| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 02/11/2003 | US6516604 Micro-colloid thruster system |
| 02/03/2003 | CA2354658A1 Hydrogen combustion robotic propulsion engine |
| 01/30/2003 | US20030021974 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
| 01/30/2003 | US20030019977 Propellant utilization system |
| 01/28/2003 | US6510694 Net molded tantalum carbide rocket nozzle throat |
| 01/23/2003 | US20030015594 Electrostatic atomizers |
| 01/23/2003 | US20030014965 System for reducing pump cavitation |
| 01/22/2003 | EP1277716A1 Method for fabricating ceramic matrix composite |
| 01/16/2003 | WO2003004852A1 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 01/16/2003 | US20030010015 Method and apparatus for ignition detection |
| 01/15/2003 | EP1275837A2 Actuator apparatus including a marker device |
| 01/15/2003 | EP0956441B1 Unfolding injector tube for propulsion unit |
| 01/14/2003 | US6505463 Pre-burner operating method for rocket turbopump |
| 01/09/2003 | US20030008067 Method for fabricating ceramic matrix composite |
| 01/09/2003 | US20030005708 Airborne gas storage and supply system |
| 01/09/2003 | US20030005701 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 01/07/2003 | US6502385 Tricoaxial injection element |
| 01/07/2003 | US6502384 Side thruster of flying object |
| 01/02/2003 | US20030000200 Gas generator for producing adjustable flow |
| 01/02/2003 | EP1162139A4 Reusable booster for the first stage of a launcher |
| 12/31/2002 | US6499696 Rocket engine with reduced thrust and stagable venting system |
| 12/31/2002 | US6499289 Pyrolytic graphite gauge for measuring heat flux |
| 12/31/2002 | US6499288 Pressurizer for a rocket engine |
| 12/31/2002 | US6499287 Integrated tankage for propulsion vehicles and the like |
| 12/27/2002 | WO2002103199A2 Method and apparatus for ignition detection |
| 12/24/2002 | US6497091 Hypergolic ignitor assembly |
| 12/19/2002 | WO2002101221A2 A method and apparatus for the preparation and usage of a cryogenic propellant or explosive system |
| 12/19/2002 | US20020193524 High strength rubber formulations, and shear ply made from the same |
| 12/19/2002 | US20020189233 Fiber-reinforced rocket motor insulation |
| 12/17/2002 | US6494402 Lateral exhaust microthruster |
| 12/17/2002 | US6494035 Towing rocket motor assembly |
| 12/12/2002 | US20020184875 Pressurizer for a rocket engine |
| 12/12/2002 | US20020184872 Hypergolic ignitor assembly |
| 12/12/2002 | DE10126926A1 Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung Combustion chamber with inner shell made from a ceramic composite material and method for producing |
| 12/12/2002 | DE10126923A1 Raketentriebwerk mit Trennung von Innenmantel und Außenmantel Rocket engine with separation of inner shell and outer shell |
| 12/11/2002 | EP1264100A1 Shaped charge engine |
| 12/11/2002 | EP1034063B1 A method for producing rotational-symmetrical articles of sheet metal with double curved surface and varying thickness of material |
| 12/11/2002 | CN1095720C Method for production of rocket nozzle |
| 12/05/2002 | US20020178712 Rocket propulsion unit with separation of inner and outer casing and method of making same |
| 12/05/2002 | DE10123957A1 To form a joint, resistant to high forces, the joint sections are prepared with matching tongues and spaces between them, to be locked together and held by a bolt. |
| 12/04/2002 | EP1261518A1 Method and apparatus for placing satellites in low earth orbit |
| 12/04/2002 | CN1383469A Rocket assembly ablative materials formed from solvent-spun cellulosic precursorc, and method of insulating or thermally protecting rocket assembly with same |
| 12/03/2002 | US6488237 Propellant cross-feed system and method |
| 12/03/2002 | US6488233 Laser propelled vehicle |
| 12/03/2002 | US6487844 Aerospike augmentation of microthruster impulse |
| 11/28/2002 | DE10123731A1 Rocket drive has an extending secondary zone which can be extended at a given flight height to lengthen the primary jet contour zone, according to ambient pressure conditions |
| 11/27/2002 | EP0870105B1 Extendable divergent tail pipe for propulsion unit |
| 11/21/2002 | WO2002092988A1 Method for extending a nozzle and extended nozzle for rocket drives |
| 11/21/2002 | US20020170285 Slip joint duct system |
| 11/21/2002 | US20020170284 Thruster device responsive to solar radiation and associated methods |
| 11/19/2002 | US6483368 Addressable diode isolated thin film cell array |
