| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 05/22/2013 | EP2594774A2 Reversible flow discharge orifice |
| 05/22/2013 | CN101915182B Solid-propellant rocket engine |
| 05/21/2013 | US8443582 Gas turbine engine with geared turbofan and oil thermal management system |
| 05/16/2013 | WO2013028027A3 Method for multistage control of flow control valve using dc motor |
| 05/16/2013 | US20130118147 Two-pulse rocket motor |
| 05/15/2013 | CN102072046B Gas-gas combustor support device for test |
| 05/10/2013 | WO2013033437A3 Thermal phase separation |
| 05/09/2013 | US20130112101 Bomb for deployment from an air vehicle |
| 05/09/2013 | US20130111874 Pulse Rocket Motor |
| 05/08/2013 | CN103090724A Solid-liquid power sounding rocket land launching sequential control system |
| 05/08/2013 | CN103089488A Adjustable cavitation venturi tube for high concentration hydrogen peroxide |
| 05/01/2013 | EP2587041A2 System and method for controlling an object traveling through exoatmospheric space |
| 05/01/2013 | EP2587040A2 Injector having Multiple Impingement Lengths |
| 05/01/2013 | CN202914201U Rocket tank discharge management device |
| 05/01/2013 | CN103075271A High-frequency conical spiral tube type pulse detonation engine |
| 05/01/2013 | CN103075270A High-pressure-intensity external pulse excitation device for T-shaped burner |
| 05/01/2013 | CN102062019B Laser propelled engine |
| 04/30/2013 | US8429894 Nano-grained aluminum alloy bellows |
| 04/25/2013 | WO2013057193A1 Device for expelling/containing liquids for a spacecraft tank |
| 04/25/2013 | US20130097995 System and method for controlling an object traveling through exoatmospheric space |
| 04/24/2013 | CN202900445U Boryl solid fuel propulsion device using plasma generator to ignite |
| 04/24/2013 | CN202900416U Jet-flow high-efficiency thermal power system |
| 04/24/2013 | CN103061919A Airtight testing device of solid-liquid rocket engine combustor |
| 04/24/2013 | CN102086022B Forming device of extruded type micro explosive column |
| 04/24/2013 | CN102052199B Test device for researching condensed phase particle collision discipline |
| 04/24/2013 | CN102052198B Experimental device for full-scale nozzle thermal structure of solid-propellant rocket engine |
| 04/24/2013 | CN101984240B Method and device for improving working frequency of pulse detonation rocket engine |
| 04/24/2013 | CN101907040B Nitrogen cold gas micro propulsion device adopting ring storage tank |
| 04/18/2013 | WO2013054027A1 Jet propulsion device and fuel supply method |
| 04/18/2013 | WO2013019876A3 Systems and methods for fabricating hybrid rocket motor fuel grains |
| 04/18/2013 | DE102011115812A1 System zur Lebensdauerüberwachung von Raketen System lifetime monitoring of missile |
| 04/17/2013 | EP2581594A2 System for lifespan monitoring of missiles |
| 04/17/2013 | CN102003303B Pulse detonation engine with secondary detonation |
| 04/17/2013 | CN101881238B Air-breathing pulse detonation engine and detonation method thereof |
| 04/10/2013 | CN103032204A Non-electric explosion propagation type redundancy control electric explosion isolating valve |
| 04/10/2013 | CN101915184B Double operating mode squeezing type conveying system and design method thereof |
| 04/09/2013 | US8413419 Regeneratively cooled porous media jacket |
| 04/04/2013 | WO2013048271A1 Propulsion system |
| 04/03/2013 | CN103016209A Cross three-dimensional forcing device of engine gimbal base |
| 04/03/2013 | CN103016208A Wheel-shaped charging device for hybrid rocket engine |
| 04/03/2013 | CN103016207A Propellant management device suitable for parallel balance emission |
| 04/03/2013 | CN102080608B Head test device of multifunctional solid-liquid hybrid rocket engine |
| 04/03/2013 | CN102042122B Portable measuring and controlling system for rocket engine ground tests |
| 04/03/2013 | CN101975124B Spark plug type electric ignition coaxial nozzle shearing device |
| 04/03/2013 | CN101956632B Air suction engine combustion chamber with turbulent flow post |
| 04/03/2013 | CN101907041B Propane liquid gas micro propulsion device suitable for micro-nano satellite |
| 04/03/2013 | CN101907039B Nitrogen cold air micro-propeller adopting three cylindrical propelling agent storage boxes |
| 04/02/2013 | US8407982 End burning type gas generator |
| 04/02/2013 | US8407981 Johnson Sexton cycle rocket engine |
| 03/28/2013 | WO2012177523A3 Constant volume combustion chamber |
| 03/28/2013 | WO2012156615A3 Power supply system and method for eliminating the pogo effect |
| 03/28/2013 | US20130074472 Injector having multiple impingement lengths |
