outlet nozzles for rocket engines |
| 07/24/2001 | US6265330 Glass fiber fabric; and resin composition coated onto said glass fiber fabric, said resin composition consists of (i) a phenolic resin, (ii) an acrylonitrile-butadiene acrylic acid terpolymer, and (iii) alumina trihydrate. |
| 07/24/2001 | US6264145 Geostationary earth observation satellite incorporating multiple thruster liquid propellant apogee maneuver system |
| 07/24/2001 | US6263665 Microthruster for heating a propellant, driving the vapors produced to a discharge section |
| 07/19/2001 | DE10054774A1 Production of a porous blank used in powder metallurgy to produce components for combustion chambers for liquid-fueled rocket engines comprises using granules having defined maximum and minimum diameters |
| 07/18/2001 | EP0932807A4 Design for a gun-launched rocket |
| 07/17/2001 | US6261432 Process for the production of an object with a hollow space |
| 07/05/2001 | DE19960330A1 Pipe valve for aggressive fluid pipelines has valve sleeve forming sliding valve closure actuated by electric motor |
| 07/04/2001 | CN1302353A Modular solid fuel rocket propelling charges with a casing, a fill-drain syctem, cooling and suspension |
| 07/03/2001 | US6254705 Liquid propellant |
| 07/03/2001 | US6253539 Convective and turbulent shear mixing injector |
| 06/28/2001 | WO2001046581A2 System and method for feeding at least a booster motor, and electrically-driven feed pump with high frequency variable reluctance actuator |
| 06/28/2001 | WO2001046279A1 Method of insulating a case of a solid propellant rocket motor |
| 06/28/2001 | WO2000079167A3 Slip joint duct system |
| 06/28/2001 | DE19958310A1 Raketentriebwerk für Flüssigtreibstoffe mit einem geschlossenen Triebwerkskreislauf Rocket engine for liquid fuels with a closed cycle engine |
| 06/26/2001 | US6250602 Positive shut-off metering valve with axial thread drive |
| 06/26/2001 | US6250586 Apparatus and method for controlling the motion of a solid body or fluid stream |
| 06/26/2001 | US6250072 Multi-ignition controllable solid-propellant gas generator |
| 06/26/2001 | US6249967 Fabrication of a rocket engine with a transition structure between the combustion chamber and the injector |
| 06/14/2001 | US20010003244 Rocket engine nozzle |
| 06/13/2001 | EP1105636A1 Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the same |
| 06/12/2001 | US6244041 Liquid-propellant rocket engine chamber and its casing |
| 06/12/2001 | US6244040 Gas generator for liquid propellant rockets |
| 06/12/2001 | CA2114218C The initiation of propellants |
| 06/06/2001 | EP1104390A2 High regression rate hybrid rocket propellants and method of selecting |
| 06/06/2001 | EP0735991B1 Process for operating a reaction-type missile propulsion system and missile propulsion system |
| 05/31/2001 | WO2001038711A1 End-burning rocket motor |
| 05/31/2001 | WO2001038710A1 Nozzleless rocket motor |
| 05/31/2001 | WO2001038170A1 Single-stage-to-orbit rocket |
| 05/31/2001 | US20010001897 Method of forming hollow channels within a component |
| 05/31/2001 | DE10050715A1 Solarwärme-Rakete Solar thermal rocket |
| 05/30/2001 | EP1103714A2 Microthruster with spike nozzle |
| 05/29/2001 | US6237340 Method for reusing a substance's thermal expansion energy |
| 05/24/2001 | US20010001360 Acoustic igniter and ignition method for propellant liquid rocket engine |
| 05/23/2001 | EP1101030A1 Compact and adjustable tailpipe for piloting aerospace craft |
| 05/23/2001 | EP0836700B1 Improved safety in solid fuel rocket motors |
| 05/22/2001 | US6235359 Rocket mmotor with solid propellant, nozzle coupled to casing, insulation from prepreg of resin matrix impregnation with carbonized reinforcement, carding and yarn spun cellulose fibers and insulation |
| 05/22/2001 | US6233919 Force driven hot gas proportional thruster valve |
| 05/15/2001 | US6231008 Method and liquid storage tank for minimizing permeation of liquid vapors through a tank dividing membrane |
