Patents
Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
06/2004
06/08/2004US6745466 Method of making a thruster device for solar radiation
06/03/2004US20040103640 Outlet nozzle and a method for manufacturing an outlet nozzle
06/03/2004US20040103639 Rocket engine member and a method for manufacturing a rocket engine member
06/03/2004US20040103638 Rocket engine member and method for manufacturing a rocket engine member
05/2004
05/27/2004WO2004043691A1 Extremely strain tolerant thermal protection coating and related method and apparatus thereof
05/26/2004EP1422018A1 Rocket engine combustion chamber having multiple conformal throat supports
05/26/2004EP0932807B1 Design for a gun-launched rocket
05/25/2004US6740408 Protecting composite material parts against oxidation
05/25/2004US6739121 Flame holder for a hybrid rocket motor
05/20/2004US20040094341 Hybrid electric vehicle using micro-thrust engines
05/20/2004US20040093852 Rocket engine combustion chamber having multiple conformal throat supports
05/18/2004US6736069 Method for generating energy by using exothermic reaction of metal
05/13/2004US20040089074 Pressure sensor and rocket engine incoporating same
05/11/2004US6734331 Process for producing olefins and diolefins
05/06/2004WO2004038208A2 Method and apparatus for thrust vectoring a flight vehicle using a multi-pulse rocket motor
05/06/2004WO2002079307A9 Fiber-reinforced rocket motor insulation
05/06/2004US20040084566 Multi-nozzle grid missile propulsion system
05/06/2004US20040084564 Low mass flow reaction jet
05/06/2004DE10346836A1 Kaltgesprühtes Kupfer für Raketentriebwerk-Anwendungen Kaltgesprühtes copper for rocket engine applications
04/2004
04/29/2004US20040081783 Laminar structures having variable angle tape wrap and method of forming same
04/29/2004US20040079072 Method and apparatus for thrust augmentation for rocket nozzles
04/28/2004EP1413738A2 Rocket
04/28/2004EP1412631A1 Method for extending a nozzle and extended nozzle for rocket drives
04/28/2004EP0871582B1 Apparatus and method for controlling the motion of a fluid medium
04/27/2004US6726154 Reusable space access launch vehicle system
04/22/2004DE10245741A1 Jet nozzle for solid fuelled rocket has reinforcing fastened on inner contour of nozzle structure and consists of fiber material with fibers orientated in circumferential direction
04/21/2004EP1411318A1 Pneumatic apparatus for increasing the safety and for reducing the vulnerability of munitions
04/21/2004CN1146510C Method for recharging batteries of hybrid electric vehicle in regeneration peroid
04/20/2004US6723972 Method and apparatus for planar actuation of a flared surface to control a vehicle
04/20/2004US6723382 Polymer impregnation and pyrolysis
04/20/2004US6723381 Organic silicon polymer is infiltrated and charged into gaps in a matrix phase of a formed fiber fabric of silicon carbide
04/18/2004CA2444917A1 Cold sprayed copper for rocket engine applications
04/15/2004US20040071877 Chemical vapour infiltration method for densifying porous substrates having a central passage
04/15/2004US20040068979 Ignition systems for hybrid and solid rocket motors
04/15/2004US20040068976 Hybrid rocket engine and method of propelling a rocket
04/15/2004DE10246201A1 Rocket propulsion unit for operation at high reaction temperatures, introduces dust particles into reaction plasma to reduce thermal conduction to walls
04/14/2004EP1407130A1 Jet engine using exhaust gas
04/08/2004US20040065075 Ultraviolet light curable rocket motor liner
04/07/2004EP0988446B1 Device for anchoring a member activating an adjustable nozzle
04/07/2004CN1487186A Commercial carrier rocket with oxyhydrogen rocket enjine
04/07/2004CN1486904A Miniature integral cold air propeller
04/01/2004WO2003074858A3 Ramjet engine combustion chamber and ramjet engine equipped with same
04/01/2004US20040061028 Method of operating a satellite for end-of-life maneuvers
03/2004
03/31/2004EP1402166A1 Rocket vehicle thrust augmentation within divergent section of nozzle
03/30/2004US6712319 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 of refining it
03/30/2004US6711901 Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same
03/30/2004US6711890 Pressure-actuated joint system
03/25/2004US20040057881 Apparatus and method for initiating a combustion reaction with slurry fuel
03/25/2004US20040055642 Cryogenic rotary coupling, and use thereof in particular in articulated fluid feed lines, and in cryogenic propellant rocket engines
03/25/2004US20040055277 Hybrid rocket motor having a precombustion chamber
