Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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09/01/1998 | US5799902 Economical launch vehicle |
08/27/1998 | WO1998036975A2 Case for combustible materials and methods for making and using the same |
08/25/1998 | US5797260 Pulse rocket engine |
08/20/1998 | DE19716524C1 Method for producing a component with a cavity |
08/20/1998 | DE19703630C1 Fixing system for injection unit in base plate of rocket motor |
08/19/1998 | EP0859143A1 Single stage regulated bootstrap pressurization system |
08/18/1998 | US5794435 Stable-combustion oxidizer vaporizer for hybrid rockets |
08/11/1998 | US5792981 Gun-launched rocket |
08/11/1998 | CA2024520C Consumable ignitor for solid-fuel rocket motor |
08/04/1998 | US5787702 Propulsion plant operating on the basis of catalytic and/or chemical decomposition of a propellant |
07/28/1998 | US5784877 Rocket-ramjet engine casing port closure |
07/16/1998 | WO1998030518A1 Method and apparatus for total energy fuel conversion systems |
07/14/1998 | US5780729 For a test cell |
07/14/1998 | US5780157 Composite structure |
07/14/1998 | US5779151 Stepped nozzle |
07/08/1998 | EP0852060A1 Electromagnetic linear actuator having movable plates and a fluid flow controller with valves controlled by said actuator |
07/07/1998 | US5775096 Process for operating a reaction-type missile propulsion system and missile propulsion system |
07/07/1998 | US5775094 Apparatus and method for controlling thruster valve |
07/07/1998 | CA2110057C Satellite propulsion and power system |
07/02/1998 | WO1998028533A1 Unfolding injector tube for propulsion unit |
06/30/1998 | US5771579 Convective and shear mixing injector assembly |
06/25/1998 | DE19651646A1 Blowing-in process for two fuel components of rocket engine |
06/23/1998 | US5768885 Regenerative piston liquid propellant rocket motor |
06/17/1998 | CN1184890A Low power arcjet propellant feed system |
06/16/1998 | US5767973 Wheelset sensing system |
06/16/1998 | US5767221 Robust propellant liner and interfacial propellant burn rate control |
06/16/1998 | US5765367 System for controlling a space vehicle by gating gas |
06/16/1998 | US5765361 Hybrid-LO2-LH2 low cost launch vehicle |
06/16/1998 | US5765360 Process for cooling engine walls and wall structure for carrying out the process |
06/10/1998 | EP0680554B1 Turbine engine control system |
06/09/1998 | US5763027 Insensitive munitions composite pressure vessels |
06/09/1998 | US5762746 Forming an insulating material comprises polyphosphazene binder and reinforcing filler such as polybenzimidazole, securing formed material to atleast one portion of combusion chamber |
05/26/1998 | US5756924 Multiple laser pulse ignition method and apparatus |
05/26/1998 | US5755091 Regenerative piston engine for combustion of liquid monopropellant |
05/19/1998 | US5752381 Method and apparatus for vectoring thrust employing electrodes generating voltages greater than the dielectric breakdown voltage |
05/12/1998 | US5749559 Device for controlling a spacecraft by gating gas via a moving nozzle |
05/12/1998 | US5749402 Integrated storage and transfer system and method for spacecraft propulsion systems |
05/07/1998 | WO1998019127A1 Design for a gun-launched rocket |
05/05/1998 | US5746050 Gaseous product delivery system |
04/28/1998 | US5743492 Payload housing and assembly joint for a launch vehicle |
04/22/1998 | EP0836700A1 Improved safety in solid fuel rocket motors |
04/22/1998 | EP0719406B1 Altitude gas turbine engine test cell |
04/15/1998 | EP0836055A1 Seal for combustion chamber tiles |
04/15/1998 | EP0836001A1 Rocket nozzle with ejectable inserts |
04/14/1998 | US5738308 Ion thruster support and positioning system |
04/09/1998 | WO1997048601A3 Method for making a rhenium rocket nozzle |
04/07/1998 | US5735463 Jetavator for rocket engine |
04/07/1998 | US5735114 Thermostatic bimetallic retaining ring for use in rocket motor assembly |
04/01/1998 | EP0832349A2 Synthesised fuel-powered reaction rocket motor |
04/01/1998 | EP0796196A4 Fluidic control thrust vectoring nozzle |
03/31/1998 | US5732883 Combustion enclosure with cooling by transpiration |
