| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 07/25/2012 | CN101787939B Detonation chamber with jetting mechanism |
| 07/25/2012 | CN101782029B Device for testing flow characteristics of gas-gas nozzle |
| 07/24/2012 | US8225507 Stereolithographic rocket motor manufacturing method |
| 07/19/2012 | US20120180451 Optimal Feedback Heat Energy Internal Combustion Engine And Its Applications |
| 07/18/2012 | EP2476887A1 Rocket engine system for realizing high-speed response |
| 07/18/2012 | EP2475866A1 Rocket engine with extendable divergent |
| 07/18/2012 | CN102588112A Jet-flow efficient thermal power system |
| 07/11/2012 | CN202325900U 一种二次爆震的吸气式组合脉冲爆震发动机 A secondary knock aspirated combination of pulse detonation engine |
| 07/11/2012 | CN102562362A Oil supply device of high-frequency electromagnetic valve type pulse detonation engine |
| 07/05/2012 | US20120167552 Rocket engine system for realizing high-speed response |
| 07/04/2012 | EP2006560B1 Resin-made cage and bearing for cryogenic temperatures |
| 07/04/2012 | CN202300706U Eddy-eliminating anti-collapse device for fuel storage box |
| 07/04/2012 | CN102536516A Continuous flow thermodynamic pump |
| 07/04/2012 | CN102536413A Evaporative cooling device for combustion chamber |
| 07/04/2012 | CN101285433B Micro engine, mini-engine and method for manufacturing the micro engine |
| 06/27/2012 | CN102175041B Dividing wall type regenerative cooling air oxygen alcohol torch type igniter |
| 06/21/2012 | DE102010063452A1 Cooled system, which is exposed to hot gas flow, comprises wall and a cooling device integrated at least partially in the wall, which is made of a porous material in a partial region and is cooled by transpiration and/or effusion cooling |
| 06/20/2012 | EP2466100A2 Method and apparatus for variable exhaust nozzle exit area |
| 06/20/2012 | EP1608863B1 Unitized hybrid rocket system |
| 06/14/2012 | WO2012076797A1 Materials and parts that can withstand high temperatures in an oxidising medium, and method for manufacturing same |
| 06/14/2012 | US20120144799 Oxidizer Compound for Rocket Propulsion |
| 06/14/2012 | US20120144797 Rocket engine with cryogenic propellants |
| 06/14/2012 | CA2820795A1 Materials and parts that can withstand high temperatures in an oxidizing medium, and method for manufacturing same |
| 06/07/2012 | US20120137912 Controllable digital solid state cluster thrusters for rocket propulsion and gas generation |
| 06/07/2012 | US20120137653 Multi-stage rocket, deployable raceway harness assembly and methods for controlling stages thereof |
| 06/05/2012 | US8191351 Insensitive rocket motor |
| 05/31/2012 | WO2012069728A1 Rocket motor combustion chamber injection head |
| 05/31/2012 | WO2012069711A1 System for steering, about its axes of rotation, a moving body propelled by jet reaction, particularly a missile |
| 05/31/2012 | US20120132099 Nontoxic, noncorrosive phosphorus-based primer compositions and an ordnance element including the same |
| 05/31/2012 | US20120131903 Rocket engine with cryogenic propellants |
| 05/30/2012 | EP2458319A1 System for piloting a jet-propelled mobile about the axes of rotation thereof, in particular a missile |
| 05/30/2012 | CN102483013A Tiered porosity flashback suppressing elements for monopropellant or pre-mixed bipropellant systems |
| 05/24/2012 | WO2012068369A1 Propellant compositions and methods of making and using the same |
| 05/23/2012 | EP2454466A1 Rocket engine with cryogenic propellants |
| 05/23/2012 | EP2454465A1 Rocket engine with cryogenic propellants |