| 03/27/2013 | CN202832855U Preposition jet flow igniter with function of low-pass filtering |
| 03/27/2013 | CN202832854U Combined type heat protective structure in the rear portion of a solid rocket engine combustion chamber |
| 03/27/2013 | CN102996284A Solid-liquid rocket engine annular igniter suitable for head jet of hydrogen peroxide |
| 03/27/2013 | CN102996283A Sealing assembly structure of glass material and metal for rocket engine |
| 03/27/2013 | CN102052197B Head injector of low-thrust engine for electric discharge and ignition by utilizing nozzle clearance |
| 03/27/2013 | CN102022225B Test device for hydrogen-rich/oxygen-rich gas multinozzle gas-gas injector |
| 03/27/2013 | CN101782030B Multiunit coaxial injector component for test and manufacturing method |
| 03/27/2013 | CN101737805B Low-cost inside diameter-variable combustion chamber and design and test method thereof |
| 03/27/2013 | CN101737538B Flow control valve device and design method for flow control type hole |
| 03/21/2013 | DE102011113539A1 Thermalisolation für Raketentriebwerke Thermal insulation for rocket engines |
| 03/21/2013 | DE102010011553B4 Raketenantriebsstufe mit hydrostatischer Aufladung im Abbrandverfahren Stage rocket engine with hydrostatic charge in Abbrandverfahren |
| 03/20/2013 | EP2570642A2 Thermal insulation for rocket engines |
| 03/20/2013 | CN101915181B Controller for initiating device |
| 03/20/2013 | CN101576026B Rocket engine nozzle system |
| 03/19/2013 | US8397486 Two-pulse rocket motor |
| 03/13/2013 | CN102971519A Packaged propellant air-induced variable thrust rocket engine |
| 03/07/2013 | WO2013033437A2 Thermal phase separation |
| 03/07/2013 | WO2011104465A3 Test bench for a reaction engine |
| 03/07/2013 | US20130055918 Energetic compositions including nitrate esters, methods of forming such energetic compositions, and articles including such energetic compositions |
| 03/07/2013 | DE102011112151A1 Compressed air jet pump for feeding fuel to liquid fuel rocket engine, has compressed air container that supplies compressed air into combustion chamber through two compressed air pipes |
| 03/06/2013 | CN102953866A Spiral-eliminating and anti-collapsing device of fuel storage box |
| 03/05/2013 | US8387361 Hybrid rocket system with moveable combustion control member |
| 02/28/2013 | WO2013028027A2 Method for multistage control of flow control valve using dc motor |
| 02/28/2013 | US20130047578 Unified chemical electric propulsion system |
| 02/27/2013 | CN102943720A Supporting mechanism of engine of large slenderness ratio rocket engine running support |
| 02/27/2013 | CN102943719A Turbulence device for postcombustion chamber of hybrid rocket engine |
| 02/21/2013 | WO2013024361A2 Improved rocket engine systems and devices |
| 02/21/2013 | US20130042596 Systems and Methods for Fabricating Hybrid Rocket Fuel Motor Fuel Grains |
| 02/21/2013 | US20130042594 Terrestrial power and propulsion from nuclear or renewable metal fuels with magnetohydrodynamics |
| 02/13/2013 | CN102926889A Method for using bipropellants efficiently |
| 02/12/2013 | CA2747821C Metal hydrazide materials |
| 02/11/2013 | DE202013100254U1 Brennkammer für Feststoffraketen Combustion chamber for solid rocket |
| 02/07/2013 | WO2013019898A1 Systems and methods for casting hybrid rocket motor fuel grains |
| 02/07/2013 | WO2013019876A2 Systems and methods for fabricating hybrid rocket motor fuel grains |
| 02/07/2013 | WO2013019855A1 Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor |
| 02/07/2013 | US20130031888 Systems, Methods, and Apparatus for Providing a Multi-Fuel Hybrid Rocket Motor |
| 02/06/2013 | CN102913341A Front jet igniter with low-pass filtering function |
| 01/29/2013 | US8359825 Microjet creation and control of shock waves |
| 01/24/2013 | US20130019587 Thruster devices and methods of making thruster devices for use with thrust vector control systems |
| 01/24/2013 | US20130019586 Propulsion method and device comprising a liquid oxidant and a solid compound |
| 01/17/2013 | US20130014491 Combustion gas supply control device |
| 01/17/2013 | US20130014487 Packaged propellant air-induced variable thrust rocket engine |
| 01/17/2013 | US20130014485 Apparatus for propulsion |
| 01/16/2013 | EP2546561A1 Damper of scissor duct flex joint |
| 01/16/2013 | CN1779225B Methods and systems for operating oxidizer systems |
| 01/16/2013 | CN102877985A Boron-based solid fuel propeller igniting through plasma generator |
| 01/10/2013 | WO2013004949A1 Injection element |
| 01/10/2013 | WO2013004942A1 Cryogenic fluid tank and its use |