| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 01/24/2012 | US8099945 Hybrid propulsion system |
| 01/12/2012 | US20120006124 Methods, devices, and systems relating to a sensing device |
| 01/12/2012 | US20120006001 Solid propellant rocket motors employing tungsten alloy burst discs and methods for the manufacture thereof |
| 01/11/2012 | CN202108612U Testing device for researching distribution of jet tube plume condensed phase particles |
| 01/11/2012 | CN101806260B Multitube parallel pulse detonation combustion chamber and ignition detonation method thereof |
| 01/05/2012 | WO2011105897A3 Igniter for a rocket engine, method for ignition of a rocket engine |
| 01/04/2012 | CN102308077A Regeneratively cooled porous media jacket |
| 12/29/2011 | US20110314791 Method for combustion system |
| 12/29/2011 | US20110314790 Hybrid propulsion system |
| 12/28/2011 | EP1771700B1 Stream deflector and method for the production of a stream deflector |
| 12/28/2011 | CN102297042A 低点火阈值吸气式激光推力器 Low ignition threshold aspirated laser thruster |
| 12/21/2011 | CN102292264A 用于发射器的可再利用模块 Reusable module for transmitter |
| 12/21/2011 | CN102288070A 气体延迟反冲方法 Gas delayed recoil method |
| 12/21/2011 | CN101776028B 牵制释放仿真数据源系统 Release contain simulation data source system |
| 12/20/2011 | US8079308 Ramjet engine incorporating a tubular structure and a missile propelled by a ramjet engines of this type |
| 12/14/2011 | CN202073657U 直喷推进器 DI propeller |
| 12/14/2011 | CN102278233A 超音速转子发动机 Supersonic rotary engine |
| 12/07/2011 | EP2391802A1 Jet engine, in particular a jet engine for an aircraft |
| 12/01/2011 | DE102010035911A1 Behälter zum Aufnehmen und Speichern von Flüssigkeiten und viskosen Stoffen, insbesondere von kryogenen Fluiden, und Verfahren zu dessen Herstellung sowie dessen Verwendung Container for receiving and storing liquids and viscous materials, in particular of cryogenic fluids and method for its production and its use |
| 11/30/2011 | EP2390549A2 Container for holding and storing liquids and viscous materials, in particular cryogenic fluids and method for producing and using same |
| 11/30/2011 | CN202055936U 一种推力终止机构及其密封结构 Termination of a lift mechanism and sealing structure |
| 11/30/2011 | CN202055935U Jet engine with parallel combustion chambers |
| 11/22/2011 | US8061659 Method for detecting complete draining of a propellant tank and for propellant management on board a satellite |
| 11/16/2011 | CN202039973U Test device for researching condensed-phase particle collision law |
| 11/15/2011 | US8056319 Combined cycle missile engine system |
| 11/08/2011 | US8051640 Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains |
| 11/02/2011 | EP2382224A1 Metal hydrazide materials |
| 11/02/2011 | EP1298389B8 Coaxial spray nozzle injector |
| 11/02/2011 | CN202023654U Particle engine |
| 11/02/2011 | CN101776026B Air inlet of air-breathing pulse detonation engine |
| 11/01/2011 | CA2480220C Method and apparatus for generating power by combustion of vaporized fuel |
| 10/20/2011 | DE102010010265B4 Verfahren zum Betrieb eines Raketentriebwerks und Raketentriebwerk A method of operating a rocket engine, and rocket engine |
| 10/19/2011 | EP2376763A2 Regeneratively cooled porous media jacket |
| 10/11/2011 | US8033111 Damping of vibration of a combustion chamber by resonators |
| 10/11/2011 | US8033095 Drive device on the basis of a gel-type propellant and method for conveying propellant |
| 10/11/2011 | US8033021 Method for fabricating structural propellants |
| 10/05/2011 | EP2372299A2 Device for burning off propellants or explosive substances |
| 10/05/2011 | EP2371987A2 Thermal barrier coating member, method for producing the same, thermal barrier coating material, gas turbine, and sintered body |
| 10/05/2011 | CN202001139U Stamping engine with pneumatic turbine |
| 10/05/2011 | CN102207043A Gaseous hydrogen/gaseous oxygen eddy current cooling thrust chamber injector |
| 09/28/2011 | EP2367722A1 Reusable module for a launcher |
| 09/21/2011 | EP2366626A1 Liquid propellant tank and vapor jet emitting device including same |
| 09/21/2011 | CN201982202U 夹层强迫冷却装置 Mezzanine forced cooling device |
| 09/21/2011 | CN102192046A Thruster of hydrogen-oxygen catalytic ignition mini rocket |
| 09/21/2011 | CN101768715B Method for preparing antioxidant coating of combustion liner of aeroengine |
| 09/15/2011 | US20110219743 Injector assembly for a rocket engine |
| 09/15/2011 | US20110219742 Supersonic combustor rocket nozzle |
| 09/15/2011 | DE102010011553A1 Rocket propulsion plant for use with hydrostatic loading in combustion process, has outer tank, two pistons and oxygen tank that is provided between both pistons, where latter piston is pressed in former piston |
| 09/14/2011 | EP2365203A2 Injector assembly for a rocket engine |
| 09/14/2011 | EP1960654B1 Hybrid rocket system |
| 09/14/2011 | CN201972812U 一种微型固体火箭发动机 A miniature solid rocket motor |
| 09/13/2011 | US8015795 Aircraft combination engines plural airflow conveyances system |
