Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
01/2013
01/10/2013WO2013004259A1 Device for burning off propellants or explosive substances
01/10/2013WO2013004073A1 Carrier rocket thruster device
01/09/2013CN102863724A Halogen-free non-phosphorus poly-n-butyl methacrylate coating material used for propellant casting and coating and preparation method for coating material
01/09/2013CN102863723A Organosilicone resin composition serving as propulsive agent to wrap transition layer and steeping wrapping layer and preparation method thereof
01/08/2013US8347602 Liquid propellant rocket engine with a propulsion chamber shutter
01/08/2013CA2424697C A high temperature heat exchanger structure
01/03/2013WO2013001267A1 A bomb for deployment from an air vehicle
01/02/2013EP2539786A1 System for detecting and locating engine breakdowns and engine comprising such a system
01/02/2013EP2539571A2 Test bench for a reaction engine
01/02/2013EP2539570A2 Igniter for a rocket engine, method for ignition of a rocket engine
01/02/2013EP2539569A1 Packaged propellant air-induced variable thrust rocket engine
01/02/2013CN102852669A Modularized reusable multiunit circle-to-square compression ratio plug nozzle testing device
12/2012
12/26/2012CN1646450B Protection against oxidation of parts made of composite material
12/25/2012US8336287 Solid propellant rocket motor having self-extinguishing propellant grain and systems therefrom
12/20/2012WO2012172238A1 Cryogenic propulsion assembly and method of supplying a tank of such an assembly
12/20/2012US20120317956 Constant Volume Combustion Chamber
12/19/2012CN102828851A Cold flow test device for scaling linear plug type spray pipe carrier
12/18/2012USRE43867 Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the same
12/13/2012US20120311993 Multi-pulse rocket motor and pulse unit thereof
12/12/2012CN202596924U Sectioned long exhaust nozzle structure for solid rocket engine
12/12/2012CN202596923U Airborne solid rocket engine casing
12/12/2012CN102817745A Low-cost and simple unit round-to-square plug nozzle test device
12/12/2012CN102817744A Six-unit tile-shaped plug nozzle cold flow test device
12/06/2012US20120304620 Catalyst, gas generator, and thruster with improved thermal capability and corrosion resistance
12/05/2012EP2529986A2 Device for thrust generation
12/05/2012CN202578944U Back pressure reducing device for aspirating pulse knock air inlet channel
12/05/2012CN202578943U Jet ignition device for pulse detonation engine
11/2012
11/29/2012WO2012160297A1 System for reducing the dynamics of the mobile segment of a deployable rocket motor nozzle
11/22/2012WO2012156615A2 Power supply system and method for eliminating the pogo effect
11/22/2012WO2012156596A1 Continuous detonation wave engine and aircraft provided with such an engine
11/21/2012EP2525071A1 Continuous detonation wave engine and aircraft provided with such an engine
11/21/2012CN101400910B Resin-made cage and bearing
11/20/2012US8312705 Propellant gas control valve
11/15/2012US20120285016 Stereolithographic Rocket Motor Manufacturing Method
11/08/2012US20120279197 Nitrous oxide flame barrier
11/08/2012US20120279196 Microfluidic flame barrier
11/07/2012CN102767446A Rocket-mounted control circuit for solid/liquid power sounding rocket
10/2012
10/31/2012EP2516324A1 Propulsion method and device comprising a liquid oxidant and a solid compound
10/31/2012CN101776029B Combustion pursuing device
10/25/2012US20120269633 Closed gas generator and micro power unit including the same
10/24/2012CN202500675U High-pressure-resistant starting box based on non-metallic capsule
10/24/2012CN102748161A Particle engine
10/23/2012US8291691 Multi-functional pulse-divided rocket
10/16/2012USRE43731 Integrated air inlet system for multi-propulsion aircraft engines
10/09/2012US8281599 Device for damping the lateral forces due to jet separation acting on a rocket engine nozzle
10/09/2012US8281568 Cartridge-loaded rocket motor with castellated grain segments
10/09/2012US8281567 Deployable rocket engine in a combination jet and rocket engine
10/04/2012WO2012133041A1 Aircraft/spacecraft fluid cooling system and aircraft/spacecraft fluid cooling device
10/04/2012US20120247082 Clean up - rocket
10/03/2012CN102712546A Low-thickness thermostructural composite material part, and manufacture method
10/03/2012CN102705108A Periodic alternating current drive low-temperature plasma ignition method and system