03/25/2004US20040055274 Hybrid rocket motor having a precombustion chamber
03/18/2004US20040050282 Rocket motors with insensitive munitions systems and projectiles including same
03/18/2004US20040050061 Compact swirl augmented afterburners for gas turbine engines
03/16/2004US6705076 Rocket thrust chamber
03/16/2004US6705075 Digital solid rocket motor and gas generator
03/11/2004US20040045276 Thruster device responsive to solar radiation and associated methods
03/10/2004EP1396631A2 Liquid rocket engine and rocket comprising said engine
03/09/2004US6701705 Gas-walled rocket nozzle
03/04/2004DE10052422B4 Modulares Raketentriebwerk Modular rocket engine
03/03/2004EP1242484B1 Method of insulating a case of a solid propellant rocket motor
03/03/2004EP1163152A4 Payload carry and launch system
03/03/2004EP0963515B1 Acoustic igniter and ignition method for propellant liquid rocket engine
03/02/2004US6698693 Solar propulsion assist
03/02/2004US6698184 Thrust chamber assembly
02/2004
02/26/2004US20040035982 System and method for controlling a space-borne propulsion system
02/26/2004US20040035312 Pyrotechnic charge structure
02/26/2004DE10237381A1 Brennkammerstruktur und Verfahren zu deren Herstellung Combustion chamber structure and process for their preparation
02/25/2004EP1391604A2 Combustion chamber structure and his manufacturing method
02/25/2004EP1391385A1 Cryogenic assembly for rocket or launch vehicle such as a tank structure equipped with at least one equipment-holding device
02/19/2004WO2003092946B1 Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers
02/19/2004DE10255356A1 Reliable ramjet drive ignition device regulation has valve chamber between gas generator, combustion chamber, valve control elements in drive chamber connected to cold end of gas generator chamber
02/19/2004DE10249191B3 Jet propulsion system for motor vehicles and agricultural machines has gas acceleration device to generate esp. compressed air, with acceleration turbine, gas guide channel, and gas collection tube, and gas re-circulation device
02/19/2004DE10235645A1 Device for reliable ramjet ignition and control has regulating valve, variable valve opening, ignition/safety devices in valve chamber tested and controlled/regulated by elements in drive chamber
02/18/2004EP1162139B1 Reusable booster for the first stage of a launcher
02/17/2004US6691948 High torque rocket nozzle
02/17/2004US6691505 Fiber-reinforced rocket motor insulation
02/17/2004US6691504 Gaseous-fuel breathing rocket engine
02/12/2004US20040026572 Dual-mode airbreathing propulsion system
02/12/2004US20040025939 Missile thrust system and valve with refractory piston cylinder
02/10/2004US6688100 Combustion chamber having a multiple-piece liner and associated assembly method
02/10/2004CA2049164C Thermal protection device for the inside surface of a hollow structure to be exposed to ablation and method for the production thereof
02/05/2004US20040020187 Blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet
02/03/2004US6685141 X33 aeroshell and bell nozzle rocket engine launch vehicle
02/03/2004US6684625 Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
02/03/2004US6684624 High regression rate hybrid rocket propellants
01/2004
01/28/2004EP0852060B1 Electromagnetic linear actuator having movable plates and a fluid flow controller with valves controlled by said actuator
01/22/2004WO2004006999A1 Device for intradermal and subcutaneous injection
01/22/2004US20040011023 Combustion chamber having a multiple-piece liner and associated assembly method
01/22/2004US20040010900 Method for forming a tube-walled article
01/22/2004DE10331540A1 Kryotechnische Drehverbindungsanordnung Cryogenic joint assembly
01/22/2004DE10230231A1 Mehrschichtiger Verbundwerkstoff The multi-layered composite material
01/21/2004EP1382403A1 Method for forming a tube-walled article
01/20/2004US6679049 Hybrid rocket motor having a precombustion chamber
01/20/2004US6679048 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
01/15/2004WO2004005690A1 Swivelling nozzle for a rocket engine
01/15/2004WO2003058049A3 Apparatus and method for passive venting of rocket motor or ordnance case
01/13/2004US6675571 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines
01/07/2004EP1378652A2 Multi-layer sandwich material
01/07/2004EP1378583A1 Method of forming a hollow channel on the surface of a metal substrate, and related articles
01/06/2004US6673449 Net molded tantalum carbide rocket nozzle throat and method of making
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