03/26/1998 | WO1998012429A1 Controlled temperature rocket nozzle |
03/18/1998 | EP0829637A1 Thruster |
03/18/1998 | EP0828929A2 Reduced pollution power generation system and gas generator therefore |
03/03/1998 | US5722232 Hybrid helium heater pressurization system and electrical ignition system for pressure-fed hybrid rockets |
02/26/1998 | DE19633589A1 Outlet nozzle for reaction motor combustion chamber |
02/24/1998 | US5720451 Resilent to structural failures which allows higher specific impulse |
02/17/1998 | US5718113 Fuel strip |
02/11/1998 | EP0822860A1 Carbides and nitrides of transition elements applied on the catalytic decomposition of hydrazine |
02/11/1998 | CN1173158A Satellite fueling system and method therefor |
02/10/1998 | US5715675 For a projectile launchable from a launch platform |
02/10/1998 | US5715673 Reduced pollution power generation system |
02/04/1998 | EP0822328A2 Throat insert for rocket thrusters |
02/03/1998 | US5714711 Encapsulated propellant grain composition, method of preparation, article fabricated therefrom and method of fabrication |
02/03/1998 | US5714081 Dismountable mechanical core and procedure for implementing it |
01/28/1998 | EP0758283B1 Fabrication of tubular wall thrust chambers for rocket engines using laser powder injection |
01/28/1998 | CN1171545A Weighing charging element |
01/27/1998 | US5711348 Hot gas control valve |
01/22/1998 | WO1998002643A1 Microturbomachinery |
01/20/1998 | US5709077 Reduce pollution hydrocarbon combustion gas generator |
01/13/1998 | US5708229 Gun launch rocket propellant support filler |
01/07/1998 | EP0784781A4 Solid fuel launch vehicle destruction system and method |
01/06/1998 | US5704551 Injection element of coaxial design for rocket combustion engines |
12/30/1997 | US5701670 Method of making rocket engine combustion chamber utilizing "slide in" port liner |
12/24/1997 | WO1997048601A2 Method for making a rhenium rocket nozzle |
12/16/1997 | US5697212 Rocket propellant tank self-pressurization |
12/11/1997 | WO1997047013A1 Micro gas rheostat |
12/11/1997 | WO1997046820A1 Microvalve and microthruster for satellites and methods of making and using the same |
12/11/1997 | DE19623019A1 Engine for use as hydrazine-propelled drive system in space travel |
12/11/1997 | CA2257341A1 Micro gas rheostat |
12/10/1997 | EP0810946A1 Device for pressurising a unified two-liquid propulsion subsystem for geostationary satellites |
12/09/1997 | US5694769 Liquid oxidizer immersion type hybrid rocket |
12/09/1997 | US5694766 Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine engine exhaust nozzle using regions of locally separated flow |
12/04/1997 | DE19719777A1 Device to limit fire hazard within a turbo machine |
12/03/1997 | EP0809783A1 Fire mitigation device |
12/03/1997 | EP0809755A1 Thrust chambers |
11/27/1997 | WO1997044138A1 Electroformed multilayer flow regulator |
11/27/1997 | CA2253674A1 Electroformed multilayer flow regulator incorporating force-generating means for selectively constricting the fluid flow path, and a process for the prearation thereof |
11/20/1997 | DE19625735C1 Injection head for rocket power unit |
11/13/1997 | DE3026245C1 Two position exhaust nozzle for missile rocket motor |
11/05/1997 | EP0804362A1 Satellite fueling system and method therefor |
11/04/1997 | US5683033 Rocket nozzle for a rocket engine |
10/14/1997 | US5675966 Casting second pulse grain in fore insulator, curing, bonding barrier insulator to second pulse grain, bonding aft insulator to barrier insulator, casting first pulse grain in aft insulator, installing ignition means |
10/07/1997 | US5673550 Laser initiated non-linear fuel droplet ignition |
10/01/1997 | EP0798544A2 Load cell |
10/01/1997 | EP0773883A4 Two stage launch vehicle and launch trajectory method |
09/30/1997 | US5671599 Solid-propellant rocket engine with inner and outer burner surfaces |
09/24/1997 | EP0796196A1 Fluidic control thrust vectoring nozzle |
09/04/1997 | WO1997025623A3 Controlling motions of a solid body or fluid stream |
09/02/1997 | US5662290 For controlling a missile in flight |