| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
|---|
| 04/06/2010 | US7690192 Compact, high performance swirl combustion rocket engine |
| 04/06/2010 | US7690189 Aircraft combination engines inlet airflow control system |
| 04/06/2010 | US7690188 Combination engines for aircraft |
| 04/01/2010 | WO2010034731A1 Propulsive unit using nanoenergy fuel |
| 04/01/2010 | WO2009080595A3 Combustion chamber device |
| 03/30/2010 | US7685940 Rocket motor with pellet and bulk solid propellants |
| 03/30/2010 | US7685807 Three component injector for kerosene-oxygen rocket engine |
| 03/23/2010 | CA2426351C System for closing the opening of a pipe, particularly the opening of an air inlet into a ramjet combustion chamber |
| 03/18/2010 | US20100064661 Injector head of liquid rocket engine |
| 03/04/2010 | WO2009148625A3 Space station, launch vehicle, and method of assembly |
| 03/04/2010 | WO2009140120A3 Systems, methods and apparatus for propulsion |
| 03/03/2010 | EP2158395A1 Hydroxy amine based staged combustion hybrid rocket motor |
| 02/25/2010 | WO2010001021A3 Process for producing a self-healing layer on a part made of a c/c composite |
| 02/25/2010 | US20100043392 Mixture ratio stabilizer for liquid propellant rocket engine |
| 02/18/2010 | US20100037590 Low velocity injector manifold for hypergolic rocket engine |
| 02/18/2010 | US20100037589 Component configured for being subjected to high thermal load during operation |
| 02/17/2010 | EP2153052A2 Power unit with enhanced performance |
| 02/11/2010 | US20100034616 Fastener assembly for connecting rocket engine nozzles |
| 02/11/2010 | US20100031626 Carbon-Kevlar uni-body rocket engine and method of making same |
| 02/10/2010 | EP2150694A1 Cryotechnic space propulsion device and its control method |
| 02/10/2010 | CN101644210A Combined nozzle fuel gas fluid control valve |
| 02/10/2010 | CN101644209A Straight single-hole fuel gas fluid control valve |
| 02/04/2010 | US20100024388 Flow-Restricting Filter, Solid Propellant Gas Generator and Propulsion System Comprising the Same |
| 02/04/2010 | US20100024386 Gas-Generator Augmented Expander Cycle Rocket Engine |
| 01/28/2010 | WO2009134499A3 Pellet loaded attitude control rocket motor |
| 01/27/2010 | EP2148073A2 Ramjet engine with a melting layer applied on the exhaust duct |
| 01/26/2010 | CA2466222C Streamlined body and combustion apparatus having such a streamlined body |
| 01/21/2010 | WO2010007308A1 Method of producing a nozzle or a divergent nozzle element made of a composite |
| 01/21/2010 | WO2009134510A3 Rocket motor with pellet and bulk solid propellants |
| 01/21/2010 | US20100011742 Rocket Motor Containing Multiple Pellet Cells |
| 01/21/2010 | DE102008033429A1 Feststofftriebwerk Solid engine |
| 01/19/2010 | US7647763 Polyoxymethylene as structural support member and propellant |
| 01/14/2010 | WO2010004232A1 Thruster comprising a plurality of rocket motors |
| 01/14/2010 | US20100006677 Device for injecting mono-propellant at a flow rate that can be modulated with an injection speed that is stable |
| 01/14/2010 | US20100005807 Liquid propellant rocket engine with a propulsion chamber shutter |
| 01/14/2010 | US20100005779 Device for injecting a mono-propellant with a large amount of flow rate modulation |
| 01/13/2010 | EP2143929A1 Monoprollant injection device with flow modulation and stable injection speed |
| 01/13/2010 | EP2143928A1 Device for injecting monopropellant with high flow modulation |
| 01/13/2010 | EP2143927A1 Liquid-propellant rocket engine with propulsion chamber blanking plug |
| 01/13/2010 | EP2142788A2 Method and device for supplying a space propulsion engine with liquid cryogenic propellants |
| 01/07/2010 | WO2010001021A2 Process for producing a self-healing layer on a part made of a c/c composite |
| 01/05/2010 | US7640726 Injector assembly having multiple manifolds for propellant delivery |
| 12/31/2009 | US20090320974 Polyoxymethylene as structural support member and propellant |
| 12/31/2009 | US20090320447 Coaxial ignition assembly |
| 12/30/2009 | WO2009156062A1 Container for receiving, storing and dispensing liquids and viscous substances, in particular drinking water or fuel, and the use thereof |
| 12/30/2009 | EP2138698A1 Device for absorbing the lateral take-off forces of a jet acting on the nozzle of a rocket engine |
| 12/30/2009 | EP2137395A2 Rocket engine laval nozzle |
| 12/24/2009 | US20090313967 Polyoxymethylene as structural support member and propellant |
