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)
01/2004
01/06/2004US6672756 Fluid mixer
01/02/2004EP1373386A2 Fiber-reinforced rocket motor insulation
12/2003
12/30/2003US6668543 Rocket propulsion unit with separation of inner and outer casing and method of making same
12/18/2003US20030230071 Wall structure
12/17/2003EP1370707A1 Chemical vapour infiltration method for densifying porous substrates having a central passage
12/11/2003DE3346452C1 Inhibiting silicone elastomer coating for homogeneous block of propellant, especially rocket propellant, containing hydroxyl-terminated polydiorganosiloxane and (poly)alkyl silicate, also contains aminoorganosiloxane
12/10/2003EP1369638A2 Vessel for fluid under pressure comprising two chambers and process of manufacturing of such a vessel
12/10/2003EP1368611A1 Dissolvable thrust vector control vane
12/09/2003US6658863 Airborne gas storage and supply system
12/09/2003US6658838 Shaped charge engine
12/04/2003WO2003100243A1 Wall structure
12/04/2003WO2003047969A3 System and method for controlling a space-borne propulsion system
12/04/2003WO2002103199A9 Method and apparatus for ignition detection
12/04/2003US20030221412 Dual chamber pump and method
12/03/2003EP1367251A1 Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system
12/02/2003US6655127 Pre-burner for low temperature turbine applications
11/2003
11/27/2003US20030220417 Comprising solid filler powder, silica, carbon fibers or aramid fibers, providing adhesion, storage stability, shelf life
11/27/2003US20030217552 Engine with a central spike for a space launcher
11/27/2003US20030217547 Side thruster valve and side thruster device
11/26/2003EP1365138A1 Plug nozzle with a foldable inner cone
11/25/2003US6652248 Used in a rocket propulsion system.
11/25/2003US6651438 Rocket nozzle assembly having rotatable variable thrust control cylinders, and rocket assembly comprising the same
11/20/2003WO2002101221A3 A method and apparatus for the preparation and usage of a cryogenic propellant or explosive system
11/20/2003US20030213228 Rocket motor assembly and method for making same
11/18/2003US6648275 Asonic aerospike engine
11/13/2003WO2003092946A1 Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers
11/13/2003WO2003024797A3 Propellant utilization system
11/13/2003US20030209589 Method of forming a channel on the surface of a metal substrate, and related articles
11/13/2003US20030209005 Wick injection of liquids for colloidal propulsion
11/11/2003US6644016 Process and device for collecting air, and engine associated therewith
11/11/2003US6644015 Turbojet with precompressor injected oxidizer
11/06/2003WO2003057561A3 Variably angled propulsion/steering system
11/04/2003US6640538 Combustion chamber cooling structure for a rocket engine
11/04/2003US6640536 Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
10/2003
10/30/2003US20030200656 Insulation lining; heat shield of viscose rayon; impregnating resin matrix, reinforcement, carbonization
10/29/2003EP1357282A2 Rocket engine with internal chamber step structure
10/29/2003EP1356258A1 Pressure sensor and rocket engine incorporating same
10/28/2003US6637188 Rocket engine combustion chamber with enhanced heat transfer to cooling jacket
10/23/2003WO2002079307A3 Fiber-reinforced rocket motor insulation
10/23/2003US20030196705 Variable-gravity anti-vortex and vapor-ingestion-suppression device
10/22/2003CN1451020A Method of insulating a case of a solod propellant rocket motor
10/16/2003WO2003084899A1 Protection against oxidation of parts made of composite material
10/16/2003US20030194574 Protecting composite material parts against oxidation
10/16/2003US20030192998 Solar propulsion assist
10/16/2003US20030192997 Versatile cavity actuator and systems incorporating same
10/16/2003US20030192301 Pre-burner for low temperature turbine applications
10/15/2003EP1352170A1 Rocket engine member and a method for manufacturing a rocket engine member
