| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 07/06/2011 | CN102116217A Self-boosting process predicating method for nitrous oxide storage box |
| 07/05/2011 | US7973269 Actuators for gun-fired projectiles and mortars |
| 06/30/2011 | DE102008029150B4 Gasgenerator Gas generator |
| 06/29/2011 | EP2339161A1 Rocket engine and method for controlling supply of fuel or comburent to the rocket engine |
| 06/29/2011 | CN102108916A Nitrous oxide monopropellant thruster and design method thereof |
| 06/28/2011 | US7966809 Single-piece hybrid rocket motor |
| 06/23/2011 | US20110146231 Tiered Porosity Flashback Suppressing Elements for Monopropellant or Pre-Mixed Bipropellant Systems |
| 06/23/2011 | US20110146228 Power extraction system |
| 06/23/2011 | CA2726212A1 Rocket engine and method for controlling combustion in the rocket engine itself |
| 06/22/2011 | EP2198144B1 Device for powering the pump of a rocket engine using an inertia wheel |
| 06/22/2011 | EP2150694B1 Cryotechnic space propulsion device and its control method |
| 06/22/2011 | CN201874699U Pneumatic unlocking bolt for separation test |
| 06/22/2011 | CN101539074B Rocket nozzle and control method for combustion of the exhaust gas flow in rocket engine |
| 06/15/2011 | EP1298389B1 Coaxial spray nozzle injector |
| 06/15/2011 | CN102099313A Method of producing a nozzle or a divergent nozzle element made of a composite |
| 06/15/2011 | CN102094728A Supplying device of small-flow and high-temperature gas propellant |
| 06/15/2011 | CN101644209B Straight single-hole fuel gas fluid control valve |
| 06/14/2011 | US7958823 Controllable digital solid state cluster thrusters for rocket propulsion and gas generation |
| 06/14/2011 | US7958719 Noncircular transient fluid fuel injector control channels in propellant injector combustion systems |
| 06/14/2011 | US7958718 Precision controlled variable thrust solid propellant rocket motor |
| 06/08/2011 | CN201858046U Pulse detonation engine realizing secondary detonation |
| 06/08/2011 | CN102086022A Forming device of extruded type micro explosive column |
| 06/07/2011 | US7956104 Centerport inhibitor for a solid propellant rocket motor, a solid propellant rocket motor including same, and a method of inhibiting a centerport of a solid propellant rocket motor |
| 06/01/2011 | CN102080608A Head test device of multifunctional solid-liquid hybrid rocket engine |
| 06/01/2011 | CN102080607A Motor for forest fire extinguishing bomb |
| 06/01/2011 | CN101240757B Heavy caliber asymmetric layout swinging hose |
| 05/30/2011 | CA2721530A1 Thrust modulation in a multiple combustor pulse detonation engine using cross-combustor detonation initiation |
| 05/25/2011 | CN201843703U Device for improving work efficiency of pulse knocking rocket engine |
| 05/25/2011 | CN201843702U Device for improving work frequency of pulse knocking engine |
| 05/25/2011 | CN201843701U Detonation tube with conical inner body for pulse detonation engine |
| 05/25/2011 | CN201843700U Igniter motor shell with integral structure |
| 05/25/2011 | CN102072049A Mixed-combustion working medium generator |
| 05/25/2011 | CN102072046A Gas-gas combustor support device for test |
| 05/24/2011 | US7946107 Mixture ratio stabilizer for liquid propellant rocket engine |
| 05/19/2011 | US20110113749 Apparatus, propulsive element and method for processing non-consolidated materials |
| 05/18/2011 | CN201835942U Fall-down test device |
| 05/18/2011 | CN102062020A Transparent combustion chamber with square interior passage |
| 05/18/2011 | CN102062019A Laser propelled engine |
| 05/17/2011 | US7945353 Adaptive control in the presence of input constraints |
| 05/12/2011 | WO2011055061A1 Flying air- or spacecraft provided with a propulsion system having an directable jet nozzle |
| 05/11/2011 | CN102056864A Process for producing a self-healing layer on a part made of a C/C composite |
| 05/11/2011 | CN102052199A Test device for researching condensed phase particle collision discipline |
| 05/11/2011 | CN102052198A Experimental device for full-scale nozzle thermal structure of solid-propellant rocket engine |
| 05/11/2011 | CN102052197A Head injector of low-thrust engine for electric discharge and ignition by utilizing nozzle clearance |
| 05/05/2011 | WO2011051611A1 Low-thickness thermostructural composite material part, and manufacture method |
| 05/05/2011 | DE102009013150B4 Bauteil zum Einsatz in Heißgasströmungen Component for use in streams of hot gas |
| 05/05/2011 | CA2778383A1 Low-thickness thermostructural composite material part, and manufacture method |
| 05/04/2011 | EP2315734A1 Method of producing a nozzle or a divergent nozzle element made of a composite |