10/02/2012US8276361 Thermal protection system and related methods
09/2012
09/26/2012EP2503135A2 Dual-pulse and multi-pulse thrust generators
09/26/2012CN202451299U Ignition circuit with redundant design
09/26/2012CN102691592A Demisable fuel supply system
09/25/2012CA2633097C Hybrid rocket system
09/20/2012US20120234196 Viscous Liquid Monopropellant
09/20/2012US20120233979 Rocket multi-nozzle grid assembly and methods for maintaining pressure and thrust profiles with the same
09/19/2012CN202441474U Evaporation cooling device for combustion chamber
09/19/2012CN101806261B Method and device for measuring pneumatic thrust indirectly
09/13/2012WO2012120230A1 Injector for mixing two propellants comprising at least one injection element with a tricoaxial structure
09/13/2012US20120227374 Integrated vehicle fluids
09/12/2012CN202431396U Die for pouring propulsive agent test piece
09/12/2012CN102658066A Catalytic decomposition low-concentration hydrogen peroxide reactor, combustion chamber and application thereof
09/07/2012WO2012118536A1 Rocket nozzle assembly
09/07/2012WO2012116398A1 Engine for use in an aerial vehicle
09/07/2012CA2828968A1 Rocket nozzle assembly
09/06/2012DE102012101682A1 Injector of injection head for combustion chamber of rocket engine, has combustion chamber into which pressurized fuel mixed with other fuel is injected through downstream end of spacer
09/05/2012EP2493832A1 Low-thickness thermostructural composite material part, and manufacture method
09/05/2012CN101782028B Hydrogen-oxygen fuel-rich precombustion chamber for full flow staged combustion cycle engine
08/2012
08/29/2012CN102650245A Miniature solid rocket engine
08/29/2012CN101858278B Multi-tube detonation lateral wave ignition device
08/23/2012WO2012112688A1 Rocket engine with augmented expander cycle
08/23/2012WO2012112209A1 Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
08/22/2012EP2489866A2 Rocket engine with an extendible nozzle
08/22/2012CN202391600U Deflected rear head structure of integrated solid rocket engine housing
08/22/2012CN202391599U Front end enclosure structure of solid rocket engine shell
08/22/2012CN102648343A Rocket engine system for realizing high-speed response
08/21/2012US8245496 Control and/or drive device for a flying body
08/16/2012US20120204535 Augmented expander cycle
08/16/2012DE102011011220A1 Raketentriebwerk mit einer ausfahrbaren Düsenerweiterung Rocket engine with an extendable nozzle expansion
08/15/2012CN202384544U Civilian solid rocket motor nozzle sealing device
08/15/2012CN102639853A Rocket engine with extendable divergent
08/15/2012CN102635464A Double-unit symmetric distribution linear plug nozzle cold-flow tester
08/15/2012CN102635463A Cold-flow test device for one-unit linear plug spray pipe
08/09/2012US20120198818 Augmentation of a monopropellant propulsion system
08/09/2012US20120198814 Use of hot gases and devices
08/09/2012US20120198813 Thrust chamber and rocket engine system
08/08/2012EP2484653A2 Fiber-reinforced article and method of it's making
08/08/2012EP1718857B1 Integrated air inlet system for multi-propulsion aircraft engines
08/02/2012DE102011000383A1 Thruster device for driving e.g. spacecraft, has walls porously formed in injection area, which forms injector for injecting fuel into thrust chamber unit space, so that required fuel is injected during operation of device
08/01/2012EP2480771A1 A system and method of combustion for sustaining a continuous detonation wave with transient plasma
08/01/2012CN202360245U Simplified combined nozzle structure of engine
08/01/2012CN202360244U Gauge for detecting conical fit clearances between rocket motor nozzle and inner end of throat liner
08/01/2012CN202360243U Thermal protection structure of back joint of solid-propellant rocket engine
08/01/2012CN102619644A Structure for reducing back pressure of air-breathing type pulse detonation air inlet passage
08/01/2012CN102619643A Jet ignition device of pulse detonation engine
07/2012
07/26/2012WO2012098315A1 Device for controlling the passage of a gas jet in a nozzle of an aircraft, and aircraft comprising such devices
07/25/2012EP2479386A1 Device for controlling the passing of a gas jet in a jet nozzle of a flying vehicle, and flying vehicle comprising such devices
07/25/2012EP1585896B1 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
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