| 05/15/2001 | US6230626 Flashless MK 66 rocket motor |
| 05/10/2001 | WO2000063139A3 Family of propellant compositions and method |
| 05/08/2001 | US6228192 Double base propellant containing 5-aminotetrazole |
| 05/08/2001 | US6227486 Propulsion system for earth to orbit vehicle |
| 05/08/2001 | US6227247 Position driven hot gas proportional thruster valve |
| 05/08/2001 | US6226980 Liquid-propellant rocket engine with turbine gas afterburning |
| 05/08/2001 | US6226979 Propellant grain capable of generating buffered boundary layer for reducing rocket nozzle recession |
| 05/03/2001 | WO2001030653A1 Reusable booster for the first stage of a launcher |
| 04/27/2001 | CA2322069A1 Oxidizer package for propellant system for rockets |
| 04/24/2001 | US6220016 Rocket engine cooling system |
| 04/10/2001 | US6214248 Method of forming hollow channels within a component |
| 04/10/2001 | US6213431 Asonic aerospike engine |
| 04/10/2001 | US6212878 Gas generator module |
| 04/10/2001 | US6212876 Simplified high-efficiency propulsion system |
| 04/05/2001 | DE10044624A1 Fuel injection nozzle used in rocket technology has sleeve co-axially encompassing insert and with inner face profiled as cylindrical surfaces with different diameters and lengths, and which form at least one annular confuser |
| 04/03/2001 | US6209312 Rocket motor nozzle assemblies with erosion-resistant liners |
| 04/03/2001 | US6209199 Method of manufacturing a high heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine |
| 03/29/2001 | DE19945974A1 Hybrid rocket engine; has fixed fuel block with sector-shaped hollow spaces to form combustion chamber and central oxidator supply pipe connected to hollow spaces by channels with narrowed openings |
| 03/27/2001 | US6206684 Steam generator injector |
| 03/27/2001 | US6205772 Extendable divergent tail pipe propulsion unit |
| 03/27/2001 | US6205770 Rocket engine |
| 03/27/2001 | US6205661 Method of making a rocket thrust chamber |
| 03/20/2001 | US6202671 Control valve for cryogenic liquid propellant |
| 03/20/2001 | US6202405 Wall construction for a combustion chamber or a nozzle of a high performance propulsion plant |
| 03/15/2001 | DE10037776A1 Combustion chamber for a liquid fuel rocket motor has a porous section at the chamber wall with structured permeability towards the front plate for a transpirant cooling action |
| 03/14/2001 | EP1082213A1 Non-asbestos insulation for rocket motor casing |
| 03/13/2001 | US6199370 Acoustic igniter and ignition method for propellant liquid rocket engine |
| 03/07/2001 | EP1081115A1 Method and apparatus for manufacturing ceramic-based composite member |
| 03/07/2001 | EP1080302A1 Modular solid-fuel rocket propelling charges with a casing, a fill-drain system, cooling and suspension |
| 03/06/2001 | US6195984 Rocket engine thrust chamber assembly |
| 03/01/2001 | WO2001014705A1 Igniters for gas generators |
| 03/01/2001 | WO2000071880B1 Simplified high-efficiency propulsion system |
| 02/27/2001 | US6193187 Payload carry and launch system |
| 02/22/2001 | WO2001012971A1 Liquid propellant rocket engine (lpre) using liquid propellant with closed circuit drive of turbopump apparatus |
| 02/20/2001 | US6189315 Low-cost gas generator and ignitor |
| 02/13/2001 | US6185927 Liquid tripropellant rocket engine coaxial injector |
| 02/06/2001 | US6182442 Combustion chamber wall construction for high power engines and thrust nozzles |
| 02/01/2001 | WO2001007773A1 Hydrogen peroxide based propulsion system |
| 02/01/2001 | WO2001007772A1 Hydrogen peroxide based propulsion system |
| 01/30/2001 | US6178739 Monopropellant assisted solid rocket engine |
| 01/23/2001 | US6176077 Rocket engine nozzle |
| 01/18/2001 | WO2001004198A1 Rocket motor insulation containing hydrophobic particles |
| 01/18/2001 | WO2000071880A3 Simplified high-efficiency propulsion system |
| 01/18/2001 | WO2000057048A3 Rocket engine |