| 05/04/2011 | CN201818392U Swirl ramjet engine |
| 05/04/2011 | CN102042122A Portable measuring and controlling system for rocket engine ground tests |
| 04/27/2011 | EP2313635A1 Thruster comprising a plurality of rocket motors |
| 04/27/2011 | CN201810422U Air-breathing engine combustion chamber with spoilers |
| 04/26/2011 | US7930875 Jet-type steam engine |
| 04/21/2011 | US20110088368 Thermally-integrated fluid storage and pressurization system |
| 04/20/2011 | CN201802507U Supersonic-speed rotor engine |
| 04/20/2011 | CN201802506U Hydraulic device for debugging engine jet pipe |
| 04/20/2011 | CN102022225A Test unit for hydrogen-rich/ oxygen-rich gas multinozzle gas-gas injector |
| 04/20/2011 | CN102022224A Ignition system for large-scale solid micro-thruster array |
| 04/20/2011 | CN102022223A An eddy current ramjet engine |
| 04/14/2011 | US20110083418 Flying object |
| 04/12/2011 | US7921638 Bi-propellant rocket motor having controlled thermal management |
| 04/06/2011 | EP2304212A2 Solid-propellant rocket motor |
| 04/06/2011 | CN102003303A Pulse detonation engine with secondary detonation |
| 03/31/2011 | WO2011037597A1 A system and method of combustion for sustaining a continuous detonation wave with transient plasma |
| 03/23/2011 | CN201771630U High-reliability diaphragm breaking type igniter |
| 03/23/2011 | CN201771629U Flow regulator with automatic return device |
| 03/17/2011 | WO2011030719A1 Rocket engine system for realizing high-speed response |
| 03/17/2011 | WO2011030048A1 Rocket engine with extendable divergent |
| 03/17/2011 | WO2011004127A3 Combustion chamber comprising a condensation-proof barrier on a regenerative circuit |
| 03/16/2011 | EP2294034A2 Process for producing a self-healing layer on a part made of a c/c composite |
| 03/09/2011 | CN101984240A Method and device for improving working frequency of pulse detonation rocket engine |
| 03/09/2011 | CN101984239A Method and device for improving working frequency of pulse detonation engine |
| 03/08/2011 | US7900436 Gas-generator augmented expander cycle rocket engine |
| 03/08/2011 | US7900435 Micro-coaxial injector for rocket engine |
| 03/08/2011 | US7900434 Thermally-integrated fluid storage and pressurization system |
| 02/24/2011 | US20110042386 Pressure vessel for propellants, explosion preventing method of the same, and manufacturing method of the same |
| 02/24/2011 | US20110041475 Elastomer structures, rocket motors including elastomer structures and methods of forming structures from layered viscoelastic materials |
| 02/24/2011 | US20110041474 Method and system for detecting the ingestion of an object by an aircraft turbine engine during a mission |
| 02/23/2011 | CN101979862A Internal heating nitrous oxide monopropellant gas generator |
| 02/17/2011 | DE202009018138U1 Brennkammervorrichtung Combustion chamber device |
| 02/16/2011 | EP1529163B1 Rocket engine with swivelling nozzle |
| 02/16/2011 | CN101975125A Device for measuring linear burning rate of liquid propellant in high pressure environment |
| 02/16/2011 | CN101975124A Spark plug type electric ignition coaxial nozzle shearing device |
| 02/16/2011 | CN101975123A Knocking pipe with central cone of pulse knocking engine |
| 02/16/2011 | CN101539071B Propellant filling device of electric arc heating engine supplying pipeline |
| 02/15/2011 | US7886519 Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method |
| 02/09/2011 | EP2281114A2 Rocket motor with pellet and bulk solid propellants |
| 02/03/2011 | US20110023449 Insensitive Rocket Motor |
| 02/02/2011 | CN101963111A Sample machine on basis of principle of nitrous oxide mono-component thruster and use method thereof |
| 01/27/2011 | US20110017873 Device for powering the pump of a rocket engine using an inertia wheel |
| 01/26/2011 | CN101957159A New high-thrust rocket |
| 01/26/2011 | CN101956632A Air suction engine combustion chamber with turbulent flow post |
| 01/20/2011 | WO2011007108A1 Rocket engine with cryogenic propellants |
| 01/20/2011 | WO2011007107A1 Rocket engine with cryogenic propellants |
| 01/13/2011 | WO2011005885A1 Tiered porosity flashback suppressing elements for monopropellant or pre-mixed bipropellant systems |
| 01/13/2011 | WO2011004127A2 Condensation-proof barrier on regenerative circuit |
| 01/13/2011 | WO2011003868A1 System and method for testing devices using powders |
| 01/13/2011 | WO2010006724A3 Solid-propellant rocket motor |
| 01/13/2011 | US20110005195 Aluminum porous media |
| 01/13/2011 | US20110005193 Method and apparatus for simplified thrust chamber configurations |