| 05/23/2012 | CN101956981B Gas-liquid component high chamber-pressure large-range variable working condition combustor |
| 05/22/2012 | US8181444 Solid propellant rocket motor with notched annular fuel |
| 05/22/2012 | CA2484262C A rocket engine nozzle that is steerable by means of a moving diverging portion on a cardan mount |
| 05/17/2012 | US20120117941 Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof |
| 05/17/2012 | US20120117936 Engine Using Hydrogen As A Fuel |
| 05/16/2012 | EP2452065A2 Condensation-proof barrier on regenerative circuit |
| 05/16/2012 | EP2452064A1 Tiered porosity flashback suppressing elements for monopropellant or pre-mixed bipropellant systems |
| 05/16/2012 | EP2451712A1 System and method for testing devices using powders |
| 05/16/2012 | DE102010043337A1 Fluid supplying device, particularly for engine of vehicle, particularly missile, for supplying two fluids to mixing chamber, has fluid supplying unit for supplying fluid to mixing chamber |
| 05/16/2012 | CN202220677U Center rocket type bi-modal ramjet engine with circular structure |
| 05/16/2012 | CN101761419B Baffled air-intake device of pulse detonation engine |
| 05/16/2012 | CN101749143B Distribution-type spouting mechanism of secondary propellant of pulse detonation engine |
| 05/10/2012 | WO2009061289A3 Dual-mode chemical-electric thrusters for spacecraft |
| 05/10/2012 | US20120110978 Absolute universal engine, one from ground to orbit |
| 05/03/2012 | WO2012055801A1 Propulsion unit and method for reducing a side load on a motor apparatus |
| 05/03/2012 | DE102010043336A1 Combustion chamber apparatus for rocket engine, has casing with sections of wall of combustion chamber and forming wall of nozzle extension, and injection head that extends to opposite end of nozzle extension |
| 05/02/2012 | CN102434318A Hydraulic equipment for debugging of engine jet pipe |
| 05/02/2012 | CN102434317A Aspirating type combined pulse detonation engine with secondary detonation |
| 05/02/2012 | CN102434316A Bipropellant micro chemical propulsion array device |
| 04/26/2012 | DE102010042890A1 Triebwerksvorrichtung für einen Flugkörper, Flugkörper, Prüfstand oder Startrampe für einen Flugkörper und Verfahren zur Reduzierung einer Seitenlast bei einer Triebwerksvorrichtung Engine device for a missile, missiles, test or launch pad for a missile and method for reducing a side load on an engine device |
| 04/25/2012 | CN101509439B 微流率液体工质供给与测量系统 Micro flow rate of liquid refrigerant supply and measurement systems |
| 04/24/2012 | US8161727 System providing braking in a gas turbine engine in the event of the turbine shaft breaking |
| 04/19/2012 | WO2012049150A1 Improved thermal insulation of rocket engines |
| 04/19/2012 | US20120090292 Combustion chamber comprising a condensation-proof barrier on a regenerative circuit |
| 04/19/2012 | CA2814308A1 Improved thermal insulation of rocket engines |
| 04/18/2012 | CN202194737U 一种小流量发动机分支压力平衡装置 Branch, a small flow of the engine pressure balancing means |
| 04/18/2012 | CN202194736U 一种大范围可调节离心式喷嘴 One kind of large-scale centrifugal adjustable nozzle |
| 04/12/2012 | WO2012045939A1 Thruster for a space launcher, and method for controlling propellant consumption |
| 04/11/2012 | EP2439395A2 Device for pressurising a lift tank |
| 04/11/2012 | EP2439394A1 Improved thermal insulation of rocket engines |
| 04/05/2012 | US20120079807 Method for producing solid composite aluminized propellants, and solid composite aluminized propellants |
| 04/05/2012 | DE102008049842B4 Einspritzelement für eine Raketenbrennkammer und Einspritzsystem Injection element for a rocket combustion chamber and injection system |
