Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
07/1996
07/10/1996EP0720876A2 Fabrication of rocket chambers
07/09/1996US5533331 Method of igniting fuel fluid in a propulsion system
07/03/1996EP0719935A1 Self pressurizing tank
07/03/1996EP0719406A1 Altitude gas turbine engine test cell
06/1996
06/27/1996DE19542234A1 Duale, konzentrische Tellerventile, um das Verhältnis von zwei Fluidströmungen über einen Betriebsbereich einer Ventilöffnung im wesentlichen konstant zu halten Dual, concentric disc valves, to maintain the ratio of two fluid flows over an operating range of a valve opening is substantially constant
06/25/1996US5529648 Jet engine solid fuel comprising polymeric matrix, free of oxidizer
06/25/1996US5529264 Launch vehicle system
06/20/1996DE19515879C1 Coaxial injection unit for rocket combustion chambers
06/13/1996WO1996007024A3 Reduced pollution power generation system and gas generator therefore
06/11/1996US5524827 Method and nozzle for producing thrust
06/11/1996US5524429 Laser initiated non-linear fuel droplet ignition
05/1996
05/30/1996DE19508830C1 Solid fuel rocket drive mechanism with inner and outer burners
05/29/1996EP0637375A4 Acousto-optic tunable filter-based surface scanning system and process.
05/28/1996US5520356 System for propelling and guiding a solid object with a beam of electromagnetic radiation
05/28/1996US5519991 Increased efficiency arcjet thruster
05/23/1996DE19505357C1 Aero engine or rocket wall cooling method
05/17/1996WO1996014504A1 Discus-shaped aerodynamic vehicle for use at extremely high velocities
05/15/1996DE4439073C1 Diskusförmiger Flugkörper mit einer Strahltriebwerks- und einer Raketentriebwerksanordnung Discus-shaped missiles with a Strahltriebwerks- and a rocket engine assembly
05/07/1996US5513489 Rotary valve multiple combustor pulse detonation engine
05/02/1996WO1996012688A1 Process for operating a reaction-type missile propulsion system and missile propulsion system
04/1996
04/30/1996US5511914 Propellant grain machining device and method
04/30/1996US5511745 Vectorable nozzle having jet vanes
04/25/1996WO1996012155A1 Solid fuel launch vehicle destruction system and method
04/25/1996DE4437524A1 Verfahren zum Betreiben eines nach dem Rückstoßprinzip arbeitenden Antriebes eines Flugkörpers sowie Flugkörperantrieb Method for operating an operating according to the principle of repulsion drive a missile and missile propulsion
04/23/1996US5509517 Clutch assembly
04/23/1996US5509354 For a pyropulsive model rocket engine
04/16/1996US5507231 Solid fuel launch vehicle destruction system and method
04/09/1996US5505408 For missiles
04/04/1996DE19541044A1 Injection system for hybrid rockets with segmented fuel block
04/02/1996US5503079 Linear gas generant and filter structure for gas generator
03/1996
03/27/1996EP0703359A2 Liquid oxidizer immersion type hybrid rocket
03/26/1996US5501011 Method of manufacture of an enclosure containing hot gases cooled by transportation, in particular the thrust chamber of a rocket engine
03/21/1996WO1996008646A1 Solid-fuel, liquid oxidizer hybrid rocket turbopump auxiliary engine
03/19/1996US5499656 Integrated storage and transfer system and method for spacecraft propulsion systems
03/13/1996EP0686135A4 Bore mitigants for solid propellant rocket motors
03/12/1996US5497612 Laser initiated non-linear fuel droplet ignition method
03/07/1996WO1996007024A2 Reduced pollution power generation system and gas generator therefore
02/1996
02/22/1996DE4436112C1 Liquid fuelled propulsion unit
02/21/1996EP0697515A2 Tube-lined rocket thrust chamber construction
02/20/1996US5491973 Self-actuating control for rocket motor nozzle
02/15/1996WO1996004474A1 Slotted hybrid pressure vessel
02/15/1996WO1996004168A1 Two stage launch vehicle and launch trajectory method
02/13/1996US5490629 Rocket engine nozzle with an engine diffuser
01/1996
01/24/1996EP0693632A1 Clutch assembly
01/23/1996US5485721 Arcjet for a space flying body
01/23/1996US5485720 Laser initiated non-linear fuel droplet ignition
01/11/1996DE19524875A1 Combustion chamber for engine with tube construction