| 09/09/2011 | WO2011107090A2 Method for operating a rocket engine and rocket engine |
| 09/08/2011 | US20110214410 Propellant tank and vapor jet emitting device including same |
| 09/08/2011 | US20110214408 Liquid propellant tank and vapor jet emitting device including same |
| 09/08/2011 | DE102010010265A1 Verfahren zum Betrieb eines Raketentriebwerks und Raketentriebwerk A method of operating a rocket engine, and rocket engine |
| 09/07/2011 | CN201963418U 一种适用于凝胶推进剂的直流式喷注器 One for a DC-type gel propellant injectors |
| 09/07/2011 | CN102175041A Dividing wall type regenerative cooling air oxygen alcohol torch type igniter |
| 09/07/2011 | CN102174914A Test device for studying distribution of plume condensed-phase particles of spray pipe |
| 09/07/2011 | CN102174913A Pulse detonation engine with ejector and method for processing main detonation tube |
| 09/01/2011 | WO2011106446A1 Packaged propellant air-induced variable thrust rocket engine |
| 09/01/2011 | WO2011105897A2 Igniter for a rocket engine, method for ignition of a rocket engine |
| 09/01/2011 | WO2011104466A1 System for detecting and locating engine breakdowns and engine comprising such a system |
| 09/01/2011 | WO2011104465A2 Test bench for a reaction engine |
| 08/31/2011 | CN201953510U 大规模固体微推力器阵列点火装置 Massive array of solid micro-thruster ignition device |
| 08/31/2011 | CN102168631A Aluminum film baffle device and pulse solid engine applying same |
| 08/31/2011 | CN101768716B Aeroengine combustor liner with surface coated with oxidation resistant coating |
| 08/25/2011 | US20110203256 Motor |
| 08/25/2011 | US20110203253 Advanced fuel compositions from renewable sources, and related methods for making and using the fuel |
| 08/17/2011 | CN201934205U 一种小型推力室套筒 A small thrust chamber sleeve |
| 08/17/2011 | CN201934204U 一种液体火箭贮箱内盘旋式低温气体换热器 A liquid inside the tank rocket circling cryogenic gas heat exchanger |
| 08/17/2011 | CN102155332A Internal-heating nitrous oxide single component fuel gas generator |
| 08/16/2011 | US7997081 Gas delivery system |
| 08/16/2011 | US7997060 Rocket engine power cycle |
| 08/16/2011 | US7997059 Propulsion system |
| 08/11/2011 | WO2011096608A1 Rocket propulsion device and method for assembling rocket propulsion device |
| 08/11/2011 | US20110192137 Method for Manufacturing a Regeneratively Cooled Nozzle Extension of a Rocket Combustion Chamber and Nozzle Extension |
| 08/11/2011 | US20110192136 Solid-propellant motor |
| 08/11/2011 | DE102010007272A1 Verfahren zur Herstellung einer regenerativ gekühlten Düsenerweiterung einer Raketenbrennkammer und Düsenerweiterung A method for producing a regeneratively cooled rocket nozzle expansion of the combustion chamber and nozzle extension |
| 08/10/2011 | EP2354518A2 Method of manufacturing a regeneratively cooled divergent nozzle of a rocket combustion chamber and nozzle |
| 08/10/2011 | CN201925048U 多药室变推力推力器 Multidrug room variable thrust thruster |
| 08/10/2011 | CN102146858A Stamping engine for pneumatic turbine |
| 08/10/2011 | CN101776027B Air suction type liquid fuel pulse detonation engine |
| 08/10/2011 | CN101691849B Combustion-supporting method by activating oxygen molecules by using laser |
| 08/04/2011 | DE102010001485A1 Method for operating effusion or transpiration cooling system in e.g. heat shield of spacecraft, involves computing thickness of cooling member based on pressure difference of fluid before and after flowing through cooling member |
| 08/03/2011 | CN201916075U 一种固体火箭发动机全尺寸喷管热结构实验装置 A solid rocket motor nozzle thermal structure of the full-size experimental device |
| 07/27/2011 | CN201908744U Civil hail suppression and rainfall increment rocket engine |
| 07/27/2011 | CN102135049A Turbine powered electromechanical actuation system |
| 07/19/2011 | US7980057 Integral composite rocket motor dome/nozzle structure |
| 07/14/2011 | WO2011083252A1 Propulsion method and device comprising a liquid oxidant and a solid compound |
| 07/14/2011 | US20110167795 Nanothermite thrusters with a nanothermite propellant |
| 07/14/2011 | US20110167794 Multi-Functional Pulse-Divided Rocket |
| 07/14/2011 | US20110167793 Hybrid rocket using catalytic decomposition of oxidizer |
| 07/14/2011 | US20110167789 Rayleigh-taylor assisted combustion and combustors adapted to exploit rayleigh-taylor instability for increasing combustion rates therein |
| 07/13/2011 | EP2342444A2 Insensitive rocket motor |
| 07/13/2011 | CN201895653U Four rockets for automobile and novel braking system |
| 07/12/2011 | US7975468 Actuators for gun-fired projectiles and mortars |
| 07/12/2011 | US7975467 Apparatus for driving body with three-degree of freedom angular motion |
| 07/07/2011 | DE102010013425B3 Vorrichtung zum Abbrennen von Treibstoffen oder Explosivstoffen Apparatus for burning of fuels and explosives |
| 07/06/2011 | EP2340205A1 Container for receiving and storing liquids and viscous substances and method for the production thereof |