10/15/2003EP1352169A1 Rocket engine member and a method for manufacturing a rocket engine member
10/15/2003EP1352168A1 Rocket engine member and method for manufacturing a rocket engine member
10/15/2003EP1352167A1 Method for manufacturing outlet nozzles for rocket engines
10/15/2003EP1352166A1 An outlet nozzle and a method for manufacturing an outlet nozzle
10/14/2003US6631610 Consumable port cover for ducted integral rocket-ramjet engine
10/07/2003US6631314 Propellant utilization system
10/07/2003US6629416 Afterburning aerospike rocket nozzle
10/02/2003US20030183606 Method for manufacturing outlet nozzles for rocket engines
09/2003
09/25/2003WO2003078818A1 Solar-heated rocket engine and the operating method thereof
09/25/2003US20030177757 Propellant supply device
09/24/2003EP1346915A2 Propellant supply device
09/24/2003EP1173668B1 Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines
09/18/2003US20030175453 Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same
09/18/2003US20030172659 Method and system for densifying cryogenic propellants
09/17/2003CN1121550C Modular solid fuel rocket propelling charges with casing, fill drain system, cooling device and suspension
09/16/2003US6619031 Multi-mode multi-propellant liquid rocket engine
09/16/2003US6619029 Rocket motors with insensitive munitions systems
09/12/2003WO2003074859A1 Rocket engine
09/12/2003WO2003074858A2 Ramjet engine combustion chamber and ramjet engine equipped with same
09/12/2003WO2003016849A3 Method and apparatus for testing engines
09/10/2003EP1342981A2 Gun-launched rocket
09/10/2003EP1342905A1 Rocket motor
09/10/2003EP1342904A1 Combustion chamber for a ram-jet and ram-jet with such a combustion chamber
09/10/2003EP1264100A4 Shaped charge engine
09/04/2003US20030163986 Pressure-actuated joint system
09/03/2003EP1339654A1 Pyrotechnic charge structure
09/03/2003CN1120113C Payload carry and launch system
08/2003
08/27/2003EP1337750A1 Method and device for a multiple step rocket
08/27/2003CN1119629C Weighing charging element
08/27/2003CN1119522C Rocket assembly ablative materials formed from, as precursor, staple cellulose fibers, and method of insulating or thermal protecting rocket assembly with same
08/19/2003US6606853 Rocket propulsion system
08/19/2003US6606852 Rocket motor insulation containing hydrophobic particles
08/19/2003US6606851 Transpiration cooling of rocket engines
08/14/2003US20030152878 Streamlined body and combustion apparatus
08/13/2003CN2566005Y Air-bleed valve for combustion engine gas generator
08/07/2003WO2003064841A1 Pulse detonation engine and method for initiating detonations
08/06/2003EP1153214B1 Device for supplying fuel for a rocket propulsion unit and heat exchanger to be used in said device
08/05/2003US6601380 Hybrid rocket engine and method of propelling a rocket
07/2003
07/30/2003EP1101030B1 Compact and adjustable tailpipe for piloting aerospace craft
07/29/2003US6598385 Two stage gas pilot valve controlling gas flow to a reaction jet nozzle
07/24/2003US20030136128 Nozzle extension
07/24/2003US20030136111 Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
07/24/2003US20030136110 Flame holder for a hybrid rocket motor
07/24/2003US20030136109 Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
07/24/2003US20030136107 Hybrid rocket motor having a precombustion chamber
07/23/2003EP1144836B1 Combustion chamber cooling structure for a rocket engine
07/23/2003EP1105636B1 Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the same
07/17/2003WO2003058049A2 Apparatus and method for passive venting of rocket motor or ordnance case
07/17/2003WO2003057561A2 Variably angled propulsion/steering system
07/16/2003EP1144835B1 Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same
07/15/2003US6591867 Variable-gravity anti-vortex and vapor-ingestion-suppression device
07/15/2003US6591603 Pintle injector rocket with expansion-deflection nozzle
07/15/2003US6591602 Ejection seat rocket motors
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