01/10/1996CN1114624A Integrated storage and transfer system and method for spacecraft propulsion systems
01/09/1996US5481870 Rocket engine nozzle with selectively smaller outlet cross-section
01/09/1996US5481869 For delivering a liquid propellant to a combustion reactor
01/02/1996US5479959 Integrated storage and transfer system and method for spacecraft propulsion systems
12/1995
12/27/1995EP0688947A1 Injection system for hybrid rocket motor
12/26/1995US5477672 High-temperature, high-pressure gas generation apparatus for turbine drive
12/26/1995US5477613 Method of simultaneously forming rocket thrust chamber cooling tubes
12/26/1995CA2152334A1 Injection system for hybrid rockets
12/14/1995WO1995033620A1 Composite structure
12/13/1995EP0686824A1 Thrust generating device
12/13/1995EP0686135A1 Bore mitigants for solid propellant rocket motors
12/12/1995US5473817 Method of making cooled rocket combustion chamber construction
12/05/1995US5471833 Rocket propellant pressurization system using high vapor pressure liquids
11/1995
11/28/1995US5469701 Fluid storage and expulsion system
11/28/1995US5469700 Turbine engine control system
11/22/1995EP0683312A1 Hybrid rocket motor solid fuel grain
11/21/1995US5467528 Method of making a tubular thermal structure
11/15/1995EP0681647A1 Laser initiated non-linear fuel droplet ignition
11/14/1995US5466537 Intermetallic thermal sensor
11/09/1995WO1995030084A1 Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture
11/09/1995WO1995029785A1 Fabrication of tubular wall thrust chambers for rocket engines using laser powder injection
11/09/1995WO1995026467A3 Bipropellant rocket motor
11/08/1995EP0680554A1 Turbine engine control system
11/02/1995EP0679134A1 Radial four-blade thrust vector-------------------------------.
10/1995
10/12/1995DE4443839C1 Method for prodn. of actively cooled power plant wall
10/10/1995US5456425 Multiple pintle nozzle propulsion control system
10/10/1995US5456065 Injection element of coaxial design for rocket combustion chambers
10/05/1995WO1995026467A2 Bipropellant rocket motor
09/1995
09/28/1995DE4422195C1 Injection system for hybrid rocket propulsion unit
09/28/1995DE19514720A1 Hydrogen@ injection process for solid=fuel rockets
09/19/1995US5450720 Rocket engine nozzle having a notched diverging portion
09/13/1995EP0670776A1 High thermal conductivity non-metallic honeycomb
08/1995
08/31/1995DE19506771A1 Hybrid rocket propulsion unit for military use
08/29/1995US5445469 Sliding joint assembly for two parts subjected to large mechanical and thermal stresses
08/29/1995US5444973 Pressure-fed rocket booster system
08/22/1995US5442910 Reaction motor structure and method of construction
08/16/1995EP0380591B1 Fiber/resin composites, and method of making the same
08/15/1995US5441219 Method for attaching metallic tubing to nonmetallic pressure vessel, and pressure vessel made by the method
08/10/1995EP0681647A4 Laser initiated non-linear fuel droplet ignition.
08/08/1995US5438834 Close combustion gas generator
08/08/1995US5438824 Silicon as a high energy additive for fuel gels and solid fuel-gas generators for propulsion systems
07/1995
07/27/1995DE4418536C1 Propulsion unit, with catalytic and/or thermal decomposition of liquid fuel
07/25/1995US5435128 Pyrotechnically driven nozzle restrictor
07/19/1995EP0663524A1 Scram-stage missile
07/11/1995US5431010 High speed, amplitude variable thrust control method
07/05/1995EP0661436A1 Expandable nozzle mechanism for a rocket engine
06/1995
06/28/1995EP0659860A1 Adhesive elastomeric matrix and its use
06/27/1995US5427507 Valving for controlling a fluid-driven reciprocating apparatus
06/27/1995US5427334 Method for making nonmetallic pressure vessel with integral propellant management vane, and pressure vessel made by the method
06/22/1995DE4343332A1 Convective cooling device for sealed combustion chamber
06/22/1995DE4343009A1 Injector for jet engine with fluid nozzle
06/14/1995EP0657491A1 Improved elastomeric bonding
06/14/1995EP0463025B1 Pyrotechnic materials
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