| 12/24/2009 | DE102008029150A1 Gasgenerator Gas generator |
| 12/23/2009 | EP2136064A2 Gas generator |
| 12/17/2009 | WO2009150069A2 Combustion chamber device, and method for the operation of a combustion chamber device |
| 12/17/2009 | DE112008000323T5 Durch aktives Material betätigtes Luftklappensystem Active material actuated louver system |
| 12/16/2009 | EP2132429A2 Electrolytic igniter for rocket engines using monopropellants |
| 12/16/2009 | EP2132428A2 Electrolytic igniter for rocket engines using liquid propellants |
| 12/16/2009 | CN100570147C Laminated board sweat cooling structure by strong endothermic reaction |
| 12/10/2009 | WO2009148625A2 Space station, launch vehicle, and method of assembly |
| 12/10/2009 | DE10346836C5 Verfahren zum Aufbringen eines Beschichtungsmaterials und Herstellungsverfahren einer Raketentriebwerk-Verteilereinrichtung mit einer Kupferauflage A method for applying a coating material and method of manufacturing a rocket engine-distributing device having a copper layer |
| 12/10/2009 | DE102008022289A1 Flugkörper Missile |
| 12/08/2009 | US7628006 Thrust termination device for solid rocket motor |
| 11/25/2009 | EP2122148A1 A component configured for being subjected to high thermal load during operation |
| 11/24/2009 | US7621119 Heat exchange injector for use in a rocket engine |
| 11/24/2009 | US7621116 Gas turbine engine system |
| 11/19/2009 | WO2009140120A2 Systems, methods and apparatus for propulsion |
| 11/18/2009 | CN201347816Y Novel valve sealing structure |
| 11/18/2009 | CN101581261A Trust-deflecting nozzle |
| 11/11/2009 | CN101576026A Rocket engine nozzle system |
| 11/11/2009 | CN101576024A Heat returning closed cooling recirculation system of Brighton scramjet |
| 11/10/2009 | US7614816 Device for preventing ball and socket joint from rolling |
| 11/05/2009 | WO2009134510A2 Rocket motor with pellet and bulk solid propellants |
| 11/05/2009 | WO2009134499A2 Pellet loaded attitude control rocket motor |
| 10/29/2009 | WO2009130226A1 Flying object |
| 10/29/2009 | US20090269497 Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications |
| 10/29/2009 | US20090266049 Methods and systems for propelling a vehicle |
| 10/20/2009 | US7603843 Combustion chamber comprising a cooling unit and method for producing said combustion chamber |
| 10/15/2009 | WO2009061586A3 In situ optical probe and methods |
| 10/14/2009 | CN201326477Y Two-control-in-one-position pneumatic pilot-valve used in gelled-propellant supply system |
| 10/14/2009 | CN101556129A Rocket |
| 10/14/2009 | CN100549399C High-frequency pulse pinking engine and control method thereof |
| 10/13/2009 | US7603207 Surrogate air processor |
| 10/07/2009 | CN100547237C Plasma recombination boosting turbine fan jet aerial engine |
| 10/06/2009 | US7597273 Speed control apparatus for a rotary sprinkler |
| 10/06/2009 | US7596940 Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing |
| 10/01/2009 | US20090241511 Heat exchange injector for use in a rocket engine |
| 09/30/2009 | EP2105600A1 Pyrotechnical propulsion method and devices with thrust modulation, spacecraft comprising such a device |
| 09/30/2009 | CN101545416A Solid rocket engine |
| 09/30/2009 | CN101545415A Vortex punching jetting engine |
| 09/24/2009 | US20090235640 Pellet Loaded Attitude Control Rocket Motor |
| 09/24/2009 | US20090235639 Rocket nozzle and control method for combustion gas flow in rocket engine |
| 09/24/2009 | US20090235636 Reinforced, regeneratively cooled uni-body rocket engine |
| 09/23/2009 | EP2103799A2 Rocket nozzle and control method for combustion of the exhaust gas flow in rocket engine |
| 09/23/2009 | CN101539074A Rocket nozzle and control method for combustion of the exhaust gas flow in rocket engine |
| 09/23/2009 | CN101539073A Multi-pin micro-Newton colloid thrustor |
| 09/23/2009 | CN101539072A Visual device of filling state of liquid pipeline |
| 09/23/2009 | CN101539071A Propellant filling device of electric arc heating engine supplying pipeline |
| 09/23/2009 | CN101539070A Propellant blowing device in engine pipelines |
| 09/23/2009 | CN101539069A Pressure stability control device supplied with constant voltage by propellant |
| 09/23/2009 | CN101539068A Filling device of liquid propellant and method thereof |
| 09/23/2009 | CN101539067A Hole type micro-Newton colloid thrustor |
| 09/22/2009 | CA2465295C Rocket motors with insensitive munitions systems |
| 09/17/2009 | US20090229245 End burning type gas generator |