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