| 11/19/2002 | US6482485 Structural part including a portion made of thermostructural composite material cooled by fluid circulation |
| 11/19/2002 | US6481198 Multi-stage rocket motor assembly including jettisonable launch motor integrated with flight igniter |
| 11/14/2002 | US20020166922 Lateral exhaust microthruster |
| 11/13/2002 | EP0880645B1 Rocket engine nozzle |
| 11/12/2002 | US6479148 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |
| 11/07/2002 | DE10206701A1 Oxyhydrogen power plant has primary fuel tank containing hydrogen in a chemical bond with another substance and expelled by heat |
| 11/05/2002 | US6474573 Electrostatic atomizers |
| 10/31/2002 | US20020157557 Propellant system for solid fuel rocket |
| 10/31/2002 | US20020157399 Rocket engine nozzle comprising a jet separation control system |
| 10/31/2002 | DE19822845C2 Modulare Feststoffraketentreibsätze mit Ummantelung, Fill-drain System, Kühlung und Aufhängung Modular solid rocket propellants with shell, fill-drain system, cooling and suspension |
| 10/30/2002 | EP1200726A4 Erosion resistant rocket nozzle |
| 10/29/2002 | US6470671 Coolable nozzle and method for producing such a nozzle for a rocket engine |
| 10/29/2002 | US6470670 Liquid fuel rocket engine with a closed flow cycle |
| 10/29/2002 | US6470669 Hybrid injection thrust vector control |
| 10/24/2002 | US20020152752 Apparatus for controlling the flow separation line of rocket nozzles |
| 10/24/2002 | DE10118005A1 Micro-rocket operating with periodic explosive combustion, includes distributor, combustion chamber, igniter and flame traps in supply lines |
| 10/23/2002 | EP1250526A2 System and method for feeding at least a booster motor, and electrically-driven feed pump with high frequency variable reluctance actuator |
| 10/22/2002 | US6469424 Ignitor for liquid fuel rocket engines |
| 10/22/2002 | US6467253 Nozzle structure for rocket nozzles having cooled nozzle wall |
| 10/17/2002 | WO2000014397A3 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |
| 10/17/2002 | US20020148215 Pre-burner operating method for rocket turbopump |
| 10/17/2002 | EP1144835A3 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |
| 10/16/2002 | EP1248902A1 Rocket motor nozzle assembly comprising a refractory metal shell |
| 10/10/2002 | WO2002079307A2 Fiber-reinforced rocket motor insulation |
| 10/10/2002 | DE10117605A1 Unlocking of air inlet doors in combustion chamber of ramjets takes place through heating up of thermally or pressure sensitive spring components directly produced by combustion of starting propellant or by gas generator |
| 10/03/2002 | US20020139902 Low-thrust cryogenic propulsion module |
| 10/03/2002 | US20020139901 X33 aeroshell and bell nozzle rocket engine launch vehicle |
| 10/03/2002 | US20020139107 Solar thermal rocket |
| 10/02/2002 | EP1245629A2 High strength rubber formulations, and shear ply made from the same |
| 10/01/2002 | US6457306 Electrical drive system for rocket engine propellant pumps |
| 09/26/2002 | WO2002074622A1 Rocket engine with reduced thrust and stagable venting system |
| 09/26/2002 | WO2002018772A8 Segmented rocket drive and method for producing the same |
| 09/26/2002 | US20020134071 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines |
| 09/25/2002 | EP1243783A1 Pintle injector rocket with expansion-deflection nozzle |
| 09/25/2002 | EP1242484A1 Method of insulating a case of a solid propellant rocket motor |
| 09/24/2002 | US6454216 Reusable booster for the first stage of a launcher |
| 09/24/2002 | US6453937 Hot gas valve construction for reducing thermal shock effects |
| 09/24/2002 | CA2090669C Solid propellant rocket motor case for insensitive munitions requirements |
| 09/19/2002 | WO2002073118A1 Dissolvable thrust vector control vane |
| 09/19/2002 | US20020130216 Dissolvable thrust vector control vane |
| 09/18/2002 | EP1241341A1 Cryotechnic propulsion module |
| 09/17/2002 | US6450443 High torque 2.75-inch rocket nozzle |
| 09/17/2002 | US6450197 Magnetically actuated valve system |
| 09/17/2002 | US6449942 Slip joint duct system |
| 09/12/2002 | WO2002070775A1 Chemical vapour infiltration method for densifying porous substrates having a central passage |
| 09/10/2002 | US6446909 Reciprocating chemical muscle(RCM) and method for using same |
| 09/10/2002 | US6446427 Solid fuel regression rate control method and device |
| 09/05/2002 | US20020121081 Liquid/solid fuel hybrid propellant system for a rocket |
| 09/05/2002 | DE10106772A1 Combustion chamber used for a rocket propulsion system is made from a composite ceramic |