| 04/04/2012 | EP2435686A1 Part for attaching together the mobile portion of a deployable divergent nozzle of a propulsive unit and a mechanism for deploying said mobile portion |
| 04/04/2012 | CN102400815A 一种气氧/甲烷小推力发动机层板式喷注器 One kind of gaseous oxygen / methane thruster layer plate injector |
| 04/04/2012 | CN102400814A Solid-liquid hybrid rocket ramjet for test |
| 04/03/2012 | US8147206 Jet vane and method for manufacturing a jet vane |
| 03/28/2012 | CN102392757A Constant-temperature liquid solid lithium propellant transfer system and transfer method thereof |
| 03/27/2012 | US8141339 Injector assembly having multiple manifolds for propellant delivery |
| 03/22/2012 | US20120067023 Rocket engine and method for controlling combustion in the rocket engine itself |
| 03/21/2012 | CN101782466B Cooling water system design for test bed |
| 03/15/2012 | WO2012032273A1 Propulsion system for a flying machine, particularly for a missile |
| 03/15/2012 | US20120060468 Additive manufactured propulsion system |
| 03/15/2012 | US20120060464 Systems, methods and apparatus for propulsion |
| 03/14/2012 | CN102374071A Center rocket type bimodal ramjet with circular structure |
| 03/08/2012 | WO2011131493A3 Air breathing reaction propulsion engine |
| 03/07/2012 | CN102369207A Metal hydrazide materials |
| 03/06/2012 | US8127534 Pellet loaded attitude control rocket motor |
| 03/06/2012 | US8127527 Methods and systems for operating oxidizer systems |
| 03/06/2012 | US8127443 Method of fabricating a rocket engine nozzle using pressure brazing |
| 03/01/2012 | US20120047872 Hydrogen gas generator for jet engines |
| 02/29/2012 | EP2227629B1 Combustion chamber device |
| 02/28/2012 | US8122703 Coaxial ignition assembly |
| 02/23/2012 | WO2012022889A1 Combustion chamber provided with a tubular element |
| 02/23/2012 | US20120042629 Method And Plant For The Production Of A Casing For A Solid-Propellant Engine, And Casing Made According To Said Method |
| 02/22/2012 | CN1824940B 用于减小作用在火箭发动机的喷嘴上的不稳定横向载荷的装置和方法 Apparatus and method for reducing the role of unstable lateral load on the rocket engine nozzle |
| 02/16/2012 | US20120036831 Pellet-Loaded Multiple Impulse Rocket Motor |
| 02/16/2012 | US20120036829 System, Method and Apparatus for Lean Combustion with Plasma from an Electrical Arc |
| 02/16/2012 | DE102010034848A1 Dual fuel engine, particular position-control power unit, is based on cryogenic liquefied gases, where ignition device has catalytic converter in form of electrically heated cartridge made of ceramic or metallic material |
| 02/16/2012 | DE102010034581A1 Conveyor unit for supplying cryogenic liquid gases to engine, particularly attitude control power unit for spacecraft, has fluid-promoting piston pump for pumping of liquid gases, where connection is released by movement of piston |
| 02/16/2012 | DE102010034580A1 Thruster controller for depth control thruster used in spacecrafts operated with gaseous cryogenic fuels, has control device with control channels for gaseous fuel and oxidizer gas, respectively, and device to correct control of mass flow |
| 02/08/2012 | EP2414661A1 Deployable divergent nozzle for a propulsive unit |
| 02/03/2012 | DE202011103297U1 Einrichtung zur Entzündung einer Probe aus Raketenfeststoff Means for inflammation of a sample of solid rocket |
| 02/02/2012 | WO2011107090A3 Method for operating a rocket engine and rocket engine |
| 01/31/2012 | US8104264 Low minimum impulse bit propellant gas thruster |
| 01/26/2012 | WO2012011853A1 Cooling device for cooling combustion gases from recoilless anti-tank weapons |